Aviation Missile Command (AMCOM)

General Aviation Safety Action Message Summaries

 

 

             In brief format, this page gives the Summary of Problem as indicated in the appropriate General Aviation Safety Action Message (GEN-ASAM) issued by Commander, Aviation Missile Command (AMCOM). Take note: General ASAMs do not expire unless revised, rescinded, superceded, or incorporated and reprinted as a Technical Bulletin, becoming permanent additions to the Quality Control Library.

 

 

         

 

 

          GEN-03-ASAM-03, 19 June 2003:

Title: Updated information on Night Vision Goggles (NVGs).

Summary: This message supercedes GEN-02-ASAM-02. The intent is to use this ASAM as a change document and supplement to existing publications.

[Full Text ]

 

         

 

          GEN-03-ASAM-02, 13 March 2003:

Title: M18/M19 Landing Mat Set Operations.

Summary: As a result of unit deployments, the United States Army Safety Center (USASC) foresees an increase in the utilization of temporary landing strips and helipads. In anticipation of this increased usage, the USASC has requested units be advised of the hazards presented to aircraft and personnel when these pads are not properly secured. During a deployment to Saudi Arabia in January 1990, the rotor wash from the AH-64 aircraft caused the edge of the temporary helipad to flap up and contact the aircraft. Subsequent investigation revealed installation of the landing pad had not yet been completed when the aircraft hovered up to the edge of the pad. In addition to damaging the PNVS, the entire helipad was moved several feet from its original location.

[Full Text ]

See also 85-24335, 66-19019.

 

         

 

          GEN-03-ASAM-01, 16 December 2002:

Title: Inspection of the Battery Box [ARC-201 and ARC-220] - Corrected Copy.

Summary: CECOM issued message GPM-2002-004 to direct repair of the Battery Box, CY-8515, rivets, but many units were not on the distribution list and did not complete the required maintenance. The rivets that secure the battery holders (metal clips) inside the Battery Box, CY-8515, are denting/tearing the battery plastic film labels. This condition may result in exposing the metallic conductor under the label creating the potential for electrical shorts and leakage of corrosive materials

[Full Text Includes informative photographs. ]

 

         

 

          GEN-03-ASAM-01, 16 December 2002:

Title: Single Channel Ground and Airborne Radio (SINCGARS) ARC-201 Battery Box.

Summary: CECOM issued message GPM-2002-004 to direct repair of the SINCGARS battery box rivets, but many units were not on the distribution list and did not complete the required maintenance. The rivets that secure the battery holders (metal clips) inside the ARC-201 battery box are denting/tearing the battery plastic film labels. This condition may result in exposing the metallic conductor under the label creating the potential for electrical shorts and leakage of corrosive materials.

[Full Text Includes informative photographs. ]

 

         

 

          GEN-02-ASAM-02, 28 December 2001:

Title: Updated information on Night Vision Goggles (NVG).

Summary: This message supercedes GEN-01-ASAM-03. The intent is to use this ASAM as a change document and supplement to existing publications [Multiple important changes included].

Superceded by GEN-03-ASAM-03.

[Full Text]

 

         

 

          GEN-02-ASAM-01, 28 December 2001:

Title: Aircraft and Aviation Hydraulic Ground Units, Hydraulic Fluid Contamination Control.

Summary: Hydraulic Systems on Army aircraft and Aviation Ground Service Systems may be contaminated above the Army established baseline for both particulates and water. The Army has experienced unexplained flight control incidents where flight control binds, lock-up, or uncommanded events occurred. The first step to re-establishing effective hydraulic contamination controls will be made by identifying and ensuring correct hydraulic housekeeping procedures IAW paragraph 8 of this message are applied.

[Full Text]

 

         

 

          GEN-01-ASAM-04, 4 June 2001:

Title: Aviation Ground Support Equipment (AGSE), Hydraulic Fluid Contamination Control.

Summary: To comply with water content and cleanliness requirements contained in previous messages, AGSE that support Army aircraft are required to be maintained at substantially higher levels of purity. Water content and cleanliness requirements of these messages cannot be met without proper maintenance and careful sampling procedures.

[Full Text]

 

         

 

          GEN-01-ASAM-03, 2 May 2001:

Title: Revision to GEN-00-ASAM-01, updated information on Night Vision Goggles (NVG).

Summary: This message supercedes GEN-00-ASAM-01. The purpose of this message is to provide consolidated and updated information on aviation NVG messages. The intent is to use this ASAM as a change document and supplement to existing publications, not as a replacement.

Superceded by GEN-02-ASAM-02.

[Full Text]

 

         

 

          GEN-01-ASAM-02, 6 April 2001:

Title: Foot and Mouth Disease Aircraft Decontamination.

Summary: As a result of reported outbreaks of Foot and Mouth Disease, various countries are considering spraying aircraft (both exteriors and interiors) with various disinfectant solutions to prevent the spread of Foot and Mouth Disease. Application of unapproved disinfectants such as sodium hypo-chlorite (common household chlorine bleach) to aircraft can cause corrosion and lead to structural damage. Aircraft will be disinfected as required by the countries of destination. However, if given a choice, choose the solutions containing sodium carbonate and avoid the use of solutions containing chlorine bleach. The investigation to identify a non-corrosive disinfectant continues.

[Full Text]

 

         

 

          GEN-01-ASAM-01, 9 January 2001:

Title: Transportation of Low Voltage Batteries (General Purpose, Alkaline, and Lithium Cells).

Summary:

   A. Background -

      (1) The transportation of small batteries (AAA, AA, C, D, 9-Volt, Rechargeable, Lithium, etc.) can result in a fire when conductors short the terminals.

      (2) An AH-64 incident has raised attention concerning transportation of small batteries. Recently, a 9 volt battery was found to be the cause of an aircraft fire resulting in significant aircraft damage. The batteries were being carried loosely in a helmet bag located in the left hand storage compartment. A 9 volt battery came into contact with a steel "chart clip", causing heat and fire which quickly spread throughout the compartment resulting in extensive aircraft damage.

[Full Text]

 

         

 

          GEN-00-ASAM-01, 22 February 2000:

Title: Updated information on Night Vision Goggles.

Summary: This message supercedes GEN-98-ASAM-02 and GEN-99-ASAM-02. The purpose of this message is to provide consolidated and updated information on Aviation NVG Messages. It is not intended to replace any publication, but as a supplement to those publications.

Superceded by GEN-01-ASAM-03

[Full Text]

 

         

 

          GEN-98-ASAM-02, 25 June 1998:

Title: Revision to updated information on Night Vision Goggles.

Summary: This message supercedes GEN-98-ASAM-01. The purpose of this message is to provide consolidated and updated information on aviation NVG messages. It is not intended to replace any publication.

Superceded by GEN-00-ASAM-01.

[Full Text]

 

         

 

          GEN-98-ASAM-01, 1 April 1998:

Title: Revision to updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. It is not intended to replace any publication. [Supercedes GEN-97-ASAM-04.]

Superceded by GEN-98-ASAM-02.

[Full Text]

 

         

 

          GEN-97-ASAM-04, 10 April 1997:

Title: Revision to updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. It is not intended to replace any publication. This message does not address NVGs used for ground operations. [Supercedes GEN-96-ASAM-01.]

Superceded by GEN-98-ASAM-01.

[Full Text]

 

         

 

          GEN-97-ASAM-03, 30 December 1996:

Title: Change of procedures for loading the Crypto Keys in NAVSTAR AN/ASN-149 Global Positioning System (GPS) Receivers.

Summary: The Global Positioning System (GPS) Joint Program Office (JPO) has reported that C-17, VH-60, and HH-60 aircrews have reported errors with the navigation solution in the Receiver 3A. The failure manifests itself as a gradual navigation position solution run-off (as great as 20-40 NM) with no warning to the operator. The receiver will continue to indicate a Figure of Merit (FOM) of 1 during the run-off. This occurred during the first mission after Crypto Keys were loaded to activate the receiver's Selective Availability/Anti Spoof (SA/AS) features. Although the reported anomalies have occurred with the Receiver 3A, the failure mode is common to other receivers including the 3S, UH, OH, C4, and Manpack Receivers used in the V1, V2, and V3 configurations of AN/ASN-149 GPS sets. The problem is caused by corrupted data in the receiver and can occur when the receiver becomes authorized to operate in encrypted (P(Y)CODE) Mode. Authorization occurs when a previously-loaded GUV or CVW key is verified by the receiver. GUV keyed receivers re-verify their key each Zulu day. CVW keyed receivers are verified for the duration of the CVW key.

See also Aviation Safety Action Message CH-47-97-ASAM-06.

[Full Text]

 

         

 

          GEN-97-ASAM-02, 6 November 1996:

Title: Hydra 70 Rocket Motor suspension clarification.

Summary:

     A. A fully staffed System Safety Risk Assessment allowed the Industrial Operations Command (IOC), formerly AMCCOM, to release lots of 2.75 Inch Hydra-70 Rockets with MK-66 Rocket Motor Grains that presented early motor blow hazards to the launch vehicle in May, 1995. This SSRA included recommendations that aircrew members firing Rockets from A/MH-6, MH-60, AND AH-1 aircraft wear aviation body armor; Rockets fired from AH-64A/D and OH-58D aircraft required the aircrew to wear aviation body armor, have helmet visors down, and aircraft doors and seat side panels installed. These restrictions were transmitted to aviation units by GEN-ASAM-95-04, 021818Z June 1995.

     B. The list of authorized 2.75 Inch Hydra 70 Rocket Lots (released lots) cited in paragraph 6 of GEN-ASAM-95-04 is obsolete. IOC has, and is currently screening suspect lots of Hydra 70 Rocket Motors containing Radford and Indian head propellant grains. IOC identifies acceptable Hydra 70 lots and provides lists to HQDA. Presently, HQDA is the allocating authority and is distributing rockets that have been screened and determined to be suitable for use by aviation units.

     C. IOC attributes mishandling of the Rocket Motors during rocket production as the primary cause of early motor blows; revisions to handling procedures have been enacted. IOC prepared an abbreviated aircraft vulnerability assessment which concludes that screened lots of Hydra 70 rockets presently being allocated for training pose no credible residual risk to aviation units.

Supercedes GEN-95-ASAM-04.

   Note: Provided as info only in the GEN-ASAM sequence, not applicable to CH-47 aircraft.

[Full Text]

 

         

 

          GEN-97-ASAM-01, 25 October 1996:

Title: All US Army aircraft utilizing AN/AVS-7 System.

Summary: The navigation symbology displayed in the AN/AVS-7 System does not function properly when connected to the ASN-128B Doppler/GPS System. There have been no problems reported with the basic ASN-128 Doppler System. The problem is due to a software interface problem between the two systems.

[Full Text]

 

         

 

          GEN-96-ASAM-01, 11 January 1996:

Title: Revision to updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Supercedes GEN-95-ASAM-01.

Superceded by GEN-97-ASAM-04.

[Full Text]

 

         

 

          GEN-95-ASAM-04, 2 June 1995:

Title: Hydra 70 Rocket Motor suspension and information.

Summary:

   A. A System Safety Risk Assessment (SSRA) has been staffed. As a result of the SSRA, AMCCOM has released some lots of 2.75 Inch Hydra-70 Rockets with the MK-66 Rocket Motors with Indian Head produced propellant grain. This message is released by ATCOM to assure affected aviation units are aware of the release of specific lots of rockets and operate IAW the restrictions listed in this message when training.

   B. AMCCOM has conducted an extensive investigation into the MK66 early motor blow hazard. The below listed restrictions represent a conservative approach to mitigate the risks associated with firing the 2.75 Inch FFAR with Motors containing propellant grains extruded at the Indian Head facility. The primary suspected cause of the early motor blow on the Indian Head Rocket Motors is mishandling of the Rocket Motor. Changes to the handling procedures have been implemented and should reduce the risk of this hazard.

Supercedes GEN-95-ASAM-03.

Superseded by GEN-97-ASAM-02.

   Note: Provided as info only in the GEN-ASAM sequence, not applicable to CH-47 aircraft.

[Full Text]

 

         

 

          GEN-95-ASAM-03, 20 February 1995:

Title: Hydra 70 Rocket Motor suspension and information.

Summary: AMCCOM suspended training use of the 2.75 Inch Hydra 70 Rockets with the MK-66 Rocket Motor, (All MODS) (see references in Para 13a and 13b). This message is released by ATCOM to assure affected aviation units are aware of and implement the suspension to prevent aircraft damage.

Supercedes GEN-94-ASAM-09.

Superceded by GEN-95-ASAM-04.

   Note: Provided as info only in the GEN-ASAM sequence, not applicable to CH-47 aircraft.

[Full Text]

 

         

 

          GEN-95-ASAM-02, 25 January 1995:

Title: Procedural change to Aircraft Records Processing when the aircraft is transferred between activities. DA PAM 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary: Records are being lost or destroyed when aircraft are transferred due to a lack of adequate instructions and complicated requirements. This message clarifies and simplifies record processing for transferred aircraft, and will remain in effect until the next revision to DA PAM 738-751 is published, the records for aircraft being transferred or reclassified will be processed per this ASAM.

[Full Text]

 

         

 

          GEN-95-ASAM-01, 13 December 1994:

Title: Revision to updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Supercedes GEN-94-ASAM-03.

[Superceded by GEN-96-ASAM-01.]

[Full Text]

 

         

 

          GEN-94-ASAM-11, 31 August 1994:

Title: Approved Engine Cleaners for Army Turbine Engines.

Summary: Several units have requested that an Engine Cleaner be identified which has no hydrocarbon solvents due to Environmental Protection Agency (EPA) restrictions. The appropriate military specification for turbine engine gas path cleaning components, MIL-C-85704, has been revised to include Type II and Type IIA Cleaners which are aqueous cleaners that do not contain hydrocarbon solvents. Type II cleaners require dilution with water, while Type IIA cleaners are ready for use; no dilution required.

[Full Text]

 

         

 

          GEN-94-ASAM-10, 9 August 1994:

Title: Update to TB 43-0002-3, 29 May 92, Maintenance Expenditure Limits for Army Aircraft and TM 1-1500-328-23, 28 February 1991, Aeronautical Equipment Maintenance Policies and Procedures.

Summary:

   A. Aviation Safety Action Message GEN-93-ASAM-13 required all requests for disposition or waiver of deteriorated, damaged or destroyed aircraft to be forwarded to AMSAT-I-MDM. This address is in error.

   B. TM 1-1500-328-23 does not contain procedures for an AVIM unit to be approved to perform Depot level repair of an item. These procedures and other corrections are included in this message.

[Full Text]

 

         

 

          GEN-94-ASAM-09, 8 August 1994:

Title: Hydra 70 Rocket firing from Army helicopters.

Summary: Reports from the field indicate that specific Hydra 70 Rocket Motor Exhaust Debris from certain production lots are causing damage to Army helicopters. The damage consists of large dents in the skin (up to seven inches long, 0.5 inches deep) and sometimes holes (up to 1/2 inch in diameter). This damage can occur to Stabilators/Elevators, Skin, and Tail Rotors.

Superceded by GEN-95-ASAM-03.

Note: Provided as info only in the GEN-ASAM sequence, not applicable to CH-47 aircraft.

[Full Text]

 

         

 

          GEN-94-ASAM-08, 19 July 1994:

Title: Rescission of GEN-94-ASAM-05 concerning Vibration Analysis Equipment.

Summary: The purpose of this message is to rescind GEN-94-ASAM-05, DTG 101800Z Mar 94 concerning Vibration Analysis Equipment. Information on the standard vibration analysis equipment for Army aircraft can be found in MAM-ATCOM-94-009, DTG 132000 Jul 94.

Rescinds GEN-94-ASAM-05.

[Full Text]

 

         

 

          GEN-94-ASAM-07, 26 April 1994:

Title: Use of Global Positioning System (GPS).

Summary:

     A. To ensure the widest possible dissemination, the following is a retransmission of DIRUSAASA Message, DTG 151156Z Apr 94, Subject: U.S. Army Aviation Use of Global Positioning System.

     B. On 8 Dec 93, SECDEF announced to DOT that GPS had achieved Initial Operational Capability (IOC) as defined in the 1992 Federal Radionavigation Plan (FRP). On 28 Apr 94 Phase Three of the Federal Aviation Administration (FAA) implementation program will commence with the publication of approximately 300 instrument approach procedures (IAPs) indicating "OR GPS". Thereafter, an additional 600 "OR GPS" Civil IAPs will be added to National Ocean Survey (NOS) Flight Information Publications (FLIP) products each 56 day cycle until approximately 3,900 IAPs have been published (many of these civil IAPS also will appear in DOD FLIP). This program exists only in the United States National Airspace system (NAS). So far, other than the U.S. and FIJI, no other nations have established standards for, nor approved the use of GPS for any aeronautical purpose. Therefore, outside of the NAS, the use of GPS as a sole or primary means of navigation in civil airspace is not authorized, not even for VFR flights. We will advise you as other nations adopt the use of GPS within their airspace.

     C. Presently there are no known DOD/U.S. Army GPS systems designed or configured to meet the equivalent levels of Federal Aviation Administration TSO-C129 Safety and Performance Standards required to fly Enroute, Terminal or Non-precision Approaches under Instrument Flight Rules (IFR). Accordingly, until the U.S. Army Aviation and Troop Command (ATCOM) can certify a GPS system for IFR operations, U.S. Army use of GPS to fly IFR or to participate in the FAA's Civil GPS overlay program is not authorized. GPS also may not be used to fly IAPs designed for other area navigation systems such as VOR/DME-BASED or LORAN-C RNAV Procedures.

     D. U.S. Army installations within the NAS desiring to establish GPS overlay procedures for their airfields should provide justification and submit requests to the U.S. Army Aeronautical Services Agency (USAASA) IAW AR 95-2, Chapter 11. Due to a FAA Procedures Development backlog, we expect the process to be lengthy. However, validated requests will be prioritized and submitted to the Defense Mapping Agency for publication as production cycles permit. For the near-term, we do not expect to develop any pure GPS RNAV IAPS IAW FAA Oorder 8260.38. Neither DOD nor the U.S. Army have established a requirement to acquire Avionics capable of executing pure, GPS-ONLY Instrument Approach Procedures.

[Full Text]

 

         

 

          GEN-94-ASAM-06, 22 March 1994:

Title: Advance information on the AN/AVS-6 25 MM Eyepiece Lens Assembly.

Summary: The purpose of this message is to provide AN/AVS-6 users and maintainers with up-to-date information on the new 25 MM Eyepiece Lens Assembly, NSN 5855-01-380-5102.

[Full Text]

 

         

 

          GEN-94-ASAM-05, 10 March 1994:

Title: Non-Standard Vibration Analysis Equipment.

Summary:

     A. There have been several reports of unit level commanders and contractors, that perform maintenance for the Army, procuring and allowing the unauthorized usage of nonstandard vibration analysis equipment for the purpose of helicopter track and balance maintenance and vibration troubleshooting. Local procurement and usage of any other vibration analysis equipment not referenced in Para 4B, for the purpose of performing helicopter track and balance maintenance and/or vibration troubleshooting, is considered a direct violation of Army Regulation 70-62, Airworthiness Qualification of U.S. Army aircraft systems, paragraphs 4.D(1) (Utilization of Non-Approved Allied Equipment Testing), and 4.F(5) (Modifying Parameters Which Could Affect The Operating Limits and/or Emergency Procedures Specified in the Operators Manual).

   B. The Aviation Vibration Analyzer (AVA), NSN 6625-01-282-3746, is the standard US Army support equipment to facilitate helicopter track and balance maintenance and perform helicopter vibration troubleshooting tasks. The AVA and the Chadwick Helmuth Model 177 (Vibrex), NSN 4920-01-040-7816 are the equipment authorized for use on all US Army aircraft. The Helitune Model R5M (Rotortuner) is authorized for use on the CH-47 only. Engineering support for safe and effective track and balance maintenance can only be provided when authorized support equipment is used.

Note: There are no exceptions to this policy unless specifically authorized by the aircraft statement of airworthiness qualification or an airworthiness release.

   C. Previous use of unauthorized track and balance, and/or vibration analyzers on Army aircraft does not constitute grounding of aircraft. However, all aircraft on which unauthorized track and balance, and/or vibration equipment has been utilized, shall have rotor (main and tail) track and balance maintenance performed with equipment referenced in Para 4B at the next phase inspection or required track and balance, whichever occurs first.

Rescinded by GEN-94-ASAM-08.

[Full Text]

 

         

 

          GEN-94-ASAM-04, 2 March 1994:

Title: Reporting of Fuel Cell problems using Quality Deficiency Reports.

Summary: A Product Quality Deficiency Report (PQDR), SF 368, is an important vehicle to identify material problems in aviation. Units are encouraged to submit PQDRs for early detection of mechanical defects and non conforming parts. Actions initiated on certain Fuel Cells could have been addressed earlier if these problems were identified in the PQDR system.

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          GEN-94-ASAM-03, 20 December 1993:

Title: Revision to updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. This message revises CDRATCOM Message 091900Z Dec 93, GEN-94-ASAM-02, Para 8H and 8I concerning Modification Work Orders (MWO) and Red or White Lighting. This message provides the field with the most updated information. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Supercedes GEN-94-ASAM-02.

Superceded by GEN-95-ASAM-01.

[Full Text]

 

         

 

          GEN-94-ASAM-02, 9 December 1993:

Title: Updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. This message provides the field with the most updated information. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Superceded by GEN-94-ASAM-03.

[Full Text]

 

         

 

          GEN-94-ASAM-01, 9 December 1993:

Title: Restriction of Discolored Plastic Prescription Sunglasses With Plastic Lenses.

Summary:

Note: Brief pilots and insert a copy of this message in the Pilots Information File and pass copy to supporting Flight Surgeons.

   A. The Triservice Aeromedical Research Panel (TARP) has advised the services of the potential inability to visualize Cockpit Caution/Warning Lights when utilizing Plastic Prescription Sunglasses that are tinted too dark. Although these glasses are supposed to transmit a standard amount of light (approximately 15%), the actual transmission varies. One pair of Sunglasses that was tested had a light transmission of 2%. In addition, the current Plastic Prescription Sunglasses may have a tendency to display color distortion over time. This may be due to outdated or faulty dyes as well as exposure to adverse environmental conditions such as UV radiation or heat. The end result of both the light transmission and color distortion problems may cause aircrews to misinterpret important visual information.

[Full Text]

 

         

 

          GEN-93-ASAM-13, 31 August 1993:

Title: Update to DA Pamphlet 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary:

   A. DA Pamphlet 738-751, TAMMS-A, Dated 15 June 92, is currently under revision. DA Pamphlet 738-751 requires TAMMS-A users to forward DA Form 2408-15-2/2408-15-2-E, 2408-20/2408-20E, all completed Scheduled Maintenance Checklists and supporting Forms and Records to Corpus Christi Army Depot (CCAD) after the files becomes inactive. These requirements have been rescinded.

   B. GEN-93-ASAM-09 provided guidance for completion of Maintenance Inspection Checklists. These instructions are modified by this message.

   C. TM 1-1500-328-23 provides instructions for the documentation of Maintenance Test Flight and Maintenance Operational Check accomplishment. Those instructions are deleted by this message.

   D. TB 43-0002-3 and DA Pamphlet 738-751 provide conflicting requirements for documentation of deteriorated, damaged, or destroyed aircraft when requesting disposition or waiver from ATCOM. This message defines the required procedure.

   E. To eliminate confusion, the following instructions will be used until the next revision of DA Pamphlet 738-751 is fielded. A copy of this message will be inserted in the TAMMS-A Manual for reference and use.

[Full Text]

 

         

 

          GEN-93-ASAM-12, 19 August 1993:

Title: Pitot Static Systems Tester, Case Grounding.

Summary: There have been reports of operators getting electrical shocks by touching the case of the most recently fielded Pitot Static Tester while in use. The potential on these cases has been measured at approximately 60 volts when connected to a 115 Volt, 60 Hertz Power Source. This results from the power cords not having a ground wire.

[Full Text]

 

         

 

          GEN-93-ASAM-11, 10 August 1993:

Title: Proper Control of Depot Level Repairs.

Summary:

   A. Recent reports have indicated that some Aviation Intermediate Maintenance Units (AVIM) are using outside contractor support to perform Depot Level Maintenance on certain aircraft equipment. This practice is not permitted, unless the AVIM Unit has requested and been approved by the Department of the Army to function as a Special Repair Activity (SRA).

   B. Proper control of Depot Level tasks performed at the AVIM level, whether performed organically or commercially, is mandatory to assure Flight Safety characteristics of the equipment are not compromised. The SRA process provides this control as well as the visibility needed to assess the impact on the supply system.

   C. Provisions for obtaining SRA approval are contained in Army Regulation (AR) 750-1.

[Full Text]

 

         

 

          GEN-93-ASAM-10, 9 June 1993:

Title: Inappropriate use of Non-Fire Resistant Jackets with the Aviation Battle Dress Uniform (ABDU).

Summary:

   A. The Defense Personnel Support Center (DPSC) is currently fielding the Aviation Battle Dress Uniform (ABDU) without the companion ABDU Flight Jacket. The ABDU Flight Jacket will not be available for two years. The US Army Safety Center and user community recognize the continued requirement for Fire Resistant (Nomex) Flight Uniforms. Inquiries concerning suitable interim alternative clothing items acceptable for wear in lieu of the ABDU Jacket have been received from the field. The ABDU Jacket alternatives in order of increasing risk are as follows:

      (1) Current Sage Green Nomex Flight Jacket.

      (2) Sweater, Wool worn under ABDU.

      (3) Undershirt, Cotton, worn under ABDU.

      (4) Combinations of 1, 2, 3 above.

   Note: Synthetic Sleeping Shirts and Synthetic Field Jackets (Gortex) are unacceptable for use with the ABDU. Synthetic material clothing items increase burn severity in the event of fire, whether in flight or post-crash-survivable. Recommend that the current Nomex Flight Jacket be worn during flight until the ABDU Jacket is fielded.

[Full Text]

 

         

 

          GEN-93-ASAM-09, 24 May 1993:

Title: Maintenance Checklist Procedures to be included in DA Pamphlet 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary:

   A. DA Pamphlet 738-751, TAMM-A, dated 15 June 1993, was issued 1 Sep 92. The pamphlet deleted DA Form 4676-R and provided no alternate instructions to document the performance of Phase, Periodic, PMP and Progressive Phase Maintenance. Since then, this command has received numerous DA Forms 2028 requesting detailed instructions for documenting these inspections.

   B. To eliminate confusion, the following instructions will be used until the next revision of DA Pamphlet 738-751 is fielded. A copy of this message will be inserted in the TAMMS-A Manual for reference and use.

   Note: Units will continue to use guidance in ATCOM Message 091330Z Mar 93, Subject - Aviation Night Vision Goggle (NVG) Maintenance Documentation (GEN-93-ASAM-05) and Flightfax, dated April 93, to complete Forms and Record for Aviation NVGs.

[Full Text]

 

         

 

          GEN-93-ASAM-08, 20 May 1993:

Title: Status of the new DA Pam 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary:

   A. DA Pam 738-751, TAMMS-A, 15 Jun 92, was issued 1 Sep 92. Since then, this command has received numerous DA Form 2028's with recommended changes. All recommended changes have been resolved and will be included in the Sep 93 edition of the Pam.

   B. To eliminate confusion and cause less burden on aviation units/activities, we are providing quarterly updating of approved changes to the DA Pam. Authority for the use of these changes is granted to all U.S. Army aviation units/activities, contract support maintenance units/activities, and related audit/inspection activities. A copy of this message will be inserted in the TAMMS-A Manual for reference and use.

   Note: Units will continue to use guidance in ATCOM Message 091330Z Mar 93, Subject - Aviation Night Vision Goggle (NVG) Maintenance Documentation (GEN-93-ASAM-05) and Flightfax, DTD Apr 93, to complete Forms and Records for Aviation NVGs.

[Full Text]

 

         

 

          GEN-93-ASAM-07, 10 May 1993:

Title: All aircraft equipped with SKED Litter Systems.

Summary: Due to unreliable performance in the field the locally fabricated Weak Link as described in FM 8-10-6 dated 31 October 1991, Para E, Pages 11-10 and 11-11, will no longer be authorized.

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          GEN-93-ASAM-06, 9 March 1993:

Title: Status of new DA Pam 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary:

   A. DA Pam 738-751, TAMMS-A, 15 Jun 92 was issued 1 Sep 92. Normally, DA Pams are effective and implemented immediately upon issue. In this case, however, there were many problem areas which prevented the implementation in some aviation units/activities. The main problem was that aviation units/activities failed to receive sufficient copies of forms and records prescribed in the new DA Pam. The DA Pam was completely revised and all DA Form 2408 series forms and records were totally redesigned. The old 2408 forms in previous editions of the DA Pam are obsolete and will not be used. All DA Form 2408 series forms and records prescribed by the new DA Pam are now on hand at the U.S. Army Publications Distribution Center (USAPDC), Baltimore, MD for distribution to all Army aviation units/activities. Max quantities of the new forms for each installation have been revised to allow each unit/activity to requisition and receive proper quantities to implement and sustain the new DA Pam.

   B. It appears that other existing problems at local level are causing units/activities not to implement the new DA Pam in a timely manner. Local (CMD) publications distribution centers were originally issued small amounts of the newly designed forms and records from USAPDC. When a unit or activity requisitioned needed forms, the local pub center could only provide a limited quantity of each form, resulting in field units not being able to implement the DA Pam.

   C. This CMD solicits logistics assistance from all aviation maintenance managers in the field, especially those assigned to division and corps HQs to help resolve all local problems. Solving problems at each unit and at the local (CMD) publications centers will allow DA Pam 738-751 to be implemented without further delay.

   D. Due to problems of providing Army aviation field units/activities sufficient copies of the new forms, an extension date for implementation of the new DA Pam has been authorized by the Department of the Army Logistics Office - Aviation (DALO-AV). The extension date for implementation of the Pam is 15 Apr 93, with a completion date of implementation to occur NLT 30 calendar days thereafter.

   E. The importance of early implementation of this Pam cannot be overemphasized. Army aviation is on the threshold of extending/fielding an army aviation automation initiative called Unit Level Logistics System - Aviation (ULLS-A) in FY93/FY94. Aviation field unit/activity personnel need all the experience they can obtain on the new forms and records to allow easy transition to ULLS-A.

   Note: Units will use guidance in ATCOM Message 091330Z Mar 93, Subject - Aviation Night Vision Goggle (NVG) Maintenance Documentation (GEN-93-ASAM-05), to complete forms and records for aviation NVGs.

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          GEN-93-ASAM-05, 9 March 1993:

Title: Aviation Night Vision Goggle (NVG) Maintenance Documentation.

Summary: The purpose of this message is to update present aviation night vision goggle maintenance documentation requirements. This message becomes effective immediately upon receipt and supersedes PMNVEO Message 221530Z Mar 91 and the June 1991 Flightfax. It will be used to supplement DA Pam 738-751, dated 15 Jun 1992. This message expires on 31 Dec 93.

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          GEN-93-ASAM-04, 1 March 1993:

Title: Use of Dual Visor on SPH-4B Aviator's Helmet and related information.

Summary: AVSCOM Message 301400Z Mar 92 stated that the Dual Visor shall not be used with the Aviator's Night Vision Imaging System (ANVIS) or the GM-6 Night Vision Goggles (NVG). An Army study indicated that some pilots using the Dual Visor Assembly (DVA) with the SPH-4B helmet required additional upward tilt range. As a result of further testing, certain procedures are considered necessary and must be completed prior to the first NVG flight with the SPH-4B helmet.

Rescinds GEN-92-ASAM-06.

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          GEN-93-ASAM-03, 6 January 1993:

Title: Status of the new DA Pam 738-751, 15 Jun 92, Functional Users Manual for the Army Maintenance Management System - Aviation (TAMMS-A).

Summary: DA Pam 738-751, TAMMS-A, 15 Jun 92, was issued 1 Sep 92. Since then, this command has received numerous DA Form 2028's with recommended changes. All recommended changes have been resolved and will be included in the Sep 93 edition of the Pam.

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          GEN-93-ASAM-02, 21 December 1992:

Title: Updated information on Night Vision Goggles.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. This message provides the field with the most updated information. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Superceded by TB 1-1500-346-20.

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          GEN-93-ASAM-01, 1 December 1992:

Title: Prohibit use of BRAYCO 599 Corrosion Preventative Concentrate.

Summary:

   A. "BRAYCO 599" Corrosion Preventative Concentrate is currently specified in the preservation of AH-1, UH-1, OH-58, OH-58D, and OH-6 gearboxes and engines during aircraft storage. Information also indicates that BRAYCO 599 is being used in operating engines and gearboxes as a corrosion preventative in the field. A possibility also exists that other Army aircraft may have been serviced with BRAYCO 599.

   B. BRAYCO 599 has been linked to high iron content in oil analysis samples. The corrosion preventives in the BRAYCO 599 containers are contaminated with iron from an unknown source and are contributing to erroneous high iron readings in oil analysis samples. In many cases, engines and gearboxes are being condemned and removed due to the false oil analysis results.

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          GEN-92-ASAM-09, 14 July 1992:

Title: Safety Office Move.

Summary: The Safety Office has moved to new offices within AVSCOM and new telephone numbers have been assigned action officers.

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          GEN-92-ASAM-08, 29 April 1992:

Title: Use of Portable Computers onboard U.S. Army aircraft.

Summary: Due to inquiries for guidance on the use of portable computers onboard U.S. Army aircraft, this message is being issued to provide important information on the safe usage of these devices.

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          GEN-92-ASAM-07, 2 April 1992:

Title: Use of discrepant lots of SYN TECH Grease, P/N 3913-G1.

Summary:

   A. The U.S. Air Force has reported that certain lots of grease, P/N 3913-G1, FSCM 53592, NSN 9150-00-506-8497 manufactured by SYN-TECH LTD during June 1990 (6/90) and February 1991 (2/91), have failed to meet the required lubrication specification. AVSCOM concurs with these findings and is directing units not to use these grease lots for lubrication of Army aircraft. Grease manufactured during April 1991 (4/91) and June 1991 (6/91) marginally failed the specification requirements, however; use of these lots is considered acceptable and will continue to be authorized.

   B. The above grease has a shelf life of four (4) years. An informal survey of several field units has revealed quantities of grease that have exceeded the 4 year life.

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          GEN-92-ASAM-06, 30 March 1992:

Title: Night Vision Goggle information concerning the Dual Visor on Aviator's Helmets.

Summary:

   A. AVSCOM Message 031500Z Jan 92 [actual date was 3 February 1992, see GEN-92-ASAM-03] extended the expiration date of HQDA Message 261942Z Aug 91 until 1 Apr 92. HQDA Message 261942Z Aug 91 dealt with the Dual Visor used on the new SPH-4B Aviator's helmet. In a recent Army study, pilots using the new Dual Visor Assembly with the SPH-4B and SPH-4 Helmets stated a need for more upward tilt range. As a result of this study, additional testing on the ANVIS tilt requirements with the Dual Visor is now required.

   B. Until further notice, the Dual Visor shall not be used with the Aviator's Night Vision Imaging System (ANVIS) or the GM-6 mounted AN/PVS-5 series goggles. This restriction will be lifted upon completion of additional testing and final approval. The SPH-4B Helmet may be flown using a Single Visor with the ANVIS or the GM-6 mounted AN/PVS-5 series goggles. Single Visors, NSN 5855-01-151-4229 are available in the supply system. Exercise care when replacing to prevent damage of the Thermal Plastic Liner (TPL).

Rescinded by GEN-93-ASAM-04.

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          GEN-92-ASAM-05, 10 March 1992:

Title: All UH-1, AH-1, OV-1, OH-58, H-6, CH-47, UH-60 and AH-64 aircraft, Corpus Christi Army Depot (CCAD) Hot Line and Engine Service Center (ESC) Support for T53, T55, T63 and T700 Engines.

Summary: The purpose of this message is to provide information concerning the CCAD Hot Line and Engine Service Center to assist field units.

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          GEN-92-ASAM-04, 4 February 1992:

Title: Use of Project Codes as a result of Safety of Flight (SOF) Messages and Aviation Safety Action Message (ASAM).

Summary: Defense Management Report Decision (DMRD) 904/904C mandates the Stock Funding of Depot Level Repairables (DLRS). These parts were previously procurement funded and issued free to the field. Beginning 1 Apr 92, the Stock Fund will require reimbursement for these parts. As this date draws near, the issue of how customers will budget for and subsequently fund unexpected Safety of Flight requirements has surfaced. The plan at this time is to establish funds identified specifically to Safety of Flight costs and lift the burden off the field. In order to budget for these funds and provide parts to the customer at no cost, it is imperative that the project codes assigned and identified in Para 10B of Safety of Flight and Aviation Safety Action Messages be used when requisitioning parts. Details laying out the reimbursement procedures will be provided at a later date when final policy decisions have been made.

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          GEN-92-ASAM-03, 3 February 1992:

Title: Night Vision Goggle information concerning SPH-4B Aviators Helmet.

Summary: HQDA Message 261942Z Aug 91 dealt with the ANVIS Visor Mount incompatibility with the Dual Visor used on the new SPH-4B Aviator's Helmet. AVSCOM Message GEN-92-ASAM-02, Paragraph 4C(12) provided an expiration date of 1 Feb 92 for HQDA Message 261942Z Aug 91. The expiration date of this message is now extended to 1 Apr 92. PM-NVEO is now coordinating an effort to resolve this problem. Approval of this effort is expected within 30 days.

See also GEN-92-ASAM-06.

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          GEN-92-ASAM-02, 19 December 1991:

Title: Updated information on Night Vision Goggle Messages.

Summary: The purpose of this message is to provide consolidated and updated information on aviation NVG messages. This message provides the field with the most updated information. It is not intended to replace any publication. This message does not address NVGs used for ground operations.

Superceded by TB 1-1500-342-20-1.

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          GEN-92-ASAM-01, 4 November 1991:

Title: Inspection of T53 Engine Jetcal Analyzer, Heater Probe Assembly.

Summary: Several instances of failures of the T53 Engine Heater Probe Assembly, Heater Unit overhauled by Sacramento Army Depot (SAAD), have been reported. There is insufficient insulation of the leads from the Heater Element; therefore, they are shorting out causing sparks and/or a blown fuse. This also could cause an electrical shock to personnel.

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