N314UP

Service difficulty reports · 137

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 = 'N314UP' 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 IPXA10658073Attach Fitting · crackedINSPECTION TYPE:SPV AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR RBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 RBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.Jan 6, 2010 · N314UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10658072Skin · crackedINSPECTION TYPE:C-RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT INBD AREA AT OSS573.125 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLASSIFIED AS Jan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658071Skin · crackedINSPECTION TYPE:SPV-LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV 45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.5" THIS REPAIR IS CLASSIFIED ASJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658070Skin · crackedINSPECTION TYPE:SPV-LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS573.25 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIEDJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658069Skin · crackedINSPECTION TYPE:SPV-LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT O/B AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 45. CRACK LENGTH IS 0.090" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658068Skin · crackedINSP TYPE:SPV-LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.61 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658067Skin · crackedINSPECTION TYPE:SPV-RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT OTBD AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV45. CRACK LENGTH IS 0.100" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658066Skin · crackedINSP TYPE:SPV- RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.160" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658065Skin · crackedINSPECTION TYPE:C - RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT NR 10 SLAT INBD AREA AT OSS724.35 NOSE SKIN REPAIRED AS IAW SRM 57-43-01-2R2 FIG201 REV45 ORG MATL IS CLAD7075T6-0.063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.12Jan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658089Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 873-932 R77 TO R88 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 30, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658094Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1370-1480 R33 TO R55. FLOOR PANEL FABRICATED EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658093Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L11 TO R11 FOUND DAMAGED. FLOOR PANEL FABRICATED, EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658092Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L33 TO L55 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658091Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1480-1598 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658090Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 412-540 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658088Floor Panel · damagedINSPECTION TYPE: 7C, MCD FLOOR PANEL FOUND DAMAGE AT STN 1197+22 - 1207 L55 TO L77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658087Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1197+22 - 1207, R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658086Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1114 TO 1197+22 R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658085Floorboard · puncturedINSPECTION TYPE:7C DMI NR D415075 POSITION 5 HAS A 1/2" HOLE IN THE CENTER FLOORBOARD. FLOORBOARD FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658084Floor Panel · puncturedINSPECTION TYPE:7C DMI NR D415072 POSITION 11R MCD FLOOR HAS A 3/16" HOLE. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658083Floor Panel · puncturedINSPECTION TYPE:7C DMI NR D415073 POSITION 7R MCD HAS 2 HOLES, ONE 3/16" AND THE OTHER 1/2". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657964Control Panel · defectiveINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED & REPLACED OVERHEAD EMERGENCY LIGHT CONTROL PANEL. OPS CHECKED GOOD PER MM 33-54-08-4.Nov 26, 2009 · N314UP · Boeing 76734AF · Emergency LightingSDR IPXA09656210Light · inoperativeEMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN IN THE OFF POSITION. PERFORMED TEST OF EMERGENCY LIGHTS REF AMM 33-51-00-5. OPS CHECK NORMAL.Jun 4, 2009 · N314UP · Boeing 767300 · Emergency LightingSDR UPS09654641Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 964 RBL 4. REPAIRED PER EO B767-5320-32226-A.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654640Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 1096. REPAIRED PER SRM 53-00-50-2R.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654639Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 486 AND 491 LBL 84. REPAIRED PER EO B767-5320-32227-A.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654638Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 694. REPAIRED PER SRM 53-00-50-2R.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08652624Module · malfunctionedRUDDER TRIM STUCK AT 4 UNITS. T/S IAW FIM 27-21-00 FIG 106 FOUND RUDDER TRIM CONTROL PANEL FAULT. R/R AILERON AND RUDDER TRIM CONTROL MODULE IAW MM 27-21-23-2. OPS GOOD.Jul 1, 2008 · N314UP · Boeing 76734AF · Rudder Tab Control SystemSDR UPS08651944Skin · puncturedINSPECTION TYPE:C LEFT MLG DOOR INNER SURFACE FOUND PUNCH HOLE AT O/B AREA AS MARKED. COMPOSITE REPAIR CARRIED OUT AS PER HX RS#R-52-80-35973A AND UPS ENGINEERING FILE 767-32-20012 THE REPAIR PROCEDURE REFER SRM 51-70-05 PAR 5A (1) AND HX PROCESS CARD CONTROLMar 21, 2008 · N314UP · Boeing 76734AF · Landing Gear DoorsSDR UPS08651940Stiffener · crackedINSPECTION TYPE:C FX- MEC STA 246 LBL 40 CABIN FLOORBEAM STIFFENER FOUND CRACK (CRACK LENGTH 2"). FX MEC STA 246 LBL 40" CABIN FLOORBEAM STIFFENER REPAIRED AS PER SRM 53-10-51-2R4 FIG 201, REF UPS MPI P19656.Mar 21, 2008 · N314UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS07650667Engine · bird ingestionINSPECTION TYPE: ETOP FOD - BIRD STRIKE NR 1 ENGINE. EMERGENCY DECLARED. ON SHORT FINAL CREW REPORTED BIRD INGESTION IN NR 1 ENGINE. ENGINE VIBRATION REACHED 3.8 AND WAS REDUCED TO IDLE. A/C IS OOS. FOUND DAMAGE BLADES 24,25,26,27 BEYOND REPAIR. INSTALLSep 16, 2007 · N314UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS07650416Apu · malfunctionedINSPECTION TYPE:ETOP APU INOP, WILL NOT START DEFERRED PER MEL 49-11-1-0-2. INSTALLED NEW ECU, NO HELP. PLACARD INSTALLED. D356179 *SUPPLEMENTAL SDR* APU OPS CHECK IAW AMM 49-11-00 SATISFACTORY. DMI 356179 NOW CLOSED.Aug 8, 2007 · N314UP · Boeing 76734AF · APU Core EngineSDR UPS07650389Connector · damagedINSPECTION TYPE:ETOP LT ENGINE PRSOV INOP. FOUND CONNECTOR D17066P RUBBER DETERIORATED AND PIN 1 LOCK BROKEN. REMOVED AND REPLACED CONNECTOR PER WEM 36-11-62 & CHECKED PER MM 36-11-005 & ALL CHECKS NORMAL. ALL VALVES RETURNED TO NORMAL CONFIGURATION.Aug 1, 2007 · N314UP · Boeing 76734AF · Pneumatic System WiringSDR UPS05644140Smoke Goggles · crackedLEFT SUPERNUMERARY SMOKE GOGGLES CRACKED. REMOVED AND REPLACED SMOKE GOGGLES.Mar 19, 2005 · N314UP · Boeing 76734AF · Emergency EquipmentSDR UPS02639934Strut · failedAIR TURN BACK DUE TO NOSE GEAR DOOR UPLATCH BROKE DURING GEAR RETRACTION WITH VIBRATION. FOUND RT NOSE GEAR DOOR STRUT ASSY FAILED INTERNALLY.Nov 26, 2002 · N314UP · Boeing 767300 · Landing Gear Door Retract SectionSDR UPS01637321Panel · crackedINSPECTION TYPE:IN L-SHAPED CRACK IN NR 6 L/E SLAT LOWER SIDE, FWD OF INBOARD TRACK. REPAIRED SLAT CLOSE OUT PANEL AS PER SRM 51-70-07.Nov 20, 2001 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR UPS01635816Stringer · crackedCRACK FOUND DURING HFEC INSP OF GOUGE AT STA 460 STR 31R REMOVED FASTNERS IN AREA COMMON TO REPAIR REINSTALLED FASTNERS IAW BOEING 767 SRM 51-40-00 INTERIM REPAIR HAS BEEN RECLASSIFIED AS PERMANENT REPAIR PER BOEING AND UPS EO B767 5330-14262May 7, 2001 · N314UP · Boeing 767300 · Fuselage Main, Longeron/Stringer
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