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 IPXA11665180Floor Panel · dentedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 7 PUNCTURES AND 9 DENTS MARKS AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11665179Floor Panel · dentedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 9 PUNCTURES AND 11 DENT MARKS AT STA 412 TO 550, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11665163Floor Panel · dentedINSPECTION TYPE:C, DMI D418753, MCD FLOOR PANEL DAMAGE AT POSITION NR 14 AT STA 1480 - 1598, RBL 11" TO RBL 33". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11665162Floor Panel · dentedINSPECTION TYPE:C, DMI D418752, MCD FLOOR PANEL DAMAGED AT POSITION NR 14, STA 1480 TO 1598, LBL 11" TO LBL 33". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11665159Floorbeam · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246, RBL 10, FLOORBEAM ATTACH CLIP FOUND CRACKED. FX MAIN EQUIPMENT CTR STA 246, RBL 10, FLOORBEAM ATTACH CLIP. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 49.SDR IPXA1665099Floorbeam · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246 LBL 25" FLOORBEAM ANGLE FOUND CRACKED. FX MAIN EQUIPMENT CTR STA 246 LBL 25" FLOORBEAM ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 49.SDR IPXA1664979Escape Rope · out of trackROPE END HAD FALLEN OUT OF TRACK IN DOOR CUT OUT. STOWED ROPE END BACK IN TRACK IAW AMM 25-61-04-2.SDR IPXA1664781Packing · brokenATB - C SYS HYD QTY LIGHT FOLLOWED BY C SYS HYD PRESSURE EICAS MESSAGE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. FOUND RT LCCA FILTER COVER PACKING BROKEN. REPLACED PACKING AND LEAK CHECK OK. SERVICE RESERVOIR TO FULL. REF IPC 27-11-14-03, ITEM 140.SDR IPXA11664856Structure · crackedINSPECTION TYPE:C, NR 1 PYLON LT INTERIOR NACELLE STA 285 MOUNTING CLIP FOUND CRACKED. NR 1 PYLON LT INTERIOR NACELLE STA285 MOUNTING CLIP REPLACED IAW SRM51-10-02 AND INSTALLED IAW SRM 51-40-02.SDR IPXA11664858Fairing · delaminatedINSPECTION TYPE:C, RT 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 49.SDR IPXA11664857Panel · elongatedINSPECTION TYPE:C, LT WING NR 5 SLAT LWR CLOSURE PANEL RIVET HOLE ELONGATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5K, FIG 16,
REV 49 .SDR IPXA11664649Skin · damagedDAMAGE BY GROUND PERSONNEL AT STA 1395. FUSELAGE SKIN REPAIR AT STA 1395, STR 33L TO STR 37L ACCOMPLISHED IAW EO B767-5330-41275-A. ACFT OK FOR SERVICE.SDR IPXA1664790Angle · crackedINSPECTION TYPE:C, MAIN EQUIPMENT CTR STA 246, LBL 50", VERTICAL CLIP FOUND CRACKED. MAIN EQUIPMENT CTR STA 246, LBL 50" VERTICAL CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV.49.SDR IPXA1664789Angle · crackedINSPECTION TYPE:C, MAIN EQUIPMENT CTR STA 246, LBL 25", VERTICAL ANGLE FOUND CRACKED. MAIN EQUIPMENT CTR STA246, LBL25" VERTICAL ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 49.SDR IPXA1664737Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL ON FOUND 9EA PUNCTURES AND 3 DENTS MARKS AT STA 975 TO 1114, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.SDR IPXA1664736Floor Panel · crackedINSPECTION TYPE:C, FLOOR PANEL FOUND CRACK AND WITH 7EA PUNCTURES AT STA 930 TO 975 LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED AS IAW AMM 53-01-06.SDR IPXA11664838Web · drilledINSPECTION TYPE:C, HOLES DRILLED ON STA 785.9, RBL10.94, WING CTR SECTION FRONT SPAR VERT WEB AREA DURING STFFENER REPAIR. WING CTR TANK FRONT SPAR WEB REPAIRED IAW R57-10-36925 & B767-5710- 41478 JUST AT STA785.9, RBL10.94, ORG MATL 2024T3BARE-0090IN CHEM-MISDR IPXA11664566Bulb · inoperativeEMERGENCY LIGHTS UNARMED LIGHT BULB INOP. RELAMPED EMERGENCY LIGHT UNARMED LIGHT REF AMM 33-13-00-2.SDR IPXA1664522Wedge · dentedLT HAND OTBD FLAP T/E WEDGE HAS DENT AND DEBONDED AT STA 254.69. REPAIRED IAW EO B767-5750-40481-B.SDR IPXA11664484Warning Light · illuminatedDIVERSION - EICAS MSG FLAP/SLAT ELEC DISPLAYED AFTER TAKEOFF. T/S C/O IAW FIM 29-51-00, FIG 114, SH 1 BLOCK 1 & 21. NO FAULTS NOTED, SYS OK. FIM REV 48.SDR IPXA11664551Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 49.SDR IPXA11664550Tee Fitting · misinstalledINSPECTION TYPE:C, FX BS 955 RT SIDE TEE FITTING SHORT EDGE MARGIN FOUND AT HORIZ FLANGE AFT INBD AREA. FX BS 955, RT SIDE TEE FITTING SHORT EDGE MARGIN CONDITION IS STRUCTURALLY ACCEPTABLE AS A PERMANENT REPAIR. A NEW TEE FITTING REPLACE IAW EO B767-5350-17SDR IPXA11664543Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED AT INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 49.SDR IPXA1664496Rib · crackedINSPECTION TYPE:C, RT WING - NR 10 SLAT INBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.063" APPROX. RIB AT OSS 723.9 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & RSDR IPXA1664495Rib · crackedINSPECTION TYPE:C, RT WING- NR10 SLAT OTBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.006" APPROX. RIB AT OSS792.94 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & REPSDR IPXA1664497Rib · crackedINSPECTION TYPE:C, RT WING L/E OSS 648.595, NR 9 SLAT OTBD ACTUATOR OTBD SUPPORT RIB FWD FLANGE LWR AREA FOUND CRACK. RT WING L/E OSS648.595 NR 9 SLAT OTBD ACTUATOR OTBD SUPT RIB FLANGE REPAIRED IAW HX RS R57-00-36911, REV A & EO B767-5710-41209-A, ORG MAT'LSDR IPXA11664546Angle · crackedINSPECTION TYPE:C, BULK CARGO COMPT STA 1581, RT INBD CABIN LWR SPLICE ANGLE FOUND CRACKED. BULK CARGO COMPT STA 1581 RT INBD CABIN LWR SPLICE ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 49.SDR IPXA11664542Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 930 TO STA 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA1664521Failsafe · crackedINSPECTION TYPE:C, FX BS 955 RT FAIL SAFE STRAP FOUND CRACK AT 5 O/C POSITION AND CORROSION FROM 6 TO 10 O/C POSITION. FUSELAGE STA 955 RT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO NO B767-5350-17922-H APPENDIX D.SDR IPXA1664519Tee Fitting · corrodedINSPECTION TYPE:C, FX BS 955 RT T-FITTING FOUND CORROSION FROM 6 TO 10 O/C POSITION. T-FITTING REPLACED & INSTALLED IAW SRM 51-10-02, REV 49 & EO B767-5350-17922-H APPENDIX 'D' ORG MAT'L BAC1505-100900-7075T73511 CORROSION JUST AROUND FASTENER HOLE. A NEW FSDR IPXA1664516Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES AND 3EA DENT MARKS AT STA 1540 TO STA 1598, LBL 55 TO LBL 88. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA1664515Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 1351 TO STA 1480, LBL 11 TO RBL 11. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664458Rib · crackedINSPECTION TYPE:C, LT WING INBD AILERON INBD SUPPORT RIB OTBD FLANGE FOUND CRACKED. LT WING INBD AILERON INBD SUPT RIB OTBD FLANGE REPAIRED IAW HX RS NR R-57-00-36909 REV A AND EO B767-5740-41154-A, ORIGINAL MATERIAL IS 7075T73 FORGING, CRK LENGTH IS 0.45", CSDR IPXA11664453Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 11EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 985 TO STA 1090, LB 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664452Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 8EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 873 TO STA 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664451Floor Panel · crackedINSPECTION TYPE:C, FLOOR PANEL FOUND 5EA PUNCTURES AND CRACK AT MIDDLE TOGETHER WITH DENT RUNNING THROUGH AT STA 933 TO STA 985, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664450Floor Panel · brokenINSPECTION TYPE:C, FLOOR PANEL FOUND BROKEN AT STA1041 TO STA1114, LBL33 TO LBL55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664449Floor Panel · puncturedMCD FLOOR PANEL FOUND 9EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 975 TO STA 1114, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664549Fitting · crackedINSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 5 O/C POSITION AT FAIL SAFE STRAP APPROX .2500" IN LENGTH. FUSELAGE STA 955 LT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-H, APPENDIX C.SDR IPXA1664520Fitting · crackedINSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 4 O/C AND 5 O/C POSITION APPROX I/8" IN LENGTH AND FOUND CORROSION AROUND HOLE AT TEE FITTING. TEE FITTING REPLACED & INSTALLED IAW SRM 51-10-02, REV 49 & EO B767-5350-17922-H ASDR IPXA1664493Skin · crackedINSP TYPE:C RT WING - NR 10 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 792.5 ORG MAT'L 7075T6-0063" CRACK LENGTH 0.154" DAMAGE CUTOUT 8.875" X 7.125" THIS CLASSIFIED AS MAJOR REPAIR WITH 7075T6-SDR IPXA1664492Skin · crackedINSP TYPE:C RT WING - NR10 SLAT INBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIR IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 723.9 ORG MAT'L 7075T6-0063" CRACKED LENGTH 0.503" DAMAGE CUTOUT 8.875"X 7.25" THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 707SDR IPXA1664491Skin · crackedINSPECTION TYPE:C, RT WING NR9 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. RT WING NR9 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.5955" DAMAGE CUTOUT IS 8.875" X 7.375". THISSDR IPXA1664490Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 49 AT OSS 641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.554" DAMAGE CUTOUT 8.875"X 7.375" THIS CLASDR IPXA11664545Fitting · crackedINSPECTION TYPE:C, RT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD. RT BS 955 REAR SPAR BULKHEAD FITTING AREA FASTENER REMOVED AND REINSTALLED IAW EO B767-5350-17922, APPENDIX D, FIG 6 FOR FURTHER CONFIRMATION BSDR IPXA11664544Fitting · crackedINSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD. LT BS 955, REAR SPAR BULKHEAD FITTING AREA FASTENER REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPENDIX C, FIG 6 FOR FURTHER CONFIRMATIONSDR IPXA11664472Stiffener · crackedINSP TYPE:C, FWD CARGO COMPT -WING CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER CRACKED AT RBL32-94 & BS 785-9. STIFFENER REPAIR IAW HX RS R57-10-36906 REV A & EO B767-5710-41205-A ORG MAT'L BAC1518-749-2024T3511 CRK LENGTH 2.25" CUTOFF LENGTH 16.5" CLASSIFIESDR IPXA11664084Floorboard · damagedFLOORBOARD DAMAGED, POS 6L. FABRICATED NEW FLOOR.SDR IPXA11664076Floor Panel · damagedFLOOR PANEL DAMAGED, POS 13 LT, FABRICATED NEW PANEL.SDR IPXA11664037Control Cable · icedCREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. R & R RT POSITION MODULE CABLES AND LOWER TERMINAL ASSY/ TURNBUCKLE
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