N131UP

Service difficulty reports · 290

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 = 'N131UP' 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 IPXA11166123Seat Track · corrodedINSPECTION TYPE:10YR, SEAT TRACK BETWEEN FR79 AND FR80 AT Y0 IS CORRODED. REPAIRED SEAT TRACK BETWEEN FR79 AND FR80 AT Y0 IAW SRM 53-10-16, PARA 4, FIG 201 AND NR 437577.Mar 30, 2011 · N131UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA11166122Seat Track · corrodedINSPECTION TYPE:10YR, MDCC SEAT TRACK BETWEEN FR79 AND FR80 AT -Y1137.1 IS CORRODED. REPAIRED MDCC SEAT TRACK BETWEEN FR79 AND FR80 AT -Y1137.1 IAW SRM 53-10-16, PARA 4, FIG 201 AND RCD 437583.Mar 30, 2011 · N131UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA11166095Floor Panel · brokenINSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 152SF IS BROKEN. FABRICATED NEW AFT CARGO FLOOR PANEL 152SF IAW EO A300-5320-16407-E.Mar 30, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1165887Floor Panel · exposedINSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 152RF HAS EXPOSED CORE. REPAIRED AFT CARGO FLOOR PANEL 152RF IAW EO A300-5320-38221-B.Mar 30, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166094Floor Panel · dentedINSPECTION TYPE:10YR, BULK CARGO FLOOR PANEL 161MF HAS DENTS. FABRICATED NEW BULK CARGO FLOOR PANEL 161MF IAW EO A300-5320-16407-E.Mar 29, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166093Floor Panel · dentedINSPECTION TYPE:10YR, BULK CARGO FLOOR PANEL 161KF HAS DENTS. FABRICATED NEW BULK CARGO FLOOR PANEL 161KF EO A300-5320-16407-E.Mar 29, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166092Floor Panel · dentedINSPECTION TYPE:10YR, BULK CARGO FLOOR PANEL 161JF HAS DENTS AND IS PUNCTURED. FABRICATED NEW BULK CARGO FLOOR PANEL 161JF IAW EO A300-5320-16407-E.Mar 29, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166044Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL 261AM CRACKED. REPAIRED FLOOR PANEL 261AM IAW EO A300-5320-38221-B.Mar 3, 2011 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158305Skin · gougedINSPECTION TYPE: 4/C REPAIR SURVEY NR 131-W4-01 REPAIR DOUBLER IS GOUGED RT INBD FLAP UPPER OTBD SKIN REPAIR ACCOMPLISHED IAW EA 300-5753-01-A2139, REV. I/R AND UPS EO A30 0-5750-30419-A.Jan 19, 2010 · N131UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158303Floor Panel · misrepairedINSPECTION TYPE: 4/C, BULK PIT FLOORBOARD NR 161HF PREVIOUS REPAIR NOT IAW SRM STANDARDS REPLACE IAW EO A300-5320-16407-D FABBED IAW UPS EO A300-5320-16407-D, APPX. DJan 19, 2010 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158302Floor Panel · misrepairedINSPECTION TYPE:4/C BULK PIT FLOORBOARD 161GF PREVIOUS REPAIR NOT IAW SRM STANDARDS REPLACE IAW EO A300-5320-16407-D. FABED IAW UPS EO A300-5320-16407-D, APPX. D.Jan 19, 2010 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158289Floorboard · misrepairedINSPECTION TYPE:4C BULK PIT FLOOR BOARD 161MF PREVIOUS REPAIR NOT IAW SRM STANDARDS REPLACE FLOORBOARD REF EO-A300-5320-16407. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-D APPENDIX D.Jan 19, 2010 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158288Floorboard · misrepairedINSPECTION TYPE:4C BULK PIT FLOORBOARD 161LF PREVIOUS REPAIR NOT IAW SRM STANDARDS REPLACE FLOORBOARD IAW EO-A300-5320-16407-D. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-D APPENDIX D.Jan 19, 2010 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158299Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 131-W3-01,REPAIR DOUBLER HAS SEVERAL GOUGES REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 FIG 205 REF RCD 384317.Jan 18, 2010 · N131UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158298Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 131-W4-02, REPAIR DOUBLER HAS SEVERAL GOUGES REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 FIG 205 AND EO A300-5750-36420-A.Jan 18, 2010 · N131UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA09157265Rib · crackedLT I/B L/E WING RIB CRACKED. REMOVED AND STARTED INSTALLATION ON LEADING EDGE DIAPHRAGM ON LEFT WING. COMPLETED INSTALLATION ON DIAPHRAGM LT WING LEADING EDGE REF SRM 51-40-30. THIS IS A MINOR REPAIR AND CLEARS D407733.Aug 29, 2009 · N131UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA09156661Slide · defectiveINSPECTION TYPE:N/A ON DEPARTURE, SLIDE STUCK IN PARTIAL ARM. DEFERRED SLIDE PER MEL M404622. ***SDR FILED OPEN***Jul 14, 2009 · N131UP · Airbus A300F4622R · Escape SlideSDR IPXA09156638Floor Panel · damagedINSPECTION TYPE:N/A FWD LOWER PIT RT FLOOR PANEL DAMAGED. REPAIRED PER EO A300-5320-16407-C.Jul 13, 2009 · N131UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08153309Fairing · dentedINSPECTION TYPE:N/A, NR 4 MOVEABLE FLAP FAIRING DENTED OUT OF LIMTS. DETERMINED DAMAGE TO BE THREE DENTS. DENTS MEASURE AS FOLLOWS: DENT FWD IS 1.3" X 1.0, CENTER DENT IS 2.2" X 1.6" & AFT DENT IS .6" X 1.4". INSPECTED AND TAPED DENTS PER EO A300-5720-3052Sep 10, 2008 · N131UP · Airbus A300F4622R · Trailing Edge FlapsSDR UPS07151241Valve · openDIVERSION, NR 1 HP VALVE UNCOMMANDED OPEN. DEFERRED PER MEL. D363807 ASSIGNED. R&R NR 1 ENGINE HP BLEED CONTROL VALVE PER MM 36-11-17-04. DMI CLEARED.Dec 4, 2007 · N131UP · Airbus A300F4622R · Pneumatic Distribution SystemSDR UPS07149844Apu · shutdownCREW DECLARED EMERGENCY INTO SJU AFTER APU AUTO SHUT DOWN AND NR 1 GENERATOR WAS PREVIOUSLY DEFERRED ON M350956. [SUP 05-25-07] ACCOMPLISHED OPS CHECK IAW A300 MM 49-10-00-05. OPS CHECK NORMAL AT THIS TIME. R & R NR 1 GENERATOR CONTROL UNIT IAW A300 MM 24-22May 23, 2007 · N131UP · Airbus A300F4622R · APU Core EngineSDR UPS06147629Light · malfunctionedEMERGENCY EXIT LIGHTS FAILED TO DISARM WITH SWITCH IN THE DISARM POS. CLEANED CONNECTOR ON OVERHEAD PANEL SYSTEM, WORKS NOW NORMAL.Jul 6, 2006 · N131UP · Airbus A300F4622R · Emergency LightingSDR UPS06146769Bulb · inoperativeEMERGENCY EXIT SIGN IN SUPERNUMERARY AREA HAS SEVERAL BULBS INOP. RELAMPED WITH SERVICEABLE BULBS AND TESTED IAW 33-51-00-5. NO DEFECTS NOTED.Apr 27, 2006 · N131UP · Airbus A300F4622R · Emergency LightingSDR UPS06146683Bulb · burned outDISARM LIGHT WILL NOT ILLUMINATE (EMERGENCY LIGHT). T/S TO BURNED OUT BULB; RELAMPED, OPS CHK GOOD, REF A300 M/M 33-50.Apr 12, 2006 · N131UP · Airbus A300F4622R · Emergency LightingSDR UPS06146495Floorbeam · bentMAIN CABIN FLOORBOARD CROSSBEAM BENT AT FS 48 RBL 25. REMOVED AND REPLACED CROSSBEAM PER A300 SRM 51-40-00.Mar 17, 2006 · N131UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR UPS06146511Bracket · crackedAFT CARGO FWD BULKHEAD SIDEWALL PANEL BRACKET CRACKED LBL 60. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-20.Mar 16, 2006 · N131UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146510Bracket · crackedAFT CARGO FWD BULKHEAD SIDEWALL PANEL BRACKET CRACKED RBL 60. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-20.Mar 16, 2006 · N131UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146494Bracket · crackedAFT CARGO FWD BULKHEAD SIDEWALL PANEL BRACE CRACKED, BL 0. REMOVED AND REPLACED BRACE PER A300 SRM 51-40-20 & 51-40-00.Mar 16, 2006 · N131UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146493Bracket · crackedAFT CARGO FWD BULKHEAD SIDEWALL PANEL BRACE CRACKED, RBL 30. REMOVED AND REPLACED BRACE PER A300 SRM 51-40-20 AND 51-40-00.Mar 16, 2006 · N131UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146532Spar · crackedFOUND LEFT WING AFT OF REAR SPAR O/B SIDE OF RIB 16 WEB CRACKED. REMOVED AND REPLACED RIB PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing SparSDR UPS06146513Support · crackedSTIFFENER O/B OF STA 1132/RIB NR 16 FOUND TO BE CRACKED APPROX 1" LOWER FWD CORNER RADIUS (RT WING). REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR UPS06146512Stiffener · crackedO/B OF RIB NR 9, RT WING, STIFFENER HAS A CRACK FROM LOWER RADIUS TO FWD RADIUS OF ATTACHING POINT, LOWER WING AREA I/B OF TRACK NR 3. REMOVED AND REPLACED RIB O/B OF RIB NR 9 RT PER A300 SRM 51-40-00 AND 51-40-21.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR UPS06146509Support · crackedFOUND LT WING AFT OF REAR SPAR INBD SIDE OF RIB 16, WEB CRACKED. REMOVED AND REPLACED SKIN SUPPORT PER A300 SRM 51-20-00 AND 51-24-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR UPS06146508Web · crackedFOUND LT WING BETWEEN RIB 9 AND RIB 10 AFT SECTION OF WEB CRACKED (AFT OF REAR SPAR). REMOVED AND REPLACED WEB STIFFENER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR UPS06146507Stiffener · crackedSTIFFENER AT STA 1132/ RIB 16 (ON THE RT WING) FOUND TO BE CRACKED APPROX 1" FROM FWD LOWER RADIUS AREA. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00 AND 51-24-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR UPS06146492Rib · crackedINSPECTION TYPE:5YR LT WING KRUEGER FLAP AREA CURVED DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622R · Leading Edge DevicesSDR UPS05145259Cowling · damagedNR 2 ENG OTBD FAN COWL HAS HEAT DAMAGE. REMOVED AND REPLACED NR 2 ENG OTBD FAN COWL REF MM 71-13-02-4.Jul 17, 2005 · N131UP · Airbus A300F4622R · Engine Air Intake SystemSDR UPS04142364Control Unit · false indicationAFTER TAKEOFF FROM CAE AT 2,500 FT THE CREW RECEIVED A NR 2 FIRE INDICATION LIGHT. THE CREW MADE THE DECISION TO RETURN BACK TO CAE. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-12-11-4.May 12, 2004 · N131UP · Airbus A300F4622R · Fire DetectionSDR UPS03140660Power Supply · failedAUTONOMOUS STANDBY POWER SUPPLY UNIT FAILED BITE TEST R&R AUTONOMUS STANDBY POWER SUPPLY POWER M/M 52-73-18. THIS CLEARS M 259193 PLACARD REMOVED.May 5, 2003 · N131UP · Airbus A300F4622R · Door Warning SystemSDR UPS02139922Sensor · inoperativeLT HYD PUMP FAILED. NR 1 HIGH PRESS BLEED VALVE LIGHT ILLUMINATED. EMERGENCY DECLARED. *SUPPLEMENTAL* REACTIVATED SYSTEM PER DMP 36-11-03. REPLACED HP SENSOR 47HA PER AMM 36-11-23. BITE TESTED PER AMM 36-11-00, CHECKS GOOD.Nov 19, 2002 · N131UP · Airbus A300F4622R · Pneumatic Distribution System
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