Boeing 757-225
Service difficulty reports · 1,988
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 = '757225' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201201220301Skin · misrepairedNR 4 SLAT LT WING L/E NOSE SKIN AT OSS375 MISREPAIRED. REPAIRED IAW EA F-5750-157213 STEPS 1 THRU 4 EA. MAJOR REPAIR.SDR FDEA201201210293Skin · dentedFUSELAGE SKIN BS 1715, S 15L IS DENTED.SDR FDEA201201210292Skin · dentedFUSELAGE SKIN BS 1715, S 16L IS DENTED.SDR FDEA201201210291Skin · misrepairedFUSELAGE SKIN AT BS 620- 660 BETWEEN S-23R TP S-26R MISREPAIRED. REPAIRED IAW EA F-5330-157267.SDR FDEA201201210289Stringer · gougedFWD CARGO BAY BS 620- 640, S25R LWR SIDE GOUGED. REMOVED GOUGE IAW SRM 51-10-02 BLENDED AREA ORIG MAT .065 MATERIAL REMAINING .035, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. R & R STRINGER IAW SRM 51-40-02.SDR FDEA201201190269Crease Beam · corrodedMAIN CABIN AREA BET BS 1300-1360, S17R, RT SIDE CREASE BEAM INBD CHORD CORRODED. REMOVED CORROSION, ORIG MAT .100 AFTER MAT. REMAINING .060 MAT. LOSS IS .040 MAT. OUT OF LIMITS IAW SRM-53-60-13 DETAIL VIII FIG 101.R & R ANGLE BS 1290-1410 "CAT A, MAJOR REPAISDR FDEA201201170230Skin · misrepairedFUSELAGE SKIN AT STA 415 BETWEEN S-21R TO S-22R MISREPAIRED. REPAIRED IAW SRM 53-00-01, REPAIR 15. CATEGORY "B" MAJOR REPAIR.SDR FDEA201201170232Panel · crackedSLAT NR 2 OTBD MAIN TRACK, COVE PANEL CRACKED. REMOVED CRACKED COVE PANEL AND INSTALLED NEW IAW-SRM-51-40-02. MAJOR,CAT A REPAIR.SDR FDEA201201130161Panel · crackedSLAT NR 1 COVE PANEL AT INBD AUX TRACK HAS A CRACK AT INBD FASTENER HOLE. REMOVED CRACKED PANEL AND INSTALLED NEW COVE PANEL IAW 51-40-02. MAJOR REPAIR.SDR FDEA201201130163Panel · crackedNR 1 SLAT INBD AUX TRACK, COVE PANEL CRACKED. REMOVED DAMAGED COVE PANEL IAW SRM 51-40-02, FABRICATED NEW COVE PANEL. INSTALLED NEW COVE PANEL ON SLAT NR 1 IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201201070042Fairing · corrodedRT WING TB FAIRING 192AR CORRODED CIRCUMFERENCE OF PANEL AT FASTENER HOLES. CHECKED LIMITS OF ALL REWORKED AREAS. FOUND IN LIMITS EXCEPT 1 EA SPOT AT RBL 2.75 ORIGINAL THICKNESS .075 REMAINING THICKNESS .042 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II, LSDR 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.SDR FDEA201201060036Bulkhead · chafedAPU COMPT FWD BULKHEAD CHAFED FS -1885-RT SIDE 7". REPAIRED IAW SRM-53-80-08, FIG 101, REPAIR NR2 AND SRM-51-40-02, CATEGORY A MAJOR REPAIR.SDR FDEA201201060035Bulkhead · chafedAPU COMPT FWD BULKHEAD HAS CHAFE MARKS, FS 1885 RT SIDE 7". REPAIRED IAW-SRM-53-80-08, FIG 201, REPAIR 2.SDR FDEA201201060031Skin · dentedRT LOWER FUSELAGE SKIN HAS DENT AT BS 745, S25R. DENT DIMENSIONS= A=2.5" Y=.002 A/Y=1250, FOUND TO BE OUT OF LIMITS, ACCOMPLISHED SKIN IAW SRM-53-00-01, FIG 201, CAT B MAJOR REPAIR.SDR FDEA201201050024Seat Track · corrodedBS 418-440, RBL 45 SEAT TRACK CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .090 AFTER REWORK L=2.5 W=1.5 D=.090 MATERIAL REMAINING .000 FOUND OUT OF LIMITS IAW SRM 53-00- 52. REMOVED SEAT TRACK AT STA 418-440 RBL 45 IAW SRM 51SDR FDEA201201040018Fitting · corrodedSTA 440 RBL 45 SEAT TRACK FITTING CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .200 AFTER REWORK L=2.5 W= 1.0 D= .023 REMAINING MATERIAL .177 FOUND OUT OF LIMITS IAW SRM 53-00- 01. REMOVED SEAT TRACK FITTING IAW SRM 51-40-02SDR FDEA201112235439Stringer · corrodedSTRINGER BS 418.00 TO 440.0, S22R CORRODED. REMOVED CORROSION IAW SRM 51-10-02 . ORIGINAL MATERIAL .040 REMAINING .030, FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II. R & R STRINGER IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201112215410Frame · corrodedAFTER REMOVAL OF FLOOR SUPPORT AT STA 1500, RBL 2.50 FOUND CORROSION ON FRAME IN AFT CARGO PIT. REMOVED CORROSION AT FRAME IAW SRM 51-10-02. BLENDED AREA. ORIGINAL MATERIAL .063, MATERIAL LOSS .033, MATERIAL REMAINING .030. FOUND OUT OF LIMITS IAW SRM 53-SDR 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.SDR 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 IASDR FDEA201112205389Frame · misrepairedFRAME BS 800 BETWEEN S28L TO S28R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.SDR 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.SDR FDEA201112195371Skin · misrepairedSKIN AT BS 395, S17R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 316, CAT "B" MAJOR REPAIR.SDR FDEA201112175325Seat Track · corrodedSEAT TRACK GOUGED/CORRODED, RBL24 BS418-440. REMOVED DAMAGE AND CHECKED LIMITS. FOUND TO BE OUT OF LIMITS L=3" W=1" D=.025. ORIGINAL MATERIAL .090 AFTER REWORK .065 IAW SRM 53-00-52 FIG 101. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, STA 418-440, RBL 24. MASDR 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 REPSDR FDEA201112135256Frame · gougedFUSELAGE UPPER LOBE INTERIOR BS 365 STR 8-9R FRAME GOUGED. COMPLIED WITH EA F-5310-157243, "CAT A MAJOR REPAIR".SDR FDEA201112095234Seat Track · gougedRBL 45 SEAT TRACK GOUGED BS 1180 -1280. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 AND IAW DWG 146N5120, INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201112085219Support · corrodedBS 365-418 RBL 24, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS ORIGINAL MATERIAL .070 AFTER REWORK L=2 W=1.5 D=.030 REMAINING MATERIAL .040. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-02, FIG 101, DETAIL VII. INSTALLED NEW SESDR FDEA201112085224Floorbeam · misrepairedFLOORBEAM STA 1661, MISREPAIRED. REMOVED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. FABRICATED FLOORBEAM IAW DWG 146N5110. INSTALLED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201112085218Support · corrodedBS 365-418, RBL 45 SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .070 AFTER REWORK L=2.5 W=2 D=.025 REMAINING MATERIAL .045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. DETAIL VII. INSTALLED NEW SEAT TRACK SUPPOSDR 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 BESDR FDEA201112075209Frame · misrepairedFRAME MISREPAIRED REPAIR AT BS 1480 S24-26L. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1030. MAJOR REPAIR.SDR 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, SDR FDEA201112075204Crease Beam · gougedMAIN CABIN AREA RT SIDE AT BS 1280 CREASE BEAM GOUGED.SDR FDEA201112065178Crease Beam · corrodedRIGHT MAIN DECK CREASEBEAM CORRODED, BS 776. BLENDED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .040 MATERIAL LOSS .050. OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABED INBD CHORD FSDR FDEA201112065177Seat Track · corrodedSEAT TRACK CORRODED AND GOUGED RBL 45 , BS 640 - 440. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR 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.SDR 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.SDR 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 SDR FDEA201112015131Crease Beam · corrodedMAIN DECK RT CREASEBEAM CORRODED BS 660 - 664. BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .050 MATERIAL LOSS .040 MATERIAL OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NSDR 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-SDR FDEA201111295077Skin · damagedFOUND GOUGES, SCRIBE LINES, CORROSION ON SKIN AT BS 1625 TO 1685, S17-18R. UNDER SCUFF PLATE.SDR FDEA201111285098Floorbeam · misrepairedFLOORBEAM STA 377 MISREPAIRED. REMOVED AND REPLACED IAW 51-40-02.SDR FDEA201111255047Intercostal · corrodedUPON REMOVAL OF AFT PIT FRAME FOUND INTERCOSTAL CORRODED STA 1540-1560, BETWEEN S26L AND S26R.SDR FDEA201111225049Frame · misrepairedFRAME STA 1600 BETWEEN S-21R TO S-23R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201111184972Crease Beam · corrodedCREASE BEAM 17L BS 1350 CORRODED. ORIGINAL MATERIAL .100 AFTER BLENDING .065 MATERIAL LOSS .035 MATERIAL OUT OF LIMITS IAW SRM 53-60-13 ALLOWABLE DAMAGE 2 FIG 101 DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201111174951Frame · misrepairedFRAME BS 1420 S24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028.SDR FDEA201111174960Floorbeam · corrodedFLOORBEAM CORRODED BS 1320, BL 0-LBL 24, UPPER TEE. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201111174952Gate · corrodedL2 DOOR LWR GATE CORRODED. REMOVED L2 LOWER GATE IAW AMM 52-11-38. DETERMINTED CORROSION EXCEEDING LIMIT IAW SRM 52-10-02. REMOVED HINGE FROM LOWER GATE IAW SRM 51-40-02. INSTALLED HINGE ON NEW LOWER GATE IAW SRM 51-40-02. INSTALLED GATE ON L2 DOOR BOTTOM
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