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 B.  The steps that are necessary to protect a parked airplane and the repeat intervals are shown in the Airplane Storage Procedure. To put the airplane in a serviceable condition, do the steps in the Put the Airplane to a Serviceable Condition After Storage procedure.
 TASK 10-12-00-622-002
 2.  Airplane Storage Procedure__________________________
 A.  General
 WARNING: WHEN THE STATIC PORTS/PITOT STATIC PROBES ARE COVERED, MAKE
_______ SURE THAT CONDITION IS VISIBLE FROM THE GROUND. IN ADDITION, ATTACH TAGS TO THE LEFT CONTROL WHEEL IN THE FLIGHT DECK AS REMINDERS THAT THE STATIC PORTS/PITOT STATIC PROBES ARE COVERED. FAILURE TO OBSERVE AND REMOVE COVERINGS OVER STATIC PORTS/PITOT STATIC PROBES BEFORE FLIGHT MAY CAUSE LARGE ERRORS IN AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS, WHICH MAY LEAD TO LOSS OF SAFE FLIGHT.
 CAUTION: MAKE SURE THE PITOT-STATIC PROBE COVERS ARE IN GOOD WORKING
_______ CONDITION WITH NO EVIDENCE OF DAMAGE, ESPECIALLY FRAYING AROUND THE COVER OPENINGS. FRAYED FIBERS FROM THE COVER COMBINED WITH SUBSTANCES SUCH AS DIRT, GREASE AND FLUIDS CAN CAUSE OBSTRUCTION IN THE PROBE.
 (1)  The procedure for attaching static port covers to the airplane and the locations of the static ports and pitot static probes are given in Normal Parking - Maintenance Practices (AMM 10-11-00/201)
 B.  Consumable Materials
 (1)  
Corrosion Preventive Compound - MIL-C-16173, Grade 2 (AMM 20-30-21/201)

 (2)  
G00087 Insulation Covering - BMS 8-142, Type 1 Class 3 (AMM 20-30-51/201)

 (3)  
Grease - BMS 3-24 (AMM 20-30-21/201)

 (4)  
Grease - Aeroshell No. 5 (AMM 20-30-21/201)

 (5)  
Corrosion Preventive Compound - BMS 3-23, Type II (AMM 20-30-21/201)

 (6)  
Grease - MIL-G-23827 (AMM 20-30-21/201)

 (7)  
Grease - MIL-G-25013 (AMM 20-30-21/201)

 (8)  
Hydraulic Fluid Assembly Lubricant - BMS 3-11 (AMM 20-30-21/201)

 (9)  
Hydraulic System Lubricant - MCS-352 (AMM 20-30-21/201)

 (10)
 Jet Fuel Additive - PFA55MB (MIL-I-27686) (AMM 20-30-51/201)

 (11)
 Jet Fuel Additive (Biocide) - Biobar JF

 (12)
 Oil, Lubricating - MIL-L-7808 (AMM 20-30-21/201)

 (13)
 Oil, Lubricating - MIL-L-23699 (AMM 20-30-21/201)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 10-12-00
 ALL  ú ú 01 Page 201 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (14)
 Protective Coating - Ardrox 306-N (alkaline removable) (AMM 20-30-41/201)

 (15)
 Remover - Ardrox 302N (water base) (AMM 20-30-41/201)

 (16)
 Tape - Aluminum Foil (AMM 20-30-51/201)

 (17)
 Tape - 3M No. 471 or Permacael SVP 224 (AMM 20-30-51/201)

 C. References
 (1)
AMM 07-11-11/201, Jacking Airplane

 (2)
AMM 07-11-31/201, Jacking Airplane Axle

 (3)
AMM 09-10-00/201, Towing

 (4)
AMM 10-11-00/201, Normal Parking

 (5)
AMM 12-11-00/301, Pressure Fueling

 (6)
AMM 12-12-00/301, Hydraulic System

 (7)
AMM 12-14-00/301, Potable Water System

 (8)
AMM 12-15-31/301, Main Gear Shock Strut

 (9)
AMM 12-15-41/301, Nose Gear Shock Strut

 (10)
 AMM 12-15-51/301, Landing Gear Tires

 (11)
 AMM 12-15-11/301, Parking Brake Accumulator

 (12)
 AMM 12-15-21/301, Oxygen

 (13)
 AMM 12-16-01/301, Rain Repellent Container

 (14)
 AMM 12-17-00/301, Toilet

 (15)
 AMM 12-22-21/301, Rudder and Rudder Trim Control System

 (16)
 AMM 12-21-11/301, Aileron and Aileron Trim Control System

 (17)
 AMM 12-22-81/301, Speed Brake

 (18)
 AMM 12-22-51/301, Trailing Edge Flap System

 (19)
 AMM 12-22-61/301, Spoiler Control System

 (20)
 AMM 12-21-21/301, Nose Landing Gear

 (21)
 AMM 12-21-11/301, Main Landing Gear

 (22)
 AMM 12-25-31/301, Cargo Door

 (23)
 AMM 12-25-11/301, Aft Entry Door

 (24)
 AMM 12-25-91/301, Emergency Exit Hatch

 (25)
　
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