N307UP

Service difficulty reports · 212

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 = 'N307UP' 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 IPXA10658495Floor Panel · damagedPOS 9L HAS 1/2 INCH BY 1/4 INCH HOLE AND 2ND HOLE .900 BY .600 LOCATED 2.60 INCH AND 5. 50 INCH FROM OTBD EDGE OF PANEL AND 52 INCH FROM FWD EDGE OF PANEL REPAIRED DAMAGE PER 767 SRM 53-00-50-2R. THIS CLEARS D416520 IAW 767B SRM 53-00-50-2R.Feb 14, 2010 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658492Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 10L. REPAIRED PER SRM 53-00-50-2R.Feb 14, 2010 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658490Floor Panel · damagedMCD FLOOR PANEL DAMGED POS 8R. REPAIRED PER EO B767-5320-9693-G.Feb 14, 2010 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658489Floor Panel · damagedMCD FLOOR PANEL DAMAGED POS 4. REPAIRED PER EO B767-5320-9693-G.Feb 14, 2010 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657446Sliding Window · malfunctionedINSPECTION TYPE:N/A F/O SLIDING WINDOW WILL NOT LOCK. ADJ WINDOW PER 56-11-02-5. OPS CHECKS GOOD.Sep 24, 2009 · N307UP · Boeing 76734AF · Flight Compartment WindowsSDR 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 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 FlapsSDR IPXA09657189Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657188Fairing · delaminatedINSPECTION TYPE:C RT WING O/B FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT O/B PLACE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5.Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657187Fairing · delaminatedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT I/B PLACE. 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 FlapsSDR IPXA09657168Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 20, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657250Panel · crackedINSPECTION TYPE:C LT WING NR 6 SLAT LWR CLOSURE PANEL CRACKED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 44. REPAIR PATCH SIZE 12 X 6 INCHES.Aug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657241Support Fitting · crackedINSPECTION TYPE:7C LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP FOUND CRACKED. LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657238Skin · misrepairedINSPECTION TYPE:C SURVEY SEQUENCE 307-F1-07 BULK CARGO DOOR BETWEEN BS 1434-1447 & STR 25L - 28L AREA SKIN REPAIR DOES NOT CORRELATE TO THE SRM. REPAIR SIZE 12.5 X 14.5 INCHES. BULK CARGO DOOR BETWEEN BS 1434 - BS 1447 & STR 25L - 28L AREA SKIN REPAIRED PER Aug 19, 2009 · N307UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA09657175Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657174Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657173Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO 690, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657165Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657164Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1207 TO 1344, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657162Floor Panel · crackedINSPECTION TYPE:C MCD FLOOR PANEL FOUND CRACK AT STA 977 TO 1043, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657151Skin · crackedINSPECTION TYPE:C LT WING NR 4 SLAT I/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT I/B AREA OSS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01- 2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPAug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657150Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT O/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT O/B AREA OSS 641.49 NOSE SKIN REPAIRED AS PER SRM 57-43- 01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIAug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657252Skin · misrepairedINSPECTION TYPE:C SURVEY SEQUENCE 307-F1-01 FUSELAGE BETWEEN BS 289 TO BS 303 AND STR 24L - 26L AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. FX BETWEEN BS 289-303 & STR 24L-27L AREA SKIN REPAIRED WITHOUT ZERO TIMING AS PER SRM 53-00-01-2R12 REV 44 & BOEIAug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657172Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED 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.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657171Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657170Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657169Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657167Floor Panel · delaminatedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DELAMINATION AT STA 930 TO 975, LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657166Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657163Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, RBL 77 RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657149Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 40 FLOORBEAM ATT STIFFENER FOUND CRACKED (CRACK LENGTH 1.25 INCH). MEC COMPT STA 246 LBL 40 FLOORBEAM ATTACH STIFFENER REPAIRED REF SRM 53-10-51-2R4 REV 44. THIS IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0.063Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657124Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 50 CLIP FOUND CRACK LENGTH 0.75 INCH. MEC COMPT STA 246 LBL 50 CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657111Attach Angle · crackedINSPECTION TYPE:ETOP MEC COMPT STA 246 LBL 25 FLOORBEAM ATT ANGLE FOUND CRACK. MEC COMPT STA 246 LBL 25 FLOORBEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AN INSTALLED AS PER SRM 51-40-02 REV 44.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656177Panel · crackedINSPECTION TYPE:N/A NR 8 SLAT CLOSURE PANEL CRACK 1.5 INCH. REPAIRED PER EO B767-5750-33200B.Jun 1, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09655704Seat Track · damagedINSPECTION TYPE:N/A SEAT TRACK DAMAGED BETWEEN STA 1268 AND 1280 AT RBL 54.75. REPAIRED PER EO B767-5310-33178-B.Apr 27, 2009 · N307UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA09655243Window · stiffINSPECTION TYPE:N/A CAPT L2 SLIDING WINDOW (EMERGENCY EGRESS) EXTREMELY DIFFICULT TO OPEN/CLOSE. ADJUSTED AND TESTED IAW AMM 56-11-02-5. OPS CHECK GOOD.Mar 27, 2009 · N307UP · Boeing 767300 · Flight Compartment WindowsSDR IPXA10658276Coupler · leakingCREW REPORTED CRT HYD QTY EICAS MSG, CRT HYD SYS PRESSURE EICAS MSG, A ND WHILE ON SHORT FINAL RECEIVED A LT YAW DAMPER EICAS MSG. EMERGENCY DECLARED CTR LCCA LEAKING IN RT WHEEL WELL, REMOVED R LCCA TO SET D-5 MM 27-11 -14-4. COMPLETE INSTALLATION OF RT LCCAJan 26, 2009 · N307UP · Boeing 76734AF · Hydraulic System, MainSDR UPS08651369Control Valve · malfunctionedINSPECTION TYPE:ETOP DIVERSION - TO SLC DUE TO CABIN PRESSURIZATION PROBLEM. THE RIGHT PACK FAILED WHILE EN ROUTE TO OAK. RECEIVED AN EQUIPMENT OVERHEAT WARNING AND COULD NOT MAINTAIN CABIN PRESSURE. DECLARED EMERGENCY. PER TECH SUPPORT REQUEST, REMOVED ANJan 3, 2008 · N307UP · Boeing 76734AF · Cabin Cooling System
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