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 A.  General
 (1)  When adding fuel, you must use these requirements:
 (a)  Make sure the fuel temperature is at least 6°F (3°C) above the fuel freeze point or -45.4°F (-43°C), whichever is higher. Use the ASTM method to determine the freeze point.
 NOTE: The Fuel Quantity Indicator on the wing fuel station can
____ indicate slowly or not show numbers in extreme cold conditions. Use an external fuel flow meter to show the amount of fuel added to the airplane.
 (b)  
Use fuels that meet specification ASTM D1655; or

 (c)  
Use fuels that meet specification GOST 10277: 1) RT (PT, Russian spelling) 2) TS-1 (TC-1, Russian spelling)

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737-300/400/500MAINTENANCE MANUAL
 (d)  Approved fuel additives are:
 NOTE: Adding an anti-icing fuel additive may help in the
____
 sumping of the fuel tanks.

 1)  Fuel Additive, specification GOST 8313, Fluid I (also known as Fluid E) a) Fluid I may be used at a mixture of no more than 0.15
 percent by volume. 2) Fuel Additive, specification TU-6-10-1458, Fluid I-M (also known as Fluid E- Methanol).
 NOTE: This fuel additive is not approved for GE engines.
____
 a) Fluid I-M may be used at a mixture of no more than 0.15 percent each, by volume. 3) Fuel Additive, specification GOST 17477, Fluid TGF.
 NOTE: This fuel additive is not approved for GE engines.
____
 a) Fluid TGF may be used at a mixture of no more than 0.15 percent by volume. 4) Fuel Additive, specification TU-6-10-1457, Fluid TGF-M (also known as Fluid TGF- Methanol).
 NOTE: This fuel additive is not approved for GE engines.
____
 a)  Fluid TGF-M may be used at a mixture of no more than
 0.15 percent each, by volume.
 B.  References
 (1)  
AMM 09-10-00/201, Tow the Airplane

 (2)  
AMM 10-11-00/201, Park the Airplane (Normal Parking)

 (3)  
AMM 10-12-00/201, Prepare the Airplane for Storage for More Than 7 Days

 (4)  
AMM 12-13-21/301, CSD or VSCF Generator/Converter Oil Fill

 (5)  
AMM 12-14-00/301, Potable Water System Drain

 (6)  
AMM 12-17-00/301, Waste Tank Servicing

 (7)  
AMM 12-33-01/301, Cold Weather Maintenance Procedure

 (8)  
AMM 24-31-11/201, Main Battery Removal/Installation

 (9)  
ON AIRPLANES WITH AN APU BATTERY;
 AMM 24-31-11/201, APU Battery Removal/Installation

 (10)
 AMM 33-51-51/201, Power Supply - Battery Pack Replacement,
 Power Supply - Power Supply Replacement

 

 C.  Consumable Materials
 (1) D00109 Oil - Aircraft turbine engine, synthetic base - MIL-L-7808
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737-300/400/500MAINTENANCE MANUAL
 D. Access
 (1)  
Location Zones
 100 Lower Half of Fuselage
 200 Upper Half of Fuselage
 300 Empennage
 400 Powerplant and Nacelle Struts
 500 Left Wing
 600 Right Wing
 700 Landing Gear and Landing Gear Doors
 800 Doors

 (2)  
Access Panel
 1201L Electronic Equipment Access Door

 

 E. Procedure
 S 423-025
 (1)  Install the inlet and exhaust covers.
 NOTE: Keep the engine covers in a warm location before you install
____ them on the airplane. Covers that are cold or frozen may be difficult to install, and may freeze to the engine inlet and exhaust.
 At very low ambient air temperatures, the time for the engine to cool to -40°F (-40°C) can be greatly increased by the use of engine inlet and exhaust covers.
 S 553-026
 (2)  
Do the Cold Weather Maintenance procedure (AMM 12-33-01/301).
　
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