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 ABXA20130501429Actuator · failed27 81 05 00 EICAS MSG L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. UPON WALK AROUND MAINTENANCE FOUND THE NUMBER 8 SLAT INBOARD PORTION EXTENDED AND OUTBOARD PORTION RETRACTED. FURTHER INVESSDR ABXA20130423426Tee Fitting · corrodedCORROSION ON UPPER RIGHT WING TRAILING EDGE PANEL ATTACH TEE-CAP FROM WING REAR SPAR TO TRAILING EDGE AT WING STA 434. INSTALLED NEW WING CHORD IAW B767 SRM 51-40-02 PARA 4, 7 AND 9. AIRCRAFT WAS GROUNDED.SDR ABXA20130415424Skin · delaminatedDURING SERVICE CHECK FOUND LEFT OUBOARD AILERON SHOWING APPROX 12 INCHES OF DELAM ON LOWER SKIN TRAILING EDGE. REMOVED AND REPLACED LEFT OUTBOARD AILERON PER 27-11-02-4, ACFT WAS GROUNDED.SDR ABXA20130410423Skin · separatedRIGHT OUTBOARD AILERON UPPER SURFACE SKIN SEPERATED AND PEELED BACK. RIGHT OUTBOARD AILERON REPLACED. REMOVED AND REPLACED RIGHT OUTBOARD AILERON, ACFT WAS GROUNDED.SDR ABXA20130308412Contact · dirtyEXTERIOR EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. CLEANED CENTER CONTACT IN LIGHT SOCKET ASSEMBLY OPS CHECK GOOD IAW B767 AMM 33-51-00, ACFT WAS GROUNDED.SDR ABXA20120209383Strap · crackedLOWER FASTNER HOLE COMMON TO THE LEFT WHEEL WELL FAILSAFE STRAP AND "T" FITTING HAS .500 CRACK AND CORROSION AROUND THE HOLE AT STA 955. NEW FAILSAFE STRAP INSTALLED ON AMES DOCUMENT 47008ORD11, ACFT WAS GROUNDED.SDR ABXA20120208388Strap · corrodedCORROSION MIGRATING BETWEEN FAIL SAFE STRAP AND SKIN AT FAILSAFE STRAP TRIM OUT AT STA 955 LEFT SIDE. NEW FAILSAFE STRAP P/N 145T2524021 MATCH DRILLED IAW B767-200 SRM 51-10-02. NEW FAILSAFE STRAP INSTALLED ON AMES DOCUMENT 47008ORD11, ACFT WAS GROUNDED.SDR ABXA20120121387Tee Fitting · corrodedLEFT "TEE" FITTING CORRODED AT THE LOWER ATTACH HOLE COMMON TO THE FAILSAFE STRAP AT STA 955. HOLES MATCH DRILLED ON NEW "TEE" FITTING VERTICAL LEG IAW B767 SRM 51-10-02. AMES DOCUMENT 47008ORD11 STEP 42, ACFT WAS GROUNDED.SDR ABXA20120207395Structure · corrodedLEFT SIDE FRAME (PICKLE FORK) SEVERAL AREAS OF CORROSION, ON FORWARD MATING SURFACE COMMON TO REAR SPAR PAD AREA. REPAIRED AREAS OP CORROSION AS SPECIFIED IAW WITH AMES DOCUMENT 47033REA06. SPOT FACES 2.9" 5 EA 125R, DEPTH .020, 2EA 2.5" .125R, DEPTH .020 ARSDR ABXA20120207382Strap · crackedRIGHT FAILSAFE STRAP CRACKED LWR BOLT HOLE COMMON TO "T" FITTING AREA. FOUND DURING HIGH FREQ EDDY CURRENT INSP IAW B767 NATM 51-00-19. ALSO CONFIRMED WITH BORESCOPE. REMOVED AND REPLACED FAILSAFE STRAP IAW AMES DOCUMENT 47008ORD12, ALONG WITH EA 53500014-0SDR ABXA20120204394Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 955 S23L AROUND 3 HOLES COMMON TO THE "TEE" FITTING, AND AN AREA AT THE BOTTOM OF THE SKIN 3" FWD. REPAIRED AREAS OF CORROSION IAW JC #EA53500013-004 AND REA #47033REA04, ACFT WAS GROUNDED.SDR ABXA20120202393Structure · corrodedCORROSION FOUND ON THE INBOARD AND OUTBOARD FACE OF RIGHT PICKLE FORK LEG. REMOVED CORROSION FROM INBOARD AND OUTBOARD FACE OF RIGHT PICKLE FORK LEG PICKLE FORK LEGS IAW B767 SRM 53-50-08, PERFORMED ULTRASONIC THICKNESS INSPECTION OF BLENDED AREAS IAW B767 NDSDR ABXA20120202392Frame · crackedRIGHT SIDE FRAME FITTING OUTBD SIDE HAS A 5/16 OBLONG HOLE, AND SHOWS A CRACK INDICATION. REAMED HOLE TO CLEAN AND ROUND IAW B767 SRM 51-40-05, COMPLIED WITH REA #47033REA05 AND REA #47033REA05, NO CRACK FOUND. ACFT WAS GROUNDED.SDR ABXA20120129391Skin · corrodedCORROSION STA 955 RIGHT SIDE INNER SKIN SURFACE, AROUND 3 EA 7/16" HOLES COMMON TO FAILSAFE TRIM OUT AREA AND 3 EA ADJACENT FWD 9/16" HOLES COMMON TO SIDE FRAME FITTING AND FAILSAFE. REPAIRED SKIN IAW JC# EA-53500014-004 AND REA 47033REA01, ACFT WAS GROUNDED.SDR ABXA20120122398Spar · damagedLEFT SIDE FRAME FASTENER HOLES COMMON TO REAR SPAR WEB. HOLES NR 1, 2, 3, 12, 13 ,17, 19, 20 BEYOND BLUE PRINT LIMITS REF DOC 47008ORD05 FIG 3 REV A. REAMED HOLE TO 1/64 OVERSIZE IAW B767 SRM 51-40-05, ACFT WAS GROUNDED.SDR ABXA20120122397Spar · damagedDURING LEFT SIDE REPAIR (PICKLE FORK) REPAIR FOUND LEFT WING ROOT AREA AT REAR SPAR HAS WEB SECTION WITH A FASTENER HOLE NR 3 BEYOND BLUE PRINT LIMITS REF: DOC 47008ORD05 FIG 4 REV A. OVERSIZED HOLES TO 1/64 OR 1.015" IAW B767 SRM 51-40-05, ACFT WAS GROUNDED.SDR ABXA20120122396Structure · corrodedLEFT SIDE FRAME FITTING (PICKLE FORK) HOLES NR 10 & 11 HAS CORROSION IN THEM. REAMED HOLES TO 1/64 OVERSIZE 1.015 IAW B767 SRM 51-40-05, ACFT WAS GROUNDED.SDR ABXA20120128384Tee Fitting · corrodedRIGHT "TEE" FITTING CORRODED AT THE LOWER ATTACH HOLE COMMON TO THE FAILSAFE STRAP AT STA 955. HOLES MATCHED ON NEW "T" FITTING VERT LEG, IAW B767 SRM 51-10-02.P 42, AIRCRAFT WAS GROUNDED.SDR ABXA20120113381Fitting · corrodedSTA 1809.5 RIGHT STRINGER 10 END FITTING HAS CORROSION IN (1/2") ATTACH BOLT HOLES. REMOVED AND REPLACED S10R END CAP FWD OF STA 1809.5 IAW REA B653-60437-MR. ACFT WAS GROUNDED.SDR ABXA20120112380Fitting · corrodedSTA 1809.5 LEFT STRINGER 3 (1/2") END FITTING THRU HOLES HAVE CORROSION INCLUDING WEB AND CHORD. REMOVED AND REPLACED S3L STA 1809.5 FWD SECTION END CAP IAW REA B653-60437-MR AND ON REA B653-60437-MR, ACFT WAS GROUNDED.SDR ABXA20120112379Fitting · corrodedSTA 1809.5 LEFT STRINGER 4 (1/2") END FITTING INBOARD HOLE HAS CORROSION INBOARD AND OUTBOARD HOLES THRU WEB AND CHORD. ALSO HAVE CORROSION. REMOVED AND REPLACED S4L END CAP FWD OF STA 1809.5 IAW REA B653-60437-MR, ACFT WAS GROUNDED.SDR ABXA20120112378Fitting · corrodedSTA 1809.5 LEFT STRINGER 8 AND FITTING (1/2") BOLT HOLES THRU FITTING AND CHORD HAVE CORROSION. REMOVED AND REPLACED S8L END CAP FORWARD OF STA 1809.5 IAW REA B653-60437-MR AND REA B653-60437-MR, ACFT WAS GROUNDED.SDR ABXA20120103377Unknown · odorA STRONG BURNING ODOR COMING THROUGH THE A/C POSSIBLY THE RT PACK. RAN THE LT & RT PACKS FOR ONE HOUR THROUGH HOT AND COLD RANGE PER AMM 21-00-00-2, ACFT WAS GROUNDED. FOUND NO EVIDENCE OF ANY BURNING SMELLS. NOTE - JUST PRIOR TO TAKEOFF FROM CVG AIRCRAFT HSDR ABXA20121221376Fitting · damagedSTA 1809.5 UPPER OUTBOARD CORD LOWER FORWARD TENSION FITTING INNER SURFACE HAS TOOLING MARKS. REMOVED AND REPLACED RIGHT TENSION FITTING AND TORQUED TENSION BOLT TO 358 FT. LBS IAW B767 SRM 51-40-02 AND B767 SB 767-53A0078. ACFT WAS GROUNDED.SDR ABXA20121221375Web · damagedFASTENER HOLE NR 40 ON THE LEFT SIDE OF THE 1809.5 BULKHEAD OF DRWG 624T0020 FLAG NOTE 1 IS ELONGATED AT THE FUSELAGE, THE FITTING, AND AT THE HORIZONAL STAB. COULD NOT GET AN ACCURATE HFEC SCAN. FAB'D NEW REPAIR WEB IAW ENGINE APPROVAL & BOEING DWG #148T274SDR ABXA20121221373Angle · crackedANGLE PIECE AT TOP OF FRONT SPAR TO LEADING EDGE CRACKED AT BOTTOM LOCATED AFT AND ABOVE SLAT PDU BEHIND NUMBER 6 SLAT. REMOVED & REPLACED ANGLE IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20121219370Tee Fitting · corrodedRIGHT WING LOWER FORWARD STRUCTURE AT WING STATION 735 HAS CORROSION ON PANEL BRACE TEE CLIP STRUCTURE. REMOVED FWD BEAM AT STA 735, REMOVED TEE CLIP, FABRICATED NEW BEAM FROM 7075-T6 .063 PO 000975, FABRICATED NEW TEE CLIP FROM EXTRUSION BAC 1505-100609-7015SDR ABXA20121219368Structure · crackedRIGHT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11.25 INCHES IN FROM TOP. REPAIRED AREA IAW B767-200 SRM 51-70-12 PG 1 FIG 1, ACFT WAS GROUNDED.SDR ABXA20121218354Pressure Panel · corrodedLEFT WHEEL WELL PRESSURE DECK PANEL HAS CORROSION AT THE FWD ATTACH HOLES (UPPER SIDE). NEW PANEL FABRICATED PER BOEING DWG 145T8752. ACFT WAS GROUNDED.SDR ABXA20121217372Failsafe · crackedRIGHT FAILSAFE CRACKED. FAILSAFE STRAP TERMINATING ACTION PERFORMED ON EA 53500014-003, AMES DOCUMENT 47008ORD04, ACFT WAS GROUNDED.SDR ABXA20121217371Shim · corrodedSHIM PACK UNDER DOUBLER AT LEADING EDGE PANEL ATTACH ANGLE 20 INCHES OUTBOARD OF LEFT WING NUMBER 3 SLAT INBOARD AUX TRACK CORRODED. REMOVED FWD BEAM AT STA 735, REMOVED TEE CLIP, FABRICATED NEW BEAM FROM 7075-T6 .063 PO 000975, FABRICATED NEW TEE CLIP FROM ESDR ABXA20121217367Structure · crackedLEFT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11 INCHES FROM TOP. INSTALLED REPAIR ON LEFT NOSE LANDING GEAR VERTICAL CHORD IAW B767-200 SRM 51-70-12, ACFT WAS GROUNDED.SDR ABXA20121217349Rib · damagedRIGHT WING RIB 8 AT FORWARD SPAR INBOARD AND OUTBOARD IN ENGINE DRY BAY HAS TOOLING MARKS. REPAIR IAW REA B657-60431-MR. ACFT WAS GROUNDED.SDR ABXA20121217348Rib · damagedLEFT WING RIB 8 STA 375 AT FWD SPAR OUTBOARD SIDE HAS TOOLING MARKS. REPAIRED IAW REA B657-60430-MR. ACFT WAS GROUNDED.SDR ABXA20121214344Inertia Reel · out of positionONE INERTIA REEL FELL OUT ON THE FLOOR DURING PRE FLIGHT INSPECTION BY FLIGHT CREW. REMOVED AND DEFERRED NR 4 INERTIA REEL, ACFT WAS GROUNDED.SDR ABXA20121214369Skin · dentedFORWARD LEFT FUSELAGE STA 526 S30L-31L HAS UNMARKED DENT. REPAIRED DENT IAW B767-200 SRM 53-00-01 FIG 201 REPAIR 14, ACFT WAS GROUNDED.SDR ABXA20121214366Frame · corrodedLEFT SIDE FRAME FITTING NR 10 & 11 HOLES HAVE CORROSION AROUND THEM ON THE FWD FACE. REPAIRED AREAS OF CORROSION AROUND HOLES NR 10 & 11 IN LEFT SIDE FRAME FITTING IAW 47030REA06, ACFT WAS GROUNDED.SDR ABXA20121214363Longeron Splice · corrodedLEFT LONGERON SPLICE PLATE HAS CORROSION STA 930-943. REPAIR LEFT LONGERON SPLICES PLATE IAW REA 47030REA05, ACFT WAS GROUNDED.SDR ABXA20121214361Skin · corrodedSTA 955 FOUND CORROSION UNDER FAILSAFE TRIM OUT. CORROSION MIGATES BACK UNDER FAILSAFE AND FUSELAGE SKIN. REPAIRED AREA OF CORROSION IAW REA 47030REA03. ACFT WAS GROUNDED.SDR ABXA20121213365Frame · corrodedLEFT SIDE FRAME FITTING HAS SEVERAL AREAS OF CORROSION ON THE FORWARD FACE ABOVE HOLE 1. CLEANED AREAS OF CORROSION IAW B767-200 SRM 53-50-08. REMOVED CORROSION WITHIN LIMITS .638 REMAINING FROM ORIGINAL THICKNESS OF .700 VERIFIED WITH NDT. PRIMED AND PAINTSDR ABXA20121221374Beam · crackedOUTBOARD HYDRAULIC BAY DOOR LATCH PLATE ATTACH BEAM CRACKED AT FORWARD END. REMOVED AND REPLACED BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR ABXA20121212364Strap · corrodedLEFT FAILSAFE STRAP HAS MULTIPLE AREAS OF HEAVY CORROSION. REMOVED AND REPLACED FAILSAFE STRAP IAW B767-200 SRM 51-40-05 ON EA 53500013-008, AMES DOC. 47008ORD11, ACFT WAS GROUNDED.SDR ABXA20121212359Failsafe · crackedSTA 955 LEFT FAILSAFE LOWER HOLE CRACKED AT 2 O`CLOCK POS APPROX .310 LONG MARKED. LEFT FAILSAFE STRAP REPLACED ON EA 53500013-008, AMES DOC. 47008ORD11. ACFT WAS GROUNDED.SDR ABXA20121212358Tee Fitting · corrodedRIGHT SIDE PRESSURE DECK TEE FITTING CORRODED AT THE FOWARD LOWER HOLE COMMON TO THE FAILSAFE STRAP. REMOVED AND REPLACED TEE FITTING, REF: B767-200 SRM 51-40-05 IAW EA 53500014-003, AMES DOCUMENT 47008ORD04. ACFT WAS GROUNDED.SDR ABXA20121209343Mechanism · out of positionLEFT OVERWING ESCAPE SLIDE DOOR OPEN. UPON INSPECTION FOUND THAT THE INTERLOCK CONTROL ROD LATCH MECHANISM WAS IN THE DOWN POSITON (OPEN). LOCKED THE ROD LATCH MECHANISM BACK INTO THE CLOSED POSITION IAW AMM 25-65-09-4. ACFT WAS GROUNDED.SDR ABXA20121207346Spar · corrodedWING STATION 974 LW REAR SPAR UPPER SURFACE TRAILING EDGE PANEL SKIN BULGING SUSPECT CORROSION MARKED. REPAIRED LEFT WING REAR SPAR UPPER SKIN SURFACE WS 974 IAW REA B657-60401-MR. ACFT WAS GROUNDED.SDR ABXA20121206340Sill · corrodedBULK CARGO DOOR SILL DOUBLER CORROSION ON UPPER SURFACE FUSELAGE STATION 1147 AND STRINGER 33 LEFT FORWARD END OF SILL PLATE. REMOVED AND REPLACED BULK CARGO DOOR SILL PLATE IAW B767 SRM 51-40-02 PARA 4, PARA 5 AND PARA 7. ACFT WAS GROUNDED.SDR ABXA20121206328Strut · corrodedNUMBER 5 SLAT INBOARD AUX TRACK LOWER OUTBOARD PANEL ATTACH STRUT HAS CORROSION BETWEEN PANEL ATTACH POINT NUT PLATES. ATTACH STRUT PANEL WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW B767 SRM 51-40-02. ACFT WAS GROUNDED.SDR ABXA20121206327Keelbeam · corrodedLEFT KEEL BEAM STA 1000 TO 1010 HAS CORROSION ON LOWER HORIZONTAL LEG UPPER SURFACE. REPAIRED LEFT KEEL BEAM STA 1000-1010 ON LOWER HORIZONTAL LEG IAW REA B653-60410-MR. ACFT WAS GROUNDED.SDR ABXA20121204360Failsafe · corrodedSTA 955 RIGHT FAILSAFE CUTOUT HAS MINOR CORROSION. CLEANED CORROSION IAW B767-200 SRM 51-10-02. SPOTFACED & REPAIRED AREA IAW ABX EA 53500014-004 & AMES DOC 47008ORD10. ACFT WAS GROUNDED, 145T3310.
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