N402UP

Service difficulty reports · 329

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 = 'N402UP' 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 IPXA2026100786152Support Angle · crackedNR 2 PYLON AFT FAIRING, ACCESS PANEL 445AR, FWD, LOWER CUTOUT AREA HAS A CRACKED SUPPORT CLIP. INSTALLED 1EA NEW SUPPORT CLIP P/N:313N3052-17 B/N:0004513959 ON #2 PYLON AFT FAIRING (ACCESS 445AR) FWD LOWER CUTOUT AREAREF. B757-200 SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026100574510Skin · chafedAPU DOOR 316AR OUTER SKIN AND INNER STRUCTURE OIL SOAKED, DIRTY AND DEBRIS WITH AREAS OF LOOSE, BLISTARD AND PEELING UP PAINT THAT REQUIRES REMOVAL THIS ALSO INCLUDES AROUND DOOR EDGES. REMOVAL AND INSTALLATION.Sep 10, 2026 · N402UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2026100675524Support · gougedAPU DOOR 316AR FIRE-LOOP, SUPPORT RAIL AFT END GOUGED. REPLACED SUPPORT RAIL AT APU DOOR 316AR FIRE-LOOP, IAW SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026100276207Bulkhead · dentedMAJOR REPAIR, APU COMPARTMENT STA 1885 BULKHEAD REPAIR DOUBLE 10" INCHES RIGHT OF LIGHT SWITCH DENTED IN AND EDGES ROLLED UP. RL019 VERIFIED STEPS 22 AND 23 RII GMM 04-02Sep 10, 2026 · N402UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026092288146Bracket · crackedAFT CARGO APU DUCT BRACKET BROKEN LH OTBD TUNNEL BS 1220. REMOVED AND REPLACED 1EA BROKEN DUCT BRACKET REF. B75-200 SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026092286010Angle · crackedNR 2 PYLON PANEL LANDING O/B SIDE (ACCESS 445AR) LOWER SUPPORT CLIP IS CRACKED. INSTALLED 1 EA NEW ANGLE CLIP AT NR 2 PYLON PANEL LANDING O/B SIDE FOR ACCESS PANEL 445AR, LOWER SUPPORT AREA, IAW B757-200 SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026091476662Support Bracket · corrodedWIRE HARNESS CLAMP SUPPORT BRACKETS ATTACHED TO BS 1885 BULKHEAD HAVE LIGHT CORROSION AND MISSING PROTECTIVE FINISH.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026091488064Strap · corrodedAFT CARGO CEILING STABILIZATION STRAP RT OTBD SIDE BS 1420 HAS CORROSION ON UPPER SURFACE, VERIFIED STEP 5, 6, 7, AND 8.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026091488082Strap · corrodedAFT CARGO CEILING STABILIZATION STRAP 2ND FROM RT OTBD SIDE BS 1400-1420-1420 CORROED ON UPPER SURFACE. VERIFIED STEPS 6,7 AND 8Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026091453424Channel · corrodedRIGHT PNEUMATIC GROUND SERVICE CONNECTION SUPPORT HAS CORROSION ON THE UPPER SURFACE. INSTALLED NEW RT PNEUMATIC GROUND SERVICE CONNECTION SUPPORT IAW SRM 51-40-02-0G-0.Sep 9, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102435766Bracket · crackedRT WW L BRACKET IS CRACKED NEAR WW SEAL. INSTALLED 1EA NEW BRACKET PIN RT WW AREA SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102435745Support Channel · crackedRIGHT WW GUSSET SUPPORT STRUCTURE L BRACKET WAS CRACKED. INSTALLED GUSSET SUPPORT STRUCTURE L BRACKET ASSY. (SUPPORT CHANNEL) AND SEAL RETAINER ASSY. ON RH W/W IAW SRM 51-40-02-0G-0 AND 51-40-04-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102341715Hook · corrodedMAIN DECK CARGO DOOR AFT LOWER HOOK HAS PITTING MARKS, LOST MATERIAL. INSTALLED NEW AFT LOWER HOOK AT MAIN DECK CARGO DOOR IN REF TO CMM 52-32-03 AND AMM 20-11-00-912-001.Sep 8, 2026 · N402UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2026102135715Bracket · crackedRIGHT WW GUSSET IS CRACKED. INSTALLED GUSSET SUPPORT (BRACKET) ON RT WW IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102136117Gusset · crackedLH WW HAS A CRACKED GUSSET. INSTALLED NEW GUSSET AT LH WW PER B757-200PF SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA2026101935723Gusset · crackedRT WW GUSSET SUPPORT STRUCTURE IS CRACKED. INSTALLED GUSSET SUPPORT (BRACKET) ON RH W/W I.A.W B757-200 S.R.M 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026101835885Retainer · crackedRIGHT WW AFT SEAL RETAINER HAS A GOUGE. INSTALLED NEW SEAL RETAINER AFT OF RH WW IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Landing Gear DoorsSDR IPXA2026092236110Bracket · crackedLEFT WW LT BRACKET CRACKED. INSTALLED NEW BRACKET AT LT WW PER SRM 51-40-02-0G-0Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102328019Door Sill · delaminatedLIGHT DELAMINATION ALONG EXTERIOR VERTICAL EDGE OF APU INLET DOOR. QC MKD AS DB-13. COMPOSITE SKILL. INSTALLED APU AIR INTAKE DOOR AND PERFORMED MANUALLY OPERATE FULL CLOSED AND FULL OPENED AND VERIFIED THE APU AIR INTAKE DOOR MOVE SMOOTHLY AND VERIFIED GAP Sep 7, 2026 · N402UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026101426713Slat Track · crackedLT SLAT #4 OUTBD TRACK COVER CRACKED. INSTALLED REPLACEMENT COVER AT L/WING #4 SLAT O/B TRACK PER B757-200PF SRM 51-40-05-0G-0 & 51-40-02-0G-0.Sep 7, 2026 · N402UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA2026061806583Window · arcedL1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L. COMPLETED SECOND AND THIRD TORQUE AT !900 AND SEALED. CONNECTED SENSORS AND WIRES TO WINDSHIELD AND TORJun 17, 2026 · N402UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2026061706583Windshield · arcedL1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L.Jun 17, 2026 · N402UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025111323417Duct · leakingDURING LEFT ENGINE START, LEFT BLEED DUCT BLEED LEAK. ABORTED ENGINE START, RAN CHECKLIST SMOKE VISIBLE COCKPIT ON GROUND. RESULTED IN BTB. REPLACED 2 DAMAGED DUCTS IN AFT LOWER CARGO PIT REF M/M 36-11-01. PRESSURIZED DUCTS NO LEAKS NOTED.Nov 11, 2025 · N402UP · Boeing 75724APF · Engine Bleed Air SystemSDR IPXA2025111223417Duct · leakingDURING LEFT ENGINE START, LEFT BLEED DUCT LEAK. ABORTED ENGINE START, RAN CHECKLIST SMOKE VISIBLE IN THE COCKPT AND ON THE GROUND. RESULTED IN BTB.Nov 11, 2025 · N402UP · Boeing 75724APF · Engine Bleed Air SystemSDR IPXA2024091499980Tee Fitting · corrodedT-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 1060 R/H SIDE WITH EXFOLIATION.REMOVED CORROSION IN T-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 1060 R/H SIDE ORIGINAL MATERIAL: 0,115" MATERIAL LOSS: 0,0425", MAXIMUM MATERIAL LOSS ALLOWED: 0,011Sep 3, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024092390936Strap · corrodedINSIDE AFT TAIL COMPARTMENT EXFOILATION CORROSION AT STA 1787.4 R/H INTERNAL UPPER AT APU AIR INLET DUCT. DOT 140-007 INSTALLED 5EA REPAIR PARTS, 1EA AFT STRAP, NEW STRAP P/N 148N3138-20, 2 UPPER ANGLES STRAP, 2 LOWER ANGLES STRAP AND REPAIR WASHER IAW B757 SRSep 2, 2024 · N402UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2024091850713Tee Angle · corrodedUPPER T-CHORD BETWEEN STA 1180- STA 1200 L/H SIDE WITH EXFOLIATON. INSTALLED T-CHORD BETWEEN IN STA 1180- STA 1200 L/H, INSTALLED 2 EA HINGES IN STA 1140 - 1160 LH AND BTW STA 1140 - 1170 LH AND BTW STA1170 - 1180 LH INSTALLED STRAP IAW B757-200 SRM 51-40-02-0Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091855209Tee Angle · corrodedT-CHORD STA 1240 R/H RBL 59 WITH EXFOLIATION. INSTALLED NEW T-CHORD AT STA 1240 RH, I.A.W. SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091249582Tee Angle · corrodedLOWER T-CHORD BETWEEN STA 1180 - STA 1260 RH SIDE WITH EXFOLIATION.VERIFIED FOUND TO BE OUT OF LIMITS. REMOVED T-CHORD IAW SRM 51-40-02. VERIFIED AND DRILLED NEW T-CHORD APPLIED ALODINE P/N ALODINEE1132 PRIMER P/N 02-013-8 IAW SRM 51-20-01.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091047960Tee Angle · corrodedT-CHORD STA 1220 R/H SIDE WITH EXFOLIATION. INSTALLED T-CHORD AT STA 1220 RH IAW SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091050624Tee Angle · corrodedLOWER T-CHORD BETWEEN STA 1180- STA 1240 L/H SIDE WITH CORROSION. INSTALLED NEW LOWER T-CHORD BETWEEN STA 1180 - STA 1240 LH I.A.W. SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091427226Support · corrodedLOWER FWD WING TO BODY SUPPORT IN FRONT OF LEFT ECS BAY DOOR STA 900 HAS EXFOLIATING CORROSION DOT 47-10 VERIFIED INSTALLED NEW T-CHORD IN STRUCTURES ZONE 100 LOWER FWD WING TO BODY FRONT OF LEFT ECS BAY DOOR STA 900 IAW SRM 51-4O-02. MATERIAL USED: RIVET HI-LAug 29, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091126805Tee Fitting · corrodedRT MLG W/W FWD OUTBD PANEL SUPPORT T-CHORD LOWER AREA HAS EXFOLIATING CORROSION DOT 47-09. INSTALLED T-CHORD AT RH MLG W/W FWD O/B PANEL SUPPORT IAW SRM 51-40-02-0G.Aug 29, 2024 · N402UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024092464213Support · looseLOWER FWD WING TO BODY SUPPORT IN FRONT OF LEFT ECS BAY DOOR STA 900 HAS EXFOLIATING CORROSION DOT 47-10. INSTALLED NEW T-CHORD IN STRUCTURES ZONE 100 LOWER FWD WING TO BODY FRONT OF LEFT ECS BAY DOOR STA 900 IAW SRM 51-4O-02.Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024091164453Door Frame · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28). APPLIED TREATMENT, PRIMER AND TOP COAT AT CREW ENTRY DOOR STOP FITTING IAW B757 SRM 51-20-01 AND AMM 51-21-15; REVIEWEDAug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024082764213Skin · damagedCREW ENTRY DOOR CUTOUT, INTERNAL LINNING HAS MATERIAL LOSE. DOT 28-01. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2024082764453Stop Fitting · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024082010183Connector · misinstalledCONNECTOR PLUG NOT PROPERLY INSTALLED ON #1 ENG HYD SUPPLY SHUT OFF VALVE. THIS ENTRY IS FOR SDR PURPOSE REF SUBTASK BARCODE T3F18E0050QM9. SDR MEASUREMENTS RECORDED AS REQUIRED.SECURED AND SAFETIED CANNON PLUG (D1774) FOR #1 ENGINE SUPPLY HYD SHUTOFF VALVE RAug 16, 2024 · N402UP · Boeing 75724APF · Hydraulic Power System WiringSDR IPXA2024081610183Connector · misinstalledCONNECTOR PLUG NOT PROPERLY INSTALLED ON #1 ENG HYD SUPPLY SHUT OFF VALVE. THIS ENTRY IS FOR SDR PURPOSE REF SUBTASK BARCODE T3F18E0050QM9. SDR MEASUREMENTS RECORDED AS REQUIRED.Aug 16, 2024 · N402UP · Boeing 75724APF · Hydraulic Power System WiringSDR IPXA2024091892394Seat Track · damagedSEAT TRACK AT LOCK LOCATED AT STA 611 BL 0 IS ELONGATED, CAUSING LOCK TO BE LOOSELY INSTALLED INSTALLED SEAT TRACK SECTION, ANGLE AND STRAP BTW STA 590 TO 650 BL0 IAW SRM 53-00-52-2R-7 DETAIL I.Jun 11, 2024 · N402UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023113024472Battery · inoperativeEMERGENCY LIGHT BATTERY WON'T HOLD CHARGE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-51-07/201. OPS CHECK GOOD. REVIEW COMPLETE.Nov 16, 2023 · N402UP · Boeing 75724APF · Emergency LightingSDR IPXA2023111724472Unknown · unknown*SDR FILED OPEN* FAULT - EMERGENCY LIGHT BATTERY WON'T HOLD CHARGENov 16, 2023 · N402UP · Boeing 75724APF · Emergency LightingSDR IPXA2023050293071Floor Panel · damagedINSPECTION TYPE:NA*MAJOR REPAIR* MCD POS 1 FLOOR PANEL FASTENER HOLE NOT LOCATED ON ORIGINAL PANEL.LOCATED MISSING FASTENER HOLE PER DWG 141N5410, DRILLED AND INSTALLED INSERT PER EO B757-5320-9692-K APPX B STEPS 4 AND 5.May 1, 2023 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023050193048Floor Panel · damagedINSPECTION TYPE:NA*MAJOR REPAIR* PUNCTURE INTO FLOORPANEL FACE SHEET INTO CORE.MANUFACTURED NEW PANEL PER EO B757-5320-9692-K.May 1, 2023 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023050193047Floor Panel · damagedINSPECTION TYPE:NA*MAJOR REPAIR* PUNCTURE INTO PANELS FACE SHEET INTO COREMANUFACTURED NEW PANEL PER EO B757-5320-9692-K.May 1, 2023 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024092422420Crease Beam · damagedFUSELAGE RIGHT SIDE CREASE BEAM ELECTRICAL ARCING DAMAGE NEAR STA 1195. E.O. 861 INSTALLED 1EA NEW SHEAR WEB, 1EA CLIP AND 1EA DOUBLER IAW B757-200PF SRM 51-40-02-0G-0.Mar 6, 2023 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024091022420Crease Beam · corroded**SDR FILED OPEN** FUSELAGE RIGHT SIDE CREASE BEAM ELECTRICAL ARCING DAMAGE NEAR STA 1195. E.O. 861.Mar 6, 2023 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022092086428Frame · dentedINSPECTION TYPE:SEG1** SUPPLEMENTAL SDR ** FRAME AT STA 1500 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=1.15" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL I AND RCD 284695. ORIG SUB DATE: 9/20Sep 1, 2022 · N402UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022092086426Frame · dentedINSPECTION TYPE:SEG1FRAME AT STA 1560 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=.778" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL I AND RCD 284612Aug 31, 2022 · N402UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022091586283Frame · dentedINSPECTION TYPE:SEG1, FRAME AT STA 1520 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=3.65" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL III AND RCD 284607Aug 31, 2022 · N402UP · Boeing 75724APF · Fuselage Main, Frame
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