Boeing 757-2T7
Service difficulty reports · 666
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 = '7572T7' 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 = '7572T7' 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 FDEA201002250513Floor Support · corrodedAFT CARGO FLOOR SUPPORT, RBL 11.40 STA 1498 TO STA 1640, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED SUPPORT R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002250512Fitting · corrodedAFT CARGO STA 1375 STRINGER 23L SLOPE PANEL SUPPORT FITTING FOUND CORROSION. SUPPORT FITTING AT CARGO FOUND CORRODED THROUGH. FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002250511Attach Fitting · corrodedFWD CARGO COMPARTMENT FLOOR SIDE PANEL RBL 19.00 ATTACHED TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED AT STA 620. TIE-DOWN AT FWD CARGO STA 620, RBL 19 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002250510Floor Support · corrodedAFT CARGO FLOOR SUPPORT, RBL 7.55 STA 1200 TO STA 1341, FASTENER HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT FROM STA 1200 TO STA 1341, RBL 7.55, R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201002240507Skin · misrepairedEXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT BS 760 TO BS 780, STR 4R TO STR S5R. TO EVALUATE EXISTING REPAIR DOUBLER, REMOVED AND CARRIED OUT REPAIR IAW STA ENG EA NR 757-5331-08-E0641 REV A (SHORT EDGE MARGIN ON SKIN AT BETWEEN STA 700 AND STA 780, SDR FDEA201002240501Support Fitting · corrodedFWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED STA 615. CORRODED RETAINERS ON SCUFF PLATE FITTING AT STA 615 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002240500Retainer · corrodedFWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED STA 600. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002240499Retainer · corrodedFWD CARGO DOOR CUTOUT LOWER SCUFF PLATE SUPPORT FITTING RETAINERS FOUND WITH SURFACE CORROSION AS MARKED, STA 560. CORRODED RETAINERS AT STA 560. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002180446Panel · corrodedRUDDER EXTERIOR SURFACE LT BONDED CONDUCTIVITY FRAME WITH LIGHT SURFACE CORROSION BETWEEN RUDDER STA 381.269 TO STA 578.536. CORROSION REPAIR CARRIED OUT IAW EA NR F-5540-137419. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201002090376Floor Support · corrodedCORROSION ON FLOOR SUPPORT AROUND 2 EA ANCHOR NUT HOLE AT STA 1020-1030 RBL 64. FLOOR SUPPORT REPAIRED IAW SRM 51-70-12 FIG 1 REV. 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201002080363Frame · corrodedE & E DOOR ASSY SIDE FRAME AREA FOUND WITH CORROSION AS MARKED. R & R IAW SRM 51-40-02, REV. 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201002080362Floor Support · corrodedAFT CARGO FLOOR SUPPORT, RBL 7.55 STA 1445 TO STA 1498, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED AFT CARGO FLOOR SUPPORT FROM STA 1445 TO STA 1498, RBL 7.55. R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-1-200 CRITERIA.SDR FDEA201002080361Floor Support · corrodedAFT CARGO FLOOR SUPPORT, RBL 2.90, STA 1445 TO STA 1498, FASTENERS HOLE AREA CORROSION AS MARKED. CORRODED FLOOR SUPPORT IN AFT CARGO FROM STA 1445 TO STA 1498, RBL 2.9, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFED AS MINOR GMM 6-2-100 CRITERIA.SDR FDEA201002080360Angle · corrodedCABIN: R4 PAX DOOR SILL "L" ANGLE IS CORRODED AT AFT DOOR FRAME. CORRODED L-ANGLE ON R4 PAX DOOR SILL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201002080359Stanchion · corrodedAFT CARGO COMPARTMENT WITH LIGHT CORROSION AT RT STANCHION LOWER MOUNT AT BS 1440, RBL 19, ADJACENT TO STR 23R. STANCHION LOWER MOUNT AT AFT CARGO STA 1440, RBL 19 FOUND CORRODED THROUGH. STANCHION REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLSDR FDEA201002080358Hinge · crackedAFT CARGO DOOR CUTOUT E6 RACK COVER LOWER HINGE FOUND CRACKED AT STA 1440. CRACKED HINGE AT AFT CARGO DOOR CUTOUT R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201002030318Support · crackedAFT CARGO LT FRAME AT STA 1560 LOWER SIDEWALL SUPPORT FOUND CRACKED AT FASTENER HOLE AREA. CRACKED LT SIDEWALL SUPPORT AT STA 1560 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRTIERIA.SDR FDEA201002030317Stiffener · corrodedCABIN: R4 PAX DOOR SILL BRACKETS CORRODED 12" AND 15.5" FROM FWD LOWER END OF DOOR FRAME. CORRODED BRACKETS ON R4 DOOR SILL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201002020308Seat Track · corrodedCABIN FLOOR AFT RT INBD SEAT TRACK WITH LIGHT SURFACE CORROSION AT BS 1640, RBL 24. CORROSION ON SEAT TRACK AT BS 1640, RBL 24, FOUND OUT OF SRM LIMITS. SEAT TRACK R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201002010298Panel · crackedLT PYLON CRACK FOUND ON THE FWD LOWER CORNER OF PANEL NR 433 GR CUTOUT. REPAIRED IAW EA NR F-5450-135807. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201001310294Fitting · crackedLT ENG PYLON, 2 EACH CRACKS FOUND IN LT AFT INBD BOLT HOLE ON HORIZ FLANGE. (REF: EO F-5450-7-5006 P1 PG 13 STEP 2 FOR DETAILS). LT PYLON AFT BULKHEAD R & R IAW EA NR F-5450-135814. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201001310293Sill · corrodedCABIN: 2L PAX DOOR SILL CHORD HAS EXFOLIATION CORROSION 7" FWD OF AFT DOOR FRAME. CORRODED SILL CHORD FWD OF L2 DOOR AFT DOOR FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201001260262Cargo Track · corrodedAFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1377 LT. CORRODED TIE-DOWN FITTING AT STA 1377 IN AFT CARGO COMPARTMENT REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CSDR FDEA201001260261Angle · corrodedAFT CARGO AFT BULKHEAD STA 1720 AREA, RT ANGLE FOUND WITH CORROSION AS MARKED. CORRODED ANGLE AT BULKHEAD STA 1720 REMOVED AND REPLACED IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201001260260Fitting · crackedNR 1 PYLON, ONE EACH CRACK FOUND AT FWD OTBD HOLE OF MID BULKHEAD. REFER EO F-5450-7-5005 P1 PG 19 STEP 1.8 FOR DETAILS. CRACKED FWD OTBD HOLE ON NR 1 PYLON MID BULKHEAD REPAIRED IAW EA NR F-5450-135810 (LT PYLON MID-BULKHEAD LOWER FLANGE INBD CRACK REPAIR). SDR FDEA201001260259Fitting · crackedRT ENGINE PYLON, 2 EACH CRACKS FOUND IN RT AFT INBD BOLT HOLE ON HORIZONTAL FLANGE. REF EO F-5450-7-5006 P2, PG 12 STEP 2. RT PYLON AFT BULKHEAD R & R IAW EA F-5450-135815 (AFT BULKHEAD FITTING REMOVAL AND INSTALLATION). REPAIR IS CLASSIFIED AS MAJOR IAW GSDR FDEA201001250234Plate · corrodedCORROSION ON DECK PLATE AT STA 1715, LBL 25. CORROSION REPAIR CARRIED OUT ON DECK PLATE AT STA 1715 IAW EA F-5320-135812 (BS 1715, LBL 25 AFT DECK PLATE CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201001200201Skin · crackedRT WING PYLON PANEL 443AR (RT SIDE) CUTOUT FOUND CRACKED AT PP STA 106.75 LWR FORWARD RADIUS OF PANEL CUTOUT AREA. CANNOT DETERMINE LENGTH. CRACK EXTENDS BEHIND INTERNAL STRUCTURE. REPAIRED IAW EA F-5450-135806. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR FDEA201001200200Panel · crackedRT WING PYLON PANEL 443GL CUTOUT FOUND CRACK AT PP STA 106.75 LWR FWD RADIUS OF PANEL CUTOUT AREA. CANNOT DETERMINE LENGTH. CRACK EXTENDS BEHIND INTERNAL STRUCTURE. REPAIRED IAW EA NR F-5450-135808. RT PYLON INBD STRUT SKIN PANEL REPAIR. REPAIR IS CLASSIFSDR FDEA201001200195Splice · corrodedAFT CARGO RT SIDE PANEL SPLICE AT STA 1530 FOUND CORROSION. CORRODED SPLICE AT AFT CARGO STA 1530, RT PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201001070043Support Bracket · crackedFWD CARGO AT LT STA 843, STR 22L AREA FOUND SUPPORT BRACKET CRACKED. CRACKED BRACKET AT STA 843, STR 22L REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201001070042Skin · crackedLT PYLON LWR PAN CRACK AT LT SIDE PP STN 277. CRACKED PAN ON LT PYLON AT PP STN 277. REMOVED AND REPLACED IAW SRM 51-40-02, REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201001060026Access Panel · crackedENGINE NR 1 PYLON STRUT LT SKIN AT ACCESS PANEL CUTOUT (433AL), FLANGE LOWER FWD CORNER CRACK. REPAIRED IAW EA NR F-5450-135803. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201001060025Shim · crackedLT PYLON UPPER PANEL 433DL FWD SUPPORT BRACKETS SHIMS CRACKED AND ANCHOR NUTS CORRODED. CRACKED SHIMS (BONDING STRIP) AND CORRODED ANCHOR NUTS ON LT PYLON UPPER PANEL 433DL REMOVED AND REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6SDR FDEA201001040006Bracket · crackedLT PYLON UPPER AREA BRACKET FOUND CRACK AT PP STN 174 RT SIDE. CRACKED BRACKET AT PP STA 174 ON LT PYLON REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912234503Shim · crackedLT PYLON UPPER PANEL 43ALL FWD SUPPORT BRACKETS SHIMS CRACKED AND ANCHOR NUTS CORRODED. LT PYLON UPPER PANEL 43ALL FWD SUPPORT BRACKET DOUBLER SHIMS AND ANCHOR NUTS REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912214488Bracket · crackedLT PYLON AFT FAIRING UPPER SUPPORT LT BRACKET CRACK AT PP STA 208. CRACKED BRACKET ON LT PYLON AFT FAIRING UPPER SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912214487Bracket · crackedLT PYLON VERTICAL STIFFENER BRACKET CRACK AT PP STA 166 RT SIDE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912174482Intercostal · crackedCABIN - INTERCOSTAL AT FLOORBEAM STA 1320, RBL 45 FOUND CRACKED. CRACKED INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912174481Intercostal · crackedCABIN - INTERCOSTAL AT FLOORBEAM STA 1320, LBL 25 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912174480Angle · corrodedCABIN - 2L PAX DOOR SILL AFT "L" ANGLE HAS CORROSION. CORRODED L-ANGLE ON L2 PAX DOOR SILL R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912174479Support Bracket · corrodedCORROSION ON L1 DOOR SCUFF PLATE FWD AND AFT EDGE SUPPORT BRACKET. REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200912074372Floorbeam · corrodedCABIN - CORROSION ON FLOORBEAM AT STA 300, RBL 26-30. CORRODED FLOOR PANEL SUPPORT AT STA 300, RBL 26 TO RBL 30, R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR ANCF200800032Landing Gear · malfunctionedAIR TURN BACK, EICAS MSG GEAR DISAGREE AND GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. LT GEAR LIGHT, GEAR AMBER LIGHT AND DOORS AMBER LIGHT ILLUMINATE. IAW AMM 32-20-09 FIM PROCEDURE THE PSBU BITE TEST WAS PERFOMED AND NO FAULT CODE AND MAIN NLG PINS WERE REMOSDR ANCF200800008Warning Light · illuminatedFLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO THE RIGHT TO CENTER COLUMN. FIM PROCEDURE 27-81-00 FIG 105 WAS ACCOMPLISHED. IN ACCORDANCE AMM 27-51-01/201 FLAP SLAT ELECTRONIC UNIT NR 1 ASDR ANCF200800004Air Duct · leakingEICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIALLY AFTER THRUST REDUCTION BUT AFTER FEW SECONDS IT ILLUMINATED AGAIN). PERFORM FIM 26-11-00 AND FSDR ANCF200700015Filter · dirtyDURING CLIMB CROSSING FL 300 ASC TO FL 370, HAD SMOKE COMING FROM THE PEDALS IN THE COCKPIT. CHECK LIST WAS PERFORMED AND THEN DECIDED GOING TO MIA BECAUSE OF THE SMOKE AND ALSO THE CABIN CREW TOLD US THAT THERE WAS A LOT OF SMOKE IN THE PASSENGER CABIN. WHESDR ANCF200600046Engine · failedLT ENGIINE SURGED DURING CONSTANT POWER DURING CLIMB AT 6.000 FT. ENGINE OPS NORMAL AFTER SURGE AT LOW THRUST. BOROSCOPE INSPECTION ACCOMPLISHED TO INTERMEDIATE PRESSURE COMPRESOR, HIGH PRESSURE COMPRESOR, COMBUSTION CHAMBER, HIGH PRESSURE TURBINE BLADES, LOSDR ANCF200600034Access Panel · loosePILOT REPORT: RT ENG COVER UPPER SIDE SEPARATE DURING TAKE OFF. RT ENG INSPECTED. NO VISIBLE DAMAGE FOUND INTERNAL WING, EMPENNAGE AND FUSELAGE SKIN WERE INSPECTED NO FINDINGS, IAW AMM 05-51-18 PAG 204. THE PANEL 442AL WAS INSTALLED IAW AMM 54-52-01 PAG 401.SDR 513NA0011Warning Light · illuminatedABORTED TAKEOFF DUE TO SPOILER MASTER CAUTION LIGHT. PERFORMED BITE PROCEDURE, RESET SYSTEM BY FIM 27-61-00. OPERATIONAL CHECK OK. NEXT FLIGHT: SPOILER OVERHEAD LIGHT AND EICAS MESSAGE CAME ON IN FLIGHT. NO ADVERSE FLIGHT CONTROLS NOTICED. ACCOMPLISHED BIT
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