Boeing 767-31B
Service difficulty reports · 616
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 = '76731B' 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 = '76731B' 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 UIEA2024072200716Brake Pads · wornNOSE LANDING GEAR WHEEL WELL, WEAR ON LEFT AND RIGHT SPIN BRAKES (PADS).(<P>NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT SPIN BRAKES (PADS) WERE REPLACED IAW AMM 32-45-05-422-007 REV 142 DATE 22 APR 24. TORQUE APPLIED 35 LBIN S/N 0423902837 DATE 24 OCT 24. GOOSDR UIEA2024072200717Placard · damagedLOWER FUSELAGE EXTERNAL SKIN, ILLEGIBLE LABELS ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2.(<P>LOWER FUSELAGE EXTERNAL SKIN, ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2. LABELS WAS INSTALLED CORRECTLY IAW AMM 20-10-12-404-004 REV. 142 DATE 22 APRSDR UIEA2024072300732Access Panel · leakingRH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WITH LEAK(<P>RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033 REV 142 22-APR-24 ,</P> / <P>BONDING: 01 MILLIOHMS / SERIAL BONDING: 1534 / DATE EXP: 22-ENE-25, INSTALATION OF PSDR UIEA2024072300733Skin · delaminatedLH WING, SLAT #1, EXTERNAL SURFACE, MIDDLE SIDE WITH DELAMINATION(<P>LH WING, SLAT #1, EXTERNAL SURFACE WAS REPAIRED IAW SRM 57-43-02-2R-1 PAG 1-2 AND SRM 51-70-10-2R-4 FIG 201 SHEET PAG 8,16 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072300734Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 185(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 185 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 REV 49 APSDR UIEA2024072300735Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 169(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 169 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 PAG 6-7 RSDR UIEA2024072300736Shim · migratedFUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR.(<P>FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR. AREA ON LH WISDR UIEA2024072400740Position Unit · wornWORN ON FITTING OF TRUCK POSITIONER, LEFT MAIN LANDING GEAR(<P>LH MLG SUPORT OF TRUCK POSITIONER WAS REPLACED IAW AMM 32-32-18-404-027 REV. 142 DATE 22 APR 24. TORQUE TO BOLTS WAS APPLIED 650 LB-IN AND 200 LB-IN WITH TOOL N/S 0823114442 DATE: 15-NOV-24. GOOD FSDR UIEA2024072400741Fuel Tank · leakingRH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK(<P>RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK. THE FUEL LEAK WAS EVALUATED, SEALANT REMOVED AND REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE TEST WAS SATISFACTORY.</P>)SDR UIEA2024072400742Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN BETWEEN FSS 183.3 AND FSS 230.91.(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, PANEL SKIN BETWEEN FSS 183.3 AND AND FSS 230.91 WAS REPAIRED IAW TRE 6755078 REV 1 ISSUE DATE 18 JUL 2024, FSDR UIEA2024072500746Hydraulic Line · chafedCHAFING IN HYDRAULICS LINES RH LANDING GEAR, IN THE MIDDLE OF THE BACK(<P>RH LANDING GEAR, IN THE MIDDLE OF THE BACK. HYDRAULICS LINES WAS REPLACED IAW AMM 20-11-00-910-801 REV. 142 DATE 22 APR 24 AND AMM 20-11-00-910-802 REV. 142 DATE 22 APR 24. TORQUE APPLIESDR UIEA2024072500747Indicator · malfunctionedLH WING, INNER ACCESS PANEL 521QB, RH FUEL QUANTITY INDICATION IN 888.8(<P>RH FUEL QUANTITY INDICATOR WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FUELING QUANTITY INDICATION WAS SATISFACTORY. GOOD FOR SERVICE.</P>)SDR UIEA2024072500748Indicator · malfunctionedLH WING, INNER ACCESS PANEL 521QB, CENTER FUEL QUANTITY INDICATION, FLASHING INDICATION(<P>CENTER FUEL QUANTITY INDICATION WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FOR PRESSURE FUELING SYSTEM QUANTITY INDICATION WAS SATISSDR UIEA2024072500749Valve · failedFWD TRIM VALVE FAIL.(<P>FWD TRIM VALVE WAS REPLACED IAW AMM 21-61-07-404-011-003 REV. 142 DATE 22 APR 24. TORQUE APPLIED 45 LB-IN S/N 0823900243 DATE 15 NOV 24. BONDING TEST WAS SATISFACTORY 2.2 MILLIOMHMS S/N DC- 005040 DATE 12 DEC 24. OPERATIONAL TEST WAS SASDR UIEA2024072500750Relay · faultedAUTO SPEEDBRAKE DEPLOY INOPERATIVE WHEN T/R PULLED(<P>SYSTEM AUTO SPEED BRAKE. ACTUATOR WAS REPLACED IAW AMM 27-62-04-422-023 REV- 142 DATE 22 APR 24. TORQUE APPLIED 80 LB-IN S/N 12995 DATE 11 JUN 25. GEAR TILT PRESSURE SWITCHES LH AND RH WERE REPLACED IAW AMMSDR UIEA2024071100642Light · inoperativeEMERGENCY LIGHT OVER SEAT 5CA INOP(<P>R/R EMERGENCY LIGHT OVER 5 CA PER AMM 33-50-00. OPS CHK GOOD.</P>)SDR UIEA2024061200514Lamp · inoperativeEMERGENCY LIGHTS "UNARMED" LIGHT HALF BURNT OUT(<P>RELAMPED EMERGENCY LIGHTS "UNARMED" LIGHT IAW AMM 33-11-00. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024060600497Pbe · damagedLT AFT PBE DAMAGED. ( PBE SMOKE HOODS )(<P>PLACED AFT LEFT BULKHEAD PBE TO DMI 209909 PER MEL 35-20-01 CAT D EXP 20SEP24. PBE PLACED IN MX CLOSET. REMOVED AND REPLACED PBE AT AFT LH FA STATION PER AMM 25-64-02. OPS CHECKS GOOD. THIS CLEARS MDDR 209909</P>)SDR UIEA2024032300206Skin · dentedRIGHT WING INBOARD AFT FLAP UPPER SKIN WITH TWO DENTS(<P>UPPER SKIN WAS REPAIRED SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032300205Lamp · inoperativeTHE LEFT SIDE EXTERIOR EMERGENCY LIGHT ( L645 ) INOP(<P>SLIDE LIGHT LAMP (L645) WAS REPLACED IAW AMM 33-51-06-902-082 REV 141. OPS CHECK GOOD</P>)SDR UIEA2024032300204Light · inoperativeTHE RIGHT SIDE EXTERIOR EMERGENCY LIGHTS ( L391 AND L644 ) INOP(<P> SLIDE LIGHT LAMP (L391) WAS REPLACED IAW AMM 33-51-06-902-082 REV 141 DATED 22DEC23. OPS CHECK GOOD</P>)SDR UIEA2024032300203Light · inoperativeTHE FLIGHT DECK EMERGENCY EXIT LIGHT ( L286 ) INOP(<P>PART WAS REPLACED IAW AMM 33-51-06. OPS CHECK GOOD</P>)SDR UIEA2024022100098Tape · brokenTAPE ON ELT BROKEN/TORN(<P>TRANSFERRED TO MDDR # 203295 PER MEL 25-63-10-01, CAT D. DUE DATE 19JUN24. PLACARDS INSTALLED.</P> / <P>PART ON HAND NOT CORRECT, TAPE REQUIRED PART OF ELT ASSY. MCC NOTIFIED. NEW ELT ON ORDER. DMI #203295 REMAINS OPEN.</P> / <P>RSDR UIEA2024020500069Pressure Switch · faultedENG FUEL FILTER PRESSURE LIGHT CAME ON IN FLIGHT(<P>REMOVED AND REPLACE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER FIM 73-34-01 AND AMM 73-34-01 LEAK AND OPS CK C/W</P>)SDR UIEA2024013100056Fmc · faultedWHILE TAXIING ON GROUND IN MHT, A TURN SHOWED 26 KTS, WHICH I BELIEVE TO BE INCORRECT ON GROUND IN MHT. DURING CRUISE, ATC ADVISED WE WERE OFF COURSE AND LNAV SHOWED ON COURSE TO JWH, FIX WERE GIVEN A HEADING TO FLY. RECEIVED AN IRS NAV ONLY FLAG ON SCRATCH PASDR UIEA2023121901006Battery · unknownLH AND RH OVERWING EMERGENCY EXIT SIGNS INOP(<P>REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY M1209 PER AMM 33-51-07. OPS CHECKS GOOD</P>)SDR UIEA2023121801000Life Vest · missingMISSING 3 SPARE LIFE VEST MISSING ( NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) (120 DAYS) (NEF-CABIN GENERAL 5) )(<P>INSTALLED 3 MISSING SPARE LIFE VESTS ON AIRCRAFT IAW LOPA DWG 6725A197-EEL. DMI 199117 CLOSED. PLACARD REMOVED AND MCC NOTIFIED.</P>)SDR UIEA2023102500931Filter · unknown"L ENG FUEL FILT" EICAS MSG COMPLIED WITH QRH. EICAS MESSAGE WENT OUT AND STATUS MSG REMOVED(<P>R/R LH ENG MAIN FUEL FILTER IAW AMM 73-11-02. NO LEAKS NOTED. OK FOR SEVICE.</P>)SDR UIEA2023100300862Trim Switch · unknownUPON ROLL AT THRUST SET TO MASTER WARNING/CAUTION SIREN, EICAS MSG CONFIG / STABLIZER LOW SPEED REJECT(<P>T./S PER FIM TASK 31-51 FAULT TREE 807. R/R CONTORL "STAB TRIM POSITION SWITCH ASSY" IAW AMM 27-48-01.OPS CK GOOD NO MSG. </P>)SDR UIEA2024031500152Altimeter · failedCAPT ALTIMETER FAILED AND DISPLAYED OFF FLAG AT CRUISE. ACCOMPLISED QRH. NO CHANGE(<P>CAPTAIN ALTIMETER REMOVED AND REPLACED PER AMM 34-13-01/404. PERFOMRED OPS CHECK TO THE SYSTEM, ALL OPS CHECKED NORMAL. PITOT STATIC LEAK TEST PERFORMED, NO DEFECTS NOTED.</PSDR UIEA2023091400830Fitting · unknown#1 PYLON FAN COWL SUPPORT BEAM FITTING CRACKED.(<P>R/R #1 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO 4842022 AS PER B767 SRM 51-40-02 & DWG 311T2110. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023091400831Fitting · unknown#2Â PYLON FAN COWL SUPPORT FITTING CRACKED(<P>R/R #2 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO #4743771 AS PER BOEING DWG #311T2110 AND B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023091400832Angle · unknown#1 PYLON FAN COWL SUPPORT BEAM ANGLE P/N: 311U2510-113 IS CRACKED(<P>R/R CRACKED ANGLE R/N 311U2510-113. FABRICATED NEW ANGLE AND INSTALLED AS PER BOEING 767 SRM 51-40-02 AND DRAWING #311U2510 REV AL.</P>)SDR UIEA2023073100765Defibrillator · unknownEMERGENCY DEFIBRILLATOR IN FWD EMERGENCY EQUIPMENT CLOSET NEAR EXPIRATION DATE.(<P>REMOVED AND REPLACED DEFIBRILLATOR IN FWD EMERGENCY EQUIPMENT CLOSET REF AMM 25-64-03</P>)SDR UIEA2023062000654Medical Kit · unknownFIRST AID KIT ON OVHD BIN HAS SAFETY SEAL BROKEN(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-04-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060900623Unknown · unknownDENT ON ENG #1 PRIMARY EXHAUST OUTER SKIN AT NAC STA 341.67 BETWEEN 4/5 O'CLOCK(<P>DENT WAS EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW B767-300 SRM 54-42-30-1A-1 A.D. 1 FIG 101 SHEET 3 NOTE N DETAIL VIII REV 122 15 APR 23. DENT WAS ADDED ON DENT LOG DAMAGSDR UIEA2023060900624Unknown · unknownDURING ELECTRICAL POWER ON WITH EXTERNAL POWER AND SUPPLY THE UTILITY BUS FAIL(<P>FIM TASK 24-51 FAULT TREE 804 WAS PERFORMED AND TEST PASSED IAW AMM 24-51-05-864-014 REV 139 DATE 22-APR-2023. SATISFACTORY TEST</P>)SDR UIEA2023060900625Unknown · unknownDURING MEASURING OF THE ELECTRICAL BONDING RESISTANCE OF AC OVERRIDE PUMP LH, AC OVERRIDE PUMP RH AND APU DC FUEL PUMP ARE OUT OF LIMITS.(<P>MEASURE THE ELECTRICAL BONDING RESISTENCE OF AC OVERRIDE PUMP LH AND AC OVERRIDE PUMP RH AFTER IAW AMM 28-22-05-404-078SDR UIEA2023060900626Unknown · unknownCENTRAL FUEL TANK WITH FOAM DEFORMED.(<P>FOAM CENTRAL FUEL TANK CAVITIES 3, 4 AND 125 WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-3079, FF-00405-3078, FF-00405-4012.</P>)SDR UIEA2023060900627Unknown · unknownSEVERAL DENTS ON ENG. #2 PRIMARY EXHAUST OUTER SKIN BOTH SIDES(<P>DENT WAS EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW B767-300 SRM 54-42-30-1A-1 A.D. 1 FIG 101 SHEET 3 NOTE N DETAIL VIII REV 122 15 APR 23. DENT WAS ADDED ON DENT LOG DAMAGE CHART AS PER ATSDR UIEA2023060900628Bolt · unknownDURING MEASURING OF THE ELECTRICAL BONDING RESISTAMCE OF AC OVERRIDE PUMP LH, AC OVERRIDE PUMP RH AND APU DC FUEL PUMP ARE OUT OF LIMITS.(<P>BOLTS AND O-RINGS WERE REPLACED AND MEASURED THE ELECTRICAL BONDING RESISTENCE OF AC OVERRIDE PUMP LH AND AC OVERRIDE PSDR UIEA2023060900629Unknown · unknownWING CTR FUEL TANK WITH FOAM DEFORMED.(<P>WING CTR FUEL TANK WITH FOAM DEFORMED WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-6133, FF-00405-6032, FF00405-5132.</P>)SDR UIEA2023060900630Filter · unknownENG 1 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT.(<P>ENG 1 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT, FUEL FILTER ELEMENT WAS REPLACED IAW AMM 73-11-02-404-008-H00 REV 139 DATE 22 APR 23. NO LEAKS FOUND.</P>)SDR UIEA2023060900631Filter · unknownENG 2 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT.(<P>ENG 2 FUEL FILTER REPLACEMENT AFTER POST OPS RUNS DUE TO FOAM REPLACEMENT, FUEL FILTER WAS REPLACED IAW AMM 73-11-02-404-008-H00 REV139 DATE 22 APR 23. NO LEAKS WAS FOUND.</P>)SDR UIEA2023061000633Unknown · unknownCENTER SECTION TANK RH SIDE BETWEEN ROOT AND SPLICE STRINGER 6RH WITH FUEL LEAK(<P>CENTER TANK SEALANT WAS REPAIRED IAW AMM 28-11-00-308-013. OPS CHECK GOOD</P>)SDR UIEA2023021400116None · noneSEAT 12E HAS BURN HOLE FROM PASSENGER CELL PHONE.(<P>FOUND CONTAMINATED AREA TO BE LIMITED TO PASSENGER BAG AND CUSHION 12E. REMOVED SOILED ITEMS FROM A/C AND CLEANED AREA IAW AMM 05-51-15. NO FURTHER ACTION REQUIRED</P>)SDR UIEA2023011200017Panel · misinstalledEMERGENCY EGRESS WINDOW CAPT SIDE WILL NOT OPEN. REMOVED CAPTS WINDOW EMERGENCY EGRESS PANEL AND REINSTALLED / ADJUSTED PANEL IAW B767 AMM 20-11-00. NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2022122001212Light · inoperativeEMERGENCY LIGHT ON OUTSIDE RIGHT FUSELAGE OF WING INOP.(>RELAMPED LIGHT, OPS CHECK NORMAL I/A/W AMM 33-51-06)SDR UIEA2022120301204Fseu · faultedCLIMBING THROUGH 10,000FT FLAPS UP & IN VNAV, NOTICED THE AIRPLANE SPEED BUG WAS AT 250KTS & THAT THE OVERSPEED TAPE WAS DOWN TO 250KTS. GIVEN A CLIMB TO FL230, BUT ELECTED TO STAY BELOW FL200 AND LEVELED OFF AT FL190 250KTS OF NOTE AT APPROX 14000FT, SLOWED SDR UIEA2022122001213Light · inoperativeEMERGENCY LIGHT ON OUTSIDE LEFT FUSELAGE AFT OF WING INOP(RELAMPED LIGHT OPS CHECK NORMAL I/A/W AMM 33-51-06)
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