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Anti-icing and Biocidal Additive for Commercial Turbine Engine Fuel. The additive provides anti-icing
protection and functions as a biocide to kill microbial growths in aircraft fuel systems. Icing inhibitor conforming
to MIL-I-27686 shall be added to commercial fuel, not containing an icing inhibitor, during refueling
operations, regardless of ambient temperatures. Refueling operations shall be accomplished in accordance
with accepted commercial procedures. This additive (Prist or eq.) is not available through the Army
Supply System, but is to be locally procured when needed.
TM 1-1520-238-10
2-94 Change 6
Table 2-8. Approved Fuels -- continued
US Military Fuel
NATO Code No.
JP-4 (MIL-T-5624)
F-40 (Wide Cut Type)
JP-5 (MIL-T-5624) or JP-8 (MIL-T-83133)
F-44 or F-34 (High Flash Type)
FOREIGN FUEL NATO F-40 NATO F-44
Belgium BA-PF-2B
Canada 3GP-22F 3-6P-24e
Denmark JP-4 MIL-T-5624
France Air 3407A
Germany (West) VTL-9130-006 UTL-9130-0007/UTL 9130-010
Greece JP-4 MIL-T-5624
Italy AA-M-C-1421 AMC-143
Netherlands JP-4 MIL-T-5624 D ENG RD 2493
Norway JP-4 MIL-T-5624
Portugal JP-4 MIL-T-5624
Turkey JP-4 MIL-T-5624
United Kingdom (Britain) D. Eng RD 2454 D.Eng RD 2498
NOTE: COMMERCIAL FUEL LIMITATIONS
Anti-icing and Biocidal Additive for Commercial Turbine Engine Fuel. The additive provides anti-icing
protection and functions as a biocide to kill microbial growths in aircraft fuel systems. Icing inhibitor conforming
to MIL-I-27686 shall be added to commercial fuel, not containing an icing inhibitor, during refueling
operations, regardless of ambient temperatures. Refueling operations shall be accomplished in accordance
with accepted commercial procedures. This additive (Prist or eq.) is not available through the Army
Supply System, but is to be locally procured when needed.
TM 1-1520-236-10
Table 2-9. Approved Oils
Approved Domestic Commercial Oils for MIL-L-7808
Manufacturer’s Name Manufacturer’s Designation
American Oil and Supply Co. PQ Turbine Oil 8365
Humble Oil and Refining Co. ESSO/ENCO Turbo Oil 2389
Mobile Oil Corp. RM-184A/RM-201A
Approved Domestic Commercial Oils for MIL-L-23699
Manufacturer’s Name Manufacturer’s Designation
Americal Oil and Supply Co. PQ Turbine Lubricant 5247/
6423/6700/7731/8878/9595
Bray Oil Co. Brayco 899/899-G/899-S
Castrol Oil Co. Castrol 205
Chevron International Oil Co., Inc. Jet Engine Oil 5
Crew Chemical Corp. STO-21919/STO-21919A/STD 6530
W.R. Grace and Co. (Hatco Chemical Div.) HATCOL 3211/3611
Humble Oil and Refining Co. Turbo Oil 2380 (WS-6000)/2395
(WS-6495)/2392/2393
Mobile Oil Corp. RM-139A/RM-147A/Avrex S
Turbo 260/Avrex S Turbo 265
Mobile 254
Royal Lubricants Co. Royco 899 (C-915)/899SC/
Stauffer Jet II
Shell Oil Co., Inc. Aeroshell Turbine Oil 500
Shell International Petroleum Co., Ltd. Aeroshell Turbine Oil 550
Standard Oil Co., of California Chevron Jet Engine Oil 5
Stauffer Chemical Co. Stauffer 6924/Jet II
Texaco, Inc. SATO 7377/7730 TL-8090
Approved Foreign Commercial Oils for MIL-L-7808
Data not available at this time.
Approved Foreign Commercial Oils for MIL-L-23699
Data not available at this time.
2-95
CAUTION
TM 1-1520-238-10
2.55 PARKING.
Helicopter parking shall be in accordance with local directives
and the following minimum procedures: station
helicopter on as level a surface as possible; set
wheel brakes; lock tail wheel; turn all switches off; disconnect
external power; chock wheels; secure rotor
blades; attach static ground wire, and install engine inlet,
exhaust, and pitot covers.
2.55.1 Protective Covers. Protective covers (fig 2-47)
prevent damage from foreign objects and snow and water
buildup to vital areas. Ail protective covers are part
of the helicopter flyaway kit. The kit may be stored in
the equipment stowage bay during flight. Covers are
installed whenever the helicopter is on the ground for
an extended period of time, or if severe environmental
conditions such as ice or dust exist.
2.56 GROUND AIR SOURCE.
An external air receptacle (fig 2-46) under the No. 1 engine
nacelle provides an attachment point for an external
air line to start either engine or accomplish maintenance
functions on the helicopter. An external air
source that provides 40 psig and 30 pounds-per-minute
air flow is required to pressurize the system for engine
start. The maximum pressure from a ground source
shall not exceed 50 psig.
2.57 TOWING.
The helicopter is towed by attaching a tow bar to the
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