Boeing 767-300
Service difficulty reports · 2,148
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 = '767300' 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 = '767300' 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 IPXA2026042265192Skin · dentedDURING WALK AROUND INSPECTION FOUND DENT /HOLE IN FUSELAGE LEFT SIDE BELOW MAIN CARGO DOOR LEFT AND DOWN OF THE FORWARD STATIC PORT ABOUT STATION 478. CATEGORY B PERM SKIN REPAIR PERFORMED PER EO-97184-REQ1.SDR IPXA2026041865192Skin · dentedMAJOR REPAIR. DURING WALK AROUND INSPECTION FOUND DENT /HOLE IN FUSELAGE LEFT SIDE BELOW MAIN CARGO DOOR LEFT AND DOWN OF THE FORWARD STATIC PORT ABOUT STATION 478 FASTENERS REMOVED IN AREA OF REPAIR DOUBLER AND DAMAGED STRINGER REF SRM 51-40-02. DAMAGED SECSDR IPXA2026042066017Hinge · inoperativeDOOR HINGE COVER NOT RETRACTING REMOVED AND REPLACED CREW DOOR LOCK LATCH COVER HINGE. OPS CHECK GOOD. REMOVED AND REPLACED CREW DOOR LOCK LATCH COVER HINGE. OPS CHECK GOOD.SDR IPXA2026050856714Skin · ground damageK-LOADER HAND RAIL STRUCK AIRCRAFT FWD OF CARGO DOOR 1. I.A.W AMM 25-53-03-404-030 REV.148 INSTALLED FORWARD CARGO BALL PANEL NEAR STA 511 RBL 33.SDR FDEA202604160448Skin · delaminatedDELAMINATION IN LEADING EDGE AT 9" OF INBOARD END ON OUTBOARD FLAP LH WING LH WING, OUTBOARD FLAP AT LEADING EDGE ON 9" OF INB. EDGE WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R TABLE I, 51-70-17-0G PARAGRAPH 4A FIGURE 10 AND AMM 51-21-10-7 REV. 94 DEC 15,2025SDR FDEA202604150447Skin · delaminatedDELAMINATION ON L EDGE FLAP SKIN AT 24" FROM INB EDGE. RH OUTB FLAP RH WING, RH OUTBD FLAP ON LE FLAP SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 5 AND SRM 51-70-17-0G PAR 4A FIG 10 REV 94 DEC 15/2025SDR FDEA202604140445Skin · delaminatedDELAMINATION ON L EDGE INB MAIN FLAP AT 20" FROM OUTB EDGE. RH WING L/E INBD MAIN FLAP AT 20" FROM OUTBD EDGE RH WING WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 SHEET 5 TABLE 1 AND SRM 51-70-03-0G PAR 5A FIG 5 REV 94 DEC 15/2025SDR FDEA202604140444Skin · dentedDENT IN LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FAIRING FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP. LH WING WAS REPAIRED IAW B767 SRM 57-53-01SDR FDEA202604140443Skin · dentedDENT IN LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING WAS REPAIRED IAW B767 SRM 57-53-01SDR FDEA202604140442Skin · dentedDENT IN LOWER SURFACE ON MAIN FLAP AT 35'' OF OUTBOARD FAIRING FLAP AND 14.25" OF TRAILING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON MAIN FLAP AT 35" ON OUTBOARD FAIRING FLAP AND 14.2" OF TRAILING EDGE ON INBOARD FLAP LH WING WAS REPAIRED IAW SRM 57-5SDR IPXA2026041417434Water Separator · odorSTRONG DIRTY SOCK ODOR OBSERVED INFLIGHT. ODOR LESS NOTICEABLE WITH LEFT PACK OFF. R & R WATER SEPARATOR FOR LT PACK PER AMM 21-51-04. REVERSED DMP AND PERFORMED OPS CHECK. NO ABNORMAL SMELLS NOTED AT THIS TIME.SDR IPXA2026040917434Unknown · odorSTRONG DIRTY SOCK ODOR OBSERVED INFLIGHT. ODOR LESS NOTICEABLE WITH LEFT PACK OFF.SDR IPXA2026040707983A/C Pack · odorSTRONG SMELL OF OIL IN THE COCKPIT WHEN USING THE PACKS WITH APU ON STARTED APU AND OPERATED LEFT AND RIGHT AIR CONDITIONING PACKS IN ALL MODES FROM APU BLEEDS FOR 1 HOUR REFERENCE AMM 49-11-00 AND 21-00-00 WITH NO OIL SMELL COMING FROM VENTS IN COCKPIT AND CASDR IPXA2026040207983A/C Pack · odorSTRONG SMELL OF OIL IN THE COCKPIT WHEN USING THE PACKS WITH APU ON C/W DMP 49-11-1-1SDR IPXA2026031810844Unknown · odorSTRONG ODOR IN FLIGHT DECK. EVEN STRONGER ODORIN CARGO BAY (MCD) CREW NOTICED PHYSIOLOGICAL EFFECTS. CLEANED AND DISINFECTED FLIGHT DECK AND MAIN CARGO DECK BY ACFT MAINTENANCE AND AN OUTSIDE VENDOR TO REMOVE ODER REF 767 M/M 25-00-00 107-001. OK FOR CONTINUEDSDR IPXA2026031710844Unknown · odorSTRONG ODOR IN FLIGHT DECK. EVEN STRONGER ODOR IN CARGO BAY, CREW NOTICED PHYSIOLOGICAL EFFECTS.SDR IPXA2026031707108Unknown · odorAIRCRAFT HAS BEEN SERVICED 3 TIMES FOR A STRONG ODOR IN THE COCKPIT. MECHANIC ON ARRIVAL YESTERDAY SMELLED IT OUTSIDE. LAV FUNCTIONS NORMALLY. LOAD CREW COULD SMELL IN THE MAIN DECK. LAV SERVICED. INSPECTED CABIN AND MAIN DECK. REF: AMM 05-41-02. INSPECTED E&ESDR FDEA202603050317Escape Rope · unsecureHUB NOTIFIED THAT THE L1 DOOR ESCAPE ROPE IS HANGING OUT. STOWED L1 EMERGENCY ESCAPE ROPE, AND TAPED ESCAPE ROPE RETAINER , IAW AMM 25-61-04-8. AC OK FOR SERVICE.SDR IPXA2026031284337Transmitter · inoperativeAIR TURN BACK, UNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQ WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER AIRPLANE SUCCESSFUL ON BOTH HF RADIOS. HF RIGHT. T/S RIGHT HF SYSTEM FOUND SQUELCH ON PREVENTING RECEIVESDR IPXA2026031284304Transmitter · inoperativeATB, UNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQ WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER ARCFT SUCCESSFUL ON BOTH HF RADIOS. HF LT. T/S LT HF SYS, FOUND HF TRANSCEIVER STUCK ON 10MHZ AND FREQUENCY WOULSDR IPXA2026030384337Hf Comm · faultedUNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQ WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER AIRPLANE SUCCESSFUL ON BOTH HF RADIOS. HF RIGHT. RIGHT HF COM SYSTEM DEFERRED PER MEL 23-11-1-2A-2, PLACARD INSTALLED.SDR IPXA2026030384304Hf Comm · faultedATB, UNABLE TO RECEIVE HF RADIO TRANSMISSIONS ON EVERY HF FREQUENCY WE COULD FIND. CONTACTED DISPATCH, ATB REQUIRED. PRIOR TO DEPT HF CHECK WITH OTHER AIRPLANE SUCCESSFUL ON BOTH HF RADIOS. HF LEFT. DEFERRED LEFT HF COM SYSTEM PER MEL 23-11-1-2A-2, PLACARD INSDR IPXA2026022604803Rub Strip · chafedCHAFED WEAR STRIP, NR 1 ENG LT CORE COWL INNER FACE T/E UPPER SIDE. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV 94 AND CMM IPL 71-13-23 REV.47.SDR IPXA2026022604702Rub Strip · gougedGOUGED WEAR STRIP, NR 2 ENG RT CORE COWL T/E INNER SIDE UPPER PLATE. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV 94 AND CMM IPL 71-13-24 REV.50.SDR IPXA2026022606029Latch · wornWORN OUT - LATCH 3 EA, NO.1 ENG R/H FAN COWL OIL TANK ACCESS DOOR. (REPLACE). INSTALL NEW LATCH I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 71-11-10-51 REV. 141.SDR IPXA2026022606554Angle · crackedCRACK - ANGLE, NO.2 PYLON AFT FAIRING AFT BULKHEAD L/H AFT SIDE. (REPLACE). INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 313T2303 SH 166 REV: - AND 313T2303 SH 161 REV -.SDR IPXA2026022687694Spring · brokenBROKEN SPRING, NR 2 PYLON AFT FAIRING PANEL 446CL. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SHT 16, REV -.SDR IPXA2026022687742Door · gougedGOUGE - PLATE, NO.2 ENG R/H T/R COWL LOWER BLOWOUT DOOR L/E. (REPLACE). INSTALL BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINEERING IPC 78-32-22 REV.94.SDR IPXA2026022687780Bracket · crackedFAULT - CRACK - BRACKET, NO.1 PYLON HYDRAULIC RESERVOIR VENT TUBE AT CENTER AREA. (REPLACE). FABRICATE BRACKET (P/N:313T2380-836) PER BOEING DWG NO.:313T2380 SH 105 REV."-";PL 313T2380-836 REV."A" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 14 RESDR IPXA2026030222795Door · brokenBROKEN PANEL, LOWER FACE OF LT WING NR 3 SLAT OTBD SEAL DOOR. INSTALL NEW SEAL DOOR IAW SRM 51-40-02-0G, REV 94, AND AIPC 57-41-51-15 REV. 141.SDR IPXA2026022622496Former · crackedCRACK-FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 717.29 (REPLACE). INSTALL NEW NOSE FORMER IAW SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2164 SH 6 REV - AND UPS EO-96624-REQ1 REV1 .SDR IPXA2026022320352Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.SDR IPXA2026022320306Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.SDR IPXA2026022320466Angle · crackedFAULT - FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETESDR IPXA2026022320039Angle · crackedFAULT - FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETESDR FDEA202601120023Skin · wornWORN UPPER INSIDE SKIN TRAILING EDGE OF SLAT 5 (INBOARD). LH WING SLAT 5 T/E WEDGE UPPER INSIDE SKIN WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 (SHEET 1) AND SRM 51-70-10-2R REPAIR 4 FIG 202 (SHEET 8) REV 93 AUG 15/2025SDR FDEA202601010001Latch · crackedEMERGENCY LIFE RAFT STOWAGE COMPARTMENT LATCH CRACKED, HINDERING ACCESS. ABLE TO OPEN COMPARTMENT DOOR AND INSP, REF B767 AMM: 25-62-01-4-6/ IPC: 25-62-55-01 FIG01 SH7. FOUND ITEM 360 LATCH ASSY PLASTIC HOUSING CRACKED. AMM: 25-62-01-4-6 AMM: 25-60-00-00SDR FDEA202512302298Skin · delaminatedRH OUTBD FLAP HAD A DENT/IMPACT DAMAGE WITH AREA OF DELAM ON THE LEADING EDGE OF THE FLAP AT APPROX WS STA 741.0 REPAIRED RH WING OUTBD FLAP TRAILING EDGE NOSE SKIN L/E PNL (MPN: 113T3112-402) AT WS STA.741.0 (MARKED AREA) IN REF. TO 767 SRM 57-53-01-2R SDR CALA2025121212072Controller · failedCREW REPORTED NOISE/BANG/SHUTTER COMING FROM LT ENGINE IN TWO OCCASIONS DURING FLIGHT, AT 35K FT & THEN ON DESCENT. IN BOTH OCCASIONS N1 SPOOLED DOWN & EPR REDUCED, 0.91 OPPOSITE 1.07, EGT WAS APPROX 70 DEG HIGHER. L ENG SURGE DET MAINT MSG ON ARRIVAL. NOTEDSDR IXXA20251130002Failsafe · corrodedFLC DOOR CUTOUT STA 566 CORROSION AT FAILSAFE STRAP AND INNER CHORDSDR IPXA2025112159480Panel · crackedCRACK, PANEL OF FLOOR BEAM ( BL: 0 ), CGO STA: 1329 AT AFT CGO COMPT, ZONE : 156 (REPLACE). INSTALL NEW PANEL (P/N: 451T2603-65EG8U/WS#50823EGAT) I.A.W SRM 51-40-02-0G REV.93 AND BOEING DWG NO. 451T2612 SH 11 REV -.SDR IPXA2025112537400A/C Pack · odor**SUPPLEMENTAL SDR** ONCE TAKE OFF POWER WAS SET A TERRIBLE DIRTY WET SOCK SMELL FLOODED THE COCKPIT WE TURNED OFF THE RIGHT PACK AND THE FOUL SMELL WENT AWAY. REVERSED DMP AND RAN R/H PACK WITH R/T ENG, AND APU, ISOLATED VARIOUS LINES AND CLEANED WATER SEPARASDR IPXA2025111937400A/C Pack · odorONCE TAKEOFF POWER WAS SET A TERRIBLE DIRTY WET SOCK SMELL FLOODED THE COCKPIT. TURNED OFF THE RIGHT PACK AND THE FOUL LSMELL WENT AWAY. DEFERRED RIGHT PACK PER MEL 21-51-1-1 C/W DMP 21-51-1-1.SDR FDEA202511052131Floor Panel · dentedMAIN CARGO COMP. AT APROX. STA 300 ABOVE FLOORBOARD PANEL 222AFF RBL11 TO RBL33 SURFACE SKIN HAS INDENTATION (MARKED) FABRICATED NEW FLOOR PANEL 222AFF, MPN: 141T5856-117, RBL 11- RBL 33, STA 285-412 IN REF. TO BOEING DWG 141T5856-107, AND SR67-53-009. SEESDR IXXA20251029001Stub Beam · crackedCHORD STUB BEAM STA 903.5,LBL89, WL200 CRACKED.SDR IPXA2025100224705Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-134. (REPAIR) 1. I.A.W AMM 25-57-05-404-006, AMM 25-57-02-404-016 AND AMM 25-58-04-404-015 REV.146 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. 2. ATTACHMENT ARE UPLOADEDSDR FDEA202509271840Skin · dentedDENT ON INBD AFT FLAP WS 420 EXTERNAL SURFACE AT LH WING ON INBD AFT FLAP WS420 EXTERNAL SURFACE AT LH WING WAS EVALUATED AND REQUIRED REPAIR I.A.W SRM B767 57-53-01-2R FIG.201 SHEET 4 REV. 92 APR 15,2025 AND REPAIR I.A.W SRM B767 51-70-10-2R FIG 201 SHEETSDR IPXA2025092427547Angle · crackedFOUND CRACK-ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 OUTBD SIDE. I.A.W AMM 25-59-01-004-001 REV.146 REMOVED DADO PANEL AND G.V.I CHECK NORMAL. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 93. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 93 AND SDR IPXA2025091928923Angle · crackedFOUND CRACK-ANGLE, BULK CGO CEILING AREA, STA 1577 LBL 74 OUTBD SIDE. I.A.W AMM 25-59-01-004-001 REV.146 REMOVED DADO PANEL AND G.V.I CHECK NORMAL. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 93. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 93 AND BOEISDR IPXA2025091928882Angle · crackedFOUND CRACK-ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. I.A.W AMM 53-01-06-000-801 REV.146 REMOVED MAIN DECK CARGO PANEL/SEALANT AND G.V.I CHECK NORMAL, PANEL NO : 251CGF. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 93. INSTALLED NEW AN
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