# Service difficulty reports: N463UP

A list on [N463UP](https://openairdocs.org/aircraft/N463UP.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 · 217 reports

- [SDR IPXA2026102228872](https://openairdocs.org/sdr/IPXA2026102228872.md): Support Angle · damaged · Sep 25, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WHILE REMOVING CREASE BEAM FOUND KICKPLATE SUPPORT ANGLE BETWEEN STA 350 AND STA 358 L/H SIDE WITH ELONGATED HOLE AFTER FASTENER REMOVAL AUDIT C\W
- [SDR IPXA2026102242761](https://openairdocs.org/sdr/IPXA2026102242761.md): Landing · cracked · Sep 20, 2026 · N463UP · Boeing 75724APF · Engine Thrust Reverser
  > NR 2 INBD THRUST REVERSER UPPER PANEL LANDING HAS A CRACK.
- [SDR IPXA2026101949482](https://openairdocs.org/sdr/IPXA2026101949482.md): Bushing · cracked · Sep 15, 2026 · N463UP · Boeing 75724APF · Engine Thrust Reverser
  > NR 1-ENG. INBD THRUST REVERSER, UPON THE REMOVAL PHASE, FOUND UPR-CTR-HINGE WITH (HAT) BUSHING CRACKED AT FWD-SIDE.
- [SDR IPXA2026100354024](https://openairdocs.org/sdr/IPXA2026100354024.md): Gusset · corroded · Sep 15, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Structure
  > WHILE EVALUATING JCW T3F18E009L4M8, FOUND CORROSION AT BS 1885, BULKHEAD FWD SIDE SERVICE DOOR LATCH FITTINGS. INSTALLED 4EA NEW GUSSETS P/N 148N6614U9 B/N 4512167, PN 148N6614U8 B/N 4512168 P/N 148N6614-7SAAU, P/N 148N6614-10SAAU AND 2EA FITTINGS AT APU LOW
- [SDR IPXA2026102018336](https://openairdocs.org/sdr/IPXA2026102018336.md): Support Plate · gouged · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK BTW STA 1660 AND 1681.1 AND S-17 PLATE SUPPORT HAS SEVERAL GOUGES.
- [SDR IPXA2026101918056](https://openairdocs.org/sdr/IPXA2026101918056.md): Seat Track · gouged · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK BETWEEN STA 580 - 600, LBL 62.225 HAS GOUGES.
- [SDR IPXA2026101816920](https://openairdocs.org/sdr/IPXA2026101816920.md): Frame · cracked · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT FUSELAGE FRAME HAS A CRACK APPROX AT BS 1500, STGR 26R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98861REQ1 AND EA 757-5360-01-B0826, REV IR.
- [SDR IPXA2026101617312](https://openairdocs.org/sdr/IPXA2026101617312.md): Web · bent · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT INTERNAL FUSELAGE STRUCTURE INTERCOSTAL IS DEFORMED APPROX BTW BS 1440 & BS 1460, BTW STGR 25R AND STGR 24R, INSTALLED NEW INTERCOSTAL AT AFT CARGO COMPARTMENT INTERNAL FUSELAGE STRUCTURE BTW BS 1440 & 1460, STR 25R AND 24R IAW SRM 51-40
- [SDR IPXA2026091716966](https://openairdocs.org/sdr/IPXA2026091716966.md): Frame · dented · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT FUSELAGE FRAME HAS 2 DENTS APPROX AT BS 1460, STGR 26R, VERIFIED REMOVAL OF FITTING ON STEP 27 PER DOCUMENT AND PER GMM RII 04-02
- [SDR IPXA2026091018202](https://openairdocs.org/sdr/IPXA2026091018202.md): Floorbeam · corroded · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK, BS 860 BTW BL 0 TO LBL 24.75, FLOORBEAM HAS EXFOLATION.
- [SDR IPXA2026090912765](https://openairdocs.org/sdr/IPXA2026090912765.md): Floorbeam · corroded · Sep 6, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK STA 1500 BTW LBL 45.50 TO 54.9 FLOORBEAM HAS CORROSION AROUND SCREW HOLE. VERIFIED STEP 9 REF GMM RII 04-02. EVALUATED REWORKED AREA ON MAIN DECK STA 1500 BTW LBL 45.50 TO 54.9 FLOORBEAM UPPER FLANGE, DIMENSIONS L:1.700" W:1.300" X:0.011", ORIG. MAT
- [SDR IPXA2026101507031](https://openairdocs.org/sdr/IPXA2026101507031.md): Nut Plate · damaged · Sep 5, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK STA 1681.1 AND BTW LBL 45.50 AND 54.9 RETAINER NUT HAS CORROSION BOTTOM SURFACE OF THE TOP FLANGE, INSTALLED NEW NUT PLATE RETAINER STRIP ON MAIN DECK STA 1681.1 AND BTW LBL 45.50 AND 54.9 IAW SRM 51-40-02-0G-0 PAR.4 REV 126.
- [SDR IPXA2026101498292](https://openairdocs.org/sdr/IPXA2026101498292.md): Plate · corroded · Sep 5, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB FAIRING 342AR LOWER SIDE EXTENDING AFT TRANSITION END PLATE HAS CORROSION.
- [SDR IPXA2026100298223](https://openairdocs.org/sdr/IPXA2026100298223.md): Fairing · gouged · Sep 5, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > MAJOR REPAIR, GOUGE IN FUSELAGE SKIN EXTENDING UNDER R/H HORZ STAB LOWER SLIDING FAIRING. RL108 (NOTE: CHECK LOWER SLIDING FAIRING SCREW LENGTH TO PREVENT REOCCURRING DAMAGE) VERIFIED STEP 28 PER UPS B 757 RII GMM 04-02.
- [SDR IPXA2026091406679](https://openairdocs.org/sdr/IPXA2026091406679.md): Deck Plate · corroded · Sep 5, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Structure
  > MAIN DECK FROM BS 1681.1 - 1720, LBL 54.9 - RBL 54.9 DECK PLATE HAS MULTIPLE AREAS WITH CORROSION, REQUEST NDT UT THICKNESS. AT REWORKED AREAS IAW SRM 53-60-51-1A-1, PARA 2.C.
- [SDR IPXA2026090997871](https://openairdocs.org/sdr/IPXA2026090997871.md): Fairing · corroded · Sep 5, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORZ STAB FAIRING 332AL LOWER SIDE EXTENDING AFT TRANSITION END PLATE HAS CORROSION. VERIFIED STEPS 5 AND 6 C/W
- [SDR IPXA2026102080618](https://openairdocs.org/sdr/IPXA2026102080618.md): Skin Panel · delaminated · Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/Containment
  > APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. REPAIR FILLER AND DOUBLER MADE FROM 0.012-INCH-THICK 2024-T3 BARE AL SHT AND REPLACEMENT HONEYCOMB CORE MADE FROM BMS4-4 3-10N OR EQUIVALENT. B. REPAIRED PER SRM 53-80
- [SDR IPXA2026102380237](https://openairdocs.org/sdr/IPXA2026102380237.md): Support Bracket · damaged · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > ALL APU COMPARTMENT R/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FININSH. RL037.INSTALLED 3EA SUPPOR BRACKETS AT APU COMPARTMENT BS 1885 BETWEEN BL0 - RBL 30 WL 250.00 IAW B757-200PF SRM 51-40-02-0G-0. AUDITE
- [SDR IPXA2026101780235](https://openairdocs.org/sdr/IPXA2026101780235.md): Bracket · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/Containment
  > ALL APU COMPARTMENT L/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. INSTALLED 4EA NEW SUPPORT BRACKETS AT APU COMPARTMENT STA 1885 BETWEEN LBL 0 - LBL 30 WL 250.00 IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026101680268](https://openairdocs.org/sdr/IPXA2026101680268.md): Support Bracket · damaged · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > ALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL035. INSTALLED 3 EA SUPPORT BRACKETS P/N 287N4802-75 AT APU COMPARTMENT FWD BULKHE
- [SDR IPXA2026092678940](https://openairdocs.org/sdr/IPXA2026092678940.md): Skin · debonded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, LOWER BILGE COMPOSITE SKIN PANEL BETWEEN STA 1963 TO 1992 FWD AND AFT EDGES DISBONDED WITH AREAS OF CORROSION INCLUDING FWD EDGE LEVELING COMPOUND DETERIORATED AND NOT SECURED. RL028 VERIFIED STEP 17 OKAY TO TREAT AND PRIME REWORKED AREA. REF UP
- [SDR IPXA2026100280598](https://openairdocs.org/sdr/IPXA2026100280598.md): Skin · delaminated · Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/Containment
  > MAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1918 AND 1941 DELAMINATED. RL038 QCI(RII) VERIFIED FABRICATION OF DOUBLER PER STEP 16 AND GMM RII 04-02
- [SDR IPXA2026100280618](https://openairdocs.org/sdr/IPXA2026100280618.md): Skin · delaminated · Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/Containment
  > MAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. RL039 QCI(RII) VERIFIED STEP 13 IS C/W AND VERIFIED TOOLS PER DOCUMENTS AND GMM RII 04-02
- [SDR IPXA2026091580268](https://openairdocs.org/sdr/IPXA2026091580268.md): Bracket · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > ALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL035 QCI: VERIFIED STEP 5, C/W TOOL VERIFICATION ID # 22-840 DATE DUE 28-FEB- 2027 I
- [SDR IPXA2026091580804](https://openairdocs.org/sdr/IPXA2026091580804.md): Frame · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Frame
  > FRAME STA 1992 FWD AND AFT SIDES HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH WITH HEAVY DEBRIS ON BACK SIDE PLUGGING DRAIN HOLE.
- [SDR IPXA2026091478857](https://openairdocs.org/sdr/IPXA2026091478857.md): Frame · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT FUSLAGE FRAME STA 1963 FWD AND AFT SIDES AND ALL ATTACHING STRUCTURE CIRCUMFERENTIALLY HAVE AREAS OF CORROSION AND LARGE AREAS OF MISSING PROTECTIVE FINISH AND TOPCOAT. VERIFIED STEP 20, C/W RII GMM 04-02.
- [SDR IPXA2026090881106](https://openairdocs.org/sdr/IPXA2026090881106.md): Skin · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN BS 1862 HAS AREAS OF CORROSION AREA JUST FWD OF ACCESS DOOR 313AL. RL050 ACCOMPLISHED VISUAL INSP WITH 10X MAGNIFYING GLASS AT CORROSION REMOVAL AREAS EXTERNAL SKIN BUTT JOINT LWR BILGE BETWEEN STA. 1862 TO STA 1863 FROM S-23L TO S-19R P
- [SDR IPXA2026090880235](https://openairdocs.org/sdr/IPXA2026090880235.md): Support Bracket · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > ALL APU COMPARTMENT L/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FININSH. RL036 VERIFIED STEPS 1,2 AND 3
- [SDR IPXA2026090880237](https://openairdocs.org/sdr/IPXA2026090880237.md): Support Bracket · corroded · Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > ALL APU COMPARTMENT R/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL037 VERIFIED STEPS 1,2 AND 3
- [SDR IPXA2026101672642](https://openairdocs.org/sdr/IPXA2026101672642.md): Fitting · damaged · Sep 3, 2026 · N463UP · Boeing 75724APF · Trailing Edge Flaps
  > LH TRUNNION CANOE FAIRING I/B BEARING HAS RADIAL PLAY MARKED JK-34 ATA 57.INSTALLED FITTING 2 EACH AT L/H MLG AFT TRUNNION / FLAP FAIRING I.A.W. BOEING 757 SRM 51-40-02-0G-0. REVIEWED
- [SDR IPXA2026101678146](https://openairdocs.org/sdr/IPXA2026101678146.md): Support Bracket · damaged · Sep 3, 2026 · N463UP · Boeing 75724APF · APU Cowling/Containment
  > STR, ATA 49: APU AIR INTAKE DUCT EXTERNAL DRAIN TUBE SUPPORT BRACKET HAS CORROSION. RL020. INSTALLED NEW BRACKET SUPPORT P/N: 356N1011-1 BTCH #: 0004514718ON APU AIR INTAKE DUCT IAW B757-200PF SRM 51-40-02-0G-O. REVIEWED
- [SDR IPXA2026101448482](https://openairdocs.org/sdr/IPXA2026101448482.md): Frame · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF · Elevator Structure
  > RH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME AND UPPER SPLICE PLATE AT R/H ELEVATOR O/B AREA IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N2003 REV G. TOOL ID: 18-1041 DUE: 11/04/2026.
- [SDR IPXA2026101448406](https://openairdocs.org/sdr/IPXA2026101448406.md): Adapter · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF · Elevator Structure
  > RH ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. INSTALLED ADAPTER PLATE RH ELEVATOR STATIC DISCHARGER ON RH ELEVATOR UPPER SURFACE. IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N2229 REV A.
- [SDR IPXA2026091453546](https://openairdocs.org/sdr/IPXA2026091453546.md): Strap · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WHILE EVALUATING APU INLET SURROUND STRUCTURE FOUND CORROSION ON EXISTING AFT STRAP REPAIR AT BS 1825 BETWEEN S-3R TO S-6R. VERIFIED STEP 10, C/W SRM 53-80-15-2R-1, REPAIR 1, PARAG. 4. G. AND RII GMM 04-02.
- [SDR IPXA2026090848406](https://openairdocs.org/sdr/IPXA2026090848406.md): Static Wick · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF · Elevator Miscellaneous Structure
  > RIGHT ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. 83-023. ATA 23-60. QCI: VERIFIED STEP 1 AND 2
- [SDR IPXA2026090848482](https://openairdocs.org/sdr/IPXA2026090848482.md): Static Wick · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF · Elevator Miscellaneous Structure
  > RH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. VERIFIED STEP 5 C/W
- [SDR IPXA2026090848502](https://openairdocs.org/sdr/IPXA2026090848502.md): Frame · bulged · Sep 2, 2026 · N463UP · Boeing 75724APF · Elevator, Spar/Rib
  > RH ELEVATOR LOWER SURFACE O/B CONDUCTIVE FRAME SPLICE HAS BULGING, EVIDENCE OF CORROSION UNDERNEATH. 83-025. ATA 55-20. QCI: VERIFIED STEP 6 C/W
- [SDR IPXA2026101437466](https://openairdocs.org/sdr/IPXA2026101437466.md): Bracket · corroded · Sep 1, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > RH HORZ STAB TIP BONDING STRAP HAS CORROSION UNDERNEATH DISBONDED SEALANT. INSTALLED BONDING BRACKET, 1 EA RIB AND 1EA NEW BONDING JUMPER PN: BACJ40E20-20 BATCH: 0004505758 AT R/H HORZ STAB REAR SPAR O/B IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 183N1703. TO
- [SDR IPXA2026101636983](https://openairdocs.org/sdr/IPXA2026101636983.md): Frame · corroded · Sep 1, 2026 · N463UP · Boeing 75724APF · Elevator, Plate/Skin
  > LH ELEVATOR UPPER, O/B CONDUCTIVE FRAME HAS BULGING ACROSS FASTENERS. INSTALLED L/H UPPER CONDUCTIVE FRAME, 1 EA UPPER SPLICE PLATE AND 1 EA STATIC DISCHARGER BASE AT L/H ELEVATOR O/B AREA IAW B757-200PF SRM 51-40-02-0G-0 AND DWG 183N2003.
- [SDR IPXA2026102135854](https://openairdocs.org/sdr/IPXA2026102135854.md): Support Bracket · cracked · Sep 1, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RH WW SUPPORT BRACKET IS CRACKED MARKED JK-22 ATA 32 INSP AUDIT C/W
- [SDR IPXA2026100935479](https://openairdocs.org/sdr/IPXA2026100935479.md): Angle · corroded · Sep 1, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > LH HORZ STAB TIP T/E BONDING STRAP SUPPORT BRACKET HAS EXFOLIATION CORROSION. 83-003. ATA 55-10. INSTALLED 1 EA RIB 1EA HORZ STAB TIP STRAP ANGLE P/N 183N1341-1SAAU AND 1EA BONDING JUMPER PN: BACJ40E20-20 BATCH: 0004505758. AT L/H HORZ STAB REAR SPAR O/B IAW B
- [SDR IPXA2026101736976](https://openairdocs.org/sdr/IPXA2026101736976.md): Frame · corroded · Sep 1, 2026 · N463UP · Boeing 75724APF · Elevator, Spar/Rib
  > LH ELEVATOR LOWER, O/B END CONDUCTIVE FRAME SPLICE HAS EVIDENCE OF CORROSION UNDER SEALANT. ATA 55-20. 83-004.INSTALLED L/H LOWER CONDUCTIVE FRAME AND LOWER SPLICE PLATE AT L/H ELEVATOR O/B AREA IAW SRM 51-40-02-0G-0. AND DWG 183N2003.
- [SDR IPXA2026102034414](https://openairdocs.org/sdr/IPXA2026102034414.md): Bracket · cracked · Sep 1, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > RH WW PROX SENSOR BRACKET HAS A GOUGE.
- [SDR IPXA2026101934575](https://openairdocs.org/sdr/IPXA2026101934575.md): Bracket · cracked · Sep 1, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RH WW GUSSET IS CRACKED. INSTALLED REPLACEMENT BRACKET IN R/H WW REF B757-200 PF SRM 51-40-02-0G-0 REV 126-20.
- [SDR IPXA2026101828804](https://openairdocs.org/sdr/IPXA2026101828804.md): Strap · temp repair · Sep 1, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > ACCOMPLISH PERMANENT REPAIR AT MAIN CARGO DOOR CUTOUT LOWER STRAP AT BS 620 BTWN STR 24L-26L. IAW EO-84558-REQ001 REV 1. ACCOMPLISHED REPAIR PER EO-98915-REQ1 & EA 757-5330-01-B0828, REV. IR.
- [SDR IPXA2026100836983](https://openairdocs.org/sdr/IPXA2026100836983.md): Frame · damaged · Sep 1, 2026 · N463UP · Boeing 75724APF · Elevator Miscellaneous Structure
  > LH ELEVATOR UPPER, O/B CONDUCTIVE FRAME HAS BULGING ACROSS FASTENERS.
- [SDR IPXA2026090837466](https://openairdocs.org/sdr/IPXA2026090837466.md): Bonding Strap · damaged · Sep 1, 2026 · N463UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > RH HORZ STAB TIP BONDING STRAP HAS CORROSION UNDERNEATH DISBONDED SEALANT. REMOVED 1 EA DAMAGED BONDING JUMPER AT R/H HORZ STAB REAR SPAR TO ELEVATOR FRONT SPAR IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026101818153](https://openairdocs.org/sdr/IPXA2026101818153.md): Skin · dented · Aug 31, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > LEFT EXTERNAL FUSELAGE SKIN EXISTING REPAIR DOUBLER HAS 2 EA DENTS APPROX BTW BS 201 AND BS 222, STRG 20L THRU STGR 21L, ID STICKER NUM. (085-002). ATA 53-30. ACCOMPLISHED REPAIR PER EO-98916-REQ1 AND STE-SAA EA 757-5310-01-B0831 REV IR
- [SDR IPXA2026090814643](https://openairdocs.org/sdr/IPXA2026090814643.md): Strap · corroded · Aug 31, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SURROUND STRUCTURE (INTERIOR) HAS CORROSION AT LOWER LONGERON COMMON TO FWD STRAP,
- [SDR IPXA2026082195946](https://openairdocs.org/sdr/IPXA2026082195946.md): Unknown · odor · Aug 21, 2026 · N463UP · Boeing 75724APF · Air Distribution System
  > AT FL 390-410 ACRID BURNING TYPE SMELL COMMING FROM THE PACKS. UNABLE TO DETERMINE WHICH ONE. BACK TO NORMAL ON DESCENT. ACCOMPLISHED TROUBLSHOOTING IAW FIM REF 21-00-01/301. INSPECTED CABIN RECIRCULATION SYSTEM & ACCOMPLISHED ADJ /TEST OF CABIN RECIRCULATIO

Next page: https://openairdocs.org/aircraft/N463UP/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 = 'N463UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N463UP/reports

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