Boeing 767-300
Service difficulty reports · 2,161
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 FDEA202201120053Bracket · cracked#1 PYLON, INBD SIDE, NAC STA 377, FRAME ATTACH BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 SRM 51-40-02, ALL PARTS VERIFED PER B767 AIPC 54-53-02.SDR FDEA202201110045Floor Panel · damagedMAIN DECK FLOOR PANEL 241AGF IS DENTED IN SEVERAL AREAS ON UPPER SURFACE FABRICATED NEW FLOOR PANEL IAW FEDEX DRAWING SRZ-25-005SDR FDEA202201110046Floor Panel · damagedMAIN DECK FLOOR PANEL 241ZFF IS DENTED ON UPPER SURFACE REPAIRED DENTED FLOOR PANEL IAW B767 SRM 53-00-50-2R PARAGRAPH 4.DSDR FDEA202201110047Slat · wornRH WING SLAT #8 SKIN AFT FACE WITH WEAR ON TWO LOCATIONS OSS-430 AND OSS-495. RH WING, SLAT #8, LOWER SKIN, WEAR AT OSS 495 WAS EVALUATED AND STRUCTURAL DAMAGE NOT FOUND, ONLY PAINT DAMAGE, PAINT WAS RESTORED AND WEAR AT OSS 432 WAS REPAIRED IAW B767 SRM 5SDR CALA2022011000099Slat · false indication*EMERGENCY DECLARED* LE SLAT DISAGREE ON FINAL ABOUT 1900 FT DURING FINAL CONFIG C/W FIM 27-81 FAULT TREE 815 LE SLATS OPS CHECK GOOD DURING EXTENSION AND RETRACTION 2X NO MESSAGES.SDR IPXA2021122877335None · noneINSPECTION TYPE:NA** ATB ** EMERGENCY DECLARED ** EXITED A/C USING INERTIAL REELS ** JUST AFTER V, FIRE BELL SOUNDED AND CONTINUED TO SOUND UNTIL EVACUATION NO OTHER INDICATION NO EICAS NO ENGINE OR CARGO FIRE WARNING JUST CONTINUOUS BELL.VERBAL CREW BRIEFING SDR FDEA202112263151None · noneAFTER LOWERING THE LANDING GEAR ON FINAL APPROACH, THE LEFT MAIN GEAR LIGHT AND THE LEFT HALF OF THE RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE. PERFORMED GA, RECEIVED GROUND VISUAL CONFIRMATION THAT LEFT MAIN GEAR APPEARED DOWN, AND RAN QRH PROCEDURES. LASDR FDEA202112193111None · damagedMDIS 197 28-02 0307 19DEC21 MEM OPEN U AFTER FUELING RH WING TANK TO 40K FOUND FUEL LEAKING FROM RH WING JUST INBOARD OF THE VENT BOX. FOUND LEAK RH WING FWD OF #8 FUEL MEASURE STICK, BELIEVE #8 SLAT TRACK DRAIN. ACCOMPLISHED PRELSDR FDEA202112042990None · noneLIGHTNING STRIKE APPROX. STA 532, STR 39L. MWT 0000530614 : TURCOTTE, GARRETT S - 05-DEC-2021 15:18 INSTALLED REPAIR DOUBLER REF 767 SRM 53-00-01-2R REPAIR 1 AT SAT 532 STR 39 LSDR FDEA202111242929None · noneMDIS 110 33-50 7324 24NOV21 CDG FACT U EMERGENCY LIGHT GUARD IS BROKEN . FACT 24NOV21 03:19 CDG U R&R'D EMERGENCY LIGHT GUARD PER MM:33-51-08-4 , OPS CHK OK .SDR FDEA202111232944Autopilot Sys · faultedPASSING 32,000 ON CLIMB OUT, WITH LT AUTOPILOT ENGAGED, RECEIVED A/P EICAS ALONG WITH A/P LIGHT ON UPPER FORWARD INST PANEL. A/P REMAINED ENGAGED. DISENGAGED A/P & REENGAGED LT A/P. AFTER PASSING 36,000 RECEIVED A/P EICAS AGAIN. MANUALLY DISCONNECTING A/P SDR FDEA202111192903Switch · failedWAS ALERTED BY RAMP PERSONAL OF SMOKE COMING FROM FWD CARGO DOOR CONTROL PANEL WHEN DOOR WAS OPENED ELECTRICALLY. COMPLIED WITH EA H-3330-T0365583 P 1 LOWER CARGO LT SWITCH SHORTED ADDITIONAL MAINTERANCE PROCEDURES FOR MEL 33-37-01-05 C/7294444SDR FDEA202111192922None · noneWAS ALERTED BY RAMP PERSONAL OF SMOKE COMING FROM FWD CARGO DOOR CONTROL PANEL WHEN DOOR WAS OPENED ELECTRICALLY. SUBMITTED IN ERROR. PLEASE REFERENCE SDR# 21-2903. SUBMITTED IN ERROR. PLEASE REFERENCE SDR# 21-2903.SDR FDEA202111082797Skin · crackedPUNCTURE AND DENT DAMAGE ON SKIN PN:148T3211 BETWEEN STA 1582 AND STA 1629 AND S-33L AND S- 35L. REPAIRED SKIN PN:148T3211 PER E.A.#:H-5330-T0365358 DATED: NOV 13, 2021 "TITLE: FUSELAGE - SECTION 48 FUSELAGE SKIN - PERMANENT REPAIR OF IMPACT DAMAGE BETWEEN SDR FDEA202111022762Slat · wornSLAT #8 WITH WEAR BEHIND WEDGE AREA NEAR TO OSS 441. SLAT #8 ON WEDGE AREA NEAR TO OSS 441 WAS REPAIRED I.A.W. SRM 57-43-02-2R FIG. 101 PAGE 1-2 SHEET 1-2 AND SRM 51-70-10-2R REPAIR 4 PAGE 9,10,82,149,162 FIG. 202 SHEET 8 REV. 81 AUG 15/2021SDR FDEA202111022761Slat · crackedLH WING SLAT NO. 5 WS 433.1 TRAILING EDGE WEDGE WITH NICK. LH WING SLAT #5 T.E. WEDGE AT POSITION OSS 427.5 - 439.5 UPPER AND LOWER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R PAG. 1-2 FIG.201 REP. 1 AND SRM 51-70-10-2R PAG. 149, 159, 162,163 FIG. 202 REV. SDR FDEA202111022759Slat · crackedLH WING SLAT 5, OSS 488.8 TRAILING EDGE WITH CRACK. LH WING SLAT #5 T.E. WEDGE AT POSITION OSS 485.3-490.3 UPPER AND LOWER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R REP. 1 PAG. 1,2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 149, 159, 162, 163 FIG. 202 REV.8SDR FDEA202110202580None · crackedRIGHT WING OUTBOARD FLAP WITH CRACK ON LEADING EDGE NEAR TO WS 642.2. RIGHT WING OUTBOARD FLAP, LEADING EDGE NEAR TO WS 642.2 WAS REPAIRED IAW SRM 57- 53- 01-2R PAG. 1-5 FIG. 201 SHEET 3, 5 TABLE I AND SRM 51-70-03-OG PAG. 19, 30, 36 FIG. 5 SHEET 1 REV. 8SDR 2DYA20201021000None · nonePILOT DISCOVERED AFT RIGHT EMERGENCEY LIGHT IS INOP. MX REPLACED THE RELAY BULB IAW 33-51-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR UIEA2021101502239Pbe · nonePASSENGER CABIN FWD B/C CLOSET PBE SECURITY SEAL MISSING P/N 15-40F-80 S/N 94703002(<P><SPAN>REMOVED & REPLACED PBE AT FWD B/C CLOSET AS REQUIRED PER AMM 35-31-02 CK'D OK .</SPAN></P>)SDR UIEA2021101502240None · none#1 ENG O/B T/REV LATCH CAM IS BENT(<P><SPAN>REMOVED AND REPLACED 31 ENG O/B T/REV LATCH CAM IAW AMM 78-31-01 OPS CHECK OK</SPAN></P>)SDR UIEA2021101502241None · none#2 ENG. #4 BRG. OUTER INTERNAL SCAVENGE TUBE IS NOT SECURED & OUT OF PLACE(<P><SPAN>REMOVED #2 ENG TURBINE EXHAUST PLG IAW B767-300 AMM 78-11-02</SPAN></P> / <P><SPAN>REPOSITIONED AND SECURED INTERNAL SCAVENGE TUBE CLAMP AS REQUIRED SDR UIEA2021100102155Switch · intermittentAPU FAULT 3 ATTEMPTS WILL NOT START. CYCLED BATTERY SWITCH. APU STARTED FIRST ATTEMP. NO DEFECTS NOTED IAW B767AMM 49-11-00. OPS CKS GOOD.&NBSPSDR UIEA2021063001445Apu · malfunctionedAPU COLD START UNSUCCESSFUL 3 START ATTEMPTS -16C / FL 360(<P>NOTED BY MX PERFORMED FIM 49-11 FLT 958 MINI FLAG 141 LRU"START ABORT" RESET CLEARED </P>)SDR UIEA2021063001447Apu · malfunctionedAPU STARTS UNSUCCESSFUL / 3 START ATTEMPTS (COLD SOAK) / -23 DEGREES CELCIUS / FL 390 / MAX RPM 33% 815 DEGREE(<P>NOTED BY MX BITE PERFORMED ON ECU IAW B767 FIM 49-11 FT 858</P>)SDR P5CA2021053100218None · noneCOCKPIT PORTABLE OXYGEN FULL FACE MASK DUE TIME CHANGE MF JAN 12 P/N 10800C15F.(<P>REMOVED COCKPIT PORTABLE, OXYGEN FULL FACE MASK AS PER AMM 35-01-2-11. INSTALLED SERVICIABLE PORTABLE OXYGEN FULL FACE MASK AS
PER AMM 35-01-2-11.SDR P5CA2021053100214None · noneLAV PORTABLE OXYGEN MASK DUE TIME CHANGE MF JAN 13 P/N 289-601-212. REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS PER AMM 35-31-01.SDR UIEA2021052701202Warning Message · false indicationR ENG EEC C1 STATUS MESSAGE AFTER LANDING.(<P>CLEARED MESSAGE AS REQUIRED PER FIM 71-01 SHEET 1 - SHEET 4.SDR UIEA2021052601183Control Valve · faultedL/H PACK DID NOT TURN OFF WHEN SELECTED(<P>PERFORMED PACK TEMPERATURE CONTROL OPERATIONAL TEST IAW AMM 21-51-00-705-161. TEST PASS, NO DEFECT NOTED AT THIS TIME.</P><P>LOG PAGE 1484388: REMOVED AND REPLACED LH PACK FLOW CONTROL VALVE PER AMM 21-51-01. OPS CHK SDR UIEA2021042801014Transceiver · intermittentFO RA INTERMITTENT (NO LAND 3) REMOVED AND REPLACED RT RA XCEIVER, OPS CK OK. THIS CLEARS MDDR 146046.</P><P><SPAN></SPAN></P>)SDR FDEA202104271048Engine · overtempSTARTED DESCENT FROM FL 310, THE OIL TEMP SPIKED UP TO 165 ON THE LT ENGINE. THROTTLE WAS PULLED TO IDLE, & CHECKLIST RUN FOR HIGH OIL TEMP, LT ENGINE. OIL QUANTITY INDICATED 0 (ZERO). AFTER 7 MINUTES OIL TEMP REDUCED BELOW AMBER BAND. ENGINE REMAINED ATSDR FDEA202104210962Transmitter · out of adjustLE SLAT DISAGREE ADJUSTED FLAP HANDLE POS. TRANSMITTERS ON TSI 27-80/6190. PERFORMED FLAP AND SLAT PRIMARY DRIVES AND POSITION INDICATING SYSTEM - TEST REF AMM 27-51-00-5. ALL TEST PASSED.SDR UIEA2021041600916Ecu · malfunctionedAPU AUTO SHUTDOWN. REMOVED & REPLACED ECU PER AMM 49-61-05. OPS CHECK IS NORMAL.SDR FDEA202010242632Escape Rope · looseF/O'S ESCAPE ROPE PANEL IS LOOSE. REINSTALLED ESCAPE ROPE COVER, PER MM 25-61-02-2. A/C OK FOR SERVICE.SDR FDEA202007291700Flap System · malfunctionedON APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MSG & TRAILING EDGE LIGHT. COMPLETED THE QRH, TE FLAP ASYMMETRY CHECK LIST & USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. 'EMERGENCY DECLARED. ALL SWITCHES BACK TO NORMAL. SDR FDEA202007011419Slat · chafedRW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAWSDR ABXA20200521063Controller · malfunctionedAFT CABIN TEMPERATURE EICAS MESSAGE. AIRCRAFT WAS GROUNDED.SDR FDEA2020060390981Hmu · failedOPEN U DURING CLIMB DEPT KORD APPROX 5000 LOUD BANGING NOISE FOLLOWED BY YAW, A/P ENGAGED, LE N1 30%, FUEL FLOW APPROX. 4000PPH, RT ENG NORMAL, LT ENG BACK TO NORMAL. SECOND OCCURRENCE BANGING LOW N1 & FF ON LT ENG EICAS "L ENG HPSOV" ( SOUNDED LIKE COMPRESSOSDR 2020F00061Connector · unsecureSEAT EMERGENCY LIGHTS INOP AT 38HJ TO 41HJ. RECONECTED CONNECTOR AT SEAT 38HJ. OPS CHECK GOOD IAW MM 33-60-98.SDR CNMA2019100901Connector · defectiveINFLIGHT LOST EGT INDICATION ON RIGHT ENGINE ON BOTH UPPER EICAS AND STBY INDICATION. ACCOMPLISHED FIM 77-21. FAULT TREE 806. REMOVED & REPLACED JUNCTION BOX PER AMM 77-21. OPS CHECK NORMAL.SDR FDEA201808312337Skin · damagedR/H INBD AILERON HAS HOLES IN THE UPPER AND LOWER SURFACES EXPOSING CORE. REPAIRED UPPER AND LOWER SKINS IAW B767 SRM 57-60-01-01 FIG 1, SRM 57-60-01-2R FIG 201 REPAIR 1 AND SRM 51-70-04 PARA 5D AND EA H-2710-T0342062-P1 FLIGHT CONTROLS-AILERONS AND TABS-RSDR FDEA201808312336Skin · gougedR/H I/B AILERON FWD O/B CORNER ON L/E PANEL GOUGED REPAIRED GOUGE ON R/H WING AILERON FWD CORNER OF L/E PANEL IAW B767 SRM 57-60-01-2R, 51-70-17, AMM 51-21-00, AND EA H-2710-T0342063-P1 FLIGHT CONTROLS-AILERONS AND TABS-RSC TRACKING R/H WING INBD INBD AILSDR DALA201805239999Bushing · mismanufacturedDURING ACCOMPLISHMENT OF BOEING CMM 310T1020-3 (71-21-11) REPAIR 3-1, BUSHING REPLACEMENT, DTO WAS UNABLE TO ACHIEVE THE DIMENSIONAL REQUIREMENTS OF THE BUSHINGS. BOEING WAS CONTACTED FOR PART DISPOSITION AND RESPONDED WITH MESSAGE NUMBER DAL-DAL-18-0654-06B ISDR FDEA201802260484Escape Rope · out of positionL1 DOOR ESCAPE ROPE FOUND PULLED OUT FROM TRACK ABOVE THE DOOR. INSTALLED THE L1 DOOR ESCAPE ROPE IAW AMM 25-61-04-2-1.SDR CNMA2018010001Engine · vibrationAT 25000 FT STILL CLIMBING RIGHT ENGINE GAVE OUT A LOUD BANG FOLLOWED BY HIGH VIBRATION , LOW N1 AND HIGH N2. EGT APPEARED TO BE NORMAL. CORRECTIVE ACTION:RIGHT ENGINE REMOVED & REPLACED IAW OAI WC 71-R07-RSDR FDEA201711293320Warning Message · illuminatedPDIS 138 52-70 1261 29NOV17 MEM SHORTLY AFTER LEVEL OFF AT FL370 "MAIN CARGO DOOR" EICAS ALERT ILLUMINATED. COMPLIED WITH ORH PROCEDURES. DESCENDING THROUGH 17,000 ENROUTE TO 10,000 MAIN CARGO DOOR LITE WENT OUT. CHECKED GAP ON MAIN CARGO SDR UIEA2017112302282Smoke Detector · inoperativeMAIN CARGO SMOKE DETECTOR 1C & 2E LOOP 2 INOP. TRANSFERRED TO MDDR 86255 AS PER MEL 26-16-02-01 CAT C.SDR HALA2017112100282Wire · damagedLEFT ENGINE BLEED VALVE EICAS MESSAGE. RETURNED TO DEPARTURE. FOUND HPSOV TERM 1 CONNECTOR D4210P PIN 10 OPEN AND HPSOV TERM 2 TO D4210P OPEN. REPLACED THE TERMINAL 1 ON WIRE.SDR UIEA2017112002263Exciter · malfunctionedLEFT ENGINE REQUIRED 2 START ATTEMPTS. SECOND START SUCCESSFUL. NO PARAMETERS EXCEEDED. REMOVED AND INSTALLED A NR 1 IGNITION EXCITER BOX ON THE LEFT ENGINE IAW AMM 74-11-01. PERFORMED AUDIBLE TEST AND TEST OK. OPERATIONAL CHECK GOOD AT THIS TIME PER AMM 80-11SDR IPXA2017110823386Compressor · stalledAFTER TAKEOFF RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. RIGHT EGT STARTED TO FLUCTUATE FOLLOWED BY VIBRATIONS AND POPPING SOUNDS. THE TOWER REPORTED FLAMES FROM RIGHT ENGINE. ENGINE WAS SHUT DOWN, EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. REM
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