Boeing 767-381
Service difficulty reports · 259
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 = '767381' 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 = '767381' 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 ABXA20220925101Unknown · unknownAIRCRAFT OVERBURNED BY 4000+ LBS ENROUTE.AIRCRAFT DIVERTED TO BOS. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED VISUAL INSPT, NO LEAKS. COMPLIED WITH FUEL QUANTITY BITE TEST PER FIM 28-41 FAULT TREE 841. AIRCRAFT RELEASED NO ETOPS, BITE TEST GOOSDR ABXA2022092093Fmc · failedDURING TAXI, RIGHT FMC FAILED. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RIGHT FMC IAW MEL 34-61-1-1A. MAINTENANCE PRCEDURES COMPLIED WITH. PLACARD INSTALLED. AICRAFT RETURNED TO SERVICE.SDR 2022F00438Oil System · leakingENGINE #2 WITH OIL LEAK IN TURBINE EXHAUST SLEEVE- AFTER UPPER LOW PRESSURE RECOP TUBE. ACTION: BORESCOPE INSPECTION REVEALED OIL LEAK ON SUPPLY TUBE. ENGINE REMOVED AND REPLACED.SDR IPXA2022072684570A/C Pack · abnormalINSPECTION TYPE:ETOP** ETOPS FILED OPEN**AFT CABIN TEMP MSG AND INOP LIGHT ILLUMINATED. DEFEND AFT CABIN TEMP CONT SYS PER MEL 21-61-1-2 DMP ACCOMPLISHED BY 0556511 AUTHORIZED BY 0557835 PLACARD INSTALLED. DI LOG UPDATED.SDR IPXA2022072584562Eicas · fault messageINSPECTION TYPE:ETOPWITH RIGHT SYSTEM SELECTED "WXR FAIL" DISPLAYED ON HSI (BOTH SIDES) WXR TEST NOT ATTEMPTED ALSO STATUS MSG "WXR SYS". LEFT SYSTEM OK.WEATHER RADAR SYS TEST C/O IAW AMM 34-43-00-735-033-002 REV 136.02. WXR SYS OK.SDR 2022FA0000307None · noneAFTER ENGINE START EICAS MSG LEFT AND RIGHT EEC MODE DISPLAYED WITH CA'S PITOT STATIC INSTRUMENTS ALL DISPLAYED OFF FLAGS- SELECTED ALL DATA AIR SWITCH/FIXED. AIRCRAFT RETURNED TO GATE AND GROUNDED BY MAINTENANCE. EEC MONITOR FAULT SHOWED NO FAULTS ON RIGHT ASDR IXXA20220529115Generator · inoperativeON CLIMB OUT, RIGHT GENERATOR DRIVE INOPERATIVE. APU CURRENTLY DEFERRED. FLIGHT CANNOT CONTINUE WITH SINGLE ELECTRICAL SOURCE. AIRTURN BACK TO DEPARTURE STATION KLAX WITH EMERGENCY DECLARATION. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARSDR IPXA2022052782562Wing Root · crackedINSPECTION TYPE:C16CRACK ON R/H OVERWING EMERGENCY EXIT DOOR LOWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5501411401 AND UPS EO B767-5310-83826-ASDR IPXA2022052782561Wing Root · crackedINSPECTION TYPE:C16CRACK ON L/H OVERWING EMERGENCY EXIT DOOR ;OWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5500527955 AND UPS EO B767-5310-83822-ASDR IPXA2022052582486Support Beam · corrodedINSPECTION TYPE:C16CORROSION ON RH WING INBD SPOILER SUPPORT BEAM UPPER CHORD BETWEEN WBL 168 AND 2BL 238REPAIR I.A.W 767-300BCF SRM 57-51-02, ALLOWABLE DAMAGE 1, REV. 43.00.SDR IXXA20220515111O-Ring · failedENROUTE FROM KSFO TO KAFW AT CRUISE OIL PRESSURE WAS IN AMBER RANGE AT 29 PSI. OIL PRESSURE THEN DROPPED REACHING RED RANGE AT 10 PSI AT 20000 FEET. CREW SHUT DOWN RIGHT ENGINE IN FLIGHT. AIR TURN BACK TO KSFO WITH EMERGENCY DECLARATION. LANDING WAS UNEVENTFULSDR IPXA2022052382369Skin Panel · debondedINSPECTION TYPE:C16DISBOND DAMAGE WAS FOUND ON LOWER SURFACE OF SKIN PANEL ON R/H WING INBD AFT FLAP NEAR WBL 122REPAIR I.A.W B767-300BCF SRM 57-53-01-2R-1, SRM 51-70-10-2R REPAIR GENERAL, AND SRM 51-70-10-2R-4 REV 43.00.SDR IPXA2022052382368Skin Panel · debondedINSPECTION TYPE:C16DURING C16 CHECK OF DATUM AIRPLANE, DISBOND DAMAGE WAS FOUND ON LOWER SURFACE OF SKIN PANEL ON R/H WING INBD AFT FLAP NEAR WBL 205.REPAIR I.A.W B767-300BCF SRM 57-53-01-2R-1, SRM 51-70-10-2R REPAIR GENERAL, AND SRM 51-70-10-2R-4 REV 43.00.SDR MK1Y20220515005Duct · damagedDURING MAINTENENCE INSPECTION FOUND DAMAGE ON #2 ENGINE RIGHT CORE COWL PRECOOLER EXIT DUCT UPPER SIDE (DEEP GROOVES, HOLE AND WORNAREA)SDR MK1Y20220515004Channel · crackedDURING MAINTENENCE INSPECTION FOUND CRACK AT FASTENER LOCATION ON FWD OUTER CHORD, STA 1809, STR 12AL.SDR MK1Y20220515003Bulkhead Web · dentedDURING MAINTENENCE INSPECTION A DENT DAMAGE CAUSED TO THE AFT PRESSURE BULKHEAD WEB 6" AFT OF STA 1582, 6 O'CLOCK.SDR MK1Y20220515002Skin · damagedDURING MAINTENENCE INSPECTION FOUND SEVERAL BLED OUTS ON FUSELAGE SKIN, STA 1458- STA 1544, STR 20L-STR 22L COMMON TOFASTENERS.SDR MK1Y20220515Skin · damagedDURING MAINTENENCE INSPECTION FOUND SEVERAL BLEED OUTS ON FUSELAGE SKIN, STA 434 - STA 544, STR 36R.SDR IXXA202205120101Fitting · corrodedBS 954 RBL 99-113 WL 171-148, SIDE FITTING PN 145T2523-8 HAS NUMEROUS AREAS OF LIGHT CORROSION CIT THE LWR FORWARD MATTING SURFACE (FORK)_ NOTE: CLOSEST AREA OF CORROSION TO A FASTENER IS .20" FOR ITEM 1 ONLY. STA 954 RBL 99 WL 142 SIDE FITTING PN 145T2523-SDR IXXA2022051103Web · corrodedITEM 1
STA 955 RBL 90 WL 165
CORROSION EXISTS CIT THE AFT SIDE SURFACE OF 111T1003-5 REAR SPAR WEB
CORROSION IS 2.4'LX 1.2"W AND 0.055" D
QA NOTES PREVIOUS BLENDING EXISTS CIT R/S WEB MEASURING
2.8' L X 1.4' WAND 0.055" D NEAR THE CORROSION
ITEM2
STA 95SDR IXXA202205110101Skin · corrodedSTA955 RBL96 WL 149
THERE ARE QTY (2) AREAS OF CORROSION CIT THE IML OF THE 145T3421-4 SKIN.
MEASUREMENTS:
1 A) 2.5"L X 1.3"W
1 B) 1.8"L X .50'W REF BOEING REPAIR AGREEMENT TIN-RE-2201692 FRR-13SDR IXXA2022051104Splice Plate · crackedSTA 915-984, RBL 98, WL 182
Q1Y (6) COUNTERSUNK HOLES FOR YLR/16N HAVE NOTICEABLE DAMAGE ON THE INSIDE SURFACE OF THE
HOLES CIT 145T8840-18 LONGERON.
HOLES SHOULD BE CLEAN AND ROUND .496" - .500"
ITEM2
STA 958, RBL 98, WL 182
COUNTERSUNK HOLE FOR FASTENESDR IXXA2022051003Doubler · crackedSTA 975 RBL 96 WL 182
QTY (2) 0.186 ELONGATED HOLES EXISTS COMMON TO 145T8754-25 DOUBLER, FWD OTBD FASTENERS ONLY
ELONGATIONS, EDGE MARGINS AND MEASURMENTS ARE AS FOLLOWS:
1A) ELONGATION MEASURES 0.2395", E/M 0.35", DISTANCE TO NEAREST HOLE 0.55"
1B)) ELONSDR IXXA2022051002Intercostal · cracked145T2700--32 INTERCOSTAL FWD INBOARD HAS QTY(1) 0.186" HOLE CT 145T2703-8 AND 145T2700-30 IS ELONGATED AND CRACKED. ELONGATION MEASURES 0.236". VISIUAL CRACK IS C/T EDGE OF THE HOLE AND EXTENDS OUTWARDS FROM THE HOLE EDGE 0.0415". CRACK MEASURES 0.0415" X 0.15SDR IXXA20220506104Fairing · corrodedWING TO BODY RH AFT LWR OF WW DOOR CUT OUT IB SIDE HAS CORROSION. FAS WO N431AZ-01-01 NON ROUTINE 00124SDR IXXA2022050902Nut Plate · corrodedFWD CARGO DOOR LOWER CUTOUT APPROX STA 504 R/H SIDE BALLMAT SUPPORT ANGLE CORRODEDSDR IXXA2022041809Doubler · corrodedKEEL BEAM STA 1005 AROUND HYD GROUND SERVICE DOUBLER CORRODED. FAS WO N431AZ-01-01 NR 00133SDR IXXA2022050602Panel · corrodedRH WING FIXED LE AT WS 920 APROX LWR SUPPORT PANEL CORRODED. FAS WO N431AZ-01-01 NON ROUTINE 00353SDR IXXA2022050401Rib · crackedCRACK INDICATION ON RH REAR SPAR LOWER CHORD AT RIB POST 10. ONE CRACK INDICATION ON THE OUTBOARD SIDE OF RIB 10 AFT/OUTBOARD FASTENER TRAVELING APPROX 1/4" LONG. FAS WO N431AZ-01-01 NON ROUTINE 00327SDR IXXA2022051102Rib · crackedCRACK INDICATION NOTED ON RH REAR SPAR LOWER CHORD AT RIB POST 10. ONE CRACK INDICATION ON THE OUTBOARD SIDE OF RIB 10 AFT/OUTBOARD FASTENER TRAVELING FWD APPROX 1/4" LONG. REF FAS WO N431AZ-01-01 NON ROUTINE 00327SDR IXXA2022042405Bracket · crackedCRACKED ANGLE TAB SUPPORT LEFT WING INBOARD FRONT SPAR STA. 170. REF FAS WO N431AZ-01-01 NON ROUTINE 00142SDR IXXA20220509201Angle · crackedRH WING LE STA 522 ANGLE CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00280SDR IXXA2022042404Skin · corrodedLH WING UPPER SURFACE HAS SEVERAL AREAS (AS MARKED) WITH EVIDENCE OF CORROSION. INBD T/E AT REAR SPAR W.S. 197 REF FAS WO N431AZ-01-01 NON ROUTINE 00293SDR IXXA2022041807Angle · crackedAREA AFT OF BULK CARGO PIT STA 1577 LH OB SIDE WL 200 MAIN DECK FLOOR SUPPORT IB SPLICE ANGLE CRACKED FAS WO N431AZ-01-01 NR 00105SDR IXXA2022041806Angle · crackedAREA AFT OF BULK CARGO PIT STA 1577 LH OB SIDE WL 200 MAIN DECK FLOOR SUPPORT OB SLICE ANGLE CRACKED. FAS WO N431AZ-01-01 NR 00104SDR IXXA2022041805Angle · crackedAREA AFT OF BULK CARGO PIT STA 1577 RH OB SIDE WL 200 MAIN DECK FLOOR SUPPORT I/B SPLICE ANGLE CRACKED FAS WO N431AZ-01-01 NR 00103SDR IXXA2022041804Angle · crackedAREA AFT OF BULK CARGO PIT STA 1577 RH OB SIDE WL 200 MAIN DECK FLOOR SUPPORT OB SPLICE ANGLE CRACKED. FAS WO N431AZ-01-01 NR 00102SDR IXXA2022050801Support · crackedRH WING LE STA 656 ANGLE SUPPORT CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00279SDR IXXA2022042403Angle · crackedRH WIN LE STA 522 ANGLE CRACKED REF FAS WO N431AZ-01-01 NON ROUTINE 00280SDR IXXA2022050703Web · crackedR WING WS 522 LE, UPON REMOVAL OF CRACKED ANGLE FOUND THE ATTACHING WEB IS CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00256SDR IXXA2022050702Angle · crackedR/W STA 664 L/E LOWER RIB SUPPORT ANGLE IS CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00253SDR IXXA2022051001Floorbeam · corrodedFWD CARGO LOWER FLOOR STRUCTUREJUST I/B OF DOOR CUTOUT AT STATION 508 HAS CORROSION. FAS WO N431AZ-01-01 NON ROUTINE 00191SDR IXXA2022050701Angle · crackedRH WING LE RIB AT WS 522 HAS CRACKED LOWER ANGLE. FAS WO N431AZ-01-01 NON ROUTINE 00119SDR IXXA2022050605Angle · corrodedRH WING LE RIB AT WS 656 HAS CRACKED LOWER ANGLE. FAS WO N431AZ-01-01 NON ROUTINE 00111SDR IXXA2022042401None · crackedRH WING LE RIB AT WS 656 HAS CRACKED LOWER ANGLE REF FAS WO N431AZ-01-01 NON ROUTINE 00111SDR IXXA2022042402Structure · crackedRH WING LE RIB AT WS 522 HAS CRACKED LOWER ANGLE REF FAS WO N431AZ-01-01 NON ROUTINE 00119SDR IXXA2022041808Angle · crackedCORROSION FOUND ON ANGLE SUPPORT EXTERNAL POWER RECEPTACLE COMPARTMENT. FAS WO N431AZ-01-01 NR 00132SDR IXXA2022041803Panel Support · corrodedKEEL BEAM STA 889 PANEL SUPPORT CORRODED. FAS WO N431AZ-01-01 NR 00081SDR IPXA2021111776091None · noneINSPECTION TYPE:ETOP** ETOPS FILED OPEN**L PACK TEMP EICAS MESSAGE AFTER START. NO OTHER FAULT INDICATION. DEFERRED PER MEL 21-51-1-1. L PACK INOP. DMP C/W. DI LOG UPDATED, PLACARD REMOVEDSDR IXXA20211109080None · noneON SHORT FINAL "GEAR DISAGREE" EICAS AND MASTER CAUTION ACCOMPANIED BY "TAILSKID" EICAS. IAW B767 FAULT ISOLATION 32-20-FAULT TREE 806, CLEANED AND ENSURED THE INTEGRITY OF LANDING GEAR HANDLE. OPERATIONAL CHECK GOOD IAW B767 AMM 32-31-00. AIRCRAFT RELEASED TO
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