Jan 20/82 51-21-91
Page 702A/702B
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
DESCRIPTION OF AREA
FUSELAGE LAP JOINTS INTERNAL
STRINGERS, FRAMES AND FUSELAGE SKIN IN CROWN (STRINGER 10 AND ABOVE)
ALL STRINGERS, FRAMES AND FUSELAGE SKIN BELOW CARGO COMPARTMENT FLOORS
BODY UPPER LOBE
FUSELAGE INTERNAL PRESSURE AREA
METHOD OF BMS 3-23 APPLICATION
APPLY TO INTERNAL EDGE OF LAP JOINTS, RIVETS AND STRINGER SKIN FAYING SURFACE
WARNING: ALLOW SOLVENT TO EVAPORATE BEFORE REAPPLYING INSULATION BLANKETS. BMS 3-23 SOAKED BLANKETS ARE A POTENTIAL HAZARD.
REMOVE INSULATION BLANKETS (REF 25-52-141). MASK OXYGEN LINES AND SPRAY ALL EXPOSED STRUCTURE.
WARNING: BMS 3-23 SHOULD NOT BE SPRAYED ON OXYGEN LINES OR FITTINGS ALLOW SOLVENT TO EVAPORATE BEFORE REINSTALLING BLANKETS. BMS 3-23 SOAKED INSULATION BLANKETS ARE A POTENTIAL FIRE HAZARD.
REMOVE INSULATION BLANKETS (REF 25-52-141). SPRAY ALL EXPOSED STRUCTURE.
WARNING: ALLOW SOLVENT TO EVAPORATE BEFORE REINSTALLING INSULATION BLANKETS. BMS 3-23 SOAKED INSULATION BLANKETS ARE A POTENTIAL FIRE HAZARD.
WHEN REINSTALLING INSULATION BLANKETS, PROVIDE GAP BETWEEN BLANKET AND SKIN (REF 25-52-141). INSPECT CONDITION OF BONDED DOUBLERS WHILE AREA IS EXPOSED.
APPLY TO BODY UPPER LOBE ABOVE WL 208.1 BETWEEN STA 260 AND STA 1016, INCLUDING FORWARD FACE OF STA 1016 BULKHEAD.
APPLY TO STRUCTURE LEFT AND RIGHT HAND SIDE BETWEEN WL 208.1 AND CARGO DECK, STA 363 TO STA 520 AND STA 727 TO STA 907 INCLUDING FORWARD SIDE OF STA 907 FRAME.
APPLY TO PRESSURE SIDE OF BODY SKIN BETWEEN BODY STA 227.8 AND BODY STA 270 BELOW WL 208.1.
APPLY TO SKIN AND STRINGERS BETWEEN BODY STA 1040 AND BODY STA 1088 INCLUDING THE FORWARD FACE OF STA 1088 BULKHEAD.
Jan 20/82 51-21-91
Page 703
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
DESCRIPTION OF AREA
ELECTRONIC COMPARTMENT
AIR CONDITIONING BAY
FLOOR BEAMS, PASSENGER DECK
TOILET AND GALLEY AREAS
AFT PRESSURE BULKHEAD
SEAT TRACKS
METHOD OF BMS 3-23 APPLICATION
SPRAY FUSELAGE SKIN, FRAMES, AND STRINGERS IN BELLY. SPRAY ELECTRONIC BAY DOOR AND DOOR FRAME.
NOTE: INSULATION BLANKETS MUST BE LIFTED.
WARNING: ALLOW SOLVENT TO EVAPORATE BEFORE REINSTALLING INSULATION BLANKETS. BMS 3-23 SOAKED INSULATION BLANKETS ARE A FIRE HAZARD.
SPACE BLANKETS AWAY FROM SKIN (REF 25-52-141).
APPLY TO ENTIRE SURFACE OF FRONT SPAR, FUSELAGE SKIN, STRINGERS AND FRAMES. DO NOT APPLY TO DUCTING. COVER ALL STRUCTURE BELOW WL 208 BETWEEN STA 520 AND 540.
MASK OXYGEN LINES AND APPLY BMS 3-23 TO FACES AND FLANGES OF FLOOR BEAMS UNDER GALLEYS, TOILETS AND ENTRY DOORS.
WARNING: BMS 3-23 MUST NOT BE SPRAYED ON OXYGEN LINES OR FITTINGS AS MIXTURE IS POTENTIALLY EXPLOSIVE.
SPRAY STRUCTURE BELOW TOILET AND GALLEY AREAS INCLUDING TOILET COMPARTMENT PANS. SPRAY INSIDE SURFACE OF AFT PRESSURE BULKHEAD.
SPRAY ENTIRE AFT FACE OF STA 1016 PRESSURE BULKHEAD AND TO ALL SKIN AND STRINGERS BETWEEN BODY STA 1016 AND 1040.
MASK CARPETS AND APPLY BMS 3-23 TO INSIDE AND TOP SURFACES OF SEAT TRACK INCLUDING TRACK UNDER GALLEYS.
APPLY TO CAVITY OF ALL SEAT TRACKS BETWEEN STA 344 AND STA 947.
51-21-91 Jan 20/82
Page 704
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
DESCRIPTION OF AREA
EMPENNAGE EXTERNAL SKIN - PAINTED SURFACES ONLY
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737 AMM 飞机维护手册 结构 STRUCTURES(22)