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时间:2011-03-30 06:41来源:蓝天飞行翻译 作者:航空
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4.  Restore Airplane to Its Usual Condition for Return to Service
WARNING:  FAILURE TO REMOVE COVERS FROM PITOT PROBES BEFORE FLIGHT MAY CAUSE LARGE ERRORS IN AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS, WHICH MAY LEAD TO LOSS OF SAFE FLIGHT.
CAUTION:  REMOVE ALL COVERS. ENGINES SHOULD NOT BE OPERATED WITH COVERS IN PLACE BECAUSE THE COVERS CAN COME OFF AND DAMAGE THE ENGINES.
A.  Remove the covers from the following components:
(1) 
 Pitot probes

(2)  
Engine inlet and turbine exhaust


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May 01/03  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  10-11-0 Page 211 


B. Remove the “PITOT PROBES COVERED” tag from the left control in the flight deck.
WARNING:  FAILURE TO REMOVE BARRICADE TAPE AND VINYL ADHESIVE TAPE FROM THE STATIC PORTS BEFORE FLIGHT MAY CAUSE LARGE ERRORS IN AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS, WHICH MAY LEAD TO LOSS OF SAFE FLIGHT.
CAUTION:  REMOVE ALL BARRICADE TAPE AND VINYL ADHESIVE TAPE. ENGINES SHOULD NOT BE OPERATED WITH COVERINGS IN PLACE BECAUSE THE COVERINGS CAN COME OFF AND DAMAGE THE ENGINES.
C. Remove all barricade tape and vinyl adhesive tape from the static ports.
D. Remove the “STATIC PORTS COVERED” tag from the left control wheel in the flight deck.
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10-11-0 Page 212  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 01/98 


PROLONGED PARKING - MAINTENANCE PRACTICES
1.  General
A.  If you will park the airplane for more than 7 days, do this procedure to help prevent deterioration of the airplane. This includes the structure, finish, or system components in an area that is open to the weather.
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.
2.  Airplane Storage Procedure
A.  Consumable Materials
(1)  
Corrosion Preventive Compound - MIL-C-16173, Grade 2 (Ref. 20-30-21)

(2)  
Insulation Covering - BMS 8-142, Type 1 Class 3 (Ref. 20-30-51)

(3)  
Grease - BMS 3-24 (Ref. 20-30-21)

(4)  
Grease - Aeroshell No. 5 (Ref. 20-30-21)

(5)  
Corrosion Preventive Compound - BMS 3-23, Type II (Ref. 20-30-21)

(6)  
Grease - BMS 3-33 (Ref. 20-30-21)

(7)  
Grease - MIL-G-25013 (Ref. 20-30-21)

(8)  
Hydraulic Fluid Assembly Lubricant - BMS 3-11 (Ref. 20-30-21)

(9)  
Hydraulic System Lubricant - MCS-352 (Ref. 20-30-21)

(10)
Jet Fuel Additive -PFA55MB (MIL-I -27686) (Ref. 20-30-51)

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

(12)
Oil, Lubricating - MIL-L-7808 (Ref. 20-30-21)

(13)
Oil, Lubricating - MIL-L-23699 (Ref. 20-30-21)

(14)
Protective Coating -Ardrox 306-N (alkaline removable) (Ref. 20-30-41)

(15)
Protective Coating -Aztec 649 (alkaline removable) (Ref. 20-30-41)

(16)
Remover - Ardrox 7050-W (water base)

(17)
Tape - Aluminum Foil (Ref. 20-30-51)

(18)
Tape - 3M No. 471 or Permacel SVP224


B.  Reference
(1) 
 9-10-0, Towing

(2)  
12-11-0, Fuel Servicing

(3) 
 12-14-0, Water Servicing

(4) 
 12-15-21, Oxygen Servicing

(5)  
12-15-31, Main Landing Gear Shock Strut Servicing

(6)  
12-15-41, Nose Landing Gear Shock Strut Servicing

(7)  
12-15-51, Landing Gear Tire Servicing

(9)
12-17-0, Toilet Servicing

(10)
12-21-11, Main Landing Gear Lubrication

(11)
12-22-21, Rudder Control System Lubrication

(12)
12-22-51, Trailing Edge Flap System Lubrication

(13)
12-22-71, Leading Edge Slat System Lubrication

(14)
12-26-0, Cable Lubrication

(15)
12-40-0, Cleaning and Washing

(16)
20-30-21, Lubricants

(17)
20-30-31, Cleaners and Polishes

(18)
20-40-11, Static Grounding

(19)
24-31-11, Storage Battery

(20)
30-42-0, Windshield Wiper System

(21)
30-43-0, Rain Repellent System

(22)
32-00-01, Landing Gear Downlocks Groundlock Assembly

(23)
49-11-0, Auxiliary Power Unit

(24)
71-00-1, Power Plant

 


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May 01/01  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  10-12-0 Page 201 
 
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