Boeing 767-34AF
Service difficulty reports · 6,301
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 IPXA2026092286713Cowling · crackedCRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.SDR IPXA2026092191640Panel · erodedERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.SDR IPXA2026092289443Nose Cowl · dentedDENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026092290656Nose Cowl · dentedDENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026092290813Nose Cowl · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATSDR IPXA2026092290842Nose Cowl · dentedDENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘ DIA : 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER EDGE ‘¡ DIA : 0.4", 32.4" FROM FWD EDGE, 31" FROM UPPER EDGE, AT 6 O'CLOCK ON THE INNER BARREL OFSDR IPXA2026092186627Floor Panel · crackedCRACKED PANEL, AFT CARGO FLOOR STRUCTURE, BS 1329, BL 0. REMOVED DAMAGE PANEL I.A.W SRM 51-40-02-0G REV. 96. INSTALLED FABRICATED PANEL I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 451T2612 SHEET 2 REV. B.SDR IPXA2026091898870Smoke Goggles · damagedCENTER SUPERNUMERARY SEAT SMOKE GOGGLES CRAZED AND BUBBLED REMOVED AND REPLACED CENTER SUPERNUMERARY SEAT SMOKE GOGGLES IAW MM 25-64-00SDR IPXA2026092267592Fairing · debondedDEBONDED SKIN , RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES SDR IPXA2026092166138Skin · puncturedSKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMOVE THE DELAMINATION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 SDR IPXA2026092172110Bracket · crackedCRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR IPXA2026092172477Angle · crackedCRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND DWG 313T2303 SH. 141 REV. A AND BOEING DWG NO. 313T2303 SH. 146 REV. -.SDR IPXA2026092450293Seal Depressor · corrodedCORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8610 SH.7 REV.D.SDR IPXA2026092450484Seal Depressor · corrodedCORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED FABRICATED SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8610 SH.8 REV.D.SDR IPXA2026092350550Tee Angle · broken- BROKEN - SPLICE TEE, LOWER FACE OF KEEL BEAM AT LOWER PANEL NO.149AL FWD SUPPORT, NEAR STA 962, LBL 5. REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8629 SH.2 REV.A.SDR IPXA2026092347262Angle · gougedPREVIOUS REPAIR ON MAIN DECK FLOOR SUPPORT STRUCTURE, LOCATED AT APPROXIMATE STA. 710 OUTBD OF LT. FWD CARGO PIT SIDEWALL, IS GOUGED IN THREE PLACES. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-52-2R REPAIR 9 REV.96 AND EGAT WORK SHEET 60756.SDR IPXA2026092350293Seal Depressor · corrodedCORRODED SEAL DEPRESSOR, LOWER FUSELAGE LT ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET.SDR IPXA2026092350484Seal Depressor · corrodedCORRODED SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET.SDR IPXA2026092150993Former · crackedCRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT BRACKET, NEAR WS 441.596. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:1142241 SH 4 REV: - AND UPS SREO-54290-REQ1 REV.3.SDR IPXA2026091850925Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:114T1240 SH 6 REV: - .SDR IPXA2026091850918Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.SDR IPXA2026091850822Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.SDR IPXA2026091850792Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.SDR IPXA2026091850818Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. <BR>2. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.SDR IPXA2026091847947Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:146T5650 SH 5 REV: C.SDR IPXA2026091847888Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. (REPLACE) ACCOMPLISHED OK TO INSTALL CHECK. PANEL NO:252YFF, 252QFS,252PSF.SDR IPXA2026091845796Floor Panel · dentedMAJOR REPAIR, DENTS ON THE FLOOR PANEL NO.231AFF (P/N 143T5876-78) IN THE MAIN DECK CARGO COMPARTMENT. (REPAIR) I.A.W AMM 25-57-02-404-016 AND AMM 25-58-03-404-004 REV.149 INSTALLED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2026091845779Floor Panel · dentedMAJOR REPAIR, DENTS ON THE FLOOR PANEL NO.231FFF (P/N 143T5876-49) IN THE MAIN DECK CARGO COMPARTMENT. (REPAIR) I.A.W AMM 25-57-02-404-016, AMM 25-57-90-424-011 AND AMM 25-58-03-404-004 REV.149 INSTALLED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CSDR IPXA2026092422876Keelbeam · corrodedFORWARD RIGHT SIDE OF EXPOSED KEEL BEAM AT STA 785 RBL 9 HAS CORROSION AROUND NUT PLATE. REPAIR DAMAGE AREA I.A.W EO-98691-REQ1 REV 1 AND EGAT EI F2026A53M-1944 REV.0SDR IPXA2026092322876Keelbeam · corrodedFORWARD RIGHT SIDE OF EXPOSED KEEL BEAM AT STA 785 RBL 9 HAS CORROSION AROUND NUT PLATE.SDR IPXA2026091329466Pump · faultedRECEIVED A CHYD PUMP1 OVERHEAT. RAN QRH PROCEDURE, RAN QRH PROCEDURE, DECLARED EMERGENCY FOR PRIORITY HANDLING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CTR HYS SYS ACMP NO.1 REF AMM 29-11-02/401 UP TO AND INCLUDING AMM TASK 29-11-02-404-018 PARA 3.F.(2SDR IPXA2026091811782Panel · erodedERODED SKIN, LOWER FACE L/H WING NO.5 SLAT LOWER CLOSURE PNL, NEAR INBD TRACK. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-43-01-2R-3 REFER TO SSDR IPXA2026091811821Skin · debondedDEBONDED SKIN, INBD EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 355, TOTAL: 2 AREA. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W CMM 57-53-51 REV 39 INSTALL THSDR IPXA2026091512611Antenna · damagedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.SDR IPXA2026092174292Hinge Fitting · crackedCRACKED HINGE FITTING, RT WING T/E NR 10 SPOILER.SDR IPXA2026091176660Seal · leakingENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR FOUND SEALANT MISSING FROM SEAMS IN SILL PLATE. REPLACED SEALANT. PRESSURIZED A/C AND FOUND NO MORE LEAKAGE/NOISE FROM CREW ENTRY DOOR.SDR IPXA2026091076660Seal · leakingENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR PRESSURE CHECK ENTRY DOOR IAW AMM 05-51-24. FOUND LEAK COMING FROM THE BOTTOM OF THE DOOR.SDR IPXA2026090945477Handle · faultedYELLOW SECURITY HANDLE WONT STOW ON CREW DOOR. REPLACED CREW ENTRY DOOR INTERLOCK PAWL IAW AMM 52-11-26. OPS CHECK GOOD.SDR IPXA2026102408659Fitting · brokenGROUND CREW FOUND CENTER ROLL OVER GUIDE (BUTTERFLY) BROKEN FREE FROM THE FLOOR. ACMX FOUND SEAT TRACK MOUNTING POINT IN FLOOR DAMAGED. INSTALLED NEW FITTING IAW SRM 51-40-02-0G REV.96 AND DWG NO:457T4000, SH 11 REV.B, & DWG 457T4000, SH 31, REV A.SDR IPXA2026091418249Bleed Valve · faultedATB, LT ENG HPSOV EICAS MSG ON TAKEOFF ROLL. ACCOMPLISHED QRH PROCEDURE, BUT BLEED LIGHT REMAINED ILLUMINATE, UNABLE TO FLY IN FEINE CONDITION, RESULTED IN ATB TO SZX. PER FIM 36-10 TREE 833. R & R LT ENG HPSOV IAW AMM 36-11-07. OPS & LEAK CHECK PER AMM GOOD.SDR IPXA2026090618249Warning Message · illuminatedAIR TURN BACK, LT ENG HPSOV EICAS MSG ON TAKEOFF ROLL. ACCOMPLISHED QRH PROCEDURE, BUT BLEED LIGHT REMAINED ILLUMINATED. RESULTED IN ATB.SDR IPXA2026090361862Lamp · inoperativeL1271 EMERGENCY CEILING LT INOPERATIVE. REPLACED THE LAMP AND LIGHT TEST OK, IAW AMM 33-51-11/201.SDR IPXA2026090220809Window · failedDURING CRUISE, THE CAPTAIN`S FWD WINDOW BEGAN ARCING IN BOTTOM LEFT PART OF THE WINDOW. WINDOW HEAT WAS IMMEDIATELY TURNED OFF, AND A FEW SECONDS LATER, THE WINDOW SHATTERED. REMOVED AND REPLACED LT FWD WINDOW ASSY IAW AMM 56-11-01-401, AND M191 WINDOW HEAT CSDR IPXA2026090120809Window · arcedDURING CRUISE, THE CAPT`S FWD WINDOW BEGAN ARCING IN BOTTOM LT AREA OF WINDOW. THE WINDOW HEAT WAS IMMEDIATELY TURNED OFF, & A FEW SECONDS LATER, THE WINDOW SHATTERED.SDR IPXA2026090120360Battery Pack · no testDURING PDC, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD.SDR IPXA2026090398854Fitting · crackedFOUND MAIN DECK CARGO FLOOR FITTING CRACK DAMAGE AT BS 1109 BL 0. REMOVED DAMAGE FITTING IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FITTING IAW SRM 51-40-02-0G REV. 96 AND DWG 457T4000 SH. 11 REV. B.SDR IPXA2026083105397Door · faultedMAIN CABIN DOOR YELLOW HANDLE WILL NOT MOVE. OPENED AND CLOSED CREW ENTRY DOOR INTERNALLY AND EXTERNALLY SEVERAL TIMES OBSERVING NORMAL EXTERNAL PRIMARY CAPTURE LEVER OPERATION IAW AMM 52-12-00/201 CONFIG 1. NO FAULTS NOTED, DOOR OPERATES NORMAL AT THIS TIME.SDR IPXA2026090447613Nose Cowl · dentedFAULT - DENT - SKIN , NO. 2 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.2", 16" FROM L/E AND AT 9 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR SDR IPXA2026090443491Nose Cowl · dentedDENT - SKIN , NO.1 ENG NOSE COWL INNER BARREL NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.3", 9" FROM AFT EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.SDR IPXA2026090446102Strap · corrodedFOUND FORWARD CARGO CEILING STRUCTURE CORROSION AT STA 566 RIGHT SIDE. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV. 96. ACCOMPLISHED REPAIR I.A.W EO-98506-REQ1 REV. 1, BOEING DWG NO. 453T1001 SH. 1 REV. A AND BOEING DWG NO. 453T1183 SH. 6 REV. -.
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