Boeing 767-34AF
Service difficulty reports · 6,321
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 = '76734AF' 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 = '76734AF' 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 IPXA2673103Floor Panel · puncturedDAMAGED FLOOR PANEL AT POS 2L OTBD. REPAIRED IAW SRM 53-00-50-2R, PARA 4C.SDR IPXA2673102Floor Panel · puncturedDAMAGED FLOOR PANEL POS 4L OTBD. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA12673048Indicator · failedDUE TO CAPTAIN`S AIRSPEED INDICATION INOPERATIVE, ALTERNATE AIR DATA SELECTED, FAILED TO CORRECT PROBLEM. CHECKED CAPTAIN`S AIRSPEED INDICATOR CONDITION, POWER AND GROUNDS AT CONNECTOR D101, REF WDM 34-13-11. CHECKED OK. FIM FAULT CODE 34012030 AND 4 34-12-7SDR IPXA12672965Floor Panel · damagedFLOOR PANEL DAMAGED. BS 632 FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA12672935Circuit Card · faultyEICAS MESSAGE L/E SLAT ASSY DISPLAYED L/E LIGHT ILLUM W/FLAP LEVER IN 50. PERFORMED BITE CHECK OF PSEU, FOUND MULTIPLE FAULTS WHICH WAS AN INDICATION OF A FAULTY 006 CARD IN THE LT SIDE OF THE PSEU. R & R 006 CARD IAW AMM 32-09-06-4. FAULTS CLEARED AFTER SDR IPXA12673071Skin · wornINSPECTION TYPE: 8C, EMPENNAGE RT LOWER AIR GATE FAIRING FWD CUTOUT FAIRING SKIN PANELS FOUND WORN. RT LOWER AIR GATE FAIRING FWD CUTOUT PANELS REPAIRED SRM 53-80-012R3 FIG 201, REV 52.SDR IPXA2673135Skin · corrodedINSPECTION TYPE: 8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING. SLIGHT CORROSION IS FOUND AFTER FAIL-SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL-SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 & RSDR IPXA2673130Fitting · corrodedINSPECTION TYPE: 8C, FUSELAGE LT BS 955 BULKHEAD SIDE FITTING - A SLIGHTLY CORROSION IS FOUND AFTER FAIL SAFE - STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-SDR IPXA12673052Hinge Fitting · crackedINSPECTION TYPE: 8C, RT WING INBD MAIN FLAP, INBD HINGE ARM FITTING FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE ARM FITTING REPAIRED IAW SRM 57-53-02-2 REPAIR 1 FIG 201, REV 52.SDR IPXA2672858Wire Harness · chafedDURING CRUISE, F/O'S LOWER EFIS SCREEN BLINKED OFF THEN ON. A STRONG ELECTRICAL BURNING ODOR FOLLOWED THEN DISSIPATED AFTER 10 MINUTES, NO SMOKE WAS PRESENT. CHECKED WIRING IN THE COCKPIT AND FOUND F/O ASA AND WIRE BUNDLE W1054 CHAFED AND BURNED SLEEVE. REMSDR IPXA2673154Battery Pack · failedINSPECTION TYPE: 8C, EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINS. EMERGENCY LIGHT BATTERY PACK REPLACED AND OPS TEST CARRIED OUT NORMAL, REF AMM 33-51-07.SDR IPXA2673133Tee Fitting · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22AR CRACK WAS FOUND AT RT SIDE TEE FITTING AT 9 O`CLOCK POSITION .0625" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AREA TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPROX D, FIG 6, ORIGINSDR IPXA2673132Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955 S22AR CRACK WAS FOUND AT RT SIDE FAIL SAFE STRAP AT 9 O/C POSITION 0937" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J APPX 'D', ORIGINAL MATERIAL IS 2024T351-0SDR IPXA2673128Tee Fitting · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE TEE FITTING AT 2 O/C POSITION 3/32" APPROX FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG AREA T-FITTING. REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPX 'C' FIG 6, ORIGINAL MATERIAL SDR IPXA2673127Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE FAILSAFE STRAP AT 8 O`CLOCK POSITION .0937" APPROX. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J, APPROX C, ORIGINAL MATERIAL IS 2024SDR IPXA2673126Bulkhead · crackedINSPECTION TYPE: 8C, FX - LT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE REMOVED AND REISDR IPXA12673070Floor Panel · damagedINSPECTION TYPE: 8C, MAIN CARGO DECK FLOOR PANEL HAS NINE DENTS AND TWELVE PUNCTURES AT BS 412 TO 530, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA12673012Skin · crackedINSPECTION TYPE: 8C, RIGHT WING NR 8 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.SDR IPXA12673011Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 5 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.SDR IPXA12673010Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 4 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.SDR IPXA12673009Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 3 SLAT INBD NOSE SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2. REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR.SDR IPXA2672830Wedge · dentedLEFT WING INBD FLAP T/E WEDGE DENTED UPPER AND LWR SURFACE. REPAIRED REF EO B767-5750-46365-B.SDR IPXA2673131Fitting · crackedINSPECTION TYPE: 8C, RT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE R & R IAW EO NO B767-SDR IPXA12672735Floor Panel · damagedMAIN CARGO DECK POS 2L AFT HOLE IN FLOOR PANEL. REPAIRED IAW SRM 53-00-50-2R, PARA 4B.SDR IPXA12672734Floor Panel · damagedMAIN CARGO DECK POS 2L FWD HOLE IN FLOOR PANEL, OTBD PANEL 4"X1" DAMAGED HONEYCOMB. REPAIRED IAW SRM 53-00-50-2R 4C.SDR IPXA12672731Floor Panel · damagedFLOOR PANEL HAS DAMAGE AT DEF D473437 AND D473438 POS 1 ON MAIN CARGO DECK. FABRICATED FLOOR PANEL REF EO B767-5320-9693-H.SDR IPXA12672720Floor Panel · damagedMAIN CARGO DECK POS 2L MID 2 HOLES IN FLOOR PANEL WITHIN 2" OF EA OTHER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA12672719Floor Panel · damagedMAIN CARGO DECK POS 2L MID HOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672571Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 3 LT OTBD DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672570Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 2/3 LT OTBD SIDE DAMAGED, FABRICATED FLOOR PANE IAW EO B767-5320-9693-H.SDR IPXA2672622Floor Panel · damagedMCD POST 3 & 4 CENTER FLOOR PANEL DAMAGED MM 53-01-06-4. THIS IS A MAJOR REPAIR. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H REF /R 510721.SDR IPXA2672569Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 3 RT DAMAGED, FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672559Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 3/4 DAMAGED. FABRICATED NEW FLOOR PANEL, IAW EO B767-5320-9693-H.SDR IPXA2672558Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 2/3 CENTER DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672557Floor Panel · damagedMAIN CARGO DECK, FLOOR PANEL DAMAGED, DEF 475165. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA12672772Skin · corrodedINSPECTION TYPE:8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING - A SLIGHTY CORROSION IS FOUND AFTER FAIL-SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL-SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 &SDR IPXA12672768Skin · corrodedINSPECTION TYPE: 8C, FUSELAGE LT BS 955 BULKHEAD SIDE FITTING, SLIGHT CORROSION IS FOUND AFTER FAILSAFE TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE TEE FITTING TO THE FAILSAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 & REPROTECSDR IPXA12672767Tee Fitting · corrodedINSPECTION TYPE: 8C, FUSELAGE BS 955 TEE FITTING FWD LOWER HOLE MATTING SURFACE AREA FOUND FRETTING. TEE FITTING REPLACED AND INSTALLED IAW EO NO.B767-5350-17922-J APPX 'C' FIG 6, REPAIR IS CLASSIFIED AS MAJOR.SDR IPXA12672733Fairing · delaminatedINSPECTION TYPE: 8C, LEFT WING OTBD T/E FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1), FIG 5, REV 52.SDR IPXA2672594Connector · looseT/E FLAP DISAGREE ON APPROACH, WHEN FLAPS SELECTED PAST 5. ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR LOOSE. SYS CHECKED NORMAL IAW FIM 27-51-00, FIG 105.SDR IPXA12672519Escape Rope · exposedDURING PUSH BACK MX NOTICED L1 DOOR ESCAPE ROPE EXPOSED WITH DOOR CLOSED. RESECURED L1 DOOR ESCAPE ROPE IAW AMM 25-61-03-2.SDR IPXA12672518Autothrottle Sys · malfunctionedDUE TO A BURNING ODOR IN COCKPIT, WITH AUTOPILOT ENGAGED THRUST LEVERS CAME BACK RAPIDLY AND SPEED DEGRADED 20KTS, HAD TO PUSH THRUST LEVERS UP AND THEN NOTICED THE BURNING ODOR. ALL THIS OCURRED AT TOP OF CLIMB. PERFOMED MCDP TESTS 2,30 AND 40. ALL TESTS PSDR IPXA12672517Connector · looseT/E FLAP DISAGREE ON APP WHEN FLAPS SELECTED PAST 5, ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20 EMERGENCY DECLARED. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR PLUG LOOSE. SYS CKS NORMAL IAW FIM 27-51-00, FIG 105.SDR IPXA2672478Eadi · inoperativeCAPTAIN`S ADI WENT BLANK SELECTED ALTERNATE EFI NO CHANGE. AT 6,000`, DISPLAY CAME BACK ON. STARTED ARCING, SLIGHT SMOKE ODOR UNTIL BREAKER TRIPPED. DID NOT RESET BREAKER. ADI BLANKED ON ROTATION EADI REMOVED AND VISUAL CHECK BACK SIDE WIRING. NOTHING ABNOSDR IPXA12672771Fitting · crackedINSPECTION TYPE: 8C, BS 955 REAR SPAR BULKHEAD FITTING AREA 1 EA FASTENER HOLE FOUND CRACKED AT T-FITTING, CRACK ON 7 O/C POSITION APPROX .1250" IN LENGTH. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AREA T-FITTING. REPLACED AND INSTALLED IAW EO NR B7SDR IPXA12672770Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE RT BS 955, REAR SPAR BULKHEAD FITTING AREA 1 EA FASTENER HOLE FOUND CRACK AT FAIL - SAFE STRAP ON 4 O/C AND 10 O/C POSITION THROUGH THICKNESS AND .0625" IN LENGTH. REPAIRED IAW EO B767-5350-17922-J APPX 'D', ORIGINAL MATERIAL IS SDR IPXA12672766Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955 REAR SPAR BULKHEAD FITTING AREA HAS ONE FASTENER HOLE CRACKED AT FAIL SAFE STRAP ON 3 O/C AND 9 O/C POSITION THROUGH THICKNESS AND .0625" IN LENGTH. REPAIRED IAW EO B767-5350-17922-J APPX 'C', ORIGINAL MATERIAL IS 2024T351SDR IPXA12672745Frame · crackedINSPECTION TYPE: 8C, BS 1809.5 BULKHEAD FWD OUTER FRAME STRINGERS 6 TO 7R RADIUS AREA FOUND CRACKED. REPAIRED IAW SRM 53-80-08-2R9, FIG 201, REV 52, CRACK LENGTH APPROX 2 INCHES IN LENGTH, FRAME CUTOFF LENGTH 4.875 INCHES, CLASSIFIED AS A CATEGORY B MAJOR REPSDR IPXA2672652Structure · crackedINSPECTION TYPE: C, BS 1809.5 BULKHEAD FWD HORIZONTAL INNER CHORD RT 1EA FASTENER HOLE FOUND CRACKED. CHORD AT APPROX WL 257 & RBL28 AREA IS REPAIRED IAW SRM 53-80-08-2R10, FIG 201, REV 52, ORI MATL BAC1506-2466-7075T73511, CRACK LENGTH 0.5",TRIM OUT AREA 1.SDR IPXA2672447Skin · damagedFUSELAGE CROWN IS DAMAGED JUST FORWARD OF APU EXHAUST. REPAIRED IAW EO B767-5330-46446-A.
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