Boeing 767-281
Service difficulty reports · 1,831
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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 ABXR2020091500103Bracket · corrodedWHILE WORKING NR0736, FOUND HF ANTENNA SUPPORT STRUCTURE CORRODED. REMOVED ANTENNA AND SUPPORT STRUCTURE. CHIP AND SUPPORT BRACKET WERE FOUND TO BE OUT OF LIMITS. REPLACED CLIP AND SUPPORT BRACKET. REINSTALLED ANTENNA AND SUPPORT STRUCTURE. ALL IAW B767 SSDR ABXR2020091500101Failsafe · crackedLOWER 2 BOLT HOLES CRACKED ON RT FAIL SAFE STRAP. PERFORMED FAIL SAFE STRAP CUT OUT, IAW SB 53-A0100 AND ATLAS EO NR 6753A070.SDR ABXR2020091500100Failsafe · crackedLOWER FASTENER HOLE CRACKED ON LEFT FAIL SAFE STRAP STA 955. PERFORMED CUT OUT ON FAIL SAFE STRAP, IAW SB 53-A0100 FIG 15 AND ATLAS EO NR 6753A070.SDR ABXR2020091500099Angle · corrodedLT WHEEL WELL STA 955 LBL 97 HAS ANGLE CORRODED BEYOND LIMITS, PER SB767 53A0100. NEW ANGLE TO BE INSTALLED ON EO NR 6753A070 STEP 11.SDR ABXR2020091500098Stiffener · corrodedSKIN STIFFENER CORRODED BEYOND LIMITS, STA 1380 TO 1410, STR 35R-STR 36R. REPAIRED IAW B767 SRM 53-00-03 DETAIL 2.SDR ABXR2020091400097Skin · corrodedCORROSION FOUND BETWEEN FS 1375 AND 1417 STR 35R AND 36R. BLENDED CORROSION BETWEEN STA 1375 TO 1417 STR 35R TO 36R. ORIGINAL THICKNESS .074", REMOVED .041", REMAINING T .033" FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT. RECEIVED AMES DOC 4741SDR ABXR2020091400096Stringer Clip · corrodedCORROSION ON STR 21R JUST AFT OF FUS STA 1502. REMOVED CORROSION FROM S21R AND STA 1502 STRINGER CLIP. 100% MATERIAL LOSS. MATERIAL IS FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-03 ADI. REPLACED STRINGER CLIP IAW B767 SRM 51-40-02 PG 7.SDR ABXR2020091400095Skin · damagedFUSELAGE SKIN IS CREASED AT STA 676 STRINGER 7L. FUSELAGE SKIN CREASED AT STA 676 7L FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-01 DETAIL III. REPAIRED AREA IAW AMES DOCUMENT #47416REA17.SDR ABXR2020091400094Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13R. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12R, IAW B767 200 SRM 53-00-01 AD 1. WITH 0.027" MAT LOSS, DAMAGE EXCEEDED 15% ALLOWED & FOUND TO BE OUT OF LIMITS. REPAIRED DSDR ABXR2020091400093Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13L RUNNING NEXT TO TEAR STRAP. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12L, IAW B767-200 SRM 53-00-01 AD1. WITH 0.002" MAT LOSS, DAMAGE FOUND TO BE BEYOND 15% ALLOWED AND SDR ABXR2020091400092Stringer · corrodedSTRINGER 35R IN ALC IS CORRODED AT STA 1285. CUT OUT AND REPAIR DAMAGED SECTION STR 35R IN ALC AT STA 1285 DUE TO EXFOLIATION CORROSION ALL, IAW B767 SRM 51-40-02 & 53-00-03 REPAIR 2.SDR ABXR2020091400091Skin · damagedNR 1 PYL INBOARD SKIN IS BENT AND CREASED AT NAC STA 240. MARKED NR 1 PYLON INBOARD SKIN AT NAC STA 240, FOUND TO BE OUT OF LIMITS IAW B767 SRM 54-51-01. ALLOWABLE DAMAGE 1 DETAIL III. REPAIRED BLENDED AREA, IAW REA NR 47416REA06.SDR ABXR2020091400090Fitting · gougedNR 2 PYL INBOARD SIDE LOAD FITTING IS GOUGED BEHIND PANEL 447AL. MARKED. BLENDED GOUGE ON NR 2 PYLON INBOARD SIDE LOAD FITTING. NOMINAL .500, REMOVED .134 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-20-90 AD 1. REPAIRED AREA IAW AMES DOC 47416REA03.SDR ABXR2020091400089Structure · crackedNWW RIGHT HAND STA 287 RBL 25 VERT CHORD CRACKED NEXT TO FASTENER HEAD. REPAIR CHORD IAW BOEING 767 SRM, IAW BOEING 767 SRM 51-70-12 FIG 1 SHEET 1-7. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL SHEET 10 AND BOEING DRAWING 141T2938.SDR ABXR2020091400088Wedge · corrodedRIGHT WING NR 9 SLAT UPPER WEDGE INNER IS CORRODED IN SEVERAL AREAS. NR 9 SLAT FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED NR 9 SLAT WITH SERVICEABLE UNIT, IAW B767 AMM 27-81-02 PARA 3, H.SDR ABXR2020091400087Angle · corrodedRIGHT WING NR 8 SLAT CORRODED AT THE TIA ATTACH POINT TO SLAT. BLENDED CORROSION ON CHORD SPLICE ANGLE ON NR 8 SLAT AT TAI ATTACH POINT. REMOVED .020 FROM NOMUAL .100 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-43-02 FIG 101 DETAIL V. REMOVED AND REPLACED ASDR ABXR2020091400086Skin · delaminatedRIGHT WING UPPER TRAILING EDGE SKIN PANELS AT STA 798 AND 906 NEAR OUTBOARD FLAP OUTBOARD AREA AND NEAR NR 12 SPOILER BOARD, HAVE AREAS WITH SKIN BULGING AND FASTENERS PULLING THRU SKIN. REMOVED AND REINSTALLED RT WING TRAILING EDGE UPPER SKIN PANEL AFTER COMSDR ABXR2020091400085Stringer · corrodedALC STRINGER 38R IS CORRODED BETWEEN STA 1285 AND 1307. STRINGER CORROSION AT 39R IS FOUND TO BE EXFOLIATED COMPLETELY THROUGH. REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR SECTION, IAW B767 SRM 53-00-03 REPAIR 2.SDR ABXR2020091400084Skin · corrodedBULGE IN SKIN AT FS 1395 AND STR 35L. REPAIRED SKIN AT FS 1395 S35L, IAW AMES REA 47416 REA 02 AND B767 SRM 53-00-01 REPAIR 12.SDR ABXR2020091400083Skin · corrodedCORROSION ON SKIN AT FASTENER FS 785 STR 38R. REMOVED CORROSION FROM SKIN AT FS 785 STR 38, IAW B767 200 SRM 53-00-01 FIG 1 DET II WITH ORIG MAT 0.150", MAT LOSS 0.052". FOUND TO BE OUT OF LIMITS, IAW B767 200 SRM 53-00-01. REPAIRED SKIN DAMAGE IAW 47416REASDR ABXR2020091400082Skin · corrodedDEFORMITY IN THE SKIN LEFT OF NLG DOOR ON FS 188.5 10" FROM DOOR OPENING. REMOVED DAMAGE AT STA 196.5 10" FROM DOOR OPENING AND REPAIRED, PER AMES DOCUMENT 47416REA07.SDR ABXR2020090900081Panel · corrodedBILGE PANEL CORRODED.SDR ABXR2020090900080Frame · corrodedSTRINGER CLIP AND FRAME WEB CORROSION.SDR ABXR2020090900079Skin · corrodedCORRODED LEADING EDGE SKIN PANEL.SDR ABXR2020090900078Skin · corrodedLT WING UPPER SKIN PANEL.SDR ABXR2020090900077Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN AT BS 783, STRINGER 13 RIGHT.SDR ABXA2020090283168Actuator · wornAFTER PUSHBACK AND ENGINES STARTED EICAS MESSAGE AILERON LOCKOUT DISPLAYED, AIRCRAFT RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED. T/S IAW B767 FIM 27-11 FT 804 FAULT CONFIRMED BAD LT AILERON LOCKOUT ACTUATOR. REMOVED AND REPLACED LT AILERON LOCKOUT ACTUATOR, ISDR ABXA202009318167Warning Flag · false activationSPEED FLAG APPEARED ON ATTITUDE INDICATOR. AIRCRAFT WAS GROUNDED. CYCLED THRUST MANAGEMENT COMPUTER C/BS F-14,15, SPEED FLAGS DISAPPEARED PER FIM 22-32-00 A/C RALM STATUS DOWN GRADED TO CAT 1.SDR ABXA202009038169Seat Track · corrodedCORROSION WAS FOUND ON THE INBOARD FLANGE OF AFT LOWER CARGO COMPARTMENT SEAT TRACK (P/N: 96FS667842-107) AT STA 1307, RBL 15.01. THE DAMAGE WAS REMOVED BY BLENDING. ORIGINAL FLANGE THICKNESS IS .080 AND MINIMUM REMAINING THICKNESS IN THE BLENDED AREA IS .03SDR ABXA20200903 172Panel · gougedGOUGE DAMAGE WAS FOUND ON THE STRUT SKIN PANEL (P/N 311T1400-21) OF THE LT PYLON. THE GOUGE WAS REMOVED BY BLENDING, PER 767-200 SRM 51-10-02 EXCEEDING SRM LIMITS. ALL FASTENERS COMMON TO REWORKED AREAS, AS REQUIRED, WERE REMOVED AND HFEC OPEN-HOLE AND SURFASDR ABXA202009038173Support Fitting · corrodedDURING AIRCRAFT C-CHECK AT TAMPA, AIRBORNE MAINTENANCE WAS REQUIRED TO INSPECT THE NR 8 FLAP SUPPORT 1-3 BEAM ASSEMBLY PER ABX WORK CARD ABX-57-796-28-02. INSPECTION REVEALED CORROSION WITHIN A HOLE LOCATION. THE SUBJECT HOLE WAS REWORKED TO A CLEAN AND ROUNSDR ABXA20200803171Door Sill · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TPA), CORROSION WAS FOUND ON THE AFT LOWER CARGO DOOR CUTOUT LOWER SILL FAIL SAFE STRAP (P/N 146T8048-3), BETWEEN STA 1241 AND STA 1263 AT STRINGER S-33R. THE CORROSION WAS REMOVED AND EVALUATED PER 767-200 53-00-15 SDR ABXA20200813163Aileron Sys · lack of lubeAILERON'S STIFF AND WILL NOT RETURN TO CENTER. AIRCRAFT WAS GROUNDED. CLEANED AND LUBE ROD BEARING. C/W INSPECTION FOR AILERON PULLEYS, ALL CHECKS NORMAL. LUBED AILERON PULLEYS AS PRECAUTIONARY. C/W OPS CHECK. AILERON ZERO OUT ON BOTH LH AND RH YOLK. REF AMM 2SDR UIEA2020081711749Sensor · failedL ENG HI STAGE EICAS MSG DURING CLIMB. REMOVED AND REPLACED FAN AIR TEMP SENSOR IAW AMM 36-11-17. OPS CK GOOD.SDR ABXA202009038170Skin · corrodedWHILE PERFORMING THE SCRIBE LINE INSPECTION, PER ABX TASK CARD ABX-SCL-5330-0016-23145 REFERENCE AD 2010-06-16 AND BOEING SB 767-53A0193, CORROSION WAS FOUND ON THE FUSELAGE SKIN (P/N 146T3330-41 ASSY) IN ZONE A AT STRINGER S-17L BETWEEN STA 1395 AND STA 1417.SDR ABXA20200803159Display · malfunctionedLOWER EICAS SCREEN WOULD NOT DISPLAY THE FLIGHT CONTROL PAGE. AIRCRAFT WAS GROUNDED.SDR ABXA202008053156Warning Message · illuminatedFORWARD CARGO DOOR EICAS MESSAGE ON DISPLAY.AIRCRAFT WAS GROUNDED.SDR ABXA20200803154Pump · failedLEFT ENGINE HAD NO FUEL FLOW ON START. AIRCRAFT WAS GROUNDED.SDR ABXA20200713125Actuator · failedR ENG FUEL VAL EICAS MSG. AIRCRAFT WAS GROUNDED.SDR ABXA20200710123Duct · rupturedAFTER ENGINE START, OVERHEAT (OVERHEAD LIGHT) ILLUMINATED ON EQUIPMENT COOLING PANEL WITH ASSOCIATED EICAS MESSAGE FORWARD EQUIPMENT COOLING OVERHEAT. VERY LOW AIRFLOW THROUGH AC GASPERS. AIRCRAFT WAS GROUNDED.SDR ABXR2020070200034Trunnion · corrodedRT MLG FORWARD TRUNNION WAS CORRODED IN THE LOWER SUPPORT ASSEMBLY BUSHING SHOULDER. REMOVED CORROSION AND INSTALLED OVERSIZED BUSHING PER 47401REA18 WITH 8100-9 BY AR-831084. REFERENCE NR 123447.0007SDR ABXA202006296099Sensor · defectiveLEFT ENGINE SLOW TO SPOOL WITH SOME STRANGE INDICATION COMPARED TO RIGHT ENGINE WITH N1'S MATCHED N2 (LEFT ENGINE) IS 10% HIGHER, OIL TEMP IS 10 DEGREES C HIGHER, OIL PRESSURE IS 10 PSI HIGHER AND N1 SHOWS A COMMAND BOX INDICATION FUEL FLOW WAS SLIGHTLY HIGHERSDR ABXA202006296098Warning Light · illuminatedRUDDER RATIO LIGHT AND MESSAGE DISPLAYED ON PUSH BACK. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062419070Warning Message · illuminatedL ENG STARTER EICAS MESSAGE ILLUMINATED DURING ENGINE START. AIRCRAFT WAS GROUNDED.SDR ABXA202006182067Egt Indication · activatedAFTER STARTING #2, EGT INDICATOR DROPS TO 18C IN BOTH PRIMARY AND STBY DISPLAYS.AIRCRAFT WAS GROUNDED.SDR ABXA2020061105066Warning Light · illuminatedAFTER ENG. START THE F/O PITOT DISCREET LIGHT REMAINED ILLUMINATED WITH F/O PITOT EICAS MESSAGE DISPLAYED. AIRCRAFT WAS GROUNDED.SDR ABXA20200603065Valve · malfunctionedLEFT BLEED AIR ISOLATION VALVE LIGHT STAYS ON. AIRCRAFT WAS GROUNDED.SDR ABXA20200522119Angle · crackedNR 2 PYLON AFT FAIRING UPPER INBD AND OUTBD ANGLES CRACKED. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522118Angle · wornNR 2 OTBD FWD ZEE ANGLE WORN. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522117Structure · corrodedFORWARD CARGO COMPARTMENT DOOR INNER SKIN 2ND FROM BOTTOM CORRODED MINOR CHORD AND ASSOCIATED PARTS. THE AIRPLANE WAS GROUNDED.
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