# Service difficulty reports: N457UP

A list on [N457UP](https://openairdocs.org/aircraft/N457UP.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 7 · 307 reports

- [SDR IPXA2026102374753](https://openairdocs.org/sdr/IPXA2026102374753.md): Guard · missing · Oct 22, 2026 · N457UP · Boeing 75724APF · Emergency Equipment
  > CAPT AND FO EVAS SPLASH GUARD MISSING. INSTALLED ALL SPLASHGUARDS AS REQUIRED MM 25-69-00-200-801-C3
- [SDR IPXA2025102280275](https://openairdocs.org/sdr/IPXA2025102280275.md): Retainer · corroded · Oct 15, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT MAIN CARGO COMPARTMENT ANGLE RETAINER SUPPORT FROM BS 1610 - 1681.80, LBL 60. REMOVED CORRODED ANGLE RETAINER IAW SRM 51-40-02. INSTALLED ANGLE RETAINER SUPPORT IAW SRM-51-40-02.
- [SDR IPXA2025102162001](https://openairdocs.org/sdr/IPXA2025102162001.md): Support · cracked · Oct 8, 2025 · N457UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > RH PYLON PANEL 443KL SUPPORT STRUCTURE HAS (1EA) CRACK. REMOVED RH PYLON PANEL 443KL SUPPORT STRUCTURE IAW B757-200PF SRM 51-40-02. ++INSTALLED NWE SUPPORT AT RH PYLON IAW B757-200PF SRM 51-40-02. INSTALLED PANELS: 442AL, 443KL.
- [SDR IPXA2025101787567](https://openairdocs.org/sdr/IPXA2025101787567.md): Tie Clip · corroded · Oct 4, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CORRODED STRUCTURE FOUND AT BS 680, AFT SIDE OF FLOOR FRAME AT RIGHT SIDE OUTBD SEAT TRACK AS SEEN FROM THE FWD LOWER CARGO PIT. REMOVED CLIP ON AT STA 680, AFT SIDE OF FLOOR FRAME AT RIGHT SIDE OUTBD SEAT TRACK AS SEEN FROM THE FWD LOWER CARGO PIT. IAW SRM 5
- [SDR IPXA2025101571181](https://openairdocs.org/sdr/IPXA2025101571181.md): Floor Support · corroded · Oct 3, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN CABIN COMPARTMENT FLOOR STRUCTURE, BS 1720, LBL 25 HAS (1EA) PLATE EXFOLIATED. REMOVED PLATE 1 EA AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE STA 1720 LBL 25 IAW B757-200 SRM 51-40-02. INSTALLED NEW ANGLE FROM MAIN CABIN COMPARTMENT FLOOR STRUCTURE, STA 17
- [SDR IPXA2025102734451](https://openairdocs.org/sdr/IPXA2025102734451.md): Floor Support · cracked · Oct 1, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN CABIN COMPARTMENT BS 880-900, RBL 70, FLOOR SUPPORT CRACKED. ACCOMPLISHED REPAIR IAW EO-95420-REQ1 AND VT-MAE EA 757-5330-27-A4177.
- [SDR IPXA2025102339051](https://openairdocs.org/sdr/IPXA2025102339051.md): Shear Web · corroded · Oct 1, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN CABIN COMPARTMENT STA 1180-1200 RBL 70-75 WEB HAS CORROSION. REMOVED MAIN CABIN COMPARTMENT STA 1180-1200 RBL 70-75 WEB IAW SRM 51-40-02. INSTALLED DOUBLER IAW SRM 51-70-13-0G-0. INSTALLED WEB FROM MAIN CABIN COMPARTMENT BS 1180-1200, RBL 70-75 IAW SRM 5
- [SDR IPXA2025100941015](https://openairdocs.org/sdr/IPXA2025100941015.md): Support Angle · corroded · Oct 1, 2025 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TAIL CONE BELOW APU EXHAUST DUCT, SUPPORT ANGLE HAS CORROSION. REMOVED CORRODED SUPPORT ANGLE AT ZONE.TAIL CONE BELOW APU EXHAUST DUCT IAW B757-200 SRM 51-40-02. ++INSTALLED NEW ANGLE FROM TAIL CONE BELOW APU EXHAUST DUCT, SUPPORT IAW B757-200 SRM 51-40-02-0
- [SDR IPXA2025102887933](https://openairdocs.org/sdr/IPXA2025102887933.md): Floorbeam · corroded · Sep 28, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR - MDC, BS 1680, FLOOR STR HAS EVIDENCE OF CORROSION AROUND 3EA SCREW HOLES, BTW BL0 AND LBL 24.75. PERMANENT REPAIR ACCOMPLISHED IAW UPS EO: EO-95421-REQ 1 AND VT MAE EA 757-5360-27-A4175 REV-.
- [SDR IPXA2025100979085](https://openairdocs.org/sdr/IPXA2025100979085.md): Skin · delaminated · Sep 28, 2025 · N457UP · Boeing 75724APF · Aerodynamic Fairings
  > TAIL CONE STA1963-1992 BOTTOM SKIN INTERNAL BELOW THE APU EXHAUST MANIFOLD CORRODED/DELAMINATED. REMOVED SKIN BELOW APU EXHAUST MANIFOLD IAW SRM 51-40-02. INSTALLED NEW BOND ASSY (SKIN PANEL) IAW SRM 51-40-02-0G-0 AND DWG 148N3770. INSTALLED APU EXHAUST DUC
- [SDR IPXA2025102273248](https://openairdocs.org/sdr/IPXA2025102273248.md): Frame · dented · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT Z-100 STR: FWD CARGO COMPARTMENT AT STA 820 R/H BETWEEN STR 23 TO STR 24 FRAME HAS A DENT. INSTALLED PANEL 122KW IAW B757-200 AMM 25-50-02 404-006. ACCOMPLISHED REPAIR PER EO-95418-REQ1 AND VT-MAE EA 757-5330-27-A4167, REV-. REVIEWED.
- [SDR IPXA2025102977740](https://openairdocs.org/sdr/IPXA2025102977740.md): Skin · cracked · Sep 27, 2025 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 2 ENG OUTBD T/R AFT OF SECOND FROM TOP BLOCKER DOOR HAS A CRACK AT PERFORATED SKIN AREA. WORK ACCOMPLISHED PER UPS EO: EO-95442-REQ1 AND VT MAE EA 757-7831-27-A4184 REV-.
- [SDR IPXA2025102176477](https://openairdocs.org/sdr/IPXA2025102176477.md): Crease Beam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Structure
  > MAIN CABIN UPPER FLIGHT DECK STA 320 AT LBL 62.225 INNER CHORD HAS A SEVERE CORROSION. ACCOMPLISHED PER UPS EO-95416-REQ 1 AND VT MAE 757-5310-27-A4172 REV-.
- [SDR IPXA2025101373232](https://openairdocs.org/sdr/IPXA2025101373232.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM STA 1200 RBL 45-60 LOWER SURFACE HAS CORROSION AT NUTPLATE. INSTALLED REPAIR PARTS IAW SRM 51-40-02. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 757-5360-27-A4171, REV. -.
- [SDR IPXA2025102168027](https://openairdocs.org/sdr/IPXA2025102168027.md): Door Frame · damaged · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Structure
  > CREW ENTRY DOOR FRAME UPPER FWD ROLLER GUIDE FITTING HAS DEEP SCRATCH/GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025101372331](https://openairdocs.org/sdr/IPXA2025101372331.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM STA 1100 RBL 25-45 HAS (4EA) AREAS WITH CORROSION. DOT 28-712. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-10-08 AND FOUND NO MORE DAMAGE. AFTER THE 2ND EVALUATION PERFORMED AREA WAS RESTORED A
- [SDR IPXA2025100972261](https://openairdocs.org/sdr/IPXA2025100972261.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOOR BEAM STA 1100 LBL 25-45 HAS (4EA) AREAS WITH CORROSION. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-10-08 AND FOUND NO MORE DAMAGE. AFTER FURTHER EVALUATION FOUND ALL THE AREAS ARE IN LIMITS IAW
- [SDR IPXA2025100972265](https://openairdocs.org/sdr/IPXA2025100972265.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM BS 1100 LBL 0-25 HAS (3EA) AREAS WITH CORROSION. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-10-08 AND FOUND NO MORE DAMAGE. AFTER FURTHER EVALUATION FOUND ALL THE AREAS ARE IN LIMITS IAW SRM 5
- [SDR IPXA2025100972378](https://openairdocs.org/sdr/IPXA2025100972378.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOOR BEAM STA 1100 RBL 0-25 HAS (2EA) AREAS WITH CORROSION. REMOVED CORROSION ON 2 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-10-08 AND FOUND NO MORE DAMAGE. INSTALLED PREVIOUS REPAIR AT STA 1100 BETWEEN RBL0 TO RBL12 IAW
- [SDR IPXA2025100972465](https://openairdocs.org/sdr/IPXA2025100972465.md): Floorbeam · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM BS 1100, RBL 45-60 HAS (1EA) AREA WITH CORROSION. REMOVED CORROSION ON 1 AREA IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-10-08 AND FOUND NO MORE DAMAGE. AFTER FURTHER EVALUATION FOUND THE AREA IS IN LIMITS IAW SRM 53-00-
- [SDR IPXA2025100665445](https://openairdocs.org/sdr/IPXA2025100665445.md): Support Bracket · corroded · Sep 27, 2025 · N457UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > ACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT 4EA SUPPORT BRACKETS ARE CORRODED. REMOVED 2EA SUPPORTS AND 4 ANGLES IN ACCESS DOOR 313AL I.A.W. B757-200PF SRM 51-40-02-0G.INSTALLED 4 EA SUPPORT BRACKETS IAW SRM 51-40-02.REINSTALLED 2 EA STOP SUPPORT
- [SDR IPXA2025092968027](https://openairdocs.org/sdr/IPXA2025092968027.md): Fitting · gouged · Sep 27, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Structure
  > CREW ENTRY DOOR FRAME UPPER FWD ROLLER GUIDE FITTING HAS DEEP SCRATCH/GOUGE.
- [SDR IPXA2025102158712](https://openairdocs.org/sdr/IPXA2025102158712.md): Cam · damaged · Sep 26, 2025 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR UPPER CAM LATCH HAS A GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025102158881](https://openairdocs.org/sdr/IPXA2025102158881.md): Cam · damaged · Sep 26, 2025 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR LOWER CAM LATCH HAS A GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025100857008](https://openairdocs.org/sdr/IPXA2025100857008.md): Skin · damaged · Sep 26, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > RIGHT EXTERNAL UPPER FUSELAGE, STA 700-720 BETWEEN STR 6R-7R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN PREVIOUS REPAIR. REMOVED 1 EA RIVET AT RH EXTERNAL UPPER FUSELAGE, STA 700-720 BETWEEN STR 5R-6R IAW B757-200PF SRM 51-40-02. INSTALLED REPAIR DOUBLE
- [SDR IPXA2025101463121](https://openairdocs.org/sdr/IPXA2025101463121.md): Tee Angle · corroded · Sep 26, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Structure
  > RIGHT MIDDLE LOWER FUSELAGE STA 900 RBL 25 TEE CHORD HAS CORROSION. REMOVED THE DAMAGED PORTION OF THE TEE CHORD IAW SRM 51-70-12-0G-0. INSTALLED ALL REPAIR PARTS IAW SRM 51-40-02-0G.
- [SDR IPXA2025100955989](https://openairdocs.org/sdr/IPXA2025100955989.md): Skin · damaged · Sep 26, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > EXTERIOR RT FUSELAGE STA 1320-1340, BETWEEN STR 7R-8R HAS (1EA) HOLE AT SKIN CAUSED BY LIGHTNING STRIKE. EVALUATED DAMAGE: ORIGINAL TICKNESS: 0.045 IN, 100% MATERIAL LOSS FOUND IT OUT OF LIMITS IAW SRM 53-00-01-1A-1. INSTALLED RIVET IAW SRM 51-40-02 AND SRM 5
- [SDR IPXA2025100857342](https://openairdocs.org/sdr/IPXA2025100857342.md): Skin · damaged · Sep 26, 2025 · N457UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > RIGHT EXTERNAL UPPER FUSELAGE, STA 540-560 BETWEEN STR 7R-8R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN.PERFORMED HFEC SURFACE INSPECTION ON EXTERNAL SKIN ONLY AT STA 540-560 BTW STR 7R-8R IAW. NTM 51-00-19 PART6.INSTALLED FASTENER ON. RH EXTERNAL UPPER
- [SDR IPXA2025092908881](https://openairdocs.org/sdr/IPXA2025092908881.md): Latch · gouged · Sep 26, 2025 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR LOWER CAM LATCH HAS A GOUGE APPROVED.
- [SDR IPXA2055092908712](https://openairdocs.org/sdr/IPXA2055092908712.md): Latch · gouged · Sep 26, 2025 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR UPPER CAM LATCH HAS A GOUGE APPROVED.
- [SDR IPXA2024020896523](https://openairdocs.org/sdr/IPXA2024020896523.md): Transition Panel · corroded · Jan 16, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SUPPLEMENTAL SDR* FAULT: AFT CARGO COMPT, R/H SIDE PANELS, BETWEEN STA 1380 TO STA 1440, FOUND EXFOLIATED CORROSION. INSTALLED SIDE PANEL IAW SRM 51-40-02-0G-0. REVIEWED.
- [SDR IPXA2024012446523](https://openairdocs.org/sdr/IPXA2024012446523.md): Panel · corroded · Jan 16, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > **SDR FILED OPEN**FAULT: AFT CARGO COMPT, R/H SIDE PANELS, BETWEEN STA 1380 TO STA 1440, FOUND EXFOLIATED CORROSION. REVIEWED.
- [SDR IPXA2024012943372](https://openairdocs.org/sdr/IPXA2024012943372.md): Transition Panel · corroded · Jan 15, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SUPPLEMENTAL SDR* FAULT: AFT CARGO COMPT, R/H TRANSITION PANEL, BETWEEN STA 1440 TO STA 1520, FOUND EXFOLIATED CORROSION. INSTALLED DOUBLER (06) AND INSTALLED TRANSITION PANEL I.A.W. B757-200 S.R.M. 51040-02-OG. REVIEWED.
- [SDR IPXA2024012443372](https://openairdocs.org/sdr/IPXA2024012443372.md): Transition Panel · corroded · Jan 15, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > **SDR FILED OPEN**FAULT: AFT CARGO COMPT, R/H TRANSITION PANEL, BETWEEN STA 1440 TO STA 1520, FOUND EXFOLIATED CORROSION. REF STEP 20 AND 21. INSPECTED AND VERIFIED DOUBLER AND TRANSITION PANEL IS INSTALLED
- [SDR IPXA2024020844456](https://openairdocs.org/sdr/IPXA2024020844456.md): Support Bracket · cracked · Jan 9, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT - AFT CARGO PIT SIDE LH FR 1540 UNDER PANEL 161AW, BRAKET SUPPORT AIR CONDITION DUCT BOTH SIDE CRACKED. INSTALLED BRACKETS-APU DUCT SUPPORT WITH P/N BACB3OMY6K6 BTCH 0004210209 AND P/N BACC30M6 BTCH 000421974 I.A.W SRM 51-40-02-0G-0. REVIEWED
- [SDR IPXA2024020844406](https://openairdocs.org/sdr/IPXA2024020844406.md): Panel · cracked · Jan 9, 2024 · N457UP · Boeing 75724APF · Fuselage Main, Structure
  > FAULT - AFFT CARGO PIT FWD BULKHEAD AIR CONDITION DUCT WITH CRACKED UNDER PANEL 151BZ. REPAIRED AIR CONDITION DUCT WHITH CRACKED IAW 757-AMM, TASK 21-23-01-308-016. MAT: 50-A1, BATCH: 4169233; BMS9-3, BATCH: 3512880. REVIEWED.
- [SDR IPXA2024011053278](https://openairdocs.org/sdr/IPXA2024011053278.md): Unknown · unknown · Jan 9, 2024 · N457UP · Boeing 75724APF · Fuselage Main, Frame
  > PROTRUDING DENT AFT OF FRAME STA 1460 R.H SIDE NEAR STRINGER 17R. DOT 142-99
- [SDR IPXA202401104406](https://openairdocs.org/sdr/IPXA202401104406.md): Unknown · unknown · Jan 9, 2024 · N457UP · Boeing 75724APF · Air Distribution System
  > AFT CARGO PIT FWD BULKHEAD AIR CONDITION DUCT WITH CRACKED UNDER PANEL 151BZ APPROVED.
- [SDR IPXA202401104456](https://openairdocs.org/sdr/IPXA202401104456.md): Unknown · unknown · Jan 9, 2024 · N457UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FAULT - AFT CARGO PIT SIDE LH FR 1540 UNDER PANEL 161AW, BRAKET SUPPORT AIR CONDITION DUCT BOTH SIDE CRACKED. APPROVED.
- [SDR IPXA2024010803867](https://openairdocs.org/sdr/IPXA2024010803867.md): Unknown · unknown · Jan 6, 2024 · N457UP · Boeing 75724APF · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STABILIZER UPPER SURFACE HAS MULTIPLE DENTS. APPROVED
- [SDR IPXA2024021679317](https://openairdocs.org/sdr/IPXA2024021679317.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON INBD SKIN, INNER SKIN FWD OF PANEL# 443HL OPENING HAS CORROSION. DOT 8-003. APPLIED TREAT AND PRIMER I.A.W SRM 51-20-01, PRIMER MIXED IN CUP P/N 02-012-176.
- [SDR IPXA2024021679125](https://openairdocs.org/sdr/IPXA2024021679125.md): Seal · deteriorated · Jan 4, 2024 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW INNER DOOR SEAL DETERIORATING TOP. SEAL FOR CREW INNER DOOR REPLACED IN TASK CARD NUMBER T3F18E003P9EP. INSTALLED NEW CREW DOOR SEAL IAW AMM 52-09-02-404-004. C/W
- [SDR IPXA2024021679020](https://openairdocs.org/sdr/IPXA2024021679020.md): Seal · torn · Jan 4, 2024 · N457UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRANCE DOOR SEAL TORN OUTER SEAL. INSTALLED NEW CREW DOOR SEAL IAW AMM 52-09-02-404-004. C/W.
- [SDR IPXA2024013079249](https://openairdocs.org/sdr/IPXA2024013079249.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON INBD SKIN, INNER SKIN FWD OF PANEL# 443JL HAS CORROSION. DOT 8-002. INSTALLED FILLER AND DOUBLER I.A.W. S.R.M. 51-40-02-OG AND EA 757-5450-27-A3485 STEP 15 PRELIMINARY 1
- [SDR IPXA2024021679612](https://openairdocs.org/sdr/IPXA2024021679612.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON OUTBD SKIN, INNER SKIN FWD OF PANEL 433BL OPENING, HAS A LITTLE SPOT OF CORROSION. DOT 8-009. APPLIED PROTECTIVE TREATMENT, INNER SKIN FWD OF PANEL 433BL I.A.W. SRM 51-20-01-0G.
- [SDR IPXA2024013079006](https://openairdocs.org/sdr/IPXA2024013079006.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR. NR 2 OUTBD PYLON, INNER SKIN FWD OF PANEL #443CR OPNENING HAS EXFOLITATION CORROSION. DOT 8-001, PLACED ON THE OUTSIDE. JOB WAS ACCOMPLISHED IAW UPS EO: EO-89254-REQ1 AND VT MAE EA-757-5450-27-A3484, REV.- WITHOUT ANY DEVIATIONS. REVIEWED.
- [SDR IPXA2024013079351](https://openairdocs.org/sdr/IPXA2024013079351.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > *SUPPLEMENTAL SDR* FAULT- #2 PYLON INBD FWD HINGE PANEL 443GL, INNER FRAME STRUCTURE HAS EXFOLITATION CORROSION. DOT 8-004. JOB ACCOMPLISHED PER UPS EO: EO-89238-REQ1 AND VT MAE EA-757-5450-27-A3490 REV -. WITHOUT ANY DEVIATIONS. REVIEWED
- [SDR IPXA2024020979580](https://openairdocs.org/sdr/IPXA2024020979580.md): Doubler · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR* FAULT- #1 PYLON OUTBD SKIN, INNER SKIN AFT OF PANEL#433BL OPENING, HAS EXFOLITATION CORROSION. DOT 8-008. JOB WAS ACCOMPLISHED PER UPS EO: EO-89227 AND VT MAE EA 757-5450-27-A3486 REV -. WITHOUT ANY DEVIATIONS. REVIEWED.
- [SDR IPXA2024020979528](https://openairdocs.org/sdr/IPXA2024020979528.md): Skin · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON INBD SKIN, INNER SKIN FWD OF PANEL#433HR OPENING HAS CORROSION. DOT 8-007. REMOVED DAMAGE, IAW SRM 51-10-02, MATERIAL REMOVED 0.004, ORIGINAL MATERIAL 0.057, REMAINING MATERIAL 0.053, FOUND TO BE WITHIN LIMITS, IAW SRM 54-50-01-1A, AS MEASURED USING
- [SDR IPXA2024013079451](https://openairdocs.org/sdr/IPXA2024013079451.md): Doubler · corroded · Jan 4, 2024 · N457UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT- #1 PYLON INBD SKIN, INNER SKIN AFT OF PANEL# 433HR OPENING HAS EXFOLIATION CORROSION. DOT 8-004. JOB WAS ACCOMPLISHED PER UPS EO: EO-89234-REQ1 AND VT MAE EA 757-5450-27-A3488 REV -. WITHOUT ANY DEVIATIONS. REVIEWED.

Next page: https://openairdocs.org/aircraft/N457UP/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 = 'N457UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N457UP/reports

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