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 2005UALA01214Wedge · delaminatedT/E WEDGE DELAMINATED. WEDGE REPLACED.SDR 2005UALA01164Warning System · activatedANTI-SKID EICAS AND VIBRATION DURING TAKEOFF ROLL AND GEAR RETRACTION. REPLACED WIRING FR0M D2040 TO TB211, FOUND OPEN ON WIRE W4904-2501R-20. RE-SECURED SHIELDING PINS AT TB211 (LA4 AND LE4) ALL PER WD32-42-11. OPS CHK NORMAL.SDR 2005UALA01163Relief Valve · openLOSS OF CABIN PRESSURE. LOWER POSITIVE PRESSURE RELIEF VALVE FOUND OPEN. REPLACED VALVE, OPS CHECKED OK. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA01150Clamp · looseEMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURE CONTROL. FOUND CLAMPS TO LEFT AND RIGHT CABIN AIR SUPPLY CHECK VALVES LOOSE. SECURED CLAMPS. LEAK AND OPS CHECKED OK PER MM21-31-00. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA01154Line · crackedFLIGHT DIVERTED DUE TO CABIN ALTITUDE WARNING AND INABILITY TO MAINTAIN CABIN PRESSURE. ORD FOUND RIGHT AIR CONDITIONING PACK WATER SEPARATOR DRAIN LINES CRACKED. REPLACED PART NUMBERS 213N1001-16 AND 213N1001-15. RETURNED AIRCRAFT TO SERVICE. NOTE: THIS SDR 2005UALA01152Odor · detectedACRID ODOR AND SLIGHT AMOUNT OF SMOKE IN CABIN. SOURCE OF SMELL DETERMINED TO BE RIGHT AIR CONDITIONING PACK. RAN RIGHT PACK FOR 20 MINS PER MM 21-00-01. NO SMELL NOTED. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA01151Warning Light · illuminatedLANDED UNDER AMBER ALERT DUE TO INOP GENERATOR & APU OIL QTY STATUS MESSAGE. APU REMOVED. DIAGNOSTIC TEST FOUND NO HOC/ OIL LEAKS. APU DISSASSEMBLED FOR LIFE LIMITED PART. APU OIL QTY MESSAGE DISPLAYED ON EICAS. - NO HOC IN AMIS (ENGOIL) EXCEPT ONE AMBER HSDR 2005UALA01176Light · inoperativeEMERGENCY AISLE LIGHTS FROM ROW 29 TO 32 ARE INOP. REMOVED AND REPLACED BATTERY.SDR 2005UALA01139Floorbeam · crackedBS 700 CABIN FLOORBEAM UPPER CAP HAS DAMAGE. BS 700 LBL 25 FLOORBEAM UPPER CHORD SPLICE REPAIR ACP'D PER MM 53 00 98 825 DUE TO CRACK IN RADIUS.SDR 2005UALA01083Light · cutROW 23 THROUGH 24 EEL LIGHTS INOP. REPAIRED CUT IN STRIP. REPLACED STRIP AT SEAT 25.SDR 2005UALA01082Wire · damagedEEL FLOOR STRIP BETWEEN SEAT ROWS 9 AND 12 IS INOP. REPAIRED EEL JUMPER CABLE.SDR 2005UALA01070Light · burnedSMOKE COMING FROM LIGHT FIXTURE IN FORWARD GALLEY. ACCOMPLISHED VISUAL INSPECTION. FOUND NO BURNT WIRES NO CHAFFING, BALLASTS OK , NO ARCING, 0-2 GEN OK. OP CHECK LIGHTS FOR 20 MINUTES NO SMELL OR SMOKE. NO FURTHER INCIDENTS SINCE.SDR 2005UALA01057Skin · dentedSKIN DENT AT STA 750, STR 16L. TRIMMED OUT DAMAGE, INSURE CUT, INSTALLED FILLERS, DOUBLER, AND TRIPLER REPAIR PER REO-G11 002-C AND EVA-50676SDR 2005UALA01051Battery Pack · inoperativeEMERGENCY EXIT LIGHT ABOVE ROW 16 LT INOP. REPLACED BATTERY PACK AT POWER SUPPLY LOC, M10699 (ROW 23DEF).SDR 2005UALA01049Skin · dentedFUSELAGE EXTERIOR AT BS 258 AND STR 28L HAS 1 DENT. REMOVED DAMAGE AND ACP HFEC NO CRACK INDICATION FABRICATED DOUBLER RPR IAW MM 53-30-95.SDR 2005UALA01044Odor · detectedAFTER APU START AT DEPARTURE WITH PACKS ON FOR SEVERAL MINUTES FLT CREW NOTED ELECTRICAL ODOR THROUGHOUT CABIN AND FLIGHT DECK. MAINTENANCE RAN PACKS USING APU PNEUMATICS FOR 20 MINS IN ACCORDANCE WITH MM21-00-01 WITH NO FURTHER SMELL NOTED. RETURNED AIRCRAFSDR 2005UALA01024Skin · wornLT WING INBD FOREFLAP HAS WORN AREA AT UPPER OTBD END. SUPPLEMENTASDR 2005UALA01041Light · cutEEL INOP AT GALLEY G2A AND G2B. SUPPLEMENTAL DATA UPDATE, G2B EEL FOUND CUT, REPLACED EEL LIGHT.SDR 2005UALA01018Switch · shortedELECTRICAL SMOKE SMELLED, WHITE SMOKE SEEN BRIEFLY IN AFT LAV. REPLACED DOOR LOCK SWITCH.SDR 2005UALA01017Odor · detectedLIGHT SMOKE AND BURNING ODOR IN COCKPIT WITH RIGHT PACK OPERATING OFF APU. ACCOMPLISHED AIR CONDITIONING SYSTEM OIL CONTAMINATION MAINTENANCE PRACTICES PER MM21-00-01. NO SMELLS NOTED. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA01075Wedge · delaminatedSLAT HAS DAMAGED DELAMINATED T/E WEDGE. WEDGE REPLACED.SDR 2005UALA00994Skin · dentedSKIN DENT STA 600, RBL 8. REMOVED SKIN DAMAGE, INSTALLED DOUBLER AND TRIPLER REPAIR PER TIMCO REO-G10977B AND EVA- 50640 WITH FAA APPROVAL VIA 8100-9.SDR 2005UALA00995Hydraulic System · malfunctionedRETURNED TO FIELD DUE TO HYDRAULIC PROBLEMS. FOUND HYDRAULIC PRESSURE LINE WITH STREAMING LEAK. REPLACED HOSE, REPLACED RETURN AND CASE DRAIN FILTERS, AND SERVICED SYSTEM TO FULL. LEAK CHECKED SAME. PRESSURE WASHED FUSELAGE BELLY AS REQUIRED. RETURNED AIRSDR 2005UALA00981Odor · detectedACRID OIL SMELL IN COCKPIT THROUGHOUT FLIGHT. ACCOMPLISHED ENGINE BURNOUT PROCEDURE PER MM21-00-01 PG210. SMELL DIMINISHED AFTER ENGINE RUN. RETURNED AIRCRAFT TO SERVICE.SDR 2005UALA00972Skin · damagedFUSELAGE SKIN AT BS 1701 AND STR 14L. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER TIMCO REO G10893 AND UA-EVA- 50622.SDR 2005UALA00971Frame · dentedFWD PIT FRAME IS DENTED 2 PLACES AT STA 620 BETWEEN STR 26L AND 24L. *S/D* TRIMMED OUT DAMAGE AND INSURANCE CUT, FAB NEW SPLICE AND REPAIR ANGLE AND INSTALLED.SDR 2005UALA00970Frame · dentedFWD PIT FRAME AT STA 520, STR 24L, IS DENTED. TRIMMED OUT DAMAGE AND INSURANCE CUT, FABBED J-ANGLE REPAIR AND INSTALLED.SDR 2005UALA00978Warning System · activatedRETURNED TO FIELD DUE TO FUEL FLOW INDICATION. DURING TROUBLESHOOTING FOUND DAMAGE TP WIRE INSULATION AT CONNECTOR D5004 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH APPROXIMATELY A HALF INCH FROOM THE BACKSHELL. REPAIRED WIRING PER MM 71-51-00 PAGES 820/821.SDR 2005UALA00969Frame · dentedFWD PIT FRAME IS DENTED AT STA 540, STR 24L TO 26L. TRIMMED OUT DAMAGE AND INSURANCE CUT, FABBED NEW SPLICE AND REPAIR ANGLE AND INSTALLED.SDR 2005UALA00968Frame · dentedFWD PIT FRAME IS DENTED AT STA 600, BETWEEN STR 24L AND 25L. TRIMMED OUT DAMAGE WITH INSURANCE CUT, FAB J-ANGLE AND INSTALLED.SDR 2005UALA00967Frame · dentedAFT PIT FRAME DENTED STA 1400 AT STR 25L. TRIMMED OUT DAMAGE, INSURANCE CUT, HFEC INSP, FABBED J-ANGLE REPAIR AND INSTALLED.SDR 2005UALA00966Frame · dentedDENT ON PIT FRAME STA 1420, STR 24L. TRIMMED OUT DAMAGE, INSURANCE CUT, INSTALLED NEW PRODUCTION SPLICE AND ANGLE REPAIR.SDR 2005UALA00965Frame · dentedAFT PIT FRAME IS DENTED AT STA 1500 & STR 25L. TRIMMED DAMAGE, INSURANCE CUT, HECT VERIFY NO CRACKS. FAB NEW PRODUCTION SPLICE, AND INSTALLED WITH REPAIR ANGLE AND NEW STR CLIPS.SDR 2005UALA00964Skin · dentedON ARRIVAL FOUND TWO EA DENTS ON FUSELAGE JUST FWD & BELOW WATERLINE OF DOOR 2L. DENTS ARE ON AN EXISTING DOUBLER. *S/D* FOUND AT RATIO OF 15.5 TO BE BEYOND LIMITS IN SRM 53-00-01 PG 103. DAMAGE IS DEFERRABLE AS PER SRM 53-00-01 PG 102 ITEM I.SDR 2005UALA00963Skin · dentedSKIN DENTED STA 540, STR 19R. TRIMMED OUT DAMAGE AND ACCOMP INSURANCE CUT. INSTALLED FILLERS AND DOUBLER.SDR 2005UALA00959Pressure Panel · damagedAFT CABIN FLOOR LEVEL, AFT PRESS DECK PLATE HAS DAMAGE. REPAIRED PER MM 53-60-97.SDR 2005UALA00950Frame · dentedFWD PIT FRAME IS DENTED 2 EACH PLACES AT BS 580 BETWEEN STR 22L & STR 24L ON INBOARD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.SDR 2005UALA00934Skin · dentedAFT CARGO PIT DOOR CUTOUT, LOWER SKIN DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLERS PER TIMCO REO (EVA) G10924, REV.D.SDR 2005UALA00930Skin · damagedNR 1 PYLON OB SKIN DAMAGED. REPAIRED PER SRM 54-31-99.SDR 2005UALA01047Slide · rupturedTUBE RUPTURED DURING OVERPRESSURE (PROOF) TEST. TEST PRESSURE WAS AT 3.41 PSI FOR FIVE MINUTES. INFLATABLE FAILED OVERPRESSURE TEST DUE TO SEAM FAILURE. INFLATABLE WAS BEYOND REPAIR PER CMM. SLIDE WAS SENT TO OEM FOR INFLATABLE REPLACEMENT.SDR 2005UALA00920Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 1640, UPPER T-CAP HAS CORROSION IN SEVERAL PLACES AROUND FASTENER HOLES, UPPER AND LOWER SURFACES, LBL 9 TO RBL 60. REMOVED EXISTING SPLICES AND DAMAGED T-CAP SECTION, FABRICATED NEW T-CAP AND SPLICE ANGLES AND STRAPS PER MM 53-0SDR 2005UALA00919Skin · dentedOUTSIDE DOOR 1R TO LEFT OF NOSE NUMBER SMALL CREASE AND DENT IN FUSELAGE.SDR 2005UALA00954Skin · damagedLOWER AFT FUSELAGE LIGHTNING STRIKE AT STA 1715, S28L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR DOUBLER.SDR 2005UALA00916Cable · inoperativeEMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED CABLE AT STA 1076 AND JUMPER WIRE AT STA 880 TO 902.SDR 2005UALA00907Warning Horn · activatedON DESCENT HAD FIRE WARNING HORN GO OFF.SDR 2005UALA00906Hydraulic System · malfunctionedRETURNED TO ANC UNDER AN AMBER ALERT DUE TO A HYDRAULIC PROBLEM. LEFT HAND ENGINE HYDRAULIC PUMP FAILED. REPLACED LEFT HAND PUMP PER MM29-11-05. ALSO REPLACED PRESSURE FILTER AND CASE DRAIN FILTERS. CHECKED AND REPLACED ELECTRIC HYDRAULIC PUMP CASE DRAIN FSDR 2005UALA00902Skin · damagedLOWER AFT FUSELAGE LIGHTNING STRIKE AT BS 1787.43 LBL 8 AT FASTENER AND SKIN. REMOVED DAMAGE, ACP HEFC INSP, NO CRACKED NOTED. INSTALL REPAIR DOUBLER PER SRM 53-00-01, AND TIMCO REO-G10914, REV A.SDR 2005UALA00915Light · inoperativeEEL STRIP IN FRONT OF MID CABIN LAV IS INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY.SDR 2005UALA00908Engine · flamed outENGINE FLAMEOUT DURING NR 2 ENGINE START.SDR 2005UALA00901Frame · dentedFRAME DENTED AT STA 1420 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HFEC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO GEO-10827.
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