Boeing 767-323
Service difficulty reports · 8,545
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 = '767323' 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 = '767323' 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 AALA20160123001Connector · disconnectedAIRCRAFT WAS NOT GNDED. EMER PATH LIGHTING IS INOPERATIVE AT SEAT 34B. FOUND LOOSE CONNECTOR UNDER THE SEAT. CONNECTED ELEC CONNECTOR IAW MM 33-51-10. SYS CHECKED GOOD.SDR AALA20160118002Plate · corrodedAIRCRAFT WAS IN BASE MX. FLOORBEAM CHANNEL ATTACHED PLATE & FASTENERS AT FS 764 ARE CORRODED, BETWEEN RBL 23 & 26. REPAIRED IAW SRM 53-00-51-2R-1.SDR AALA20160122010Floorbeam · corrodedAIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 764, IS CORRODED AT RBL 26. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1 & EA 257609.SDR AALA20160119013Angle · crackedAIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL UPPER ANGLE IS CRACKED, BETWEEN FS 1197.22 & 1197.44 AT LBL 42. R & R ANGLE IAW SRM 63-60-51, AARD 51-00-05 & DWG 146T5400.SDR AALA20160119014Angle · crackedAIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL UPPER ANGLE, BETWEEN FS 1241 & 1263 AT LBL 36 IS CRACKED. R & R ANGLE IAW SRM 63-60-51, AARD 51-00-05 & DWG 146T5400.SDR AALA20160115011Skin · corrodedAIRCRAFT WAS IN BASE MX. LT WING UPPER SKIN HAS TWO CORRODED AREAS UNDER THE WING TO BODY FAIRING, JUST BELOW & AFT OF THE AFT EMER EXIT HATCH. REPAIRED IAW EA 257121.SDR AALA20160115002Gcu · faultyAIRCRAFT WAS NOT GNDED, AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT RT ENG IDG OFF LIGHT ILLUMINATED. IDG WOULD NOT RESET. R & R RT GCU IAW AMM 24-22-02-004-001. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.SDR AALA20160114008Frame · crackedAIRCRAFT WAS IN BASE MX. DURING ACCOMPLISHMENT OF ECO C3241AC_0001, A CRACK WAS FOUND IN THE RT SIDE OF THE MAIN FRAME AT FS 883.5. ACCOMPLISHED ECO C3241AC_0001 WITH EA 257316.SDR AALA20160113002Connector · disconnectedAIRCRAFT WAS NOT GNDED. EMER PATH LIGHTS FROM 35HJ TO 41HJ ARE INOPERATIVE. SECURED SEAT HARNESS CONNECTOR AT SEAT 35HJ. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.SDR AALA20160119015Seat Track · corrodedAIRCRAFT WAS IN BASE MX. CABIN SEAT TRACK NR 8 IS CORRODED, BETWEEN FS 390 & 397. R & R SEAT TRACK SECTION IAW AARD 51-00-05 & DWG 141T5121.SDR AALA20160112008Fan · inoperativeAIRCRAFT WAS GNDED, AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, CREW REPORTED STRONG ELEC ODOR IN COCKPIT & CABIN. R & R LT RECIRCULATION FAN IAW AMM 21-25-01. OPERATIONAL CHECKED GOOD.SDR AALA20160112007Shear Tie · corrodedAIRCRAFT WAS IN BASE MX. SHEAR TIE AT FS 1395, BETWEEN STRINGER 38L & 39L IS CORRODED. REMOVED SHEAR TIE, FABRICATED REPLACEMENT SHEAR TIE FROM SAMPLE ON SHOP ORDER C7NU, INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-10-02-0G.SDR AALA20160112001Light · damagedAIRCRAFT WAS NOT GNDED. SEAT 5J EMER LIGHT ASSEMBLY IS DAMAGED. R & R EMER LIGHT ASSEMBLY AT SEAT 5J IAW MM 33-60-98. OPERATIONAL CHECKED GOOD.SDR AALA20160201001Skin · corrodedAIRCRAFT WAS IN BASE MX. CORROSION ON UPPER SURFACE OF CTR FUEL TANK, UPPER SKIN AT FS 955 & BL 0. REPAIRED SKIN IAW SRM 51-10-02 & EA 257525 DATED 01 29 2016.SDR AALA20160110002Floorbeam · corrodedAIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 347 IS CORRODED, AROUND SCREW HOLES, BETWEEN RBL 55 & RBL 74. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1, 51-10-02-0G, 51-40-02-0G, 51-20-01-0G, EA 256937 & 257128.SDR AALA20160109005Floorbeam · corrodedAIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 325 IS CORRODED, BETWEEN RBL 20 & RBL 50. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1, 51-40-02-0G & 51-10-02-0G.SDR AALA20160109009Hydraulic Line · leakingAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE RECEIVED CTR HYD QTY EICAS MSG WITH QTY INDICATION OF .45 RF. ALL CTR PUMPS TURNED OFF. NO FURTHER QTY LOSS. ALL CTR PUMPS BACK ON FOR APPROACH. QTY AT GATE .31 RFSDR AALA20160108005Indicator · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING FLIGHT A CLICKING NOISE WAS IN OVERHEAD, FOLLOWED BY FLUCTUATING FLAP INDICATION & LE SLAT ASYMMETRY & LE LIGHT WARNINGS. MAINTENANCE REMOVED AND REPLACED FLASDR AALA20160104009Warning System · false activationGOING FROM FLAPS 20 - 25, THE LE ASYMMETRY, LE SLAT ASYMMRYTY, LIGHT CAME ON. AUTO PILOT HANDLE WENT BACK TO 20. THE FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. NO FAULTS ON FSEU. RAN FLAPS & SLATS UP & DOWN SEVERAL TIMES, NO FAULTS. INSTALSDR AALA20151231006Sign · unsecureDOOR 4L EXIT SIGN FELL OFF. SECURED EXIT SIGN ON SIDE OF 4L DOOR. THE ACFT WAS NOT GNDED.SDR AALA20160113006Relay · faultyAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT. DURING APPROACH AFTER FLAPS 1 SELECTED FLPS1 RECEIVED, LE SLAT DISAGREE, ACCOMPANIED BY A SPLIT IN FLAP INDICATOR. MX COULD NOT DUPLICATE SLAT DISAGREE. R & R FSEU IAW AMM 27-51-01SDR AALA20151228001Fseu · faultyAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH AFTER FLAPS 1 SELECTED FLPS1 RECEIVED, LE SLAT DISAGREE. ACCOMPANIED BY A SPLIT IN FLAP INDICATOR. FOLLOWED QRH & LIGHT WENT OUT. COULD NOT DUPLICATE SLAT DISAGRESDR AALA20151228003Charger · inoperativeAIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER PATH LIGHTING INOPERATIVE ON SEATS 20C - 24C. R & R BATTERY PACK & CHARGER FOR SEATS 20C - 24C. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-07, SYS CHECKED NORMAL. SEE ALSO AALA20151227004.SDR AALA20151227004Battery Pack · dischargedAIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER PATH LIGHTING INOPERATIVE ON SEATS 20C - 24C. R & R BATTERY PACK & CHARGER FOR SEATS 20C - 24C. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20151228003.SDR AALA20151223011Floorbeam · corrodedAIRCRAFT WAS IN BASE MX. FLOORBEAM CORRODED AT FS 654 + 44 INCHES & RBL 6. REPAIRED FLOORBEAM IAW SRM 53-00-07-2R.SDR AALA20151223015Connector · disconnectedAIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER LIGHTS AT SEATS 31H & 32H ARE INOPERATIVE. RECONNECTED CONNECTOR AT SEAT 30H. SYS CHECKED NORMAL.SDR AALA20151223001Light · inoperativeAIRCRAFT WAS NOT GNDED. EMER LIGHT AT SEAT 21H INOPERATIVE. R & R IN SEAT EMER LIGHT ASSEMBLY IAW AMM 33-51-10. SYS CHECKED NORMAL.SDR AALA20151222013Door Seal · damagedAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT ACFT AIRFRAME FLUTTERED, STARTING AT 270 KTS, INCREASED UP TO 295 KTS, THEN DISSIPATED AS WE SLOWED PAST 260 KTS. ENG INDICATIONS NORMAL. FOUND GAP INSDR AALA20151217008Terminal · disconnectedLEFT OVERWING EMERGENCY EXIT IDENTIFIER AT ROW 21A WOULD NOT TEST. FOUND IDENTIFIER, L00978, DISCONNECTED AT TERMINAL D11734. SECURED IAW WDM 33-51-14 & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-09. SYS CHECKED NORMAL.SDR AALA20160122009Power Supply · inoperativeAIRCRAFT WAS IN BASE MX. EMER EXIT LIGHT AT SEAT 25AB IS INOPERATIVE. R & R POWER SUPPLY M739 IAW AMM 33-51-07.SDR AALA20151215006Battery Pack · faultyEMERGENCY LIGHTING ON RT & LT AFT ENTRY DOOR EXIT SIGNS UPPER & LOWER IS INOPERATIVE. AIRCRAFT WAS GROUNDED. R & R CHARGER & BATTERY ASSEMBLIES M1210 IAW AMM 33-51-07. SYS CHECKED NORMAL.SDR AALA20151215005Charger · failedEMERGENCY LIGHTING ON LT AFT ENTRY DOOR EXIT SIGNS UPPER & LOWER IS INOPERATIVE. AIRCRAFT WAS GROUNDED. R & R CHARGER ASSEMBLY M1210 IAW AMM 33-51-07. SYS CHECKED NORMAL.SDR AALA20151215004Light · shortedEMERGENCY LIGHTING ON SEATS 25 - 31 LT SIDE ARE INOPERATIVE. AIRCRAFT WAS GROUNDED. FOUND LIGHT ASSEMBLY SHORTED AT 25B. R & R LIGHT ASSEMBLY IAW AMM 33-51-10 & PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.SDR AALA20151214001Ballast · faultyDURING CRUISE A FLIGHT ATTENDANT REPORTED STRONG ODOR OF SOMETHING HOT NEAR L1 DOOR. ODOR STOPPED AFTER UTILITY BUSS SWITCHES SELECTED OFF. R & R BALLAST M658 FWD DIRECT CEILING LIGHTS. OPERATIONAL CHECKED NORMAL, TEMPERATURE NORMAL AT DIM MODE IAW AMM 33-2SDR AALA20151212003Warning System · false activationEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH WHEN SELECTED FLAPS FROM 1 TO 5, CREW RECEIVED A TE FLAP ASYMMETRY WARNING. PERFORMED FSEU BITE IAW FIM 27-51-00 WITH FAULT MSG 27-51104 RETURNED. PERFORMED TROUBLESHOOTING IAW FISDR AALA20151212002Slide · unlacedMCM 0917 R2 DOOR SLIDE UNLACING. REPLACED DOOR SLIDE R2. THE ACFT WAS NOT GNDED.SDR AALA20151212001Charger · inoperativeEMERGENCY LIGHTS FROM ROW 25AB - 31AB INOPERATIVE. REPLACED BATTERY & CHARGER BPS7-3 AT ROW 25AB IAW AMM 33-51-07. OPERATIONS NORMAL, THE ACFT WAS GNDED.SDR AALA20151213004Light · corrodedLEFT FWD OVERWING EGRESS LIGHT IS DIM. REPLACED LIGHT ASSEMBLY IAW AARD 51-00-05. THE ACFT WAS NOT GNDED.SDR AALA20151202010Antenna · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. ACFT WAS GNDED. DURING CLIMB WEATHER RADAR FAILED. R & R WEATHER RADAR ANTENNA ASSEMBLY IAW AMM 34-43-05. SYS CHECKED NORMAL.SDR AALA20151201008Flashlight · damagedFOUND FLIGHT ATTENDANT FLASHLIGHT AT 4R DOOR BLINKING RED. FOUND FLASHLIGHT DAMAGED. R & R FLASHLIGHT.SDR AALA20151201007Lens · missingEMERGENCY LIGHT LENS COVER MISSING OUTSIDE M2 LAVATORY. REPLACED MISSING LENS.SDR AALA20151130006Stiffener · crackedFLOORBEAM STIFFENER AT STATION 246 & RBL 15 IS CRACKED. FABRICATED & INSTALLED REPLACEMENT BRACKET IAW SRM 53-10-51-2R-3.SDR AALA20151130001Window · crackedAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, BURN MARKS APPEARED ON THE FIRST OFFICER`S NR 1 WINDOW, FOLLOWED BY CRACKING OF THE WINDOW. R & R FIRST OFFICER`S NR 1 WINDOW IAW AMM 56-11-01 & THE ASSOCIATED WINDOW HEAT CONSDR AALA20151128003Controller · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, BURN MARKS APPEARED ON THE FIRST OFFICERS NR 1 WINDOW, FOLLOWED BY CRACKING OF THE WINDOW. R & R FIRST OFFICER’S NR 1 WINDOW IAW AMM 56-11-01 & THE ASSOCIATED WINDOW HEAT CONTSDR AALA20151127007Mechanism · faultyCREW REPORTS AILERON LOCKOUT AT 300 KNOTS. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R RT AILERON LOCKOUT MECHANISM IAW MM 27-11-44, RIG & OPERATIONAL CHECKED GOOD. ACCOMPLISHED RT AILERON LOCKOSDR AALA20151124014Attach Angle · crackedCOOLING LINE ATTACH ANGLE IS CRACKED FWD SIDE OF FRAME 246 AT APPROX RBL 11. INSTALLED NEW SERVICEABLE COOLING LINE ATTACH ANGLE 141T5146-5 IAW DOCUMENT NR 141T5104 & IAW SRM 53-10-51-2R-3.SDR AALA20151124005Actuator · faultyCREW REPORTS AILERON LOCKOUT AT 300 KNOTS. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R RT AILERON LOCKOUT ACTUATOR IAW MM 27-11-44, RIG & OPERATIONAL CHECK GOOD. ACCOMPLISHED RT AILERON LOCKOUT SDR AALA20151121003Actuator · malfunctionedDURING CLIMB, PASSING APPROX 270 KTS, GOT EICAS MSG AILERON LOCKOUT WITH OVERHEAD LIGHT, ALSO, AIL-LOCK. FLIGHT CONTINUED, DECLARED EMER DURING APPROACH. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE LT OTBD AILERON LOCKOSDR AALA20151121001Engine · leakingDURING FLIGHT, RT ENG LOST 10 QUARTS OF OIL IN 5.5 HRS. FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. TROUBLE SHOT SYS & FOUND TUBE B SCAVENGE LEAKING THRU GASKET IAW IPC IAW 79-21-00-01 DETAIL N ITEM 112. REPLACED GASKESDR AALA20151120010Proximity Switch · faultyLEADING EDGE ASYM LIGHT ON AFTER TAKEOFF & FLAP RETRACTION. FLAP INDICATOR MOVED BACK & FORTH, BETWEEN UP & .5. REPLACED NR 6 INBD PROXIMITY SWITCH M281. OPERATIONALLY CHECKED NORMAL IAW MM 27-88-01.
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