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 IPXA11667324Floor Panel · brokenINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND BROKEN AND TOGETHER WITH 5 DENT MARKS AT STA 731 TO 833, RBL55 TO RBL77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11667325Floor Panel · dentedINSPECTION TYPE:8C, FLOOR PANEL FOUND 8 EA DENT MARKS AT BS 933 TO 985, RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1667018Floor Panel · damagedHOLE IN MCD FLOOR PANEL 4" FED OF 3RD LOCK FROM AFT END, 6 0" FROM FWD EDGE OF POS 10L. REPAIRED IAW SRM 53-00-50-2R, PARA 4.C.SDR IPXA1667017Floor Panel · damaged.7500" HOLE IN FLOOR PANEL, POS 14L. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1667015Floor Panel · damagedMAIN CARGO POS 9R FLOOR PANEL 1 EA .250 HOLE. REPAIRED IAW EO B767-5320-9693-H.SDR IPXA1667014Floor Panel · damagedMCD FLOOR PANEL POS 9 CENTER HAS 5 EA .2500" HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA1667396Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING SUSPECT CRACK FOUND AT FAIL-SAFE STRAP AREA. REMOVE FASTENER FOR NDT CONFIRMATION FUSELAGE LT BS955 REAR SPAR BULKHEAD FAIL SAFE STRAP ATT MOST LOWER BOLT REMOVED AND REINSTALLED IAW EO B76SDR IPXA1667393Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING SUSPECT CRACK FOUND AT FAILSAFE STRAP AREA. REMOVE FASTENER FOR NDT CONFIRMATION FUSELAGE RT BS955 REAR SPAR BULKHEAD FAIL SAFE STRAP ATTACH MOST LOWER BOLT. REMOVED AND REINSTALLED IAW EO B7SDR IPXA11667216Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP CRACK FOUND RUNNING FWD AND AFT. FX BS 955 RHS REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIR IAW EO B767-5350-17922-H, APP D, ORG MATERIAL IS 2024T351-0.750" MACHISDR IPXA11667215Failsafe · damagedINSPECTION TYPE:8C, DURING ACCOMPLISH EO B767-5350-17922-H, BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP INSPECTION, A FASTENER HOLE WAS FOUND WHICH LARGER THAN EO CALL OUT AT LT SIDE. FX BS955 LT SIDE NEAR STR-23L REAR SPAR BULKHEAD SIDE FITTING FASDR IPXA11667214Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR B/H SIDE FITTING, TEE FITTING FOUND CRACKED. FUSELAGE LT BS 955, REAR SPAR B/H SIDE FITTING, TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H, APP C, ORG MATERIAL IS 7075-T73 DIE FORGING, THIS REPAIRSDR IPXA11667213Tee Fitting · crackedFUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, TEE FITTING FOUND CRACKED. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H, APPEND D, ORG. MATERIAL IS 7075-T73 DIE FORGING, THIS REPAIR IS CLSDR IPXA11667209Skin · corrodedINSPECTION TYPE:8C, FUSELAGE LT BS 955 BULKHEAD SIDE FTG - A SLIGHT CORROSION IS FOUND AFTER FAIL SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE TEE FITTING TO THE FAIL SAFE STRAP AREA. FX LT BS 955 BULKHEAD SIDE FITTING, A SSDR IPXA11667208Bulkhead · corrodedINSPECTION TYPE:8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING - A SLIGHTLY CORROSION IS FOUND AFTER FAIL SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO FAIL SAFE STRAP AREA. REMOVED IAW SRM 51-10-02 & REPROTECTED SDR IPXA1667089Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.SDR IPXA1667093Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION AT OTBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 50.SDR IPXA1667092Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD END CAP CRACKED FIBERGLASS. WET LAY UP REPAIR CARRIED OUT IAW RS NR R-57-50-37100 REV A, REFER EO NR B767-5750-42998-A.SDR IPXA1667090Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 50.SDR IPXA11666867Charger · inoperativeAT CRUISE ALT (350) STATUS MSG, MAIN BATTERY CHARGER. T/S C/O, FOUND MAIN BATTERY CHARGER AT FAULT. R & R MAIN BATTERY CHARGER IAW AMM 24-31-02-4, REV 49.1 12/22/10. OPS CHECKED OK.SDR IPXA11666866Skin · damagedFUSELAGE SKIN DAMAGE AT STA 263 AND 265 STR 2R AND 3R. REPAIRED IAW EO B767-5330-42424-B.SDR IPXA11666864Floor Panel · damagedFLOOR PANEL DAMAGED, POS 3 FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693.SDR IPXA11666863Floorboard · damagedINSPECTION TYPE:PS, FLOORBOARD DAMAGED POS3 LT SIDE. FABRICATED PANEL IAW EO B767-5320-9693.SDR IPXA11667147Wedge · damagedINSPECTION TYPE:8C, RT WING - NR 8 SLAT UPPER WEDGE, LWR SURFACE AT MID AREA FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 200, SHEET 8, REV 50.SDR IPXA11666856Floorboard · damagedINSPECTION TYPE:PS, REF D438203 POSITION 4 MAIN DECK RT CENTER FLOOR INTERIM REPAIR TO .7500 INCH HOLE IN , 16 INCHES AFT OF FWD LINE. IDENTIFIED FLOORBOARD AS FROM POSITION 4 RT CENTER FLOORBOARD IAW EO B767-5320- 9693H. FABRICATED A REPLACEMENT FLOORBOARDSDR IPXA11667148Panel · delaminatedINSPECTION TYPE:8C, VERTICAL STAB LT FSS 11.787 TO 92.250 FIXED PANEL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 50.SDR IPXA1667067Floor Panel · crackedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 2 CRACKS AND 5 DENT MARKS AT STA 1041 TO STA 1114, LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALL IAW AMM 53-01-06.SDR IPXA1667097Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 3 PUNCTURES AND 6 DENT MARKS AT STA 1425 TO STA 1540, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1667096Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 3 PUNCTURES AND 8 DENT MARKS AT STA 412 TO STA 540, LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1667095Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 4 PUNCTURES AND 6 DENT MARKS AT STA 654+22 TO STA 690. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1667094Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 4 PUNCTURES AND 4 DENT MARKS AT STA 654+22 TO STA 690 LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1667049Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 5 PUNCTURES AND 3 DENT MARKS AT STA 873 TO STA 933, LBL 77 TO LBL 88. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1666741Display · failedATB - ON CLIMB OUT LOST CAPT'S EHSI SCREEN, ALT SELECTED STILL NO SCREEN. APPROX 2 MINUTES LATER CAPT LOST EADI THEN UPPER EICAS SCREEN. AFTER 30 SECONDS, BOTH CAPT AND F/O SMELLED ELECTRICAL BURNING. FOUND SLIGHT WATER CONDENSATION ON CAPTS EHSI. R & R SAMSDR IPXA1666734Skin · delaminatedINSPECTION TYPE:C, RT WING INBD AFT FLAP UPPER SURFACE INBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW ARM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 49.SDR IPXA1666733Skin · delaminatedINSPECTION TYPE:C, RT WING INBD AFT FLAP UPPER SURFACE OTBD AREA FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 49.SDR IPXA1666640Floor Panel · damagedFLOOR PANEL POS 8L HAS .5" HOLE ON FWD SIDE OF PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA1666639Floor Panel · damagedFLOOR PANEL POS 9R HAS HOLE AT FWD RT SIDE .5" DIAMETER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA1666638Floor Panel · damagedFLOOR PANEL POSITION 2R RT AFT SIDE HAS A 2" X 1" HOLE REF D432651. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA1666735Wing · debondedINSPECTION TYPE:C, RT WING INBD AFT FLAP UPPER SURFACE AT MID AREA FOUND DEBOND. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 1 REV 49.SDR IPXA1666679Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP, T/E WEDGE, LWR SURFACE AT MID AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5(A), FIG 9, REV 49.SDR IPXA1666678Wedge · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP LWR SURFACE T/E WEDGE AT MID AREA DELAMINATION. FIBERGLASS PREPAGE LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 49.SDR IPXA1666731Rib · crackedINSPECTION TYPE:C, RT WING INBD AILERON INBD HINGE SUPPORT RIB UPPER FLANGE FOUND CRACKED. RIB UPPER FLANGE REPAIRED IAW HX RS R-57-50-37081, REV A & EO B767-5740-42723-A JUST AT WS 468.11, ORG MAT DIE FORGING 7075-T73 CRK LENGTH 0.40" FINAL CUTOUT SIZE 0.80 SDR IPXA1666677Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR AT STA 785.9, RBL 10.94 VERTICAL STIFFENER FOUND CRACKED. VERTICAL STIFFENER REPAIRED IAW SRM 57-10-10-2R2. REPAIR 2, FIG 201, REV 49 JUST AT STA 785.9, RBL 10.94 ORG MAT'L BAC1518-912-2024T3511 CRACK LESDR IPXA1666676Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR AT STA 785.9, RBL 32.94 VERTICAL STIFFENER FOUND CRACKED. VERT STIFFENER REPAIRED IAW SRM 57-10-10-2R2. REPAIR 2, FIG 201, REV 49 AT STA 785.9, RBL 32.94 ORG MAT'L BAC1518-749-2024T3511 CRACK LENGTH IS SDR IPXA11666523Skin · dentedDENT NR 1 D449024 AND DENT NR 2 D449025 LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE DENTS. REPAIRED BOTH DENTS USING ONE REPAIR IAW SRM 51-70-10-2R AND EO B767-5 750-41819-B.SDR IPXA11666522Skin · dentedD449026 DENT NR 3 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN DENT REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42592-A.SDR IPXA11666521Skin · dentedDENT 4 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42593-A.SDR IPXA1666287Element · shortedINSPECTION TYPE:ETOP, ATB- ON CLIMB OUT THROUGH FLIGHT LEVEL 14,000, RT ENGINE DUCT LEAK. THEN RECEIVED FWD EQUIPMENT OVERHEAT MSG. CHECKLIST ACCOMPLISHED. T/S IAW FIM 26-18-00, F104 STEP 1 TO 34. FOUND SENSING ELEMENT TS216 SHORTED. R & R TS216 IAW WDM 26SDR IPXA1666288Counterbalance · out of adjustCREW ENTRY DOOR VERY DIFFICULT TO OPEN (DOOR ITSELF, NOT HANDLE). NO FEELING OF "ASSIST" IN RAISING DOOR TO OPEN POSITION. ADJUSTED COUNTER BALANCE IAW MM 52-12-16-5. NO HELP. LUBED CREW ENTRY DOOR IAW MM 12-21-18-3. DOOR OPS CKS GOOD IAW MM 52-12-16-5.SDR IPXA1666285Blade · damagedINSPECTION TYPE:ETOP, BIRD STRIKE DEPARTING VCP AT 5000' MSL. EXCESSIVE LT ENGINE VIBRATION AND NOISE. RETURNED TO VCP. WILL ACCOMPLISH BORO INSP AND REPLACEMENT OF DAMAGED FAN ROTOR BLADES IAW FIM AND AMM.SDR IPXA1666275Floor Panel · dentedMAIN DECK FLOOR PANEL 9L OTBD HAS DENT 1.5 INCH DIA AT ST STA 1263 LBL80. REPLACED MAIN DECK FLOOR PANEL IAW EOB767-5320-9693-H.
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