# Service difficulty reports: N418UP

A list on [N418UP](https://openairdocs.org/aircraft/N418UP.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 5 · 239 reports

- [SDR IPXA2026071148660](https://openairdocs.org/sdr/IPXA2026071148660.md): Bracket · cracked · Jun 25, 2026 · N418UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR PROXIMITY SENSOR BRACKET IS CRACKED. REMOVED SENSOR BRACKET (SUPPORT ASSY) AT CREW ENTRY DOOR IAW SRM 51-40-02-0G-0. INSTALLED CREW ENTRY DOOR WARNING SENSOR IAW AMM-52-71-00-400-802. PERFORMED ADJUSTMENT AND OPS CHECK IAW AMM-52-71-00-735-05
- [SDR IPXA2026071878612](https://openairdocs.org/sdr/IPXA2026071878612.md): Floor Support · dented · Jun 21, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRINGER HAS 2 EA DENTS, APPROX BTW BS 1240 AND BS 1260, LBL 7.55, INSTALLED NEW FLOOR STRINGER AT CARGO COMPARTMENT LBL 7.55 AND BETWEEN BS 1200 TO BS 1340 IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026070271202](https://openairdocs.org/sdr/IPXA2026070271202.md): Retainer · corroded · Jun 21, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Structure
  > RIGHT MLG WW, AT AFT OTBD DOOR-CUTOUT, UPON THE REMOVAL OF BULB SEAL, FOUND THE RETAINER WITH CORROSION END TO END. REMOVED DAMAGED SEAL RETAINER AT AFT OTBD DOOR-CUTOUT UPON IAW SRM 51-40-02-0G-0, REQUEST FABRICATE SEAL RETAINER. INSTALLED CHANNEL SE
- [SDR IPXA2026063078648](https://openairdocs.org/sdr/IPXA2026063078648.md): Floor Support · corroded · Jun 21, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION AT NUT PLATE BOTTOM AREA, APPROX AT BS 1200, LBL 2.90. REMOVED CORROSION AT AFT CARGO COMP. FLOOR STRINGER AT NUT PLATE AREA UPPER AND LOWER SIDE AT APPROX BS 1200 LBL 2.90. INSTALLED NEW FLOOR STRINGER AT AF
- [SDR IPXA2026062778873](https://openairdocs.org/sdr/IPXA2026062778873.md): Sidewall Panel · corroded · Jun 21, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS, APPROX BTW BS 1410 AND BS 1530, LBL 16.10 THRU LBL 25, REMOVED CORROSION AT AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL FROM BETWEEN BS 1495 BS 1530 L/H IAW SRM 51-10-02-0G
- [SDR IPXA2026063066478](https://openairdocs.org/sdr/IPXA2026063066478.md): Floor Support · corroded · Jun 20, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO RH SIDE OTBD FLOOR STRINGER UPPER SURFACE HAS CORROSION STA 1510. INSTALLED REPAIR CHANNEL AT AFT CARGO RT SIDE OTBD FLOOR STRINGER AT BS 1510, RBL 10.45 IAW SRM 53-00-53-2R-1, REPAIR 1, PARAG 4, DETAIL XII AND SRM 51-40-02-0G-0.
- [SDR IPXA2026070154082](https://openairdocs.org/sdr/IPXA2026070154082.md): Isolation Mount · cracked · Jun 19, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Structure
  > COCKPIT CEILING ABOVE OVERHEAD PANEL ISOLATOR BRACKET CRACKED. REMOVED DAMAGED BRACKET AT COCKPIT CEILING ABOVE OVERHEAD PANEL BS 297 IAW SRM 51-40-02-0G-0 PAR 4. INSTALLED PANEL 232N1642-4 AT COCKPIT CEILING ABOVE OVERHEAD IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026062754538](https://openairdocs.org/sdr/IPXA2026062754538.md): Pad · corroded · Jun 19, 2026 · N418UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE O/B CORE COWL T/E RUB PAD, 3RD FROM BOTTOM, HAS AREA OF CORROSION. INSTALEED SERVICEABLE PART AT NR 1 ENGINE OTBD CORE COWL T/E STOP PAD, 3RD FROM BOTTOM IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026071737767](https://openairdocs.org/sdr/IPXA2026071737767.md): Bracket · broken · Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > IAW TASK CARD T3F18E004V6MO LINE 267 STEP 10, LEFT STRUT STA 149.5 BRACKET WAS INSPECTED AND FOUND BROKEN, FLL-050, INSTALLED FRAME ANGLE AT #1 PYLON UPPER SIDE IAW B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026071426239](https://openairdocs.org/sdr/IPXA2026071426239.md): Attach Angle · worn · Jun 18, 2026 · N418UP · Boeing 75724APF · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB TRAILING EDGE PANEL 324AL LOWER AFT CORNER SUPPORT STRUCTURE SECTION MISSING AND FUSELAGE ATTACH ANGLE WORN THIN IN SEVERAL AREAS. DAMAGED WELL MARKED RL004. REMOVED 1EA DAMAGED ANGLE FIN FAIRING AT VERTICAL STABILIZER TRAILING EDGE PANEL 324AL L
- [SDR IPXA2026063033532](https://openairdocs.org/sdr/IPXA2026063033532.md): Skin · corroded · Jun 18, 2026 · N418UP · Boeing 75724APF · Trailing Edge Flaps
  > LEFT WING INBD FLAP HAS CORROSION AT T/E OTBD UPPER SURFACE.
- [SDR IPXA2026070724890](https://openairdocs.org/sdr/IPXA2026070724890.md): Splice Plate · corroded · Jun 18, 2026 · N418UP · Boeing 75724APF · Elevator Structure
  > RIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME, LOWER CONDUCTIVE FRAME, UPPER SPLICE PLATE, LOWER SPLICE FRAME AND STATIC WICK BASE ASSY AT RT ELEVATOR T/E IAW SRM 51-40-02-
- [SDR IPXA2026062431723](https://openairdocs.org/sdr/IPXA2026062431723.md): Cover · corroded · Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FUSELAGE INTERIOR CENTER SECTION FLOOR PANEL 241XAF PLATE SUPPORT FLOOR PANEL HAS CORROSION, INSTALLED FLOOR SUPPORT HAT CHANNEL AND SUPPORT COVER IN MAIN CABIN, INTERIOR WING CENTER SECTION UNDER FLOOR PANEL 241XAF REF B757-200PF-SRM 51-40-02-0G-0.
- [SDR IPXA2026061925530](https://openairdocs.org/sdr/IPXA2026061925530.md): Skin · damaged · Jun 18, 2026 · N418UP · Boeing 75724APF · Elevator, Plate/Skin
  > RIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. OKAY TO FABRICATE PER DOCUMENTS ON STEP 1.
- [SDR IPXA2026062032578](https://openairdocs.org/sdr/IPXA2026062032578.md): Skin · damaged · Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > AFT LOWER EXTERNAL FUSELAGE SKIN AT SEAM AT STA. 1460 HAS SMALL AREAS OF BUBBLING PAINT, LIGHT CORROSION PRESENT. SRM 53-00-01-1A-1 DETAIL II FIG 101. OK TO TREAT AND PRIME.
- [SDR IPXA2026061936844](https://openairdocs.org/sdr/IPXA2026061936844.md): Gusset · corroded · Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON 4EA GUSSETS, BS 1885.20 BETWEEN S25R AND S25L REMOVED FOUR CORRODED GUSSETS AT BS 1885.20 BETWEEN S-25R TO S-25L IAW SRM 51-40-02-0G-0 PAR 4 AND 7. INSTALLED THE NEW GUSSETS AT STA 1885.20 BETWEEN S-25R TO S-25L IAW SRM 51-40-02-0G-0 AND D
- [SDR IPXA2026061936748](https://openairdocs.org/sdr/IPXA2026061936748.md): Strap · corroded · Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME STRAP P/N 148N6613-2 STA 1885.20 S25R TO S25L. INSTALLED 1 EA NEW STRAP IAW SRM 51-40-02-0G-0 AND DWG 148N6613.
- [SDR IPXA2026071104567](https://openairdocs.org/sdr/IPXA2026071104567.md): Retainer · corroded · Jun 17, 2026 · N418UP · Boeing 75724APF · Elevator Miscellaneous Structure
  > LEFT ELEVATOR T/E COUNT FROM OTBD TO INBD NR 2 STATIC WICK BASE HAS CORROSION. REMOVED AND REPLACED NR 2 STATIC WICK BASE ( MOUNTING STATIC DISCHARGER) P/N 16335, BATCH 0004414980 AND WICK DISCHARGER P/N 10-900-25A, BATCH 0004493176 ON SUPPORT PLATE IAW AMM
- [SDR IPXA2026070219049](https://openairdocs.org/sdr/IPXA2026070219049.md): Support Angle · cracked · Jun 17, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT AFT WTB PANEL LANDING UPPER SUPPORT ANGLE HAS A CRACK. REMOVED SUPPORT ANGLE AT RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW SUPPORT ANGLE RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-OG-0.
- [SDR IPXA2026071492921](https://openairdocs.org/sdr/IPXA2026071492921.md): Skin · damaged · Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > FWD FUSELAGE BTW BS 540 - 560 AND S-29L TO S-29R HAVE LIGHTNING STRIKES 3 EA, FLL-006, INSTALLED 3 EA 7/32" DIAMETER PROTRUDING RIVETS ON FWD FUSELAGE BETWEEN BS 540-560 AND S-29L-S-29R IAW SRM 53-00-01-2R-6 REPAIR 6, FIGURE 201.
- [SDR IPXA2026070198178](https://openairdocs.org/sdr/IPXA2026070198178.md): Pan · cracked · Jun 16, 2026 · N418UP · Boeing 75724APF · Flight Compartment Equipment
  > FLIGHT COMPT RT FIRST OBSERVERS SEAT BACK PAN IS CRACKED. REPLACED FIRST OBSERVERS SEAT IN FLIGHT COMPARTMENT IAW B757 AMM 25-11-01-000-802 AND B757 AMM 25-11-01-402-061.
- [SDR IPXA2026070193398](https://openairdocs.org/sdr/IPXA2026070193398.md): Door · damaged · Jun 16, 2026 · N418UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > AFT FUSELAGE RT APU DOOR ACCESS 316AL IS BENDED ON FWD CORNER AND HAS SEVERAL GOUGES ALONG OUTER EDGE, FLL-015, INSTALLED 2 EACH REPAIR DOUBLERS AND 2 EACH FILLERS ON R/H APU DOOR LWR SURFACE AT FS 1925.329 AND FS 1946.774 IAW SRM 51-70-13-0G-0 FIG 1 AND SRM
- [SDR IPXA2026062794337](https://openairdocs.org/sdr/IPXA2026062794337.md): Support · corroded · Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > APU COMPARTMENT L/H LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION, ACCOMPLISHED REPAIR PER EO-98077-REQ1 AND STE-SAA EA 757-5330-01-B0762, REV IR
- [SDR IPXA2026062794351](https://openairdocs.org/sdr/IPXA2026062794351.md): Longeron · corroded · Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU COMPARTMENT RT LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION. ACCOMPLISHED REPAIR PER EO-98076-REQ1 AND STE-SAA EA 757-5330-01-B0763, REV IR
- [SDR IPXA2026062792720](https://openairdocs.org/sdr/IPXA2026062792720.md): Frame · corroded · Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Structure
  > RIGHT FWD LOWER FUSELAGE WASTE DISPOSAL ACCESS PANEL 118AR HAS CORROSION ON INNER AND LOWER FRAME. INSTALLED PANEL 118AR IN FWD FUSELAGE LAVATORY DISPOSAL IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061994597](https://openairdocs.org/sdr/IPXA2026061994597.md): Access Panel · corroded · Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Structure
  > AFT FUSELAGE INSIDE ACCESS PANEL 313AL STA 1885.20 AND FROM S-25L TO S-25R HAS CORROSION, FLL-030, REMOVED CORRODED CHORD AT BS 1885.20 BETWEEN S-23L TO S-23R IAW SRM 51-40-02-0G-0 PAR. 4 AND 7. REINSTALLED 2 EA BRACKETS, 1 EA FENCE-DRIP AND INSTALLED NEW CHO
- [SDR IPXA2026070666531](https://openairdocs.org/sdr/IPXA2026070666531.md): Pitot Tube · damaged · Jun 14, 2026 · N418UP · Boeing 75724APF · Pitot/Static System
  > AUX 1 PITOT PROBE ON RT SIDE SHOWS SIGNS OF OVERHEATING
- [SDR IPXA2026070666517](https://openairdocs.org/sdr/IPXA2026070666517.md): Pitot Tube · overheated · Jun 14, 2026 · N418UP · Boeing 75724APF · Pitot/Static System
  > CAPTAIN PITOT PROBE ON LH SIDE SHOWS SIGNS OF OVERHEATING. INSTALLED NEW CAPTAIN PITOT PROBE ON LH SIDE IN REF TO B757 AMM 34-11-01-024-041
- [SDR IPXA2025011826274](https://openairdocs.org/sdr/IPXA2025011826274.md): Frame · no discrepancy · Jan 16, 2025 · N418UP · Boeing 75724APF · Standard Practices/Structures
  > REF HEAVY CHECK REPAIR T3F18E004SYHW, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. COMPLIED WITH EO-92551. REVIEWED.
- [SDR IPXA2024083095805](https://openairdocs.org/sdr/IPXA2024083095805.md): Torque Tube · unserviceable · Aug 28, 2024 · N418UP · Boeing 75724APF · Trailing Edge Flap Control System
  > FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT. REPLACED TORQUE TUBES 251N4281-16,-17,-18 WITH 251N4281-26,-27,-28. REPLACED BEARING 251N4318-1 WITH 251N4381-6. ACCOMPLISHED PER AMM 27-
- [SDR IPXA2024082995805](https://openairdocs.org/sdr/IPXA2024082995805.md): Flap System · faulted · Aug 28, 2024 · N418UP · Boeing 75724APF · Trailing Edge Flap Control System
  > EMERGENCY DECLARED, FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT PER THE FIM 27-51 TREE 809,DID A FSEU BITE PER 27-51-00 FIG 104. FOUND A RIGHT FLAP DRIVE FAULT. MORE TROUBLE SHOOT
- [SDR IPXA2024073089425](https://openairdocs.org/sdr/IPXA2024073089425.md): Battery Pack · inoperative · Jul 24, 2024 · N418UP · Boeing 75724APF · Emergency Lighting
  > FAULT EMERGENCY EXIT LIGHT INOP.REMOVED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07-902-001.INSTALLED NEW EMERGENCY LIGHT BATTERY PACK AND PERFORMED OPS CHECK IAW AMM 33-51-07-902-001. OPS CHECK GOOD.
- [SDR IPXA2024072589425](https://openairdocs.org/sdr/IPXA2024072589425.md): Light · inoperative · Jul 24, 2024 · N418UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOPERATIVE.
- [SDR IPXA2024072345670](https://openairdocs.org/sdr/IPXA2024072345670.md): Seat Track · corroded · Jul 10, 2024 · N418UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MCD, AT STA 1671, LBL 24.5 SEAT TRACK FLANGE, SHOWS EVIDENCE OF CORROSION. DOT 72-033.REMOVED DAMAGE SEAT TRACK SECTION BETWEEN STA 1640+9.45 IN TO STA 1681.8, LBL 24.5 PER SRM 53-00-52-2R-5, STEP 2.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-5
- [SDR IPXA2024072631238](https://openairdocs.org/sdr/IPXA2024072631238.md): Doubler · corroded · Jul 9, 2024 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MCD, AFT DECK AREA (ON DOUBLER REPAIR) AT STA 1681.8 BTW BL 0/RBL 24.75 IS CORRODED. REMOVED AND REPLACED DOUBLER REPAIR ON AFT DECK AREA AT STA 1681.8 BTW BL 0 TO RBL 24.7. IAW B757-200 SRM 51-40-02.
- [SDR IPXA2024072331663](https://openairdocs.org/sdr/IPXA2024072331663.md): Seat Track · corroded · Jul 9, 2024 · N418UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > FAULT: STR Z200 MCD, AFT AREA STA. 1681.8 SEAT TRACK LBL 45.5 IS CORRODED. DOT 34-008. INSTALLED SEAT TRACK IN STA 1681.8 LBL 45.5 IAW SRM 53-00-52-2R-5,SRM 51-40-02. REVIEWED
- [SDR IPXA2024072214234](https://openairdocs.org/sdr/IPXA2024072214234.md): Handle · gouged · Jul 8, 2024 · N418UP · Boeing 75724APF · Passenger/Crew Doors
  > **SUPPLEMENTAL SDR** FAULT. FOUND GOUGE ON CREW DOOR HANDLE.RESTORED SURFACE IN AREA IAW SRM 51-20-01 AMM 51-21-15 P/N ALONINE 1132 BATCH 004253000 P/N 02-013-8 BATCH 4168824 P/N G6-W2-G2 BATCH 4159202. REVIEWED
- [SDR IPXA2024071014234](https://openairdocs.org/sdr/IPXA2024071014234.md): Handle · gouged · Jul 8, 2024 · N418UP · Boeing 75724APF · Passenger/Crew Doors
  > OPEN. FOUND GOUGE ON CREW DOOR HANDLE.
- [SDR IPXA2024072301272](https://openairdocs.org/sdr/IPXA2024072301272.md): Seat Track · corroded · Jul 7, 2024 · N418UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACKS AT STA 1680 BL 0.-REMOVED SEAT TRACK DAMAGED SECTION BETWEEN STA 1680-1650 BL PER SRM 53-00-52. ACCOMPLISHED REPAIR PER 757-200PF SRM REV 120 CHAP 53-00-52-2R-7.
- [SDR IPXA2024072202331](https://openairdocs.org/sdr/IPXA2024072202331.md): Frame · dented · Jul 7, 2024 · N418UP · Boeing 75724APF · Fuselage Main, Frame
  > DENT ON FRAME IN STA 720 RH BETWEEN STR 23R AND 25R. INSTALLED FRAME REPAIR, IAW SRM 53-00-07-2R-5, DETAIL I, MAT.
- [SDR IPXA2024072695371](https://openairdocs.org/sdr/IPXA2024072695371.md): Tee Angle · corroded · Jul 6, 2024 · N418UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > TEE CHORD WITH CORROSION AT BS 900 RT, UNDER PANEL 194AR. INSPECTED & VERIFIED INSTALLATION OF NEW MATERIAL IAW SRM 51-70-12-0G-0 ON STA 900.
- [SDR IPXA2024072494273](https://openairdocs.org/sdr/IPXA2024072494273.md): Transition Panel · corroded · Jul 6, 2024 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TRANSITION PANEL STA 1440-1520 RH WITH CORROSION. INSTALLED TRANSITION PANEL IAW SRM 51-40-02. INSTALLED PANELS 161BF,161AF IAW SRM 51-40-02. INSTALLED LOWER MBA SYSTEM IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024071994561](https://openairdocs.org/sdr/IPXA2024071994561.md): Nut Plate · corroded · Jul 6, 2024 · N418UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > FAULT: NUTPLATES UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED 1 NUTPLATE IAW B757-200 SRM 51-40-02. NUTPLATE P/N BACN10KE3DCD BTCH 4278069 RIVET P/N NAS1097AD3-8 BTCH 4234826. INSTALLED SHIM PLATE IAW B757-200, SRM 51-40-02 RIVET P/N NAS1097AD6-6 BTC
- [SDR IPXA2024072394617](https://openairdocs.org/sdr/IPXA2024072394617.md): Nut Plate · corroded · Jul 6, 2024 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > SUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED ANGLE AND SUPPORT NUTPLATE IAW B757 SRM 51-40-02 PARAGRAPH 4. RIVET P/N:MS20426AD6-10 BATCH:0004244858 REVIEWED
- [SDR IPXA2024072294617](https://openairdocs.org/sdr/IPXA2024072294617.md): Nut Plate · corroded · Jul 6, 2024 · N418UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > SUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION.
- [SDR IPXA2024071682131](https://openairdocs.org/sdr/IPXA2024071682131.md): Mount · gouged · Jul 5, 2024 · N418UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. VERRIFIED RESTORED SURFACE PROTECTION IAW AMM 51-21-15-370-81A. P/N ALODINE1132 BTCH 4297395. PRIMER P/N 10-P4-2/2TU BTCH 4268566. TOPCOAT P/N PG6-W24Q BTCH 4281366.
- [SDR IPXA202407082131](https://openairdocs.org/sdr/IPXA202407082131.md): Mount · gouged · Jul 5, 2024 · N418UP · Boeing 75724APF · Fuselage Main, Structure
  > OPEN, CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. REMOVED MARK BY METHOD ABRASION BY HAND AT CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 IAW SOPM 20-30-03.
- [SDR IPXA2022072084380](https://openairdocs.org/sdr/IPXA2022072084380.md): Skin · cracked · Jul 5, 2022 · N418UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C18UPON HFEC OF A 15: DENT AT FS 1380 - FS 1400 BETWEEN STRINGERS 28L AND 27R NDT FOUND A 15" CRACK RUNNING ALONG THE RECESS OF DENT 15", CRACK DOES NOT GO ALL THE WAY THROUGH THE SKIN AND IS LOCATED ON THE OML OF SKIN PANEL.REPAIRED SKIN PANEL
- [SDR IPXA2018122137128](https://openairdocs.org/sdr/IPXA2018122137128.md): Clamp · loose · Dec 20, 2018 · N418UP · Boeing 75724APF · Air Distribution System
  > CLIMBING THROUGH FL 280, AN EICAS MESSAGE & WARNING HORN FOR CABIN ALTITUDE WERE ANNUNCIATED AND SOUNDED. EMERGENCY DECLARED, PERFORMED AN EMERGENCY DESCENT. LEFT PACK WAS OFF DURING CLIMB OUT, AFTER RETURNING LEFT PACK TO AUTO, STARTED TO REGAIN CABIN ALTITUD
- [SDR IPXA2018101835141](https://openairdocs.org/sdr/IPXA2018101835141.md): Floor Panel · damaged · Oct 18, 2018 · N418UP · Boeing 75724APF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL 241XKF DAMAGED. FABBED PANEL 241XKF PER SREO B757-5320-9692-K.

Next page: https://openairdocs.org/aircraft/N418UP/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 = 'N418UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N418UP/reports

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