Boeing 767-34AF
Service difficulty reports · 6,321
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 = '76734AF' 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 = '76734AF' 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 IPXA10659877Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 2" X 2.5" AT BS 985 TO 1087 RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659869Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 540 TO 654+22 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659868Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 3 PUNCTURE HOLES 1.75" X 1.5" AND 1" X 1.25" AT BS 412 TO 540 LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED AMM 53-01-01.SDR IPXA10659867Floor Panel · gougedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG DEEP GOUGE AND TEAR AT BS 412 TO 540 RBL 55" TO RBL 77". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659866Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 2.5" AT BS 412 TO 540 RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659865Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 2 PUNCTURE HOLE 1.2" X 1.5" AND 1.2" X 1.8" AT BS 1480 TO 1598 RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659864Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 690 TO 764 LBL 77" TO LBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659863Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 1.75" AT STN1480 TO 1598 LBL33" TO LBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659843Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 2" AT BS 764 TO 873 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659842Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND (2) PUNCTURE HOLES 1.5" X 2" AND 1.75" X 2" AT BS 873 TO 935 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659841Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 654+22 TO 690 LBL 77 OT LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659818Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 1.75" AT STN731 TO 833 RBL33" TO RBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659815Failsafe · crackedINSPECTION TYPE:C, BS 955 WL 200 SUSPECTED CRACK INDICATIONS WERE FOUND AT BOTH LT AND RT OF BS 955 FAILSAFE STRAP. FUSELAGE BS 955 REAR SPAR BULKHEAD SIDE FITTINGS FAILSAFE STRAPS REPAIRED IAW UPS EO B767-5350-17922 APPENDIX C & D.SDR IPXA10659812Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.2" X 1.5" AT BS 1351 TO 1480 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659797Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD NOSE SKIN AT OSS723.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7"SDR IPXA10659796Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD SE SKIN RIVET HOLE FOUND CRACKED RT WING NR9 SLAT L/E OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.875" X 7.125"SDR IPXA10659795Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E INBD NOSE SKIN AT OSS572.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.125SDR IPXA10659794Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD 7075T6-0.063IN, CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.875" X 7.1SDR IPXA10659792Skin · crackedINSPECTION TYPE:C, LT WING NR3 SLAT L/E OTBB NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT L/E OTBD NOSE SKIN AT OSS792.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 1, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7SDR IPXA10659791Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK LT WING NR 3 SLAT L/E INBD NORE SKIN AT OSS723.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD 7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.1SDR IPXA10659768Skin · crackedINSPECTION TYPE:C, RT WING NR 11 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 11 SLAT L/E INBD NOSE SKIN A OSS871.63 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 6.75" THISSDR IPXA10659766Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE FTG FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1 FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 1.25", OTBD FLANGE IS 1.25" DAMAGED SDR IPXA10659598Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 11R HAS 1" HOLE 12"AFT OF FWD LOCK LINE MFG AND INSTALLED NEW PANEL IAW B767-5320-9693G AND MM53-01-06-4.SDR IPXA10659597Floor Panel · damagedMAIN DECK CARGO COMPT FLOOR DAMAGE AT POS 10R 48" FWD OF AFT EDGE 1" HOLE MFG AND INSTALLED NEW PANEL IAW B767-5320-9693G AND MM53-01-06-4.SDR IPXA10659596Floor Panel · damagedMAIN DECK CARGO COMPT FLOOR DAMAGED AT POS 7R DAMAGE LOCATED 12" AFT O OF FWD EDGE OF LT PANEL. MFG AND INSTALLED NEW PANEL IAW EO B767-5320-9693G AND MM53-01-06-4.SDR IPXA10659595Floor Panel · damagedMAIN DECK CARGO COMPT FLOOR DAMAGED AT 8L AFT OF RT PANEL 1" HOLE. MFG AND INSTALLED NEW PANEL IAW B767-5320-9693G AND B767 MM53-01-06-4.SDR IPXA10659546Crank Assy · bindingL2 WINDOW CRANK BINDING TOWARD CLOSE. ADJUSTED THE L2 WINDOW IAW MM 56-11-02-5. OPS GOOD.SDR IPXA10659516Shim · unknownINSPECTION TYPE:C FUS REMOVE FASTENERS / PARTS IDENTIFIED IN EO B767-5350-17922-E APP C, FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM FASTENER / PARTS. REMOVED AND REINSTALLED IAW EO B767-5350-17922-E APPENDIX C FIG 6 IN ORDER TO INSTALL A PROTECTIVE SHIM SDR IPXA10659433Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQ NR 302-F1-02 FUSELAGE BETWEEN BS 439 TO BS 463 AND STR 23R-25R EXISTING REPAIR DOES NOT CORRELATED TO A SRM. SURVEY SEQ 302-F1-02 FX BTN BS436-463 & STR23R-25R SKIN REPAIRED IAW RS R53-00-36706, EO B767-5330-37489, ORG MATL IS 20SDR IPXA10659519Failsafe · crackedINSP TYPE:C FUS RT BS 955 BULKHEAD FITTING AREA CRACK AT FAIL SAFE STRAP APPROX .2500" & .3750" IN LENGTH. REFER NRC 50422 FOR DETAIL, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.SDR IPXA10659512Fitting · crackedINSPECTION TYPE:C, FUS RT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.SDR IPXA10659485Fitting · corrodedINSPECTION TYPE:C, FX - RT STA 955 BULKHEAD FITTING AREA CORROSION FOUND AT "T" FITTING HOLE AROUND THE HOLE BORE SURFACE. RT STA 955 BULKHEAD FITTING AREA "T" FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX D, FIG 6.SDR IPXA10659409Bracket · crackedINSPECTION TYPE:C, LT WING - L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. LT WING L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET, REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR IPXA10659390Wedge · crackedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AFT EDGE AREA CRACKED. COMPOSITE PREP REG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14.SDR IPXA10659515Failsafe · crackedINSPECTION TYPE:C FUS LT B S955 BULKHEAD FITTING FAIL SAFE STRAP CRACK FOUND AT FWD SIDE THRU THICKNESS AT 9 O/C POSN AFT SDE CRACK AT 5 O/C POSITION (LOCKING INBD) APPROX 0.040" REF NRC 50425 FOR DETAIL. FUSELAGE LT BS955 REAR SPAR BULKHEAD FITTING AREA FAIL SDR IPXA10659486Fitting · crackedINSPECTION TYPE:C FX - LT STA 955 BULKHEAD TEE FITTING CRACK FOUND AT 7 O`CLOCK POSITION APPROX .0625" LONG. FX - LT STA 955 BULKHEAD TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX C, FIG 6.SDR IPXA10659588Support Angle · crackedINSPECTION TYPE:C, RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE FOUND CRACKED CRACK LENGTH .3750". RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10659518Panel · chippedINSP TYPE:C EMP - RT INBD ELEVATOR T/E OTBD CORNER UPPER SURFACE CHIPPED COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW RS R55-20-36704, REV A AND EO B767-5520-37442-A.SDR IPXA10659513Fitting · crackedINSPECTION TYPE:C FUS LT BS955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX C.SDR IPXA10659326Floor Panel · misrepairedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 833 TO STN933 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659325Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE DAMAGE AT STN975 TO 1114 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659324Floor Panel · misrepairedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 654+22 TO STN690 LBL33" TO LBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659323Floor Panel · puncturedINSP TYPE:C, MCD FLOOR PANEL FOUND PUNCTURED, DAMAGED AT STN 588 TO 654+22 RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659549Rib · crackedINSPECTION TYPE:8C, LT WING - INBD AILERON INBD RIB FITTING UPPER AFT FLANGE FOUND CRACKED. LT WING INBD AILERON INBD RIB FITTING UPPER AFT FLANGE REPAIRED IAW HX RS NO R-57-00-36699 REV A & UPS EO NO. B767-5740-37473-A. ORG MAT'L IS 7075T73 FORGING, CRK LSDR IPXA10659432Rib · crackedINSPECTION TYPE:C, RT WING INBD AILERON INBD RIB FTG UPPER AFT FLANGE FOUND CRACKED. RT WING INBD AILERON INBD RIB FTG UPR AFT FLANGE REPAIRED IAW RS R57-00-36698 & EO B767-5740-37472-A, ORG MATL IS 7075T73FORGING, CRACK LENGTH IS 1.1", FINAL CUTOUT SIZE IS 1SDR IPXA10659431Floorbeam · crackedINSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH ANGLE FOUND CRACKED AT LBL 25". MAIN DECK STA 246 FLOORBEAM AT LBL 25" ATTACH ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.SDR IPXA10659430Floorbeam · crackedINSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH CLIP FOUND CRACKED AT LBL 50" MAIN DECK STA 246 FLOORBEAM AT LBL50" ATT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.SDR IPXA10659410Stiffener · crackedINSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94" WING CTR SECTION FRONT SPAR VERT STIFFENER REPAIRED IAW RS R57-00-36703, EO B767-5710-37458 JUST AT STA785.9 RBL10.94" ORG MATL IS BAC1518-749-2024T3511SDR IPXA10659389Hinge Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG201, ORG MATL IS 7075T73 FORGING, CRACK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGEDSDR IPXA10659388Hinge Fitting · crackedRT WING - INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. RT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGED CUTOUT SIZE AR
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