Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA2021314034Panel · delaminatedTHERE IS DELAMINATION ON THE CORNERS OF 2 RIGHT WING UPPER T/E PANELS, FWD OF THE RIGHT O/B AILERON AT W.S.1030. REMOVED I/B AND O/B TE PANELS AT W/S 1030, REMOVED CORROSION BY .025" FROM NOMINAL .080" AND FOUND REMAINING .055" FOUND TO BE OUT OF LIMITS IAW B7SDR ABXA202143023Shutoff Valve · stuckRT ENG BLEED OFF LIGHT ON WITH ALSO THE RT PACK OFF LIGHT ON DURING TAXI. AIRCRAFT LINED UP FOR TAKE OFF AND RT ENG. BLEED LIGHT DID NOT EXTINGUISH DURING ENGINE ACCELERATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. REMOVESDR ABXA2021331020Door · unlatchedAFTER TAKE OFF, MX CARGO DOOR LIGHT ILLUMINATED.AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO ORIGIN. AIRCRAFT WAS GROUNDED BY MAINTENANCE. FOUND THE MCD DOOR DOOR NOT LATCHED LIGHT ON. OPERATED THE UNLOCK SWITCH UP, UNLOCKED DOOR AND POSITIONED THE CLOSED SWSDR ABXA2021324029Structure · corrodedWHILE IN C-CHECK, THERE IS CORROSION ON THE INTERIOR STRUCTURE OF THE ALC DOOR, AROUND LIGHTENING HOLES, AROUND NUTPLATE HOLES, AND INSIDE ALL OF THE LIGHTENING HOLES AT THE TOP OF THE ALC DOOR, MARKED. THE CORROSION WAS FOUND TO BE OUT OF LIMITS ON VARIOUS STSDR ABXA2021318030Stringer · crackedWHILE IN C CHECK, FUSELAGE STRINGER 21L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S21L @ FS 676 IAW B767 SRM 53-00-03 REPAIR 2 AND SB #368-53-038SDR ABXA2021316031Stringer · crackedDURING C CHECK, FUSELAGE STRINGER 22L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S22L @ F.S. 676 IAW B767 SRM 53-00-03 REPAIR 2.SDR ABXA2021228017Pca · leakingL HYD QTY LOW EICAS MSG,FLIGHT CREW DECLARED AN EMERGENCY AND EXECUTED AN AIR TURN BACK AND LANDED UNEVENTFULLY. MAINTENANCE DETERMINED #1 SPOILER WAS LEAKING HYDRAULIC FLUID AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED #1 SPOILER PCA OPS CHECK/RIG CHECK GOSDR ABXA2021223016Fseu · faultedTE FLAPS DISAGREE CAUTION MESSAGE RAN THE QRH IN-FLIGHT. TRAILING EDGE DISCREET LIGHT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED BY MAINTENANCE. BITE TESTED FSEU AS PER FIM 27-51 FT 809. EXTRACTED FAULT MSG NO. 27-51102 " L FLAP.STAB POS" PERFOSDR ABXA2021215009Generator · shutdownWHILE ON GROUND AND LEFT ENGINE SHUTDOWN RIGHT GENERATOR DROPPED OFFLINE. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE PERFORMED MANUAL RESET OF #2 ENG. FIELD IAW B767 AMM 24-11-00. RESET SUCCESSFUL. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA202112621Control Panel · defectiveAFTER PUSH BACK, LEFT ENGINE WOULD NOT START DUE TO NO PNEUMATIC AIR. AIRCRAFT BTB AND GROUNDED. REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL PANEL, IAW B767 AMM 36-11-26. OPERATIONS CHECK NORMAL, AIRCRAFT RELEASED.SDR ABXA20200803229Hydraulic System · leakingON TAXI OUT, RIGHT HAND HYDRAULIC FLUID QTY LOSS ON EICAS. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE PLACED HYDRAULIC QTY ON DEFERRAL AND AIRCRAFT RELEASED TO RESUME FLIGHT OPERATIONS.SDR ABXA20200803228Apu · unknownAPU AUTO SHUTDOWN AFTER PUSH BACK, BTB AIRCRAFT GROUNDED BY MAINTENANCE. CHECKED APU ECU, IAW B767 FIM 49-11 FAULT TREE 958, AND FOUND NO MESSAGES. STARTED APU AND RAN FOR .75 HOURS, RAN BOTH PACKS, DRY MOTORED NR 1 ENGINE AND NO DISCREPANCIES NOTED, IAW B76SDR ABXA20200803215Autothrottle Sys · malfunctionedON PUSH, AUTOTHROTTLES WENT INOPERABLE FOLLOWED BY LOSS OF THRUST SETTINGS BEING DELETED. WILL NOT TAKE ANY THRUST SETTINGS. AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED. ACCOMPLISHED OPERATIONS CHECK OF TMS DISPLAY AND TMC, REF AMM 22-31-01, C/W MCDP TESTS 0SDR ABXA20200803216Shutoff Valve · intermittentHOLDING NR 1, SUDDENLY GOT WARM IN COCKPIT. WINDOWS FOGGED, THEN EICAS COMPACTED. BOTH PILOT EADI/EHSI WENT FULL BRIGHT. THEN F/O'S EADI BLANKED. AIRCRAFT BACK TO BLOCK AND GROUNDED. CONDUCTED EQUIPMENT COOLING SYSTEM BIT, IAW B767 FIM 21-58 FT 873, NO FAUSDR ABXA20200803210Line · leakingON TAXI OUT, LT HYDRAULIC SYSTEM LOW QTY EICAS MESSAGE IN VIEW STATUS PAGE SHOWS ZERO QTY. AICRAFT BACK TO BLOCK AND GROUNDED. UPON INSPECTION FOUND LEAKING RETURN LINE FROM EDP IN THE LT PYLON. REMOVED LINE, REPAIRED HYD LINE WITH RYNGLOK, REF B767 MM 20-1SDR ABXA20200803208Autothrottle Sys · malfunctionedSPEED FLAGS ON BOTH CA/FO PED'S. AIRCRAFT BACK TO BLOCKS AND GROUNDED BY MAINTENANCE. RESET TMC FLAG CLEARED. NO MESSAGE, OK FOR SERVICE, FIM 22-32 FT 804. A/C DOWNGRADED TO CAT 1 PENDING 30 + 40 TEST.SDR ABXA20200803207Valve · bindingAFT CARGO OVERHEAT LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE INSPECTED AND DEFERRED SYTEM AIRCRAFT WAS RELEASED FOR FLIGHT.SDR ABXA20200803204Line · crackedINFLIGHT EMGERGENCY DECLARED FOR LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE ON FINAL APPROACH. AIRCRAFT LANDED SAFELY AND WAS TOWED FROM RUNWAY. AIRCRAFT WAS GROUNDED BY MAINTENANCE. T/S & FOUND HYDRAULIC LINE IN RT WHEEL WELL CRACKED FOR SLAT SYSTEM AT S846 SDR UIEA2020100902198Escape Reel · unsecureESCAPE REEL NOT SECURED. RESECURED DESCENT DEVICE, IAW AIA 25-61-03.SDR ABXA20200803185Igniter · failedNO START ON RIGHT ENGINE WITH NR 1 IGNITER, HAD TO PULL BACK TO GATE FOR TRAFFIC. AIRCRAFT GROUNDED. REMOVED AND REPLACED RIGHT ENGINE NR 1 IGNITOR PLUG, IAW AMM 74-21-02. RAN ENGINE IAW AMM 71-00-00 TABLE 501 TEST 3. ENGINE OPERATION CHECK GOOD. DI CLEARSDR UIEA2020092802089Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 783.5, 13R. REPAIRED IAW REA 47416 REA10.SDR UIEA2020092802090Skin · corrodedLT WING UPPER SKIN PANEL CORRODED. REPAIRED CORROSION IAW AMES 47416REA16.SDR UIEA2020092802091Skin · corrodedCORRODED LEADING EDGE SKIN PANEL. REPAIRED IAW REA 47416 REA 04.SDR UIEA2020092802092Stringer Clip · corrodedSTRINGER CLIP AND FRAME WEB CORROSION. REPLACED STRINGER CLIP AND FRAME WEB, IAW B767 SRM 51-40-02 PG 2.SDR UIEA2020092802093Panel · corrodedCORROSION ON BULGE PANEL. REMOVED CORROSION ON BULGE PANEL IAW B767 SRM 53-60-53.SDR UIEA2020092802094Stringer · corrodedCORRODED STRINGER. REMOVED DAMAGE IAW DOCUMENT 47416 REA04.SDR UIEA2020092802095Skin · corrodedCORROSION ON SKIN. REPAIRED SKIN DAMAGE IAW 47416 REA15.SDR UIEA2020092802096Skin · corrodedBULGE IN SKIN (CORROSION). REPAIRED SKIN IAW REA 47416 REA 02.SDR UIEA2020092802097Stringer · corrodedSTRINGER 38R IS CORRODED BETWEEN 1285 AND 1307. REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIRED SECTION, IAW B767 SRM 53-00-03 REPAIR 2.SDR UIEA2020092802098Skin · corrodedCORRODED WING SKIN. REPAIRED IAW REA 47416 REA 20.SDR UIEA2020092802099Splice · corrodedCHORD SPLICE CORRODED. REPLACED CHORD SPLICE, IAW B767 SRM 51-40-02.SDR UIEA2020092802100Structure · corrodedCORRODED SLAT. REPLACED SLAT, IAW B767 AMM 27-81-02.SDR UIEA2020092802101Structure · crackedCRACKED CHORD. REPAIRED CHORD, IAW B767 SRM 51-70-12.SDR UIEA2020092802102Fitting · gougedNR 2 PYLON INBOARD SIDE LOAD FITTING IS GOUGED BEHIND PANEL 447. BLENDED GOUGE ON NR 2 PANEL INBOARD REPAIRED, IAW DOC 47416 REA 03.SDR UIEA2020092802103Skin · bentSKIN BENT AND CREASED. REPAIRED IAW REA 47416 REA 06.SDR UIEA2020092802104Stringer · corrodedSTRINGER AT 35R IN ALC IS CORRODED STA 1285. REPAIRED STRINGER ON 35R IN ALC STA 1285, IAW B767 SRM 51-40-02 REPAIR 2 AND 53-00-03.SDR UIEA2020092802105Skin · corrodedCORROSION ON INTERNAL SKIN STA 783 ABOUT STRINGER 13L. REMOVED CORROSION AND REPLACED SKIN, IAW AMES DOC 47416 REA 49.SDR UIEA2020092802106Skin · corrodedFUSELAGE SKIN CORROSION AT STA 783 STR 12R. REMOVED CORROSION AND REPAIRED, IAW AMES DOC 47416REA10.SDR UIEA2020092802107Skin · damagedFUSELAGE SKIN CREASED AT STA 676 STRINGER 7L. REPAIRED SKIN, IAW AMES DOC 47416 REA 17.SDR UIEA2020092802108Stringer Clip · corrodedCORROSION ON STR 21R AND STA 1502 STRINGER CLIP. REMOVED CORROSION FROM 21R AND STA 1522 STRINGER CLIP. REPLACED CLIP, IAW B767 SRM 53-00-03 AND 51-40-02.SDR UIEA2020092802109Structure · corrodedCORROSION FOUND BETWEEN 1375 AND 1417 S35R-36R. BLENDED CORROSION AND REPAIRED, IAW AMES DOC 47416 REA 13.SDR UIEA2020092802110Stiffener · corrodedSKIN STIFFNER CORRODED BEYOND LIMITS AT STA 1380 TO STA 1410, STR 35R-36R. REPAIRED IAW B767 SRM 53-00-03 DETAIL 2.SDR UIEA2020092802111Tee Fitting · corrodedLT WHEEL WELL STA 955 LBL 97 "T" FITTING HAS CORRSION ON RACK AFT OF LT WHEEL WELL. CORRODED "T" ANGLE FOUND TO BE OUT OF LIMITS, IAW SB 767 53A0100 STEP 9. INSTALLED NEW ANGLE ON EO NR 6753A070 STEP NR 11.SDR UIEA2020092802112Failsafe · crackedLT FAIL SAFE STRAP AT STA 955 LOWER FASTENER HOLE CRACKED. PERFORMED CUT OUT OF FAILSAFE STRAP, IAW BSB SB 53-A0100 FIG 15 + ATLAS 6753A070 (EO).SDR UIEA2020092802113Failsafe · cracked2 EA LOWER BOLT HOLES CRACKED ON RT FAIL SAFE STRAP STA 955 RBL 98. PERFORMED CUT OUT ON FAIL SAFE STRAP, IAW SB 53-A0100 FIG 15 AND ATLAS EO 6753A070.SDR UIEA2020092802114Web · corrodedFLC FLOOR WEB CORROSION AT STA 544 RBL 32. REMOVED AND REPLACED WEB, IAW 51-40-03 AND BOEING DRAWING 143T5200.SDR UIEA2020092802115Support Bracket · corrodedANTENNA AND SUPPORT CORROSION STA 1310 TO 1323. REPLACED CHIP AND SUPPORT BRACKET, REPAIRED IAW 52-60-53.SDR UIEA2020092802116Skin · corrodedCORROSION FOUND LE WING AT LES 897. REPAIRED CORROSION, IAW B767 SRM 57-41-13-2R-1 REPAIR 1.SDR ABXR2020091500104Skin · corrodedCORROSION FOUND ON LEADING EDGE OF WING UNDER PNL 521ZB AT LES 897.00 UNDER 2 NUTPLATES. PERFORMED B767 SRM 57-41-13-2R-1 REPAIR 1 TO REPAIR CORROSION AT WING LES 897.00 THAT WAS 100% EXFOLIATED ON LEADING EDGE OF WING STATION PNL 521ZB.SDR ABXR2020091500102Web · corrodedFLC STA. 544, RBL 32 TOP OF FLOOR WEB IS CORRODED. REMOVED AND REPLACED WEB, IAW B767 51-40-03 AND BOEING DWG 143T5000.
Back to Boeing 767-281