# Service difficulty reports: N427UP

A list on [N427UP](https://openairdocs.org/aircraft/N427UP.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 · 229 reports

- [SDR IPXA2026030476823](https://openairdocs.org/sdr/IPXA2026030476823.md): Skin · damaged · Feb 12, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, UPPER FUSELAGE EXTERNAL SKIN AT BS 1370, S4L - S5L HAD A LIGHTNING STRIKE. TEMPORARY FASTENER INSTALLED. REMOVED FASTENER IN FUSELAGE FOR LIGTHNING STRIKE IAW SRM 51-40-02. INSTALLED DOUBLER IAW 53-00-01-2R-28, TABLE 205.
- [SDR IPXA2026022820240](https://openairdocs.org/sdr/IPXA2026022820240.md): Tee Fitting · corroded · Feb 9, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Structure
  > LOWER FUSELAGE BS 1220 LT SIDE TEE FITTING EXFOLIATED. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.
- [SDR IPXA2026030320044](https://openairdocs.org/sdr/IPXA2026030320044.md): Tee Angle · corroded · Feb 9, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT FUSELAGE BS 1147 TEE ANGLE GOUGED AND CORRODED. INSTALLED A NEW TEE ANGLE, TWO STRAPS, & ONE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026030320240](https://openairdocs.org/sdr/IPXA2026030320240.md): Tee Angle · corroded · Feb 9, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > LOWER FUSELAGE BS 1220, LT SIDE TEE ANGLE EXFOLIATED.
- [SDR IPXA2026022786894](https://openairdocs.org/sdr/IPXA2026022786894.md): Skin · delaminated · Feb 7, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, APU COMPT LOWER SKIN BELOW THE EXHAUST DUCT INNER SURFACE DELAMINATED AT BS 1992. THE PROTECTIVE COATING WAS RESTORED IAW AMM 51-21-15-370-802.
- [SDR IPXA2026022486878](https://openairdocs.org/sdr/IPXA2026022486878.md): Skin · delaminated · Feb 7, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR APU COMPT LH WALL INNER SKIN DELAMINATED IN AREA ABOVE THE OIL COOLER AIR EXIT DUCT. PREPARED AREA AND FABRICATED REPAIR PARTS IAW B757-200PF SRM 51-70-10-2R-4.
- [SDR IPXA2026030387426](https://openairdocs.org/sdr/IPXA2026030387426.md): Bracket · cracked · Feb 7, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > LEFT MLG WW INBD SEAL RETAINER SUPPORT STRUCTURE BRACKET 6EA, FOUND CRACKED AFTER REMOVAL OF SEAL RETAINER BS 1060. INSTALLED NEW BRACKETS IAW SRM 51-40-02.
- [SDR IPXA2026022593920](https://openairdocs.org/sdr/IPXA2026022593920.md): Support Angle · corroded · Feb 7, 2026 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO AT STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19 HAS CORROSION DOT 5842-11 REMOVED CORROSION AT THE STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19. I.A.W SRM 51-10-02. AFTER FURTHER EVALUATION IT WAS FOUND OUT OF LIMITS. I.A.W SRM 51-10-
- [SDR IPXA2026021691664](https://openairdocs.org/sdr/IPXA2026021691664.md): Transition Panel · dented · Feb 7, 2026 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO TRANSITION PANEL AT STA 630 RBL 22 HAS A GOUGE. REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALLED REPAIR PART ON SIDE PANEL AT STA 630 RBL22. IAW B757-200 WITH SREO-3220-REQ003, SRM 51-70-13 FR
- [SDR IPXA2026030267696](https://openairdocs.org/sdr/IPXA2026030267696.md): Bracket · corroded · Feb 6, 2026 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > ACCESS DOOR 313AL LT & RT LATCH STOPS AT THE CUT-OUT, TWO BRACKETS ARE CORRODED. REMOVED ADJACENT STRIP AT BS 1885 TO FACILTATE MAINTENANCE, FOR REMOVAL OF ACCESS DOOR 313AL LT & RT LATCH STOPS AT THE CUT-OUT IAW SRM 51-40-02. INSTALLED TWO BRACKETS AND AD
- [SDR IPXA2026021468498](https://openairdocs.org/sdr/IPXA2026021468498.md): Strap · corroded · Feb 6, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > APU INLET DOOR FWD OF OPENING HAS CORROSION. REMOVED STRAP IAW SRM 51-40-02. INSTALLED NEW STRAP IAW SRM 51-40-02 IN APU INLET DOOR FWD.
- [SDR IPXA2026030360879](https://openairdocs.org/sdr/IPXA2026030360879.md): Intercostal · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.
- [SDR IPXA2026030359670](https://openairdocs.org/sdr/IPXA2026030359670.md): Tee Angle · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.
- [SDR IPXA2026022760898](https://openairdocs.org/sdr/IPXA2026022760898.md): Intercostal · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.
- [SDR IPXA2026022860882](https://openairdocs.org/sdr/IPXA2026022860882.md): Intercostal · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.
- [SDR IPXA2026030360752](https://openairdocs.org/sdr/IPXA2026030360752.md): Tee Angle · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > LEFT WING TO BODY, BS 1030 BEHIND PANEL 197AL TEE ANGLE CORRODED AT LBL 26. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026021961043](https://openairdocs.org/sdr/IPXA2026021961043.md): Shim · corroded · Feb 5, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT/STR/ZONE 100 EXTERIOR RIGHT SIDE. WINGB / BODY PANEL 198KR STRUCTURE HAS CORROSION. REMOVED 01 EA SHIM LOCATED BTW STA 1180 TO STA 1240 AND RBL57. IAW B757-200 SRM 51-40-02 INSTALLED SPACER SHIM IAW SRM B757-200 TASK: 51-40-02
- [SDR IPXA2026030841896](https://openairdocs.org/sdr/IPXA2026030841896.md): Tee Angle · corroded · Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 10 - 40 HAS CORROSION AT NUTPLATE HOLES. INSTALLED TEE-ANGLE AND PLATES AT RT WING TO BODY IAW SRM 51-40-02.
- [SDR IPXA2026030243996](https://openairdocs.org/sdr/IPXA2026030243996.md): Panel · cracked · Feb 4, 2026 · N427UP · Boeing 75724APF · Wing, Center Box
  > NR 2 PYLON GAP PANEL HAS A CRACK IN LOWER SURFACE. INSTALLED ONE DOUBLER & FILLER WASHERS IAW SRM 51-40-02, AND SRM 57-41-01-2R-3, REPAIR 3.
- [SDR IPXA2026022839378](https://openairdocs.org/sdr/IPXA2026022839378.md): Frame · dented · Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO FRAME AT BS 1500 RT, DENTED. VERIFIED ACCOMPLISHMENT OF EO-96676-REQ1, AND EA 757-5360-27-A4324, REV- AS RII IAW UPS GMM 04-02-01-15.
- [SDR IPXA2026030443086](https://openairdocs.org/sdr/IPXA2026030443086.md): Tee Fitting · gouged · Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT - STR - Z100 - LH UPPER WING TO BODY T-CHORD AT STA 1147 HAS GOUGE ON EDGE DOT 5698-08 INSTALLED T-CHORD AT LH WING STA 1147 I.A.W. B757 SRM 51-40-02.
- [SDR IPXA2026020942975](https://openairdocs.org/sdr/IPXA2026020942975.md): Support · cracked · Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > LEFT MLG I/B SEAL RETAINER SUPPORT STRUCTURE HAS A CRACK IN THE CORNER AT BS 1060 VERIFIED INSTALLED SEAL RETAINER SUPPORT STRUCTURE AT LT MLG INBD BS 1060 IAW SRM 51-40-02.
- [SDR IPXA2026022139192](https://openairdocs.org/sdr/IPXA2026022139192.md): Frame · dented · Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Frame
  > MAJOR REPAIR, AFT CARGO FRAME AT STA 1300 RH IS DENTED. VERIFIED STEP 47. COMPLIED WITH EO-96677-REQ1, AND EA 757-5360-27-A4325, REV-.
- [SDR IPXA2026030342999](https://openairdocs.org/sdr/IPXA2026030342999.md): Tee Angle · corroded · Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > LEFT WING TO BODY TEE ANGLE, BS 1260, BEHIND PANEL 197LL, CORRODED.
- [SDR IPXA2026030340724](https://openairdocs.org/sdr/IPXA2026030340724.md): Tee Angle · corroded · Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > LEFT WING UNDER UPPER WING TO BODY PANEL 195BL HAD CORROSION. INSTALLED A TEE ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026030341147](https://openairdocs.org/sdr/IPXA2026030341147.md): Doubler · corroded · Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT WING TO BODY TEE ANGLE, BS 1040 - 1059, RBL 40 - 60, INLET STRUCTURE HAD CORROSION. INSTALLED RAMP EXHAUST DOUBLER & PAX EXHAUST ASSY AT RT WING TO BODY TEE ANGLE IAW SRM 51-40-02-OG.
- [SDR IPXA2025120140366](https://openairdocs.org/sdr/IPXA2025120140366.md): Door Seal · torn · Nov 25, 2025 · N427UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR SEAL TORN (FAA FINDING). TRIM ENTRY DOOR SEAL TO CLEAR DOOR LATCH MECHANISM IAW DWG 232N1643 SH3. OPS CHECKED NORMAL.
- [SDR IPXA2025112640366](https://openairdocs.org/sdr/IPXA2025112640366.md): Door Seal · torn · Nov 25, 2025 · N427UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR SEAL TORN.
- [SDR IPXA2025022044028](https://openairdocs.org/sdr/IPXA2025022044028.md): Lever · binding · Feb 19, 2025 · N427UP · Boeing 75724APF · Flight Compartment Windows
  > CAPTAINS WINDOW UNLOCK LEVER HARD TO MOVE. ACCOMPLISHED ADJUSTMENT OF N2 WINDOW IAW AMM 56-11-02-825-001 REV 136. OPERATIONAL TEST IAW AMM 56-11-02-715-020 REV 136 SATIS.
- [SDR IPXA2025011305368](https://openairdocs.org/sdr/IPXA2025011305368.md): Window · faulted · Jan 3, 2025 · N427UP · Boeing 75724APF · Flight Compartment Windows
  > L SIDE WINDOW *EICAS. LH NO.2 SLINGING WINDOW REPLACED BY SERVICEABLE. I.A.W AMM 56-11-02/401 REV 135, CONFIRM THE WINDOW IS CORRECT ELECTRICAL CONNECTED IAW GMM MTX 04.02.01 REV.9. OPERATIONAL CHECK AND ADJUST C/O O.K WINDOW AND SYSTEM CONSIDERED FULLY SE
- [SDR IPXA2025010305368](https://openairdocs.org/sdr/IPXA2025010305368.md): Controller · malfunctioned · Jan 3, 2025 · N427UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > *SDR FILED OPEN* L SIDE WINDOW *EICAS( ACCOMPLISHED TROUBLESHOOTING PER WDM 30-41-12-1 REV 97. SWAPPED WINDOW HEAT CONTROLLER LEFT WITH RIGHT. SAME FAULT. SWAPPED BACK TO ORIGINAL POSITION PER AMM 30-41-01 PB 401 REV 135. MEASURED RESISTANCE ON WINDOW CONTROL
- [SDR IPXA202410290001](https://openairdocs.org/sdr/IPXA202410290001.md): O-Ring · deformed · Oct 15, 2024 · N427UP · Boeing 75724APF · Hydraulic System, Main
  > LOST THE LEFT HYD ALMOST COMPLETELY DURING DESCENT TO LHBP (BUDAPEST, LISZT FERENC NATIONAL AIRPORT HUNGARY). THE A/C LANDED AND STOPPED SAFELY ON RNWY 13R. A/C TOWED TO STAND T/S STARTED TO INVESTIGATE THE CAUSE OF HYD LOSS L/H HYD SYS. LINE MTC TROUBLE S
- [SDR IPXA2024101636812](https://openairdocs.org/sdr/IPXA2024101636812.md): Packing · leaking · Oct 15, 2024 · N427UP · Boeing 75724APF · Hydraulic System, Main
  > *EMERGENCY DECLARED* L HYD SYS PRESS PERFORMED QRH PROCEDURES ENG 1 CASE DRAIN MODULE UNION AND PACKING REPLACED IAW AMM 29-11-17,LEAKAGE CHECK SATIS,IAW AMM 29-11-17,
- [SDR IPXA2024031116195](https://openairdocs.org/sdr/IPXA2024031116195.md): Intercostal · corroded · Feb 29, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FAULT: L/H FWD OF HOT AIR EXHAUST HAS CORROSION. DOT 33-007 INSTALLED NEW INTERCOSTAL IAW B757 SRM 51-40-02-0G. INSTALLED HOT AIR EXHAUST L/H COVER IAW B757 AMM 21-53-04-404-012. VERIFIED INSTALLATION OF COVER, JOB COMPLETE
- [SDR IPXA2024031805314](https://openairdocs.org/sdr/IPXA2024031805314.md): Floorbeam · corroded · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FLOORBEAM BS 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING INSTALLED T-CHORD STA 1040 I.A.W. B757 SRM 51-40-02-OG. JOB WAS ACCOMPLISHED PER UPS EO: EO-89720-REQ1 AND VT MAE EA 757-5340-27-A3538 REV -. WITHOUT ANY DEVIATIONS.
- [SDR IPXA2024031405260](https://openairdocs.org/sdr/IPXA2024031405260.md): Floorbeam · corroded · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FAULT- T-CHORD STA 900 BETWEEN LBL 20 TO LBL 40 LOWER SURFACE WITH CHAFING. INSTALLED T-CHORD AND (8 EA) REPAIR SPLICE PLATES I.A.W. B757-200 SRM 51-40-02-0G AND SRM 51-70-12-05-0 DETAIL LLL.
- [SDR IPXA2024031405314](https://openairdocs.org/sdr/IPXA2024031405314.md): Floorbeam · chafed · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > T-CHORD STA 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING VERIFIED ACCOMPLISHMENT OF EA 757-5340-27-A3538 STEPS 1-3 PRELIMINARY 1
- [SDR IPXA2024031406476](https://openairdocs.org/sdr/IPXA2024031406476.md): Frame · dented · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO PIT STA 1320, SRG 26 RH HAS A DENT ON FRAME ACCOMPLISH REPAIR PER EO-89673-REQ1 REV 1 AND VT-MAE EA 757-5360-27-A3530, REV. -., PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2024031306423](https://openairdocs.org/sdr/IPXA2024031306423.md): Shear Tie · dented · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Internal Mounting Structure
  > AFT CARGO PIT STA 1320, STG 25 LH HAS A DENT ON FRAME. VERIFIED ACCOMPLISMENT OF STEPS 12-27 OF EA 77-5360-27-A3533 REV. WITH NOTED DEVIATION.
- [SDR IPXA2024031204950](https://openairdocs.org/sdr/IPXA2024031204950.md): Tee Fitting · corroded · Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > *SDR FILED OPEN* FAULT - T-CHORD STA 1040 BETWEEN RBL 10 TO RBL 20 LOWER SURFACE WITH CHAFING. VERIFIED: INSTALLED T-CHORD STA 1040 I.A.W. B757 200 51-40-02-OG. INSTALLED COVER HOT AIR EXHAUST ACTUADOR I.A.W. SRM 51-40-02-OG. VERIFIED COVER INSTALLED
- [SDR IPXA2024031371410](https://openairdocs.org/sdr/IPXA2024031371410.md): Transition Panel · corroded · Feb 26, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL HAS EXFOLIATION CORROSION ARROUND TIE DOWN FITTINGS AT STA 1620, 1600 AND 1580 INSTALLED DOUBLER AND TRANSITION PANEL I.A.W. B757-200 S.R.M. 51-40-02-OG.
- [SDR IPXA2024031371207](https://openairdocs.org/sdr/IPXA2024031371207.md): Transition Panel · corroded · Feb 26, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL BETWEEN STA 1360 AND 1380 HAS EXFOLIATION CORROSION. INSTALLED TRANSITION PANEL BTW STA 1360 AND 1380 RH IAW SRM 51-40-02-0G.
- [SDR IPXA2024030471433](https://openairdocs.org/sdr/IPXA2024030471433.md): Tie Down · corroded · Feb 26, 2024 · N427UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > FAULT: AFT CARGO PIT - TIE DOWN FITTING STA 1500 RH SIDE WITH EXFOLIATION CORROSION INSTALLED TIE DOWN FITTING P/N 146N5440-56 BATCH 4245698 AT STA 1500 RH IAW SRM 51-40-02-0G. VERIFIED TIE DOWN FITTING P/N 146N5440-56 INSTALLED. JOB COMPLETE
- [SDR IPXA2024022771207](https://openairdocs.org/sdr/IPXA2024022771207.md): Transition Panel · corroded · Feb 26, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL BETWEEN STA 1360 AND 1380 HAS EXFOLIATION CORROSION. REMOVED TRANSITION PANEL BETWEEN STA 1310 TO STA 1380 R/H SIDE I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2024022771410](https://openairdocs.org/sdr/IPXA2024022771410.md): Transition Panel · corroded · Feb 26, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *** SDR FILED OPEN *** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL HAS EXFOLIATION CORROSION ARROUND TIE DOWN FITTINGS AT STA 1620, 1600 AND 1580 REMOVED CORROSION I.A.W. B757-200 S.R.M. 51-10-02. SIDE PANEL IS OUT OF LIMITS I.A.W. B757-200 S.R.M 53-00-53-
- [SDR IPXA2023121901449](https://openairdocs.org/sdr/IPXA2023121901449.md): Unknown · unknown · Dec 19, 2023 · N427UP · Boeing 75724APF · Outside Air Temperature Indicator/Sensor
  > *** DIVERSION *** AT APPROX V/R CAPT PFD DISPLAYED WINDSHEAR WITH FULL SCALE A/S AND ALT DEVIATIONS OVERSPEED, RUDDER RATIO AND MACH SPEED TRIM EICAS ILLUMINATED. F/O PFD WAS NORMAL. A/T WERE DISENGAGED TO STOP A/T FLU C/W 30 CHECK IAW MM 34-12-00-715-001, 22-
- [SDR IPXA2023051293198](https://openairdocs.org/sdr/IPXA2023051293198.md): Engine · fire · May 11, 2023 · N427UP · Boeing 75724APF · Powerplant System
  > INSPECTION TYPE:NAR- ENG FIRE ON GRND. SECURED ENG. 1 BOTTLE FIRED *DOES NOT MEET SDR CRITERIA*PCMCIA CARD DOWNLOADED AND RE-INSTALLED IAW AMM 31-31-90-401. ENGINEERING REPORTS ENGINES PARAMETERS NORMAL AND RIGHT ENGINE NOT STABILIZED WHEN ABORTED. RAN RIGHT E
- [SDR IPXA2022040380790](https://openairdocs.org/sdr/IPXA2022040380790.md): Splice Strap · corroded · Apr 3, 2022 · N427UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:S-4AFT CARGO SHEAR TIE AND BUTT SPLICE BEAR STRAP AT STA 1400, BETWEEN S-30R AND S-29L HAS CORROSIONREPAIRED IAW UPS EO B757-5330-83317-A AND VT MAE EA 757-5360-27-A2882 REV-
- [SDR IPXA2022032480445](https://openairdocs.org/sdr/IPXA2022032480445.md): Floor Panel · damaged · Mar 24, 2022 · N427UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:INTMAIN CARGO COMPARTMENT, FLOOR PANEL 232XSF DAMAGEDFABBED PANEL 232XSF FROM 5024N400001SS-G, BATCH # 3855547 PER SREO B757-5320-9692-K
- [SDR 145Y20200707001](https://openairdocs.org/sdr/145Y20200707001.md): Union · sheared · Jul 2, 2020 · N427UP · Boeing 75724APF · Hydraulic System, Main
  > ENGINEER REPORTED AN OCCURRENCE FROM THE STATION PRG. OCCURRED AT 02.07.2020 AND WAS REPORTED AT 06.07.2020 TO HEALTH AND SAFETY DEPARTMENT QA/H&S NAYAK AIRCRAFT SERVICES. RELATED AIRCRAFT IS N-487UP OF OPERATOR UPS. ON DESCENT RECEIVED L HYD PRESS MSG AND SY

Next page: https://openairdocs.org/aircraft/N427UP/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 = 'N427UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N427UP/reports

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