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 2005UALA00665Shear Tie · damagedSHEAR TIE AT FS 580, STR 14L-15L HAS OVERSIZE FASTENER HOLE. MANUFACTURED SHEAR TIE PER TIMCO EA REO-G10727, REV 1R, UA-EVA-50456.SDR 2005UALA00664Skin · dentedAPPROX 8 INCH FWD OF C2 DOOR CUTOUT NEAR UPPER CORNER, AIRCRAFT SKIN HAS LARGE DENT. CUT OUT DAMAGE AREA, ACP NDT HFEC INSPECTION, NO CRACK FOUND. FABRICATE AND INSTALL DOUBLER REPAIR PER TIMCO EA REO-G10749, REV A, UA-EVA-50463.SDR 2005UALA00662Frame · dentedFRAME 600 IS DENTED AT STRINGER 23L. TRIM OUT DAMAGE, ACP HEFC INSP, NO CRACK NOTED. REPAIRED PER GSO EA G10674 REV B.SDR 2005UALA00661Shear Tie · damagedSHEAR TIES AT FUSELAGE STA 600 STR 16L-18L HAS OVERSIZE FASTENER HOLES. FABRICATE AND REPLACE SHEAR TIES PER TIMCO EA REO-G10727 AND MM 51-40-02.SDR 2005UALA00663Packing · leakingRETURNED TO FIELD DUE TO INDICATION OF LOSS OF HYDRAULIC FLUID. HYDRAULIC FLOW LIMITER PACKINGS WERE LEAKING AT THE UNIONS, THE PACKINGS WERE REPLACED. THE LEFT HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE.SDR 2005UALA00660Power Supply · dischargedEMERGENCY LIGHTS INOP AT FOLLOWING LOCATIONS: AISLE LIGHT IN BULLNOSE AT ROW 25, CEILING EXIT SIGN AT ROW 16 AND EXTERIOR SLIDE LIGHT ON AFT CARGO DOOR. POWER SUPPLIES LOW CHARGE, REPLACED.SDR 2005UALA00659Connector · brokenEEL TEST SWITCH ABOVE 2L DOOR BROKEN CONNECTOR. BROKEN CONNECTOR ON EEL TEST SWITCH. REPLACED SWITCH.SDR 2005UALA00657Apu · inoperativeRETURNED TO THE FIELD AT SFO AFTER THE APU WOULD NOT START AT TOP OF CLIMB. APU WAS REMOVED FROM AIRCRAFT AND TESTED IN APU TEST CELL. NO FAULT FOUND WITH APU S/N 61832. PASSED ALL TEST AND RETURNED TO SERVICE. AFTER APU REPLACEMENT, MECHANIC FOUND APU BATTSDR 2005UALA00650Wire · damagedEEL JUMPER AND FEEDER DAMAGED AT STA 895. DAMAGED EEL CABLE WAS REPLACEDSDR 2005UALA00649Skin · damagedFUSELAGE STATION 1595, STR 19R IS DAMAGED. THE REPAIR WAS MODIFIED PER EVA IND-3213A TO REPLACE RIVETS WITH HILOCKS ON THE STRINGER ROW. PERMANENT REPAIR PER SRM 53-00-01 PG 206-208.SDR 2005UALA00648Skin · damagedFUSELAGE STATION 1598, STR 19R HAS DAMAGE. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACE REPAIRED DOUBLER AT FUSE STA 1598, STR 19R PER TIMCO EA REO-G10703 AND UA-EVA-50446.SDR 2005UALA00790Light · inoperativeEEL AT 1-R DOOR INTERIOR AND EXTERIOR INOP. REPLACED EXIT LIGHT.SDR 2005UALA00642Radar · failedWEATHER RADAR FAILED JUST AFTER TAKEOFF. FLIGHT DIVERTED DUE TO THUNDERSTORMS. MAINTENANCE REPLACED THE RADAR ANTENNA ASSY (P/N 2041444-0401). THE COMPONENT SHOP TESTING DID NOT REVEAL ANY FAILURES, HOWEVER THE AZIMUTH GEAR ASSY WAS FOUND WITH WATER CONTAMISDR 2005UALA00623Wire · tornEEL FEEDER MID CABIN BY L2 DOOR IS TORN. REPLACED EEL STRIP.SDR 2005UALA00613Skin · dentedEXTERNAL FUSELAGE SKIN DENTED 1 INCH BELOW FLOOR LEVEL AND 10 INCHES FORWARD OF 2 LT MED. MAJOR REPAIR WAS ACCOMPLISHED PER UA-EVA-50430.SDR 2005UALA00606Wire · damagedRETURNED TO FIELD DUE TO AIR/GROUND SENSOR FAILURE, MANUAL GEAR RETRACTION. FOUND TRIPPED SYS 2 AIR GROUND CB AND CHAFED WIRE IN P37 PANEL (W1270-5852-22).REPLACED CIRCUIT BREAKER AND ACCOMPLISHED REPAIR OF DAMAGED WIRE.SDR 2005UALA00655Fan · failedSTRONG ODOR IN REAR OF CABIN ON TAXI OUT. RIGHT RECIRC FAN FAILED. DEFERRED PER MEL, THEN REPLACED FAN. OPS CHECK OK. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA00596Smoke · detectedRETURNED TO THE FIELD DUE TO SMOKE IN THE COCKPIT. CAUSE OF INCIDENT WAS A FAILED THRUST DISK & BEARING IN LT ACM. COMPONENT FINDINGS WERE A FAILED THRUST DISK & A FAILED BEARING WHICH ALSO DAMAGED TURBINE & COMPRESSOR SECTIONS. THRUST DISK, BEARING TURBINESDR 2005UALA00646Skin · lightning strikeTOP OF FUSELAGE HAS 2 LIGHTNING STRIKES. REMOVED DAMAGE AND MANUFACTURED REPAIR REF SRM 53-00-01.SDR 2005UALA00533Frame · dentedAFT PIT LT SIDE STA 1540 HAS 3 EACH DENTS BETWEEN STR 25L AND 26L, ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED NEW PRODUCTION SPLICE ANGLE PER TIMCO REO (EVA) G10550, REV. B.SDR 2005UALA00532Engine · malfunctionedDIVERTED DUE TO RT ENGINE OIL QTY AND PRESSURE IND. RT ENGINE SHUTDOWN. IN CRUISE LOSS OIL QTY & PRESSURE. CREW SHUTDOWN ENGINE. UPON LANDING FOUND EXHAUST OIL WETTED. ENGINE REMOVED. UPON DISASSEMBLY OF ENGINE FOUND NR 5 BEARING BAY HEAVILY COKED & NR 5 SCASDR 2005UALA00551Relief Valve · leakingEES WAS TEST FIRED AND PRESSURE RECORDED GOOD. HOWEVER, THE BOTTOM TUBE WENT FLAT WITHIN 5 MINUTES OF INFLATION PRESSURE RELIFE VALVE FOUND LEAKING. PRESSURE RELIEF VALVE ASSEMBLY WAS REPLACED.SDR 2005UALA00527Attach Angle · crackedFWD NOSE AREA STA 202 BULKHEAD, RT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER REAR SIDE OF BULKHEAD, RBL 30-36. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U2 AND INSTALLED PER SRM 51-40-2.SDR 2005UALA00526Attach Angle · crackedFWD NOSE AREA, STA 202 BULKHEAD, LT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER SIDE LBL 36 AREA, REAR SIDE OF BULKHEAD. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U1 AND INSTALLED PER SRM 51-40-2SDR 2005UALA00525Terminal Block · crackedRETURNED TO FIELD DUE TO MULTIPLE CB'S TRIPPED PRIOR TO ROTATION, MULTIPLE EICAS MSG'S. LEFT GENERATOR CONTACTOR, C901, PHASE -B- TERMINAL LUG WAS FOUND CRACKED / BROKEN, PROMOTING ELECTRICAL PROBLEMS AND CAUSING SOME CIRCUIT BREAKERS TO POP. THE TERMINAL LUSDR 2005UALA00524Floorbeam · corrodedRIGHT SIDE BS 1640 FLOORBEAM, RBL 0 - RBL 60, TOP CAP IS CORRODED. DAMAGE DUE TO CORROSION IN TYPICAL WET AREA. REMOVED CORRODED REPAIR STRAP AND INSTALLED NEW REPAIR STRAP.SDR 2005UALA00523Floorbeam · corrodedFLOORBEAM CORRODED AT STA 367, RBL 56 UPPER SURFACE. REPLACED SUPPORT 141N5161- 52 PER SRM 51-40-02.SDR 2005UALA00511Skin · dentedDENT IN FUSELAGE FROM APPROXIMATELY STATION 1720 TO 1701. DENT IS BETWEEN STRINGER 22L & 23L. INSTALLED DOUBLER PER SRM 53-00-01 REPAIR NR 3.SDR 2005UALA00505Frame · dentedAFT PIT LT SIDE STA 1440 FRAME HAS A DENT ON INBOARD FLANGE BETWEEN STR 25L AND 26L. REPAIRED FRAME WITH A FABRICATED PRODUCTION SPLICE ANGLE DOUBLER PER TIMCO REO(EVA) G10548, REV B.SDR 2005UALA00504Frame · dentedAFT PIT STA 1480 FRAME HAS DENT ABOVE STR 26L ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED NESTED J-ANGLE PER TIMCO REO(EVA) G-10556, REV. C.SDR 2005UALA00503Frame · dentedAFT PIT STA 1520 FRAME HAS DENT BETWEEN STR 25L AND 26L ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED PRODUCTION SPLICE ANGLE DOUBLER PER TIMCO REO(EVA) G10549, REV B.SDR 2005UALA00502Frame · dentedAFT PIT LT SIDE AT STA 1460, FRAME HAS DENT ON INBOARD FLANGE BETWEEN STR 25L-26L. REPAIRED FRAME WITH FABRICATED PRODUCTION SPLICE ANGLE-DOUBLER PER TIMCO REO(EVA) G10547, REV. B.SDR 2005UALA00501Skin · dentedFUSELAGE SKIN DENTED STA 600-640, STR 27L TO 16L. TRIMMED OUT DAMAGE AND INSTALLED SKIN SPLICE REPAIR PER SRM53-30-12, AND EVA-50352 AND REO -G10623A.SDR 2005UALA00492Stringer · crackedLT FUSELAGE STRINGER 16L IS CRACKED AT STA 610. REMOVED DAMAGE AND FABRICATED NEW STRINGER SECTION PER SRM 53-30-03.SDR 2005UALA00491O-Ring · leakingNEEDLE IN RED (LOW). PRESSURE GAGE FITTING LEAKING. REPLACED O-RING.SDR 2005UALA00477Skin · misdrilledLT FUSE SKIN AT STA 1181 STR 16L HAS DRILL DAMAGE. REMOVED DAMAGED AREA AND FABRICATED FREEZE PLUG AND DOUBLER PER REO G09831 AND EVA-40157SDR 2005UALA00479Frame · dentedAFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. FRAME HAS BEEN REPAIRED PER TIMCO REO G-09850, REV A, WITH A J-ANGLE PER EVA 40168.SDR 2005UALA00478Frame · damagedFUSELAGE FRAME AT STA 600 BETWEEN STR 24L AND 24L REQUIRE DTA TO BE ACCOMPLISHED. REMOVED FRAME SECTION AND FABRICATED REPAIR PARTS PER REO G09843 REV 1.SDR 2005UALA00466Doubler · corrodedAFT CABIN FLOOR SHEAR WEB DOUBLER IS CORRODED STA 1681, RBL 48-55. REMOVED EXISTING REPAIR, REMOVED CORROSION INSTALLED DOUBLER REPAIR PER REO-G10512C AND SRM51-20-01SDR 2005UALA00465Frame · dentedAFT PIT FUSELAGE FRAME IS DENTED AT STA 1480 STR 25L. CUT OUT DAMAGE AND ACP HFEC WITH NO CRACK INDICATION. PER GSO TIMCO REO G10464, FABRICATED RPR AND INSTALLED.SDR 2005UALA00464Skin · dentedFUSELAGE SKIN DENTED STA 600 STR 17L DENT IS APPROX 3 INCHES BY .067 DEEP. RMV DAMAGE AREA AND ACP HFEC WITH NO CRACK INDICATION FABRICATED REPAIR AND INSTALLED PER MM 53-30-92SDR 2005UALA00463Frame · dentedAFT PIT FUSELAGE FRAME IS DENTED AT STA 1520, STR 25L. REMOVED DAMAGE AND INSTALLED J ANGLE REPAIR PER RE0-G10463, EVA-50283, AND SRM51- 40-02.SDR 2005UALA00462Frame · gougedFRAME STA 1520 FROM STR 22R TO 25R IS GOUGED FROM SCREWS IN 6 PLACES. REMOVED DAMAGE AND ACP HFEC NO CRACKS INDICATED. PER REO G10474 FABRICATED NESTLED ANGLE REPAIR AND INSTALLED.SDR 2005UALA00461Frame · dentedFWD PIT FRAME IS DENTED AT STA 600 STR 24L. CUT OUT DAMAGE AND ACP HFEC WITH NO CRACK INDICATED. FABRICATED RPR PER REO G-1042 AND INSTALLED.SDR 2005UALA00460Frame · corrodedAFT PIT FRAME PREVIOUS REPAIR IS CORRODED AT STA 1600 - STR 25L TO 27L. REMOVED DAMAGE AND FABBED NEW PRODUCTION SPLICE AND ANGLE REPAIR AND INSTALLED PER REO-G10504B AND SRM51-40-02 AND EVA-50287.SDR 2005UALA00456Skin · dentedLEFT SIDE OF ACFT BETWEEN FR 740 & 760 STRS 15L AND 16L HAS 1 DENT. FABRICATED DOUBLER RPR PER SRM 53-00-01 AND INSTALLED.SDR 2005UALA00455Intercostal · corrodedAFT CARGO INTERCOSTAL IS CORRODED BS 1360 TO 1380 RBL 26. REMOVED CORROSION AND FABRICATED INTERCOSTAL RPR AND INSTALLED PER SRM 53-00-04 AND BAC DWG 146N5427SDR 2005UALA00454Shear Web · corrodedAFT CABIN FLOOR SHEAR WEB IS CORRODED AT STA 1681 LBL 60. REMOVED CORROSION AND FABRICATED NEW TEE CAP. REPAIRED AND INSTALLED PER MM 53-00-98SDR 2005UALA00453Floorbeam · corrodedFWD GALLEY STA 365 RBL 11 FLOORBEAM TOP IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED ANGLE REPAIR IAW MM 53-00-98 AND INSTALLED PER MM 53-00-98SDR 2005UALA00476Skin · damagedMAJOR REPAIR ACCOMPLISHED ON SKIN AT STA 1701 AND STR 18R.
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