N308UP

Service difficulty reports · 175

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N308UP' AND registry_match = 'registration'
  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 IPXA10659177Floor Panel · damagedREF MMR NR 10659175, REF D411572, MCD FLOOR PANEL POS 4L HAS .5" HOLE. DAMAGE LOCATED AT STA 654+121, LBL45 AND 10" AWAY FROM EDGE. REPAIR THE DAMAGE IAW SRM53-00-50-2R.Apr 10, 2010 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659172Floor Panel · damagedMAIN DECK FLOOR PANEL POS5L DAMAGED 1.5"X 5/8". LESS THAN 3" AWAY FROM THE EDGE. REF D411571. REPLACED FLOOR PANEL IAW EO B767-5320-9693-G.Apr 10, 2010 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656675Support · crackedINSPECTION TYPE:7C RIGHT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. RIGHT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Jul 7, 2009 · N308UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09656660Fairing · delaminatedINSPECTION TYPE:C RIGHT 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 44.Jul 7, 2009 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656653Slat · debondedINSPECTION TYPE:7C LEFT WING - NR 4 SLAT O/B UPPER CORNER FOUND DEBOND. DEBOND AREA REPAIR PERFORMED AS PER SRM 51-70-10, REPAIR 1, FIG 201, SHEET 1, REV 44.Jul 7, 2009 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656684Skin · crackedINSPECTION TYPE:7C NR 2 PYLON - ACCESS PANEL 442AL CUTOUT SKIN CRACKED. NR 2 PYLON I/B ACCESS FWD HOLE CUTOUT SKIN REPAIRED AS PER HX RS R54-51-36368 REV A AND UPS EO B767-5430-34212-A. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AMS4911-0090IN AJul 6, 2009 · N308UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR IPXA09656683Fairing · delaminatedINSPECTION TYPE:7C LEFT WING - OUTBOARD T/E FLAP L/E INBOARD FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1), FIG 5, REV 44.Jul 6, 2009 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656652Fairing · delaminatedINSPECTION TYPE:7C LEFT WING - O/B FLAP L/E MID FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1), FIG 5, REV 44.Jul 6, 2009 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656651Skin Panel · dentedINSPECTION TYPE:7C LEFT WING L/E PANEL 511PT UPPER SURFACE FOUND DENT. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 2, FIG 203, REV 44.Jul 6, 2009 · N308UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA09656624Attach Angle · crackedINSPECTION TYPE:7C AFT OF BULK CARGO COMPT STA 1582 LBL 81 MAIN DECK FLOORBEAM O/B ATT ANGLE FOUND CRACKED. MAIN DECK DOOR BEAM O/B ATTACH ANGLE AT BS 1582 LBL 81 AREA REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Jul 6, 2009 · N308UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656655Skin · dentedINSPECTION TYPE:7C LEFT WING NR 4 SLAT UPPER SURFACE FOUND DENT. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4, FIG 202, SHEET 8, REV 44.Jul 5, 2009 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656607Attach Angle · crackedINSPECTION TYPE:7C AFT OF BULK CARGO COMPT STA 1582 LBL 80 MAIN DECK FLOORBEAM ATTACH ANGLE FOUND CRACK. MAIN DECK FLOORBEAM ATTACH ANGLE AT BS 1582 LBL 80 AREA REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Jul 5, 2009 · N308UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656598Attach Fitting · crackedINSPECTION TYPE:C MAIN E/E COMPT STA 246 RBL 10 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK (CRACK LENGTH 1.25 INCH). MAIN DECK E/E COMPT STA 246 RBL 10 FLOORBEAM ATTACH CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Jul 5, 2009 · N308UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656674Fitting · crackedINSPECTION TYPE:7C AFT CARGO COMPARTMENT BILGE AREA STA 1087 LBL 26 CLIP FOUND CRACK. AFT CARGO COMPARTMENT BILGE AREA STA 1087 LBL 26 CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656673Fitting · crackedINSPECTION TYPE:7C AFT CARGO COMPARTMENT BILGE AREA STA 1087 RBL 26 CLIP FOUND CRACKED. AFT CARGO COMPARTMENT BILGE AREA STA 1087 RBL 26 CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656659Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B NOSE SUPPORT SKIN FOUND CRACKED (CRACK 0.125 INCH LENGTH). LEFT WING NR 4 SLAT OSS 573.18 AREA NOSE SKIN REPAIRED AS PER SRM 57-43-01- 2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-Jul 4, 2009 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656654Hinge Fitting · crackedINSPECTION TYPE:7C LEFT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FIG FOUND CRACKED. LEFT WING I/B MAIN FLAP I/B AFT FLAP HINGE FIG REPAIRED AS PER SRM 57-53-02- 2R1, FIG 201, REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075TJul 4, 2009 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656650Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 730 TO 833, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656646Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656645Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 690 TO 764, RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656644Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1197+22 TO 1207, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656643Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 730 TO 833, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656642Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 933 TO 870, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656641Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 654+22 TO 690 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656640Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656630Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO STA 1041, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER SRM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656629Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL DAMAGE AT STA 833 TO 930, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656628Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 933 TO STA 970, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656627Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO STA 933, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656626Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1480 TO 1598, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656625Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 970 - 1114 RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656623Floor Panel · damagedINSPECTION TYPE:ETOP MCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO 654+22, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656622Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO STA 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656621Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 283 TO 412 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656620Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO 933, LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656619Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 654+22 TO 690, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656618Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656617Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO STA 550, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656616Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 936 TO STA 985, RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656615Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 368 TO 412, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656614Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 283 TO STA 412, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656613Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 550 TO STA 654+22, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656612Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1207 TO 1344, LBL 33 TO L55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656611Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656610Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 985 TO STA 1087, RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656609Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 764 TO 876, RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F, AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656608Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1370 - 1480, RBL 77 - R88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656605Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL PUNCTURE AT STA 970, LBL 48. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R, FIG 201 REV 44.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656604Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND PUNCTURE AT STA 1197, RBL 82. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R FIG 201 REV 44.Jul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656603Stiffener · crackedINSPECTION TYPE:7C MAIN EQUIPMENT CENTER STA 246 LBL 40 STIFFENER FOUND CRACK. MAIN EQUIPMENT CENTER STA 246 LBL 40 FLOORBEAM ATTACH STIFFENER REPAIRED AS PER SRM 53-10-51-2R-4, FIG 201, REV 44. THIS REPAIR IS CLASSIFIED AS CATEGORY 'B' MAJOR REPAIR AS PER SJul 4, 2009 · N308UP · Boeing 76734AF · Fuselage Miscellaneous Structure
Back to N308UP