N941FD

Service difficulty reports · 150

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N941FD' AND registry_match = 'registration'
  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 FDEA201202080520Skin · damagedFOUND SCRIBE LINE AT S-26L FROM BS 659.812 TO BB 661 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, "FUSELAGE PLATES AND SKINS- AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"Feb 8, 2012 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201202080519Skin · damagedFOUND SCRIBE LINE AT S26L FROM BS 661.156 TO BS 662.312 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, FUSELAGE-PLATES AND SKINS-AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"Feb 8, 2012 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201270354Stringer Clip · damagedSTRINGER CLIP AT STA 1640,STR 26R HAS A OVERSIZED FASTENER HOLE. REPAIRED IAW EA NR 757-5361-16-F3621 REV AND STAM NR 47327520001 REF 8110-3.Jan 27, 2012 · N941FD · Boeing 757225 · Fuselage Main, Attach FittingsSDR FDEA201201210293Skin · dentedFUSELAGE SKIN BS 1715, S 15L IS DENTED.Jan 21, 2012 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201210292Skin · dentedFUSELAGE SKIN BS 1715, S 16L IS DENTED.Jan 21, 2012 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201060029Skin · crackedPANEL RACK NR 2 PYLON BULL NOSE PANEL CRACKED AT AFT END, BY RUB SEAL. REMOVED SKIN IAW SRM 51-40-02. FABRICATED NEW SKIN IAW EA F-5710-156984. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 114N1802. MAJOR REPAIR.Jan 6, 2012 · N941FD · Boeing 757225 · Nacelle/Pylon, Plate/SkinSDR FDEA201112215408Door Frame · corrodedL2 DOOR CUTOUT LOWER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL 3, PAGE 106. R & R CHORD ASSY IAW SRM 51-40-02, AND DWG 143N8328. MAJOR REPAIR.Dec 21, 2011 · N941FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201112205392Crease Beam · corrodedCREASE BEAM AT S-17R BET BS 418 TO BS 440 INNER CHORD HAS CORROSION. REMOVED CORROSION BY BLENDING IAW SRM 51-10-02. CHECKED LIMITS ORIG MATERIAL WAS .071 AFTER REWORK = .049, FOUND OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. R & R CREASE BEAM IADec 20, 2011 · N941FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201112195372Skin · misrepairedFUSELAGE SKIN AT BS 425-430, STR -24L MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, AT BS 425-430, S24L. CAT "B" MAJOR REPAIR.Dec 19, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201112195371Skin · misrepairedSKIN AT BS 395, S17R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 316, CAT "B" MAJOR REPAIR.Dec 19, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201112135255Skin · corrodedLEFT NACELLE STRUT PANEL 433GR CUT OUT INTERNAL SURFACE CORRODED. REMOVED CORROSION IAW SRM 54-50-01; BEFORE: .130", AFTER: .070", LOSS: .060", FOUND OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL 3. R & R SKIN IAW DWG 311N5193, AND SRM 51-40-02. MAJOR REPDec 13, 2011 · N941FD · Boeing 757225 · Nacelle/Pylon, Plate/SkinSDR FDEA201112075222Butt Joint · gougedUPON REMOVAL OF SEALANT FROM BUTT JOINT, FOUND VERTICAL SCRIBE LINE ON BUTT JOINT STRAP SURFACE AT BS 1621 FROM APPROX S-10 L THROUGH S-14L. REMOVED SPLICE PLATE AT STA 1621 BETWEEN S-10L TO S-14L IAW SRM 51-40-02. FABRICATED NEW SPLICE PLATE AT STA 1621 BEDec 7, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201112075209Frame · misrepairedFRAME MISREPAIRED REPAIR AT BS 1480 S24-26L. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1030. MAJOR REPAIR.Dec 7, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201112075221Skin · damagedUPON REMOVAL OF SEALANT FROM BUTTJOINT FOUND VERTICAL SCRIBE LINE ON BUTT JOINT STRAP SURFACE AT BS 1621 FROM APPROX S-14L, THROUGH S-16L. HFEC INSPECTION OF SCRIBE LINE IAW NDTM53-30-09, NO CRACKS NOTE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 5, Dec 7, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201112025128Frame · misrepairedEXISTING FRAME REPAIR AT BS 1340, STR 22R-26R MISREPAIRED. REMOVED AND REPLACED FRAME AND SPLICE BS 1340 IAW SRM 51-40-02 AND DRAWING146N1028. MAJOR REPAIR.Dec 2, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201112015129Skin · delaminatedLEFT WING INBD FLAP UPPER SURFACE AT MAIN FLAP STA 200 HAS AN AREA WITH SIGNS OF DELAMINATION. REPAIRED IAW SRM 51-70-10, REPAIR NR 4. REF EA F-5750-147773. MAJOR REPAIR.Dec 1, 2011 · N941FD · Boeing 757225 · Trailing Edge FlapsSDR FDEA201112015105Seat Track · damagedSEAT TRACK, BS 1540-1640, LBL 45.5 GOUGED AND CORRODED. BLENDED SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 1, PAGE 102, AND FOUND TO BE OUT OF LIMITS, ORIG: .145", AFTER: .117", LOSS: .028". REMOVED SEAT TRACK IAW SRM Dec 1, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112015107Beam · chafedFWD CARGO DOOR LOWER AFT CORNER EDGE BEAM HAS CHAFING AND GOUGE. REMOVED CHAFING IAW SRM 52-30-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 52-30-02, FIG. 101, DETAIL 1 & 2; BEFORE: .050", AFTER: .037", LOSS: .017". REMOVED LOWER AFT CORNER IAW SRM 51-Dec 1, 2011 · N941FD · Boeing 757225 · Cargo/Baggage DoorsSDR FDEA201111295077Skin · damagedFOUND GOUGES, SCRIBE LINES, CORROSION ON SKIN AT BS 1625 TO 1685, S17-18R. UNDER SCUFF PLATE.Nov 29, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201111255047Intercostal · corrodedUPON REMOVAL OF AFT PIT FRAME FOUND INTERCOSTAL CORRODED STA 1540-1560, BETWEEN S26L AND S26R.Nov 25, 2011 · N941FD · Boeing 757225 · Fuselage Miscellaneous StructureSDR FDEA201111174951Frame · misrepairedFRAME BS 1420 S24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028.Nov 17, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201111174959Fill Port · corrodedLT WING TANK OVERWING FILL PORT FAILED FUNCTIONAL BONDING CHECK.Nov 17, 2011 · N941FD · Boeing 75728A · Fuel StorageSDR FDEA201111104870Skin · dentedFUSELAGE SKIN CREASED BS 1390-1410 S15-16L.Nov 10, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201111104868Frame · misrepairedFRAME AT BS 1400, STR 24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028. MAJOR REPAIR.Nov 10, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201111084817Crease Beam · damagedMAIN DECK CREASE BEAM BS 900-1040 RT HAS AN ELONGATED HOLE. REMOVED EXISTING CREASEBEAM IAW SRM 51-40-02. . LOCATED, DRILLED AND INSTALLED NEW CREASEBEAM IAW SRM 51-10-02. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT PER AMM 51-00-07. MAJOR REPAIRNov 8, 2011 · N941FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111084806Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 1397-1404, RBL 45.50 UPPER SURFACE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-02, FIG.101, SHEET 2 OF 6. REMOVED SEAT TRACK IAW SRM 51-40-02. INSTALLED NEW SEAT TRACK, BS 1320-1540, RBL 45.50, PENov 8, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111034737Skin · wrinkledFUSELAGE SKIN JUST AFT OF BS 660 TO 675 S20-23L HAS WRINKLING/BUCKLING. REPAIRED IAW SRM 51-40-02 & 53-00-01, REPAIR 16. MAJOR REPAIR.Nov 3, 2011 · N941FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201111024729Floor Panel · corrodedMAIN CABIN DECK PLATE STA 1681.8 TO STA 1720 BL-0 TO RBL-58 HAS SEVERAL AREAS OF CORROSION. R & R MAIN CABIN DECK PLATE, BS 1681-1720, RBL 58 - LBL 58, IAW SRM 51-40-02.Nov 2, 2011 · N941FD · Boeing 757225 · Fuselage Floor PanelSDR FDEA201111014717Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 1180 TO 1280, RBL 45.50 HAS SEVERAL AREAS OF BARE METAL AND CORROSION. BLENDED CORRODED AREAS PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK PER SRM 51-40Nov 1, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111014716Frame · misrepairedFRAME BS 1500, STR 24-26L MISREPAIRED. REMOVED FRAME IAW SRM 51-40-02. INSTALLED NEW FRAME IAW SRM 51-40-02, AND DWG 146N1030.Nov 1, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201110314696Seat Track · corrodedSEAT TRACK AT STA 440-530, LBL 45 NICKED, GOUGED & HAS SURFACE CORROSION. BLENDED AREAS IAW SRM 51-10-02. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, FIG 101, PAGE 102. R & R SEAT TRACK AT LBL 45.50, BS 440-680, IAW SRM 51-40-02, 53-30-Oct 31, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110284680Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 1661 BL 0 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. R & R FLOORBEAM IAW SRM 53-60-51, AND DWG 146N5180. MAJOR REPAIR.Oct 28, 2011 · N941FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201110284682Seat Track · gougedMAIN CABIN SEAT TRACK BS 1220, RBL 24.75 UPPER LOBES GOUGED. GOUGE BLENDED IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I, PG 102. ORIGINAL MATERIAL 0.145 LOSS 0.024 REMAINING 0.021. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED Oct 28, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110264658Frame · misrepairedFRAME AT BS 1320 STR 22L- 26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1028.Oct 26, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201110254647Floorbeam · bentFLOORBEAM, STA 879 BL 0, BENT. FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, PAGE 101. REMOVED AND REPLACED FLOORBEAM PER SRM 51-40-02 AND DWG 143N5072.Oct 25, 2011 · N941FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201110254649Frame · misrepairedFRAME MISREPAIRED REPAIR AT BS 1440, S24-26L. R & R FRAME IAW SRM 51-40-02, AND DWG 146N1028. MAJOR REPAIR.Oct 25, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201110254648Frame · misrepairedFRAME AT BS 1540, STR 24L-26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1030.Oct 25, 2011 · N941FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201110194587Floorbeam · corrodedFLOORBEAM UPPER TEE IS CORRODED BS 1681.8, LBL 25. CORROSION OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-60-51 AND DWG 146N5091. INSTALLED IAW SRM 51-40-02 AND DWG 146N5091. MAJOct 19, 2011 · N941FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201110194585Seat Track · damagedSEAT TRACK AT BS 365-440, RBL 45.50 HAS NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK. ORIGINAL: .080", REMAINING: .062", FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7, PAGE 104. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-0Oct 19, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110194584Seat Track · damagedMDC SEAT TRACK AT BS 365-440 RBL 24.75 HAS SEVERAL NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK, ORIGINAL MATERIAL .080", MATERIAL REMOVED .021", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101, DETAIL VII, PAGE 104. REMOVED AND REPLACEOct 19, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110184572Seat Track · damagedSEAT TRACK BS 879-900 LBL 24 NICKED & GOUGED. BLENDED DAMAGE IAW SRM 51-10-02 AND FOUND OUT OF LIMITS PER SRM 53- 00-52 FIG.101, DETAIL 1, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02, AND DWG 143N5481. MAJOR REPAIR.Oct 18, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110184573Seat Track · damagedSEAT TRACK BS 440-570 LBL 24.75 NICKED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 & 53-00-52. MAJOR Oct 18, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110144506Floorbeam · corrodedFLOORBEAM BS 1640, BL15L-R CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-60-51, AND DRAWING 146N5180. FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3, PAGE 103. MAJOR REPAIR.Oct 14, 2011 · N941FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201110144497Gate · gougedL4 DOOR LOWER GATE OTBD FWD AND AFT CORNERS GOUGED. REMOVED DAMAGE AND CHECKED LIMITS OF DAMAGE IAW SRM 52-10-02, SRM 51-10-02. OUT OF LIMITS FOR DAMAGE IAW SRM 52-10-02, FIG 101, DETAIL V. R & R L4 DOOR LOWER GATE AND OPS CHECKED IAW AMM 52-11-38, AMM 52-11Oct 14, 2011 · N941FD · Boeing 757225 · Passenger/Crew DoorsSDR FDEA201110134474Seat Track · gougedSEC 41 SEAT TRACK BS 1180-1240, LBL 24.75 GOUGED AND CORRODED. BLENDED AREA ON SEAT TRACK PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1, PAGE 102. ORIGINAL MATERIAL: .145", LOSS: .058:, REMAINING: .087". REMOVED SEAT TRACK IAW SOct 13, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110134484Seat Track · gougedSEAT TRACK, BS 1320-1540, LBL 45.50 GOUGED AND CORRODED. BLENDED SEAT TRACK IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.Oct 13, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110134480Crease Beam · corrodedCREASEBEAM BS 1300-1320 LBL 58.22 CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 8, P 105. R & R CREASEBEAM IAW SRM 51-40-02, AND DWG 146N8322. MAJOR REPAIR.Oct 13, 2011 · N941FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201110114418Seat Track · corrodedMDC AT STA 377-440 LBL 24.45 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7; BEFORE: .050", AFTER: .030", LOSS: .020". MAJOROct 11, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110114420Seat Track · damagedMCD STA 377-440 AT LBL 45.50 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. R & R SEAT TRACK IAW-SRM-51-40-02. REMOVED CORR0SION FROM SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS ORIG MATERIAL WAS .070, AFTER REWORK .052, TOTAL MATERIAL LOSS WAS .028, FOUOct 11, 2011 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201110104410Floorbeam · corrodedFLOORBEAM AT STA 365, RBL25 UPPER TEE CORRODED. REMOVED CORROSION ORIG MAT .125, AFTER BLEND .108, TOTAL MAT REMOVED .017, MAT. FOUND TO BE OUT OF LIMITS IAW SRM-53-00-51, FIG 101, DET III, REPAIRED FLOORBEAM IAW-SRM-53-00-51, FIG 201 REPAIR B NR 3. MAJOR Oct 10, 2011 · N941FD · Boeing 757225 · Fuselage Main, Floor Beam
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