BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~............................................................................... | | Procedures Repeat Intervals (Days) | | ....................................... | | | | | | | | | As| | Item | Initial | 7 | 14| 30| 60| 90|180|Rqd| .................................................................................
| | | | | | | | | |
| POWER PLANT AND APU___________________ | | | | | | | | |
| | | | | | | | | |
| 1. Refer to AMM 71-00-03/201 for the | | | | | | | | |
| steps to store the engine. | | | | | | | | |
| 2. Refer to AMM 49-11-00/201 for the | | | | | | | | |
| steps to store the APU. | | | | | | | | |
2.........................................….........…...…...…...…...…...…...…...1
TASK 10-12-00-632-001
3. Put the Airplane to a Serviceable Condition After Storage
_________________________________________________________
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. 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 12-11-00/301, Pressure Fueling
(5)
AMM 12-12-00/301, Hydraulic System
(6)
AMM 12-14-00/301, Potable Water System
(7)
AMM 12-15-31/301, Main Gear Shock Strut
(8)
AMM 12-15-41/301, Nose Gear Shock Strut
(9)
AMM 12-15-51/301, Landing Gear Tires
(10)
AMM 12-15-11/301, Parking Brake Accumulator
(11)
AMM 12-15-21/301, Oxygen
(12)
AMM 12-16-01/301, Rain Repellent Container
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10-12-00
ALL ú ú 02 Page 224 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(13)
AMM 12-17-00/301, Toilet
(14)
AMM 12-22-21/301, Rudder and Rudder Trim Control System
(15)
AMM 12-21-11/301, Aileron and Aileron Trim Control System
(16)
AMM 12-22-81/301, Speed Brake
(17)
AMM 12-22-51/301, Trailing Edge Flap System
(18)
AMM 12-22-61/301, Spoiler Control System
(19)
AMM 12-21-21/301, Nose Landing Gear
(20)
AMM 12-21-11/301, Main Landing Gear
(21)
AMM 12-25-31/301, Cargo Door
(22)
AMM 12-25-11/301, Aft Entry Door
(23)
AMM 12-25-91/301, Emergency Exit Hatch
(24)
AMM 12-25-21/301, Fwd Entry Door
(25)
AMM 12-25-41/301, Galley Door
(26)
AMM 12-25-51/301, Service and Access Door
(27)
AMM 12-40-00/201, Airplane Servicing (Washing and Cleaning)
