# Service difficulty reports: N402UP

A list on [N402UP](https://openairdocs.org/aircraft/N402UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 298 reports

- [SDR IPXA2026101280317](https://openairdocs.org/sdr/IPXA2026101280317.md): Skin · corroded · Oct 3, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > AFTER REMOVAL OF ADF ANTENNA FOUND UPPER FUSELAGE SKIN WITH DEEP PITTING CORROSION AND TOOLING MARKS.
- [SDR IPXA2026101718066](https://openairdocs.org/sdr/IPXA2026101718066.md): Support Bracket · corroded · Sep 24, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > REMOVED SUPPORT BRACKET BETWEEN APU DOOR ACTUATOR AND DOOR HOUSING ASSY DIRTY WITH DETERIORATED CIC AND AREAS OF LITE CORROSION AROUND FASTENER HOLES. RL049 QCI: VERIFIED STEP 5
- [SDR IPXA2026101276017](https://openairdocs.org/sdr/IPXA2026101276017.md): Floor Skin · corroded · Sep 22, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Structure
  > DURING BUYBACK IN LH NOSE TUNNEL FOUND MAIN CABIN SUBFLOOR WITH EXFOLIATION ON LOWER SKIN STA 333.5 LBL 49 STR ATA 51-00.
- [SDR IPXA2026101355189](https://openairdocs.org/sdr/IPXA2026101355189.md): Retainer · damaged · Sep 21, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Structure
  > BS 1963, LOWER RT SIDE SEAL RETAINER WAS DAMAGED. INSTALLED SEAL RETAINER AT STA 1963 LOWER R/H SIDE I.A.W B757-200 S.R.M 51-40-02-0G-0.
- [SDR IPXA2026101613332](https://openairdocs.org/sdr/IPXA2026101613332.md): Panel · delaminated · Sep 18, 2026 · N402UP · Boeing 75724APF · APU Cowling/Containment
  > MAJOR REPAIR, LOWER AFT APU PANEL BETWEEN BS 1963 TO 1992 IS DELAMINATED VERIFIED STEP 14 IS ACCOMPLISHED AND HEAT CON. TAP TEST. NO DISBONDS OR DELAMINATIONS NOTED. OKAY TO TREAT AND PRIME. REF GMM RII 04-02.
- [SDR IPXA2026101740890](https://openairdocs.org/sdr/IPXA2026101740890.md): Closeout Panel · corroded · Sep 14, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > COCKPIT CLOSEOUT PANEL OVER SUPERNUMERARY AREA HAS CORROSION, FLL-096, C/W SRM 51-40-05-0G-0.
- [SDR IPXA2026101240869](https://openairdocs.org/sdr/IPXA2026101240869.md): Closeout Panel · corroded · Sep 14, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > OFF A/C PARTS, COCKPIT CLOSEOUT OVER SUPERNUMERARY AREA HAS CORROSION. FABRICATED SPLICE I.A.W. DWG 141W6007/SAMPLE WORK ACCOMPLISHED ON TRAVELER 7003475011.
- [SDR IPXA2026102117121](https://openairdocs.org/sdr/IPXA2026102117121.md): Strap · corroded · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1540 TO 1580 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, INSTALLED STABILIZATION STRAP AND 1EA STABILIZATION STRAP SPLICE PLATE AT STA. 1540-1610 LBL 45.50 IAW B757-200 SRM. 51-40-02-0G-0. OK TO INSTALL DESCOMPRESIO
- [SDR IPXA2026102217366](https://openairdocs.org/sdr/IPXA2026102217366.md): Skin · bulged · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > AGING A/C INSPECTION A BULGE WAS NOTED BELOW THE LH FIXED COCKPIT WINDOW OF BS 255.
- [SDR IPXA2026102116974](https://openairdocs.org/sdr/IPXA2026102116974.md): Strap · corroded · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1560 TO 1580 AND LBL 24.75 STABILIZATION STRAP HAS CORROSION, INSTALLED NEW STABILIZATION STRAP AND 2 EACH SPLICE PLATES IAW SRM 51-40-02-0G-0 PAR 4.
- [SDR IPXA2026101316528](https://openairdocs.org/sdr/IPXA2026101316528.md): Floor Support · dented · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO COMP FLOOR SUPPORT LBL 2.90 AT STA. 662 HAS A DENT AT UPPER SURFACE. 83-043. ATA 53-30. INSTALLED NEW FLOOR SUPPORT ON FWD CARGO AT STA. 662 LBL 7.25 IAW B757-200PF SRM 51-40-02-0G-0 REV. 125 20 MAY 2026, AUDITED
- [SDR IPXA2026092217121](https://openairdocs.org/sdr/IPXA2026092217121.md): Floor Support · corroded · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1540 TO 1580 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, FLL-042, ATA 53. REQ. NDT (HFEC) CHECK FOR CRACK ON CUT OUT
- [SDR IPXA2026091717519](https://openairdocs.org/sdr/IPXA2026091717519.md): Floor Support · corroded · Sep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK CABIN FLOOR STRUCTURE STA 800 TO 820 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, FLL-065, VERIFIED STEPS 14 AND 15
- [SDR IPXA2026101698760](https://openairdocs.org/sdr/IPXA2026101698760.md): Skin · delaminated · Sep 11, 2026 · N402UP · Boeing 75724APF · APU Cowling/Containment
  > MAJOR REPAIR, APU COMPARTMENT SKIN PANEL HAS EVIDENCE OF DELAMINATION APPROX BTW BS 1885 AND BS 1896, STGR 17R AREA,
- [SDR IPXA2026101599728](https://openairdocs.org/sdr/IPXA2026101599728.md): Retainer · broken · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB ASSY ANGLE SUPPORT HAS A SEAL RETAINER BROKEN APPROX AT BS 1963.80, BL 0 THRU RBL 10, LOCATED AND DRILLED SEAL RETAINER AT STA 1963 BL 0 THRU RBL 10 SIDE I.A.W B757-200 S.R.M 51-40-05-0G-0.
- [SDR IPXA2026101203705](https://openairdocs.org/sdr/IPXA2026101203705.md): Floor Support · corroded · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STGR SPLICE EXFOLIATED IN 2 PLACES STR 30L, BS 1460 REMOVED THE INCOMING REPAIR INSTALLED BY SB 757-53A0053 R1. IAW E.A 757-5360-01-B0851, REVISON: P2, STEP 9
- [SDR IPXA2026100500255](https://openairdocs.org/sdr/IPXA2026100500255.md): Door Frame · chafed · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Structure
  > APU COMPARTMENT ACCESS DOOR 315 AL FRAME ASSY LOWER FLANGE HAS A CHAFING APPROX AT BS 1885.2, STGR 17L AREA. REMOVAL AND INSTALLATION ACCOMPLISHED. FRAME IAW DWG 148N6663 AND IPC 52-48-05-01.
- [SDR IPXA2026100403755](https://openairdocs.org/sdr/IPXA2026100403755.md): Support Web · corroded · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP ABOVE DOOR CUTOUT CEILING SUPPORT WEB CORRODED BS 1440.
- [SDR IPXA2026100603845](https://openairdocs.org/sdr/IPXA2026100603845.md): Nut Plate · corroded · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > BULK CARGO MAIN CABIN FLOOR RH SIDE STA 1680 NUT PLATE RETAINER CORRODED STR ATA 51-00 GM014.
- [SDR IPXA2026093099320](https://openairdocs.org/sdr/IPXA2026093099320.md): Doubler · corroded · Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Structure
  > LEFT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB HAS EVIDENCE OF CORROSION ON LOWER AREA APPROX AT BS 1992.8,
- [SDR IPXA2026102188082](https://openairdocs.org/sdr/IPXA2026102188082.md): Strap · corroded · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING STABILIZATION STRAP 2ND FROM RH OTBD SIDE STA 1400-1420-1420 HAS CORROSION ON UPPER SURFACE. INSTALLED REPLACEMENT STABILIZATION STRAP BETWEEN STA. 1440 TO 1390 AND REINSTALLED STABILIZATION STRAP BETWEEN STA. 1390 TO 1360 AND INSTALLED REPA
- [SDR IPXA2026101986516](https://openairdocs.org/sdr/IPXA2026101986516.md): Pad · chafed · Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT FAIRING I/B ACCESS DOOR 445AL AFT LATCH AND PAD HAS DEEP CHAFE WEAR. 83-009. INSTALLED NEW PLATE (STOP PAD) ON #2 PYLON AFT FAIRING I/B ACCESS DOOR 445AL I.A.W B757-200PF SRM 51-40-02-0G-0 PAR. 4 AND PAR. 9.
- [SDR IPXA2026101876234](https://openairdocs.org/sdr/IPXA2026101876234.md): Stiffener · worn · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU COMPARTMENT BULKHEAD STA 1885 HORZ STIFFENER JUST BELOW LIGHT SWITCH ASSY DOOR SAFETY CATCH EDGE WORN. INSTALLED NEW RETAINER AT APU COMPARTMENT BULKHEAD STA 1885 HORZ STIFFENER I.A.W B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026100786152](https://openairdocs.org/sdr/IPXA2026100786152.md): Support Angle · cracked · Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT FAIRING, ACCESS PANEL 445AR, FWD, LOWER CUTOUT AREA HAS A CRACKED SUPPORT CLIP.
- [SDR IPXA2026100574510](https://openairdocs.org/sdr/IPXA2026100574510.md): Skin · chafed · Sep 10, 2026 · N402UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > APU 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.
- [SDR IPXA2026100675524](https://openairdocs.org/sdr/IPXA2026100675524.md): Support · gouged · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU 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.
- [SDR IPXA2026100276207](https://openairdocs.org/sdr/IPXA2026100276207.md): Bulkhead · dented · Sep 10, 2026 · N402UP · Boeing 75724APF · APU Cowling/Containment
  > MAJOR 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 04-02
- [SDR IPXA2026092288146](https://openairdocs.org/sdr/IPXA2026092288146.md): Bracket · cracked · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2026092286010](https://openairdocs.org/sdr/IPXA2026092286010.md): Angle · cracked · Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR IPXA2026091476662](https://openairdocs.org/sdr/IPXA2026091476662.md): Support Bracket · corroded · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WIRE HARNESS CLAMP SUPPORT BRACKETS ATTACHED TO BS 1885 BULKHEAD HAVE LIGHT CORROSION AND MISSING PROTECTIVE FINISH.
- [SDR IPXA2026091488064](https://openairdocs.org/sdr/IPXA2026091488064.md): Strap · corroded · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING STABILIZATION STRAP RT OTBD SIDE BS 1420 HAS CORROSION ON UPPER SURFACE, VERIFIED STEP 5, 6, 7, AND 8.
- [SDR IPXA2026091488082](https://openairdocs.org/sdr/IPXA2026091488082.md): Strap · corroded · Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING STABILIZATION STRAP 2ND FROM RT OTBD SIDE BS 1400-1420-1420 CORROED ON UPPER SURFACE. VERIFIED STEPS 6,7 AND 8
- [SDR IPXA2026091453424](https://openairdocs.org/sdr/IPXA2026091453424.md): Channel · corroded · Sep 9, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR IPXA2026102135715](https://openairdocs.org/sdr/IPXA2026102135715.md): Gusset · cracked · Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT WW GUSSET IS CRACKED.
- [SDR IPXA2026102136117](https://openairdocs.org/sdr/IPXA2026102136117.md): Gusset · cracked · Sep 8, 2026 · N402UP · Boeing 75724APF · Wing Miscellaneous Structure
  > LH WW HAS A CRACKED GUSSET.
- [SDR IPXA2026101935723](https://openairdocs.org/sdr/IPXA2026101935723.md): Gusset · cracked · Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > RT 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.
- [SDR IPXA2026101835885](https://openairdocs.org/sdr/IPXA2026101835885.md): Retainer · cracked · Sep 8, 2026 · N402UP · Boeing 75724APF · Landing Gear Doors
  > RIGHT WW AFT SEAL RETAINER HAS A GOUGE.
- [SDR IPXA2026092236110](https://openairdocs.org/sdr/IPXA2026092236110.md): Bracket · cracked · Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LEFT WW LT BRACKET CRACKED. INSTALLED NEW BRACKET AT LT WW PER SRM 51-40-02-0G-0
- [SDR IPXA2026101426713](https://openairdocs.org/sdr/IPXA2026101426713.md): Slat Track · cracked · Sep 7, 2026 · N402UP · Boeing 75724APF · Leading Edge Devices
  > LT 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.
- [SDR IPXA2026061806583](https://openairdocs.org/sdr/IPXA2026061806583.md): Window · arced · Jun 17, 2026 · N402UP · Boeing 75724APF · Flight Compartment Windows
  > L1 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 TOR
- [SDR IPXA2026061706583](https://openairdocs.org/sdr/IPXA2026061706583.md): Windshield · arced · Jun 17, 2026 · N402UP · Boeing 75724APF · Flight Compartment Windows
  > L1 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.
- [SDR IPXA2025111323417](https://openairdocs.org/sdr/IPXA2025111323417.md): Duct · leaking · Nov 11, 2025 · N402UP · Boeing 75724APF · Engine Bleed Air System
  > DURING 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.
- [SDR IPXA2025111223417](https://openairdocs.org/sdr/IPXA2025111223417.md): Duct · leaking · Nov 11, 2025 · N402UP · Boeing 75724APF · Engine Bleed Air System
  > DURING LEFT ENGINE START, LEFT BLEED DUCT LEAK. ABORTED ENGINE START, RAN CHECKLIST SMOKE VISIBLE IN THE COCKPT AND ON THE GROUND. RESULTED IN BTB.
- [SDR IPXA2024091499980](https://openairdocs.org/sdr/IPXA2024091499980.md): Tee Fitting · corroded · Sep 3, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > T-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: 0,011
- [SDR IPXA2024092390936](https://openairdocs.org/sdr/IPXA2024092390936.md): Strap · corroded · Sep 2, 2024 · N402UP · Boeing 75724APF · Aerodynamic Fairings
  > INSIDE 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 SR
- [SDR IPXA2024091850713](https://openairdocs.org/sdr/IPXA2024091850713.md): Tee Angle · corroded · Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > UPPER 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 51-40-02-0
- [SDR IPXA2024091855209](https://openairdocs.org/sdr/IPXA2024091855209.md): Tee Angle · corroded · Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > T-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.
- [SDR IPXA2024091249582](https://openairdocs.org/sdr/IPXA2024091249582.md): Tee Angle · corroded · Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR IPXA2024091047960](https://openairdocs.org/sdr/IPXA2024091047960.md): Tee Angle · corroded · Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > T-CHORD STA 1220 R/H SIDE WITH EXFOLIATION. INSTALLED T-CHORD AT STA 1220 RH IAW SRM 51-40-02-0G.
- [SDR IPXA2024091050624](https://openairdocs.org/sdr/IPXA2024091050624.md): Tee Angle · corroded · Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER 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.

Next page: https://openairdocs.org/aircraft/N402UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N402UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.