Boeing 767-34AF

Service difficulty reports · 6,321

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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.

SDR IPXA09657390Angle · crackedINSPECTION TYPE:C RT WING LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 1 INCH. RT WING - LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-Sep 3, 2009 · N311UP · Boeing 76734AF · Wing SparSDR IPXA09657361Support Fitting · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 25 FLOOR PANEL SUPPORT CLIP FOUND CRACK. CRACK LENGTH 1 INCH. AFT CARGO STA 1087 LBL 25 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657360Support Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 FLOOR PNL SUPPORT CLIP FOUND CRACK. CRACK LENGTH 1 INCH. AFT CARGO STA 1087 RBL 25 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657338Attach Angle · crackedINSPECTION TYPE:C MAIN DECK STA 1581 LEFT O/B FLOOR PANEL SUPPORT ATTACH ANGLE FOUND CRACK. CRACK LENGTH 1 INCH. MAIN DECK STA 1581 LEFT O/B FLOOR PANEL SUPPORT ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657322Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE 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.Sep 3, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657312Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412 , LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657311Floor 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.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657310Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657309Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO 690 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657308Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657307Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 875 TO 932, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657306Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657381Angle · crackedINSPECTION TYPE:C LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 0.5 INCH. LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4Sep 2, 2009 · N311UP · Boeing 76734AF · Wing SparSDR IPXA09657380Skin · misrepairedINSPECTION TYPE:C SURVEY SEQ 311-W3-01 LT WING NR 4 SLAT OUTER SKIN L/E 42 INCHES FROM O/B EDGE EXISTING REPAIR DOES NOT CORRELATED TO A SRM. LEFT WING NR 4 SLAT NOSE SKIN BETWEEN OSS 638 TO OSS 645 REPAIRED AS PER UPS EO B767-5750-34944-A AND HX RS R57-43-36Sep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657368Skin · misrepairedINSPECTION TYPE:C SURVEY SEQ 311-F1-02 FX SKIN REPAIR BETWEEN BS 1836 TO 1850 LBL 7 TO LBL 15 AREA. EXISTING REPAIR DOES NOT CORRELATE TO A SRM. FX SKIN REPAIR BETWEEN BS 1836-1850 LBL 7 TO LBL 15 AREA INCORRECT TYPE OF FASTENERS REPAIRED (REPLACED) PER HX RSep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657337Angle · crackedINSPECTION TYPE:C MEC COMPT FLOORBEAM STA 246 ANGLE FOUND CRACKED AT LBL 25. CRACK LENGTH 0.75 INCH. MEC COMPT FLOORBEAM STA 246 ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 25.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657336Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP FOUND CRACK AT RBL 10. CRACK LENGTH 1.5 INCH. MEC COMPT STA 246 FLOORBEAM CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT RBL 10.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657335Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP FOUND CRACK JUST AT LBL 50. CRACK LENGTH 1 INCH. MEC COMPT STA 246 FLOORBEAM CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 50.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657320Floor 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.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657319Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 833 TO 930 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657318Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 550 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657317Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657316Floor 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.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657315Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598 , RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657314Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1207 TO 1344, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657313Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657304Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACK. CRACK LENGTH 0.125 INCH. LT WING - NR 4 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 573.25. THIS IS CLASSIFIED A MAJOR REPAIR WSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657303Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT O/B NOSE SKIN AFT O/B SUPPORT WEB RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RT WING - NR 9 SLAT O/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 641.62 INCH. THIS IS CLASSIFIED AS A MAJSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657302Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). RT WING NR 9 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS573.25". THIS IS CLASSIFIED A MAJOR REPAIR WSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657298Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 40 ( CRACK LENGTH 1.125" ). MEC COMPT STA 246 FLOORBEAM STIFFENER REPAIRED AS PER SRM 53-10-51- 2R4 FIG 201 AT LBL 40. THIS IS CLASSIFIED A MAJOR REPAIR WITH MATERIAL 7075T6-0063. RESep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657249Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED POS 1R. FABRICATED FLOOR IAW B767-5320-9693-F.Aug 30, 2009 · N332UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657248Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED POS 2R. FABRICATED NEW PANEL IAW EO B767-5320-9693-F.Aug 30, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657184Vent · openETOP ATB - AT 11,200 RECEIVED CABIN ALT WARNING AND LATE CABIN AUTO INOP. FORMED QRH FOR BOTH INDICATIONS AND UNABLE TO MAINTAIN CABIN ALT. NO OTHER EICAS MSGS. AFTER RETRIEVING DATA FROM FILGHT DATA RECORDER INFO SHOWED MAIN CARGO DOOR WAS NOT LATCHED COMPLAug 27, 2009 · N332UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA09657240Wedge · damagedINSPECTION TYPE:7C LEFT O/B ELEVATOR LOWER O/B T/E AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-04 PAR 5G, FIG 9, REV 44.Aug 24, 2009 · N307UP · Boeing 76734AF · Elevator Miscellaneous StructureSDR IPXA09657195Panel · delaminatedINSPECTION TYPE:C EMP - VERT STAB LT LWR FIXED PANEL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 44, 51-70-10 REPAIR 4 FIG 201.Aug 24, 2009 · N307UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA09657123Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POS 7R DAMAGED. REPAIRED PER EO B767-5320-34683-A.Aug 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657122Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POS 6 DAMAGED. REPAIRED PER EO B767-5320-34684-A.Aug 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657121Floor Panel · misrepairedINSPECTION TYPE:N/A MCD POS 9 RT OUTBOARD FLOOR PANEL INTERIM REPAIR. FABRICATED FLOOR PANEL PER EO B767-5320-9693-F.Aug 23, 2009 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657251Wedge · damagedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44, REPAIR PATCH SIZE 11 X 7 INCHES.Aug 21, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657194Skin · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER SURFACE I/B TRAILING EDGE AREA, EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5C FIG 10 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657193Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE, EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657192Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657191Skin · damagedINSPECTION TYPE:C RT WING NR 7 SPOILER LWR SURFACE PUNCH HOLE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PAR 4A FIG 10 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · SpoilersSDR IPXA09657186Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER SURFACE LEADING EDGE FAIRING EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657182Floor Support · crackedINSPECTION TYPE:C MAIN DECK FLOOR SUPPORT STA 1582 LBL 75 SUPPORT ANGLE FOUND CRACKED (CRACK LENGTH 1.5 INCH). MAIN DECK FLOOR SUPPORT STA 1582 LBL 75 SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657181Floor Support · crackedINSPECTION TYPE:C MAIN DECK FLOOR SUPPORT STA 1582 LBL 77 SUPPORT ANGLE FOUND CRACK (CRACK LENGTH 1 INCH). MAIN DECK FLOOR SUPPORT STA 1582 LBL 77 SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657126Stiffener · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 LBL 26 BELOW FLOOR, STIFFENER FOUND CRACK. AFT CARGO COMPT STA 1087 LBL 26 BELOW FLOOR, STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657125Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 26 BELOW FLOOR STIFFENER FOUND CRACK. AFT CARGO COMPT STA 1087 RBL 26 BELOW FLOOR STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 21, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657242Support Fitting · crackedINSPECTION TYPE:7C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACKED. RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 20, 2009 · N307UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09657190Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN 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 44.Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge Flaps
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