# Service difficulty reports: N422UP

A list on [N422UP](https://openairdocs.org/aircraft/N422UP.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 · 271 reports

- [SDR IPXA2026040685799](https://openairdocs.org/sdr/IPXA2026040685799.md): Support Strap · corroded · Mar 15, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CORROISION FOUND ON FWD CARGO CEILING GILL LINER SUPPORT STRAP UNDER NUT PLATE STA 820 LBL 45. FOUND WHILE WORKING EO.89712-REQ007 DECOMPRESSION PANEL.ATA 25. INSTALLED STRAP P/N STESAA7003345555-7 AT FWD CARGO CEILING SUPPORT STA 760 TO STA 840 LBL 45.5 PE
- [SDR IPXA2026031475944](https://openairdocs.org/sdr/IPXA2026031475944.md): Web · corroded · Mar 14, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN.
- [SDR IPXA2026031425145](https://openairdocs.org/sdr/IPXA2026031425145.md): Floorbeam · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR, AGING A/C INSP DOT AA024 STR ATA 53-00 MAIN CABIN FLOORBEAM CORRODED STA 1420 RH OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR INSTALLED FABRICATED -1 REPAIR ANGLE, FABRICATED -2 FILLER AND FABRICATED RADIUS FILLER REPAIR PARTS PER B757-200PF SRM
- [SDR IPXA2026032324391](https://openairdocs.org/sdr/IPXA2026032324391.md): Splice Strap · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Floor Panel
  > WORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510. SPLICE STRAP P/N 453N1611-23 TO BE INSTALLED. AUDITED
- [SDR IPXA2026032324635](https://openairdocs.org/sdr/IPXA2026032324635.md): Splice Strap · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP BS 1470. FABRICATED 01 EA SPLICE STRAP P/N 453N1611-25 IAW DWG 453N1611 SHT 1 REV. A AND IAW SRM 51-40-05-0G-0.
- [SDR IPXA2026031424391](https://openairdocs.org/sdr/IPXA2026031424391.md): Splice Strap · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510 ATA 53-60 PRODUCTION AUDIT C/W
- [SDR IPXA2026031424635](https://openairdocs.org/sdr/IPXA2026031424635.md): Splice Strap · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1470 PRODUCTION AUDDIT C/W
- [SDR IPXA2026022825145](https://openairdocs.org/sdr/IPXA2026022825145.md): Floorbeam · corroded · Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CORRODED BS 1420 RT OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR VERIFIED STEP 17. FORMED TWO REPAIR ANGLES IAW SRM 53-00-51-2R-6.
- [SDR IPXA2026022845547](https://openairdocs.org/sdr/IPXA2026022845547.md): Floor Skin · corroded · Feb 22, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Structure
  > CORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN. REMOVED CORROSION FROM 2EA. FLOOR WEB PANELS IAW B757-200PF SRM 51-10-02-0G-0. INSTALLED 2EA. FLOOR WEB PANELS, 1EA. STRAP, AND 2EA. FILLERS IAW B757-200PF SRM51-40-02-0G-0, AND SEALED IAW B757-200PF AMM 5
- [SDR IPXA2026031635090](https://openairdocs.org/sdr/IPXA2026031635090.md): Floorbeam · corroded · Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR. UPON REMOVAL OF DAMAGED ON DECK PLATE, FOUND FLOORBEAM UPER FLANGE EXFOLIATED BS 1681, LBL 28 - 33. REMOVED THE DAMAGE. CUT OUT THE FLOORBEAM UPPER TEE AND CUT AWAY ANY DAMAGE ON FLOORBEAM VERTICAL WEB AS REQUIRED IAW E.A. 757-5310-01-B0703
- [SDR IPXA2026032038490](https://openairdocs.org/sdr/IPXA2026032038490.md): Floor Support · corroded · Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, ID STICKER NUM. (085-002). REMOVED 2 EA NUTPLATES AND REMOVED CORROSION AT STA 1470 AFT CARGO COMP FLOOR STRUC
- [SDR IPXA2026030838490](https://openairdocs.org/sdr/IPXA2026030838490.md): Floor Support · corroded · Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, INSTALLED 4 EA NUTPLATES AT AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER BTW STA 1440 AND STA 1480 LBL 16.10 I
- [SDR IPXA2026031138732](https://openairdocs.org/sdr/IPXA2026031138732.md): Floor Support · corroded · Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 7.55, ID STICKER NUM. (085-004). ATA 53-10 VERIFIED STEP 24, C/W B757-200PF AMM 51-24-09-377-001.
- [SDR IPXA2026031810473](https://openairdocs.org/sdr/IPXA2026031810473.md): Floor Panel · gouged · Feb 20, 2026 · N422UP · Boeing 75724APF · Fuselage Floor Panel
  > APPROX. 1 INCH LINE GOUGE, DIRT/ DEBRIS ON AFT CARGO FLOOR PANEL TAGGED, FROM BS 1460 - 1500. BLENDED DAMAGE. ORIGINAL MATERIAL THICKNESS IS.071, MATERIAL REMOVED IS.021. FABRICATED, LOCATED, DRILLED AND COUNTERSUNK NEW FLOOR PANEL 161AF IAW SRM 51-40-05-
- [SDR IPXA2026031499164](https://openairdocs.org/sdr/IPXA2026031499164.md): Floorbeam · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR, MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOOR BEAM UNDERNEATH SURFACE REF SRM 51-10-02-0G-0 REPAIRED PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAI
- [SDR IPXA2026032299492](https://openairdocs.org/sdr/IPXA2026032299492.md): Stringer Splice · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMP FLOOR STGR AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. INSTALLED 1 EA NEW FLOOR STRINGER AT AFT CARGO COMPARTMENT STA. 1460, RBL 15 IAW B757-200PF SRM 51-40-02-0G-0 PAR 4 AND PAR 7.
- [SDR IPXA2026031493675](https://openairdocs.org/sdr/IPXA2026031493675.md): Support Angle · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION. LOWER SUPPORT ANGLE APU INLET P/N 148N3152-2 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N LINE # 614
- [SDR IPXA2026031699642](https://openairdocs.org/sdr/IPXA2026031699642.md): Strap · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP LH SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN BS 1560 & 1580 IS CORRODED. INSTALLED NEW CEILING DECOMPRESSION PANEL STABILIZATION STRAP, AND 1EA. REPAIR SPLICE AT STA. 1610 L/HÂ IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026031393618](https://openairdocs.org/sdr/IPXA2026031393618.md): Strap · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE AFT STRAP IS CORRODED ATA 53-80 INSTALLED, 1EA REPAIR STRAP, 2EA REPAIR FILLER, 1EA STRAP AND 1EA EXISTING STRAP AT APU INLET SUPPORT STRUCTURE AFT IAW 757-200PF-SRM 53-80-15-2R-1 REPAIR 1.
- [SDR IPXA2026031499075](https://openairdocs.org/sdr/IPXA2026031499075.md): Floorbeam · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR AREA STA 1681 LBL 31 METAL PLATE PANEL SURFACE BULGING SIGN OF CORROSION. ACCOMPLISHED REPAIR PER SRM 53-60-51-2R-6 REPAIR 6.
- [SDR IPXA2026031499159](https://openairdocs.org/sdr/IPXA2026031499159.md): Retainer · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Structure
  > MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 ANGLE BAR SURFACE BULGING AND FASTENER HEAD FULL THROUGH SIGN OF CORROSION. INSTALLED NEW ANGLE BAR FASTENER RETAINER AT MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026031499642](https://openairdocs.org/sdr/IPXA2026031499642.md): Strap · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP LT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1560 AND 1580 IS CORRODED. 83-015. ATA 53-00 QC AUDIT C/W
- [SDR IPXA2026031499696](https://openairdocs.org/sdr/IPXA2026031499696.md): Strap · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP RT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1400 AND 1420 HAS CORROSION. 83-018. INSTALLED DECOMPRESSION PANEL LANDING ON AFT CARGO COMP RH SIDE CEILING DECOMPRESSION PANEL STRAP IAW B757-200PF SRM 51-41-02-0G-0.
- [SDR IPXA2026031499056](https://openairdocs.org/sdr/IPXA2026031499056.md): Seat Track · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORROSION. INSTALLED FABRICATED FILLER AT MAIN DECK RBL45 SEAT TRACK P/N 146N5337-1SAAU IAW B757 SRM 51-40-02-0G-0 AND DWG 146N5337.
- [SDR IPXA2026031693647](https://openairdocs.org/sdr/IPXA2026031693647.md): Support Angle · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION.
- [SDR IPXA2026031693675](https://openairdocs.org/sdr/IPXA2026031693675.md): Support Angle · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION ATA 53-80 PRODUCTION AUDIT C/W
- [SDR IPXA2026031493686](https://openairdocs.org/sdr/IPXA2026031493686.md): Support Angle · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE FWD SIDE SMALL UPPER SUPPORT ANGLE HAS CORROSION. FABRICATED LOWEER SUPPORT ANGLE APU INLET IAW DWG 148N3141/ SAMPLE, WORK ACCOMPLISHED ON TRAVELER 7003344123. LOWER SUPPORT ANGLE APU INLET WILL BE INSTALLED ON JOB CARD T3F18E008AL
- [SDR IPXA2026031498924](https://openairdocs.org/sdr/IPXA2026031498924.md): Support Angle · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION ATA 53-80 UPPER SUPPORT ANGLE APU INLET P/N 148N3152-1 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N.
- [SDR IPXA2026022399164](https://openairdocs.org/sdr/IPXA2026022399164.md): Floorbeam · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION.
- [SDR IPXA2026022899492](https://openairdocs.org/sdr/IPXA2026022899492.md): Floor Support · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP FLOOR SUPPORT AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. 83-010. VERIFIED REMOVAL OF FLOOR SUPPORT ON STEP 7.
- [SDR IPXA2026022399056](https://openairdocs.org/sdr/IPXA2026022399056.md): Seat Track · corroded · Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORRODED. 7VERIFIED STEP 6 HAS BEEN ACCOMPLISHED.
- [SDR IPXA2026031355302](https://openairdocs.org/sdr/IPXA2026031355302.md): Support Strap · corroded · Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INTAKE SUPPORT STRUCTURE FWD STRAP CORRODED FWD O/B SIDE. 61-016 ATA 53-80 INSTALLED 1EA UPPER SUPPORT ANGLE P/N: 148N3152-2, 1EA LOWER SUPPORT ANGLE P/N: 148N3152-1 APU INTAKE SUPPORT STRUCTURE BETWEEN STA 1787.45 AND STA 1825.00 STR 3R AND STR 6R IAW 757
- [SDR IPXA2026022355337](https://openairdocs.org/sdr/IPXA2026022355337.md): Nut Plate · corroded · Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > CORROSION AROUND NUT PLATE 5 INCHES FWD OF STATION 1720 BTWN 24.75LB AND 0 LB AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1715 BTWN 24.75BL TO 0 BL IAW SRM 51-40-02-0G-0. OK TO REINSTALL PAN.
- [SDR IPXA2026030956993](https://openairdocs.org/sdr/IPXA2026030956993.md): Drain Mast · corroded · Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Structure
  > RIGHT AFT FUSELAGE RT APU EXHAUST CONE DRAIN MAST BASE EXFOLIATED. REMOVED CORROSION AT RT AFT FUSELAGE AT APU EXHAUST DRAIN MAST BASE IAW SRM 51-10-02-0G-0. INSTALLED DRAIN MAST FROM RT AFT FUSELAGE RH APU EXHAUST CONE IAW IAW AMM 28-25-05-404-162.
- [SDR IPXA2026030855388](https://openairdocs.org/sdr/IPXA2026030855388.md): Nut Plate · corroded · Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > CORROSION AROUND NUT PLATE 6 INCHES AFT OF STA 1701 BTWN LBL 45.5 AND 62. AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1707 BTWN LBL 45.5 AND LBL 62 IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025121057370](https://openairdocs.org/sdr/IPXA2025121057370.md): Brake · inoperative · Dec 10, 2025 · N422UP · Boeing 75724APF · Landing Gear Brake System
  > UPON BLOCK IN AT DF THE PARKING BRAKE WAS SET THE BRAKES WERE RELEASED AND I FELT THE A\C MOVING. LOOKED UP AND QUICKLY SET THE FOOT BRAKES. ATTEMPTED TO SET THE PARKING BRAKE BUT IT WOULD NOT HOLD TESTED BRAKE IAH FIM 32-44. NORMAL OPERATION
- [SDR IPXA2025071881182](https://openairdocs.org/sdr/IPXA2025071881182.md): Sign · inoperative · Jul 17, 2025 · N422UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY EXIT SIGN HAS 7 EACH LIGHTS INOP. ++REPLACED 7 EACH BULBS IN EMERGENCY EXIT SIGN IAW AMM 33-51-01 OPS CHECK GOOD
- [SDR IPXA2025012126292](https://openairdocs.org/sdr/IPXA2025012126292.md): None · none · Jan 16, 2025 · N422UP · Boeing 75724APF · Standard Practices/Structures
  > REF HEAVY CHECK REPAIR T3F18E004J5QK, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3771, REV- COMPLETED.COMPLIED WITH EO-92554. REVIEWED.
- [SDR IPXA2025012222873](https://openairdocs.org/sdr/IPXA2025012222873.md): Window · scratched · Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment Windows
  > **SUPPLEMENTAL SDR**FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. <BR>INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-0
- [SDR IPXA2025011622873](https://openairdocs.org/sdr/IPXA2025011622873.md): Window · scratched · Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment Windows
  > FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-02.
- [SDR IPXA2024102987439](https://openairdocs.org/sdr/IPXA2024102987439.md): Windshield · cracked · Oct 27, 2024 · N422UP · Boeing 75724APF · Flight Compartment Windows
  > LEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING. COMPLETED #1 WINDSHIELD INSTALL IAW AMM 56-11-01. WITNESSED TERMINAL HARDWARE TORQUE OF THE #1 WINDSHIELD. C/W AS REQUIRED PER GMM 04-02 AND TORQUES WERE DONE PER AMM 56-11-01.
- [SDR IPXA2024102887439](https://openairdocs.org/sdr/IPXA2024102887439.md): Windshield · cracked · Oct 27, 2024 · N422UP · Boeing 75724APF · Flight Compartment Windows
  > LEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING REMOVED AND REPLACED #1 WINDSHIELD REF AMM 56-11-01 UP TO STEP 13 (A) FIRST TORQUE. INITIAL TORQUE HAS BEEN ACCOMPLISHED @0330L ON 10/28/2024.
- [SDR IPXA2024061824985](https://openairdocs.org/sdr/IPXA2024061824985.md): Floor Support · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > R/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION. VERIFIED INSTALLED NUT PLATE IN T-CHORD STA 1040 -1060 RBL 0-68 IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024061428155](https://openairdocs.org/sdr/IPXA2024061428155.md): Floor Support · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT FLIGHT DECK ENTRANCE STA 297 SECTION 41 LOWER FLOOR BRACKET CORROSION DOT 44-44 INSTALLED ANGLE FROMFLIGHT DECK ENTRANCE STA 297, SECC 41, I.A.W. SRM 51-40-02-0G REVIEWED
- [SDR IPXA2024061425327](https://openairdocs.org/sdr/IPXA2024061425327.md): Tee Angle · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > L/H T-CHORD FROM STA 1040-1060 LBL 0-37 HAS EXFOLIATED CORROSION (NEXT TO RAM EXHAUST) INSTALLED NEW LH T-CHORD ON STA 1040-1060 LBL0-37IAW B757 SRM 51-40-02 REVIEWED
- [SDR IPXA2024061225283](https://openairdocs.org/sdr/IPXA2024061225283.md): Tee Angle · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *** SUPPLEMENTAL SDR *** FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) INSTALLED NEW T-CHORD AT STA 1045 L/H. FASTENER P/N NAS603-16P, BATCH # 0004207085. IAW SRM 51-40-02-0G.
- [SDR IPXA2024060924985](https://openairdocs.org/sdr/IPXA2024060924985.md): Tee Angle · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FAULT: R/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION JOP COMPLETE.
- [SDR IPXA2024060725283](https://openairdocs.org/sdr/IPXA2024060725283.md): Tee Angle · corroded · May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > **SDR FILED OPEN**FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) VERIFIED INSTALL
- [SDR IPXA2024061899986](https://openairdocs.org/sdr/IPXA2024061899986.md): Floor Support · corroded · May 22, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > **SUPPLEMENTAL SDR** FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION.INSTALLED NEW T-CHORD IAW SRM 51-40-02. INSTALLED NUT PLATES IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024060899986](https://openairdocs.org/sdr/IPXA2024060899986.md): Tee Angle · corroded · May 22, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION VERIFIED INSTALL.

Next page: https://openairdocs.org/aircraft/N422UP/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 = 'N422UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N422UP/reports

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