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 ABXA201004120051Stringer · crackedCENTER WING UPPER STRINGER U-1C AFT BAY OF CENTER DRY BAY HAS A 10 INCH CRACK AT LBBL 87 APPROX AT FSS 945. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER U-1C IAW 767 SRM 57-00-03 REPAIR 1 FIGURE 201.SDR ABXA201004120050Structure · crackedNOSE WHEEL WELL VERTICAL CHORD AT RBL 25 STA 287 IS CRACKED IN RADIUS LOCATED 11.5 INCHES BELOW W/W CEILING. CRACK IS APPROX .437 INCH IN LENGTH. REPAIRED VERTICAL CHORD IAW 767 SRM 51-70-12.SDR ABXA201004120049Structure · crackedNOSE WHEEL WELL VERTICAL CHORD AT LBL 25 STA 287 IS CRACKED IN RADIUS LOCATED 11.5 INCHES BELOW CEILING. CRACK IS APPROX .625 INCH IN LENGTH.SDR ABXA201004120046Skin · chafedNR 1 NACELLE STRUT, FWD TORQUE BOX, OUTBOARD SKIN HAS 2 SMALL CHAFE AREAS JUST BELOW ACCESS PANEL 432AL. REPAIRED IAW REA B654-58718.SDR ABXA201004120045Skin · chafedNR 1 NACELLE STRUT FWD TORQUE BOX OUTBOARD SKIN HAS TWO LONG CHAFES AT METAL STRIP FOR T/R SEAL. REPAIRED IAW REA B654-58712-MR.SDR ABXA201004120044Fitting · corrodedCORROSION ON FIXED LEADING EDGE LOWER SIDE JUST OUTBOARD OF OUTBOARD SLAT DRIVE UNIT NR 5 SLAT WS 500. REMOVED AND REPLACED LEADING EDGE ANGLE IAW 767 SRM 51-40-02.SDR ABXA201004120043Rib · corrodedCORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST OUTBOARD OF INBOARD AUX TRACK NR 2 SLAT WS 879. REMOVED AND REPLACED RIB IAW 767 SRM 51-40-2.SDR ABXA201004120042Rib · corrodedCORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST INBOARD OF OUTBOARD AUX TRACK NR 2 SLAT WS 934. REMOVED AND REPLACED FIXED LEADING EDGE RIB IAW 767 SRM 51-40-02.SDR ABXA201004120041Rib · corrodedCORROSION AT FIXED LEADING EDGE RIB LOWER SIDE JUST INBOARD OF OUTBOARD AUX TRACK NR 3 SLAT WS 722. REMOVED AND REPLACED RIB IAW 767 SRM 51-40-02.SDR ABXA201004120040Intercostal · corrodedINTERCOSTAL AT RBL 16.4 BETWEEN STA 610 AND 632 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW 767 SRM 51-4-02.SDR ABXA201004120039Stringer · corrodedFOUND 2 AREAS OF CORROSION ON STRINGER 38L BETWEEN STA 412 AND 434. REMOVED AND REPLACED FITTING. INSTALLED WITH HI-LOKS IAW 767 SRM 53-02.SDR ABXA201004090038Floorbeam · crackedDURING CARGO CONVERSION FOUND CORROSION AND 2.5 INCH CRACK ON UPPER CHORD OF FLC FLOORBEAM AT STA 632 RBL 15 TO RBL 20. REPAIRED CHORD IAW B767 SRM 53-00-7.SDR ABXA201003260013Skin · corrodedDISCOVERED CORROSION ON WING SKIN UNDER RIGHT WING PANEL P/N 113T1655-22 APPROX RT WING WS 916.75. REPAIRED AREA IAW REA'S B657-58728, B657-58729 AND B657-58730.SDR ABXA201003290032Structure · crackedNWW LT VERTICAL CHORD STA 287 LBL 25 HAS A CRACK APPROX 11.5 DOWN, 1.25 LONG. REPAIRED DAMAGED AREA IAW SRM 51-70-12 FIG 1. P/N 141T2938-15.SDR ABXA201004120048Rib · corrodedCORROSION AROUND NUT PLATE ON RIB NOSE FOR NR 4 SLAT INBOARD AUX TRACK APPROX. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02.SDR ABXA201003260014Flap · damagedRIGHT I/B FLAT BOTTOM OF TRAILING EDGE HAS 3 FASTENERS PULLED THRU. REMOVED AND REPLACED RIGHT I/B MAIN FLAP IAW 767 AMM 27-51-03-4.SDR ABXA201003260018Stringer · corrodedCENTER HORIZ STAB SECTION INTERIOR STRINGER 9 CORRODED AT RIGHT TOP FORWARD SIDE WHERE IT ATTACHES TO R/B 2 RIGHT. REPAIRED IAW 767 SRM 55-10-03 FIG 201 REPAIR 1 AND REA B655-58683-MR.SDR ABXA201003250012Structure · crackedLBL 25 NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED. REPLACED LBL 25 VERTICAL CHORD AT STA 287 IAW 767 SRM 51-70-12 FIG 1 SH 4.SDR ABXA201003250011Structure · crackedRBL 25 NOSE WHEEL WELL VERTICAL CHORD IS CRACKED. REPAIRED VERTICAL CHORD AT RBL 25 IAW 767 SRM 51-70-12 FIG 1 SH 4.SDR ABXA201003260017Attach Angle · corrodedFWD ATTACH ANGLE ON THE PANEL SUPPORT FOR 197 CL & DL IS CORRODED BELOW HYD LINES. REMOVED AND REPLACED FWD ATTACH ANGLE IAW B767 SRM 51-04-02.SDR ABXA201002090007Bracket · out of positionDURING CLIMB "MAIN CARGO DOOR" LIGHT ILLUMINATED AT FL350. INSPECTED MAIN CARGO DOOR NO DEFECTS NOTED. PLACED DOOR INDICATION SYSTEM ON DI 65443 PER B767 MEL 52-71-1-2 AND COMPLIED WITH MAINTENANCE PROCEDURES. DOOR VERIFIED CLOSED AND LOCKED. PERFORM MAIN SDR ABXA201002080006Warning System · malfunctionedON DESCENT MN CARGO DOOR ILLUM. PRESS REMAINED NORMAL. INSPECTED MAIN CARGO DOOR SWITCHES. NO DEFECTS NOTED. OPENED AND CLOSED DOOR SEVERAL TIMES AND DOOR WARNING INDICATES NORMAL PER AMM 52-32-00-5.SDR ABXA201003250010Failsafe · crackedLT FAIL SAFE STRAP CRACKED HORIZONTALLY AT LWR THRU BOLT OF INSP AREA. FAIL SAFE STRAP REPAIRED IAW REA B653-5868MR.SDR ABXA201003250009Failsafe · crackedRT FAIL SAFE STRAP CRACKED HORIZONTALLY AT LWR THRU BOLT OF INSP AREA. CRACK REPAIRED IAW REA B65-58685MR.SDR ABXA2010032615Thrust Reverser · crackedRT ENGINE OUTBOARD T/R 2ND CASCADE SECTION FROM BOTTOM CRACKED TOWARD FORWARD SECTION. REMOVED AND REPLACED RT OUTBOARD T/R.SDR ABXA201001060002Warning System · malfunctionedCLIMBING OUT OF FL 180 MAIN CARGO DOOR LIGHT ILLUMINATED ACCOMPLISHED NON NORMAL PROCEDURE. DEFERRED MAIN DECK CARGO DOOR IAW ABX AIR MEL 52-71-1-2 MAINT PROCEDURE COMPLIED WITHIN 2-52-71-1-10 AND 52-71-1. MBCB 01-06-10 CAT C CODE 11 PLACARD INSTALLED (MUST SDR ABXA201001060001Warning System · malfunctionedMAIN CARGO DOOR LIGHT ON OUT OF FL280 PERFORMED NON NORMAL PROCEDURE. INSPECTED MAIN CARGO DOOR, NO DEFECTS NOTED OPERATED MAIN CARGO DOOR SEVERAL TIMES, SYSTEM CHECKS NORMAL.SDR ABXA200911250069Power Supply · dischargedGALLEY AREA CENTER EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY, OPS CHECKS OK.SDR ABXA200911180066Switch · out of adjustMAIN CARGO DOOR LIGHT ILLUMINATED W/SIREN AT 29000 FT MSL. ACCOMPLISHED ABNORMAL. PRESSURIZATION NORMAL. LIGHT EXTINGUISHED AT 15000 FT MSL. ADJUSTED DOOR DOWN SWITCHES S9019 AND S9020 IAW B767 AMM 52-71-09. DOOR WARNING CHECKS GOOD.SDR ABXA200911170065Switch · out of adjustMAIN CARGO DOOR LIGHT ILLUMINATED W/SIREN AT 29000 FT MSL. ACCOMPLISHED ABNORMAL. PRESSURIZATION NORMAL. LIGHT EXTINGUISHED AT 15000 FT MSL. ADJUSTED DOOR DOWN SWITCHES S9019 AND S9020 IAW B767 AMM 52-71-09. DOOR WARNING CHECKS GOOD.SDR ABXA200911170064Warning System · false activationLEAVING CRUISE ALTITUDE "MAIN CARGO DOOR" LIGHT W/SIREN COME ON. PRESSURIZATION NORMAL. ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AT 12000FT MSL. PERFORMED INSPECTION MAIN CARGO DOOR INDICATION SYSTEM IAW B767MM 52-71-09-2. SYSTEM CHECKS NORMAL.SDR ABXA200911170063Mec · malfunctionedLEFT ENGINE FLAMED OUT AT APPROXIMATELY 1,000 AGL AFTER VNAV SELECTED. RE-LIGHT OF LEFT ENGINE SUCCESSFUL. (WHEN VNAV IS SELECTED THIS CHANGES THE THRUST PROFILE. FLAME OUT OCCURRED AS THROTTLES CAME BACK.) INSPECTED SUMPS AND FOUND NO WATER. FUEL FILTERSSDR ABXA200910300060Structure · crackedNOSE WHEEL WELL VERTICAL CHORD AT LBL 25 AND STA 287 IS CRACKED IN RADIUS APP .687 INCH IN LENGTH. LOCATED 11.5 INCHES BELOW W/W CEILING PNL. REPAIRED VERTICAL CHORD AT LBL 25 AND STA 287 IAW B767 SRM 51-70-12.SDR ABXA200910300059Structure · crackedNOSE WHEEL WELL VERTICAL CHORD AT RBL 25 AND STA 287 IS CRACKED IN RADIUS- APP .625 INCH IN LENGTH. LOCATED 11.5 INCHES BELOW W/W CEILING PNL. REPAIRED VERTICAL CHORD IAW B767 SRM 51-70-12.SDR ABXA200910300058Jackscrew · corrodedAREA OF DISTORTION ON BALL SCREW THREAD AND SMALL SPOT OF CORROSION ON BOTTOM THREAD OF JACKSCREW. REMOVED AND REPLACED HORIZONTAL STAB JACKSCREW IAW B767 AMM 27-41-4.SDR ABXA200910300057Fitting · crackedFORWARD LOWER CARGO DOOR CUTOUT CENTER HORIZONTAL ROLLER GUIDE FITTING CRACKED. CRACK LENGTH 4.5 INCH. ROLLER FITTING MISSING ALL 4 BOLTS (PUT TOGETHER WITH PIN). REMOVED AND REPLACED FITTING IAW B767-200 SRM 51-40-02.SDR ABXA200910300056Cowling · crackedNR 2 ENG O/B FAN COWL IS CRACKED ON EXTERIOR SURFACE AFT OF STATIC SENSE PORT. CRACK LENGTH 4 INCHES. REMOVED NR 2 ENG O/B COWL. REPAIRED ON WO 10074-0006. RE-INSTALLED NR 2 ENG O/B COWL REF AMM 71-11-04.SDR ABXA200910220055Probe · obstructedF/O'S AIRSPEED INDICATED 0, CAPT'S WAS READING 80 ON TAKEOFF, (ABORTED) AT 90 KNOTS CAPT'S AIRSPEED. F/O READS APPROX 65 KNOTS. REMOVED F/O'S PITOT STATIC PROBE, FOUND SMALL OBSTRUCTION, CLEANED PER 767 AMM 34-11-01-7. REINSTALLED F/O'S PITOT STATIC PROBE PSDR ABXA200910180052Unknown · malfunctionedON APPROACH FROM FLAPS 28-30 DISAGREE EICAS MESSAGE - GO AROUND SLAT PERFORMED - NON NORMAL PROCEDURE OPERATIONAL SATISFACTORY. LOWERED FLAP AND SLAT INSPECT THE ENTIRE FLAP AND SLAT FOUND EVERYTHING FINE AND NORMAL. NO DAMAGE, DID THE BITE TEST ON FSCU PER SDR ABXA200910160053Window · malfunctionedLEFT SIDE OF CAPTAIN'S INSTRUMENT PANEL PRODUCING A STRONG BURNING ODOR, NO SMOKE OR VAPOR SEEN. LT 2 & RT 2 WINDOWS REPLACED.SDR ABXA10150051Fire Detector · malfunctioned26-11-05-01 FIRE PROTECTION SYSTEM FAIL LIGHT ILLUM EICAS MSG: FIRE/OVHT SYS DISPLAYED, ENG FIRE LP2 DISPLAYED. "OCCASIONALLY INTERMITTENT FIRE WARNING IN TURBULENCE." REMOVED AND REPLACED L ENGINE DETECTOR CARD ASSY IAW MM 26-10-1-4. REMOVED AND REPLACED ASDR ABXA200910020049Battery Pack · dischargedBOTH EMERGENCY LIGHT BATTERIES ARE DEAD. REMOVED AND REPLACED BOTH EMERGENCY LIGHT BATTERY PACKS IAW B767 AMM 33-51-07-2.SDR ABXA200909240045Duct · leaking09/16/09 - 26-11-02-01 L ENG FIRE LP2 - TROUBLESHOT, NO FAULTS FOUND - RESISTANCE GOOD FOR ALL LOOP 2 DETECTORS. FWD LWR LOOP CHAFING, REPOSITIONED LOOP. 09/17/09 - 26 11 02 01 L ENG FIRE LP2 - DEFERRED. T/S SWAPPED FIRE DETECT CIRCUIT CARD. 09/18/09 WORKISDR ABXA200908280043Flashlight · defectiveCOCKPIT EMERGENCY FLASHLIGHT IS DIM. REMOVED & REPLACED COCKPIT EMERGENCY FLASHLIGHT, OPS CHECKED GOOD.SDR ABXA200907230035Connector · not seatedEMERGENCY EXIT LIGHT OVER R1 DOOR WILL NOT TEST. RESEATED ELECTRICAL CONNECTOR 9084. EMERGENCY EXIT LIGHT OPS CK GOOD.SDR ABXA20090715Battery Pack · dischargedEMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED UPPER EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.SDR ABXA200907130032Stringer · crackedNOSE WHEELWELL CHORD STA 287, RBL 25 IS CRACKED. FOUND WITH HFEC.SDR ABXA07130031Stringer · crackedNOSE WHEELWELL STRINGER STA 287, LBL 25 IS CRACKED. FOUND WITH HFEC.SDR ABXA200905300029Rib · corrodedL/E RIB HAS EXFOLIATION O/B SIDE BY TAI DUCT APPROX LES 456. REMOVED AND REINSTALLED NEW RIB IAW B767 SRM 51-40-02.SDR ABXA200905300028Structure · corrodedTWO SPOTS OF EXFOLIATION ON UPPER L/E STRUCTURE APPROX LES 466. REPAIRED IAW REA B625-58391.
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