Boeing 757-2Y0
Service difficulty reports · 830
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 = '7572Y0' 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 = '7572Y0' 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 FDEA201805161248Switch · failedON SELECTING FLAPS 15 FROM 5, LE SLAT ASYMETERY CAUTION MESSAGE WAS RECEIVED. LE SLAT DISAGREE DISPLAYED AT THE COMPLETION OF THE QRH THE FLAPS WERE SELECTED INTO 30 POSITION VIA THE ELECTRIC. R & R THE LT INBD SLAT LOSS SWITCH IAW MM 27-81-41-4. OPS CHECKEDSDR FDEA201804120970Hydraulic System · overservicedDURING A MAIN DECK CARGO FIRE PROTECTION CHECK, SMOKE CAME OUT BOTH FLIGHT DECK VENT DIFFUSERS. RAN QRH AND SMOKE CLEARED. OPERATED PACKS WITH ENGINES AS PNUEMATIC SOURCE IAW JRH. COULD NOT DUPLICATE SMOKE IN COCKPIT. OPERATED PACKS WITH APU AS PNEUMATISDR FDEA201804040851Skin · delaminatedDURING SANDING, FOUND LEFT WING T/E OTBD AFT FLAP UPPER SURFACE TABS DELAMINATED, WS 481 AFT OF THE NR 3 SPOILER. ACCOMPLISHED PERMENANT REPAIR IAW SRM 57-53-01-2R, TABLE II, AND SRM 51-70-04, PAR 5A1.SDR FDEA201804030838Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HAD TWO DENTS, HSS 127 - 133 AND FOUND TO BE OUT LIMITS. CUT OUT THE DAMAGE & APPLIED PERMANENT REPAIR IAW SRM 51-70-10-2R, REPAIR 3 & 4.SDR FDEA201804030837Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 138 - 143, ONE DENT FOUND OUT OF LIMITS. REMOVED DAMAGE, APPLIED PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.SDR FDEA201804030836Skin · dentedLEFT HORIZONAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT STAB 144 - 150 HAD TWO DENTS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-70-10-2R, REPAIR 3 & 4,SDR FDEA201804030839Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 124 - 130 DENTED OUT OF LIMITS. REMOVED DAMAGE, APPLIED A PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.SDR FDEA201804020828Skin · crackedCRACK GOING OUT FROM SKIN AFT SIDE OF THE NR 1 SLAT FROM FASTENER. COMPLIED WITH EA F-5750-T0339279 P1. FABRICATED TWO REPAIR DOUBLERS, FILLERS & INSTALLED IAW SRM 57-43-01-2R, REPAIR 4.SDR FDEA201803240771Floorbeam · damagedMAIN CABIN FLOORBEAM FWD FLANGE BS 620, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339088.SDR FDEA201803240770Floorbeam · damagedMAIN CABIN FLOORBEAM AT BS 580 FWD FLANGE, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339086, P1.SDR FDEA201803240769Floorbeam · damagedMAIN CABIN FLOORBEAM BS 600 FLOOR PANEL MOUNT HOLE AT APPROX. LBL 40 IS OBLONG. REPAIRED IAW EA F-5310-T0339087.SDR FDEA201803210747Attach Fitting · crackedMAIN CABIN FLOORBEAM ATTACH FITTING AT BS 580, LBL 45 CRACKED IN AFT UPPER FLANGE. REPAIRED IAW EA F-5310-T0338866 P1.SDR FDEA201802010286Transmission · malfunctionedARRIVED AT 210 KIAS, FLAPS SELECTED TO 1, FLAPS DID NOT MOVE, RECIEVED TRAILING EDGE ANNUNCIATORS. USED ALTERNATE FLAPS IAW QRH. REMOVED AND REPLACED THE NR 5 FLAP TRANSMISSION. OPS TESTED GOOD IAW MM 27-51-06-4. FLAPS OPERATE NORMAL. OK FOR SERVICE.SDR FDEA201801120069Warning System · activatedWHEN FLAPS SELECTED TO 1, TE EDGE FLAP DISAGREE LIGHT CAME ON & FLAPS INDICATED UP. RAN QRH AND LANDED WITH FLAPS 20 PERFORMED BFIM 27-51 FT 808 FLAPS AND SLATS NOW OPERATE AND INDICATE NORMAL ALL SELECTED POSITIONS. A/C OK FOR SERVICE.SDR FDEA201711223298Bottle · dischargedNR 1 PASSENGER DOOR ASSIST BOTTLE DISCHARGED, REQUIRES SERVICING. REMOVED AND REPLACED CYLINDER EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.SDR IXXA20171113343Skin · corrodedTHE RIGHT INBOARD FLAP LOWER SKIN HAS SURFACE CORROSION. REMOVED AND REPLACED THE LOWER SKIN PANEL IAW SRM 51-40-08, AND 51-40-05.SDR IXXA20171113342Strap · corrodedCORROSION AROUND THE PERIMETER OF THE APU AIR INLET DOOR PANEL, AND AT THE BS 1787 LAP SEAM IN THE AREA BELOW THE DOOR. REMOVED AND REPLACEDTHE CORRODED FWD FRAME STRAP. REMOVED AND REPLACED THE ANGLES IAW SRM 51-40-02, PAR 4, 7, 9, AND DWG 148N3152.SDR FDEA201710243032Pressure Switch · failedRECEIVED A LT HYD SYS PRESSURE EICAS MESSAGE, ALONG WITH RUDDER RATIO EICAS MESSAGE ON EXTENDING FLAPS TO 1. LEFT HYDRAULIC QTY 1.0, LEFT HYDRAULIC PRESSURE 3100 PSI. R & R THE LT HYD SYS PRESSURE SWITCH IAW AMM 29-11-17-4. LEFT HYD PRESSURE SWITCH OPS ANDSDR IXXA20171109341Skin · corrodedFOUND CORROSION ON THE LT WING UPPER SURFACE VORTEX GENERATORS NR 10, & 14. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW REA 47285REA07.SDR IXXA20171113344Skin · corrodedRIGHT WING INBD FLAP UPPER SURFACE HAS BUBBLED PAINT. CLEANED THE AREA, REMOVED CORROSION IAW SRM 57-53-01. FABRICATED AND INSTALLED A REPAIR IAW SRM 51-70-10, AND SRM 57-53-01.SDR IXXA20171109334Web · corrodedMULTIPLE SPOTS OF CORROSION FOUND IN RT MLG WW VERTICAL WEB BETWEEN BS 1080 - 1100 BL 0. KEEL VERTICAL WEB REPLACED IAW TIN-RE-1705379.SDR IXXA20171109333Web · corrodedMULTIPLE SPOTS OF CORROSION IN THE RT MLG WW ON VERTICAL WEB BETWEEN BS 1160 - 1170, BL 0. THE WEB WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109328Stiffener · corrodedRT MLG WW PRESSURE DECK LONGITUDINAL STIFFENER BS 1150, RBL 9 CORRODED. REPAIRED THE STIFFENER IAW TIN-RE-1705379.SDR IXXA20171109327Stiffener · corrodedRT MLG WW PRESSURE BULKHEAD LONGITUDINAL STIFFENER BS 1156 - 1170, RBL 39 CORRODED IN SEVERAL AREAS, INCLUDING LOWER FLANGE UPPER SIDE. REPAIRED THE STIFFENER.SDR IXXA20171107324Stiffener · corrodedRT MLG WW PRESSURE DECK, LONGITUDINAL STIFFENER, BS 1104 - 1112, RBL 46 CORRODED. ALSO CORRODED ON THE OTBD SIDE OF VERTICAL LEG. THE PRESSURE DECK LONGITUDAL STIFFENER WAS REPAIRED.SDR IXXA20171109337Pressure Deck · corrodedRT MLG WW PRESSURE DECK WEB HAS CORROSION AT BS 1072, RBL 11. REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109332Pressure Deck · corrodedCORROSION IN THE RT MLG WW UPPER WEB BS 1170 - 1178, RBL 54. REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109326Bulkhead Web · corrodedRT MLG WW PRESSURE BULKHEAD WEB BS 1070 - 1178, RBL 54 CORRODED. REPAIRED.SDR IXXA20171107325Bulkhead Web · corrodedRIGHT MLG WW PRESSURE BULKHEAD WEB BS 1077 - 1079, RBL 27 - 32 CORRODED. REPAIRED THE BULKHEAD WEB.SDR IXXA20171109331Stiffener · corrodedLT MLG WW PRESSURE DECK LONGITUDINAL STIFFENER CORRODED BS 1112, LBL 17. THE STIFFENER WAS REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109339Fitting · corrodedRT MLG WW BS 1180, RBL 25 AFT BULKHEAD FLAP ASSEMBLY ATTACH FITTING HAS CORROSION AROUND FASTENER. THE FITTING ASSEMBLY WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109338Fitting · corrodedRIGHT MLG WW BS 1180, RBL 39, AFT BULKHEAD FLAP ASSEMBLY ATTACH FITTING HAS CORROSION AROUND THE FASTENER. THE FITTING ASSEMBLY WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109335Doubler · corrodedDOUBLER FOR PNEU DUCT AT WL 193 AND 198, RBL 19 ON FWD SIDE OF THE BS 1180 BULKHEAD HAS AREAS OF CORROSION. THE DOUBLER WAS REPLACED IAW TIN-RE-1705379.SDR IXXA20171109330Stiffener · corrodedLT MLG WW PRESSURE BULKHEAD LONGITUDINAL STIFFENER CORRODED BS 1097, 1107 -1112, LBL 25. THE LONGITUDAL STIFFENER WAS REPAIRED IAW TIN-RE-1705379.SDR IXXA20171109329Stiffener · corrodedLT MLG WW PRESSURE BULKHEAD LONGITUDINAL STIFFENER CORRODED AT BS 1095.5 - 1112, LBL 32. THE STIFFENER WAS REPAIRED IAW TIN-RE-1705379.SDR IXXA20170929320Window Frame · corrodedUPPER CARGO WINDOW FRAME L21 HAD CORROSION ON THE LOWER TURFACE AREA. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02, PARAGRAPH 7, AND DRAWING 144N3200.SDR IXXA20170927297Window Frame · corrodedUPPER CARGO R8 WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REPAIRED IAW ENGINEERING AUTHORIZATION 47285REA04.SDR IXXA20170927296Window Frame · corrodedUPPER CARGO R5 WINDOW FRAME HAS CORROSION. THE WINDOW FRAME WAS REPAIRED IAW ENGINEERING AUTHORIZATION 47285REA04.SDR IXXA20170927312Window Frame · corrodedUPPER CARGO WINDOW FRAME L7 HAS CORROSION ON THE LOWER SURFACE AREA. THE WINDOW FRAME WAS REPAIRED IAW REA 47285REA04.SDR IXXA20170927310Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME L3 HAS PITTED CORROSION ON LOWER SURFACE AREA. WINDOW FRAME WE REPAIRED IN ACCORDANCE WITH REA 47285REA04.SDR IXXA20170927309Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME L1 HAS PITTED CORROSION ON LOWER SURFACE AREA. WINDOW FRAME WE REPAIRED IN ACCORDANCE WITH REA 47285REA04.SDR IXXA20170927304Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-19 HAS PITTED CORROSION ON LOWER SURFACE AREA. WINDOW FRAME WE REPAIRED IN ACCORDANCE WITH REA 47285REA04.SDR IXXA20170927303Window Frame · corrodedUPPER CARGO WINDOW FRAME R15 HAD CORROSION ON THE LOWER SURFACE AREA. THE WINDOW FRAME WAS REPAIRED IAW REA 47285REA04.SDR IXXA20170927300Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-6 HAS PITTED CORROSION ON LOWER SURFACE AREA.SDR IXXA20171109336Window Frame · corrodedUPPER CARGO WINDOW FRAME CORRODED ON LOWER SURFACE AREA. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02, PARA 7, AND DWG 144N3200.SDR IXXA20170921313Window Frame · corrodedAIRCRAFT GROUNDED FOR HAVY MAINTENANCE. UPPER CARGO WINDOW FRAME L-9 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED LEFT HAND 9 CABIN WINDOW FRAME P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-025 PARAGRAPH 7 AND DRAWING 14SDR FDEA201709162581Fseu · malfunctionedTRAILING EDGE FLAP DISAGREE LIGHT. LOCKED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FSEU BITE PROCEDURE IAW FIM 27-51-00, FIG 104, FOUND NO CURENT FAULTS FOR NR 1 FSEU FOUND FLA FAILDED ON SEVERAL TRIES COULD NOT GET A GOOD BITE ON NR 2 FSEU. REMOVED ANSDR IXXA20171003292Skin · damagedLEFT WING UPPER SURFACE OVERWING FILL PORT FAILED A BOND CHECK. FOUND CORROSION AT FUEL PORT WS 481.5, S6L, REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01. ALLOWABLE DAMAGE 3, DETAIL 1, FIG 101. REPAIRED IAW REA 47285REA02.SDR IXXA20171109340Skin · corrodedCORRODED AREA NEXT TO FASTENER ON THE LT WING OTBD FLAP SKIN LOWER SURFACE JUST INBD OF THE OTBD FLAP HINGE AT WBL 468. REMOVED, FABRICATED A NEW PANEL IAW DWG 11N3600. INSTALLED THE PANEL IAW SRM 51-40-02, PAR 6.SDR IXXA20171006294Window Frame · corrodedUPPER CARGO R3 WINDOW FRAME HAS A CORROSION. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02, PARAGRAPH 4, AND DRAWING 144N3200.
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