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 IPXA09657505Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657504Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657476Hinge Fitting · crackedINSPECTION TYPE:N/A RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.875 INCH. RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02 -2R1 FIG 201 REV 45.SDR IPXA09657541Skin · damagedINSPECTION TYPE:C SURVEY SEQ 312-F1-05 E&E DOOR RT FWD CORNER SKIN AT BETWEEN BS 305-311 AND STR 38R - 39R AREA SEM WAS FOUND AT SKIN CUTOUT. FX E&E DOOR EXTERIOR SKIN AT BETWEEN BS 305 TO BS 323.5 STR 38L-38R AREA REPLACED AND INSTALLED AS PER SRM 51-10-02 ASDR IPXA09657536Skin Panel · damagedINSPECTION TYPE:C SURVEY SEQ 312-F1-06 FX BETWEEN BS 442-463 AND STR 23R - 27R EXISTING REPAIR DOUBLER HAS MANY ABRASIVE SANDING LINES, DEEP COUNTERSUNK FOUND AT SEVERAL LOCATIONS. AT THE EDGE OF REPAIR DOUBLER, FX BETWEEN BS 442-463 & STR 23R-27R EXISTING CUSDR IPXA09657534Angle · crackedINSPECTION TYPE:C LT WING - L/E LES 160 UPPER AREA FRONT SPAR ANGLE FOUND CRACKED. CRACK LENGTH 0.75 INCH. LT WING L/E LES 160 UPPER AREA FRONT SPAR ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657523Panel · delaminatedINSPECTION TYPE:C LT WING NR 6 SLAT LOWER CLOSURE PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.SDR IPXA09657515Doubler · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP L/E AREA THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.SDR IPXA09657503Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657502Fairing · delaminatedINSPECTION TYPE:C LEFT WING O/B TRAILING EDGE FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657495Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1425 TO 1540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657477Support Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG FLANGE FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.625 INCH. LEFT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 RSDR IPXA09657475Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT I/B AREA AT OSS 724.61 NOSE SKIN CUT 9 X 7.125 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJORSDR IPXA09657474Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT O/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT O/B AREA AT OSS 641.49 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJOSDR IPXA09657472Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT I/B AREA AT OSS 573.25 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJSDR IPXA09657471Skin · crackedINSPECTION TYPE:N/A RIGHT WING NR 10 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 10 SLAT I/B AREA AT OSS 724.6 NOSE SKIN CUT 7.125 X 9 INCH REPAIR AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJORSDR IPXA09657524Doubler · delaminatedINSPECTION TYPE:C RT WING NR 8 SPOILER T/E LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-04 PAR 5G FIG 9 REV 45.SDR IPXA09657516Doubler · delaminatedINSPECTION TYPE:C LT WING NR 3 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.SDR IPXA09657514Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.SDR IPXA09657494Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657493Floor Panel · crackedINSPECTION TYPE:C MCD FLOOR PANEL FOUND CRACKED AT STA 930 TO 975 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657492Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 930 TO 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657491Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540 LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657490Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657489Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657488Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657487Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1370 TO 1480 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657486Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657485Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 873 TO 933, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657484Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657483Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657482Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1197+22 TO 1207 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657481Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 520 , RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657480Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 985 TO 1090, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657479Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 545, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657478Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 654+22 TO 690, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.SDR IPXA09657458Floor Support · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP FOUND CRACK AT LBL 25. AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 25.SDR IPXA09657457Floor Support · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP FOUND CRACK AT RBL 25. AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-10-02 REV 45 JUST AT RBL 25.SDR IPXA09657533Skin · noneINSPECTION TYPE: C, SURVEY SEQUENCE NR 312-F1-05 BS 305 -311, STR 38R - 39R E&E DOOR RT FWD CORNER SKIN EXISTING REPAIR PATCH WAS FOUND. SURVEY SEQ NR 312-F1-05 FX E&E DOOR EXTERIOR SKIN AT BETWEEN BS 305 TO BS 323.5 STR 38L - 38R AREA REPLACED AND INSTALLED SDR IPXA09657443Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP AT RBL 10 FOUND CRACK. CRACK LENGTH 1.5 INCH. MEC COMPT BS 246 FLOORBEAM AT RBL 10 ATTACHED CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657425Angle · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM ANGLE AT LBL 25 FOUND CRACKED. CRACK LENGTH 0.5 INCH. MEC COMPT BS 246 FLOORBEAM AT LBL 25 ATTACHED ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657424Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP AT LBL 50 FOUND CRACKED. CRACK LENGTH 1 INCH. MEC COMPT BS 246 FLOORBEAM AT LBL 50 ATT CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657330Actuator · malfunctionedINSPECTION TYPE:N/A DIV - SMOKE IN THE COCKPIT AT FL 39. DECLARED AN EMERGENCY. INSPECTED WIRING, C/B PANELS, LAV, PACKS, WINDOW TEMP SENSORS CONNECTIONS, & E&E WIRING ALL CHECKED GOOD WITH NO DEFECTS. RAN PACKS WITH APU AND ENGINES WITH NO DEFECTS. FOUND SDR IPXA09657321Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657290Skin · damagedINSPECTION TYPE:N/A LT OTBD FLAP T/E WEDGE LOWER SKIN DAMAGE REF D-406042 LP 300440. REPAIRED IAW EO B767-5750-34485-B / SRM 51-70-17.SDR IPXA09657382Fitting · crackedINSPECTION TYPE:C LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. CRACK LENGTH 0.375 INCH. LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4SDR IPXA09657334Attach Fitting · crackedINSPECTION TYPE:C NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 FOUND CRACK. CRACK LENGTH 0.5 INCH. NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657333Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA UPPER SURFACE, THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.SDR IPXA09657332Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA LOWER SURFACE THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 45.SDR IPXA09657305Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.
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