Air_Worthiness_Release.pdf

6 Sep 17 | R18

RDMR-AE 15 Mar 02

SUBJECT: Airworthiness Release (AWR) for UH-60A/L and HH-60L Helicopters Equipped with SEI Industries Bambi Water Buckets (AWR 1054)

Appendix A. Restrictions and Operating Information:

1. Operate IAW the appropriate aircraft Operator’s Manual (reference 1 or 24), except as modified by this AWR.

a. Deleted

b. Bambi Bucket operations are restricted to Visual Meteorological Conditions (VMC).

c. Deleted

WARNING

The Bambi Bucket and associated system components have not been tested for

Electromagnetic Effects. Radiated electronic emissions may cause inadvertent release of external loads.

Deleted

The potential for static electricity shock exists when the Remote Power Supply or

Bambi Power Pack are not properly grounded. Ensure proper grounding prior to operation.

NOTE

Bambi Bucket System components may not operate below -7°C (+20°F).

Weight limitations shall be strictly observed. This AWR is not intended as authorization to exceed the aircraft weight limitations stipulated in the Operator’s

Manual. Depending on aircraft configuration, cargo, and/or personnel on board, weight limitations may prohibit full load capacity carried in the Bambi Bucket.

d. Deleted

e. In-flight charging of the Remote Power Supply or Bambi Power Pack is prohibited.

f. Airspeed shall not exceed 95 knots with the Bambi Bucket (without Long Line) empty, and shall not exceed 50 knots during dumping operations.

g. Water replenishment will be conducted from a stabilized hover. The bucket will be lowered vertically into the water and, once filled, withdrawn from the water vertically. Forward movement will not be attempted until the bucket is clear of the surface of the water.

CAUTION

Rapid lateral cyclic inputs shall be avoided with the Bambi Bucket full with a

Long Line. The resulting lateral load oscillation could result in aircraft damage.

During missions under authority of the US Forest Service, Long Lines of no less than 50 feet in length shall be used (reference 30).

Sacksafoam II and III are not necessarily cross-compatible with the same Bambi

Buckets as the original Sacksafoam (I) system.

Excessive hovering with an empty Bambi Bucket will cause the bucket and suspension lines to twist, and will lead to increased bucket filling times.

It is suggested that the speed be increased slowly with the empty Bambi Bucket to determine the maximum safe airspeed for the helicopter.

h. Airspeed shall not exceed 75 KIAS with the Bambi Bucket empty while using a Long Line.

i. Deleted

j. This AWR shall be considered temporary in order to serve the priority needs of typical fire fighting missions. This AWR is not intended to cancel other existing AWRs on the aircraft for other nonstandard equipment, unless such equipment interferes with the installation of the

Bambi equipment. Due to the priority of Bambi Bucket missions, it may be necessary to remove interfering nonstandard equipment. Subject equipment shall be removed upon mission completion.

k. Torrentula Valve-equipped Bambi Buckets with the PowerFill System shall be operated

IAW the Operator’s Manuals (references 27 and 28), or most current manufacturer’s instructions.

l. HH-60A/Ls are not authorized to operate Bambi Buckets with the Powerfill System installed.

m. UH/HH-60A/Ls are authorized to operate Bambi MAX buckets with Bambi Power Packs

IAW the Bambi MAX Operations Manual (reference 34) and Bambi MAX Power Pack Manual

(reference 37). Aircraft power shall not be used for Bambi MAX operation.

2. Performance: Drag: With the Bambi Bucket installed, add 80 square feet of drag (8.0 drag multiplying factor).

3. Use of Bambi Buckets when snow skis are installed is authorized.

To verify interference does not exist between the Bambi Bucket and the Public

Safety frequencies collectively referred to as the "700 and 800 MHz bands";

exercise the Bambi Bucket's electronics on the ground with the mission frequencies to verify no interaction. If mission frequencies have been utilized in previous missions and no interference was noted, then there is no need to perform.

If interference is detected on mission frequencies, then an alternate frequency may be required. The Radio Frequency Interference's impact will be to cause a reduction in the receiver's reception range but only during the duration of the

Bambi Bucket's operation, e.g. fill, dump, or fire retardant loading.

Appendix B. Configuration and Installation Detail:

1. The basic UH-60A/L and HH-60L helicopters are defined in their respective Operator’s Manual with exceptions as noted within this Airworthiness Release.

2. The following table identifies the subject equipment’s compatibility and authorized use with other

UH-60 nonstandard systems authorized by existing AWRs. Each line in the following table indicates a one-for-one compatibility comparison between the subject equipment and the individual system listed.

The table does not indicate the subject equipment’s compatibility with the total combination of the following equipment systems. Unknown physical, electrical, and/or electromagnetic compatibility

(EMC) issues may exist during use of this subject equipment in aircraft configured with varying combinations of the following equipment. Changes to aircraft configuration incur a requirement of a

Functional Compatibility Check (FCC). Contact the POC for this AWR to determine requirements to establish compatibility of the subject equipment with any non-standard equipment not listed below.

This AWR does not supersede or negate the requirements, limitations, or inspections mandated by the original AWR authorizing the below mentioned equipment. This equipment is compatible with all current existing Interim

Statements of Airworthiness Qualification (ISAQ).

AWR Equipment Description

744 Pilot Steps with Tow Rings on UH-60A/L and HH-60L

893 UH-60A/L Helicopters with Vertical Support Pylon Fairing Modifications

966 Fuel Sample Accessory Box Installed on UH-60A/L Helicopters

1189 Deleted

1203 Mylar Tear-Off Windshield Cover (MTOWC) on UH-60A/L/M and HH-60L/M 1223 Infrared (IR) Anti-Collision Light Lens Installed on US Army UH-60A/L/M, HH-60L 1309 Oregon Aero Seat Cushions on UH-60A/L and HH-60L 1310 ARC-164 HAVE QUICK II on UH-60A/L and EH-60A 1343 UH-60A/L with Modified Application of Blade Erosion Tape in Combat Operations

1452 UH-60A/L Helicopters Equipped with the LC-6 Digital Chronometer

1459 Simula Seat Cushion for the Pilot/Copilot and Crewchief/Gunner 1515 UH-60A/L and HH-60L with CN-1552B/A & CN-1564C/A MEMS Rate Gyroscopes

1516 UH-60A/L/M and HH-60L/M Aircraft with the EBC 406HM Emergency Locator Transmitter (ELT)

1524 UH-60A/L and HH-60L with Protective Materials Company Ballistic Armor Protection System (BAPS)

1539 UH-60A/L/M and HH-60L/M with Aerospace Filtration Systems (AFS) APU Inlet Barrier Filters

3. The following equipment is not compatible with the subject equipment and shall not be used simultaneously with the subject equipment:

AWR Equipment Description

980 Rescue Hoist Equipment on UH/HH-60 Helicopters

1127 Helibasket with Electric Longline on UH-60A/L

1308 Goodrich 42305-5 Internal Rescue Hoist (IRH) on UH-60A/L MEDEVAC 1330 Deleted

1374 UH-60A/L Fast Rope Insertion/Extraction System (FRIES) Equipment Installed

1454 UH-60A/L Helicopters Equipped with the Family of Loud Speakers (FOL)

1930 MEDEVAC UH-60A/L and HH-60L Helicopters Equipped with Patient Movement Items (PMI)

4. Additional Configuration Information:

a. The Bambi Bucket shall be installed IAW references 2 through 4, 16 through 21, and/or 24, or most current manufacturer’s instructions. UH-60L aircraft shall utilize references 5, and 16 through 20, or most current manufacturer’s instructions. For either installation used, one of the following conditions shall apply:

(1) The breakaway connector shall be a standard household plug type and be lightly taped with two wraps of nylon tape. The breakaway resistant force of the nylon tape shall be measured and shall not be more than ten pounds. The plug shall be rated at a minimum of 15 amperes.

(2) The breakaway connector assembly shall consist of an MS-3101A24-11S plug and an

MS3107A24-11P quick disconnect with MS3057-16A backshell cable clamps. The MS3057-16A backshell cable clamps shall be shimmed to accommodate small gage wire by using a four-inch section of 3/8-inch inside diameter (ID) neoprene hose and a two-inch section of 5/8-inch ID neoprene hose to accomplish a tight fit.

b. Torrentula Valve-equipped Bambi Buckets with the PowerFill System shall be powered by

Pin A of J227 (28 V DC and 130 DC amps), and installed and operated IAW references 27 and 28, or most current manufacturer’s instructions.

c. The following items are optional equipment and may be used at the discretion of the local command.

(1) The Sacksafoam (I) foam-dispensing system shall be installed and operated IAW reference 6, or most current manufacturer’s instructions.

(2) The Sacksafoam (I) foam-dispensing unit shall not be used with Torrentula Valve-equipped Bambi Buckets.

(3) Sacksafoam II and Sacksafoam III systems shall be installed and operated IAW references 7, 13, 31 and 32, or most current manufacturer’s instructions.

(4) Sacksafoam II and III shall be secured to the aircraft floor with two cargo straps forward and aft, two cargo straps laterally, and IAW paragraph 6.20.3 of reference 1.

CAUTION

Sacksafoam II and III (Models SFF2-5598 and SFF3-6598) manufactured before

July 1998 will suffer failure when the polarity of the power supply is accidentally reversed. Correct polarity is critical to both the Sacksafoam power and Bambi dump power circuits. If reverse polarity in the Sacksafoam circuit has occurred, several components in the system may need replacement: (1) the 10 amp fuse,

(2) the dip tube switch, (3) the fill pump relay, (4) the diode across the fill pump relay primary coil. If the fuse has blown, it is indicating that a short has occurred in the Sacksafoam circuit, and that above items 2, 3 and 4 must be tested and replaced as necessary. If the polarity of the Bambi dump power is reversed, the

Sacksafoam controller will malfunction when the dump switch is depressed.

(5) The Suppression Agent Injection System (SAIS) shall be installed and operated IAW reference 11.

(6) The Marine Recovery Device for Bambi Buckets shall be installed IAW reference 15, or most current manufacturer’s instructions.

Attachment of the breakaway cord shall be made at the cargo hook to airframe attachment location (shaft).

d. Substitution of a manual water door release cable is authorized in place of the electrical solenoid IAW reference 8, subject to the following restrictions as requested in reference 9.

(1) The cable shall be attached to the bucket release arm by suitable means to prevent its release through normal use and jettison. Safety wire shall not be used to attach the cable to the bucket.

(2) The aircraft end of the release cable shall be attached in the hook well vicinity with a suitable breakaway method, not exceeding ten pounds tension. The cable and breakaway attachment shall be routed and attached in a manner that minimizes the potential for entanglement with hook well components during jettison.

(3) Bambi Buckets equipped with the Torrentula Valve may not be operated by manual water door release cable, as stated above.

The following power source configuration is applicable only to UH-60 helicopters with the rescue hoist modification kit as described in reference 17.

The HH-60A/L shall not be configured with the internal rescue hoist modification kit as described in reference 17.

e. UH-60 aircraft fitted with the rescue hoist modification kit provide a 28 volt DC power source capable of supplying power to operate the Torrentula valve Bambi Bucket and the optional

Sacksafoam II or III with the hoist control master switch placed in the on position. J227 in the right aft cargo compartment provides power to the internally mounted rescue hoist. Pin A of J227 carries 28 V DC and 130 DC amps for operation of the rescue hoist. The Bambi Bucket and

Sacksafoam II or III require a combined total of up to 41 amps DC available for normal operation.

f. Hoist connector P227 is required to correctly connect the Bambi Bucket junction box to the rescue hoist wiring. P227 connector plug pins used for the Bambi Bucket installation are correctly sized to accommodate the 10 AWG wire that is supplied with the Bambi Bucket. A short pigtail is also attached to pin A of P227 using 14 AWG wire for power for the Sacksafoam II or III. The 14

AWG pigtail connected to pin A of P227 shall have a 15-amp circuit breaker installed as close as possible to where the pigtail is attached to 10 AWG wire or P227 but visible to the crew (outside the sound proofing).

g. The new wires for the subject equipment shall be routed and clamped in such a manner that assures protection from physical abuse, i.e., being stepped on, door slammed on, or hung from as a handhold and will not cause tripping or other hazards to crew or maintenance personnel. Particular attention shall be given to adequate bonding of neutral wires. The wires shall be adequately protected from vibration, chafing, or stretching. Do not clamp wires to control tubes or cables, fuel lines, hydraulic lines, etc. Care should be taken to insure the cable will not interfere with other items of the aircraft or personnel. All equipment shall be installed to insure there is no interference with emergency egress from the aircraft in the event of aircraft incident.

h. Installation of Torrentula Valve-equipped Bambi buckets on UH-60A aircraft without the

Rescue Hoist Modification Kit shall be as follows:

(1) Connector J265, in the left aft cargo compartment, provides power for a command console. Pin B of J265 carries 28 V DC and 25 amps.

(2) Connector J265 pins used for the Bambi Bucket installation are correctly sized to accommodate the 10 AWG wire that is supplied with the Bambi Bucket.

(3) Due to power requirements, the Torrentula Valve-equipped Bambi Bucket and the

Sacksafoam III may not be simultaneously operated in this configuration.

i. The only extended Long Lines authorized by this AWR are:

(1) Bridon American Dyform 18 rotation-resistant steel rope, 30-ft to 80-ft.

(2) 30-ft polyester sling (NSN 1670-01-388-3917), up to 70-ft (NSN 1670-01-388-3965).

(3) Up to 80-ft Plasma 12 Strand (5/8inch diameter) This line has a working load limit of

6425 lbs; therefore, buckets with a capacity greater than 680 gallons shall be adjusted so that their gross weight CANNOT exceed 6425 lbs. (weight for 80ft line is 8.5lbs)

j. The HH-60A/L helicopters may utilize the SEI Industries Bambi Water Buckets with electric or manual deployment release. Optional installation and operation of Sacksafoam I, II and

III, Fire Fighting Enhancement System, Bambi Bucket Recovery Device, and Long Lines (listed above) are also authorized. The plastic foam tank (reference 11) will be secured as cargo IAW

Chapter 6, Section VI, of reference 24.

5. Torrentula Valve Remote Power Supply (RPS):

WARNING

There is potential for static shock from use of the RPS. Ensure that the grounding cable (reference 38) is properly connected to an adequate metallic grounding point.

a. Operate and maintain IAW reference 33.

b. When installed, the RPS shall be floor-mounted with tie down straps IAW chapter 6, Cargo

Loading, of reference 1 or 24. Connect the RPS grounding cable between the RPS charging receptacle and an adequate metallic grounding point.

6. Bambi MAX buckets with Bambi Power Pack:

a. Bambi MAX buckets shall be installed and maintained IAW references 35 and 36.

b. When installed, the Power Pack shall be operated IAW reference 37, and floor-mounted with tie down straps IAW chapter 6, Cargo Loading, of reference 1 or 24.

7. Alternate power connection and control for operation of Bambi Bucket and/or remote hook with Long Line may be fabricated and operated IAW reference 39. CMWS flares shall not be installed while this configuration is installed.

8. If the configuration of this helicopter is changed by the application of a Modification Work

Order (MWO), which is considered standard equipment, subsequent to the installation of non-standard equipment, i.e. generally speaking, non standard equipment is not described by the

UH-60 Operator’s Manual or MWO, the nonstandard equipment may result in either physical or electrical conflict with the standard MWO equipment. The installation of an MWO takes precedence over any installed non-standard equipment. When an approved MWO is applied to this aircraft during the existence of the non-standard equipment, additional testing and/or analysis may be required to support compatibility of standard and nonstandard equipment. If interference occurs, notify the POC for corrective actions.

9. Weight and Balance data can be found in references 2, 6, 7, 16, 26, 27 and 33 through 37.

Appendix C. Inspections, Maintenance, and Logbook Instructions:

1. A 10 hour/14 day visual inspection shall be made of the subject installation to ensure that no progressive structural deterioration is occurring, that there is no loss of security, and that no damage to the host helicopter exists. Any occurrence of the preceding shall be corrected prior to further flight operations.

2. A qualitative EMC check, IAW reference 10 or 25, shall be conducted on at least one aircraft of each different configuration, prior to first flight with the newly installed equipment. A copy of the completed checklist shall be provided to usarmy.redstone.rdecom-amrdec.mbx.ae-u-tts@mail.mil.

3. Any/all logistics support required for such equipment/system installation must be established and maintained by the operating unit with appropriate, locally established, support activities. Parts needed for this modification may not be available in the supply system. Your activity/facility must locally procure/manufacture the modification parts (plus any additional spare parts). This

Airworthiness Release is not authorization to procure any material or sources "Sole Source."

4. In the event any operating limits established by this release is exceeded, in addition to the normal entry on DA Form 2408-13, appropriate inspections for security and condition of modifications shall be performed prior to next flight. Any incident or malfunction of the aircraft suspected of being related to these configuration modifications shall be reported immediately to the POC.

5. This helicopter shall be returned to standard configuration prior to transfer or turn-in to an overhaul facility.

6. Logbook Entries:

a. In accordance with Department of the Army (DA) Pamphlet 738-751, the following entries shall be made on the DA Form 2408-13-1 and shall be perpetuated on each form during the period of installation or until superseded by another Airworthiness Release, or until reason for limitation is removed:

(1) Place a circled "X" in the Status block IAW DA Pamphlet 738-751. In the

Faults/Remarks block, make the following entry: "Operate within limitations and restrictions specified in AWR 1054, dated 6 Sep 17."

mailto:usarmy.redstone.rdecom-amrdec.mbx.ae-u-tts@mail.mil

(2) Place a dash in the Status block to be followed in the Faults/Remarks block with

"One-time EMC check required prior to the first flight with new equipment installed IAW AWR

1054, dated 6 Sep 17."

(3) Deleted

(4) Place a dash in the Status block to be followed in the Faults/Remarks block with the following entry: "Perform visual inspection as required by AWR 1054, dated 6 Sep 17."

(5) For installation at hoist connector P227, (Appendix B, paragraph 2e): Place a circled

"X" in the Status block to be followed in the Faults/Remarks block with the following entry:

"Aircraft is restricted from use of the Bambi Bucket prior to installation of 15 amp circuit breaker modification as required by AWR 1054, dated 6 Sep 17."

b. For Army Materiel Status System (AMSS) or DA Form 1352 reporting purposes, the above write-ups shall not cause the aircraft to be reported as Partially Mission Capable (PMC). Aircraft which are nonstandard configured and operating under this release may be reported as Fully

Mission Capable (FMC).

c. The aircraft DA Form 2408-15 shall be annotated to cite this Airworthiness Release by subject and date. The 2408-15 shall be annotated to reflect temporary installations as well as permanent changes to configuration.

d. The EMC check required in Appendix C of this AWR need only be performed on one aircraft of each different configuration. The successful completion of the check for a configuration shall be considered sufficient for all other similarly configured aircraft. Annotate the DA Form

2408-15 and the ACTION block of DA Form 2408-13-1/1E to reflect that the EMC check has been successfully completed on another specified aircraft.

e. Unit Level Logistics System-Aviation (ULLS-A) users shall use the equivalent electronic form.

Appendix D. References:

1. Technical Manual 1-1520-237-10, Operator’s Manual for Army Models UH-60A, UH-60L and

EH-60A Helicopters, 25 Sep 09, with all changes.

2. Bambi Bucket Operations Manual (All Models), Version E, S.E.I. Industries, Jun 10.

3. Memorandum, Headquarters, 17th Aviation Brigade, KAAV-STD, 22 Feb 92, subject:

Airworthiness Release for CH-47D and UH-60 Aircraft Utilizing SEI Industries Bambi Bucket.

4. DATAFAX, UH-60 Section, CW2 Kunkle, HHC 1-4 Attack Battalion, 18 Mar 92.

5. Memorandum, Office of the Adjutant General, CAAO, 12 Jun 92, subject: Airworthiness

Release for UH-60 Helicopters with Bambi Bucket Installed.

6. Operator’s Manual, Sacksafoam I, Version C, S.E.I. Industries, LTD, Feb 08.

7. Sacksafoam II (Model 8044) Manual, Version C, S.E.I. Industries, LTD, Oct 08.

8. Memorandum, Stetson Troop, 4th Squadron, 3d Armored Cavalry Regiment, AFVF-H-R-S, 11 Feb 97, subject: Bambi Bucket.

9. Memorandum, HQ, USAATCOM, AMSAT-R-X, 17 Mar 97, subject: Proposed Revision 3 for

Bambi Bucket Installation on UH-60A/L Aircraft.

10. U.S. Army Aviation Engineering Directorate Qualitative EMC Checklist UH (EH)-60A/L

Black Hawk Helicopter, 27 May 15 (Enclosure 7).

11. Memorandum, Headquarters, 4th Brigade, 4th Infantry Division (Mechanized), AFZC-AV-CO, 7 Jul 00, subject: Request for Airworthiness Release (AWR) for Bambi Bucket

Fire Fighting Enhancement System.

12. Deleted

13. Product Bulletin, SEI Industries, Ltd., 9 Jul 98, subject: Operators Sacksafoam II and III

(Models SFF2-5598 and SFF3-6598) Manufactured Before July 1998 (Enclosure 1).

14. Deleted

15. Marine Recovery Device Manual, Version C, SEI Industries, LTD, Jun 09.

16. Operator’s Manual, Bambi Bucket with the Torrentula Valve, SEI Industries, LTD, Sep 99.

17. E-mail, NEARNG, 1SG Troy D. Johnson, 6 Jul 00, subject: Wiring and Power Source for

Bambi Bucket with Torrentula Valve Used on UH-60A.

18. Deleted

19. Product Bulletin, SEI Industries, Ltd., 16 Mar 99, subject: All Bambi Bucket Models; Control

Head linkage Stop Bolt (Enclosure 2).

20. Product Bulletin, SEI Industries, Ltd., 14 Mar 00, subject: All Bambi Bucket Models; Tripline

Bullet Enlargement (Enclosure 3).

21. DATAFAX, Michigan Army National Guard, Randy Bebee, 14 Aug 01, subject: Request for

Revision of AWR 920 R-2, 8 Jun 01.

22. Deleted

23. Memorandum, Military Department of Arkansas, DCSAVN-AMO, 25 Sep 02, subject:

Request for Revision to Bambi Bucket AWR 920.

24. Technical Manual 1-1520-253-10, Operator’s Manual for the HH-60A/L Helicopter, 30 Jun 10, with all changes.

25. US Army, AMCOM, Aviation Engineering Directorate Qualitative EMC Checklist, HH-60A/L Aircraft, 22 Nov 08 (Enclosure 4).

26. Operator’s Manual, Torrentula Valve Bambi Bucket with Model B Electrical Controls, Rev

J.2, SEI Industries, LTD, Sep 04.

27. Operator's Manual, PowerFill System & PowerFill II System, SEI Industries, LTD, Revision

B, May 02.

28. E-mail, SEI Industries, Mr. Bob Thompson, 1 May 03, subject: PowerFill Technical

Summary (Enclosure 5).

29. Deleted

30. Aviation Safety Alert, United States Department of Agriculture, Forest Service, No. 2004-4, 4 Apr 04, subject: Helicopter bucket operations (Enclosure 6).

31. Sacksafoam II (Model 5598) Manual, Version C, S.E.I. Industries, LTD, Jul 08.

32. Sacksafoam III Manual, Version C, S.E.I. Industries, LTD, Jul 08.

33. Operator’s Manual, Torrentula Valve Remote Power Supply, BTSN00769, SEI Industries, Ltd, Jun 04.

34. Bambi MAX Operations Manual, Version B, S.E.I. Industries, LTD, Apr 13.

35. Bambi MAX Service Manual, Models 1518-3542, Version C, S.E.I. Industries, LTD, Aug 14.

36. Bambi MAX Service Manual, Models 4453-7590, Version B, S.E.I. Industries, LTD, Aug 14.

37. Bambi Power Pack Manual, Version B, S.E.I. Industries, LTD, Jul 13.

38. Drawing 004335, Harness, Wire, H13, RPS, S.E.I. Industries, 7 Apr 14.

39. Alternate Power Connection (CMWS/Fire Bucket Interface) Schematic and Bill of Materials, 23 Apr 15 (Enclosure 8).

COORDINATION SHEET

SUBJECT: (AWR1054R18) This is revision 18 to fleetwide AWR 1054 for UH-60A/L and

HH-60A/L helicopters equipped with SEI Industries Bambi Water Buckets and various fire fighting accessories. Complete references are available upon request.

This revision adds the alternate power connection/junction box (CMWS power), which has been approved under TTS 160919A.

MFR: This revision WILL NOT impact maintenance/inspection requirements for the affected acft.

The point of contact for this AWR is Scott Oberman, 313-3142.

RDMR-AEA_________________________________________ DATE: _______

RDMR-AEF_________________________________________ DATE: _______

RDMR-AEP_________________________________________ DATE: _______

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AED Task Tracking System Number ______________45370L______________

UHPMO Concurrence/Approval________________________________