Boeing 767-338
Service difficulty reports · 1,328
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 = '767338' 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 = '767338' 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 IXXA20240521033Actuator · leakingPOST FLT CREW REPORTED VERY LOUD BANG AT V1 & RUBBER ODOR. ACFT GROUNDED FOR INSPS & MAINT. WITH LT & RT ENGS ENGAGED IN IDLE RUN IAW AMM 71-00-00, NO FAULTS FOUND OR ODORS NOTED WHEN ISOLATING BLEEDS FOR LT & RT ENGS. LT & RT PACKS OPS CHK GOOD. ENG PARAMESDR IXXA2024051701Bracket · corrodedHYDRAULIC LINE BLOCK CLAMP BRACKET CORRODED.SDR IXXA2024051604Fastener · damaged#3 SLAT LE HAS DAMAGED FASTENER.SDR IXXA2024051602Attach Angle · cracked#1 PYLON FRAME ATTACH ANGLE COMMON TO THE OTBD SIDE LOAD FITTING IS CRACKED ACCESS THROUGH PANEL 436ALSDR IXXA2024051601Channel · crackedRIGHT SIDE OF DOOR CUTOUT ON 313AL DOOR FOUND A CRACK ON ANGLESDR ABXA20240516591Wire · brokenLE FLAP SLAT DISAGREE AFTER START CHECKLIST. AC RETURNED TO BLOCK AND MAINTENANCE GROUNDED AC T/S IAW WDM 27-81-11, REPLACED RELAY K624 NO HELP. FOUND THE INBD SLAT BYPASS VALVE IN POS 1 NO POWER FOUND ON PIN 2 CONN D1515 FOUND OPEN. CK FROM CONN D5316P PIN 42SDR IXXA2024051501Panel · damagedP32 PANEL HAS DAMAGE AROUND WIRE PASS THRUSDR IXXA2024051202Angle · corrodedLAV/GALLEY DRAIN HOLE REINFORCEMENT STIFFENER CORROSION NEXT TO GROUND WIRE ATTACH POINT LOCATION IN LOWER LOBE OF FLC BETWEEN FS 654+121 AND 676 BETWEEN STR 35L AND 36LSDR IXXA2024051201Shear Tie · corrodedCORROSION ON FLC LOWER LOBE SHEAR TIE LOCATED ON AFT SIDE OF FRAME 742 AND BETWEEN STR 39R AND RIGHT KEEL BEAM EXTENSIONSDR IXXA2024051110Frame · damagedFRAME WEB DAMAGEDSDR IXXA2024051109Seal · wornPANEL 345AFB SEAL IS WORN.SDR IXXA2024051108Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED AT MID AUX TRACK.SDR IXXA2024051107Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED. OB OF MID AUX TRACK.SDR IXXA2024051106Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED.SDR IXXA2024051105Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED.SDR IXXA2024051103Bracket · crackedSLAT BRACKET CRACKED RT LE STA. 270SDR IXXA2024051102Bracket · crackedRW LE STA. 278 HAS CRACKED BRACKETSDR IXXA2024051101Bracket · crackedRW LE BRACKET CRACKED.SDR IXXA2024050603Support Angle · cracked#1 STRUT FAIRING LONGERON SUPPORT ANGLE IS CRACKED AT NAC 364SDR IXXA2024050602Skin Panel · crackedLEFT WING FIXED L/E PANEL CRACKED IN 2 PLACES UNDER #5 SLATSDR IXXA2024050601Skin · cracked#9 SPOILER LE AROUND 1 FASTENER CRACKEDSDR IXXA2024050502Skin Panel · damagedRH VERTICAL STAB BETWEEN AUX SPAR AND FRONT SPAR AT RIB 2-3 HAS EDGE CORE DAMAGESDR IXXA2024050501Access Panel · delaminatedRH VERTICAL STABILIZER BETWEEN AUX SPAR AND FRONT SPAR RIBS 2-3 HAS DELAMINATIONSDR ABXA2024050488Shutoff Valve · malfunctionedR HPSOV VALVE MESSAGE APPEARED IN CRUISE CREW DIVERTED FROM SJO TO MIA. DESTINATION WAS CVG. MAINTENANCE GROUNDED AC AND DEFERRED RH HPSOV AND LOCK OUT IAW MEL 36-11-2 .AND RETURNED AC TO SERVICE TO CONTINUE TO FLY TO CVG . WHERE THEY REPLACED THE PRSOV AND CSDR ABXA2024050387Module · malfunctionedRUDDER RATIO EICAS MSG & DISCRETE LIGHT CAME ON TAXI OUT AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE DEFERRED RUDDER RATIO SYSTEM . IAW ABX-MEL -27-21-1. AND REMOVED/REPLACED CSEU M538 1 RIGHT, PERFORMED RUDDER RATIO OPS OK PER AMM 27-21-0SDR IXXA2024050303Seat Track · crackedCAPTAINS FORWARD OB SEAT TRACK CRACKED.SDR IXXA2024050302Seat Track · wornCAPTAINS IB AFT TRACK HOLES WORN.SDR IXXA2024050301Seat Track · crackedFIRST OFFICERS FORWARD IB SEAT TRACK CRACKED.SDR IXXA2024050202Seat Track · crackedCAPTAIN'S FORWARD IB SEAT TRACK CRACKED AT FORWARD STOP PIN HOLE.SDR IXXA2024050201Seat Track · wornFO'S IB AFT TRACK HOLES WORN ELONGATED.SDR IXXA2024060301Skin · crackedL1 DOOR LOWER AFT CORNER CRACKED.SDR IXXA2024050101Panel · cracked#1 OB STRUT PANEL CRACKEDSDR ABXA2024042684Pneumatic System · failedAFTER PUSH BACK APU AIR PRESSURE LOW ON ENGIN START, WILL NOPEN START VALVE AC RETURNED TO GATE MAINTENANCE DEEFERRED THE APU PNEUMATICS IAW ABX-MEL-49-11-1-1 AND RETURNED AC TO SERVICE .SDR IXXA20240422026Guide Track · fodPOST FLIGHT CREW REPORTED L2 WINDOW DIFFICULT TO CLOSE. UNWANTED MATERIAL CLEANED FROM GUIDE RAIL AND ROLLERS LUBED. OPERATIONAL CHECK OF L2 WINDOW CHECK GOOD PER BOEING AIRCRAFT MAINTENANCE MANUAL 56-11-02. NO ADDITIONAL FAULTS NOTED.SDR ABXA2024041781Control Unit · malfunctionedAFTER TAKE OFF EICAS MESSAGE LEADING EDGE SLAT DISAGREE. LEADING EDGE SLAT DISPLAYED BETWEEN UP AND 1. AC PERFORMED ATB AND LANDED , MAINTENANCE GROUNDED AC AND TROUBLESHOT REPLACING FSEU IAW B767 AMM 27-51-01. LEADING EDGE SLATS AND FLAPS CHECK GOOD AS PER SDR ABXA2024041078Door · unsecureMCD WARNING ANNUCIATORS INDICATOR ILLUMINATED DURING PUSH-BACK , AC RETURED TO THE GATE AND MAINTENANCE CLOSED AND LATCHED MAIN CARGO DOOR IAW B767 AMM 52-32-00 DOOR OPS CHECK GOOD .AC TAXIED OUT AND DEPARTED IN SERVICABE CONDITION ,.SDR IXXA2024051001Skin · crackedRI DOOR AFT LOWER CORNER CRACKEDSDR ABXA2024040576Control Panel · faultyRIGHT STARTER CUTOUT EICAS MESSAGE AND #2 ENG START VALVE LIGHT ILLUMINATED ON TAXI OUT. REMOVED AND REPLACED START CONTROL PANEL IAW B767 AMM 80-11-51. OPS CHECK GOOD, PLACARDS REMOVED. A/C VERIFIED NO ETOPS. NO MAINT PROCEDURES REQUIRED.SDR ABXA2024040273AWire Harness · damagedRT HYD QUANTITY LIGHT ON OVER HEAD, RT HYD EICAS MESSAGE (RT.00 RF) LIGHT. DEFERRED. T/S WIRING, CK NORMAL. INTERMITTENT IND AFTER HYD PLACED ON OFF POSITION. FOUND CONNECTOR D60 QTY ASSY LOCKING MECHANISM DAMAGED IAW WDM 29-33-11. REMOVED AND REPLACED CONN D6SDR ABXA2024040272Wire · damagedIN FLIGHT RT ENGINE SHUTDOWN & RT ENGINE FUEL VALVE EICAS MESS. ENGINE RUNNING NORMAL, ALSO FALSE EGT EXCEEDANCE. AIRCRAFT IS AOG. REMOVED W388-008-18 WIRE AND INSTALLED NEW WIRE FROM D4238P TO D4220J ALL PER B767 SWPM 20-10 REF B767 WDM 76-11-11. AC RETURNED SDR ABXA2024040300273Warning Message · illuminatedRT HYD QUANTITY LIGHT ON OVER HEAD, RT HYD EICAS MESSAGE (RT.00 RF) LIGHT. DEFERRED.SDR ABXA202404030272Warning Message · false indicationIN FLIGHT RT ENGINE SHUTDOWN & RT ENGINE FUEL VALVE EICAS MESS. ENGINE RUNNING NORMAL, ALSO FALSE EGT EXCEEDANCE. AIRCRAFT IS AOG FOR TROUBLESHOOTING.SDR ABXA2024033171Control Module · faultyAPPROXIMATELY 25 MINS INTO FLIGHT THE EICAS DISPLAYED "R ENG SHUTDOWN" AND "R ENG FUEL VAL". IN-FLT START PARAMETERS WERE ALSO DISPLAYED. RIGHT "ENG VALVE" LIGHT ON CONTROL DISPLAYED CONTINUED PANEL. CONDUCTED T/S PER FIM 76-11 F.T. 813 R MEC REPLACEMENT REQUISDR ABXA2024032766Shutoff Valve · inoperativeRT ENGINE HPSOV MSG DURING CRUISE FLIGHT. (REASON FOR DIVERSION TO IND: HPSOV MESSAGE (NO ICING)- ICING AT CVG/JFK) ACCOMPLISHED THUMB TEST ON HPSOV FROM CONTROLLER SIDE OF SENSE LINE, NO FAULTS PRESENT. REPLACED HPSOV IAW B767 AMM 36-11-07 AND RH BLEED CONTROSDR ABXA20240325363Skin · damagedUPON LANDING PTY TAIL STRIKE, TAILSKID EICAS MESSAGE, AIRSPEED DROPPED OFF AND ADDED THRUST, NO BOUNCED LANDING. ACCOMPLISHED TAIL STRIKE/SKID CONDITION INSPECTION IAW B767 AMM 05-51-32, FOLLOWING DAMAGE WERE FOUND, SKIN DENTED, CRACKED BETWEEN STA. 1395 AND 1SDR IXXA20240322018Lamp · inoperativeDURING SCHEDULED MAINTENANCE, OVERWING ESCAPE LIGHT LAMP INOPERATIVE. OVERWING ESCAPE LIGHT LAMP REMOVED AND REPLACED PER B767 AIRCRAFT MAINTENANCE MANUAL 33-51-06. OPERATIONAL CHECK GOOD. NO ADDITIONAL SYSTEM FAULTS NOTED.SDR ABXA2024031558Apu · shutdownAPU SHUTDOWN ON PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC . AND DEFERRRED THE APU FOR DEPARTURE IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE. AC DEPARTEDSDR ABXA2024031156Plug · installedDURING PUSH BACK ,L ENG HPSOV EICAS STATUS MESSAGE L ENG BLEED LIGHT, L+R DUCT LEAK LIGHTS ALL ILLUMINATED AFTER ENGINE WERE STARTED PACKS + BLEEDS TURNED OFF PER QRH + LIGHTS STAYED ILLUMINATED ENGINES SHUT.AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC , TSDR IXXA20240307012Electronic Unit · faultedPOST FLIGHT CREW REPORTED, FWD CARGO AND LEFT EMERGENCY DOOR EICAS DISPLAYED ONCE ON CLIMB OUT AND ONCE IN CRUISE FOR APPROXIMATELY 2 SECONDS. PRESSURIZATION WAS NORMAL. FLIGHT CONTINUED UNAFFECTED AND WITHOUT INCIDENT. PSEU BITE CHECK NOTED THE FOLLOWING FAULSDR ABXA20240307653Shutoff Valve · faultedLEFT WING HYD VALVE MESSAGE CAME ON DURING PUSH BACK, AC RETURENED TO GATE AND MAINTENANCE GROUNDED AC , MAINTENANCE DEFERRED LEFT WING LATERAL CONTROL HYD SHUTOFF VALVE IAW MEL ABX-27-03-1 RETURNED AC TO SERVICE AND DEPARTED .
Back to Boeing 767-338