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 IPXA10658714Skin · crackedINSPECTION 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 AS PER SRM 57-43-01-2R2 FIG 201 REV46 ORG MAT'L IS CLAD7075T6-0.063 INCH CRACK LENGTH IS 0.13 INCH DAMAGED CUTOUT IS 8 15SDR IPXA10658713Skin · 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 AS PER SRM 57-43-01-2R2 FIG 201 REV46 ORG MAT'L IS CLAD7075T6-0.063" CRACK LENGTH IS 0.12 INCH DAMAGED CUTOUT IS 8 7/8 INCH SDR IPXA10658712Skin · crackedINSPECTION TYPE:C RT - NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT NR 10 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 ORG MAT'L IS CLAD7075T6-0063" CRACK LENGTH IS 0.09 INCH DAMAGED CUTOUT IS 8 7/8 INCH BY 7 1/8SDR IPXA10658711Hinge Fitting · crackedINSPECTION TYPE:C RT - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT INBD FLAP INBD HINGE FTG AT IFS179.75 REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 46 ORG MAT'L IS FORGING 7075T73, CRACK LENGTH AT INBD FLANGE IS 1.375 INCH AND OTBD FLANGE IS 0.5 INCH DASDR IPXA10658763Floor Panel · damagedINSP TYPE:C -MCD POS 11R FLOOR DAMAGE 28.5 INCHES, RT BS LINE 79 INCHES FROM FWD PANEL. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10658629Stiffener · deformedINSPECTION TYPE:C, BULK CARGO RT STA 1502 BELOW FLOOR RBL 14" STIFFENER FOUND DEFORMED. BULK CARGO RT STA1502 BELOW FLOOR RBL14" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658628Stiffener · deformedINSPECTION TYPE:C, BULK CARGO LT STA1480 BELOW FLOOR LBL8" STIFFENER FOUND DEFORMED. BULK CARGO LT STA1480 BELOW FLOOR LBL8" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658627Stiffener · deformedINSPECTION TYPE:C, BULK CARGO RT STA 1502 BELOW FLOOR RBL 8" STIFFENER FOUND DEFORMED. BULK CARGO RT STA1502 BELOW FLOOR RBL8" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658559Floorbeam · crackedINSPECTION TYPE:6C, BULK CARGO LT STA 1417 LBL 8" FLOOR SUPPORT RIVET HOLE FOUND CRACK. BULK CARGO LT STA 1417 LBL 8" FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658556Support · crackedINSP TYPE:6C, BULK CARGO LT STA 1417 LBL 14" FLOOR SUPPORT RIVET HOLE FOUND CRACKED. BULK CARGO LT STA 1417 LBL 14" FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658555Stiffener · deformedINSP TYPE:6C, BULK CARGO LT STA 1439 LBL 8" BELOW FLOOR STIFFENER FOUND DEFORMED. BULK CARGO LT STA 1439 LBL 8" BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658554Stiffener · deformedINSP TYPE:6C, BULK CARGO RT STA 1480 BELOW FLOOR RBL 8" STIFFENER FOUND DEFORMED. BULK CARGO RT STA 1480 BELOW FLOOR RBL 8" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.46.SDR IPXA10658584Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA230.5 COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5 REV 46.SDR IPXA10658583Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA210. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 46.SDR IPXA10658495Floor Panel · damagedPOS 9L HAS 1/2 INCH BY 1/4 INCH HOLE AND 2ND HOLE .900 BY .600 LOCATED 2.60 INCH AND 5. 50 INCH FROM OTBD EDGE OF PANEL AND 52 INCH FROM FWD EDGE OF PANEL REPAIRED DAMAGE PER 767 SRM 53-00-50-2R. THIS CLEARS D416520 IAW 767B SRM 53-00-50-2R.SDR IPXA10658492Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 10L. REPAIRED PER SRM 53-00-50-2R.SDR IPXA10658490Floor Panel · damagedMCD FLOOR PANEL DAMGED POS 8R. REPAIRED PER EO B767-5320-9693-G.SDR IPXA10658489Floor Panel · damagedMCD FLOOR PANEL DAMAGED POS 4. REPAIRED PER EO B767-5320-9693-G.SDR IPXA10658498Fuel Filter · warning lightINSPECTION TYPE:ETOP ATB - RT ENG FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED RT ENGINE FUEL FILTER PER B767 73-11-02-4. LEAK CHECK GOOD GROUND RAN ENGINES 30 MINUTES. NO PROBLEMS FOUND. A/C OK FOR SERVICE. OLD FILTER APPEARED TO BE OK PER FIM 73-31-SDR IPXA10658552Floor Panel · puncturedINSP TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 731 TO 833, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10658551Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 930 TO 975, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10658539Skin · misrepairedINSP TYPE:6C, SURVEY SEQUENCE NR 329-F1-05 STA 1197+48 BETWEEN STR 29R & 31R, THE EXISTING REPAIR DOES NOT CORRELATED TO A SRM DUE THE EXISTING FILLER NOT FULLY FILL THE EXISTING SKIN CUTOUT. FX SKIN REPAIRED IAW SRM 53-00-01-2R1, FIG 201, REV 46 JUST BETWEENSDR IPXA10658616Floorbeam · crackedINSPECTION TYPE:C, MEC CABIN FLOOR SUPPORT BEAM STA246 RBL10" FWD CLIP FOUND CRACKED. MEC CABIN FLOOR SUPPORT BEAM STA246 RBL10" FWD CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658558Floorbeam · crackedINSPECTION TYPE:6C, MEC CABIN FLOOR SUPPORT BEAM STA246 LBL50" AFT CLIP FOUND CRACKED. MEC CABIN FLOOR SUPPORT BEAM STA 246 LBL 50" AFT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.46.SDR IPXA10658557Angle · crackedINSP TYPE:6C, MEC CABIN FLOOR SUPPORT BEAM STA 246 LBL 25" FWD ANGLE FOUND CRACKED. ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658553Stiffener · crackedINSP TYPE:6C, FWD CARGO WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. STIFFENER REPAIRED IAW HX RS. R57-10-36618 REV A & EO NR B767-5710-36713-A. ORIN. MAT'L 1518-749-2024T3511, CRK LENGTH 3.25", CUTOSDR IPXA10658538Skin · crackedINSPECTION TYPE:6C, LT WING - NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 46 JUST AT OSS572.5, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.07", DAMAGED CUTOUT SIZE ISDR IPXA10658537Skin · crackedINSP TYPE:6C, 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 REV 46, JUST AT OSS641.9, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.09", DAMAGED CUTOUT SIZE IS 8.8SDR IPXA10658536Hinge Fitting · crackedINSPECTION TYPE:6C, LT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. LT WING - INBD MAIN FLAP HINGE FTG, REPAIRED IAW SRM 57-53-02-2R1, FIG 201, REF 46, ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 1", OTBD FLANGE IS 0.9", DAMSDR IPXA10658535Hinge Fitting · crackedRT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 2 201, REV 46 ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH INBD FLANGE IS 1.125" & OTBD FLANGE IS 1.25", DAMAGED CUTOUT SIZE SDR IPXA10658514Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS723.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.12" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" TSDR IPXA10658513Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR3 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS792.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.13" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" THSDR IPXA10658512Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RHW 9 SLAT INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 JUST AT OSS572.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.08 INCH DAMAGED CUTOUT SIZE IS 8.875 INCH BY 7.37SDR IPXA10658511Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS641.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH IS 0.15 INCH, DAMAGED CUTOUT SIZE IS 8.875"SDR IPXA10658505Stiffener · crackedINSPECTION TYPE:C MEC, CABIN FLOOR SUPPORT BEAM STA246 LBL40 FWD STIFFENER FOUND CRACKED MEC CABIN FLOOR SUPPORT STA 246 LBL40 INCH STIFFENER REPAIRED AS PER SRM 53-10-51-2R4 FIG 201 REV46, ORG MATL IS BAC1490-2793-7075T62, CRACK LENGTH IS 1 INCH, THIS REPAIR SDR IPXA10658426Actuator · leakingATB - C HYD QTY DECREASED TO ZERO AND SYS PRESS LIGHT ILLUM. EICAS MSG C HYD SYS PRESS AND C HYD QTY DISPLAYED. FOUND NR 8 INBD SPOILER ACTUATOR LEAKING AT FILTER CASE. REPLACED O'RING IAW AMM 27-61-02-4. SERVICED C HYD SYS 12-12-01-3. LEAK CKD OK.SDR IPXA10663039Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 4L. MFG NEW FLOOR PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR IPXA10663038Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 4R. MFG NEW MCD FLOOR PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR IPXA10663037Floor Panel · damagedREF D418725 - MCD FLOOR PANEL DAMAGED AT POS 1. MFG NEW PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10663036Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 2L. MFG NEW PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR IPXA10663035Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 2R. FABRICATED NEW PANEL IAW EOB767-5320-9593G.SDR IPXA10658412Floor Panel · damagedMAIN DECK FLOOR PANEL POS 9L HAS DAMAGE 3/4" BY 1/2" GOUGE THROUGH UPPER SKIN ONLY. REPAIRED IAW EO B767-5320-9693-G.SDR IPXA10658370Warning Message · false indicationINSPECTION TYPE:E TOP, DURING FIRST SEGMENT OF APPROACH FIRE/OVERHEAT WARNING DISPLAYED. ACCOMPLISHED QRH. PUSHED SYS RESET SWITCH. WARNING REMAINED OFF REMAINDER OF FLIGHT. ACCOMPLISH FIM 26-11-00/101 FIG 104. NO FAULTS FOUND ACFT. OK FOR SERVICE.SDR 2010F00023Control Cable · icedON ARRIVAL, CREW REPORTED STAB TRIM NO MOVEMENT IN NORM OR ALT MODES. ON INVESTIGATION STAB BAY FOUND TO HAVE ICE FORMATION APPROX 10 INCHES DEEP IN BILGE AREA. ICE FORMATION HAD PREVENTED POSITION MODULES AND FOLLOW UP CABLES FROM MOVING. THIS RESULTED IN CASDR IPXA10658388Skin · erodedINSPECTION TYPE:6C, LT WING INBD AFT FLAP INBD FWD (NEAR L/E) FOUND ERODED AND WORN METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR.4 FIG 202 SHEET 1 REV.46.SDR IPXA10658300Floor Panel · delaminatedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DELAMINATION AND PUNCTURED AT STA731 TO 833 LBL11 TO RBL11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10658353Floor Support · crackedINSPECTION TYPE:C, MAIN DECK COMPT STA 1581 RBL 70" FLOOR PANEL SUPPORT INBD ANGLE FOUND CRACKED. MAIN DECK COMPT STA1581 RBL70" FLOOR PANEL SUPPORT INBD ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10658352Floor Support · deformedINSPECTION TYPE:C, BULK CARGO COMPT STA 1415 LBL 30" FLOOR PANEL SUPPORT SURFACE FOUND DEFORMED. FLOOR PANEL SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658351Stiffener · deformedINSPECTION TYPE:C, BULK CARGO COMPT STA 1481 LBL 8" FLOOR PANEL SUPPORT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA1481 LBL8" FLOOR PANEL SUPPORT VERTICAL STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10658350Stiffener · deformedINSPECTION TYPE:C, BULK CARGO COMPT STA 1502 LBL 8" FLOOR PANEL SUPPORT VERTICAL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA1502 LBL8" FLOOR PANEL SUPPORT VERTICAL STIFFENER. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.
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