Boeing 767-222
Service difficulty reports · 956
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 = '767222' 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 = '767222' 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 2008FA0000838Precooler · fracturedNR1 PYLON PRECOOLER CRACKED IN SEVERAL PLACES. REMOVED AND REPLACED NR1 ENG PRECOOLER IAW MM 36-11-15. WORK PERFORMED ON NR 35501 S/O 599197.SDR UALA2008112006587Smoke Detector · faultyLAV K SMOKE DETECTOR WILL NOT RESET.SDR UALA2008111306230Receptacle · damagedBURNING ODOR REPORTED. MID LAV FLOW LIGHT AFT LAMP RECEPTACLES ARE CHARRED. NEED REPLACEMENT. REMOVED LAMPS FROM MIRROR LAMP. DOME LAMP WORKS NORMAL.SDR TIPR200736008Skin · dentedBULK CARGO DOOR EXTERIOR SURFACE DENTED NUMEROUS PLACES. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-30-01 FIG 101. REFERENCE SERVICE ORDER- 599125 OPERATION-23372.SDR TIPR200736007Stringer · corrodedAFT PIT STA 1540, STRINGER 39R, CORROSION AS MARKED. FABRICATED AND INSTALLED STRINGER REPAIR IAW SRM 53-00-03.SDR TIPR200736006Skin · corrodedAFT PIT STA 1540 HAS CORROSION UNDER STRINGER 39R. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201. REFERENCE SERVICE ORDER-599125 OPERATION 26209.SDR TIPR360200706Skin · gougedAFT FUSELAGE SKIN UNDER UPPER LT STAB FAIRING STA 1835 DEEP GOUGES. FABRICATED AND REPLACED REPAIR DOUBLER IAW SRM 53-80-01- REFERENCE SERVICE ORDER 599125 OPERATION 25071.SDR TIPR200736005Structure · crackedCRACK INDICATIONS ON LT AND RT VERTICAL STIFFENERS IN NOSE WHEEL WELL APPROX 12 INCHES DOWN FROM TOP OF CHORD. REPAIRED LT AND RT CHORDS IN ACCORDANCE WITH B767 SRM 51-70-12 FIG 1 AND AD 2005-02-02. REFERENCE SERVICE ORDER 599125 OPERATION 26110.SDR TIPR200736004Skin · gougedFUSELAGE EXTERIOR SKIN GOUGED BS 1197 STRINGER 36L TO 37L. REMOVED FASTENERS TO FACILITATE OTHER MAINTENANCE IN ACCORDANCE WITH B767 SRM 51-40-02. REMOVED DAMAGE FOUND TO BE BEYOND LIMITS PER THE Z DIMENSION MEASUREMENT IN ACCORDANCE WITH B767 SRM 53-00-01. SDR TIPR200736003Skin · corrodedAFT PIT STA 1320 BETWEEN STRINGER 36L TO STRINGER 37L SKIN HAS CORROSION. REMOVED CORROSION IN ACCORDANCE WITH B767MM51-00-53. ORIGINAL MATERIAL THICKNESS .056 MATERIAL REMOVED .019 MATERIAL REMAINING .037. FOUND TO BE BEYOND LIMITS IN ACCORDANCE WITH B767 SDR TIPR200736002Skin · corrodedAFT PIT SKIN CORRODED AT FS 1356 TO FS 1359 STRINGER 39L TO STRINGER 38L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH B767-200 SRM 53-00-01. ORIGINAL MATERIAL THICKNESS IS .105 MATERIAL REMAINING .057 MATERIAL REMOVED .048. FABRICATEDSDR TIPR200736001Floorbeam · corrodedAFT PIT FLOORBEAM UPPER T-CAP AT UPPER AND LOWER SURFACES HAS CORROSION AT BS1197 BETWEEN RBL 22 TO RBL 44. REMOVED CORROSION IAW MM 51-00-53. FOUND TO BE BEYOND LIMITS IAW SRM 53-00-07. MATERIAL ID IS BAC1506-3123 IAW DRAWING 146T1206. FABRICATED NEW T-CAP SDR USAA050729Intercostal · corrodedBFM - C4- INTERCOSTAL UPPER CHORD, 20 INCHES L X 1 INCH W X .008 INCH D, CORROSION; LEVEL 1; TASK C53-252-03; CABIN FLOOR BS 1661-1680, RBL 10. FAB NEW INTERCOSTAL UPPER CHORD IAW SRM. (K)SDR 2004UALA00732Compressor · stalledRT ENG COMPRESSOR EXPERIENCED A COMPRESSOR STALL. STALL STOPPED WHEN RT THROTTLE RETARDED. RESET BLEED ALL INDICATIONS NORMAL. ALL POST-COMPRESSOR STALL TROUBLESHOOTING ACCOMPLISHED IMMEDIATELY AFTER EVENT, NO DEFECTS FOUND. DECIDED TO WATCH ENG FOR ANY RESDR 2004UALA00627Warning Light · illuminatedCABIN ALT WARNING & EXCESSIVE HOT AIR CAUSED DIVERSION OF FLIGHT. AT FLIGHT LEVEL 330 THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE. THE CARGO DOOR DEPRESSOR SEAL WAS FOUND DAMAGED CAUSING A LARGE AIR LEAK.SDR 2004UALA00522Warning Light · illuminatedLANDED LAX UNDER AMBER ALERT DUE TO FLAP DISAGREE INDICATION. ACCOMPLISHED FLAP POSITION TRANSMITTER SYNCHRONIZATION CHECK ON 3, 4, AND 5 FLAP POSITION TRANSMITTERS. FOUND NR 4 OUT OF LIMITS. ADJUSTED TRANSMITTER.SDR 2004UALA00370Engine · malfunctionedDIVERTED DUE TO LOSS OF LT ENGINE POWER. ENGINE HUNG DURING ACCELERATION. TSI WAS 10 HRS. FOUND PCB 3.5, PTT2 TOTAL AIR TEMP AND PIR INTERSTAGE RETURN PSI TUBE FROM TT2 SENSOR LOOSE. ALL WERE SECURED AND SAFETIED.SDR 2004UALA00318Roller · sparksFWD CARGO PIT POWER DRIVE ROLLER SPARKING AND SMOKING. POWER DRIVE UNIT CABLE CHAFED AGAINST CLAMP ATTACH SCREW ON BOTTOM OF PDU, DUE TO BROKEN CABLE CLAMP. SCREW APPEARS TO HAVE BURN MARKS FROM ARCING. PDU REPLACED.SDR 2004UALA00418Bolt · shearedNOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKNOWN. REPLACED BOLT.SDR 2004UALA00231Fitting · wornRIGHT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED RIGHT WING INBOARD FLAP COLLAR FITTING.SDR 2004UALA00230Fitting · wornLEFT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED LEFT WING INBOARD FLAP COLLAR FITTING.SDR 2004UALA00228Skin · crackedNR 2 PYLON ACCESS 446BR, UPPER FWD CORNER OF ACCESS CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00227Stringer · crackedAFT PIT AT STA 1088, STR 33L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH -U- AND -J- CHANNEL SPLICE ANGLES.SDR 2004UALA00220Keelbeam · corrodedKEELBEAM AT BS 800.81 AND RBL 9.5, HAS AREA OF CORROSION AND EXFOLIATION ON LOWER SURFACE AT PANEL ATTACH HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED KEELBEAM FLANGE WITH RETAINER.SDR 2004UALA00031Switch · misusedRETURNED TO BLOCKS DUE TO ANTI ICE VALVE WARNING. THIS INCIDENT OCCURRED MOST LIKELY WHEN THE LT ENGINE ANTI-VALVE WAS DEFERRED INOPERATIVE PER THE MEL, AND, THE LT ENGINE ANTI-ICE VALVE SWITCH WAS LEFT IN THE INCORRECT POSITION AFTER REVIEWING THE MEL PROCEDSDR 2003UALA00943Solenoid · activatedABORTED TAKEOFF DUE TO A NR 1 ENGINE GENERATOR INDICATION. REPLACED THE IDG. SHOP FINDINGS REVEALD THAT THE DISCONNECT SOLENOID FAILED. SOLENOID AND FILTER WERE REPLACED.SDR 2003UALA00917Skin · corrodedAFT CARGO PIT AT BS 1080-1087 BETWEEN STR 37L- 38L, SKIN IS CORRODED AROUND DRAIN FITTING. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.SDR 2003UALA00869Actuator · failedRETURNED TO FIELD DUE TO CABIN PRESSURE PROBLEMS. AUTO PRESS MODE FAILED. *S/D* THE OUTFLOW DOOR DC MOTOR WAS FOUND TO FAIL WHEN EXPOSED TO COLD SOAK NOT ALLOWING THE AC MOTOR TO OPERATE.SDR 2003UALA00864Motor · failedRETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEMS. AUTO CABIN INOP EICAS MESSAGE. MANUAL CONTROL FAILED ON DESCENT. *S/D* THE OUTFLOW DOOR DC MOTOR WAS FOUND TO FAIL WHEN COLD SOAKED.SDR 2003UALA00817Skin · dentedDENT IN SKIN AT STA 651, STR 32R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & TRIPLER REPAIR.SDR 2003UALA00708Oil Cooler · failedDIVERTED TO SYR DUE TO NR 1 ENGINE OIL PRESSURE INDICATION. REPLACED OIL COOLER. SHOP TEST CONFIRMED OIL COOLER MATRIX LEAKING INTERNALLY, ALLOWING FUEL TO CONTAMINATE THE ENGINE OIL SYSTEM.SDR 2003UALA00703Light · damagedEMERGENCY EXIT LIGHTS-FLOOR LIGHT DAMAGED DOOR 2R. FOUND EEL TRACK COVER OFF FWD OF DOOR 2R. SECURED COVER AND OPS CHECKED EMERGENCY LIGHTS. OPS CHECKED NORMAL.SDR 2003UALA00618Keelbeam · corrodedKEELBEAM WEB DRAIN HOLE HAS CORROSION AT BS 786, BL0.SDR 2003UALA00632Wedge · delaminatedT/E WEDGE DELAMINATED. T/E WEDGE REPLACED.SDR 2003UALA00531Proximity Sensor · dirtyUNSCHEDULED LANDING DUE TO FWD CARGO DOOR EICAS. CHECKED DOOR LOCKED AND CLOSED PROXIMITY SENSORS FOR PROPER GAPS. ALL CHECK WITHIN LIMITS. SHOOK OUT PROX SENSOR WIRING WHILE ACCOMPLISHING TARGET NEAR/FAR TESTS. CHECKED WITH AIRCRAFT PRESSURIZED. UNABLE TSDR 2003UALA00480Shear Tie · corrodedBS 1335, BETWEEN STRINGERS 33R AND 34R, SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE.SDR 2003UALA00479Stringer · damagedBS 1361-1379 STRINGER SECTION REQUIRES REPLACEMENT IN ORDER TO MAINTAIN 20 INCH MINIMUM SPACING BETWEEN STRINGER SPLICE AT STATION 1337, STRINGER 34R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SECTION AND SPLICE.SDR 2003UALA00478Skin · puncturedFUSELAGE TAILCONE SKIN AT STA 1848, LBL 24 PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.SDR 2003UALA00477Stringer · corrodedAFT CARGO STRINGER 34R AT STA 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIRED ACCOMPLISHED. INSTALLED SPLICE REPAIR.SDR 2003UALA00476Web · corrodedAFT CARGO PIT AT BS 1329-1351, LOWER DOOR SILL LOWER WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. INSTALLED WEB AND SPLICE REPAIR.SDR 2003UALA00470Clip · damagedBS 1346, STR 34R, FRAME ATTACH CLIP REQUIRES REPLACEMENT FOR STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.SDR 2003UALA00465Stringer · misrepairedSTATION 1361 TO 1379, STRINGER 34R, STRINGER SECTION AND SPLICE DO NOT HAVE REQUIRED EDGE DISTANCE BETWEEN REPAIR SPLICES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER & SPLICE REPAIRS.SDR 2003UALA00464Stringer · corrodedAFT CARGO STRINGER 34R AT STATION 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION AND DOUBLER REPAIR.SDR 2003UALA00458Stringer · corrodedAFT CARGO PIT AT BS 1081-1087, STRINGER 37L IS CORRODED AT END FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SECTION AND SPLICE.SDR 2003UALA00398Wire · looseEMERGENCY EXIT LIGHTS FROM SEAT 26F AFT TO AFT GALLEY INOP. SUPPLEMENTAL DATA UPDATE SECURED LOOSE LEAD WIRE CONNECTORS AT EEL.SDR 2003UALA00416Warning Light · illuminatedA/C RECEIVED LEFT GENERATOR DRIVE LIGHT INDICATION. DISCONNECTED IDG AND FELT VIBRATION. REMOVED AND REPLACE THE LEFT IDG. SHOP FINDINGS SHOW THAT THE UNIT HAD A FAILURE IN THE HYDRAULIC LOG.SDR 2003UALA00300Control Unit · malfunctionedA/C RECEIVED EICAS MESSAGE. LEADING EDGE SLAT REMAINED IN EXTENDED POSITION. CLEARED BITE HISTORY FROM PSEU. CYCLED FLAPS AND COULD NOT DUPLICATE EICAS MESSAGE.SDR 2003UALA00285Skin · gougedA/C DAMAGED BY LOADER AFT OF FWD CARGO DOOR. VARIOUS DENTS AND GOUGES MAJOR REPAIR ACCOMPLISHED WITH DOUBLERS IN AREA FWD OF CARGO DOOR BELOW RT WING LITE.SDR 2003UALA00261Sign · damagedGREEN EMERGENCY LIGHT EXIT SIGNS AT MED 2L AND 2R ARE INOP. REPAIRED DAMAGED SECTIONSDR 2003UALA00181Sensor · malfunctionedLEFT HYDRAULIC QUANTITY LIGHT ILLUMINATED. QUANTITY LEVEL .02. QUANTITY RETURNED TO NORMAL AFTER LANDING. REPLACED HYDRAULIC QUANTITY MONITORING UNIT. VENDOR SHOP FINDINGS IDENTIFIED LEFT CHANNEL INOP.
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