Boeing 757-2Q8

Service difficulty reports · 2,798

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '7572Q8'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201109163908Seat Track · gougedSEAT TRACK AT BS 418 - 440, LBL 24, IS GOUGED. BLENDED GOUGE AREA; ORIGINAL: .200", AFTER: .150", FOUND TO BE OUT OF LIMTS IAW SRM 53-00-52, FIG 101, DETAIL 1, REWORK AREA 2"X.9". R & R SEAT TRACK IAW SRM 51-40-02, REPLACEMENT SEAT TRACK, BATCH NR 00019046Sep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109163907Seat Track · gougedSEAT TRACK AT STA 418-STA 440 RBL 24 GOUGED. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02. TREATED AND PRIMED PER SRM 51-20-01. PAINTED PER SRM 51-20-01. INSTALLED NEW SEAT TRACK, PER SRM 51-40-0Sep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109163906Seat Track · gougedSEAT TRACKAT STA 418, STA 440, RBL 48 IS GOUGE. BLENDED GOUGE ORIGINAL MAT .200, AFTER REPAIR .130 MATERIAL, REMOVED .070, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I, FIG 101. R & R SEAT TRACK MATERIAL BAC1520-792, BATCH 1904663 IAW SRM 51-40-02, MASep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109153895Skin · misrepairedSKIN AT BS 1681 S-17L -S-18L MISREPAIRED. R & R REPAIR IAW SRM 51-40-02, FABRICATED NEW REPAIR IAW SRM 53-00-01, TABLE I & III FIG 101, PG 203. MAJOR REPAIR.Sep 15, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201109143876Skin · misrepairedSKIN AT STA 1500, S-28L MISREPAIRED. SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 15. MAJOR REPAIR.Sep 14, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201109133863Door Frame · gougedPASENGER DOOR 1 L FWD DOOR FRAME AT BS 337.5, ADJACENT TO S8L GOUGED. BLENDED GOUGE IAW 51-10-02 CHECKED LIMITS, ORIGINAL MAT .063" AFTER REWORKED .038" FOUND TO OUT LIMITS IAW SRM 53-10-15, FIG 101 DETAIL IV. REMOVED FRAME IAW SRM 51-40-02, FABRICATED, LOCASep 13, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201109103820Tee Fitting · corrodedMCD AFT PRESSURE DECK UPON REMOVAL FOUND TEE ANGLE CORRODED BS 1720 LBL-50 REMOVED TEE ANGLE FOR ACCESS TO CORROSION, PER SRM 51-40-02. REMOVED CORROSION PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-80-05, DETAIL 9, P.109. LOCATED AND DRILLED NEW TEESep 10, 2011 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201109103819Cusp Web · corrodedAFT PRESSURE DECK UPON REMOVAL OF DECK FOUND CUSP WEB CORRODED LBL-55, STA 1701-STA 1720.Sep 10, 2011 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201109093813Wedge · damagedRT WING INBD FLAP, TRAILING FLAP WEDGE HAS DAMAGE AT T/E 21 INCHES FROM OTBD EDGE. REPAIRED IAW SRM 51-70-10 REPAIR 4. MAJOR REPAIR.Sep 9, 2011 · N995FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201109093808Depressor · dentedAFT CARGO DOOR AFT EDGE, APPROXIMATELY HALFWAY UP EDGE, DENTED. BLENDED AREA IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02, FIG 101 DETAIL V. DEPTH .026, A=1.50 Y=.200 A/Y=4.35. REMOVED SEAL DEPRESSOR IAW SRM 51-40-02. LOACATED AND DRILLED NSep 9, 2011 · N996FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201109093810Beam · dentedAFT CARGO DOOR LOWER CTR EDGE BEAM DENTED AND CHAFED ON ENTIRE EDGE. DAMAGED AREA FOUND OUT OF LIMITES IAW SRM 52-30-02, FIG 101, DETAIL V. R & R LOWER CTR EDGE BEAM IAW SRM 51-40-02. MAJOR REPAIR.Sep 9, 2011 · N996FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201109093807Frame · damagedFRAME AT BS 1300 S1 HAS ELONGATED HOLE. REPAIRED FRAME IAW SRM 53-00-07.Sep 9, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201109083764Seat Track · gougedGOUGES ON MAIN DECK SEAT TRACK RBL 25 BS 1576-1595. BLENDED SEAT TRACK IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. REMOVED SEAT TRACK IAW SRM 51-40-02. TRIMMED NEW TRACK IAW SRM 53-00-52. LOCATED AND DRILLED NEW TRACK IASep 8, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109083765Seat Track · gougedMAIN DECK SEAT TRACK GOUGED RBL 45, STA 1594. BLENDED SEAT TRACK IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I. R & R SEAT TRACK, IAW SRM 51-40-02. MAJOR REPAIR.Sep 8, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109073741Door Frame · corrodedSTA 1380 NR 2 CARGO DOOR STR 22 CORRODED ON DOOR FRAME.Sep 7, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201109063718Frame · damagedFWD CARGO DOOR FWD LOWER CORNER ANGLE FRAME DAMAGE. REPLACED LOWER CORNER ANGLE FRAME IAW SRM 51-40-02, CHECKED LIMITS MAT FOUND TO BE PUNCTURED THROUGH THE LOWER CORNER FRAME & EXCEED THE ALLOWABLE DAMAGE IAW SRM 52-30- 02, FIG 101 NOTE L=1.0" W=0.5" RECEISep 6, 2011 · N995FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201109033645Skin · corrodedLWR FUSELAGE HAS CORROSION ON SKIN RUNNING UNDER RAIN DIVERTER FOR POTABLE WATER SERVICE AT BS 1661.Sep 3, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108313598Crease Beam · gougedCREASEBEAM AT BS 1290-1370 HAS NUMEROUSE GOUGES AND SCRATCHES. FUTHER INVESTIGATION FOUND A PUNCTURE HOLE WAS FOUND, IAW SRM 53-60-15, FIG 101, DETAIL IV. NOTE C, PUNTURE HOLES ARE NOT PERMITED ADJACENT TO FASTENER HOLES LESS THAN 1" AWAY, R & R DAMAGEAug 31, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201108303584Structure · chafedNR 3 SPOILER PCU CHAFING OTBD FLAP TOP SIDE L/E BOTTOM OF PCU. GOUGE OUT OF LIMITS PER SRM 57-53-01 FIG 101 DETAIL VI. INSTALLED REPAIR PARTS IAW SRM 57-53-01 FIG 201 REPAIR 2 . REPAIR FABRICATED PER SRM 57-53-01 FIG 201 REPAIR 2. MAJOR REPAIR.Aug 30, 2011 · N996FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201108293570Frame · damagedUPPER LOBE STRUCTURE FRAME HAS DOUBLED DRILLED HOLE AT STA 800 BETWEEN S-2L TO S-3L DUPLICATE SDR SEE 11-2919 FOR ENTRIES.Aug 29, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108253486Gate · corrodedL-2 DOOR LOWER GATE HAS PITTED CORROSION AT SEAL RETAINER BRACKET. REMOVED CORROSION, CHECKED LIMITS ORIG .200 REMOVED .035 REMAINING .165 FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101. REMOVED LOWER GATE ASSY IAW AMM 52-11-38. RECEIVED NEW GATE ASAug 25, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108243461Seat Track · misalignedSEAT TRACK, RBL 45, STA 440. DOES NOT JIG (MISALIGNED). SPLICED A NEW SEAT TRACK SECTION BETWEEN BS 440-490, RBL 45, IAW SRM 53-00-52, FIG 201. MAJOR REPAIR.Aug 24, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108233434Frame · damagedFRAME BS 1500 BETWEEN S26-27L, UPPER AREA GOUGED AND DENTED. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. MAJOR REPAIR.Aug 23, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA1149356802Oven · dirtyCREW REPORTED SMOKE FROM THE GALLEY OVENS AND PULLED THE OVEN CIRCUIT BREAKERS. MAINTENANCE FOUND GREASE AND CONDENSATION BEHIND OVENS NR 4 AND NR 5. CLEANED BEHIND ALL FOUR OVENS, CHECKED THE WIRING AND LIGHTING. OPERATED OVENS FOR 20 MINUTES WITH NO SMOKEAug 19, 2011 · N703TW · Boeing 7572Q8 · Buffet/GalleysSDR FDEA201108183359Frame · damagedAFT PIT 1540 FRAME LT AT STR 26L FRAME FLANGE GOUGED AND DENTED. BLENDED OUT GOUGED AREA IAW SRM 51-10-02. ORIGINAL MATAERIAL THICKNESS. .071, REMAINING MATERIAL .066. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL AD2. R & R FRAME IAW SRM Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108183372Intercostal · corrodedFWD CARGO DOOR LWR AREA INTERCOSTAL TEE, INNER ANGLE HAS CORROSION ON THE EDGE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. MAJOR REPAIR.Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108183371Intercostal · corrodedFWD CARGO DOOR INTERCOSTAL TEE, INNER ANGLE HAS CORROSION ON THE EDGE. BLENDED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. MAJOR REPAIR.Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108183370Intercostal · corrodedFWD CARGO DOOR INTERCOSTAL TEE, INNER ANGLE HAS CORROSION ON THE EDGE. BLENDED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. MAJOR REPAIR.Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108183369Intercostal · corrodedFWD CARGO DOOR INTERCOSTAL OUTER TEE, INNER ANGLE HAS CORROSION ON THE EDGE. BLENDED CORROSION IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. MAJOR REPAIR.Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108183367Intercostal · corrodedFWD CARGO DOOR INTERCOSTAL OUTER TEE, INNER ANGLE HAS CORROSION ON THE EDGE. BLENDED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMAINING MATERIAL .030 ORIGINAL MATERIAL .050. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. Aug 18, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201108173317Frame · dentedAFT PIT FRAME AT STA 1560L ABOVE STR 26L AREA ON UPPER FRAME GOUGED. FOUND GOUGE TO BE A DENT. DENTS NOT ALLOWED IN FLANGE OF FRAME IAW SRM 53-00-07, FIG 101 ALLOWABLE DAMAGE 2. R & R FRAME STA 1560 S-24L TO S-24R IAW SRM 51-40-02. MAJOR REPAIR.Aug 17, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108133263Skin · misrepairedREPAIR LOCATED AT STA 288.5 S18-19L DOES NOT CONFORM TO CURRENT SRM REQUIREMENTS. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-40-02 AND 53-00-01 FIGURE 201, REPAIR 16. "CAT.B REPAIR, MAJOR"Aug 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108133267Beam · gougedFWD CARGO DOOR LWR MIDDLE EDGE BEAM GOUGED AND DENTED.Aug 13, 2011 · N996FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201108133262Skin · misrepairedSKIN LOCATED AT STA 418, S14-18L MISREPAIRED. FABRICATED AND INSTALLED NEW REPAIR IAW SRM-53-00-01, REPAIR 15, FIG 201. CAT. B MAJOR REPAIR.Aug 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108133260Gate · corrodedL-4 DOOR LOWER GATE CORRODED AT SEAL RETAINER BRACKET. REMOVED CORROSION AT LOWER SEAL AREA . CHECKED LIMITS ON WORKED AREA FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101. ORIG MAT .200 MAT LOSS .040 REM. 160. REMOVED L-4 LOWER GATE IAW 51-40-02. RECEIVEDAug 13, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108133259Skin · dentedDOOR OUTER SKIN HAS AN OUTER DENT AT S13R,4" FROM L/E. EVALUATED DENT ON R-1 DOOR OUTER SKIN AT S13R, 4" FROM THE L/E;W=.008", D=.007, A/Y=114. DENT IS W/I LIMITS IAW SRM 52-10-01, FIG.101, DETAIL7. HFEC IAW NTM 51-00-19,PT.6, NO CRACKS NOTED. APPLIED DENAug 13, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108053106Gate · corrodedL1 DOOR LOWER GATE CORRODED AT SEAL RETAINER ATTACHED POINT. REMOVED CORROSION IAW SRM 51-10-02, ORIG MAT THICKNESS = .208 , MATERIAL REMOVED IS .085, MAT REMAINING = .123. FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL VII. R & R L1 DOOR LOWER GATEAug 5, 2011 · N996FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108043099Floorbeam · corrodedFLOORBEAM AT LBL 45 CORRODED AT STA 377. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201, REPAIR NR 3 AT STA 377 FROM RBL 24 TO LBL 70. MAJOR REPAIR.Aug 4, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201108033088Pressure Deck · corrodedPRESSURE DECK WEB HAS CORROSION AT STA 1681.8-1720, RBL 50. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS MAT THICKNESS .071", BLENDED MAT, .053" FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DET III, REMOVED PRESSURE WEB IAW SRM 51-40-02. FABRICATED PRAug 3, 2011 · N995FD · Boeing 7572Q8 · Fuselage Floor PanelSDR FDEA201108033086Frame · gougedMAIN DECK FRAME STA 1280, RT, BETWEEN S11-12R, DEEP GOUGE IN FRAME FLANGE. REMOVED GOUGE ON FRAME STA 1280 BETWEEN S-11R TO S-12R IAW SRM 51-10-02. ORIGINAL THICKNESS .071, REMAINING THICKNESS .011. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101, DETAILAug 3, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201108023316Skin · gougedAPU DOOR 316AR EXTERNAL SKIN LATCH HOLES, -2- PLACES GOUGED WITH KNIFE EDGE.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Auxiliary Power Unit (APU) DoorsSDR FDEA201108023430Seat Track · misalignedSEAT TRACK, LBL 45, BS 440 MISALIGNED. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW DWG 143N5110, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05 AND DWG 143N5110 INSTALLED SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5110 AND PART MARKEDAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201108023142Stringer · corrodedDURING A CHECK, INSTALLED DOUBLER REPAIR AT STA.1500, STR 22L,FOUND S-22L CORRODED AROUND FASTENER HOLES AT STA 1510. CUT OUT DAMAGED STRINGER 22L BTW BS 1510 TO BS 1530 IAW SRM 53-00-03 REPAIR 2 PG 201, RECEIVED FABRICATED STRINGER, FABRICATED SPLICE Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201108023431Skin · dentedSKIN DENTED AT BS 1540, S-23-24R. REMOVED DAMAGE & FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, DETAIL 3, FIG. 101 & SRM 51-40-02. HFEC , NO CRACK INDICATION NOTED. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 / 3, FIG. 201, REPAIR 16. INSTALLED DOUBLER PAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023314Seat Track · gougedSEAT TRACK GOUGE AT STA 1210 TO 1220, LBL 45 AROUND THE CROWN AREA. REMOVED ANGLE AND SEAT TRACK IAW SRM 51-40-02, FABED NEW PART IAW SRM 53-00-52, FIG 201 SHEET 1, BATCH 1904663, PN BAC 1520-792, LOCATED AND DRILLED IAW SRM 51-40-05, TREATED AND PRIMED ANAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023070Gate · corrodedL2 DOOR LOWER GATE CORRODED AT SEAL RETAINER POINT. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL IV MATERIAL LOSS 0.115 EXCEEDS MAX ALLOWABLE OF 0.100. R & R LOWER GATE IAW AMM 52-11-38-4, NO RIG DISTURBED. MAJOR REPAIR.Aug 2, 2011 · N996FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108023364Seat Track · misinstalledSEAT TRACK STA 440, RBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK AT BS 440-470 IAW SRM 53-00-52, REPAIR 1. FABRICATED NEW SEAT TRACK AND REPLACED IAW SRM 53-00-52, FIG 201 REPAIR 1. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023322Seat Track · misalignedSEAT TRACK, STA 440-470, LBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, FIG 201, SHEET 1 OF 5, REPAIR 1. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023278Skin · misrepairedSKIN AT 1560-1580, S-18R-S19R DOES NOT MEET SRM REPAIR STANDARDS. CORRECTED REPAIR IAW SRM 53-00-01. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023096Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 343-346, S-21R-S-23R IS NOT IN COMPLINCE WITH SRM. REMOVED EXISTING REPAIR AT BS 343-346 S-21R - S-23R IAW SRM 51-40-02 , HFEC INSP IAW NTM 51-00019 PT6 & 51-00-16 PT6, FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 53-00-01 REPAIR Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
Back to Boeing 757-2Q8