Boeing 767-3Y0
Service difficulty reports · 1,443
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 = '7673Y0' 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 = '7673Y0' 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 UIEA2026012900019Tape · damagedFIRST OBSERVER ELT TAPE IS DAMAGED(<P>RESECURED TAPE AS PER HONEYWELL CMM JOB TASK 25-60-10. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026012900020Fitting · wrong partLAVATORY PORTABLE O2 BOTTLE MASK HAS INCORRECT FITTING TO ATTACH TO O2 BOTTLE.(<P>REMOVED & REPLACED O2 MASK ASSY IAW AMM 35-31-00. OPS CHK OK.THIS CLEARS MDDR 246793. </P>)SDR UIEA2026012000015Elt · inoperativeELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(<P>R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED</P>)SDR UIEA2025122701359Elt · looseELT NEAR RH CB PANEL TAPE IS LOOSE & 1 LATCH WILL NOT CLOSE. INSTALLED TAMPER TAPE ON FWD ELT IAW AMM 25-61-05-200-801. NO DEFECTS NOTED.SDR UIEA2025121501345Stowage Box · no testDURING PREFLIGHT, FOUND OBS SEAT O2 MASK DOES NOT RESET DURING TEST. R & R OBSERVER'S O2 MASK ASSY IAW AMM 35-11-51 & IPC 35-11-51. OPS & LEAK CHECK GOOD AT THIS TIME.SDR UIEA2025112601326Elec Connector · damagedGEAR DISAGREE, GEAR DOORS EICAS MESSAGE AFTER GEAR UP SELECTION. PERFORMED PSEU LDG SYS 1 & 2. NO FAULT FOUND IAW AMM 32-09-04-204-013. PERFORMED PSEU LDG SYS 1 & 2, NO FAULTS FOUND IAW AMM 32-09-04-204-013. INSTALLED & REMOVED RT MAIN GEAR PIN ON SIDE BRSDR UIEA2025112501325Pseu · faultedRH LANDING GEAR TOOK EXCESSIVELY LONG TO EXTEND AND / OR RH MAIN GEAR TO ILLUMINATE, LH AND NOSE GREEN LIGHTS WERE THE ONLY LIGHTS FOR 5-6 SECONDS. AT GEAR UP SELECTION, RECEIVED GEAR DISAGREE EICAS CAUTION MSG, GEAR DOORS EICAS ADVISORY MSG, AND A LDG GEAR MOSDR UIEA2025102001275Engine · no discrepancyON TAKE OFF ROLL, RECEIVED LT & RT ENG BLEED EICAS MSG & MASTER CAUTION LIGHT. RTO, PERFORMED BITE TEST IAW FIM 36-20 FT 804. FOUND 0 MSG ON THIS FLT LEG. EICAS MSG CLEARED. ALSO, PERFORMED WEU TEST IAW AMM 31-51-00, OPS CHK GOOD. FOUND MSG TO BE NORMAL.SDR UIEA2025101001264Shutoff Valve · faultedC HYD SYS PRESS EICAS MESSAGE DISPLAYED IN FLIGHT, HMG INOP. HYD PRESS INDICATION OPERATES NORMAL PER AMM 29-31-00-001. PERFORMED ADP SYS TEST PER B767 AMM 29-11-00. NO DEFECTS NOTED. TRANSFER TO DMI 239843 PER MEL 24-25-01-01D CAT A. R & R SOV PER AMM 24-2SDR UIEA2025101001266Regulator · leakingPAX OXYGEN TANK (BOTTLE 2) REGULATOR LEAK(<P>REMOVED AND REPLACED PAX OXYGEN TANK REGULATOR IAW B767 AMM 35-11-03. LEAK & PRESSURE CHK OK</P>)SDR UIEA2025090801169Hook And Loop · damagedHOOK AND LOOP FOR EVAS ON CAPT SIDE NEEDS TO BE ATTACHED. EVAS IS SECURED WITH BOLTS. NO HOOK AND LOOP ON EVAS IAW AMM 25-60-99. NO FURTHER DEFECTS NOTEDSDR 21GA20250906018Warning Message · false activationON APPROACH, SELECTED FLAPS TO 20. RECEIVED TE FLAP DISAGREE EICAS MESSAGE. DID GO AROUND, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURE. NO DEFECTS NOTED.SDR UIEA2025080401084Flashlight · no discrepancyL1 DOOR ENTRY WAY EMERGENCY FLASHLIGHT INOPERATIVE. OPS CHK ENTRY WAY FLASHLIGHT IAW AMM 25-05-03, OPS CHECK GOOD.SDR UIEA2025073001069Lens · scratchedOBSERVER SMOKE GOGGLES LENS SCRATCHED. REPLACED OBS SMOKE GOGGLE PER IPC 25-64-54-01B ITEM 30. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100925Structure · no discrepancyAT APPROXIMATELY 310 KIAS, APPROXIMATELY 10 KNOTS OVERSPEED WITH OVSPD WARNING WHILE IN DESCENT 0 FLAPS ADVISE FLT LEVEL 200. WORK WITH MCC AND PER AMM 05-51-08. COMPLETED PHASE 1 INSPECTION, NO DAMAGE WAS FOUND. LOG ITEM CLOSED.SDR UIEA2025070400832Fmc · odorCAPT REPORTS ELECTRICAL ODOR IN COCKPIT AFTER BLOCK, DETERMINED CAPT FMS CDU BLANKED AND CIRCUIT BREAKER OPEN.(<P>COLLARED CIRCUIT BREAKER, PART ORDERED FOR NGO. REPLACED CA FMC CDU IAW AMM 34-61-02. CLEARED MDDR 233639. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030600213Structure · damagedDAMAGE TO AFT LOWER CORNER OF FWD CARGO DOOR, CW SRM 5230011A1. PERMANENT REPAIR OF DOOR REQUIRED AT THE NEXT CHECK OR BEFORE 24 MONTHS.(<P>CRACK WAS REPAIRED IAW TRE6752055 & CMA-TLS-25-0009-05B. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030600214Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR RH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENTS WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)SDR UIEA2025030600217Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR LH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENT WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)SDR UIEA2025030600219Actuator · leakingRH WING SPOILER #12 WITH LEAK.(<P>POWER CONTROL ACTUATOR SPOILER #12 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-60-00-825-072 REV 144. NO LEAK FOUND, SPOILER 12 IS GOOD FOR SEVICE.</P>)SDR UIEA2025030600220Skin · crackedFWD ENTRY DOOR, AFT LOWER CORNER, HOLE 4 WITH CRACK INDICATION ON BEAR STRAP APPROX 10 O'CLOCK, AND HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 10 O'CLOCK, 4 AND 11 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51SDR UIEA2025030600221Skin · crackedSERVICE DOOR, AFT LOWER CORNER, HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 2 AND 8 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51-40-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030600222Lamp · inoperativeEMERGENCY LIGHTS OF THE CABIN LH INOP.(<P>TASK CARD A-06-040-01/002 EMERGENCY LIGHTS OF THE CABIN LH, LAMPS WERE REPLACED IAW AMM 33-22-01 DATE. 10MAY10. TEST WAS PERFORMED SATISFACTORY.</P>)SDR UIEA2025030800224Sign · looseEMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE (2 EACH).(<P>TASK CARD A-06-040-01/004 EMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE. TWO SCREWS WERE INSTALLED CORRECTLY IAW AMM 33-51-01-412-003 REV 144 DATE 22DEC24. NO FURTHER DEFECTS NOTED.</P>SDR UIEA2025030800225Actuator · leakingLH WING SPOILER ACTUATOR #2, WITH LEAK EVIDENCE.(<P>POWER CONTROL ACTUATOR SPOILER #2 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-61-00-825-072 REV 144. NO LEAK FOUND, SPOILER 2 IS GOOD FOR SERVICE.</P>)SDR UIEA2025030800226Skin · corrodedRH WING INBOARD TE FLAP, CORROSION ON LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 RI ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025030800227Feel Unit · leakingLEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE.(<P>LEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE. ELEVATOR FEEL UNIT WAS REPLACED AND TEST WAS PERFORMED IAW AMM 27-31-19-424-015SDR UIEA2025030800229Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTW OUTB AND MAIN TANK, STRG 6, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 6 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT PS 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISFACTSDR UIEA2025030800231Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 10, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 10 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISSDR UIEA2025030800236Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 15, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 15 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISSDR UIEA2025030800239Skin · corrodedUPPER FUSELAGE SURFACE WITH CORROSION AT THE BASE OF THE TOP TCAS ANNTENA.(<P>UPPER FUSELAGE SURFACE CORROSION AT THE BASE OF THE TOP TCAS ANNTENA. REPAIR WAS PERFORMED IN ACCORDANCE WITH TRE6753716 FEB 24, 2025. FVC TITLE REPAIR- FUSELAGE SKIN- CROWN AREA-CORSDR UIEA2025030800242Transmitter · faultedTRANSMITER POSITION FLAPS M489 LOW INSULATION RESISTANCE.(<P>FLAP POSITION TRANSMITTER M489 WAS REPLACED IAW AMM 27-51-45-422-030 REV 144. FLAP POSITION TRANSMITTER M489 ADJUSTED AND TEST PERFORMED IAW AMM 27-51-45-822-161 REV 144. NO FURTHER DEFECTS NOTED.</PSDR UIEA2025030800245Skin · dentedLOWER HALF OF FUSELAGE, BTW STA 654+44 AND 654+66, BTW STR 34L AND 33L, DENT ON SKIN.(<P>THE DENT WAS EVALUATED AND FOUND OUT OF LIMIT. IT WAS REPAIRED IAW SRM 53-00-01-2R-29 REPAIR 29. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031100258Servo · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN BOTH YAW DAMPER SERVOS.(<P>YAW DAMPER SERVOS LH AND RH WERE REPLACED IAW AMM 22-21-02-414-016 REV 144. (OFF PART RH PN: 1540500-9 SN: 973BC, LH PN: 1536600-5 SN: 1856BA) INSTALLATION TEST WAS SATISFACTORY.SDR UIEA2025031100259Actuator · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN SERVO VALVE.(<P>RUDDER RATIO CHANGER ACTUATOR WAS REPLACED I.A.W AMM 27-21-15-422-024 OPERATONAL TEST WAS PERFORMED AND NO LEAKS FOUND, TORQUE APPLIED 280 LB-IN, 360 LB-IN S/N 0823114404 DATE 12DEC2026.</PSDR UIEA2025031800355Skin · corrodedVERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".(<P>VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".THE VERTICAL STABILIZER LEADING EDGE TIP HAS BEEN REPLACED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025031800356Skin · corrodedVERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A).<BR>(<P>VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A) WAS REPLACED IAW SRM 51-10-02-0G-0 REV. 127 15-DEC-24.SDR UIEA2025032100365Stowage Box · no testDMI 225437 PASSENGER #3 OXIGEN MASK REST SWITCH DOESN'T TEST. SEAT NOT ALLOWED TO BE OCCUPIED.(<P>STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001 REV 144, 22DEC2024 AND TEST WAS SATISFACTORY. NO FOUND LEAKS.</P>)SDR UIEA2025032100366Skin · dentedRH WING, INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WITH DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 SDR UIEA2025032100367Skin · dentedRIGHT WING INBD FLAP UPPER AND LOWER SKIN WITH SEVERAL DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DESDR UIEA2025032100368Skin · delaminatedRH WING, OUTBOARD FLAP, LOWER SURFACE, 9" TO 24" FROM INBOARD EDGE AND 23.5" TO 34" FROM LEADING EDGE, DELAMINATION.(<P>RH WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 PAG 1,4 FIG 201 SHEET 3 REV 127 15-DECSDR UIEA2025032100369Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1646, LH SIDE.(<P> APU FUEL SHROUD LINE WAS REPLACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDI NG TEST 0.5 MILLIHOMS SN: B0005830 DATE: 04-JSDR UIEA2025032100370Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1720.5, LH SIDE.(<P>APU FUEL SHROUD LINE WAS REPL ACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDING TEST 0.5 MILLIHOMS SN B0005830 DATE: 04-JSDR UIEA2025032100371Fuel Line · bentACCESS PANEL 197DL, FUEL LINE BENT.(<P>ACCESS PANEL 197DL, FUEL LINE WAS REPLACED. IAW AMM 28-13-06-404-005. REV 144. DEC 22, 2024. NO MORE ACTIONS REQUIRED. GOOD FOR SERVICE.</P>)SDR UIEA2025032100372Anti-Skid Valve · no testMLG, WHEEL #5, BRAKE UNIT, WHEN TEST WAS BEING PERFORMED, THE RECORDED PRESSURE WAS LOWER THAN PERMITTED.(<P>ANTISKID VALVE OF BRAKE #5 WAS REPLACED. IAW AMM 32-42-03-404-017. REV 144. DEC 22, 2024. TORQUE APPLIED: 105 LB IN. S/N: 0524121903. DATE: 15-MAY-25. SDR UIEA2025032200376Skin · corrodedRH WING INBOARD TE FLAP, CORROSION LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 R1 ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025020500119Oxygen Mask · inoperativePASSENGER #3 OXYGEN MASK INOP.(<P>TRANSFER TO DMI 225437 PER MEL 35-11-03-02A CAT C DUE DATE 15FEB25</P> / <P>LP 1810355 ITEM M10, 21MAR25: STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001. TEST SATISFACTORY, NO FOUND LEAKS. IPC 35-11-52-15 REV 76 22FEB25SDR UIEA2025012600108Elt · abnormalELT AT ENTRANCE HAS MASKING TAPE OVER THE WATER SOLUABLE TAPE(<P>R/R L1 DOOR L1 & BRACKET STRAP OPS CHK GOOD IAW AMM 25-63-03-400-802 & AIPC 25-63-52-97. DMI 224932 CLOSED</P>)SDR UIEA2024120301162Seal · damagedRIGHT O/B T/E FLAP WITH SEAL DAMAGED AT INBOARD SIDE.(<P>REMOVED DAMAGED SEAL AT R/H O/B T/E FLAP, I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW SEAL AS REQUIRED AT R/H O/B T/E FLAP, I/B SIDE AREA PER BOEING 767-300 AMM 57-25-01-05 & AMMSDR UIEA2024120301163Latch · brokenENG #2 NACELLE STRUT, INBOARD ACCESS PANEL WITH LATCH BROKEN.(<P>REMOVED DAMAGED LATCH AT ENG #2, NACELLE STRUT INBOARD ACCESS PANEL AREA, LOCATED, CLEANED, TRIMMED, SECURED, ADJUSTED, SAFETY WIRE, INSTALLED NEW LATCH AS REQUIRED AT ENG #2 NACELLE STRUT, INBOA
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