N430UP

Service difficulty reports · 270

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 = 'N430UP' 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 IPXA10561565Bracket · crackedINSPECTION TYPE:C2, NAC-STRUT NR 1 STA 203-85 INBD SIDE VERTICAL CHANNEL HAS ATTACH LOWER ANGLE BRACKET CRACKED. R & R INBD SIDE VERTICAL CHANNEL IAW SRM 51-10-02, SRM 5 51-40-02.Jul 24, 2010 · N430UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10561564Channel · chafedINSPECTION TYPE:C2, NAC-STRUT NR1 STA 203.85 INBD SIDE VERTICAL CHANNEL HAS EXTERIOR SURFACE CHAFED. R & R NAC STRUT INBD SIDE VENT CHANNEL.Jul 24, 2010 · N430UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10561537Splice · chafedINSPECTION TYPE:C2, CHAFING ON NR 2 PYLON STRUCTURE AT UPPER INBD CORNER OF AFT MATING SURFACE FOR NR 2 PYLON FAIRING NR 441AT REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-02, SRM51-40-08.Jul 24, 2010 · N430UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10562098Frame · crackedINSPECTION TYPE:C2, AFT LWR CARGO DOOR HAS IMPACT DAMAGE AT AFT INBD LWR FRAME. R & R LOWER AFT CARGO DOOR BEAM IAW SRM 51-40-05-0G, SRM 51-40-08-0G, SRM 52-30-02-1A1, AMM 51-41-00-2.Jul 23, 2010 · N430UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA09556700Skin · gougedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGE AT FS 648 STRINGER 23L. REPAIRED DAMAGE SKIN IAW B757 SRM 53-30-01-2R REPAIR 3 AND EO B757-5 330-34287. REFERENCE LOG PAGE 298659-1 AND NRC 354160. THIS CLEARS THIS ITEM.Jul 18, 2009 · N430UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09556601Skin · dentedINSPECTION TYPE:N/A DENTS ON RT SIDE OF FUSELAGE BETWEEN STA 460 AND 480 STR 23R AND 24R. REF D403923 AND LOG PAGE 210799. REPAIRED IAW EO B757-5330-34196-A. DEFERRAL REQUIRED FOR REPEAT INSP FOR REPAIR DOUBLER.Jul 12, 2009 · N430UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555862Battery Pack · inoperativeFOUND DURING ASE EMERGENCY LIGHT INOP. ILLUMINATES BUT WITHIN A FEW SECONDS SELF EXTINGUISHES DURING TEST. REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-07-2. OPS CHECK GOOD.May 13, 2009 · N430UP · Boeing 75724APF · Emergency LightingSDR IPXA09555709Module · faultyINSPECTION TYPE:N/A HOT CUP CAUSED BURNING SMELL AND SMOKE WITH HOT CUP ON. TURNED HOT CUP OFF WHICH PUT OUT SMOKE. DEFERRED MODULE ASSY AS INOP PER B757-200 NEF LIST 25-20-25-30-01. CONTROL NUMBER M399714 ASSIGNED. PLACARD INSTALLED. FOUND THE OVEN/HOT CApr 28, 2009 · N430UP · Boeing 75724APF · Buffet/GalleysSDR UPS08553412Light · inoperativeINSPECTION TYPE:N/A ENTRY DOOR EMERGENCY LIGHT HAS 4 LAMPS OUT. RELAMPED EMERGENCY EXIT SIGN PER AMM 33-51-01-2.Sep 27, 2008 · N430UP · Boeing 75724APF · Emergency LightingSDR UPS08552929Skin · dentedINSPECTION TYPE-C, RT IB MAIN FLAP UPPER SURFACE JUST OB OF AFT FLAP HAS MULTIPLE SMALL DENTS. MEASURED ALL DENTS ON RT IB FLAP UPPER SURFACE IAW SRM 57-53-01- 1A, DETAIL VII, FOUND (1EA) DENT AT GRID LOCATION "J5" TO BE OUT OF LIMITS. MEASUREMENT FOR THE DJul 20, 2008 · N430UP · Boeing 75724APF · Trailing Edge FlapsSDR UPS07550681Escape Rope · out of positionINSPECTION TYPE:N/A ESCAPE ROPE NEEDS TO BE PACKED. REPACKED ESCAPE ROPES PER B757 AMM 25-61-00-4.Sep 17, 2007 · N430UP · Boeing 75724APF · Emergency EquipmentSDR UPS07548841Bleed Valve · odorBURNING SMELL DETECTED DURING FLIGHT AFTER R ENG BLEED VAL DISPLAYED, FOLLOWED FIM 36-10-00 FIG 110. REPLACED RT ENG HPSOV PER MM 36-11-07. OK TO CONTINUE.Jan 4, 2007 · N430UP · Boeing 75724APF · Compressor Bleed ValveSDR UPS06547837Doubler · mismanufacturedNR 2 PYLON LT AFT DOUBLER GAS SHORT E.D. ON FWD END TRIMMED AND CHAMFER DISCREPANT DOUBLER-TRIMMED APPROX 0.75 MANUFACTURED A NEW FILLER BASE ON 311N 3401-6. INSTALL 311N3401-15 DOUBLER INSTALL FILLER IAW EA 757-5410-27-A1521.Aug 22, 2006 · N430UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR UPS06547862Frame · dentedDENT IN AFT CARGO FUSELAGE FRAME STA 1480, S26L. DIMENSIONS OF THE DENT = 1.2"L BY 1.0"W BY 0.063"D. THE DISTANCE B/W THE CTR OF THE DENT TO THE FLOOR TRANSITION PANEL IS 6.85". THE DISTANCE B/W THE CENTER OF THE DENT AND EDGE OF THE PROD SPLICE ANGLE IS 9.Aug 10, 2006 · N430UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547861Frame · dentedDENT IN AFT CARGO FUSELAGE FRAME STA 1540 BET S25L TO S26L. DIMENSIONS OF THE DENT NEAR THE FLOOR TRANSITION PANEL IS 0.80"L BY 1.0"W BY 0.012"D. THE DIMENSIONS OF THE DENT NEAR THE PROD SPLICE ANGLE IS 1.0" BY 1.0"W BY 0.036"D. DISTANCE B/W CENTER OF BOTH DAug 10, 2006 · N430UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547860Frame · dentedDENT IN AFT CARGO FUSELAGE FRAME STA 1480, S26R. DIMENSIONS OF THE DENT ARE 1.1"L BY 1.1"W BY 0.042"D. THE DISTANCE B/W CENTER OF THE DENT TO THE EDGE OF FLOOR PANEL IS 3.65". THE DISTANCE B/W CENTER OF THE DENT AND PROD SPLICE ANGLE EDGE IS 11.0".Aug 10, 2006 · N430UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547859Frame · dentedDENTS IN AFT CARGO FUSELAGE FRAME STA 1280, BET S25R TO S26R. DIMENSIONS OF THE DENT = 1.9" BY 1.0"W BY 0.035"D THE DISTANCE FROM THE CENTER OF THE DENT AND FLOOR TRANSITION PANEL IS 9.2" AND THE DISTANCE B/W CENTER OF DENT TO THE EDGE OF PROD SPLICE IS 6.1".Aug 10, 2006 · N430UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547848Frame · dentedDENTS IN AFT CARGO FUSELAGE FRAME STA 1540 BET S25R TO S26R. REPAIRED FRAME PER FINAL EA NR 757-5362-27-A1518 AND UPS EO NR B757-53 10-24991-A.Aug 10, 2006 · N430UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS00532239Bypass Valve · intermittentINSPECTION TYPE: N/A, DURING APPROACH TO BFI, T/E FLAP DISAGREE MESSAGE AT FLAPS LESS THAN 1 DEGREE CHECKLIST RUN & LANDING AT BFI FOUND T/E FLAP BYPASS VALVE INTERMITTANT INOP. REMOVED AND REPLACED VALVE.Apr 12, 2000 · N430UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR UPS96521233Skin · damagedINSPECTION TYPE-3C, FIBER IS DAMAGED ON THE RT ELEVATOR LOWER TRAILING EDGE 68 INCHES OUTBOARD FROM INBOARD END. REPAIRED PER SRM 55-20-01, 51-70-04, 51-20-05 AND SRM 51-40-02.Oct 3, 1996 · N430UP · Boeing 75724APF · Elevator, Plate/Skin
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