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 IPXA09656274Floor Panel · damagedINSPECTION TYPE:6C STA 544 TO 654 + 22, LBL 33 TO LBL 55, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656273Floor Panel · damagedINSPECTION TYPE:6C STA 730 - 833, LBL 11 TO RBL 11, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656272Floor Panel · damagedINSPECTION TYPE:6C STA 970 TO STA 1109, LBL 11 TO RBL 11 MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656271Floor Panel · damagedINSPECTION TYPE:6C STN 933 TO 970, LBL 11 TO RBL 11, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656270Floor Panel · damagedINSPECTION TYPE:6C STA 1430 TO 1540, LBL 55 TO LBL 77, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656269Floor Panel · damagedINSPECTION TYPE:6C STA 1480 TO 1580, LBL 33 TO LBL 54, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656268Floor Panel · damagedINSPECTION TYPE:6C STN 1460 - 1540, RBL 55 TO RBL 77, MCD FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.SDR IPXA09656306Skin · crackedINSPECTION TYPE:C LT WING - NR 3 SLAT NOSE SKIN AT I/B SUPPORT WEB FOUND CRACKED (CRACK 0.125 INCH LENGTH). LT WING NR 3 SLAT I/B SUPPORT WEB OSS 724-11, NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44 THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MSDR IPXA09656304Slat · crackedINSPECTION TYPE:6C LT WING - NR 4 SLAT NOSE SKIN AT O/B SUPPORT WEB FOUND CRACKED. LT WING NR 4 SLAT O/B SUPPORT WEB OSS641.5 NOSE SKIN REPAIR AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0071IN AS DOUSDR IPXA09656303Skin · crackedINSPECTION TYPE:6C LT WING - NR 5 SLAT I/B NOSE AREA SKIN FOUND CRACKED. LT WING - NR 5 SLAT OSS389.71 I/B NOSE SKIN REPAIR AS PER HX RS R57-43-36343 REV A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6-0063IN AS DOUBLER & REPAIR SIZE 4.5 SDR IPXA09656299Skin · crackedINSPECTION TYPE:6C RT WING - NR 9 SLAT NOSE SKIN AT O/B SUPPORT WEB FOUND CRACKED. RT WING - NR 9 SLAT AT O/B SUPPORT WEB OSS641.5 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 0.071IN7075-0SDR IPXA09656298Skin · crackedINSPECTION TYPE:6C RT WING - NR 10 SLAT NOSE SKIN AT I/B SUPPORT WEB FOUND CRACKED. RT WING - NR 10 SLAT I/B SUPPORT WEB OSS724-11 NOSE SKIN REPAIR AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0071IN ASDR IPXA09656297Hinge Fitting · crackedINSPECTION TYPE:6C LT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA FOUND CRACK. LT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH 10134-2007-7075T6511 AS REPAISDR IPXA09656286Fairing · delaminatedINSPECTION TYPE:6C RT WING O/B FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03, PARA 5A (1), FIG 5, REV 44.SDR IPXA09656284Hinge Fitting · crackedINSPECTION TYPE:6C RT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA FOUND CRACKED. RIGHT I/B MID - FLAP INBOARD AFT HINGE FITTING REPAIR PER SRM 57-53-02-2R1 FIG 201 REV 44.SDR IPXA09656266Stiffener · crackedINSPECTION TYPE:6C MAIN E/E CENTER STA 246 LBL 40 M/D FLOORBEAM ATT STIFFENER FOUND CRACKED. MAIN E/E CENTER STA 246 LBL 40 FLOORBEAM ATT STIFFENER REPAIRED AS PER SRM 53-10-51-2R 4 FIG 201 REV 44, THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-006SDR IPXA09656264Support Bracket · crackedINSPECTION TYPE:6C NR 2 PYLON - INTERNAL VERTICAL STIFFENER UPPER ATT SUPPORT BRACKET CRACKED AT NAC STA 280 LT SIDE NR 2 PYLON. INTERNAL VERTICAL STIFFENER UPPER ATT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44 JUST ASDR IPXA09656177Panel · crackedINSPECTION TYPE:N/A NR 8 SLAT CLOSURE PANEL CRACK 1.5 INCH. REPAIRED PER EO B767-5750-33200B.SDR IPXA09656174Wedge · delaminatedINSPECTION TYPE:N/A LT WING OUTBOARD FLAP T/E WEDGE DELAM. REPAIRED PER EO-B767-5750-30880-B.SDR IPXA09656308Attach Angle · crackedINSPECTION TYPE:6C AFT OF BULK CARGO COMPT STA 1582 LBL 81 MAIN DECK FLOOR SUPPORT BEAM ATTACH ANGLE FOUND CRACK. AFT OF BULK CARGO COMPT STA 1582 LBL 81 MAIN DECK FLOOR SUPPORT BEAM ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 SDR IPXA09656307Attach Angle · crackedINSPECTION TYPE:6C AFT OF BULK CARGO COMPT STA 1582 RBL 81 MAIN DECK FLOOR SUPPORT BEAM ATTACH ANGLE FOUND CRACK. AFT OF BULK CARGO COMPT STA 1582 RBL 81 MAIN DECK FLOOR SUPPORT BEAM ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 SDR IPXA09656283Attach Fitting · crackedINSPECTION TYPE:6C MAIN E/E CENTER STA 246 RBL 10 M/D FLOORBEAM ATT CLIP FOUND CRACKED. MAIN E/E CENTER STA 246 RBL 10 M/D FLOORBEAM ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.SDR IPXA09656265Attach Angle · crackedINSPECTION TYPE:6C MAIN E/E CENTER STA 246 LBL 25 MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACKED. MAIN E/E CENTER STA 246 LBL 25 MAIN DECK FLOORBEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.SDR IPXA09656263Attach Fitting · crackedINSPECTION TYPE:6C MAIN E/E CENTER STA 246 LBL 50 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACKED. MAIN E/E CENTER STA 246 LBL 50 MAIN DECK FLOORBEAM ATT CLIP REPLACED AS PER SRM 51-10-02 AND SRM 51-40-02 REV 44.SDR IPXA09656144Attach Fitting · crackedINSPECTION TYPE:7C MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP CRACKED. MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656113Attach Angle · crackedINSPECTION TYPE:C MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE CRACKED. CRACKED 0.75 INCH LENGTH. MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656138Skin · crackedINSPECTION TYPE:7C LT WING - NR 4 SLAT EXT SKIN FOUND CRACK AT O/B STRINGER FASTENER AREA. LT WING NR 4 SLAT OSS641-74 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6.071" AND 7075T6.063" ASSDR IPXA09656122Panel · delaminatedINSPECTION TYPE:C EMP VERTICAL STAB RT LWR FWD EXTERNAL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 43, 51-70-10 REPAIR 4 FIG 201, DOUBLER MATERIAL 7075T6BARE0025IN, REPAIR DOUBLER SIZE: 16.125 X 13 INCHES.SDR IPXA09656117Stiffener · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 LBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.SDR IPXA09656116Fairing · delaminatedINSPECTION TYPE:7C LT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05, PAR 5A (1), FIG 5, REV 43.SDR IPXA09656115Stiffener · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 RBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 RBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.SDR IPXA09656146Skin · crackedINSPECTION TYPE:7C NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT CRACKED. NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT REPAIRED AS PER HX RS R-54-51-36328 REV A. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AMS4911-00901IN AND AIS1-301-00161INFH, REPAIR SIZE SDR IPXA09656143Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 1576 LBL 11 FOUND PUNCTURE ABOUT 1 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.SDR IPXA09656142Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 654+3, RBL 74 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R, REV 43, FIG 201.SDR IPXA09656141Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 326, LBL 6 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43, FIG 201.SDR IPXA09656140Skin · crackedINSPECTION TYPE:7C RT WING - NR 9 SLAT I/B UPPER AREA FOUND CRACKED. RT WING - NR 9 SLAT OSS573 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201, REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0063IN AND 7075-0-0071IN. REPAIR DOUBLER ANDSDR IPXA09656139Skin · crackedINSPECTION TYPE:7C RT WING - NR 9 SLAT O/B UPPER AREA FOUND CRACKED. RT WING NR 9 SLAT OSS641.74 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6.071 AND 7075T6.063 AS REPAIR DOUBLERS AND REPSDR IPXA09656137Stringer · chafedINSPECTION TYPE:7C M/D STA 1241 - 1263 STR 16R FOUND DEEP CHAFING MARK. MAIN DECK BS 1233 TO 1271 STR 16R STRINGER REPAIR AS PER SRM 53-00-03-2R1 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A CATEGORY 'A' REPAIR WITH MATERIAL BAC1498-208 7075T62 AND BAC1498-20SDR IPXA09656124Support Bracket · crackedINSPECTION TYPE:7C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET FOUND CRACKED. RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656123Doubler · delaminatedINSPECTION TYPE:C RT WING I/B AFT FLAP LOWER O/B EXISTING REPAIR FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 REV 43. REPAIR DOUBLER MATERIAL 2024T3-0040IN AND ADHESIVE FILM AF163-2K0010IN REPAIR DOUBLER SIZE: 9 XSDR IPXA09656121Hinge Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG FOUND CRACKED 1.5 INCH LENGTH AT I/B FLANGE AND 0.9 INCH LENGTH AT O/B FLANGE. LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 43.SDR IPXA09656120Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-02, FX BS 388-400 BETWEEN STR 29L AND 30L, THE SKIN REPAIR CANNOT BE CORRELATED TO SRM. FX REPAIRED AS PER SRM 53-00-01-2R1 FIG 201 REV 43 JUST AT STA 385 - 415 BETWEEN STR 28L AND 31L. THIS IS CLASSIFIED AS A MAJOR SDR IPXA09655932Floor Panel · damagedHOLE MAIN CARGO FLOOR POS 8R. REPAIRED PER SRM 53-00-50-2R. PROCURED FIBERGLASS REPAIR.SDR IPXA09656145Stiffener · crackedINSPECTION TYPE:7C FWD CARGO COMPT STA 786, WL 196, RBL 33 WING CENTER SECTION FRONT SPAR ATT STIFFENER FOUND CRACKED. FWD CARGO COMPT BS 786 RBL 33 CENTER TANK FRONT SPAR STIFFENER REPAIR AS PER HX RS R57-11-36330 REV A WITH MATERIAL 2024T351.0250 AND 2024T3SDR IPXA09656114Cylinder · corrodedINSPECTION TYPE:7C LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SIDE AND O/B SIDE NUMEROUS LOCATIONS FOUND RUSTY ABOVE TORSION LINK UPPER FTG UP TO 56 INCHES TOP AREA HAND BLEND AREA 50" X 14" REWORK DEPTH 0.001". LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SDR IPXA09656147Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-05 FUSELAGE BS 1241 - 1263 STR 15R - 17R DOUBLER AND TRIPLER FOUND IDENTIFY REQUIRE. SKIN REPAIR AS PER SRM 53-00-01-2R1 FIG 201 REV 43. SUBSEQUENT INSP ARE NECESSARY AS PER SRM 53-00-01-2R1 FIG 201 SHT 9 TABLE V. TSDR IPXA09655819Skin · damagedINSPECTION TYPE:N/A FLAP LWR SKIN DAMAGED. REPAIRED SKIN PER EO B767-5750-33319-B.SDR IPXA09655816Floor Panel · dentedINSPECTION TYPE:N/A POS 8L SIDE AT FWD END 3RD PNL FROM LT SIDE DENTED. REPAIRED PER SRM 53-00-50-2R.SDR IPXA09655752Panel · defectiveINSPECTION TYPE:N/A UPON POWER UP, CREW NOTICED ELECTRICAL SMELL. MOST APPARENT NEAR CENTER OF COCKPIT NEAR CIRCUIT BREAKER PANEL OVERHEAD. A/C PACKS NOT ON, APU ON. AIR EXHAUST FROM COOLING OVERBOARD EXHAUST NORMAL. T/S IAW FIM 21-00-21. FOUND PILOTS OVESDR IPXA09655704Seat Track · damagedINSPECTION TYPE:N/A SEAT TRACK DAMAGED BETWEEN STA 1268 AND 1280 AT RBL 54.75. REPAIRED PER EO B767-5310-33178-B.
Back to Boeing 767-34AF