# Service difficulty reports: N413UP

A list on [N413UP](https://openairdocs.org/aircraft/N413UP.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 · 256 reports

- [SDR IPXA2026061187755](https://openairdocs.org/sdr/IPXA2026061187755.md): Bracket · corroded · Jun 3, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF LWR SKIN PANEL AT SECTION 48 WHILE ACCOMPLISHMENT OF T.C T3F18E008WDGE. FOUND 2EA ANGLE BRACKETS CORRODED AT BS 1963.8 AND BS 1992.8. INSTALLED NEWS BRACKETS 2 EA BS 1963.8 AND BS 1992.8 IAW SRM 51-40-02-0G.
- [SDR IPXA2026061648877](https://openairdocs.org/sdr/IPXA2026061648877.md): Support · cracked · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, INTERCOSTAL IS CRACKED AT BS 990. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061148884](https://openairdocs.org/sdr/IPXA2026061148884.md): Tee Angle · corroded · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, TEE ANGLE HAS EXFOLIATED CORROSION, BTWN BS 1040 AND BS 1060 AT RBL 68. INSTALLED NEW TEE ANGLE RT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, BTWN BS 1040 AND BS 1060 AT RBL 68 IAW SRM 51-40-02-0G.
- [SDR IPXA2026061249095](https://openairdocs.org/sdr/IPXA2026061249095.md): Frame · corroded · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, FRAME-WEB HAS CORROSION AT BS 1200 RBL 60. INSTALLED 1 EA FRAME WEB IAW SRM 51-40-02.
- [SDR IPXA2026060648764](https://openairdocs.org/sdr/IPXA2026060648764.md): Support Bracket · cracked · Jun 1, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LEFT MLG WHEEL WELL, 1EA BRACKET SUPPORT IS CRACKED AT THE 1180 BULKHEAD LWR SECTION. INSTALLED WEB REMOVED FOR ACCESS IN STEP 1 AND NEW BRACKET SUPPORT P/N UP-144N2503-133 INSTALLED IAW 757-200 SRM 51-40-02
- [SDR IPXA2026060949184](https://openairdocs.org/sdr/IPXA2026060949184.md): Support Angle · cracked · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT-STR-Z100- R/H WING TO BODY FAIRING SUPPORT STRUCTURE AT BS 1300, UPPER T-CHORD BRACKET SUPPORT IS CRACKED. DOT 21-14 INSTALLED NEW ANGLE SUPPORT P/N UP-149N7665-8 IAW 757-200 SRM 51-40-02
- [SDR IPXA2026060248829](https://openairdocs.org/sdr/IPXA2026060248829.md): Splice Plate · corroded · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > RT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, SUPPORT WEB HAS CORROSION AT BS 860 BL0. SURFACE PROTECTION RESTORATION COMPLIED WITH IAW SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.
- [SDR IPXA2026060249026](https://openairdocs.org/sdr/IPXA2026060249026.md): Angle · corroded · Jun 1, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > R/H LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, T-CHORD "L" ANGLE HAS CORROSION AT BS 1040 AT RBL 68. VERIFIED STEP 3.INSPECTED SURFACE PROTECTION RESTORATION COMPLIED WITH IAW B757-200 SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.
- [SDR IPXA2026061741991](https://openairdocs.org/sdr/IPXA2026061741991.md): Frame · gouged · May 31, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Frame
  > FRAME 1380 RT SIDE HAS MULTIPLE GOUGES TO THE FRAME INNER CHORD (EXTERIOR RADIUS) BETWEEN S-25R TO S-27R. ACCOMPLISHED THE CATEGORY B REPAIR PER EO-97741-REQ1 AND VT-MAE EA 757-5360-27-A4515 REV.
- [SDR IPXA2026061620751](https://openairdocs.org/sdr/IPXA2026061620751.md): Support Bracket · corroded · May 29, 2026 · N413UP · Boeing 75724APF · Wing Miscellaneous Structure
  > RH WING LOWER SURFACE SIDE OF BODY SPLICE INTERNAL TRIANGULAR SHAPE PANEL 194CR MID SUPPORT BRACKET ANGLE CORRODED/ DOT.139.032. INSTALLED 1EA FRAME, 1EA BRACKET, 1EA FITTING AND 2EA ANGLES IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026061201031](https://openairdocs.org/sdr/IPXA2026061201031.md): Strap · corroded · May 28, 2026 · N413UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR AFT STRAP HAS CORROSION STA1825.00,S-3R TO S6R. INSTALLED PARTS OF REPAIR (STRAP 1, STRAP 2, FILLER 3, FILLER 4 AND OUTER STRAP) I.A.W. B757-200 PF SRM 51-40-02-0G-0 DETAIL I.
- [SDR IPXA2026061202381](https://openairdocs.org/sdr/IPXA2026061202381.md): Angle · corroded · May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS CORROSION. INSTALLED NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026061303166](https://openairdocs.org/sdr/IPXA2026061303166.md): Tee Angle · corroded · May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > BS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW TEE ANGLE AT BS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026060903107](https://openairdocs.org/sdr/IPXA2026060903107.md): Intercostal · corroded · May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > BS 1040 LWR SURFACE, AROUND OF RH A/C PACK HOT AIR EXHAUST, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026060103232](https://openairdocs.org/sdr/IPXA2026060103232.md): Tee Angle · corroded · May 28, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > STA 900 APPROX, LWR SURFACE, JUST IN FRONT OF LH A/C PACK PANEL, FRAME WITH EVIDENCE OF CORROSION. VERIFIED RESTORATION OF SURFACE PROTECTION IAW B757-200PF SRM51-20-01 AND AMM51-21-15.
- [SDR IPXA2026060584560](https://openairdocs.org/sdr/IPXA2026060584560.md): Seal Depressor · cracked · May 27, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CARGO DOOR UPPER AFT CORNER HAS A CRACK. INSTALLED NEW CORNER SEAL DECOMPRESSOR FROM CARGO DOOR IAW SRM 51-40-02-0G-0
- [SDR IPXA2026061366314](https://openairdocs.org/sdr/IPXA2026061366314.md): Tee Angle · corroded · May 26, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT A/C PACK PANEL, AFT FRAME WITH EVIDENCE OF CORROSION IN DIFERRENT AREAS. INSTALLED NEW TEE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061366338](https://openairdocs.org/sdr/IPXA2026061366338.md): Tee Angle · corroded · May 26, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LEFT A/C PACK PANEL, AFT FRAME WITH EVIDENCE OF CORROSION IN DIFERRENT AREAS. INSTALLED TEE ANGLE AND 2 EA CLIP SUPPORTS IAW SRM 51-40-02.
- [SDR IPXA2026060663496](https://openairdocs.org/sdr/IPXA2026060663496.md): Bracket · cracked · May 26, 2026 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CRACK ON PRESS/CD FILTER MOD R SYS BRACKET MLG RH WHEEL WELL. INSTALLED NEW BRACKET AT MLG RH WHEEL WELL IAW SRM 51-40-02-0G-0
- [SDR IPXA2026061244839](https://openairdocs.org/sdr/IPXA2026061244839.md): Angle · corroded · May 24, 2026 · N413UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > FAULT Z-300 STR: APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R HAS CORROSION INSTALLED NEW LOWER CORNER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026061744578](https://openairdocs.org/sdr/IPXA2026061744578.md): Tail Cone · corroded · May 24, 2026 · N413UP · Boeing 75724APF · Aerodynamic Fairings
  > APU EXTERNAL AREA NEXT TO TAIL CONE (STA. 1992) SHOWS EVIDENCE OF CORROSION. INSTALLED BOND ASSY SKIN LOWER PANEL 1 EA AT APU EXTERNAL AREA NEXT TO TAIL CONE BS 1992 IAW B757-200 SRM 51-40-02-0G-0
- [SDR IPXA2026061244983](https://openairdocs.org/sdr/IPXA2026061244983.md): Strap · corroded · May 24, 2026 · N413UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR FWD STRAP HAS CORROSION INSTALLED NEW FWD STRAP I.A.W SRM 51-40-02-0G-0.
- [SDR IPXA2026061344863](https://openairdocs.org/sdr/IPXA2026061344863.md): Angle · corroded · May 24, 2026 · N413UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR BETWEEN BS 1787.45 TO BS 1825 S-6R, LOWER ANGLE HAS CORROSION. INSTALLED NEW LOWER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061634755](https://openairdocs.org/sdr/IPXA2026061634755.md): Skin · corroded · May 23, 2026 · N413UP · Boeing 75724APF · Rudder, Plate/Skin
  > LH RUDDER SURFACE CONDUCTIVE FRAME ABOVE STA. 380 SHOWS EVIDENCE OF CORROSION. DOT 65-001 INSTALLED FAIRING P/N 173N2603-3, FAIRING P/N 179N1000-7, BRACKET SUPPORT P/N 173N2507-9001 AND STATIC DISCHARGE. IN LH RUDDER SURFACE CONDUCTIVE FRAME ABOVE STA. 380. IA
- [SDR IPXA2026061768095](https://openairdocs.org/sdr/IPXA2026061768095.md): Door Frame · dented · Apr 24, 2026 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > (MAIN CARGO DOOR FRAME INSTALLATION (STA 600+12.9 & 600+17.25) DAMAGE - TEMPORARY REPAIR) [T3F18E008QANF]
- [SDR IPXA2025123066036](https://openairdocs.org/sdr/IPXA2025123066036.md): Bulb · inoperative · Dec 29, 2025 · N413UP · Boeing 75724APF · Emergency Lighting
  > FLIGHT DECK EXIT LIGHT HAS 11 INOP BULBS. RE-LAMPED FLIGHT DECK EXIT SIGN 11 EACH BULBS IAW AMM 33-51-01-962-001
- [SDR IPXA2025102914495](https://openairdocs.org/sdr/IPXA2025102914495.md): Door · binding · Oct 29, 2025 · N413UP · Boeing 75724APF · Passenger/Crew Doors
  > CAPT REPORTS ISSUES WITH CREW ENTRY DOOR OPEN/CLOSE.
- [SDR IPXA2024122688367](https://openairdocs.org/sdr/IPXA2024122688367.md): Channel · unsecure · Dec 24, 2024 · N413UP · Boeing 75724APF · Emergency Equipment
  > RUBBER CABLE CHANNELS FOR DESCENT DEVICES HANGING FROM CEILING. RE SECURED GUIDE BLOCKS IAW MM 25-64-00 OPS CK GOOD
- [SDR IPXA2024081284700](https://openairdocs.org/sdr/IPXA2024081284700.md): Stud · inoperative · Aug 9, 2024 · N413UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR OUTER HANDLE, REQUIRES STUD REPLACEMENT. REMOVED AND REPLACED CREW ENTRY DOOR OUTER HANDLE STUD PER MM 52-12-01.
- [SDR IPXA2024061744408](https://openairdocs.org/sdr/IPXA2024061744408.md): Light · inoperative · Jun 13, 2024 · N413UP · Boeing 75724APF · Emergency Lighting
  > NTERIOR EMERGENCY LIGHT. R&R BATTERY PACK PER AMM 33-51-07 OPS CHECK GOOD THIS CLEARS MEL 33-51-1-1 PLACARD REMOVED
- [SDR IPXA2024061344408](https://openairdocs.org/sdr/IPXA2024061344408.md): Light · unknown · Jun 13, 2024 · N413UP · Boeing 75724APF · Emergency Lighting
  > INTERIOR EMERGENCY LIGHT DEFERRED PER MEL 33-51-1-1. OPEN
- [SDR IPXA2023091435148](https://openairdocs.org/sdr/IPXA2023091435148.md): Bleed Air Sys · inoperative · Sep 13, 2023 · N413UP · Boeing 75724APF · Engine Bleed Air System
  > R ENG BLEED OFF WITH R PACK OFF. RESULTED IN DIVERSION TO SDF REMOVED AND REPLACED FAN AIR VALVE PER AMM 36-11-16. REMOVED AND RPLACED FAN AIR TEMP SENSOR PER AMM 36-11-13
- [SDR IPXA2023091335148](https://openairdocs.org/sdr/IPXA2023091335148.md): Unknown · unknown · Sep 13, 2023 · N413UP · Boeing 75724APF · Pneumatic Distribution System
  > *SDR FILED OPEN* *DIV* R ENG BLEED OFF WITH R PACK OFF. RESULTED IN DIVERSION TO SDF REMOVED AND REPLACED FAN AIR VALVE PER AMM 36-11-16 REMOVED AND REPLACED FAN AIR TEMP SENSOR PER AMM 36-11-13
- [SDR IPXA2023041392870](https://openairdocs.org/sdr/IPXA2023041392870.md): Unknown · inoperative · Apr 13, 2023 · N413UP · Boeing 75724APF · Pitot/Static System
  > INSPECTION TYPE:NA*EMERGENCY DECLARED* AIRSPEED UNRELIABLE ON CAPT SIDE AT FLT LVL 250. CHECKLIST RESTORED CAPT INSTS BY USE OF "AIR DATA" SWITCHMCDP FAULT 210401 ADC SYST L FOUND. R&R LH AIR DATA COMPUTER IN REF TO AMM 34-12-01. BITE CHECK GOOD AT THIS TIME.
- [SDR IPXA2022081485215](https://openairdocs.org/sdr/IPXA2022081485215.md): None · none · Aug 13, 2022 · N413UP · Boeing 75724APF · Standard Practices/Structures
  > INSPECTION TYPE:DIRH LOWER FUSELAGE AT STA 700, S-24R HAS A TEMPORARY LIGHTINING STRIKE REPAIR. REQUIRES PERMANENT REPAIR. SKIN P/N: 143N3691-2, ORIGINAL MAT: STOCK 0.080" THICKNESS, 2024-T3 CLAD SHEETACCOMPLISHED REPAIR PER 757-200PF SRM REV 114.0, CHAPTER 53
- [SDR IPXA2022070983986](https://openairdocs.org/sdr/IPXA2022070983986.md): Floorbeam · corroded · Jul 9, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4MCD STA 1600 FLOOR BEAM HAS CORROSION DAMAGE ON UPPER CHORD AFT FLANGE LOWER SURFACE AND WEB BETWEEN RBL 40 AND RBL 60.REPAIRED PER UPS EO B757-5310-84157-A AND VT MAE EA 757-5360-27-A2970 REV.
- [SDR IPXA2022070783904](https://openairdocs.org/sdr/IPXA2022070783904.md): Floor Panel · damaged · Jul 7, 2022 · N413UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SEG4MCD FLOOR PANEL 241XHF HAS DELAMINATION AND SEPARATING.FABRICATED PANEL 241XHF FROM 5024N400001SS-G, BAT: 3855547, PER SREO B757-5320-9692-K
- [SDR IPXA2022070683860](https://openairdocs.org/sdr/IPXA2022070683860.md): Skin · corroded · Jul 6, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4LH WING UPPER SURFACE SHOWING SIGNS OF CORROSION BETWEEN WS 150.00 - WS 177.50 DOT 33-022UPPER SKIN BLENDED IS WITHIN LIMITS PER SRM 57-20-01-1A-1 TABLE IV LIMITS. REPAIRED AREA IAW SRM 57-20-01-1A-1 DETAIL M PART 2. WORKED PER UPS RCD 2711
- [SDR IPXA2022070683859](https://openairdocs.org/sdr/IPXA2022070683859.md): Tie Clip · corroded · Jul 6, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4COCKPIT FLOOR HAS CORROSION IN NUMEROUS SPOTS ON 1ST OFFICERS SIDE TO INCLUDE UNDER 1ST OBERVERS SEAT.REMOVED CORROSION, PERFORMED HFEC INSP, ALL AREAS WITHIN LIMITS IAW SRM B757-53-10-51-1A-1, TABLE 102.
- [SDR IPXA2022070683867](https://openairdocs.org/sdr/IPXA2022070683867.md): Frame Angle · cracked · Jul 6, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1560 R/H BETWEEN STR 23 TO STR 28WORKED PER UPS EO B757-5310-26178-C, UPC RCD 271103, AND VT MAE EA 757-5360-27-A2656 REV -
- [SDR IPXA2022070283714](https://openairdocs.org/sdr/IPXA2022070283714.md): Seat Track · corroded · Jul 2, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT SEAT TRACK STA 1190 LBL 45 HAS CORROSIONAFTER TO REWORK AREA, FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1 REMOVE AND REPLACE SEAT PER SRM 51-40-02
- [SDR IPXA2022070283723](https://openairdocs.org/sdr/IPXA2022070283723.md): Floor Support · corroded · Jul 2, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4EXFOLIATION CORROSION AROUND DOME NUT ON LOWER SIDE OF T CHORD AT STA 1200 LBL 47 AT MAIN CARGO COMPARTMENTFOUND TO BE OUT OF LIMITS. REPAIR PER EA 757-5360-27-A2961 REV -
- [SDR IPXA2022070283710](https://openairdocs.org/sdr/IPXA2022070283710.md): Frame Splice · dented · Jul 2, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT LOWER LEFT SIDEWALL STA 1320 HAS DENTDENTS ARE NOT ALLOWED AT THE UPPER FLANGE OF THE FRAME PER SRM 53-00-07-1A-1 FRAME REPAIRED PER SRM 53-00-07-2R-5 DETAIL III
- [SDR IPXA2022070283709](https://openairdocs.org/sdr/IPXA2022070283709.md): Frame Angle · dented · Jul 2, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT LOWER FRAME STA 1300 LH HAS A DENT ABOVE S-26LDENTS ARE NOT ALLOWED AT THE UPPER FLANGE OF THE FRAME PER SRM 53-00-07-1A-1 FRAME REPAIRED PER SRM 53-00-07-2R-5 DETAIL III
- [SDR IPXA2022062983615](https://openairdocs.org/sdr/IPXA2022062983615.md): Skin · damaged · Jun 29, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEG4RIGHT SIDE LOWER FUSELAGE LIGHTNING STRIKE DAMAGED REPAIR AT STA 700 AND S-24 R PERMANENT REPAIRREMOVE TEMPORARY REPAIR DOUBLER PER SRM 51-40-02, FABRICATED AND INSTALLED NEW DOUBLER ON MATERIAL 2024-T3.071" PER 53-00-01-2R-29
- [SDR IPXA2022070583845](https://openairdocs.org/sdr/IPXA2022070583845.md): Frame Angle · dented · Jun 22, 2022 · N413UP · Boeing 75724APF · Cargo Compartments
  > INSPECTION TYPE:C20L/H AFT CARGO COMPARTMENT AT FRAME STA 1600 IS DENTED (S-26L)REPAIRED PER EA# 757-5360-27-A2960
- [SDR IPXA2022070883959](https://openairdocs.org/sdr/IPXA2022070883959.md): Frame Angle · damaged · Jun 21, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:C20AFT CARGO FRAME AT STA 1520 R/H SIDE IS DENTED ON THE TOP OF THE FRAME FLANGE BY S-26RREPAIR PER SRM 53-00-07-2R-5 DETAIL I AND RCD 271205
- [SDR IPXA2022070583850](https://openairdocs.org/sdr/IPXA2022070583850.md): Skin · corroded · Jun 21, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN L/H SIDE AT LOWER WEB ABOVE CLAMSHELL DOOR, AFT OF FWD HINGE (2 SPOTS) DOT 46-06WORKED PER RCD 271218, 757-200PF REV 114.00 CHAPTER 51-70-10-2R-4 PER SRM 53-80-01-2R, FIG 201
- [SDR IPXA2022070583831](https://openairdocs.org/sdr/IPXA2022070583831.md): Skin · corroded · Jun 21, 2022 · N413UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:CK20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN LH LOWER WEB AREA ABOVE CLAMSHELL DOOR, AFT OF AFT HINGE. DOT 46-06WORKED PER RCD 271220. 757-200PF REV 114.0 CHAPTER 51-70-10-2R-4 PER SRM 53-80-01-2R, FIG 201
- [SDR IPXA2021081972919](https://openairdocs.org/sdr/IPXA2021081972919.md): Controller · inoperative · Aug 17, 2021 · N413UP · Boeing 75724APF · Cabin Pressure Controller
  > EMERGENCY DECLARED, IN MANUAL MODE (R) PACK ON (R) ENG BLEED OFF ! TURNED ON (L) PACK AND TURNER OFF (R) PACK. PRESSURIZATION REGAINEDPERFORMED BITE TEST ON BOTH AUTO PRESS CONTROLLERS. NO HARD FAULTS FOUND PER AMM 21-31-02

Next page: https://openairdocs.org/aircraft/N413UP/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 = 'N413UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N413UP/reports

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