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 UIEA2024120301164Shutoff Valve · faultedLEFT TR INOP(<P>REMOVED DEFECTIVE REVERSER PRSOV REF 767-300 M/M 78-34-05-004-001-H00. OK TO INSTALL SERVICEABLE UNIT.</P> / <P>INSTALLED SERVICEABLE PRSOV REF 767-300 M/M 78-34-05-404-009-H00. INDICATOR AND OPERATION GOOD WITHOUT ENGINE OPERATING REF 767-300 SDR UIEA2024112801118Shutoff Valve · faultedDURING CRUISE, RECEIVED A MASTER WARNING "CABIN ALT". COMPLIED W/ QRH. FL380. CABIN ALT 11,000' DPSI 7.0. USED MANUAL PRESSURIZATION MODE TO CONTROL & STABILIZED CABIN ALT. "CABIN AUTO INOP" CAUTION MSG. COMPLIED W/ QRH PROC. "CABIN ALT AUTO 1" AND "CABISDR UIEA2024111501092Lamp · burned outEMERGENCY LIGHTS "UNARMED" DISCRETE LIGHT HAS BURNED OUT LIGHT BULB(<P>RELAMPED EMERGENCY UNARMED LIGHT PER AMM 33-10-00. OPS CHECK NORMAL</P>)SDR UIEA2024101801052Screen · cloggedATB - FWD EQUIP OVHT EICAS MSG. WENT TO STBY IAW QRH, DID NOT CLEAR. WENT TO OVRD IAW QRH, EICAS MSG CLEARED. DID NOT ENTER ETOPS(<P>FOUND EQPT COOL SUPPLY AIR INLET GRILL DIRTY AND PARTIALLY BLOCKED. CLEANED PER AMM 21-58-10. FOUND SUPPLY FAN SCREEN EQUIPMENTSDR UIEA2024101501005Attach Fitting · corrodedLH UPPER HORIZONTAL STABILIZER PIVOT FITTING ATTACHMENT WITH CORROSION(<P><SPAN DATA-OLK-COPY-SOURCE="MESSAGEBODY">REMOVE FASTENERS FROM ALTERNATE ROWS, REAM THE AFFECTED HOLES THRU THE ENTIRE STACK-UP IN 1/64 INCH INCREMENTS UNTIL FASTENER HOLE IS CLEAN, ROUNSDR UIEA2024101501008Fuse Pin · crackedSUPPORT #6 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101501010Fuse Pin · crackedSUPPORT #3 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101501011Panel · damagedEVALUATE AND REPAIR AS REQUIRED, INDUCED DAMAGE TO RH HORIZONTAL STABILIZER T/E PANEL(<P>RH HORIZONTAL STABILIZER T/E PANEL WAS REPAIRED IAW SRM 55-10-01-2R-1 FIG 201 SHEET 4 PAGE 1-5 AND SRM 51-70-07- 0G-0 PAR 5.D FIG 11 PAG 16,37 REV 126 15/AUG/24</P>)SDR UIEA2024101501012Pivot Assy · corrodedHORIZONTAL STABILIZER - PIVOT FITTING - UPPER ATTACHMENT - MOST OUTBOARD REAR BOLT HOLE WITH INDICATION OF CORROSION(<P>TRE6755057 WAS PERFORMED AND NIL DAMAGE FOUND, TRE6755057 WAS BASED ON OEM MESSAGES CMA-PAO-24-0103</P>)SDR UIEA2024101501014Support Fitting · wornFLAP SUPPORT #1 FITTING OUTBOARD ACTUATOR SPAR FITTING WEAR FOUND 3 HOLES WITH CORROSION INDICATION (LOCATED 12:00, 08:00 AND 10:00 O´CLOCK)(<P>CORROSION WAS REMOVED, REAMING THE AFFECTED HOLES AND FREEZE PLUGS WERE INSTALLED. THIS REPAIR WAS BASED ON CMA-PASDR UIEA2024101501017Pin · corrodedLEFT 6-6 PIN FLAP SUPPORT #4 WITH CORROSION(<P>PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-04-402-135. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101701042Transmitter · failedLEFT WING TRANSMITTER FLAP POSITION #1 WITH FAIL(<P>LEFT WING TRANSMITTER FLAP POSITION #1 WAS REPLACED AND TESTED IAW AMM TASK 27-51-45-422-030 REV 143 DATE 22 AUG 24, TEST OK, 50 IN LB WERE APPLIED. S/N 0818911494 DUE DATE 04 APR 25</P>)SDR UIEA2024101701050Packing · leakingFUEL LEAK IN MAIN FUEL BOOST PUMP WING RH(<P>THE PACKING AT THE MAIN FUEL BOOST PUMP WING RH WAS REPLACED. NO LEAKS WERE FOUND IAW AMM 24-22-03-004-001 AND 28-22-03-404-027 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 55 LB-IN AND 35 LB-IN. S/N: 0821902601 DATE: SDR UIEA2024101701051Union · leakingFUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH(<P>FUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH WAS R/R & NO LEAKS WERE FOUND IN IAW AMM 28-41-09-004-001-002 AND 28-41-09-404-028-002 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 240 LB-IN S/N:SDR UIEA2024092400931Pdu · leakingRIGHT WING, SLAT PDU INBOARD, WITH EVIDENCE OF HYD LEAK(<P>RIGHT WING, SLAT PDU INBOARD WERE REPLACED IAW AMM 27-81-10-424-023 AND AMM 27-81-10-024-001, LEAK CHECK WERE PERFORMED, NO LEAK WAS FOUND.</P>)SDR UIEA2024092400932Skin · detachedRH WING, SLAT #7, SURFACE INNER SIDE, UPPER AND LOWER AREA WITH SEVERAL POINTS OF DETACHED.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27- 81-01-424-143. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400933Skin · corrodedRH WING, SLAT #7, SURFACE INNER SIDE, AREA UPPER MIDDLE, WITH TWO POINTS OF CORROSION EVIDENCE.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27-81- 01-424-143. OPS CHECK GOOD</P>)SDR UIEA2024092400934Pca · leakingLEFT WING, OUTER AILERON, INNER PCA, WITH EVIDENCE OF HYD LEAKAGE(<P>LEFT WING, OUTER AILERON, INNER PCA, WAS REPLACED, ADJUSTED AND LEAK TEST WAS PERFORMED IAW AMM 27-11- 49-422-028 AND AMM 27-11-49-022-014. NO LEAKS WERE FOUND.</P>)SDR UIEA2024092400935Skin · detachedLEFT WING, LEFT INBOARD AILERON, LEADING EDGE MIDDLE AREA DETACHED.(<P>LEFT WING, INBOARD AILERON, LEADING EDGE MIDDLE AREA WAS REPAIRED IAW SRM 57-60-01-2R-1 FIG 201 SHEET 9 PAG 1-10 AND SRM 51-70-17-0G-0 PAR 4G FIG 15</P>)SDR UIEA2024092400936Fuel Cell · leakingRH WING, FUEL LEAK ON LOWER SKIN AND SPLICE BTW WBL 97.95. TO WS 226.3 AND BTW STGR L7 TO L15(<P>FUEL LEAK WAS REPAIRED AND LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)SDR UIEA2024092400937Fire Bottle · expiredENG 2 BOTTLE EXTINGUISHER #2 DATE OFF(<P>ENG 2 BOTTLE EXTINGUISHER #2 WAS REPLACED AND TEST WAS SATISFACTORY IAW AMM 26-21-03-424-095</P>)SDR UIEA2024092400938Skin · crackedDOUBLER INSTALLED ON EMERGENCY LIGHT OF THE MCD SURROUND SKIN CIRCUMFERENTIAL SPLICE STA 654+22 AT AFT FASTENER ROW IN THE SECOND LOWER FASTENER HOLE WITH CRACK INDICATION.(<P>THE SECOND LOWER FASTENER HOLE WAS ENLARGE UP TO SECOND OVERSIZE AND WAS REPAIRED IASDR UIEA2024092400939Skin · crackedAT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER ONE HOLE WITH CRACK INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK.(<P>HOLE INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK. CRACK WAS REPAIREDSDR UIEA2024092400940Skin · crackedAT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER TWO HOLES WITH CRACK INDICATION ON FUSELAGE SKIN APPROX 10 O´CLOCK.(<P>AT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER ON FUSELAGE SKIN APPROX 10 O´CLOCK DAMAGES WERE REPAIRED IAW FVCI #24153-2 A FAA FORM 8110-3 (09/20SDR UIEA2024092400941Skin · wornLH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN WITH WEAR.(<P>LH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN DAMAGE WAS REPAIRED IAW FVCI #24153-3 AN APPROVAL FORM FAA 8110-3 WAS ISSUED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400942Seal · wornLEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WITH WORN SEAL(<P>THE WORN SEAL ON LEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WAS REPLACED IAW AMM 33-44-01-002-017. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092400943Frame · corrodedFWD CARGO COMPARTMENT, EVIDENCE OF CORROSION ON WEB FRAME AT BS 764 BTW S37L AND S38L.(<P>WEB FRAME AT BS 764 BTW S37L AND S38L. PAINT WAS REMOVED, REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND. ALLODINE, PRIMER AND PAINT WAS RESTORED IAW SRM 53-00-07-1A-1. NSDR UIEA2024092400944Jumper · brokenRH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BROKEN BONDING JUMPER (2E/A'S) BTW RIB 6/7.(<P>THE BROKEN BONDING JUMPER (2E/A'S) ON RH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BTW RIB 6/7 WERE REPLACED IAW SWPM 20-20-10 REV</P>)SDR UIEA2024092400945Sealant · missingRH WING, INSIDE FUEL TANK REAR SPAR, MISSING FILLET SEALANT ON SHUT OFF VALVE (2 E/A'S) BTW RIB 1/6.(<P>RH WING, INSIDE FUEL TANK REAR SPAR, FILLET SEALANT ON SHUT OFF VALVE WAS APPLIED IAW AMM TASK 28-21-02-404-021. NO FURTHER DEFECT NOTED</P>)SDR UIEA2024092400946Actuator · leakingLH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA WITH HYDRAULIC LEAK.(<P>LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA LEAK CHECK WAS PERFORMED, NO LEAKS WERE FOUND</P>)SDR UIEA2024092500948Access Panel · puncturedSYS LH HYD BAY, (ACCESS PANEL 437BL), SURFACE INERSIDE AREA LOWER RIGH TSIDE, ANGLE WITH PUNCTURE.(<P>SURFACE INERSIDE AREA LOWER RIGHTSIDE, ANGLE WAS REPAIRED IAW TRE 6754195 ISSUED DATE 13/SEP/24 & CMA-TLS-24-0190, RDR WAS ISSUED. NO FURTHER DEFECTS NOTED</PSDR UIEA2024092500949Access Panel · wornSYST LH HYD BAY, (ACCESS PANEL: 437BL) INNER RIGHTSIDE, LOWER REAR CORNER AREA, PLATE-STRICKER WITH WORN.(<P>LOWER REAR CORNER AREA, PLATE ASSY WAS REPLACED SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500950Fire Seal · detachedENGINE ONE NACELLE STRUT FIRE SEAL DETACHED ON FWD CORNER LH AND RH SIDE(<P>ENGINE ONE NACELLE STRUT FWD CORNER LH AND RH SIDE; SEAL WAS REPAIRED IAW AMM 54-54-03-308-014. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500951Fill Port · corrodedRH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(<P>OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND IAW SRM 57-20-01-1A-1</P>)SDR UIEA2024092500952Bracket · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, AFT STA 1540, BTW S-38R, AND S-39R, BRACKET WITH EVIDENCE OF CORROSION.(<P>BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500953Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WAS REPAIRED IAW SRM 53-00-03-2R-2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500954Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WAS REPAIRED IAW SRM 53-00-03-2R-2</P>)SDR UIEA2024092500955Fire Seal · brokenENG 2, RIGHT T/R DOOR, UPPER AFTER SECTION, FIRE SEAL BROKEN(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500956Seal · damagedENG 2, RIGHT T/R DOOR, UPPER SECTION, FIRE SEAL, RESTORE SEALANT (THE ENTIRE PERIPHERY)(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500957Fire Seal · damagedENG 2, LEFT T/R DOOR, UPPER SECTION, FIRE SEAL, RESTORE SEALANT (THE ENTIRE PERIPHERY)(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024092500958Display · inoperativeFLIGHT MANAGEMENT COMPUTER SYSTEM, ASSY-FLIGHT PANEL P9, MCDU RIGHT SIDE INOPERATIVE(<P>MCDU RIGHT WAS REPLACED IAW AMM 34-61-02-400-802. OPS CHECK GOOD</P>)SDR UIEA2024092700960Fuel Cell · leakingRH WING, LOWER SKIN BETWEEN WBL 97.95 TO WS 226.3 AND STGR 10 WITH EVIDENCE OF FUEL LEAK(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD</P>)SDR UIEA2025081501124Warning Light · false activationMAIN CARGO DOOR DISCRETE LIGHT ON AFTER 2ND ENGINE START(<P>MDC CHECKED IAW AMM 52-31-00. OPENED & INSPECTION CHECKED GOOD. THIS CLOSES MDDR 236249 </P>)SDR UIEA2025081501125Starter · failedJUST BEFORE ENGINE START, A VERY STRONG ELECTRICAL SMELL OVERWHELMED THE FLIGHT DECK. SMELL GOES AWAY AFTER PACKS ARE SHUT OFF(<P>APU STARTER WAS BURNT AND WAS DETERMINED TO BE THE CAUSE OF THE SMOKE SMELL. R/R APU STARTER PER AMM 49-41-01. OPS CHK OK. NO DEFESDR UIEA2024080500789Rvdt · out of rigCLIMBING OUT OF RFD, WE WENT FLAPS UP AND THEN GOT LE SLAT DISAGREE MSG. PERFORMED FSEU BITE CHECK IAW FIM 27-51 FT 809. FOUND FAULT CODE 27-S1040 FOR LVR 1 NOT IN DETENT, CHECKED RIGGING OF FLAP LEVER RVDT IAW AMM 27-51-26. FOUND RVDT 1 OUT OF LIMITS IN UP PSDR UIEA2024072400743Escape Reel · unwanted deploy1 EA ESCAPE INERTIAL REEL DEVICE FULL OUT(<P>TRANSFER TO DMI 213408 PER MEL 25-61-01-01 CAT C DUE DATE 4AUG2024. PN 379103D-29</P> / <P>LP 1239968 ITEM 5 / ONT / 27JUL24: INSTALLED 1 EA INERTIA REEL IAW B767 AMM 25-61-01. NO FUTHER DEFECTS NOTED. THIS CLEARS MSDR UIEA2024062700570Harness · malfunctionedTHREE ESCAPE HARNESSES INOP. INSTALLED SAFETY HARNESS IAW AMM 25-61-05. MCC NOTIFIED, PLACARDS REMOVED. THIS CLOSES DMI #211594.</P>)SDR UIEA2024062200564Elevator System · noneCAN'T GET FULL TRAVEL WITH FWD ELEVATOR(<P>PERFORMED OPS CHECK OF ELEVATOR POSITION INDICATION SYSTEM IAW AMM 27-38-00. VERIFIED ALL INDICATIONS WITHIN LIMITS. AC OKAY FOR SERVICE.</P>)SDR UIEA2024060700500Control Panel · faultedFO SIDA UNABLE TO TURN VOR EMERGENCYIN MANUAL MODE(<P>REMOVED AND REPLACED VOR CONTROL PANEL IAW AMM 34-51-02. NO DEFECTS NOTED AT THIS TIME. VERIFIED PART EFFECTIVITY IAW IPC 31-11-11-17</P>)SDR UIEA2024060500494Stowage Box · unknown/FO OXYGEN STOWAGE BOX REQ REPLACEMENT(<P>R/R F/O'S OXYGEN STOWAGE BOX REF 35-11-51 LEAK CHECK GOOD OPS CHECK GOOD. PART EFFECTIVITY VERIFIED IAW AIPC 35-11-52-15</P>)
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