Boeing 757-225

Service difficulty reports · 1,988

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '757225'
  ORDER BY difficulty_date DESC"

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SDR BB06013Strap · unsecureON CLIMB-OUT, CREW REPORTED BANGING NOISE OUTSIDE OF L1 DOOR. FLIGHT RETURNED TO CLT. MAINTENANCE FOUND THE L1 DOOR SAFETY STRAP OUTSIDE OF DOOR. MAINTENANCE STOWED THE STRAP AND PERFORMED AN OVERWEIGHT LANDING INSPECTION. NO DEFECTS WERE NOTED.Feb 16, 2006 · N620AU · Boeing 757225 · Passenger/Crew DoorsSDR AWXA200600452Seat Track · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT BS 1340+10" TO BS 1402, WL 208.1 AND BL 24.75L. CORROSION WAS FOUND OUT OF BOEING 757-200 SRM LIMITS. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 757-200 SRM 53-00-52-2R. RECEIVED NEW SEATFeb 13, 2006 · N913AW · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600297Stringer · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON STRINGER 28R AT FWD CARGO COMPARTMENT, BS 561. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 28R IAW BOEING 757-200 SRM 53-00-03-2R FIG 201. FABRICATED ANGLE, FILLER AND CHANNELS IAW BOEING 757-200 SRM 53-00-0Feb 13, 2006 · N913AW · Boeing 757225 · Fuselage Main, Longeron/StringerSDR AWXA200600296Plate · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON PLATE LOWER ANGLE AT BS 1357.5, BL 64R IN THE PAX CABIN. MAINTENANCE REMOVED AND INSTALLED NEW PLATE IAW BOEING 757-200 SRM 51-10-02 FROM BS 1357 TO BS 1360 AT BL 64R.Feb 13, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060228Structure · crackedFOUND CRACK R2 DOOR BEHIND UPPER FWD DOOR STOP. TRIMMED OUT DAMAGE, REPAIR DOUBLERS, PRIME AND INSTALL IAW EA 97407, DEFECT SIZE: 3".Feb 13, 2006 · N608AU · Boeing 757225 · Service DoorsSDR USAA060225Stringer · corrodedAFT CARGO, STA 1440, S-26R, WL 138. REMOVED & REPLACED STRINGER END ANGLE PER SRM 52-40-02, DEFECT SIZE: 1"L X 1"W X .011"D.Feb 10, 2006 · N600AU · Boeing 757225 · Fuselage Main, Longeron/StringerSDR USAA200602001Structure · crackedA 3 INCH CRACK FOUND AT R2 DOOR BEHIND UPPER FWD DOOR STOP. TRIM OUT DAMAGE, HFEC EDGES, FABRICATE FILLERS & REPAIR DOUBLERS, ALODINE, PRINT & INSTALL PER EA 97407.Feb 7, 2006 · N608AU · Boeing 757225 · Service DoorsSDR AWXA200600458Web · corrodedSAL - MAJOR REPAIR - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON WEB AT BS 1329.5 AND BS 1347 AT BL 64L. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW WEB FROM BS 1320 TO BS 1360 AT BL 64L IAW BOEING 757-2Feb 4, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600457Web · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON WEB AT BS 1620 TO BS 1640 AT BL 60L. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW WEB AT BS 1620 TO BS 1640 AT BL 60L IAW BOEING 757-200 SRM 51-40-02.Feb 4, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600454Angle · corrodedSAL - DURING C11 CHECK LEVEL 2 CORROSION FOUND AROUND NUT PLATE ON ANGLE AT BS 1667.5 AND BL 56.5L. MAINTENANCE REPAIRED ANGLE AT STA 1667.5 TO BS 1680.5 IAW BOEING 757-200 SRM 51-70-11 FIG 1.Feb 4, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600436Skin · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON INTERNAL SKIN AT AFT BODY FAIRING FUSELAGE FROM BS 1825 TO BS 1844 BETWEEN STR 25L AND STR 25R. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE REPAIRED FUSELAGE SKIN PANEL AT THE AFT BODY FAIRING FROM Feb 4, 2006 · N913AW · Boeing 757225 · Fuselage Main, Plate/SkinSDR AWXA200600435Skin · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON INNER SKIN OF 313AL SERVICE DOOR, ELEVATOR ACCESS, BETWEEN BS 1880 AND BS 1885.2 FROM STR 25L TO STR 25R AT WL 199.1. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE BOEING 757-200 SRM. MAINTENANCE BLENDED OUT THEFeb 4, 2006 · N913AW · Boeing 757225 · Fuselage Main, Plate/SkinSDR AWXA200600434Structure · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION ON INNER CHORD AT BS 1351 AND BL 64L. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 SRM 53-60-13-1A. DAMAGED AREA WAS CUT OUT IAW BOEING 757-200 SRM 51-70-11-06. FABRICATED REPAIR ANGLE IAW BOFeb 4, 2006 · N913AW · Boeing 757225 · Fuselage Main, StructureSDR AWXA200600451Floorbeam · corrodedDURING C11 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOOR BEAM AT BS 1661, WL 208.10 AND BL 21R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 757200 SRM 757-200 53-00-51-1A-1. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 757-200 SRM 53-00-51-2R5 PAGE 1 DETFeb 3, 2006 · N913AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200600459Skin · crackedSAL - MAJOR REPAIR - DURING C11 CHECK DISCOVERED LEFT ELEVATOR UPPER SKIN CRACKED, 2.5 INCHES, AT ELEVATOR STATION 52.55 + 10 INCHES, INBOARD SIDE. MAINTENANCE REMOVED DAMAGED AREA AND PREPPED FOR REPAIR IAW BOEING 757-200 SRM 51-70-17-0G. FABRICATED CORE ANFeb 3, 2006 · N913AW · Boeing 757225 · Elevator, Plate/SkinSDR AWXA200600453Angle · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON ANGLE AT BS 1688.8 WL 208.10 AND BL 6R. NO ALLOWABLE LIMITS WERE FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED FABRICATED ANGLE AT BS 1683.8, WL 208.10 AND FROM BL 6L TO BL 6R IAW BOEING 75Feb 3, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600450Floorbeam · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON SUPPORT AT BS 1683.8, WL 208.10 AND FROM BL 6L TO BL 6R. NO ALLOWABLE LIMITS WERE FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED FABRICATED SUPPORT AT BS 1683.8, WL 208.10 AND FROM BL 6L TO Feb 3, 2006 · N913AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200600449Support · corrodedSAL - MAJOR REPAIR - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON SUPPORT AT BS 1688 TO BS 1715 AND BL 6L. NO ALLOWABLE LIMITS WERE FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED FABRICATED SUPPORT AT BS 1688 TO BS 1715 AND BL 6L IAW BOEING Feb 3, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600448Floor Skin · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON DECK PLATE AT STA 1681.8 AND BL 13R. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 757-200 SRM 53-00-51-1A. MAINTENANCE REPAIRED PANEL BY REMOVING DAMAGE AND INSTALLING DOUBLER IAW BOEING 757-200 SRM 53-60-51-2R.Feb 3, 2006 · N913AW · Boeing 757225 · Fuselage Floor PanelSDR AWXA200600433Sill · corrodedSAL - MAJOR REPAIR - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON SILL (DECK PLATE) AT BS 1661+2 INCHES AND BL 57R. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 757-200 51-70-11-Feb 3, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600340Plate · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION ON DECK PLATE AT STA 1715.3 ON BL 12.5L AND 24L, ON FLOOR IN PAX CABIN. CORROSION WAS FOUND TO BE OUT OF LIMIT IAW BOEING 757-200 SRM 53-00-51-1A1 FIG 101. PERFORMED LAYOUT OF REPAIR ON DECK PLATE IAW BOEINFeb 3, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600339Plate · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION ON DECK PLATE AT STA 1714 ON BL 25R AND 39R, ON FLOOR IN PAX CABIN. CORROSION WAS FOUND TO BE OUT OF LIMIT IAW BOEING 757-200 SRM 53-00-51-1A1 FIG 101. PERFORMED LAYOUT OF REPAIR ON DECK PLATE IAW BOEING 757-200 SRFeb 3, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600456Bulkhead · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON WEB AT BS 1714, PRESSURE BULKHEAD, AT BL 25L UNDER AFT GALLEY AREA. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR WEB AT BS 1714, PRESSURE BULKHEAD, AT Feb 2, 2006 · N913AW · Boeing 757225 · Fuselage Main, BulkheadSDR AWXA200600432Frame · corrodedSAL - MAJOR REPAIR - DURING C11 CHECK DISCOVERED CORROSION ON FRAME AT BS 1540 FROM BL 14R TO BL 19R IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF SRM LIMITS. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR PLATE AND SPLICEFeb 2, 2006 · N913AW · Boeing 757225 · Fuselage Main, FrameSDR AWXA200600727Fitting · corrodedDURING C8 CHECK DISCOVERED CORROSION ON THE FORWARD BAG PIT DOOR OPENING THRESHOLD SUPPORT FITTING A THE MOST AFT SUPPORT FITTING FORWARD END AT BS 620, STR 25R AND BL 70R. MAINTENANCE REMOVED AND INSTALLED NEW THRESHOLD SUPPORT FITTING AT BS 620, STR 25R ANDFeb 1, 2006 · N907AW · Boeing 757225 · Cargo/Baggage DoorsSDR AWXA200600649Intercostal · corrodedSAL - DURING C11 CHECK DISCOVERED CORROSION, LEVEL 2, ON WEB LOWER SURFACE BETWEEN BL 10.45L AND 11.40L BS 1639 AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CORROSION AT BS 1639 BETWEEN BL 10.45L AND BL 11.40L IAW BOEING SRM 51-10-02-OG. CORROSION FOUND OUT OFFeb 1, 2006 · N913AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060158Intercostal · crackedFOUND INTERCOSTAL CRACKED BS 660 S-11L. REMOVED DAMAGE AND INSTALLED NEW PART IAW EO 5304R143, DEFECT SIZE: .375.Jan 30, 2006 · N609AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060160Intercostal · crackedFOUND INTERCOSTAL CRACKED BS 660 S-14R. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EO 5304R143, DEFECT SIZE: .375.Jan 30, 2006 · N609AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600149Battery · inoperativeSEA - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE EMERGENCY FLASHLIGHT AT THE L3 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE EMERGENCY FLASHLIGHT AT THE L3 DOOR. OPERATIONAL CHECKS WERE GOOD.Jan 27, 2006 · N913AW · Boeing 757225 · Emergency EquipmentSDR AWXA200600147Fairing · separatedDURING CLIMB, CREW REPORTED A VIBRATION AND NOISE. DISCOVERED THE LT WING TO FLAP FAIRING CAME OFF IN FLIGHT. CREW DECLARED EMERGENCY AND LANDED IN TPA. MAINTENANCE INSTALLED TEMP. REPLACEMENT PANEL AND MAINTENANCE FERRIED TO PHX. AIRCRAFT IS STILL OTS. Jan 26, 2006 · N915AW · Boeing 757225 · Trailing Edge FlapsSDR AWXA200600134Fuse · inoperativePHX - EEL - MAINTENANCE REPORTED THAT THE AFT SECTION OF ESCAPE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FUSES IN POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.Jan 26, 2006 · N913AW · Boeing 757225 · Emergency LightingSDR AWXA200600128Skin · bulgedMX DISCOVERED DURING A CHECK POSSIBLE PILLOWING CORROSION STR 28L AT BS 1460 BULGE IN SKIN RIVETS HEADS DAMAGED. MAINTENANCE REMOVED EXISTING SPLICE AT STA 1452-1465 AND STR 28L. CUTOUT STRINGER 28L AT STA 1455 TO STA 1459, CORROSION WAS OUT OF LIMITS. REMOJan 25, 2006 · N914AW · Boeing 757225 · Fuselage Main, Plate/SkinSDR AWXA200600130Skin · debondedPHX - MAJOR REPAIR - MAINTENANCE REPORTED TWO DISBONDED AREAS FOUND ON LEADING EDGE OF LOWER SKIN ON THE TRAILING EDGE WEDGE ON THE LEFT HAND WING APPROX. 2" BY 0.5" AND 1" BY 0.3" ON THE INBOARD FLAP. MAINTENANCE CUT OUT AND REMOVED DAMAGED CORE ON THE INBOAJan 23, 2006 · N915AW · Boeing 757225 · Trailing Edge FlapsSDR USAA06099Stringer · crackedSTA 686, S9L AFT END OF STRINGER CRACKED. REMOVED & REPLACED STRINGER CHORD PER SRM 51-40-02, 51-20-01, 51-10-02, DEFECT SIZE: 1.5 INCH.Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Main, Longeron/StringerSDR USAA060105Intercostal · corrodedSTA 1240 RBL 290 INTERCOSTAL AT AFT CARGO FLOOR CORRODED. REMOVED INTERCOSTAL, WEB, ANGLES & FITTING, FABRICATED & INSTALLED PER SRM 53-00-51, 51-40-02, DEFECT SIZE: 1" X 2" X .022" WEB, 1" X 1.5" X 0.58" FTG; 1.5" X 1" X .065" AREA.Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060104Shim · corrodedBS 1380-1400 S27L CORRODED. FAB SHIM & FAB STRINGER SECTION PER SRM 53-00-03, DEFECT SIZE: 5"L X 1"W.Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060103Skin · crackedSTA 1360 S27R CRACKED. REMOVED DAMAGED AREA, FABRICATED DOUBLER PER SRM 53-00-01, 51-40-02, 51-20-01, DEFECT SIZE: 1 INCHJan 20, 2006 · N600AU · Boeing 757225 · Fuselage Main, Plate/SkinSDR USAA060102Splice · corrodedAFT CARGO, STA 1468, STR 29L, WL 130; CORROSION LEVEL 1; TASK C53-155-02. REMOVED & REPLACED STR & INSTALLED NEW SPLICE PER SRM 51-40-02, 51-10-02, 53-00-03, DEFECT SIZE: 2"L X 1"W X .060"D (2 AREAS).Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060101Web · corrodedAFT CARGO STA 1500 - 1520 WL 130, S 30 CORRODED. REMOVED & REPLACED WEB PER SRM 51-40-02, 51-20-01, 51-21-10; CORROSION LEVEL 1; TASK C53-155-02, DEFECT SIZE: 7"L X 1"W X .032"D.Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR USAA060100Web · corrodedAFT CARGO, STA 1477, WL 130, RBL 12 CORRODED. REMOVED & REPLACED WEB PER SRM 51-40-02; CORROSION LEVEL 1; TASK C53-156-02, DEFECT SIZE: 5"L X 1"W X .040"D.Jan 20, 2006 · N600AU · Boeing 757225 · Fuselage Miscellaneous StructureSDR BB06004Wire · damagedCLT - UPON ARRIVAL IN CLT, CREW RECEIVED A LEFT DUCT LEAK EICAS MESSAGE ALONG WITH LEFT ENGINE EEC AND LIMITER FAULTS. MESSAGE AND FAULTS APPEARED AT ENGINE THROTTLE BACK. FLIGHT LANDED WITHOUT INCIDENT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACEDJan 19, 2006 · N603AU · Boeing 757225 · Pneumatic System WiringSDR USAA060097Skin · corrodedFOUND CORROSION AFT PIT, STA 1440 S 30R. CUT OUT DAMAGE, FAB'D DOUBLER AND FILLER PER SRM 53-00-01, 53-60-01, 51-20-01, DEFECT SIZE: 3.90"L BY 1.40"W BY .015"D.Jan 18, 2006 · N600AU · Boeing 757225 · Fuselage Main, Plate/SkinSDR USAA060096Skin · chafedFOUND RT FLAP IB END L/E CHAFFED. FABRICATED INTERNAL DOUBLER, SKIN PER EA 97228, DEFECT SIZE: 1" BY 1".Jan 18, 2006 · N600AU · Boeing 757225 · Trailing Edge FlapsSDR USAA060098Frame · crackedFOUND CRACK AFT CARGO STA 1380 BETWEEN STR 26L AND 27L. CUT OUT DAMAGED AREA, REPAIRED PER EA 97224, DEFECT SIZE: 1.60.Jan 18, 2006 · N600AU · Boeing 757225 · Fuselage Main, FrameSDR AWXA200600611Floorbeam · corrodedGYR - DURING C08 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1681 BL 53R. MAINTENANCE REMOVED CORROSION IAW 757-200 SRM 53-00-51. REWORK FOUND OUT OF SRM LIMITS. REPAIRED FLOORBEAM AT BS 1681 FROM BL 47R TO 55Jan 5, 2006 · N907AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200600612Floorbeam · corrodedGYR - DURING C08 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1681 ON LOWER SURFACE OF UPPER CHORD BL 48R TO BL 48L AT WL 208. MAINTENANCE FOUND CORROSION REWORK OUT OF LIMITS. FABRICATED REPAIR ANGLE IAW AWA ER 19-5365-06084-DF1. INSTALLEJan 4, 2006 · N907AW · Boeing 757225 · Fuselage Main, Floor BeamSDR AWXA200600634Floor Support · corrodedGYR - DURING C08 CHECK DISCOVERED CORROSION, LEVEL 2 EXFOLIATION, ON LOWER SURFACE OF FLOOR SUPPORT CHANNEL FOR FORWARD CARGO DOOR SILL. CORROSION ADJACENT TO ATTACH FASTENER HOLES AT BL 20R, BS 615, WL 160. CORROSION OUT OF SRM LIMITS. MAINTENANCE REMOVED Dec 21, 2005 · N907AW · Boeing 757225 · Fuselage Miscellaneous StructureSDR AWXA200600604Skin · dentedGYR - DURING C 08 CHECK DISCOVERED RIGHT HAND HORIZONTAL STAB UPPER SKIN HAS A PREVIOUSLY BLENDED AREA LOCATED 2 INCHES AFT OF FRONT SPAR AT STA 200 MEASURING APPROX 4 INCHES BY 1.56 INCHES BY 0.032 INCHES DEEP. MAINTENANCE REMOVED DAMAGED SKIN AND CORE IAW BDec 20, 2005 · N907AW · Boeing 757225 · Wing, Rib/BulkheadSDR USAA051599Skin · gougedFOUND 2.0"L BY 0.80"W BY .055"D AND 1.2"L BY 0.30"W BY .013"D. FAB'D OVERLAY REPAIR AND BONDED TO AREA PER SRM 51-70-17 AND EA 97150, DEFECT SIZE: 2.0"L BY .080"W BY .055"D AND 1.2"L BY .20"W BY .013"D.Dec 20, 2005 · N607AU · Boeing 757225 · Trailing Edge FlapsSDR AWXA200600730Support Fitting · corrodedDURING C8 CHECK, DISCOVERED CORROSION ON FORWARD CARGO DOOR SILL SUPPORT FITTING, FORWARD ATTACH ANGLE AT BS 600, STR 26R AND WL 156. MAINTENANCE REMOVED AND INSTALLED FABRICATED SUPPORT FITTING AT BS 600, STR 26R AND WL 156 IAW BOEING 757-200 SRM 51-20-01, 5Dec 19, 2005 · N907AW · Boeing 757225 · Fuselage Miscellaneous Structure
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