AH-64 Apache

1.1 Purpose

This MFP is published to serve as a planning document for the fielding and sustainment of the AH-64D Apache Longbow Attack Helicopter, the Fire Control Radar (FCR), and the Longbow HELLFIRE Modular Missile System (LBHMMS). It applies to all Army elements responsible for planning and supporting this system before, during, and after deployment to the field. It provides information and guidance for FORSCOM organizations and support activities to ensure orderly fielding and support for the AH-64D and its associated systems.

1.2.1 Data Source

The information in this MFP was obtained from the following data sources:

    • Basis of Issue Plan Feeder Data (BOIPFD), 17 May 1994

    • Basis of Issue Plan (BOIP), DA approval 21 July 1995: AH-64D BOIP #H136AA, FCR BOIP #H101AA

    • AH-64D Apache Longbow Integrated Logistic Support Plan (ILSP), September 1994

    • New Equipment Training Plan (NETP), Draft, 10 September 1993; Final available electronically to all Major Commands. See Appendix F.

    • Operational Requirements Document (ORD) for the Modernized Apache, 1 April 1994

    • ORD for the Longbow Fire Control Radar (FCR), 1 April 1994

    • Qualitative and Quantitative Personnel Information (QQPRI), available electronically to Major Commands (MACOMs), including AMCOM and FORSCOM, with Total Army Visibility (TAV) access.

    • AH-64A Materiel Fielding Plan, Eighth US Army (EUSA), June 1994

    • Tables of Organization and Equipment (TO&E) for AH-64A and
      AH-64D units. Tentative A-Edition TO&E are listed in Section 4.9.1.

    • Memorandum of Agreement (MOA), Subject: Processing of AH-64A Aircraft for Entry into the AH-64D Apache Longbow Program,
      signed into effect 16 Oct 97.

    • AH-64D Apache Longbow Personnel Support Plan, 25 June 1997.

    • Input from Integrated Product Team (IPT) for Fielding meetings through IPT 9, 20-22 Oct 97, at Killeen, TX.

    • Input provided following reviews of previous drafts of this MFP.

1.2.2 Data Limits

This MFP is a living document. Data presented is the best available at the time of publication and is subject to change as the Longbow program evolves or with changes to regulations or policy. Unscheduled MFP updates will be issued if or when requirements change significantly.

1.3 Agreements

The following agreements are or will be associated with this MFP:

    • Materiel Fielding Agreement (MFA), Appendix A.
    • Memorandum of Agreement (MOA) for transfer of AH-64A aircraft into the AH-64D program, Appendix B.
    • Mission Support Plans (MSPs), Appendix E.

1.3.1 Materiel Fielding Agreement (MFA)

The MFA is the major agreement between the user and the materiel developer and outlines the cooperation necessary for the best support possible for fielding of the AH-64D to FORSCOM. The signed MFA indicates that the signatories agree to the MFP in principle and will abide by its processes. Changes to the MFP or fielding process will be made only after review and acceptance by all parties, but will not necessitate re-staffing or signing a new MFA. The FORSCOM MFA is at Appendix A.

1.3.2 Memorandum of Agreement (MOA)

Coordination required for development and approval of the Memorandum of Agreement (MOA) for transfer of AH-64A aircraft into the AH-64D program. The final coordination meeting was in Washington, DC, 9-10 February 1995. US Army agencies represented included personnel from the Project Manager (PM), Apache Attack Helicopter (AAH); PM, Aviation Electronic Combat (AEC); Program Executive Officer (PEO) Aviation (AV); Aviation and Missile Command (AMCOM); the Office of the Deputy Chief of Staff for Operations and Plans (ODCSOPS); the Office of the Deputy Chief of Staff for Logistics (ODCSLOG); Armament and Chemical Acquisition and Logistics Activity (ACALA); Communications-Electronics Command (CECOM); Training and Doctrine Command (TRADOC); PEO Tactical Missiles; and FORSCOM. Representatives from each of the above organizations made changes to the MOA and agreed to its contents prior to release for signature. These same agencies reviewed the MOA, made changes, and placed a revised document into effect. The latest MOA was signed into effect 16 Oct 97.

1.3.2.1 AH-64A Induction and Staging Procedures

Per the MOA, selected units will transfer AH-64A aircraft to the 21st Cavalry Brigade site at Ft. Hood, TX, for staging prior to induction into the re-manufacture process. These aircraft will then fall under the operational control of the 21st Cavalry Brigade commander until such time as they are required for rebuild. AMCOM will direct all aircraft movement to the 21st Cavalry Brigade via message. Aircraft Survivability Equipment (ASE) turn-in will be per the MOA. M272 launchers will be turned in as directed by the AGMS Project Office per the Induction MOA.

1.3.3 Mission Support Plan (MSP).

The purpose of the MSP is to define the planned use, maintenance, and supply support structure for the planned fielding according to the latest distribution schedule. FORSCOM MSPs are at Appendix E.

 

 

1.4 Fielding and Logistic Support Concept

Because the Longbow fielding effort is primarily transition from the AH-64A to AH-64D, the program is considered one of modification; therefore it does not require issue of complete unit sets of equipment as the transition from the AH-1 Cobra to the AH-64A Apache did. The following fielding and support concepts will be implemented:

  • Longbow Support Package (LSP)
  • Interim Contractor Support (ICS)
  • Life-Cycle Contractor Support (LCCS).

The LSP will be formally handed off to the unit. The unit is provided all unique (AH-64D and FCR) PGSE, TMDE, STTE, and any special mission kits required as part of the LSP. All AH-64D- and FCR-unique spare/repair parts will be provided through a network of contractor operated supply windows and not issued to units. (See Section 3.3.2) Units will receive LBHMMS support items listed in Appendix R. Publications will be provided in accordance with Section 1.4.1.2.

1.4.1 Fielding

The Apache Longbow and LBHMMS integrated fielding and training concept is as follows:

  1. Units stand down, turning in all AH-64A aircraft and AH-64A-unique support equipment, repair parts, and other items as directed by their Major Command (lists in this MFP are references that highlight equipment no longer required to support the AH-64D and its associated systems). Units retain all A/D-common repair parts, training missiles, dummy missiles, and launcher shoe alignment fixtures. Designated unit personnel proceed from their home station to Boeing in Mesa, AZ (Boeing-Mesa); the US Army Aviation Logistics School (USAALS) at Ft. Eustis, VA; or the US Army Aviation Center (USAAVNC) at Ft. Rucker, AL, for individual training. Receiving unit headquarters will designate a home station detachment to receive the LSP. Personnel will proceed as directed to the 21st Cavalry Brigade at Ft. Hood, TX, for single station collective unit training and/or unit evaluations.

  2. Units receive AH-64D aircraft in battalion sets at the 21st Cavalry Brigade. Units will use their aircraft during collective training. The 21st Cavalry Brigade will have an A/D-common PLL package in range, depth, and quantity sufficient to maintain and sustain the Apache Longbow during collective training to preclude units from having to ship their A/D-common PLL to Ft. Hood. Longbow-unique PGSE and Missile System PLL/ASL items are to be fielded at the units’ home stations. This is the equipment found in the LSP. An identical set of equipment found in the LSP will be issued to and retained by the 21st Cavalry Brigade for use during collective unit training. Boeing-Mesa Interim Contractor Support (ICS) Technicians and LBL Contract Field Service Representatives (CFSRs) will join their assigned unit at its home station after collective training and completion of the battalion/squadron’s evaluation. Boeing ICS Technicians will be in place for the duration of applicable contracts. CFSRs will be on site for twelve months following the unit’s return to its home station upon completion of training with the 21st Cavalry Brigade standards. Further contractual agreements may extend or limit CFSR assignments.

  3. An Apache Longbow MFT Office is planned to be established at Ft. Hood, TX. This MFT will include a Commander; an experienced Apache Maintenance Test Pilot; and two senior NCOs with experience in logistics, supply, and operation of the Electronic Equipment Test Facility (EETF) as a minimum. Contractors’ representatives may work from this office.

  4. Following collective training with the 21st Cavalry Brigade, units return to home station with their aircraft and LBHLs, which will also be fielded at Ft. Hood.

  5. Unit home station detachments receive AH-64D and LBHMMS unique PGSE and LBHMMS ASL items at the unit’s home station approximately 30 days prior to aircraft home station deployment. Boeing-Mesa airframe and/or Longbow Limited (LBL) FCR contractor supply window managers will be on site and establish ICS windows prior to arrival of the aircraft.

  6. Unless otherwise directed by FORSCOM, AH-64A- and prior-generation HELLFIRE-unique PGSE, PLL, and ASL items will be cross-leveled at installations having units retaining these systems, or turned in via normal supply channels following departure of the last AH-64As from that station. Funding credits for turn-ins will be at MACOM discretion.

Note: The 21st Cavalry Brigade will have access to a full unit set of AH-64A/D common, AH-64D unique, and LBHMMS unique support equipment and repair parts; therefore, there is no need to consolidate or transport this equipment from or return it to the unit’s home station. Units will use the 21st Cavalry Brigade’s support equipment during training periods with the 21st Cavalry Brigade.

The key idea expressed in the MOA (Appendix B) is that every AH-64A battalion slated to receive the AH-64D will stand down, convert its equipment, and then stand up with the remanufactured aircraft and launcher and unique support equipment found in the LSP. Neither the AH-64D aircraft nor the Longbow HELLFIRE missile launcher will be new. The systems are re-manufactured. Serviceable components will remain with a particular airframe whenever possible. The MOA outlines the actions necessary for turn in of AH-64A aircraft and associated equipment to the re-manufacture program.

1.4.1.1 LSP Process

Under the LSP process, the AAH PMO and AGMS PMO will provide the Longbow peculiar initial support items to include PGSE, LBHMMS ASL, and other support materiel as required. The AAH PMO, AGMS PMO, and AMCOM Materiel Fielding personnel will effect the handoff of the LSP to the using unit at the 21st Cavalry Brigade and its home station. The LSP hand off at the unit’s home station will require at a minimum 8000 cu ft of space for receipt and inventory. Each unit will provide the AAH PMO a "Ship To:" address and point of contact for home station LSP handoff not later than 90 days prior to unit’s aircraft arriving at home station. The LBHMMS utilizes AVUM and AVIM level organic supply support and ICS for Depot level supply support.

1.4.1.2 Starter Publications

The fielding command will provide TM 1 1520-251-10, Operator’s Manual; TM 1-1520-251-CL, Operator’s Checklist; TM 1-1520-251-MTF, Maintenance Test Flight Manual; and AH-64 IETM described in paragraph 4.7.1. The LBHMMS Test Program Set manual will be provided in hard copy form with the LBHMMS TPS. All other required manuals listed in Section 4.7 are obtainable through the normal distribution system.

1.4.2 AH-64D Apache Longbow, FCR, and LBHMMS Maintenance Concept

The AH-64D Apache Longbow, FCR, and LBHMMS maintenance concept follows the three level Army Aviation maintenance concept outlined in AR 750-1 and will follow the established procedures in place for the AH-64A and current generation HELLFIRE. Differences will exist in that AH-64D- and LBHMMS-unique items will require only Aviation Unit Maintenance (AVUM) and Depot level maintenance actions. Carryover systems or equipment may retain some Aviation Intermediate Maintenance (AVIM) level requirements.

2.1 Functional and Physical Configuration

The Longbow system represents a systematic effort to improve the war-fighting capabilities of the AH-64A helicopter. Table 2-1 illustrates the upgrades to the AH-64A which yield the AH-64D, and Table 2-2 shows the further improvements to the AH-64D with the application of the Longbow Fire Control Radar (FCR) Mission Kit and T700-GE-701C engines. These changes result in a more combat effective aircraft with increased survivability under current and projected battlefield conditions. An illustration of the Longbow system is provided in Figure 2-1.

 

 

 

 

 

 

 

 

 

 

 

Figure 2-1

Apache Longbow Weapons System

 

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AH-64A

Increased Automatic Mission Data Loading

Longbow HELLFIRE Modular Missile System (LBHMMS)

  • Modified HELLFIRE Launcher
  • Fire & Forget Missile
  • Inertial radar-aided precision guidance
  • Multiple-target engagement
  • Stationary & moving targets
  • Adverse weather capability

Digital Data Transfer

  • Tri-Service Compatible
  • Higher Data Rates
  • Simultaneous (4 Channel) Operation

Enhanced Navigation Systems

  • Deletes HARS
  • Incorporates:
  • New DOPPLER Velocity Rate Sensor
  • Ring Laser Gyros INU
  • Embedded GPS in the INU (EGI)

Greater Target Location Accuracy

Enhanced Target Servicing

Improved Attack Coordination

Improved Rapid Assumption

Improved Fire Distribution

Target Prediction

Minimum Engagement Exposure

MANPRINT Cockpit

Integrated Visual Representation of the Battlefield
  • Sensor Video
  • Navigation Information
  • Operational Graphics
  • Intelligence Information
  • Acquired Targets
  • Attack Coordination Graphics

Secure Cockpit Lighting

Improved Communication Interface

3-Axis Hover Hold

Composite Extended Forward Avionics Bays (EFABs)

Vapor Cycle Environmental Control System (ECS)

Increased Electrical Power

Dual Weapons Processors

Dual System Processors

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

AH-64D

Table 2-1

AH-64A Enhancements Yielding the AH-64D

 

 

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AH-64D

FCR

  • Multi-Mode (Air Target Mode [ATM]/Ground Target Mode [GTM]/Terrain Profile Mode [TPM])
  • Rapid, Multi-Target Acquisition
  • Detection
  • Classification
  • Engagement Prioritization
  • Radar Frequency Interferometer (RFI)
  • Extended Range Acquisition and Engagement in Poor Weather and Through Battlefield Obscurations
  • Wide Area Search In Minimum Time
  • Primary and Secondary Target Designations for Missiles
  • Multi-Target Engagement Capability
  • Rapidly-Moving Target Engagement Capability
  • Enhanced Battlefield Awareness
  • All Targets Displayed on Tactical Situation Display
  • Full 360º Coverage in Air Target Mode
  • Virtually Independent of Battlefield Conditions

T700-GE-701C Engines

  • Improved Performance over
    -701 Engines

TADS/FCR Integration

  • Independent, Simultaneous Operation by Either Crewmember
  • Link/Slave Operations to FCR or RFI

 

 

 

 

 

 

 

 

 

 

 

 

AH-64D

With FCR Mission Kit

 

Table 2-2

AH-64D Enhancements Yielding the AH-64D With FCR

 

2.1.1 AH-64D Apache Longbow Aircraft

The AH-64D Apache Longbow increases combat effectiveness over the AH-64A by providing a more flexible digital electronics architecture and integrating computer-based on-board Built-In Test Equipment (BITE), Automatic Test Equipment (ATE), and hard copy operator or Interactive Electronic Technical Manual (IETM) troubleshooting/maintenance manuals that will easily accommodate changes resulting from system growth. In addition, upgrades to electrical power and cooling systems and the expansion of the forward avionics bays to accommodate the installation of the FCR, and provide for future growth. Navigation system accuracy is improved through integration of a miniaturized integrated Embedded Global Positioning System (GPS)/Inertial Navigation Unit (INU) (EGI), and an improved DOPPLER Velocity Rate Sensor (DVRS).

2.1.1.1 MANPRINT Cockpit

Crew effectiveness is greatly enhanced with the Manpower and Personnel Integration (MANPRINT) cockpit. Visual presentations improve battlefield situation awareness, minimize required manual inputs and the need for mental interpretation, and simplify weapons employment.

2.1.1.2 Longbow Mission Kit Integration

The fully integrated AH-64D without Longbow Mission Kit incorporates greater ordnance capability and flexibility than the AH-64A by utilizing the family of Semi-Active Laser (SAL) missiles (including the HELLFIRE II) and Longbow HELLFIRE RF Missile. The AH-64D without Longbow Mission Kit can operate in harmony with the FCR-equipped AH-64D and can accept a target hand over and fire the Longbow missile with minimum exposure to hostile forces.

2.1.2 AH-64D With Longbow Mission Kit

The Longbow Mission Kit includes the items listed below. It operates in concert with the fire-and-forget RF missile and requires installation of two T700-GE-701C engines on the AH-64D attack helicopter. The FCR and RF missile, operating together as a weapon system on the AH-64D, are known as the Longbow weapon subsystem.

The following components make up the Longbow Mission Kit:

  1. Radar Frequency Interferometer (RFI).

  2. Fire Control Radar (FCR).

2.1.2.1 FCR and Radar Frequency (RF) Missiles

The FCR is a multi-mode Millimeter Wave (MMW) sensor integrated on the Apache Longbow with the antenna and transmitter located above the aircraft main rotor head. It enhances Longbow system capabilities by providing rapid automatic detection, classification, and prioritization of multiple ground and air targets. The radar provides this capability in adverse weather and under battlefield obscurants. The FCR has four modes: (1) the Air Targeting Mode (ATM) which detects, classifies, and prioritizes fixed and rotary wing threats; (2) the Ground Targeting Mode (GTM) which detects, classifies, and prioritizes ground and air targets; (3) the Terrain Profiling Mode (TPM) which provides obstacle detection and adverse weather pilotage aids to the Longbow crew; (4) and the Built in Test (BIT) Mode which monitors radar performance in flight and isolates electronic failures before and during maintenance.

The Longbow RF missile and the Longbow HELLFIRE Launcher (LBHL) are referred to as the LBHMMS. The system incorporates a fire-and-forget missile that accepts primary and/or secondary targeting information from the FCR and single targeting information from TADS or another aircraft to acquire and engage targets. Similar to the FCR, the RF missile provides the capability to engage threats in adverse weather and through battlefield obscurants. Two acquisition modes, lock-on-before-launch (LOBL) and lock-on-after-launch (LOAL), allow engagement of ground and rotary wing threats at extended ranges. In the LOBL mode, the missile will acquire and track moving or short range stationary targets prior to leaving the launch platform. In the LOAL mode, the missile will acquire long range stationary targets shortly after leaving the launch platform.

The combination of the integrated FCR, LBHMMS and the Apache aircraft enhances battlefield awareness by providing coverage of the battle area at extended ranges, by reducing operational dependence on weather and battlefield conditions, and by rapid display of detected targets. It further improves the Longbow system’s war fighting capability and survivability by providing rapid multi-target detection and engagement ability, navigational aids, and a fire-and-forget weapon delivery system.

2.1.2.2 TADS and FCR Integration

The addition of the Longbow FCR provides a second and completely independent target acquisition sensor which may be operated by either crew member or combined to provide a degree of multi-sensor synergy. When operated independently, the pilot could use the FCR to search for air targets in the ATM mode while the copilot/gunner (CPG) searches for ground targets using the Target Acquisition Designation Sight (TADS).

Using both TADS and the FCR together combines the unique advantage of each sight. The rapid search, detection, classification, and prioritization of targets by the Longbow FCR can then be quickly and positively identified by using the electro-optics of TADS. The center of view can be focused on the location of the highest priority target and the CPG, at the touch of a switch, can view either display. Alternately, the FCR centerline can be cued to the TADS so that a rapid and narrow search could be made of a suspected target area.

In addition to the separate displays mentioned above, a combined display or
C-scope is available to the CPG when utilizing both sights. This allows overlaying FCR located target symbols and radar map on the TADS video so that their relation to terrain features can be observed.

2.1.2.3 Radar Frequency Interferometer (RFI)

The AN/APR-48A RFI is an integral part of the Longbow FCR. It has sensitivity over an RF spectrum to detect threat emitters when a threat radar is in a search and acquisition mode and also when the threat emitter is "looking" directly at and tracking the Longbow system. The RF band has been extended over that which was developed for the OH-58D Kiowa Warrior at the low end of the RF spectrum to detect newly identified air defense threats. The RFI has a programmable threat emitter library to allow additional threat signatures to be stored and/or updated.

At its location above the main rotor head, the RFI detects and identifies threat emitters 360º around the aircraft. The azimuth of a threat emitter signal can be determined when operating in the fine direction finding (DF) mode by the RFI. In the remaining sector, the RFI determines the approximate threat emitter signal azimuth angle, and still provides excellent threat warning capability.

The RFI is fully integrated with the FCR, providing identification of FCR targets which are detected on the same azimuth as the RFI detections. The integrated weapons system provides the capability to cue the FCR to perform a "mini-search" at the RFI-measured angle of arrival. It can also cue the Target Acquisition and Designation System (TADS) and other weapons to that angle of arrival.

2.1.2.4 T700-GE-701C Engine

The sea level standard day intermediate rated power performance figures are 1800 SHP for the -701C and 1698 SHP for the –701 (1690 SHP at 20,250 rpm). In the high, hot environment (defined as 4000 ft. pressure altitude, 95º F), the -701C engine develops 1404 SHP versus 1301 SHP for the 701 engine. An AH-64D Apache Longbow with FCR Mission Kit can obtain a vertical rate of climb (VROC) that meets or exceeds the 450 fpm requirement. Fitting T700-GE-701C engines to the AH-64D Apache Longbow provides the additional power required to achieve these air vehicle performance requirements.

Note: The T700-GE-701-powered AH-64D will be configured to allow for future installation of the FCR and the T700-GE-701C engine. Ideally, all
AH-64D aircraft would be powered by the T700-GE-701C engine in the future, whether or not the FCR is installed. An effort is underway to determine if an appropriate upgrade to the -701 engine can be made which will improve its performance to match the -701C. This upgrade is presently unfunded.

2.1.3 Data Transfer Cartridge (DTC) Enhancement

The capability to use a data cartridge to automatically upload or download mission data has been expanded over the AH-64A to incorporate a more extensive data base that will accommodate output from the Aviation Mission Planning System (AMPS) under development. Data will include aircraft performance planning, flight planning, waypoints, targets, communications information, enemy positions, location of friendly forces, maintenance information, and other functions. This feature minimizes launch time and data input time during runup.

2.1.4 Maintenance Data Recorder (MDR)

Maintenance data was previously stored along with flight planning data in the Data Transfer Cartridge (DTC). Maintainers would not be able to gain access to maintenance data until it was downloaded to the AMPS and separated from classified data. In addition, the quantity of Maintenance Data was limited by the size of the DTC and the data was not crash protected. The MDR is a result of requiring a separate crash survivable storage device for maintenance and safety data. The MDR has one interface to the AH-64D aircraft 1553 Mux Bus as a Remote Terminal (RT) Line Replaceable Unit (LRU) and provides a means of recording and downloading maintenance and safety data while installed on the aircraft. MDR recorded data is to be downloaded at high speed to the SPORT via a 1553 interface, where Ground Analysis Software (GAS) resolves multiple fault ambiguity and launches the IETMs. The MDR has sufficient storage capability to record multiple flights’ worth of safety and maintenance data. Growth capability has been designed into the MDR for voice and other weapons systems data recording. Examples of Maintenance and Safety Parameters found on the MDR include the following:

  • Built-In Test (BIT) faults; warnings, cautions, and advisories (WCA); and system exceedances.
  • Flight data, including engine health indication test (HIT) results, flight hours, and landings.
  • Electronic logbook data, including rounds fired, equipment operating times, software versions, equipment installed, aircraft weight, aircraft center of gravity (CG), etc.
  • Aircraft drivetrain sensors such as oil and hydraulic temperatures and pressures, engine torque, Turbine Gas Temperature (TGT), Gas Generator Speed (Ng), Power Turbine Speed (Np), Rotor Speed (Nr), etc.

  • Information to aid ground analysis: equipment power applied, flight, environment, squat switch activation, MFD selection failures, etc.

  • Safety data (189 parameters defined by US Army Safety Center¾ flight

control positions, altitude, attitude, etc.).

2.1.5 Improved Data Modem (IDM)

The Improved Data Modem (IDM), which is a tri-service program, is well advanced over the Airborne Target Hand-over System (ATHS) currently in service. Interservice compatibility will allow very rapid exchange of information with virtually any aircraft, artillery battery, or command center in jam-proof "data-bursts". Four channel simultaneous data transmissions are easily accommodated. Combined with the high accuracy of the EGI, precise targeting and attack coordination information can be exchanged quickly while minimizing crew workload. The result is rapidly coordinated engagements.

2.1.6 LBHMMS

The LBHMMS, in conjunction with the FCR, will satisfy an operational requirement to provide increased lethality and survivability for the AH-64 Apache helicopter against current and future armored and air defense threats. The LBHMMS will also include a secondary capability against helicopters and will provide a true fire-and-forget capability. The system is comprised of two major items: the RF Missile and the M299 LBHL.

2.1.6.1 Longbow HELLFIRE Modular Missile (RF Missile)

The RF missile, part number 13403000, is a certified round of ammunition; therefore, it requires no field maintenance other than routine inspection and cleaning. It consists of a millimeter wave (MMW) radar seeker which contains supporting electronics, guidance and control (G&C) electronics, BIT, impact fusing sensors, and a precursor warhead integrated onto a HELLFIRE II missile bus. The HELLFIRE II bus is an item currently in production and procured from Lockheed-Martin. The missile will have a certification period of at least 10 years.

2.1.6.1.1 Environmental Cover Assembly (ECA)

Depending on environmental conditions, the ECA, part number 13403280, is used to protect the missile radome. It also prevents ice build-up during captive carry flight. Ice is removed by ejecting the ECA prior to target engagement. The ECA will be shipped in the missile shipping and storage container and installed on the missile at the AVUM level when needed.

2.1.6.1.2 Shipping and Storage Container

The container, part number 13403167, is a reusable, stackable metal container for transporting and storing the missile. It contains a replaceable desiccant unit used in conjunction with an internal humidity indicator to control moisture. The container is the stretched HELLFIRE missile container currently used for the Interim HELLFIRE Warhead (IHW) missile, modified to accept the RF missile and other HELLFIRE configurations.

2.1.6.2 Longbow HELLFIRE Launcher (LBHL)

The M299 LBHL, part number 13425104, is a modified M272 HELLFIRE launcher. It has a MIL-STD-1760A aircraft interface and can launch all configurations of the HELLFIRE missile. Modifications to the LBHL include development of the Launcher Electronics Assembly (LEA), which replaces the Electronics Command Signals Programmer (ECSP); redesigned upper and lower rail harnesses; elimination of the hoist adapter; and a reduced hardback and lower rail support weight. The LEA design incorporates self-contained, microprocessor-controlled BIT and a smaller number of LRMs. Weapon functions previously performed by the aircraft processor are now accomplished by the LEA. The LEA also includes software used to provide a simulated RF missile training capability. This function is called the Training Missile Emulator.

2.1.6.3 LBHMMS Component Physical Characteristics

Component

Missile

Missile Container

Launcher

Weight

108 lbs

90 lbs

145 lbs

Dimensions

69" Long x 7" Diameter

84.0" Long x 14.6" Wide x 15.6" High

59.8" Long x 20.4" Wide x 21.4" High

2.2.1 Operational Equipment

No separate equipment is required to operate the system. Peculiar Ground Support Equipment (PGSE), as described in Appendix P, is required to support the system and is discussed in Section 4.3.

The following list contains the AH-64A/D-common ASIOE to be retained:

LIN

AVUM

AVIM

Item Description

C20722

24

0

AN/ALQ-136(V)5

D03159

24

0

AN/APR-39A(V)1

D20060

24

0

Dispenser M130

J01917

24

0

AN/ALQ-144A(V)3

L45131

48

0

Launcher Rocket 2.75

M18594

68

2

Protective Mask CB M43A1

R82903

48

  

AN/PRC-112 Radio Set

T60156

12

1

Test Set M-91, M-130

T60338

0

1

Test Set ALM-178/ALQ-144

T72099

4

0

Test Set TS3614/ALQ-136

T72167

0

1

Test Set TS3615/ALQ-136

T77181

5

1

Test Set M-92, M-130

X22266

24

  

KIT-1C TSEC Computer

F63271

2

1

Boresight Kit (CBHK)

E01933

0

1

Electronic Equipment Test Facility

Z33570

73

2

Helmet, IHADSS

Z39433

12

1

Loader/Downloader

J97569

    

Z-AHQ/TSEC Interface Adapter

P44627

4

  

AGPU

S01441

24

  

KY-58/TSEC Secure Voice

Z24013

    

Diagnostic Troubleshooting Aid

Z84264

    

Test Set, TADS Turret Continuity Tester

G95741

21

0

Dummy Missile M34

G96350

7

0

SAL Training Missile M36
     

Shoe Alignment Fixture

Z79338

4

1

SM-674A Radar Signal Simulator

The following is a list of the AH-64D peculiar ASIOE to be issued:

LIN

AVUM

AVIM

ITEM DESCRIPTION

L67410

96

  

Launcher, LBHMMS (M299)

The following is a list of the AH-64A ASIOE which will be turned in:

LIN

AVUM

AVIM

ITEM DESCRIPTION

T59490

27

  

Metric Tool Set

G95863

    

Test Set, Guided Missile System AN/TSM-205

 

The unit shall return the AN/TSM-205 Test Set (NSN 4935-01-393-6351) , Initial Spares contained in cases PN# 301-247-1 & 301-247-2, related technical manuals, the AC power supply (NSN 6130-01-267-4467 to include the 400hz installed signal generator NSN 6625-00-148-1794), and the DC power supply (NSN 6130-01-383-6820). These assets will be shipped to:
 

PEO Tactical Missiles

AGMS Project Office

ATTN: SFAE-MSL-HD-S (Greg Bliss)

Redstone Arsenal, AL 35898-5610

The POC for turn in is Greg Bliss, AGMS PMO, (205) 842-0923 or DSN 788-0923. The following items are to be turned in as part of the AN/TSM-205 Test Set ("COEI" indicates that the item is a Component of the End Item):

NSN

PN

COEI
Qty

Spare
Qty

AMCOM
Description

AMDF
Description

4935-01-393-6351

13481200

    

AN/TSM-205 TS, GMS

  

5945-01-167-5956

MS27743-18

  

3

Relay, High Current 25 Amp

Relay, Electromagnet

5945-01-396-0626

MS83536/
10-024M

  

7

Relay, High Current 10 Amp

Relay, Electromagnet

4920-01-412-6723

13531340

1

1

Power Adapter

Adapter, Cable Break

4920-01-412-6725

13531338

1

1

Rail Adapter

Adapter, Cable Break

4920-01-412-6726

13531339

1

1

ECSP Adapter

Adapter, Cable Break

6150-01-412-6727

13531336

1

1

1553 Cable

Cable Assembly, Spec

7025-01-412-6732

13481188

  

1

Scanner Board

Multiplexer, Digital

7050-01-412-6733

13481191

  

1

A/D & D/A Converter

Converter, Digital T

5998-01-412-6734

13481186

  

1

1553 Interface Board

Electronic Component

6145-01-412-6735

13531330

1

1

Pylon Cable

Cable, Special Purpose

6625-01-412-6736

13481180

1

1

Remote Control Unit

Control, Test

5998-01-412-6737

13481181

  

1

Multi Function Board

Circuit Card Assembly

5998-01-412-6738

13481184

  

1

Indicator Board

Electronic Component

4935-01-412-6739

13481198

1

1

Self Test Adapter

Adapter, Test

5998-01-412-6741

13481190

  

1

CPU Board

Electronic Component

5998-01-412-6742

13481182

  

1

Power Board

Circuit Card Assembly

5998-01-412-6743

13481183

  

1

Communication Board

Electronic Component

7025-01-412-6744

13481193

  

1

Solid State Disk

Disk Drive Unit

6150-01-412-6745

13531332

1

1

Power Cable

Cable Assembly, Power

6145-01-412-6746

13531331

1

1

Umbilical Cable

Cable, Power, Electrical

6145-01-412-6747

13531334

1

1

Utility Cable

Cable, Special Purpose

4920-01-412-6748

13531337

1

1

Pylon Adapter

Adapter, Cable Break

6020-01-412-6749

13531333

1

1

Remote Cable

Cable Assembly, Fiber

5998-01-412-8859

13481185

  

1

PIO Board

Electronic Component

6625-01-412-8863

13481187

  

1

Digital Multimeter

Multimeter, Fiber Op

5998-01-414-4240

13481192

Depot

  

Passive Backplane

Backplane Assembly

6150-01-416-3179

13531321

  

1

1553 Harness

Cable, Assembly, Spec

4920-01-438-0440

13531337-1

1

  

Pylon Extender Cable

Adapter, Cable Break
 

301-240

LAR

  

Data Backup Unit

  
 

301-247-1

1

  

Carrying Case, CCA Spares

  
 

301-247-2

1

  

Carrying Case, Cable Spares

  
 

301-045

TMDE

  

Calibration Harness

  
 

13531326

    

OH-58D 1553 Adapter

  
 

The following items are ASIOE in the AVUM No. 1 Tool Set. Once a unit receives the NATS Aviation Footlockers, these items become ASIOE to the AVUM No. 2 and must be transferred prior to turning in the AVUM No. 1 shop sets.

NSN

LIN

DESCRIPTION

4310-00-075-6290

E70064

Compressor, Air: 5 cfm, 175 PSIG

4310-00-878-7969

E70817

Compressor, Air: 4 cfm, 3000 PSIG

4310-00-509-9790

E70886

Compressor, Air: 15 cfm 3500 PSIG

6115-00-914-4642

J49055

Generator Set: 7.5 kw 28v df

4520-00-446-7314

K24931

Heater Portable: 400,000 BTU

1730-00-734-9382

L10532

Jack, Hydraulic, Tripod: 3 Ton

1730-00-516-2018

L10559

Jack, Hydraulic, Tripod: 5 Ton

1730-00-912-3998

L10589

Jack, Hydraulic, Tripod: 12 Ton

1730-00-294-8883

M02504

Maintenance Platform: 3-7 Ft

1730-00-529-6235

M02751

Maintenance Platform: 4-12 Ft

6625-01-139-2512

M60449

Multimeter: AN/PSM-5

1730-00-540-2343

L09135

Jack, Acft Landing Gear: 5 Ton

1730-00-203-4697

L09340

Jack, Hydraulic, Hand: 10 Ton

2.2.2 Transport Equipment

Transportability equipment, part of the PGSE package, is required for shipment by air, sea, or land. Transportability equipment illustrations can be found with the PGSE descriptions at Appendix P.

2.2.2.1 Transport Procedures

Transportability procedures are contained in TM 1-1520-APACHE/LONGBOW. This TM prescribes methods and procedures for cleaning, preservation, packing, marking and loading the AH-64 helicopter. It is used for CONUS and OCONUS destinations.

2.2.2.2 Transport Preparation

Care, preservation, packing, packaging, and handling will be in accordance with TM 1-1520-APACHE/LONGBOW.

2.3 Operational Requirements Document (ORD) Information

Apache Longbow equipped battalions or squadrons will be organic to Army active and reserve component armored, mechanized, and air assault divisions; selected Armored Cavalry Regiments (ACRs); and other units at the Corps level. The system and its support package will be fielded down to company level. The AH-64D Apache Longbow will operate in all levels of conflict, providing a highly mobile and lethal attack capability against personnel, ground, and air targets. The AH-64D is capable of completing missions which are conducted during day and night; in Nuclear, Biological, and Chemical (NBC) conditions; adverse weather; and extreme environments.

The Longbow system meets the requirements of worldwide environment extremes for operation as described in AR 70-30. These extremes include the following parameters:

    1. Moderate turbulence.
    2. Temperatures from -18ºC to 49ºC without cold weather kits.
    3. Temperatures from -40ºC to 49ºC with appropriate cold weather kit installation.
    4. Light rain, blowing sand and dust, and snow.
    5. Fungus and sea salt fallout resistance.

Adaptation to these operational extremes allows the Longbow system to perform its assigned mission of providing direct aerial fires under day, night, and adverse weather conditions.

2.3.1 Utilization Rates and Maintainability

The Apache Longbow aircraft will achieve a 75 percent mission capable (MC) availability based on the planning figures for logistic support:

a. Peacetime: 174 flight hours per aircraft per year; 14.5 hours/mo.

b. Combat: 820 flight hours per aircraft per year.

2.4 Deployment Schedule

The following table lists the tentative deployment schedule for fielding the Apache Longbow and its associated equipment packages to FORSCOM line units. This list is subject to change, particularly the mix of aircraft with and without the Longbow FCR Mission Kit. Operational Readiness Float (ORF) aircraft will be located by the MACOM based on MACOM needs.

The FUE is 1-227 Aviation, 1st Cavalry Division, to be fielded in July 1998. The schedule that follows shows the projected dates for fielding as of the publishing date of this MFP. The full schedule, showing all AH-64D units, is at Appendix Q.

Unit

Location

Fielding Date

Acft w/FCR

Acft w/o FCR

1-227 AVN

Ft. Hood

Jul 98

9

15

2-101 AVN

Ft. Campbell

Jun 99

9

15

1-101 AVN

Ft. Campbell

Nov 00

9

15

1-3 AVN

Hunter AAF

Mar 01

9

15

3-101 AVN

Ft. Campbell

Mar 02

9

15

4-3 ACR

Ft. Carson

Jun 02

6

10

1-229 AVN

Ft. Bragg

Apr 03

9

15

3-229 AVN

Ft. Bragg

Feb 04

9

15

1-4 AVN

Ft. Hood

Apr 06

9

15

ORF-F (Float)

TBD

FY 99-FY 06

0

23

2.4.1 Support Maintenance Unit Fielding Information

Although Longbow-unique items require only AVUM and Depot level maintenance, AVIM units will continue to support Longbow units with supply and passback AVUM functions. Support equipment packages, if any, for dedicated AVIM units may be fielded up to thirty days in advance of the AVUMs organic to the attack helicopter battalions and air cavalry squadron listed above; however, under no circumstances will supporting AVIM packages be fielded after the supported AVUM. Under interim contractor support (ICS), no AH-64D-unique authorized stockage list (ASL) aircraft repair parts will be fielded to supporting AVIMs. Required ASL support will be provided through the ICS windows. Missile system repair parts will be issued to AVIMs as appropriate by the fielding MACOM. The table below lists the line units and their supporting AVIMs (subject to change). It does not list DoD civilian or contract support AVIMs.

 

 

Unit

Location

AVIM

  

1-227 AVN

Ft. Hood

615 DASB

  

2-101 AVN

Ft. Campbell

8-101 AVN

  

1-101 AVN

Ft. Campbell

8-101 AVN

  

1-3 AVN

Hunter AAF

603 DASB

  

3-101 AVN

Ft. Campbell

8-101 AVN

  

4-3 ACR

Ft. Carson

K/158 AVN

  

1-229 AVN

Ft. Bragg

I/159 AVN

  

3-229 AVN

Ft. Bragg

I/159 AVN

  

1-4 AVN

Ft. Hood

404 DASB

  

3.1.1 Fielding Command and Control (C2) Procedures

As the lead command, AMCOM is identified as the Fielding Command (FC) for purposes of AH-64D Apache Longbow fielding. Other organizations¾ including PEO AV, PEO Tactical Missiles, CECOM, and ACALA—are included in the total weapon system fielding effort. The MOA, signed into effect 16 Oct 97, (Appendix B) expresses the necessary command and control procedures for induction of AH-64A aircraft into the re-manufacture process. Additionally, the MOA outlines the turn-in procedures for M272 HELLFIRE missile launchers, Aircraft Survivability Equipment (ASE) suites, and Communication Security (COMSEC) equipment which require handling procedures different from the aircraft.

3.1.1.1 Fielding Command (FC) Responsibilities

The FC will:

  1. Produce total Longbow Support Package (LSP) in coordination with supporting commands and Program Managers (PMs).

  2. Provide all items included in the LSP.

  3. Establish and maintain records to provide visibility and formal accountability of the LSP until it is provided to the gaining units.

  4. Coordinate identification of Unit Materiel Fielding Point(s) (UMFP) and staging point(s) with the Defense Logistics Agency (DLA) for the system to be fielded if required. The UMFPs will be Ft. Hood and the unit’s home station unless otherwise advised.

  5. Coordinate with the US Army Communication Security Logistic Agency (USACSLA) to ensure successful fielding when COMSEC Materiel is being fielded in support of the EI/WS.

  6. Advise gaining command of the level of fill of the LSP prior to hand-off. Include identification of any shortages with estimated availability date, criticality, readiness impact, and work around.

  7. Provide shipping instructions provided by the PMs to staging point, storage depot(s), and/or contractors as appropriate.

  8. Coordinate for and conduct joint inventory of the LSP with the user.

  9. Prepare joint inventory documentation to include listing of shortage items still due the user at both the 21st Cavalry Brigade and home station.

  10. Determine any additional facility requirements.

  11. Provide interface with and guidance to prime contractors for execution of ICS. (Note: The window operations will require storage and office space providing physical security. The location for the window will be as designated by the appropriate installation or unit commander. This space must be negotiated at each installation well in advance of unit fielding and finalized not later than 60 days prior to establishment of the ICS Window.)

3.1.2 Gaining MACOM Command and Control (C2) Procedures

FORSCOM is defined as the Gaining Command (GC) for this MFP. The GC will receive the Longbow EI/WS using the following procedures.

3.1.2.1 Gaining Command (GC) Responsibilities

The GC’s role includes the following:

  1. Identifying the MTO&E or TDA for the unit receiving the AH-64D Apache and the support equipment. Ensuring facilities are available for contractor operated supply windows.

  2. Completing and updating the Mission Support Plan (MSP) as required and identifying the units and other support elements which will be involved in the fielding.

  3. Providing Points of Contact (POCs) responsible for coordination of requirements including providing sufficient personnel to participate in inventories, de-processing, and documentation at hand-off sites (POCs should include the DODAACs that will be used for each unit).

  4. Reviewing the MSL and related coordination documentation.

  5. Participation in all formal coordination meetings.

  6. Reviewing the support package requirements to determine any items which should not be furnished as a part of the materiel package.

  7. Identifying and verifying the UIC and the DODDAC of the gaining unit and the total supply system that supports the gaining unit.

  8. Coordinating the staging hand-off points with the FC and HQ, AMC.

  9. Ordering all maintenance, operations, and training related publications (initial issue is limited to maintenance publications).

  10. Ordering Class III, POL; Class V, Ammunition (including RF missiles); and Class VIII, Medical Supplies requirements. NOTE: RF missiles are ammunition for the LBHMMS, and will be pre-positioned at Anniston Army Depot (ANAD). Where authorized for rapid deployment force (RDF) units, missiles may be prepositioned at the ammunition supply point (ASP) serving the unit.

3.1.3 Shared Responsibilities

Both the FC and GC will share in the following actions.

3.1.3.1 Staging

Materiel responsibilities. The FC will provide all materiel requirements (except bulk POL, ammunition, and certain medical supplies) which are to be included in the LSP for the gaining unit. The FC will assist the GC by coordinating with the appropriate commodity managers to ensure that required bulk POL, ammunition and medical supplies will be available at home station handoff.

a. The gaining unit will receive a record of all shortages to the LSP as listed in the MFP, at hand off. The GC determines if shortages will cause excessive problems and agrees or not to field with known shortages.

b. The Longbow Support Package (LSP) will be inspected for damage and inventoried to make sure there are no shortages. When the FC and gaining unit verify that the requirements for the LSP have been met the package will be handed off at the unit’s home station. This should take place at least 30 days prior to the aircraft move from 21st Cavalry Brigade to the home station.

c. The aircraft will be flown from the manufacturer to Ft. Hood, TX. Four LBHLs per aircraft will be staged at Anniston Army Depot and issued to units undergoing collective training at the 21st Cavalry Brigade

d. The FC will obtain GC call forward concurrence prior to movement of materiel to the GC facility. Together, the FC and GC will verify hand-off schedules, locations, and support needs.

3.1.3.2 Joint Inventory

GC representatives will participate in a joint inventory of the LSP at the hand off site (unit home station or 21st Cavalry Brigade as designated). The date for this inventory will be determined by the FC and GC.

AMCOM, PEO Tactical Missiles, and PEO AV are responsible for establishing a handoff team that will include personnel required to conduct the joint inventory of the LSP. Team members and functions will be defined by the FC and that information passed to the GC at least ninety (90) days before hand off.

3.2 Logistic Assistance

The Logistic Assistance Program (LAP) for the Apache Longbow will comply with the requirements of AR 700-4 and follow the procedures already in place for the AH-64A. Initial logistics assistance will be provided to units in training by the PEO AV Apache Longbow Materiel Fielding Team. Following return of the AH-64D aircraft to the unit’s home station, logistic assistance will be provided in accordance with AR 700-4 by each AMC Major Subordinate Command (MSC). This assistance can be realized through the Logistics Assistance Representatives (LARs), Logistics Engineering Technical Services (LETS), Contractor Engineering Technical Services (CETS) and/or Contractor Field Service Representatives (CFSR) at each installation. Some CFSR/LETS/CETS representatives will serve more than one unit at a given location.

When used, CFSR support is limited to one year with PM funding. Continuing CFSR support beyond the one year regulatory limit will be IAW AR 700-4. Funding and waiver requirements beyond this limit will be the responsibility of the using MACOM. There will be one year of CFSR support for the LBHMMS.

3.2.1 USAMC LAP

The Commanding General, USAMC, provides, manages, and controls the USAMC worldwide LAP. AMC Logistic Support Activity (LOGSA) is the executive agent for administration of the LAP.

3.2.1.1 Worldwide Support

The applicable geographic logistic assistance office (LAO) or offices for this system are as follows:

    • LAO Europe
    • LAO Far East

    • LAO Continental United States (CONUS)

3.2.1.2 Regional Logistic Assistance Offices

This section deleted. These offices no longer exist.

3.2.1.3 Area Logistic Assistance Offices

The applicable area logistic assistance office (LAO) or offices for this system are as follows:

    • LAO Fort Bragg (1st COSCOM)
    • LAO Fort Campbell
    • LAO Fort Eustis
    • LAO Fort Rucker
    • LAO Fort Stewart
    • LAO Fort Hood (1st Cav Div, 4th Inf DIv, 13th COSCOM)
    • LAO Fort Knox
    • LAO Fort Carson

    • LAO Fort Irwin

    • LAO Fort Lewis

3.2.1.4 Fielding Command Readiness Directorate

The Logistics Operations Directorate from the FC will continually review the MFP and provide assistance as applicable.

3.2.2 Other MSC Logistic Assistance

Logistic assistance will be provided by ACALA and CECOM Logistics Assistance Representatives (LARs) in addition to those from the host command, AMCOM. Additional support may be provided by CFSR/LETS/CETS hired by MSCs other than AMCOM, the FC. The limitations and conditions of CFSR support as defined in Paragraph 3.2 apply. Current planning is for one window location for each fielding location—i.e., one window per installation.

Boeing maintains a 24-hour help line, 1-800-588-4224, when local LARs, Technical Representatives, or CFSRs are not available.

3.3.1 Organic Support

Organic depot support for the AH-64A/AH-64D common items will be performed at the depot designated by Industrial Operations Command (IOC). Future organic depot support for AH-64D Apache Longbow peculiar items will be determined at a later date prior to the closure of ICS. The depots currently designated by HQ IOC to support the AH-64D Apache Longbow are listed below:
 

Corpus Christi Army Depot (CCAD)

Letterkenny Army Depot (LEAD)

Anniston Army Depot (ANAD)

Tobyhanna Army Depot (TYAD)

3.3.2 Contractor Support

For AH-64D Apache Longbow unique items, the AH-64D prime contractors will provide depot level maintenance at their facilities and other maintenance as specifically directed by the AAH PMO to sustain operational availability of the AH-64D. The use of contractor depot maintenance is planned as an interim measure providing a cost effective program because of the low density of
AH-64Ds during the early years of production.

Boeing-Mesa and LBL are slated to establish a network of contractor-operated supply windows, each with a distinct Department of Defense Activity Address Code (DODAAC). These will serve as contractor/user interface points for Apache Longbow unique wholesale support. The optimum situation places each contractor’s window collocated with the supporting AVIM supply operation. It essentially performs the supply function for the peculiar items associated with the AH-64D aircraft and FCR.

The ICS windows have specific obligations to provide requisitioned parts in a timely fashion (within 24 hours in most cases). A key element of their ability to sustain this requirement will be timely turn-in of the failed parts for depot repair keeping the spares pipeline full at all times. To this end the GC must turn in failed assets to the contractor simultaneously with the request for a spare, but in no cases greater than 24 hours of the issue of the spare from the window.

3.3.2.1 ICS Deployment Plan

The ICS support augmentation provides AH-64D technical assistance and the "unique" repair parts necessary to support the Apache Longbow aircraft. When combined with the A/D common parts maintained by the unit, it provides a complete PLL/ASL supply package for the unit.

Each Apache Longbow unit will be staffed with a minimum of one civilian ICS supply support representative and two civilian ICS technical representatives (one Boeing and one LBL). This civilian augmentation is an integral part of the Apache Longbow unit and it is the responsibility of the unit to include this augmentation in all deployment planning activities IAW Draft DA Pam 715-XX, Contractor Support Guide.

Based on the mission and the anticipated OPTEMPO, the deploying unit, the AVIM, and the ICS personnel will determine the supply and support equipment requirements for A/D-common and D-unique assets.

3.3.3 Interim Contractor Support (ICS)

ICS includes AVIM- and depot-level supply (S) and maintenance (M) functions necessary to provide additional readiness capability not initially provided by organic organizations; ICS is limited by contract to the length of time specified in the table in Section 3.3.4. The individual systems and length of time each is covered by ICS are illustrated in the table in Section 3.3.4. ICS will continue during times of conflict involving the United States.

3.3.4 Life Cycle Contractor Support (LCCS)

LCCS is maintenance support provided by a contractor for the useable life cycle of training device systems. Its support level is reduced as systems are phased out or retired. Carryover AH-64A systems currently supported by LCCS, particularly the TADS/PNVS and RF missile, will continue to be supported by LCCS. New Longbow unique items may be converted to LCCS in the future.

The Longbow Training Device Suite described in paragraph 4.10.1.3 will be maintained by LCCS for the life of the system. After the first year of interim support provided by Boeing-Mesa for the Longbow Crew Trainer (LCT); Longbow Collective Training System (LCTS); Airframe, Engine, and Drivetrain Systems Trainer - L6 (AEDST-L6); and the Multiplex, Avionics, Visionics, Weapons Electrical Systems Trainer-L7 (MAVWEST-L7), STRICOM Logistics Readiness will assume the maintenance support of these training devices.
 

Organic

ICS/LCCS

Systems

AVUM

AVIM

Depot

AVUM

AVIM

Depot

AH-64A Carryover Systems

M/S

M/S

M/S

    

M/S*

AH-64D Unique Mechanical Systems

M/S

S

    

5 yrs**

5 yrs**

AH-64D Unique Electronic/Electrical Systems

M/S

S

    

5 yrs**

5 yrs**

FCR Mission Kit Electronic/Electrical Systems

M/S

S

    

5 yrs**

5 yrs**

AH-64D Unit-Level Training Equipment (Simulators)

      

M/S

M/S

M/S

LBHMMS Unique Items

M/S

S

      

M/S ***

HELLFIRE Carryover Items

M/S

M/S

M/S

      

* Life-Cycle Contractor Support (LCCS) for TADS/PNVS.

** ICS includes both maintenance (M) and supply (S) activities at the AVIM and depot levels during the current MY contract which expires Feb 02.

*** Minimum of 3 years ICS for the LBHL. LCCS for RF missile maintenance.

3.3.5 Contractor Support for Initial Fielding

Aircraft, FCR, and LBHMMS contractors may provide CFSRs/CETS and Window Managers to installations as AH-64D Apache Longbow aircraft are fielded per applicable contracts following the guidelines in AR 700-4 and Section 3.2. These individuals, in conjunction with the AMCOM LARs, will act as on-site subject matter experts to assist soldiers in properly maintaining the new equipment, enhancing training provided during individual MOS qualification classroom instruction.

 

3.4 Materiel Defects Correction

The report required when a deficiency in materiel or the logistics system is discovered is the Quality Deficiency Report (QDR), Standard Form (SF) 368. For Problems relating to the AH-64D, FCR components, or LBHMMS, address the QDR to:

Commander

US Army Aviation and Missile Command

ATTN: AMSAM-MMC-RE

Bldg 5309

Redstone Arsenal, AL 35898
 

Receiving units will make a thorough inspection of the AH-64D, FCR, and LBHMMS upon receipt and report deficiencies on SF 368. Receiving units will correct minor deficiencies. Instructions for completing the QDR are outlined in DA PAMs 738-750 and 738-751.

3.5.1 Coordination

The PM AAH established the Integrated Product Team (IPT) for fielding to ensure coordination between key agencies throughout the fielding process. Representatives from the AAH and AGMS PMOs, DCSOPS, DCSPER, DCSLOG, AMCOM, CECOM, ACALA, TRADOC, the gaining MACOM, Boeing, and LBL, as well as the 21st Cavalry Brigade and various FORSCOM units have participated in IPT meetings to raise issues and provide solutions to fielding issues.

The AAH PMO and AMCOM will ensure this coordination is complete prior to fielding. AAH PMO personnel will conduct pre-fielding visits prior to the first Apache Longbow being fielded at a given location. These visits are designed to identify and resolve fielding issues well in advance of the fielding effort.

Specific plans for visits will be determined and published closer to actual fielding dates.

3.5.2 Introductory Fielding Team Visits

A New Materiel Introductory Briefing Team (NMIBT) visit is normally made to the gaining unit prior to fielding the unit’s AH-64Ds. The NMIBT will present an executive level briefing on the functions, capabilities, support, and other characteristics of the Longbow weapon system to unit commanders and other key personnel. Final coordination prior to the first AH-64D’s arrival will be made by the NMIBT. The NMIBT chief will be the AH-64D Project Manager or his designated representative. A Doctrine and Tactics Training (DTT) Team will visit gaining units in conjunction with the NMIBT. TRADOC will form and brief the DTT. The timeline/checklist for each unit as found at Appendix G will indicate the NMIBT schedule.

 

4.1 Maintenance

a. The Apache Longbow maintenance plan follows standard Army Aviation three-level maintenance planning; however, all Longbow-unique items utilize only the AVUM and Depot levels, with ICS in place for Depot level maintenance activity. MOS 67R- and 68-series soldiers and/or equivalent civilian contractor personnel will maintain the AH-64D and FCR.

b. LBHMMS maintenance procedures are similar to the two level concept for the newly developed aircraft components. Common HELLFIRE/LBHMMS components will continue to be supported by three level maintenance. MOS 68X personnel will perform AVUM maintenance. AVUM tasks include the following for the respective components:
 

Missile:

Visual inspection

Cleaning

Spot painting

Environmental Cover removal/replacement

Evacuating unserviceable missiles to depot

Launcher:

Launcher BIT execution

Removal/replacement of launcher and LRMs

Depot maintenance will consist of complete repair of the LBHMMS and its associated components deemed economically repairable. Missile repair will be performed by a contractor technician. The following items will be shipped to the depot via normal supply channels: missile; shipping and storage container; ECA; launcher and components.

4.1.1 Maintenance Reporting Requirements

The general objective of aircraft readiness is to achieve 75% Mission Capable. Fielded AH-64D aircraft will be subject to the Army readiness reporting system governed by AR 220-1, Unit Status Reporting; AR 700-138, Army Logistics Readiness and Sustainability; and DA PAM 738-751, Functional Users Manual for the Army Maintenance Management System- Aviation (TAMMS-A). Because of the separate Line Item Numbers (LINs) for the FCR and aircraft, specific DA Form 1352 reporting procedures for FCR- and non-FCR-equipped aircraft will have to be developed and incorporated into appropriate regulations. Until changes are made to appropriate manuals, MACOMs and units will be advised on how to report Longbow aircraft and components during the NMIB. The LBHL and RF missile are reportable on DA Form 2408-9 per AR 710-3 and DA PAM 738-750. Various components may be reportable on DD Form 2410; however, the specific components requiring DD 2410 information are subject to change; therefore, units will be notified at a later date regarding specific DD 2410 requirements.

4.1.2 AH-64D Apache Longbow Maintenance Concept

The maintenance concept for the Longbow system is the three level Army Aviation Maintenance Concept as outlined in AR 750-1 with the following exceptions:

(a) Electronics equipment maintenance requiring the use of the Electronic Equipment Test Facility (EETF [OQ 290 (V)2/MSM]) will be accomplished at selected AVIMs.

(b) Longbow unique systems will utilize the two level maintenance concept, AVUM and depot. Refer to Section 3.3 for depot level support.

4.1.2.1 Phased Maintenance (PM) Inspections

The PM inspections are based on a schedule having 1000 flight hour cycles with 250-hour phases. TM 1-1520-APACHE/LONGBOW contains the Phased Maintenance Checklist for the AH-64D.

4.1.2.2 10 Hour/ 14 Day Inspections

The inspections prescribed by TM 1-1520-APACHE/LONGBOW will be performed at 10 flight hour or 14 day intervals by AVUM activities with assistance from AVIM activities when required.

4.1.2.3 Preflight Inspections

These inspections constitute flight readiness inspections and are performed by the flight crew in conjunction with normal flight operations. Refer to TM 1-1520-251-10 or TM 1-1520-251-CL for specific preflight inspection procedures.

4.1.2.4 AVIM Support

AVIM support for FORSCOM AH-64D units will be in accordance with the Mission Support Plans (MSPs) found at Appendix E. Supply Support Activities (SSAs) will remain in place at the AVIM level.

4.1.2.5 Depot Support

Depot support for AH-64A carryover items will continue to receive support as in the past. Newly created Longbow-unique items will receive support per the information contained in Section 3.3.

4.2.0 General Information

Warranty Claims Actions (WCA) will be submitted by the using unit IAW DA PAM 738-750. The using unit must submit both a WCA (DA Form 2407) and a Quality Deficiency Report (QDR) (SF-368). A copy of each form must accompany the repair part to the depot repair facility where the WCA will be validated. The local AMC LAO can assist in the submission of the WCA. The LAO is also the Warranty Control Office (WARCO).

4.2.1 AH-64D

All AH-64D-unique supplies, including spares, will be under warranty coverage for one year or 200 flight hours (whichever occurs first). The one-year calendar time begins on the date of DD250 delivery. Ordinary wear and tear and maintenance are not included under the warranty. See also Appendix I for warranty information excerpted from the contract. NOTE: The applicable contract is the only legal instrument for warranty implementation. Extracts at Appendix I are for reference only and are not legally binding.

4.2.2 FCR

Contractual agreements are not yet finalized. Proposed FCR warranties cover 12 months for performance, materiel and workmanship defects, and 12 months for manufacture and design defects.

4.2.2.1 RFI

Proposed RFI warranty is for 24 months after acceptance by the government. This period can be extended due to lengthy storage periods.

4.2.3 LBHMMS

Items covered by warranty are the LBHL, LBHMM, LBHMM container, and ECA. Warranty begins at DD 250 delivery date. The warranty period for all LRIP I items is 24 months. LRIP II warranty provides coverage for 72 months for the LBHMM, and 24 months for the LBHL, LBHMM container and ECA. Detailed warranty program information is identified in the Warranty Implementation and Management Plan (WIMP) for the Longbow HELLFIRE Modular Missile System. The WIMP is available through the AGMS Project Office, Logistics Division, (205) 876-3941 or DSN 746-3941. Refer to TB 9-1425-1475-20, Warranty Program For Longbow HELLFIRE Modular Missile System.

4.2.4 Training Devices

The Longbow Crew Trainer (LCT); Longbow Collective Training System (LCTS); Airframe, Engine, and Drivetrain Systems Trainer-L6 (AEDST-L6); and the Multiplex, Avionics, Visionics, Weapons Electrical Systems Trainer-L7 (MAVWEST-L7) will be maintained by LCCS for the life of the system as described in Section 3.3.4. After the first year of interim support, provided by Boeing-Mesa, STRICOM Logistics Readiness is expected to assume the maintenance support of the training devices. For the AEDST-L6 and MAVWEST-L7, the Army will provide repair parts from crash damaged aircraft or unserviceable items able to serve as training aids whenever possible to reduce cost.

4.3.0 Support Equipment and TMDE

Standard Army Aviation Ground Support Equipment (GSE) and new PGSE unique to the AH-64D Apache Longbow will be required to support this system. All general purpose and special purpose TMDE required to support the AH-64D Apache Longbow will be identified and coordinated with the U.S. Army Test, Measurement, and Diagnostic Equipment Activity (USATA) for supportability evaluation.

4.3.0.1 New Aviation Tool Set (NATS) Program Update

1. The program has been expanded to include a new Armament Repairer Tool Kit (B09, LIN W59034) and an Armament Repair Tool Set (Team Box, B10, LIN W59171). The B09 kit will be constructed similar to the other NATS kits and the B10 team box will look like an Aviation Foot Locker (AFL).

The basis of issue for the new armament tool kit is one per MOS 68X in support of AH-64D aircraft. The armament team box basis of issue is one per five mechanics or fraction thereof for MOS 68X AH-64D aircraft. This new armament tool kit and team box will replace the current Tool Kit Armament Basic, Tool Kit Armament Supplemental, and Tool Kit Armament Metric.

2. Fielding has been suspended while an issue with one of the tool suppliers is corrected. This issue has resulted in the replacement of all Wright Tool Co tools in the NATS program. There have also been some other design changes based upon input from the field. The results are a new foam insert for the general mechanics tool kit (GMTK, LIN W30949) and the powertrain tool kit (P/T TK, LIN W49238). The Aviation Footlocker (AFL) has also been redesigned.

Preliminary plans called for a retrofit program during 2nd-3rd Qtrs, FY98. This will replace foam inserts and specific tools in all GMTK and P/T TK kits previously fielded. There is no change to the authorizations, quantities, or NSN/LIN of these two kits as a result of this retrofit. The new armament tool kit and armament team box will be fielded to these units at the same time.

Wright tools in the Electrical (B06, LIN W36703), Sheet Metal (B02, LIN W30675), and Engine (B07, LIN W38073) Tool Kits will not be replaced during this retrofit. The AFL (B90, LIN T65997) and AVUM #2 (A92, LIN W60206) will also not be updated. These tools will be replaced through attrition.

3. New supply catalogs were published 31 Mar 97 for the B01, B02, B06, B07, B13, and A92. The current AFL SC is dated 22 May 96. Unfortunately, these SCs do not contain the NSNs for the tools that replaced the Wright tools. However, this data will be provided to the field during the retrofit process. Changes have been submitted for another round of SCs, but there are no immediate plans to republish these catalogs. New SCs are in development for the B09 and B10.

4. The SCIT warranty process is being reworked to better serve the soldiers in the field.

5. FORSCOM fielding is planned to resume in 4th Qtr. FY98. This will include both NATS and the armament kits.

4.3.1 Special Tools and Tool Sets

The Longbow configuration of the AH-64 deletes some AH-64A special tool sets. It modifies other AH-64A special tool sets by removing the AH-64A-unique items and inserting the AH-64D item; some new special tool sets are unique to the AH-64D. Many of the special tools and tool sets are common to the AH-64A and AH-64D.

4.3.1.1 AH-64A Special Tools and Tool Sets

The following special (peculiar) tools and kits are used only on the AH-64A-model Apache helicopters and are not needed by the gaining unit to support the D-model. Notify FORSCOM DCSLR, AFLG-FMMC-HT, of excess tools that cannot be cross-leveled locally.

ITEM

NSN

P/N

AVUM

AVIM

Air Data System Alignment Kit

4920-01-329-6825

  

1

1

Cal. Adapt., Rotor Blade De-ice

4920-01-357-2019

140034 (60168)

1

1

Armament Breakout Box

  

LEX-D-0040-001

1

1

Crane, Aircraft Mounted

1730-01-246-1351

7-262100002-603

1

1

Electrical Utility Breakout Box

  

LEX-D-0121-001

1

1

Electrical Flight Control Breakout Box

  

LEX-D-0161-001

1

1

Electrical Connector Breakout Box

  

LEX-D-0221-001

1

1

 

FLYAWAY KIT

1730-01-384-8885

7-262100004-611

    

Omni Directional Air Speed Sensor Cover

1730-01-083-4507

7-262120030

    

TOOL SET

        

Armament, Metric (B11)

5180-01-110-7629

LIN T59490

27

  

Electrical Repairman (B06)

5180-00-323-4876

LIN W36703

11

  

TRANSPORTABILITY KIT

        

Wing Stowing Kit

1740-01-220-8492

7-367310001

    

4.3.1.2 Modified AH-64A Special Tools and Tool Sets

The following special (peculiar) tools and kits are AH-64A items modified as required to allow them to support the AH-64D.

UNIT PROPERTY

ITEM

AH-64A

PART NO.

AH-64A

NSN

AH-64D

PART NO.

AVUM

AVIM

AVIM TOOL KIT

7-263100001-601

4920-01-182-8811

7-562100013-601

1*

1*

Leveling Kit

7-262110013-601

  

7-53100001-601

1*

1*

Bracket Assy., Blumb Bob

7-262120007

  

7-562120007-1

1**

1**

Target, Aircraft Leveling

7-262120003

  

7-262120003-3

1**

1**

Aviation Vibration Analyzer (AVA)

Rotor Track & Balance Kit

7-262100008-607

7-262100008-613

4920-01-245-6004

4920-01-328-8013

TBD

3*

4*

Bracket Assembly

29240100

  

7-511010030-1

**

**

GROUND SUPPORT KIT (AVUM)

7-262100011-605

4920-01-240-6743

7-262100011-607

2*

1*

Component Handling

Adapter

    

7-562107001-1

0

3**

Component Sling Set

7-262100005-607

1730-01-246-6781

7-262100005-609

1* (3***)

1* (1***)

DU/Torque Tube Sling

    

7-562108002

1** (3***)

1** (1***)

Sling Only

7-262100005-607

1730-01-246-6781

TBD

(3***)

(1***)

FCR Pins

    

7-562108004-601

3** (6***)

3** (3***)

* Quantity authorized by TOE

** Quanity added to kit

*** Increase recommendation based on Val/Ver. PMO to pursue recommendation. If approved and funded, PMO will back fill any units that did not receive the increased quantity as initial issue.

AIRCRAFT PROPERTY

ITEM

AH-64A

PART NO.

AH-64A

NSN

AH-64D

PART NO.

QTY per

Aircraft

Aux Fuel Kit (PART 1)

7-367100000-11

1680-01-297-4121

7-567100000-1

1

Hose Assembly

7-367100012-3

  

7-567100012-3

1

Hose Assembly

7-367100012-4

  

7-567100012-4

1

Hose Assembly

7-367100013-3

  

7-567100013-5

2

Hose Assembly

7-367100013-4

  

7-567100013-6

2

Hose Assembly

7-367100013-5

  

7-567100013-7

1

Hose Assembly

7-367100013-6

  

7-567100013-8

1

Cable Assembly

7-267100002-7

  

7-567100002-1

4
         

FLYAWAY KIT

7-262100004-611

1730-01-384-8885

7-562110004-601

  

ENCU Exhaust

Cover (Becomes a

cooling air inlet

cover on AH-64D)

7-262120018

1730-01-187-8504

7-262120018

1 per Acft

4.3.1.3 AH-64D Special Tools and Tool Sets

The following special (peculiar) tools and kits are AH-64D-unique items developed to support the AH-64D:

Unit Property

ITEM

AH-64D

PART NO.

AVUM

AVIM

Environmental Control

System (ECS) Kit

7-562104000

2*
(1**)

1* (1**)

ECS Servicing Cart

7-562104012-601

2*
(1**)

1* (1**)

ECS Tool Kit

7-562104013-601

2*
(1**)

1* (1**)

R134A Freon & Tank (43 lbs)

NSN: 6830-01-439-0614

2*
(1**)

1* (1**)

Wire Harness Adapter

Troubleshooting (WHAT)

Kit

7-562106000

2*

1*

Transportability Kit

      

Tiedown Extensions

7-567310002

2 per Acft*

  

Wing Stow Fixture

7-567310001

2 per Acft*

  

Horizontal Stab Stow

Fixture

7-567310003

1 per Acft*

  

Torque Tube Stow

Fixtures

7-567310009-601

7-567310010-601

1*

1*

  

MMA Container Wheel Kit

(2 Assemblies per kit)

TBD

1*

  

* Authorized by BOIP ** Increase recommendation based on Val/Ver. See 4.3.1.2.

Aircraft Property

FLYAWAY KIT

7-562108000-601

  

ECS Plugs

7-5621090002-601

INLET

7-5621090003-601

EXHAUST

2 per ACFT

MMA Cover (per Acft with FCR)

1560-01-432-2694

1 per ACFT

Air Data Sensor Cover

209-072-485-101

1730-01-066-9634

2 per ACFT

4.3.1.4 Engine Special Tools

The gaining unit will retain all special tools and kits for the T700-GE-701/-701C engines. There are no new peculiar special tools and kits required for the engine. Special tools for the -701/-701C engines are listed in the appropriate engine TMs.

4.3.2 Common Army Aviation Tools and Tool Sets

Units will continue using common Army Aviation tool sets currently found in AVUM and AVIM units with the AH-64D Apache Longbow aircraft and its associated systems. Unless otherwise directed, gaining units will retain them for use on the new model AH-64D Apache Longbow.

4.3.3 Special TMDE (to include special calibration equipment)

Specially sized (i.e., not normally found in Army Aviation support units) torque wrenches may be required for the AH-64D and FCR. If required for production aircraft and components, issue quantity will be determined and items included with the LSP. There are no special TMDE requirements for the LBHMMS.

4.3.4 Test Program Sets (TPSs) for Special TMDE

There are no Special TMDE TPSs for AH-64D-unique items, the FCR, or LBHMMS.

4.3.5 Common TMDE (to include calibration equipment)

TMDE and all associated calibration equipment currently used with the AH-64A Apache will remain in units until no operational AH-64As are based at that location. Units will turn in AH-64A and HELLFIRE TMDE not required for the AH-64D and LBHMMS per instructions to be issued prior to replacing all AH-64As with AH-64Ds at a given location. If not previously issued to the gaining unit, the Soldier Portable On-System Repair Tool (SPORT) computer will be issued per the BOIP and used on the Longbow weapon system components.

The current SPORT fielding schedule states the first production models will be available in Jan 98. In the event that the SPORT fielding schedule slips and SPORTs are not available for the initial fielding of the Apache Longbow, commercial equivalent lap top or notebook computers will be procured by the AAH PMO in the same quantities as the BOIP for the first aircraft to be fielded. The decision to buy commercial computers must be made NLT 15 Jan 98.

4.3.6 Test Program Sets for Common TMDE

There are no Common TMDE TPSs for AH-64D-unique items or the FCR. TPSs are under development for LBHMMS TMDE.

4.3.7 Performance Monitoring and Maintenance Indicators

The AH-64D has an on-board Data Management System (DMS) that uses Built-In Test (BIT)/Built-In Test Equipment (BITE) to monitor and identify faults in the aircraft's electrical and electronic subsystems. The DMS then diagnoses the indicators as a go/no-go to the flight crew or fire control repairman. The DMS further identifies the no-go subsystem component and its location within the helicopter. The Apache Longbow BIT/BITE is inherent to the system, searching for and identifying trouble spots via the MIL-STD-1553B bus.

The pilot's and copilot/gunner's Multifunctional Display (MFD) provides the capability for controlling most of the avionics systems, and serves as the primary targeting display for the Fire Control Radar (FCR). The MFD allows a crewmember to customize the way he monitors aircraft and weapons systems during a mission. The MFD is an interactive display through which systems can be controlled via bezel buttons or the remotely located sensor controllers. Page pushbuttons are used to select the desired page on the MFD.

Most warning indications are by a flashing illuminated MSTR WARN pushbutton and messages on the Up Front Display (UFD) and the MFD. There are dedicated warning lights for ENG 1, ENG 2, and APU FIRE/DET EXTG. Caution and advisory indications are illuminated on the UFD.

Additionally, the Interactive Electronic Technical Manual (IETM) to be fielded with the AH-64D Apache Longbow includes detailed troubleshooting capabilities. The IETM can be hosted on a personal computer or one of the Army's Contact Test Set (CTS) computers already fielded or under development. It will be used most often on the SPORT computer.

4.3.8 Special Purpose Kits

New Special Purpose Kits associated with the AH-64D Apache Longbow are discussed in Appendix P.

4.3.9 Other Support Equipment

Maintenance platforms and stands, cranes, and other vehicles currently used by Army Aviation units and found on MTO&E will remain in use with the AH-64D Longbow Apache. TDA items such as the Warehouse Tractor (commonly known as the "Tug") normally assigned to Aviation units will also remain in use. MTO&E for the AH-64D Apache Longbow and its associated weapons systems will authorize these items.

4.3.10 Interim Substitute Support Equipment

Based on current production and delivery schedules, limited amounts of interim support equipment may be fielded with the first AH-64D aircraft. These items, such as a substitute for the SPORT computer if it is not available to support FUE, will be replaced upon receipt of the production items. Interim support equipment, if required, will be handed off to the receiving organization’s home station detachment at its home station with the LSP. Disposition regarding turn-in of the interim support items will be forwarded to the unit by the FC.

4.3.11 Local Fabrication Requirements

TM 1-1520-APACHE/LONGBOW lists all locally manufactured items required to support the AH-64D Longbow Apache (including A/D common items). Local manufacture will be accomplished IAW TM 1-1520-APACHE/LONGBOW.

4.4.0 Supply

Supply support is established using initial stockage allowances developed from maintenance engineering estimates based on LSAR data. Projections are made using the Selected Essential-Item Stockage for Availability Method (SESAME) computer program. Data from Force Development Test and Experimentation (FDTE) and Initial Operational Test and Evaluation (IOTE) results are also used.

Standard Army Aviation supply system procedures, per AR 710-2 and AR 725-50, will be used to provide repair parts for the AH-64D. The statement of work (SOW) in the airframe and FCR production contracts requires that both contractors provide ICS for Longbow unique parts from DD250 end item delivery until five years after fielding. Through this agreement, the contractors have set objectives that all High priority (01-08) requisitions will be filled within 24 hours, all other requisitions will be filled within 5 days. Depot level repairs will have a 45 day turn-a-round time average (dock to dock). To meet these objectives, the contractors will maintain the stockage for D-unique components have the ability to transfer items between locations as needed.