Boeing 767-34AF
Service difficulty reports · 6,281
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 IPXA2026102276179Lock Mechanism · faultedCREW REPORTS RIGID BARRIER DOOR UNABLE TO OPEN ON PREFLIGHT. PRIMARY LATCH LOCKING MECHANISM FAULTY. PRM ISO VALVE C/B K-3 AT P-33 OPENED AND COLLARED TO SHUT OFF AIR FLOW INTO THE PRM.SDR IPXA2026102133469Floor Panel · damagedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE ,SDR IPXA2026102108780Floor Panel · damagedMAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.149 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMAL.IAW AMM 53-01-06-000-801 REV.149, REMOVED MAIN DECK CARGO FLOOR PANEL. SDR IPXA2026101806238Skin · puncturedDURING WALKAROUND, FOUND A PUNCTURE AT SLAT NR 10 (WS 624). SLAT CRACKED AT SEVERAL SPOTS, NUMEROUS RIVETS SHEARED. R/R SLAT #10 (STATION 624) IAW MM 27-81-02-024. ACCOMPLISHED OPS TEST PER MM 27-81-02/501 TEST FAIL. DUE TO NO SLAT TARGETS. S296,S310 SENSOR TASDR IPXA2026101456665Adc · malfunctionedEMERGENCY DECLARED, IN CRUISE EXPERIENCED AIRSPEED UNRELIABLE SITUATION PER QRH CHECKLIST WE DETERMINED THE LEFT SIDE WAS UNRELIABLE. DUE TO NON SPECIFIC FIM TASK, USED FAULT CODE INDEX WITH CODE 34 12 77 01 REV 149, REPL L ADC IAW AMM 34-12-01/401 REV 149, SDR IPXA2026101442976Flap System · faultedAIR TURN BACK, EMERGENCY DECLARED. AFTER TAKEOFF ON FLAP RETRACTION EICAS MESSAGE LE SLAT ASYMMETRY. FOLLOWED QRH PROCEDURE COULD NOT RETRACT SLAT. RETURNED SDF.SDR IPXA2026101325515Controller · faultedFO`S R2 WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED LT FWD AND RT SIDE WINDOW HEAT CONTROLLER UNIT (M191) IAW AMM 30-41-01/401. BITE TEST PASSED IAW B767 AMM 30-41-01-404-007. REVERSED DMP, AND REMOVED PLACARD.SDR IPXA2026101092858Life Raft · partial deployLIFE RAFT IN STOWAGE COMPARTMENT PARTIALLY DEPLOYED. REPLACED LIFE RAFT REF MM 25-62-01/401SDR IPXA2026102268685Skin · damagedMAJOR REPAIR, PANEL AFT OF 321D RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 7.5€? FROM BOTTOM & 12€? FROM LEADING EDGE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, IAW NDT MANUAL PART 1 51-01-SDR IPXA2026102268850Skin · damagedMAJOR REPAIR, PANEL AFT OF 321C RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 43€? FROM TOP & 14€? FROM TRAILING EDGE. SEE ATTACHED PICTURE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, I.A.W. 767SDR IPXA2026100856727Skin · debondedFAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W UPS SREO-70175-RSDR IPXA2026100857298Skin · crackedFAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300FSDR IPXA2026100553573Former · brokenBROKEN FORMER, LT WING OUTBD L/E FOLDING NOSE INNER SIDE AT OSS 441.60, ADJACENT NR 5 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 96. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 96, DWG 114T2241, SH 4, REV -, AND SREO-54290-REQ1, RSDR IPXA2026100560445Lens · missingCOCKPIT EMERGENCY LIGHT PANEL -LIGHT INDICATION MISSING LENS, REPLACED LENS IN REF WITH AMM 33-16-02 OPS CK NORMALSDR IPXA2026100259603Door Latch · bindingENTRY DOOR SECURE LATCH IS VERY HARD TO CLOSE /LATCH. LUBRICATED CREW ENTRY DOOR SECURE LATCH PER AMM 12-21-18/301.OPS CHECK OF CREW DOOR OK.SDR IPXA2026100503114Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.2", 18.2" FROM L/E, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR SDR IPXA2026100503125Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 3 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.25", 20.5" FROM L/E, AT 3 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FORSDR IPXA2026100603239Skin · dentedFAULT - DENT - SKIN , NO.2 ENG NOSE COWL INNER BARREL AT 8 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 8.2" FROM T/E, AT 8 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 SDR IPXA2026100603252Skin · dentedDENTED SKIN , NR 2 ENG NOSE COWL INNER BARREL AT 5 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM T/E, AT 5 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS SDR IPXA2026093002770Trim Panel · detachedMAIN ENTRY DOOR SEAL TRIM CAME OFF WHEN CLOSING DOOR REINSTALLED SEAL ITEM 15 INTO RETAINER ITEM 20 PER IPC 52-11-02-10A NO AMM REFERENCE COULD BE FOUND FOR THE INSTALLATION OF THIS DOOR CUTOUT/LINING SEALSDR IPXA2026093001662Seal · detachedFORWARD UPPER L1 DOOR SEAL PARTIALLY DETACHED. REINSTALLED FORWARD UPPER UNPRESSURIZED SEAL IN RETAINER OF FWD SIDE DOORWAY LINING PER AIPC 25-20-00-01B.SDR IPXA2026093004390Handle · bindingLIFE RAFT BIN HANDLE HARD TO OPEN LUBRICATED AS NEEDED. HANDLE. OPS CK OKSDR IPXA2026100465120Stiffener · crackedMAJOR REPAIR, STIFFENER CRACK AT CENTER FRONT BS 785.9 RBL 33. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV.96 AND EGAT WORK SHEET NO.60769 AND UPS SREO-58151-REQ001 REV2.SDR IPXA2026100465056Stiffener · crackedSTIFFENER CRACK AT CENTER FRONT BS 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2, REV 96 AND EGAT WORK SHEET NR 60770 AND SREO-58151-REQ001 REV 2.SDR IPXA2026092829503Handle · bindingCREW ENTRY DOOR CAPTURE LEVER STICKS IN INBOARD POSITION. ++ FOUND DOOE CREW ENTRY DOOR INTERLOCK PAWL WORN, REMOVED AND REPLACED INTERLOCK PAWL REF 767 M/M 52-11-26 OPERATED CREW ENTRY DOOR REF 767 M/M 52-12-00-862-001-001. DOOR OPERATES OK.SDR IPXA2026092495235Pawl · not seatedL FWD ENT DOOR SECURE HANDLE WILL NOT SEAT FOUND DEEP GOUGES IN ENTRY DOOR INTERLOCK PAWL. REPLACED INTERLOCK PAWL IAW AMM 52-11-26-404-003. OPS CHECK GOOD IAW AMM 52-11-26-710-801.SDR IPXA2026092364703Unknown · odorVERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180 REF AMM 71-00-00-795-034-H03 TEST NO. 3 - GROUND TEST - IDLE LEAK TEST. RAN ENGINES FOR 15 MINUTES WITH NO NOXIOUS ODOR NOTED AT THIS TIME WHILE ENGINE 2 SOLE SOURCE OF BLESDR IPXA2026092379070Accelerometer · oscillatesDURING CLIMB EXPERIENCED NOTICABLE OSCILLATIONS COMING FROM THE TAIL THAT DISSIPATED AT CRUISE. ALL ENG INDICATIONS NORMAL VERTICAL STABILIZER ACCESS PANELS AND RH ELEVATOR PCU PANLES CLOSED IAW AMM 27-31-05 REV149. FOUND FAULT DURING YAW DAMPER SYSTEM BITE PRSDR IPXA2026092264312Warning Message · false activationEMERGENCY DECLARED ON APPROACH TO LANDING. FLAPS 25 SELECTED AND LE-SLAT DISAGREE EICAS CAME ON. TROUBLESHOT IAW FIM 27-51 FT 808, NO FAULTS NOTED. EXTENDED AND RETRACTED SLATS/FLAPS IAW AMM 27-81-00. OPS CHECKED GOOD.SDR IPXA2026092264703Unknown · odorVERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180. PERFORMED GVI IN BOTH PACK BAYS WITH NO OBVIOUS FAULTS NOTED. DURING RIGHT ENGINE RUN, EXHAUST FUMES WERE DETECTED IN THE FLIGHT DECK. SWAPPING BETWEEN PACK 1 AND PACK 2 SDR IPXA2026092308451Skin · ground damageMAJOR REPAIR, CAN BLEW OFF THE K LOADER DUE TO JET BLAST IS UNDER BELLY OF AIRCRAFT LT SIDE STATION 698-720 STRINGER S39-S36 FABRICATED FREEZE PLUG PER STEP 10 OF EO-98676-PRELIM2. SKIN REPAIR COMPLETED PER EO-98676-REQ1.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.
Back to Boeing 767-34AF