Boeing 767-34AF
Service difficulty reports · 6,302
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 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. -.SDR IPXA2026090346191Angle · crackedFAULT - FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G RE.96. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 218T4100 SHEET 3 REV. B AND SDR IPXA2026090346129Former · crackedCRACKED FORMER , RT WING CAVITY FORMER OF THE CRACK AT OSS 648. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV 96, & DWG 114T2513, SHT 1, REV D, AND SREO-50900-REQ001, REV 2.SDR IPXA2026090428170Support Angle · crackedFOUND FWD CARGO DOORWAY CEILING SUPPORT CRACK AT BS 600. REMOVED DAMAGE SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96 AND DWG 143T8540, SHT 2, REV B.SDR IPXA2026090324513Bulkhead · crackedCRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL 437DD, INNER AREA. REMOVED DAMAGE BULKHEAD IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW BULKHEAD IAW SRM 51-40-02-0G, REV 96 AND DWG 313T3360, SHT 15, REV B.SDR IPXA2026090324466Bracket · crackedCRACKED BRACKET, NR 1 AFT FAIRING INNER DRAIN TUBE SUPPORT BRACKET. REPLACEED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96 AND DWG 272T0333, SHT 8, REV-.SDR IPXA2026090126837Bracket · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER OPEN ROD STOW AREA. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR IPXA2026090123388Bracket · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN HOLE ROD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-23, REV 47.SDR IPXA2026090123395Bracket · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN HOLD ROD BRACKET. REMOVED THE DAMAGED BRACKETS IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR IPXA2026082726958Doubler · crackedCRACKED DOUBLER, LT WING OTBD L/E CAVITY UPPER FIXED PANEL LOWER RIB LWR CHORD. REPAIRED AREA, NEAR OSS 531. ACCOMPLISH REPAIR ON DAMAGE AREA IAW SRM 57-41-09-2R-4, REV 96, & EGAT WORK SHEET 60681.SDR IPXA2026090407154Flap Track · erodedERODED SKIN, LT WING NR 1 FLAP TRACK FWD FAIRING EXTERNAL SKIN. REMOVED THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-53-70-2R-1, REFER TO SRM 51-70-17-0G-0 REV. 96SDR IPXA2026090907726Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. IAW AMM 52-11-26-004-001, REV 149 AND AMM 52-11-26-404-003, REV 149. REPLACED THE PAWL.SDR IPXA2026090307096Fairing · debondedDISBOND - SKIN, L/H WING NO. 3 FLAP TRACK MID FAIRING INBD T/E SKIN. 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 57-53-70-2R-1 REFER TO SRSDR IPXA2026090107073Skin · erodedEROSION SKIN, L/H WING NO. 2 SLAT OUTBD CLOSURE PANEL. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. 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 57-43-01-2R-3 REFER TSDR IPXA2026090107012Skin · erodedEROSION SKIN, L/H WING NO. 2 SLAT INBD CLOSURE PANEL AREA. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. MEASURE THE DAMAGE SIZE AND LOCATION ( L : 1", W : 0.5", 1.2" FROM AFT EDGE, 38.5" FROM INBD EDGE ). BOND THE REPAIR PLIES WITH FILM ADHESIVE SDR IPXA2026082611932Control Panel · faultedON DEPARTURE FOUND EXTERIOR EMERGENCY LIGHTS ON WITH SWITCH IN THE ARMED POS. R&R EMERGENCY LIGHTS PANEL ASSY PER AMM 33-51-08/401SDR IPXA2026082507726Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)SDR IPXA2026090192196Bracket · chafedCHAFED BRACKET, NR 1 ENGINE, LT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & IPC 78-32-31, REV 96.SDR IPXA2026090192222Bracket · chafedCHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & IPC 78-32-31, REV 96.SDR IPXA2026093083485Drag Brace · corrodedAFTER OTBD BUSHING REMOVAL, FOUND PITTING CORROSION ON CHAMFER FACE OF RT MLG FORWARD DRAG BRACE FITTING, AT WS 240 REAR SPAR, INSTALL NEW SERVICABLE BUSHINGS AT RT FWD DRAG BRACE FITTING IAW EA 767-5751-01-B0821, REV P3. ACCOMPLISHED REPAIR PER EO-98727-REQSDR IPXA2026082496541Control Handle · faultedGEAR DISAGREE MSG. WENT AROUND RAN QRH. GEAR DISAGREE MSG LIGHT EXTINGUISHED, GEAR EXTENDED ON SECOND ATTEMPT. ON EXTENSION ON FIRST TIME IT FELT STIFF GOING TO DOWN POSITION.? DETERMINED WITH PROXIMITY SWITCH TESTING PER MM 32-09-04 THAT GEAR DISAGREE WAS CAUSDR IPXA2026081809155Display · inoperativeEMERGENCY DECLARED, CAPT / FO LOST ALL PFD/MAP EICAS ALL LARGE DISPLAY SCREENS WERE LOST FROM FL200 TO PARK SPOT STBY INSTRUMENTS WORKED. REPLACED LT, RT & CNTR GGU'S REF AMM 31-65-02, OPS CHECK GOOD. REPLACED LT, RT & CNTR LDU'S IAW AMM 31-65-00, OPS CHECK GSDR IPXA202608179155Display · failedEMERGENCY DECLARED, CAPT / FO LOST ALL PFD/MAP EICAS ALL LARGE DISPLAY SCREENS WERE LOST FROM FL200 TO PARK SPOT STBY INSTRUMENTS WORKED.SDR IPXA2026081350986Hinge Pin · migratedFLIGHT DECK. CREW ENTRY DOOR. DOOR HANDLE COVER PLATE, SPRING LOADED. HINGE PIN MIGRATED 1/4 OF WAY OUT. RE-ALIGNED HINGE PIN. OPS CK GOOD. OK TO CONTINUE. REF IPC 52-12-01-02 ITEM # 474 & 52-12-00/601.SDR IPXA2026081225594Life Vest · expiredFLT DECK RT SUPERNUMERARY SEAT CREW LIFE VEST EXPIRED. REMOVED AND REPLACED RT SUPERNUMERARY SEAT CREW LIFE VEST PER AMM 25-62-00.SDR IPXA2026083182839Escape Rope · unwanted deployESCAPE ROPE AT CREW ENTRY DOOR DEPLOYED. REPLACED FLIGHT COMPARTMENT DESCENT ROPE COVER ASSY AND REINSTALLED DESCENT ROPE PER AMM 25-61-04SDR IPXA2026081088170Light · inoperativeEXIT LIGHT IS COMING OUT OF ITS SOCKET NEAR MAIN ENTERANCE DOOR CAREFULLY PUSHED THE LENS INTO ITS POSITION IAW AMM 33-51-01-402-030 4(B)(3)SDR IPXA2026081461884Former · crackedCRACKED FORMER, RT WING FIXED L/E NOSE BEAM SUPPORT STRUCTURE AT STA OSS 499. REMOVE DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95 AND DWG 114T2161, SH 1, REV E, & EO SREO-50900-REQ001, REV 2.SDR IPXA2026081146435Floor Panel · crackedFOUND AFT CARGO FLOOR PANEL CRACKED. IAW SRM 53-00-50-2R-0 REV. 95, CUT OUT THE DAMAGE AND CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 170F FOR 2 HOURS WITH A MINIMUM VACUUM OF 20 IN/HG IAW SRM 53-00-50-2R-0, REV 95.SDR IPXA2026081244447Cowling · dentedDENTED NR 2 ENG NOSE COWL INLET AT 7 & 5 O'CLOCK POSITIONS. CUT OUT THE DAMAGE & CLEAN, MEASURE THE CUT OUT ( (1) DIA : 1", 15.5" FROM FWD EDGE AT 7 O'CLOCK , (2) DIA : 1" , 15.3" FROM FWD EDGE AT 5 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL. BONDED TSDR IPXA2026080944690Former · crackedCRACKED FORMER, LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 499.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 1 REV. E AND EO SREO-50900-REQ001 REV2.SDR IPXA2026080842558Fairing · debondedDEBONDED SKIN, RT AFT WING TO BODY FAIRING EXTERNAL, PANEL 198CR. IAW SRM 52-40-02-2R-4, REF SRM 51-70-17-0G-0, & SRM 51-70-14-0G-0, REV 95. REMOVED DEBONDED MATERIAL & CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 220 MINUTES WITH MINIMUM VASDR IPXA2026081527200Shaft · corrodedFOUND LT WING OTBD FLAP NR 2 SUPPORT CRANK ARM AND INPUT SHAFT CORROSION. IAW AMM 27-51-21-024-001, REV 148, REMOVED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUT SHAFT. IAW AMM 27-51-21-424-032, REV 148. INSTALLED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUTSDR IPXA2026081903745Skin · crackedMAJOR REPAIR, SKIN , DURING PERFORM T/C : EO-24301-JIC001 FOUND SKIN CRACK AT BS 1725.5 , S-7R. ACCOMPLISH THE REPAIR I.A.W EO-24301-JIC3 REV7 AND SRM 53-80-01-2R-5 REV.95 AND EGAT WORK SHEET NO.60614 AND EO-98363-REQ1 REV1.SDR IPXA2026081706832Ring · crackedFOUND NR 1L T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT IAW EO-87822-REQ01L-REPL REV3.SDR IPXA2026081706840Ring · crackedFOUND NR 1R T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT I.A.W EO-87822-REQ01R-REPL REV4.SDR IPXA2026081303363Angle · crackedFOUND THE FIRE DETECTION LOOP FASTENER STRIP CRACKED AT BS 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 218T4100 SH 3 REV: B AND BOEING DWG NO: 218T4SDR IPXA2026081107438Angle · crackedTHE BULK CARGO INBOARD ANGLE AT BS 1578, LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650, SH 5, REV C.SDR IPXA2026081107416Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV.95 AND DWG 146T5650, SH 5, REV C.SDR IPXA2026081107408Angle · crackedTHE BULK CARGO OTBD ANGLE AT BS 1578, RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G REV.95 AND DWG 146T5650 SH 5 REV.C.SDR IPXA2026080803361Floor Panel · crackedCRACKS ON THE FLOOR PANEL NO. 251XFF (P/N 146T5869-89) IN THE MAIN DECK CARGO COMPARTMENT. REMOVED THE FLOOR PANEL IAW AMM 53-01-06-000-801 REV. 148. IAW AMM 53-01-06-400-801 REV.148. INSTALLED THE FLOOR PANEL 251XFF.SDR IPXA2026081187679Angle · crackedTHE BULK CARGO INBOARD ANGLE AT BS 1578, RBL 80 IS CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650 SH 5 REV.C.SDR IPXA2026080988147Former · crackedCRACKED FORMER , LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 648.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG NR 114T2163 SH 1 REV. E, AND EO SREO-50900-REQ001 REV2.SDR IPXA2026080790105Wedge · debondedDEBONDED SKIN , LT WING NR 4 SLAT TE WEDGE INBD. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE DAMAGE AREA I.A.W. 767-300F SRM 57-43-02-2R-1. INSTALL THE REPAIR CORE PLUG, FILLER AND INTERNAL DOUBLER WITH FILM ADHESIVE AND COMPOUND I.A.W. 767-300F SRM 51-70-10-2R-SDR IPXA2026080792047Antenna · erodedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN IAW SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 95. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026080344837Lens · brokenEXIT SIGN AT CREW ENTRY DOOR BROKEN/DETACHED. RESECURED EXIT SIGN COVER ON CREW ENTRY DOOR IAW AMM 20-00-00 STANDARD MAINTENANCE PRACTICES.SDR IPXA2026072859394Unknown · odorON DEPARTURE @ HIGH POWER SETTINGS STRONG SMELL OF DIRTY SOCKS? ON THE FLIGHT DECK. STAY UNTIL PASSING 10000 COULD NOT DUPLICATE PROBLEM UNPIN ARRIVAL. T/S PER FIM 21-00-00 NO EVIDENCE OF LEAKS. VERIFIED RAM AIR INLET IS CLEAR.SDR IPXA2026072316966Control Panel · inoperativeEMERGENCY DECLARED, DIVERTED. RECEIVED CABIN ALT WARNING AT 40,000 FT. AUTO 1 AND AUTO 2 NOT WORKING. WAS ABLE TO REGAIN PRESSURIZATION CONTROL IN MANUAL MODE REMOVED AND REPLACED CABIN PRESSURIZATION SELECTOR PANEL IAW AMM 21-31-01. OPS TEST GOOD REMOVED ANSDR IPXA2026072263413Elevator · damaged***SUPPLEMENTAL SDR*** LINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LH INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESSED OPS CHECKS PER GMM 04-02. INSTALLED LEFT INBD ELEVATOR. REF MM 27-31-01-401.ALL BOLTS TORQUED SDR IPXA2026072163413Elevator · damagedLINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LT INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESSED OPS CHECKS PER GMM 04-02.
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