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 IPXA10659365Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT OTBD NOSE SKIN AT OSS792.5 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LEGNTH IS 0.09". DAMAGED CUTOUT IS 8.875" X 7.125" THIS RESDR IPXA10659364Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS 572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.08" DAMAGED CUTOUT IS 8.875" X 7.25" THIS IS CSDR IPXA10659363Skin · crackedINSP TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.09" DAMAGED CUTOUT IS 8.875" X 7.125". THIS IS CSDR IPXA10659362Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LTW NR4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 JUST AT OSS572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS IS CLASSISDR IPXA10659361Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7" THIS IS CLASSISDR IPXA10659360Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT INBD NOSE SKIN AT OSS723.9 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.8750" X 7.1250". THIS SDR IPXA10659359Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT OTBD NOSE SKIN AT OSS792.5 SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.8750" X 7" THIS REPAIR SDR IPXA10659358Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD NOSE SKIN AT OSS723.9 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.8750" X 7.2500". THIS SDR IPXA10659185Floor Panel · damagedMCD POS 1 FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320--9693-G.SDR IPXA10659184Floorboard · damagedFLOORBOARD DAMAGED. FAB NEW FLOOR IAW B767-5320-9693-G.SDR IPXA10659182Floorboard · damagedFLOORBOARD DAMAGED. FAB NEW FLOOR IAW B767-5320-9693-G.SDR IPXA10659181Floorboard · damagedMAIN DECK FLOOR DAMAGED. FAB NEW FLOORBOARD IAW B767-5320-9693-G.SDR IPXA10659180Floorboard · damagedMAIN DECK FLOOR DAMAGED. FAB NEW IAW B767-5320-9693-G.SDR IPXA10659179Floor Panel · damagedFLOOR PANEL DAMAGED. FABRICATED NEW IAW B767-5320-9693-G.SDR IPXA10659177Floor Panel · damagedREF MMR NR 10659175, REF D411572, MCD FLOOR PANEL POS 4L HAS .5" HOLE. DAMAGE LOCATED AT STA 654+121, LBL45 AND 10" AWAY FROM EDGE. REPAIR THE DAMAGE IAW SRM53-00-50-2R.SDR IPXA10659174Floor Panel · damagedMCD FLOOR PANEL 8R/8R/ HAS 1.5" X .2500" HOLE, .2500" X .2500" HOLE AND .7500" X .5" DENT AT STA 1153. REPLACED FLOOR PANEL IAW EO B767-5320-9693-G.SDR IPXA10659173Floor Panel · damagedMCD FLOOR PANEL 9R HAS .7500" X .5" HOLE AT STA 1157. REPLACED MCD FLOOR PANEL IAW EO B767-5320-9693-G.SDR IPXA10659172Floor Panel · damagedMAIN DECK FLOOR PANEL POS5L DAMAGED 1.5"X 5/8". LESS THAN 3" AWAY FROM THE EDGE. REF D411571. REPLACED FLOOR PANEL IAW EO B767-5320-9693-G.SDR IPXA10659141Rib · crackedINSPECTION TYPE:C, LT WING L/E OF OSS607.247 FIXED FAIRING SUPPORT RIB FWD FLANGE FOUND CRACKED. LT WING L/E OF OSS607.247 FIX FAIRING SUPPORT RIB FWD FLANGE REPAIRED IAW RS R57-41-36687 ORG MATL IS FORGING 7075T73, CRK LENGTH IS 0.875" CUT OUT SIZE IS 0.9" SDR IPXA10659140Floor Support · crackedINSP TYPE:6C, BULK CARGO COMPT STA 1417 LBL 8" FLOOR CHANNEL LOWER RIVET AREA FOUND CRACKED. BULK CARGO COMPT STA 1417 LBL 8" FLOOR CHANNEL REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659137Stiffener · deformedINSP TYPE:6C BULK CARGO COMPT STA 1480 LBL 15" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 LBL 15" FLOOR BEAM ATT VERTICAL STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659136Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1439 LBL 22" FLOORBEAM ATT STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1439 LBL 22" FLOORBEAM ATT STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659135Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1480 LBL 22" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 LBL 22" FLOORBEAM ATT VERTICAL STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659134Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1461 RBL 8" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1461 RBL 8" FLOOR BEAM ATT VERTICAL STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10659133Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1439 LBL 29" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1439, LBL 29" FLOORBEAM ATT VERTICAL STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659132Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1439 LBL 8" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1439 LBL 8" FLOORBEAM ATT VERTICAL STIFFENER FOUND IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659131Floor Support · crackedINSP TYPE:6C, BULK CARGO COMPT STA 1417 LBL 15" FLOOR CHANNEL LOWER RIVET AREA FOUND CRACKED. BULK CARGO COMPT STA 1417 LBL 15" FLOOR CHANNEL REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659130Stiffener · deformedINSPECTION TYPE:6C, BULK CARGO COMPT STA 1480 RBL 15" FLOORBEAM ATT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 RBL 15" FLOORBEAM VERTICAL STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10659025Floor Support · crackedBULK CARGO PIT FLOOR SUPPORT STRINGER AT 22.33 LBL AT STA 1480 AFT FASTENER HOLE ON OTBD SIDE IS CRACKED. R & R STRINGER AND SUPORT ANGLES IAW DWG 146T1219.SDR IPXA10659128Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A, FIG 5, REV 46.SDR IPXA10659126Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03, PAR 5A (1) FIG 5, REV 46.SDR IPXA10659125Fairing · delaminatedINSPECTION TYPE:C RT WING OTBD T/E FLAP L/E MID FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR5A (1) FIG 5, REV 46.SDR IPXA10659124Wedge · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP, T/E WEDGE LWR SURFACE MID AREA DELAMINATION . COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-06 PAR 5A (1) FIG 9. REV 46.SDR IPXA10659163Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-06 FUSELAGE BETWEEN BS 604 TO BS 628 STR 1R TO STR 4R EXISTING REPAIR WAS FOUND. BETWEEN BS604-628 STR1R-4R SKIN IAW R53-31-36683A MAT'L 2024T3 SKIN 0.093"-0.056" AT CUTOUT AREA WITH CUTOUT SIZE 4.18"X5.5". MAJOR REPAIRSDR IPXA10659157Skin · delaminatedINSP TYPE:C, LT OTBD ELEVATOR UPPER SKIN PANEL INBD AFT CORNER DELAMINATION COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW EO B767-5520-37266-A REFER RS R55-20-36688, REV A.SDR IPXA10659155Spar · crackedINSPECTION TYPE:6C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. LT WIING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10659145Attach Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT LBL25". AFT CARGO COMPT STA1087 LBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.SDR IPXA10659144Attach Fitting · crackedINSPECTION TYPE:C, AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT RBL25". AFT CARGO COMPT STA1087 RBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10659123Panel · crackedINSP TYPE:C EMP - LT INBD ELEVATOR T/E AREA CRACK COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW RS R55-23-36680 REV A.SDR IPXA10659090Floor Panel · gougedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND DEEP AND LONG GOUGE AT STN 731 TO STN 833. RBL 11" TO RBL 33". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659040Skin · crackedINSPECTION TYPE:C, LTW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPASDR IPXA10659039Structure · crackedINSP TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS572.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.375" THIS REPAIR ISDR IPXA10659038Structure · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPSDR IPXA10659037Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLD FOUND CRACKED. RT WING NR 9 SLAT INBD AREA AT OSS572.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.3" THIS REPASDR IPXA10659036Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS641.9. NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.16" DAMAGED CUTOUT IS 8.875" X 7.25" THIS RESDR IPXA10659034Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR10 SLAT OTBD AREA AT OSS792.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7" THIS REPAISDR IPXA10659010Floor Panel · damagedREF D ITEM 412865 MCD CTR PANEL POS 4R HAS A HOLE, PANEL NR 143T5876-44. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-G.SDR IPXA10659009Floor Panel · damagedMCD FLOOR PANEL AT POS CTR L 3/4 HAS SEVERAL HOLES, SPONGY, AND DAMAGE D INSERTS. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-G.SDR IPXA10659160Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-02 BULK CARGO DOOR AT BETWEEN STA 1430-1439 STR 26L-27L AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. BETWEEN STA 1426-1456 STR 25L-28L AREA SKIN REPAIRED RS R52-00-36681A ORG MAT'L IS 2024T3 .050" CHEM-MILLED SKIN.SDR IPXA10659156Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 326-F1-01 FUSELAGE BETWEEN BS443-461 & S22R-26R EXISTING REPAIR DOES NOT CORRELATE TO A SRM. SURVEY SEQ NR 326-F1-01 FX BTN BS443-461 & STR22R-26R EXISTING REPAIR ADD FASTENERS ARE ADDED AND INSTALLED COMMON TO REPAIR DO
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