Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 2008UALA02297Girt Bar · obstructedDOOR 1L WON'T ARM. FOUND VELCO D-RING NOT SECURED AND CAUGHT IN DOOR GIRT BAR. RESECURED D-RING, DOOR ARMS/DISARMS NORMALLY.SDR 2008UALA02292Frame · dentedAFT PIT AT BS 1540 AND STR 26L, FRAME INBOARD FLANGE DENTED. REMOVED DAMAGE FABRICATED AND INSTALLED RPR IAW 53-00-07 RPR 5.THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC THEREAFTER. INSSDR 2008UALA02280Software · malfunctionedL EICAS STATUS MSG WILL NOT CLEAR. -L EICAS STATUS MSG WILL NOT CLEAR -L EICAS COMP REPLACED EARLIER TODAY. REPLACED L EICAS COMPUTER REF MM 31-41-02 AND LOADED OPS SOFTWARE REF MM31-41-02. MSGS HAVE CLEARED AND ALL DISPLAYS NORMALSDR 2008UALA02268Circuit Breaker · openAPU GEN DOES NOT TAKE L BUSS AUTOMATICALLY WHEN L GEN TAKEN OFF LINE PER CREW. OUND APU BATTERY BUSS CIRCUT BREAKER OPEN. CLOSED BUSS CIRCUT BREAKER . RERACKED BPCU AND APU ECU. ACCOMPLISHED ENG IDLE RUN. POWER TRANSFER CHECKS OK. SDR 2008UALA02266Cover · crackedEEL LIGHT LENS COVER CRACKED FWD OF MAIN ENTRY DOOR 2R BUSINESS CLASS GALLEY. REPLACED LENS/EXIT SIGN.SDR 2008UALA02265Lamp · inoperativeEXTERIOR EMERGENCY LIGHTS HAS 2 INOP LIGHTS, ONE AT THE DPP R R2 AND ONE AT THE LEFT WING. FOUND BULBS OUT/INOP. RELAMPED BULBS, ALL OPS CHECKS OK.SDR 2008UALA02264Feeder Cable · looseA ZONE EEL INOP. FOUND POWER FEEDER WAS LOOSE. RECONNECTED POWER FEEDER AND OPS CHECKED OK.SDR 2008UALA02246Frame · damagedRT FRAME REPAIR WAS ACP'D BS 1681, WL-209. ACCOMPLISHED MAJOR, PER EVA MOC1-8433 REVA. AFTER DTA, THIS REPAIR IS CONSIDERED TO BE A CAT 'A' TIME LIMITED REPAIR. THIS REPAIR MUST BE REPLACED PER REVISED EVA-40093, NO LATER THAN NEXT HMV CURRENTLY SCHEDULED SDR 2008UALA02245Skin · damagedDOUBLER INSTALLED STA 1700 STR 19 TO 20L. SUPPLEMENTAL , REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR DOUBLER AND VERIFIED ALL DAMAGE REMOVED BY HFEC INSPECTION. FABRICATED AND INSTALLED A NEW DOUBLER
AND STRUCTURAL FILLER.SDR 2008UALA02244Connector · looseDOOR 4R EMERGENCY LIGHT INOP BY 107639, RESEATED CONNECTOR. OPS CHK'D OK. RESECURED/RESEATED CONNECTOR, OPS CHECKED NORMAL.SDR 2008UALA02243Wire · damagedEEL STRIP LIGHTS ON SIDE OF COACH SEATS 18C, 22C ARE INOP. FOUND A SHORT IN ASSY WIRING/FIXTURE. REPLACED LIGHT STRIPS, OPS CHECKED NORMAL.SDR 2008UALA02225Wire · cutEEL LIGHT STRIP INOP IN FRONT OF MID AFT LAV. SPLICED EEL STRIP, OPS CHECKED OK.SDR 2008UALA02224Wire · cutEEL LIGHT STRIP INOP IN FRONT OF MID LAV. SPLICED EEL STRIP, OPS CHECKED OK.SDR 2008UALA02206Carbon Seal · failedFLIGHT DIVERTED WITH A FUEL ODOR ON THE FLIGHT DECK. FOUND CARBON SEAL FAILED AT NR 3 BEARING, OIL WETTING OF AREA. REPLACED NR 1 ENG, PERFORMED PACK BURN OUT.SDR 2008UALA02239Skin · puncturedRT WING FIXED L/E UNDER NR 9 OTBD SLAT HAS PUNCTURE AND DENT. REPAIRED FIXED LEADING EDGE UNDER NR 9 SLAT PER SRM 57-41-01 TABLE 3 REPAIR 1 PAGE 207SDR 2008UALA02235Eec · erraticNR 1 ENG EICAS MSG ENG SEC CONT DISPLAYED. REPLACED LEFT ENGINE EEC PER FIM 71-EPCS MSG INDEX S274-24. AND MM73-21-04. CHECKED ALL CONNECTORS ON EEC AND FIREWALL, FOUND OK. RAN ENGINE NO FAULTS.SDR 2008UALA02234Housing · crackedR-1 DOOR HANDLE BOX CRACKED AT CAM MOUNT HOLES. REPLACED HANDLE BOX.SDR 2008UALA02233Battery · inoperativeDOOR L2 EXTERIOR EMERGENCY LIGHT INOP. FOUND BATTERY CHARGER INOP. REPLACED BATTTERY CHARGER, OPS CHECKED NORMAL.SDR 2008UALA02222Frame · dentedAFT PIT STA 1400 STR 26L IS DENTED ON FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 2. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING IN 25,000 FLIGHT CYCLES AND 11,000FC THERE AFTER.SDR 2008UALA02221Frame · chafedAFT PIT STA 1520 AT STR 26L, FRAME CHAFED. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE SDR 2008UALA02220Frame · dentedAFT PIT STA 1420, STR 27L HAS 1 FRAME DENT. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 2. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING IN 25,000 FLIGHT CYCLES AND 11,000FC THERE AFTER.SDR 2008UALA02219Frame · dentedAFT PIT STA 1440 HAS 3 EACH DENTS STRINGER 26L - 24L. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,00SDR 2008UALA02218Frame · dentedAFT PIT STA 1500 STR 26L FRAME HAS 1 DENT. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC THERE ASDR 2008UALA02217Frame · dentedAFT PIT STA 1580 STR 22R HAS DENTED FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC THERE SDR 2008UALA02216Frame Splice · gougedAFT PIT STA 1520 FRAME SPLICE GOUGED BETWEEN STR 22R AND 24R. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES ANSDR 2008UALA02215Frame · dentedAFT PIT STA 1600 RT SIDE STR 24R HAS DENTED FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC TSDR 2008UALA02214Frame · dentedAFT PIT BS 1540, FRAME INBOARD FLANGE DENTED AT STR 24R. REMOVED DAMAGED FABRICATED RPR AND INSTALLED IAW SRM 53-00-07 RPR 5 TABLE II THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES ANDSDR 2008UALA02213Skin · damagedL2 DOOR UPPER ARM CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: PERFORMED INSURANCE CUT & INSTALLED DOUBLER REPAIR.SDR 2008UALA02212Skin · damagedR2 DOOR UPPER HINGE ARM CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: PERFORMED INSURANCE CUT & INSTALLED DOUBLER REPAIR.SDR 2008UALA02179Wire · arcedSMOKE AND ARC'S IN FWD GALLEY PER CREW. FOUND WIRE ON TOP OF COFFEE MAKER M10 THAT HAD BEEN GROUNDED AND ARCING. REPLACED COFFEE MAKER M10-ALL OPS WERE GOOD
SDR 2008UALA02194Crease Beam · corrodedRT CREASE BEAM CORRODED AROUND SEVERAL FASTENERS AT STA 1183, RBL 67, WL 208.10. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM.SDR 2008UALA02196Heat Exchanger · leakingLEFT ENGINE OIL LEAK OUT OF LIMITS. LEAK FROM NR 5 DRAIN. FOUND LEAK AT FUEL OIL HEAT EXCHANGER. REMOVED NR 1 ENG FUEL OIL HEAT EXCHANGER AND BYPASS VLV. REPLACED, LEAK CHECKED AND ENGINE RUNS WERE GOOD.SDR 2008UALA02195Gate · corrodedR2 DOOR LOWER GATE HAS CORROSION AROUND LUG FTG HOLES. REPLACED GATE PER SRM 51-40 -02.SDR 2008UALA02193Light · missingEMERGENCY EXIT LIGHT STRIP MISSING AT 34C. FOUND MISSING STRIP AND RESECURED IT. OPS TESTED OK.SDR 2008UALA02192Fuse · blownEEL LIGHTS INOP AT ROW 16 THRU 20. FOUND INVERTER FAULTY, BLOWN FUSE. REPLACED EEL LIGHT INVERTER M10830, BLOWN FUSE IN M10770 EMER LIGHT PWR SUPPLY AND LAMP IN BULLNOSE AT SEAT 14ABC. EEL LIGHTS AT ROW 16-20 AND AISLE LIGHT AT 14ABC. CHECKS OKSDR 2008UALA02197Feeder Cable · shortedEEL LIGHTS STRIP INOP FROM ROW 31 TO 34. FOUND A SHORT IN THE EEL STRIP. REPLACED EEL LIGHT STRIPS, OPS CHECKS OK.SDR 2008UALA02168Oxygen Mask · faultyCAPTAIN'S OXYGEN RESET SWITCH STICKY. REPLACED CAPTS WITH OBSERVERS O2 MASK ASSY CHECKS OK
SDR 2008UALA02166Frame · dentedAFT PIT STA 1540, BETWEEN STR 25L AND 27L FRAME DENTED (3 EA DENTS). AFT PIT STA 1540, BETWEEN STR 25L AND 27 L FRAME DENTED (3 EA DENTS) REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTING AT 50000 TOTAL FLISDR 2008UALA02165Frame · dentedAFT PIT STA 1480, STR 26L FRAME DENTED. AFT PIT STA 1480, STR 26L FRAME DENTED. REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTING AT 50000 TOTAL FLIGHT CYCLES AND 12000FC THERE AFTER .SDR 2008UALA02164Structure · crackedCRACK INDICATION UNDER FLAKING TEFLON PAINT ON UPPER SURFACE OF THE RT WING FIXED LEADING EDGE BELOW NR 10 SLAT. REMOVED DAMAGED AREA APPLIED A PRE-PREG FIBERGLASS REPAIR IAW SRM 57-41-01 AND 51-70-07SDR 2008UALA02163Bolt · out of rigCAPTAIN'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: EXCESSIVE BACK PRESS REQUIRED ON TO. 3.3 SET OVER 6 UNITS REQUIRED TO TRIM OUT PRESSURE. OK IN FLT. FOUND CAPTAINS AFT QUADRANT STOP BOLT OUT OF RIG. REMOVED ONE WASHER AT STOP BOLT. RECHECKED AFTER RISDR 2008UALA02158Wire · damagedWHEN CHECKING FIRST OFFICERS WIPER MOTOR FOR OPERATION, FOUND STRONG ELECTRICAL ODOR AND SMOKE COMING FROM BACK OF FIRST OFFICER'S INSTRUMENT PANEL. EXTINGUISHED FLAMES WITH FIRE EXTINGUISHER BOTTLE. FOUND SHORTED WIRING IN HARNESS LEADING TO WIPER MOTOR- FOSDR 2008UALA02198Oxygen System · reads lowCREW OXYGEN LOW. SERVICED CREW OXYGEN TO 1500PSI, NO LEAKS WERE NOTED AT TIME OF SERVICE.SDR 2008UALA02157Slide · inoperativeDOOR 1L ARMED LIGHT DOES NOT COME ON. REPLACED DOOR 1L SLIDE LIGHT ASS'Y. OPS CK NORMAL.SDR 2008UALA02156Warning Message · illuminatedEICAS MESSAGE 'R ENG PRI CONT' DISPLAYED. REPLACED THE NR 2 ENGINE PERFORMED ALL REQUIRED TESTS AND RUNS, PERFORMED A SATISFACTORY VERIFICATION FLIGHT. NO REPEATS.SDR 2008UALA02136Squib · noneRIGHT NUMBER ONE EMERGENCY ESCAPE SLIDE DOES NOT TEST ON SQUIB PANEL. TESTED SQUIB 20 TIMES, OPS CHECKS GOOD EVERY TIME.SDR 2008UALA02123Motor · malfunctionedFLIGHT DIVERTED DUE TO A CABIN PRESSURIZATION PROBLEM. REPLACED AC MOTOR ASSY AND NR 2 AUTO PRESSURE CONTROLLER, OPS CHECKED GOOD, NO REPEATS.SDR 2008UALA02155Skin · damagedDOOR 2L UPPER HINGE ARM CUT OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D HFEC. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 2008UALA02154Skin · damagedDOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D HFEC. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 2008UALA02153Wire · deteriorated"R" LAV SMOKE DETECTOR WIRE DETERIORATED. REPLACED BOTH WIRES FOR SMOKE DETECTOR IN "R" LAV. OPS CHECKED GOOD.
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