Boeing 767-3S2F
Service difficulty reports · 2,378
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 = '7673S2F' 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 = '7673S2F' 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 FDEA2020020420257Skin · bent#10 SLAT EXTERIOR UPPER SURFACE INBD AFT END IS BENT UP. REPAIRED #10 SLAT UPPER I/B SURFACE IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.SDR FDEA202001310251Bracket · crackedLEFT NACELLE RIB AFT OF PANEL 437BL LH BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02, AND DWG 313T3380, REV N.SDR FDEA202001310250Attach Angle · crackedNR 2 ENGINE PYLON AFT END INBD ATTACH ANGLE AT THE AFT FRAME WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02 AND DWG 313T3380, REV N.SDR FDEA2020013090234Sensor · out of toleranceON CLIMBOUT PASSING 280, "MAIN CARGO DOOR" LIGHT ILLUMINATED. FOLLOWED CHECKLIST, RTB. PASSING APPROX 4,000 FT LIGHT EXTINGUISHED. NO OTHER INDICATIONS WERE PRESENT. T/S PER FIM 52-71 FT 809. FOUND S891 DOOR LATCHED SENSOR READING 6.7. OTHER SENSOR CK OK.SDR FDEA2020012750227Brake · damagedON LANDING AND TAXI IN, WHEN LEFT BRAKE IS APPLIED THERE IS A LOUD NOISE AND A VIBRATION. BRAKES WERE STILL WORKING REMOVED ALL FOUR TIRES FROM LEFT GEAR IAW 32-45-01-4. INSPECTED LEFT GEAR WHEELS IAW 32-45-03-2, INSPECTED LEFT GEAR BRAKES IAW 32-41SDR FDEA202001210181Warning Light · false activationMAIN CARGO DOOR LIGHT ILLUMINATED ON THE EICAS, APPROACHING 370, LIGHT WENT OUT 20-40 MINUTES LATER.SDR FDEA2020012190167Unknown · noiseAIR TURN BACK. DURING CLIMB ( 14000-16000) A LOUD BANGING SOUND STARTED. WE WERE AT ( 280-290 KTS). SLOWED SOUND STOPPED. AROUND 250 KTS FO'S WINDSHIELD WIPER WAS VIBRATING OPERATED WINDSHIELD WIPERS IAW AMM 30-42-00-5. WINDSHIELD WIPERS OPERATED NORMASDR FDEA202001100096Unknown · odorENGINE EXAUST (BURNING OIL) SMELL AT 10000 FT DECENDING AND SLOWING FROM 290 IAS TO 230 KNOT IAS. CABIN ALT 1000', CABIN DIF 4.0. SMELL WENT AWAY AT 7,000 FT, 230 KIAS, 500 CABIN ALT, DIF 3.0. SMELL CAME BACK ON THE TAXI TO THE GATE WHEN RIGHT ENGINE SHUT DSDR FDEA202001050021Skin · dentedMAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,SDR FDEA2020010650021Skin · dentedMAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,SDR FDEA201912240001Skin · damagedFUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1.SDR FDEA2019122313277Ecu · malfunctionedCRUISE FL370 SCANNING OVERHEAD PRIOR TO DESCENT. OBSERVED RT EEC ALTN IN MODE SWITCH. NO ACCOMPANY EICAS. REFERENCED QRH, DECIDED TO PUT BOTH EEC IN SAME MODE "ALTN". ACCOMPLISHED QRH. UPON PUSHING THROTTLES UP N1 AND EGT BEGAN FLUXING. FF AT IDLE WOULD NSDR FDEA201912053180Autopilot Sys · failedAUTOPILOT ON APPROACHING 2600' IN FLCH AT APPROXIMATELY 210 KIAS AIRCRAFT ABRUPTLY PITCHED NOSE DOWN MISSING ALT CAPTURE BY ROUGHLY 200' REQUIRING A/P DISENGAGEMENT TO CORRECT AIRCRAFT. A/P CENTER WAS IN USE. NO PREVIOUS HISTORY. PERFORMED CFDS CURRENT FASDR FDEA2019120653180Autopilot Sys · malfunctionedAUTOPILOT ON APPROACHING 2600' IN FLCH AT APPROXIMATELY 210 KIAS AIRCRAFT ABRUPTLY PITCHED NOSE DOWN MISSING ALT CAPTURE BY ROUGHLY 200' REQUIRING A/P DISENGAGEMENT TO CORRECT AIRCRAFT. A/P CENTER WAS IN USE.SDR FDEA201911243085Skin · dentedINCOMING ITEM : LOWER LH FUSELAGE AT STA 1225, BETWEENSTRINGERS 32L-33L HAS A DENT COMPLIED WITH EA H-5310-T0350997 A. TITLED "FUSELAGE-MAINFRAME-FUSELAGE SKIN, STA 1225 BETWEEN S32L-33L, DENT". REMOVED AND REINSTALLED PIT SIDEWALL PANEL IAW B767 AMM 25-SDR FDEA2019112203017Warning Message · false activationPDIS 107 27-50 5327 20NOV19 CRK FACT U LOGPAGES:3138465 AFTER SELECTING FLAPS 30 TE FLAP ASSYM ON EICAS, COMPLIED WITH QRH. FACT 20NOV19 23:26 CRK U FOLLOW FIM 27-51-00-815-811, FSEU BITE PERFORMED FOUND FAULT CODE " LE DISAG" , MSG NO. 2SDR FDEA2019111522939Brake · damagedPDIS 125 32-43 4006 12NOV19 CDG OPEN U LOGPAGES:2841209 ON LANDING ROLLOUT APPLIED BRAKES MANUALLY FELT VIBRATION. ON SHUTDOWN BRAKE TEMP LIGHT IS ON BRAKE TEMPS 4435 WITH LIGHT BRAKING SHGN 12NOV19 20:11 CDG U UPON CAPTAIN'S FEEDBACK DECSDR FDEA201911082913Gcu · failedAFTER BLOCK IN AND POWER TRANSFER TO GPU NOTICED BURNING ELECTRICAL SMELL. EICAS MESSAGE "L BUS ISOLATED". CIRCUIT BREAKER "BAT 1 R SIDE PNL" IS OUT. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT IAW AMM 24-22-02-4. OPS CHECK GOOD. REF WRI 24-00/04SDR FDEA201911012813Fseu · malfunctionedLE SLAT DISAGREE ON FINAL. AFTER GO AROUND AND QRH, EICAS WENT AWAY FOR NORMAL CONFIGURATION AT LANDING. NO STATUS MESSAGE. FSEU SHOWED INTERMITTENT FAULTS WITH DIFFERENT CODES. R & R THE FSEU IAW AMM 27-51-01-4 & BITE CHECKED IAW FIM 27-51, FAULT TREE SDR FDEA201910312799Screw · unsecureUPON RETRACTING FLAPS AND SLATS CLIMBING OUT AFTER TO MOVING FLP/SLT LEVER HANDLE FROM 1 TO 0 LE SLAT ASYM EICA LT ILLUMINATED WIH CORRESPONDING WING ROLL TO THE LEFT FOLLOWED QRH AND RETURNED TO FOR LANDING MSP. FOUND R/H PDU OUTBOARD TORQUE TUBE COUSDR FDEA201910172682Skin · dentedLEFT WING O/B FLAP LOWER SKIN HAS NUMEROUS DENTS. REPAIRED LEFT WING O/B FLAP LOWER SKIN DENTS IAW B767 SRM: 57-53-01-01A, 51-70-00-2R, 51-70-07-2R-G, 51-70-07-0G, AMM: 51-61-00-0, 51-21-10-307-020, 51-21-10-07; H-2750-T0350063- P1 FLIGHT CONTROL-T/E FLAPSDR FDEA201910142641Sleeve · corrodedNR 2 ENGINE, OUTBOARD THRUST REVERSER OUTER SHELL, INNER SURFACE, LOWER AREA CORRODED. REMOVED AND REPLACED THE NR 2 ENGINE OUTBOARD THRUST REVERSER SLEEVE IAW AMM 78-31-15-4 AND AMM 78-31-104, ADJUSTMENT AND OPS CHECK OF THE #2 OTBD THRUST REVERSER SLEEVE CHSDR FDEA201910012396Control Panel · burnedELECTRICAL FIRE IN LOWER LEFT SIDE OF OVERHEAD LIGHTS CONTROL PANEL CREW SAW AN ELECTRICAL FIRE ON OVERHEAD PANEL. SMOKE AND BURNING ODOR DETECTED. TROUBLESHOOT AND FOUND THE PANEL/FLOOD SWITCH S1 WIRES BURNED. REMOVED AND REPLACED THE LIGHT SWITCH IAWSDR FDEA201909262351Tire · wornDURING TAKEOFF ROLL, WE EXPERIENCED EXCESSIVE VIBRATIONS FROM THE GEAR ONCE AIRBORNE. VERBALLY SPOKE WITH CREW.. THE AIRPLANE EXPERIANCED A SMALL AMOUNT OF VIBRATION ON TAKE OFF ROLL AND AN EXCESSIVE AMOUNT ONCE THE ACFT BECAME AIRBORNE. IT WAS STATED TSDR FDEA201909192287Wedge · chafedLEFT WING #5 SLAT T/E WEDGE LOWER SURFACE CHAFED. REPAIRED THE T/E OF THE #5 SLAT IAW 57-43-02-2R, 51-70-10 AND EA H-2780-T0349554-P1 FLIGHT CONTROL- L/E SLATS AND FLAPS--#5 SLAT, RSC SRM REPAIR TRACKING.SDR FDEA201909172272Skin · dentedRIGHT WING I/B MAIN FLAP LOWER SURFACE HAS A DENT. REPAIRED RW I/B MAIN FLAP LOWER SURFACE IAW SRM 57-53-01-1A AND 51-70-10-1R AND EA H- 2750-T0349512 FLIGHT CONTROL T0349512 FLIGHT CONTROL-T/E FLAPS - RT INBD MAIN FLAP, LOWER SKIN, DENT, RSC SRM REPAIR TRACKSDR FDEA201909132268Pump · leakingAPPROX 2HRS INTO FLT, EICAS ALERT 'L HYD QTY', LT HYD QTY SLOWLY DECREASED FROM ABOVE 0.9 TO 0.01 WITH 'RF' INDICATED. EICAS ALERT 'HYD PRIM PUMP' DISPLAYED SHORTLY THEREAFTER QRH COMPLIED WITH AND LT ENG PRIMARY PUMP SELECTED 'OFF'. LT HYD PRESS STAYED IN NOSDR FDEA201909112212Pressure Switch · failedUNSCHD STAB TRIM FOR APPROXIMATELY 2 SECONDS ON EICAS, PASSING 8000 FT DURING DESCENT SPEED 210 KTS FLAP 1. REPLD C HYD PRESS SWITCH S29. PRESSURE SWITCH LEAK CKS GOOD. PERFORMED OPS CK OF ADP REF AMM 29-11-03-4-0. T/S UNSCHED STAB TRIM REF FIM 27-09 FAULT TRESDR FDEA201909052109Warning System · false activationINFO ONLY: EXPERIENCED SLAT DISAGREE DURING APPROACH FROM FLAPS 20 TO 25. WENT AROUND DISAGREE DISAPPEARED WHEN FLAPS TRANSITED TO 20. INFO NOTED. CHECKED FSEU FOR FAULTS, NONE FOUND. PERFORMED OPS CHECK OF FLAPS AND SLATS, OPS CHECK GOOD REF AMM 27-51-00-5.SDR FDEA2019080871812Wedge · gougedLEFT WING #5 SLAT TRAILING EDGE WEDGE GOUGED REPAIRED DAMAGED IAW EA# H-2780-T0348663 - P1 FLIGHT CONTROL- L/E SLATS-#5 SLAT, TRAILING EDGE SKIN- GOUGE GOUGE-RSC SRM REPAIR TRACKINGSDR FDEA2019080871811Wedge · chafedRIGHT WING #8 SLAT TRAILING EDGE WEDGE CHAFFED REPAIRED DAMAGE IAW EA# H-2780-T0348645 FLIGHT CONTROLS - L/E SLATS & FLAPS - NO. 8 SLAT, RSC SRM REPAIR TRACKING.SDR FDEA201907181629Latch · wornPDIS 101 25-60 6211 18JUL19 ICN OPEN U LOGPAGES:3139917 F/O EMER ESCAPE ROPE DOORS KEEPS DROPPING OPEN AND WOULD NOT REMAINED CLOSED. ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 25-10-26 FO ESCAPE ROPE STOWAGE COVER DOOR INOP.SDR FDEA201907171624Transceiver · malfunctionedON ARRIVAL, COM L AND COM R BOTH HAD A INTERMITTANT SOUND IN HEADSETS. SPEAKERS WERE ON, TURNED OFF, NO CHANGE. TRIED L & R INDEPEDANTLY- NO COM. SWITHCED TO CENTER TO REGAIN ATC/FLT COMS. R COM WORKED AFTER LANDING. T/S FOUND L VHF T/R INOP AND NOT TESTINGSDR FDEA201907151548Seal · defectiveUPON CLIMBING THROUGH FL 250 A LOUD SQUEEL STARTED AND CONTINUED THROUGH FL 370. PRESSURIZATION SEEMED NORMAL: DIFF 7.9, CABIN ALT 5900! NOT SURE WHICH SEAL ON WHICH WAS BAD. TOO LOUD TO CONTINUE FLIGHT. UPON DISCENDING THROUGH FL 250 SQUEEL STOPPED. CONTINUESDR FDEA201907111533Fairing · chafedLEFT WING OUTBOARD FLAP INBOARD LEADING EDGE CHAFFED. ACCOMPLISHED REPAIR IAW EA H-5750-TO348082.SDR FDEA201907051488O-Ring · rupturedGOT A "L HYD QTY" EICAS MESSAGE APROXIMATELY 2.5 HOURS INTO FLIGHT. L HYD QTY WAS .46 ON STATUS PAGE WITH RF MAGENTA. ALSO HAD "QTY" LIGHT ON OVERHEAD. HYD QTY .07 ON SHUTDOWN. FLIGHT CREW VERBALLY RELAYED TO ACMX THAT THE LEFT HYDRAULICS NEVER LOST PRESSURESDR FDEA201906291428Unknown · odorON DEPARTURE STRONG SMELL OF" DIRTY SOCKS" ON CLIMB OUT. POSSIBLE FUME EVENT. ACCOMPLISHED A VISUAL INSPECTION OF THE PACK COMPARTMENTS NO DEFECTS FOUND. ACCOMPLISHED VISUAL INSPECTION OF RIGHT AND LEFT HAND ENGINES FOR ANY EXTERNAL OIL LEAKS NON FOUND. STARTESDR FDEA2019062751408Escape Rope · unsecureDURING A PREFLIGHT INSPECTION, FOUND THE ENTRY DOOR EMERGENCY ESCAPE ROPE NOT STOWED. STOWED THE ESCAPE ROPE IAW AMM 25-10-00-2. ACFT OK FOR SERVICE.SDR FDEA201906211399Sensor · out of adjustPASSING FL336 RECEIVED EICAS MAIN CARGO DOOR- FOLLOWED QRH PRO. DECLARED EMERGENCY & RETURNED TO MEM. PASSING 10000 EICAS ALERT WENT OUT. FOUND S891 & S892 OUT OF ADJUSTMENT WITH NOT QUITE HALF OF THE SENSOR COVERED BY THE TARGETS. S891 WAS ALSO OUT OF GAP ADSDR FDEA2019062081354Module · malfunctionedDESCENDING FROM 4000'O 3000' AND ABOUT 3800' AGL THRUST AT IDLE FLAPS AT 1, 210KTS IN FLCH , MASTER WARNING SOUNDED WITH CONFIG LIGHT AND "GEAR NOT DOWN " EICAS MESSAGE. LASTED ABOUT 1 SECONDAND THEN CEASED. FACT 18JUN19 12:12 BOS U T/S SYSTEM IAW FIM SDR FDEA201906171323Slat System · malfunctionedWHEN FLAPS 25 SELECTED GOT A LE SLAT DISAGREE EICAS. DECLARED AN EMERGENCY RAN QRH CHECKLIST AND UNEVENTFUL LANDING WMKP 04, WE DID EXECUTE A MISSED APPROACH FSEU BITE CHK FOUND FAULT CODE 27-81045 LEG 0. NO EXISTING FAULT. CYCLED FLAP 3 TIMES, PERFORMSDR FDEA2019061741303Lamp · inoperativeLEFT MAIN GEAR LIGHT OUT AFTER SELECTING GEAR DOWN. PERFORMED LAMP CHECK LIGHT STILL OUT. REPLACED BOTH LEFT MAIN GEAR LIGHT. PERFORMED LAMP CHECK LIGHTS WORKED GOT 3 GREEN AFTER SELECTING GEAR DOWN. PER CREW DEBRIEF, VERIFIED LAMPS REMOVED BY THE SDR FDEA201906131288Skin · gougedR/W SLAT #12 INNER UPPER SURFACE HAS SEVERAL GOUGES REPAIRED #12 SLAT PER FEDEX EA H-2780-T0347440 P1SDR FDEA2019061321278Skin · dentedL/W O/B FLAP I/B LEADING EDGE DENTED 6" O/B FROM I/B EDGE. REPAIRED FLAP PER FEDEX EA H-2750-T0347475 P1SDR FDEA201906071255Skin · damagedLEFT WING, O/B FLAP, I/B LEADING EDGE PANEL IS DENTED 6" FROM I/B EDGE REPAIRED FLAP PER EA H-2750-T0347475 P1SDR FDEA201905261173Unknown · malfunctionedPDIS 140 34-10 2316 26MAY19 MEM OPEN U LOGPAGES:2923349 "ALT DISAGREE" EICAS WARNING IN DESCENT. F/O AND CAPT ALTIMETERS HAD 250 FT DIFFERENCE. AT ALTITUDE THE SPLIT WAS 180 FT, BUT "ALT DISAGREE" EICAS IN CRUISE, FL360. PERFORMED PITOT STATISDR FDEA201905231124Probe · defectiveON T/O ROLL CAPT AIRSPEED ERRATIC THEN BACK TO 30KTS AFTER LIFTOFF EICAS L & R EEC, AILERON LOCKOUT, RUDDER RATIO, AUTOTHROTTLES CLICKED OFF, F/O'S FLT DIR WENT OFF, CAPT RESET AND IT CAME BACK. CAPT'S AIRSPEED AND STBY AIRSPEED STAYED @ 30KTS. RTB. FOUND CSDR FDEA201905171091Tire · puncturedRIGHT NOSE TIRE FLAT, ZERO PSI DUE TO F.O.D. PUNCTURE, WAS FLAT ON ARRIVAL TO RDU. REMOVED AND REPLACED RT NOSE TIRE ASSY. REF. MM 32-45-02-4-0. SEE WRI 32-41-2281 FOR LEFT TIRE R&R. A/C OK FOR SERVICE.SDR FDEA201905161087Light · inoperativeLEFT MAIN GEAR LIGHT DID NOT ILLUMINATE GREEN NO OTHER INDICATIONS PRESENT TO INDICATE UNSAFE GEAR. RELAMPED LEFT GEAR INDICATOR IAW AMM 33-13-00-2. OPS CHECKED GOOD. A/C OK FOR FLIGHT.SDR FDEA201905051002Transmitter · failedTE FLAP DISAGREE/AT FLAPS 20. RAN QRH TE FLAP DISAGREE WHICH TOOK US TO FLAP ASYMMETRY. LANDED FLAPS 20. NO ROLL NOTICED IN FLIGHT. REMOVED AND REPLACED NR 1 AND NR 4 FLAP TRANSMITTERS IAW AMM 27-51-45-2. REMOVED AND REPLACED LEFT FLAP/STAB POSITION MODULE AS
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