(73)
AMM 29-33-00/501, Hydraulic Fluid Quantity Indicating System
(74)
AMM 29-35-00/501, Hydraulic Reservoir Pressure Indication System
(75)
AMM 30-31-00/501, Pitot Static Probe Anti-icing
(76)
AMM 30-42-03/401, Windshield Wiper System
(77)
AMM 30-43-00/201, Windshield Rain Repellant System
(78)
AMM 32-00-15/201, Landing Gear Door Ground Operations and Locking Procedures
(79)
AMM 32-00-20/201, Landing Gear Downlocks
(80)
AMM 32-12-00/501, Main Gear Door
(81)
AMM 32-20-00, Nose Landing Gear and Doors
(82)
AMM 32-21-09/401, Nose Gear Torsion Links
(83)
AMM 33-51-07/201, Emergency Light Batteries
(84)
AMM 34-11-00/501, Pitot Static System
(85)
AMM 35-11-00/201, Crew Oxygen System
(86)
AMM 35-11-51/401, Crew Oxygen Mask/Stowage Box
(87)
AMM 38-32-00/501, Toilet System
(88)
AMM 49-11-00/201, Auxiliary Power Units
(89)
AMM 52-11-30/601, Emergency Power Reservoir
(90)
AMM 71-00-00/201, Power Plant
C. Procedure
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MAINTENANCE MANUAL
S 862-082
WARNING: WHEN THE STATIC PORTS/PITOT 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 STATIC PORTS/PITOT PROBES ARE COVERED. FAILURE TO OBSERVE AND REMOVE COVERINGS OVER STATIC PORTS/PITOT 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 PROBE COVERS ARE IN GOOD WORKING CONDITION
_______ WITH NO EVIDENCE OF DAMAGE, ESPECIALLY FRAYING AROUND THE COVER OPENING. FRAYED FIBERS FROM THE COVER COMBINED WITH OTHER 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 probes are given in Normal Parking - Maintenance Practices (AMM 10-11-01/201).
(2)
Use the tables that follow to store the airplane.
S 552-073
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757
MAINTENANCE MANUAL
~............................................................................... | | Procedures Repeat Intervals (Days) | | ....................................... | | | | | | | | | As| | Item | Initial | 7 | 14| 30| 60| 90|180|Rqd| ................................................................................. | EXTERNAL SURFACE PROTECTION | | | | | | | | |
___________________________ ................................................................................. | Inspection Criteria | | | | | | | | |
___________________ .................................................................................
| 1. Remove the dirt and contamination | | | | | | | | X |
| you can see on the surfaces that | | | | | | | | |
| are not painted. | | | | | | | | |
| The maximum time recommended between | | | | | | | | |
| the contamination and the cleaning | | | | | | | | |
| is 24 hours (AMM 12-25-01). | | | | | | | | |
| | | | | | | | | |
|
NOTE:____ When the airplane skin | | | | | | | | |
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