# Service difficulty reports: N410UP A list on [N410UP](https://openairdocs.org/aircraft/N410UP.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 3 · 130 reports - [SDR IPXA2026061692797](https://openairdocs.org/sdr/IPXA2026061692797.md): Fuel Tank · warning message · Jun 16, 2026 · N410UP · Boeing 75724APF · Fuel Storage > RIGHT CENTER FUEL TANK PRESS ICAS. CENTER TANK HAD 3.8K USABLE FUEL ACCOMPLISHED DMP PER MEL 28-22-2-0-1 - [SDR IPXA2026020246985](https://openairdocs.org/sdr/IPXA2026020246985.md): Lamp · inoperative · Jan 30, 2026 · N410UP · Boeing 75724APF · Emergency Lighting > EMERGENCY EXIT LIGHT- MANY LAMPS INOP. RELAMPED ALL EMERGENCY EXIT LIGHT, OPS CHECKS NORMAL IAW AMM 33-51-00-501. - [SDR IPXA2026012369147](https://openairdocs.org/sdr/IPXA2026012369147.md): Tee Fitting · corroded · Jan 12, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > RIGHT WW EXTERNAL STRUCTURE BETWEEN BS 1040 - 1060 INTERCOSTAL DELAMINATED. INSTALLED NEW T-FITTING, IAW SRM 51-40-02-0G-0. - [SDR IPXA2026012769147](https://openairdocs.org/sdr/IPXA2026012769147.md): Intercostal · delaminated · Jan 12, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > RIGHT W/W EXTERNAL STRUCTURE BETWEEN STA 1040 TO 1060 INTERCOSTAL WITH DELAMINATION DOT 07-060 REVIEWED - [SDR IPXA2026012356310](https://openairdocs.org/sdr/IPXA2026012356310.md): Tee Fitting · corroded · Jan 11, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > LOWER FUSELAGE RT SIDE STA 1200 T-FITTING EXFOLIATED. INSTALLED A NEW T-FITTING IAW SRM 51-40-02-0G. - [SDR IPXA2026012353616](https://openairdocs.org/sdr/IPXA2026012353616.md): Tee Angle · corroded · Jan 11, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > EXTERNAL FUSELAGE LT W/W BETWEEN STA 1060 TO 1080 INTERCOSTAL HAS CORROSION. INSTALLED NEW T-CHORD / INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0. - [SDR IPXA2026012314754](https://openairdocs.org/sdr/IPXA2026012314754.md): Tee Fitting · corroded · Jan 8, 2026 · N410UP · Boeing 75724APF · Aerodynamic Fairings > RT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-FITTING EXFOLIATED. INSTALLED NEW T-FITTING 1 EA RT WING TO BODY FAIRING PANEL 196CR BTW STA 1180 AND 1200 IAW B757-200 SRM 51-40-02. INSTALLED FRAME SECTION FROM STA 1140 -1200 I.A.W. B7 - [SDR IPXA2026012314576](https://openairdocs.org/sdr/IPXA2026012314576.md): Tee Fitting · corroded · Jan 8, 2026 · N410UP · Boeing 75724APF · Fuselage Main, Structure > RIGHT RAM AIR EXHAUST, BTWN BS 1040 AND 1060, OTBD T-FITTING CORRODED. INSTALLED NEW T-CHORD/ INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0 - [SDR IPXA2026012734754](https://openairdocs.org/sdr/IPXA2026012734754.md): Tee Fitting · corroded · Jan 8, 2026 · N410UP · Boeing 75724APF · Aerodynamic Fairings > RIGHT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-CHORD EXFOLIATED. DOT 90-018 REVIEWED - [SDR IPXA2026012174949](https://openairdocs.org/sdr/IPXA2026012174949.md): Skin · cracked · Jan 6, 2026 · N410UP · Boeing 75724APF · Wing, Plate/Skin > LEFT WING FIXED L/E COMPOSITE SKIN WAS CRACKED, 5 INCHES IN LENGTH, UNDER SLAT NR 2. ACCOMPLISHED THE PERMANENT REPAIR IAW EO 96311-REQ1 & EA 757-5741-27-A4276 REV -. - [SDR IPXA2026011271869](https://openairdocs.org/sdr/IPXA2026011271869.md): Angle · corroded · Jan 6, 2026 · N410UP · Boeing 75724APF · Fuselage Main, Structure > APU INLET DOOR UPPER ANGLE FROM BS 1787.45 - 1825.00, S3R WAS CORRODED. INSTALLED A NEW UPPER ANGLE IAW SRM 51-40-02-0G-0. - [SDR IPXA2026012174971](https://openairdocs.org/sdr/IPXA2026012174971.md): Skin · cracked · Jan 6, 2026 · N410UP · Boeing 75724APF · Leading Edge Devices > RIGHT WING FIXED L/E COMPOSITE SKIN WAS CRACKED UNDER SLAT NR 7, ON OTBD END. WORK ACCOMPLISHED IAW EA 757-5741-27-4268, REV-, PRELIM 1 EO-96233 REQ 1, AND EA 757-5741-27-A4268 REV-. - [SDR IPXA2026011572116](https://openairdocs.org/sdr/IPXA2026011572116.md): Strap · corroded · Jan 6, 2026 · N410UP · Boeing 75724APF · Fuselage Main, Structure > MAJOR REPAIR. APU INLET DOOR AFT STRAP AT BS 1825.00 FROM S3 - 6R WAS CORROED (EXISTING REPAIR FOUND IN THE AREA) INSTALLED NEW FILLER MIDDLE STRAP IAW SRM 51-40-02-0G-0. - [SDR IPXA2026011272419](https://openairdocs.org/sdr/IPXA2026011272419.md): Angle · corroded · Jan 6, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > APU INLET DOOR LOWER CORNER ANGLE AT STA 1787.45 AT S-6R HAS CORROSION. INSTALLED NEW LOWER CORNER ANGLE I.A.W. B757-200 SRM 51-40-02-0G-0. - [SDR IPXA2026011271946](https://openairdocs.org/sdr/IPXA2026011271946.md): Angle · corroded · Jan 6, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825.00 S-6R HAS CORROSION. INSTALLED NEW LOWER ANGLE IAW SRM 51-40-02-0G-0. REVIEWED - [SDR IPXA2026012644037](https://openairdocs.org/sdr/IPXA2026012644037.md): Skin · delaminated · Jan 4, 2026 · N410UP · Boeing 75724APF · APU Cowling/Containment > MAJOR REPAIR. APU COMPARTMENT LT SIDEWALL INNER SKIN WAS DELAMINATED APPROX 8"X10" AREA BETWEEN BS 1918 AND 1941 17 INCHES ABOVE THE LWR FRAME. VERIFIED COMPLETION OF REPAIR IS A CATEGORY A REPAIR. NO FURTHER ACTION REQUIRED. - [SDR IPXA2026012643865](https://openairdocs.org/sdr/IPXA2026012643865.md): Skin · dented · Jan 4, 2026 · N410UP · Boeing 75724APF · APU Cowling/Containment > MAJOR REPAIR, APU COMPARTMENT RT SIDEWALL INNER SKIN HAS DENTED & CRACKED BETWEEN BS 1918 AND 1941 APPROX 26 INCHES ABOVE THE LWR FRAME. VERIFIED REPAIR IS A CATEGORY A REPAIR. NO FUTHER ACTION IS REQUIRED. - [SDR IPXA2026012843933](https://openairdocs.org/sdr/IPXA2026012843933.md): Skin · delaminated · Jan 4, 2026 · N410UP · Boeing 75724APF · APU Cowling/Containment > MAJOR REPAIR, COMPOSITE APU COMPARTMENT: APU COMPARTMENT INNER SKIN INCLUDING OUTER SKIN HAS DELAMINATION BETWEEN BS 1918 & 1941 17 INCHES ABOVE THE LWR FRAME APPROX. 8"X10" AREA. VERIFIED REPAIR IS A CATEGORY A REPAIR, NO FUTHER ACTION REQUIRED. - [SDR IPXA2026011240212](https://openairdocs.org/sdr/IPXA2026011240212.md): Strap · corroded · Jan 3, 2026 · N410UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors > BS 1787.45, CORROSION ON THE UNDERSIDE OF THE APU DOOR SURROUND STRUCTURE FROM S3 - 6R. INSTALLED A NEW FWD STRAP IAW SRM 51-40-02-0G-0. - [SDR IPXA2026011740349](https://openairdocs.org/sdr/IPXA2026011740349.md): Tee Fitting · corroded · Jan 3, 2026 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > CORROSION FOUND AT WTB T-FITTING FROM BS 1180 TO 1240 RBL 63 INSTALLED NEW T-FITTING IAW SRM 51-40-02-0G. - [SDR IPXA2024100790244](https://openairdocs.org/sdr/IPXA2024100790244.md): Floorboard · corroded · Aug 9, 2024 · N410UP · Boeing 75724APF · Fuselage Floor Panel > MCD RT SIDE #2 PALLET LOCATION FLOOR BOARD CORRODED/MISSING SEALANT BETWEEN NEXT PANEL REMOVED FLOORBOARD FOR RII AND INSTALLED REF AMM 53-01-01-424-023. - [SDR IPXA2024081291000](https://openairdocs.org/sdr/IPXA2024081291000.md): Floorboard · damaged · Aug 9, 2024 · N410UP · Boeing 75724APF · Fuselage Floor Panel > MCD FLOOR BOARD DAMAGED - 6TH AFT OF BULKHEAD ( AFT OF MAIN CARGO DOOR) PANEL REMOVED AND ROUTED TO SHEET METAL SHOP REF B757 AMM 53-01-01. VERIFIED MATERIAL USED FOR FABRICATED FLOOR PANEL ON MAIN CARGO DECK. CONFIRMED INSERT INSTALLATION. DONE PER SREO-9692 - [SDR IPXA2024030435420](https://openairdocs.org/sdr/IPXA2024030435420.md): Metering Valve · faulted · Mar 1, 2024 · N410UP · Boeing 75724APF · Landing Gear Brake System > DURING PREFLIGHT BRAKE PRESSURE ACCUMULATOR LOSES PRESSURE FROM 3000 PSI TO 2500 PSI IN 1 MINUTE. POSSIBLE PRESSURE LEAK IN ACCUMULATOR. PRESSURIZED TO RESET STAB TRIM & SET PARKING BRAKE. CAPPED RETURN LINES TO PARKING BRAKE VALVE, LEAK DOWN STILL OUT OF LIMI - [SDR IPXA2024012989730](https://openairdocs.org/sdr/IPXA2024012989730.md): Fairing · cracked · Jan 11, 2024 · N410UP · Boeing 75724APF · Nacelle/Pylon, Main Frame > FAULT: L/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 INSTALLED NEW CHORD IAW SRM 51-40-02. - [SDR IPXA2024011289730](https://openairdocs.org/sdr/IPXA2024011289730.md): Unknown · unknown · Jan 11, 2024 · N410UP · Boeing 75724APF · Nacelle/Pylon, Main Frame > L/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 APPROVED - [SDR IPXA2024012945677](https://openairdocs.org/sdr/IPXA2024012945677.md): Latch · worn · Jan 9, 2024 · N410UP · Boeing 75724APF · Passenger/Crew Doors > *** SUPPLEMENTAL SDR *** FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT47-07 TREATED AND PRIMED LATCH CAM IAW SRM 51-20-01 STEP 5 - [SDR IPXA2024012943096](https://openairdocs.org/sdr/IPXA2024012943096.md): Skin · damaged · Jan 9, 2024 · N410UP · Boeing 75724APF · Leading Edge Devices > *** SUPPLEMENTAL SDR *** FAULT: # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT REPAIRED SEALANT IAW SOPM 20-50-19 STEP 20. - [SDR IPXA2024012935491](https://openairdocs.org/sdr/IPXA2024012935491.md): Structure · delaminated · Jan 9, 2024 · N410UP · Boeing 75724APF · Elevator Structure > FAULT: L/H ELEVATOR O/B T/E TIP HAS DELAMINATED. DOT 33-002 FABRICATED SHIMS PER BMS7-335 STEP 5.2 ON MATERIAL 2024T30.040 BATCH#0003813619, INSTALL SHIM PER SOPM 20-50-20 FIG 2. APPLIED TOP COAT ON AREA IAW B757 AMM 51-21-15-370-801A PAINT MIXED IN CUP P/N CC - [SDR IPXA2024012435373](https://openairdocs.org/sdr/IPXA2024012435373.md): Rod End · corroded · Jan 9, 2024 · N410UP · Boeing 75724APF · Horizontal Stabilizer Structure > FAULT: L/H HORIZONTAL STAB O/B POGO STICK ROD END HAS CORROSION. DOT 33-000. REMOVED AND INSTALLED LH HORIZONTAL STAB O/B POGO STICK ROD END IAW AMM 27-31-05-024-001 AND 27-31-05-424-067, VERIFIED. REVIEWED - [SDR IPXA2024011745677](https://openairdocs.org/sdr/IPXA2024011745677.md): Latch · worn · Jan 9, 2024 · N410UP · Boeing 75724APF · Passenger/Crew Doors > FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT47-07 CREW DOOR UPPER LATCH CAM WE WILL INSTALL ON N/R 6100412629; T3F18E003R8UZ - [SDR IPXA2024011043096](https://openairdocs.org/sdr/IPXA2024011043096.md): Unknown · unknown · Jan 9, 2024 · N410UP · Boeing 75724APF · Wing, Plate/Skin > *SDR FILED OPEN* FAULT: # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT APPROVED - [SDR IPXA2024010935491](https://openairdocs.org/sdr/IPXA2024010935491.md): Unknown · unknown · Jan 9, 2024 · N410UP · Boeing 75724APF · Elevator Structure > *SDR FILED OPEN* FAULT: L/H ELEVATOR O/B T/E TIP HAS DELAMINATED. DOT 33-002 - [SDR IPXA2024012928961](https://openairdocs.org/sdr/IPXA2024012928961.md): Exhaust Cone · gouged · Jan 8, 2024 · N410UP · Boeing 75724APF · Engine Collector/Tailpipe/Nozzle > FAULT#2 ENG EXHAUST CONE LOWER OUTBD AREA BETWEEN 4 AND 5'0' CLOCK POSITION HAS A GOUGE DOT 47-04 AFTER REVEIWING DAMAGED AREA THE DISCREPANCY WAS FOUND TO BE A DENT. THE DENT MEASURED AT 1.7 INCHES WIDE AND WAS.014 DEPTH AT DEEPEST LOCATION, EQUALING 121.42 - [SDR IPXA2024010928961](https://openairdocs.org/sdr/IPXA2024010928961.md): Unknown · unknown · Jan 8, 2024 · N410UP · Boeing 75724APF · Engine Collector/Tailpipe/Nozzle > *SDR FILED OPEN* FAULT#2 ENG EXHAUST CONE LOWER OUTBD AREA BETWEEN 4 AND 5'0' CLOCK POSITION HAS A GOUGE DOT 47-04 APPROVED - [SDR IPXA2024012908224](https://openairdocs.org/sdr/IPXA2024012908224.md): Skin · damaged · Jan 6, 2024 · N410UP · Boeing 75724APF · Fuselage Main, Plate/Skin > *** SUPPLEMENTAL SDR *** FAULT- TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 AFTER FURTHER EVALUATION NO DAMAGE WAS FOUND. ONLY TOP COAT WAS AFFECTED. CLEANED AREA PER SOPM 20-30-03. NO MATERIAL LOST. VERIFIED WITH TR T17807 + TR8 - [SDR IPXA2024010808224](https://openairdocs.org/sdr/IPXA2024010808224.md): Unknown · unknown · Jan 6, 2024 · N410UP · Boeing 75724APF · Fuselage Main, Plate/Skin > OPEN. TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 APPROVED - [SDR IPXA2023122288826](https://openairdocs.org/sdr/IPXA2023122288826.md): Oil System · abnormal · Dec 21, 2023 · N410UP · Boeing 75724APF · Powerplant System > *** DIVERSION *** *** IFSD *** IN CRUISE, RT OIL PRESSURE 0, OIL PRESS RED (APPROX 45) QRH PROCEDURE FOLLOWED, ENG SHUTDOWN PERFORMED WINDMILL INSPECTION, REF T31F8E003LYY1. PER FINDINGS, REMOVED AND REPLACED #2 ENG REF T31F18E003MO3S AND T3F18E003MO3T - [SDR IPXA2023122288097](https://openairdocs.org/sdr/IPXA2023122288097.md): Engine · shutdown · Dec 21, 2023 · N410UP · Boeing 75724APF · Engine (Turbine/Turboprop) > *** SUPPLEMENTAL SDR *** DUE TO RH ENGINE SHUTDOWN IN FLIGHT ENGINE WINDMILLING INSPECTION IAW AMM 72-00-216-499-P00 REQUIRED NO. 2 ENGINE: REMOVE ESN 717921 (T3F18E003M03S), AND INSTALL ESN 717903 (T3F18E003M03T). DUE TO FINDINGS ON ENGINE WINDMILLING INSPECT - [SDR IPXA2023122188097](https://openairdocs.org/sdr/IPXA2023122188097.md): Unknown · unknown · Dec 21, 2023 · N410UP · Boeing 75724APF · Engine (Turbine/Turboprop) > *** DIVERSION *** *** IFSD *** DUE TO RH ENGINE SHUTDOWN IN FLIGHT ENGINE WINDMILLING INSPECTION IAW AMM 72-00-216-499-P00 REQUIRED DUE TO FINDINGS ON ENGINE WINDMILLING INSPECTION IAW AMM 72-00-216-499-P00 7(D)5. ENGINE NEEDS TO GET REMOVED FOR INSPECTION OF - [SDR IPXA2022112388381](https://openairdocs.org/sdr/IPXA2022112388381.md): A/C Pack · noisy · Nov 23, 2022 · N410UP · Boeing 75724APF · Cabin Cooling System > AT HIGH POWER SETTINGS (I.E TAKE OFF ROLL) RIGHT PACK MAKES A VERY LOUD HIGH PITCH NOISE. DEFERRED RT PACK SYS PER MEL 21-51-1. DMP C/W. PLACARD INSTALLED. THIS CREATES M796076.R/R R/H RE-HEATER ASSY REF AMM 21-51-07-404-014. LEAK CHECK GOOD. ORIG SUB DATE: - [SDR IPXA2022022079195](https://openairdocs.org/sdr/IPXA2022022079195.md): Frame · none · Jan 31, 2022 · N410UP · Boeing 75724APF · Fuselage Miscellaneous Structure > INSPECTION TYPE:C** SUPPLEMENTAL SDR**PREVIOUS REPAIR AT FRAME STA 1240, FROM S-25R TO S-28RREPAIRED PER UPS EO B757-24237-C AND VT MAE EA 757-5360-A2812 REV- - [SDR IPXA2022022079197](https://openairdocs.org/sdr/IPXA2022022079197.md): Frame · none · Jan 31, 2022 · N410UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:CPREVIOUS REPAIR AT FR STA 1300, BETWEEN STR 23L AND 28LREPAIRED PER UPS EO B757-5310-24249-C AND VT MAE EA 757-5360-27-A2816 REV- - [SDR IPXA2022022079196](https://openairdocs.org/sdr/IPXA2022022079196.md): Frame · none · Jan 31, 2022 · N410UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:CPREVIOUS REPAIR AT FRAME STA 1280, FROM S-23R TO S-26RREPAIRED PER UPS EO B757-5310-82771-A AND VT MAE EA 757-5360-A2813 REV- - [SDR IPXA2020112562770](https://openairdocs.org/sdr/IPXA2020112562770.md): Warning Message · illuminated · Nov 23, 2020 · N410UP · Boeing 75724APF · Pitot/Static Anti-Ice System > INSPECTION TYPE: N/A ATB. TAT PROBE EICAS ON TAKEOFF, AIR TURN BACK. REMOVED AND REPLACED TAT PROBE, IAW MM 34-12-02-024-033. OPERATIONS CHECKS GOOD. IPC 34-12-02-05 ITEM 005. - [SDR IPXA2020022655502](https://openairdocs.org/sdr/IPXA2020022655502.md): Floor Panel · damaged · Feb 25, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:C1FLOOR PANEL 211XAF IS DAMAGEDFABRICATED NEW PANEL 211XAF IAW SREO B757 5320-9692-K - [SDR IPXA2020022645440](https://openairdocs.org/sdr/IPXA2020022645440.md): Floor Panel · damaged · Feb 24, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:C1MAIN CARGO COMPARTMENT, FLOOR PANEL 251XRF DAMAGEDFABBED PANEL 146N5361-29 FROM 5024N400001SS-G, BATCH# 3525521 PER SREO B757-5320-9692-K - [SDR IPXA2020022645435](https://openairdocs.org/sdr/IPXA2020022645435.md): Floor Panel · damaged · Feb 24, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:C1MAIN CARGO COMPARTMENT, FLOOR PANEL 252XUF DAMAGEDFABBED PANEL 146N5361-45 FROM 5024N400001SS-G, BATCH 3525521 PER SREO B757-5320-9692-K - [SDR IPXA2020022152333](https://openairdocs.org/sdr/IPXA2020022152333.md): Floor Panel · damaged · Feb 21, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 252XRF DAMAGEDFABBED PANEL 146N5361-18 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K - [SDR IPXA2020022152332](https://openairdocs.org/sdr/IPXA2020022152332.md): Floor Panel · damaged · Feb 21, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 114N5410-6 DAMAGEDFABBED PANEL 114N5410-6 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K - [SDR IPXA2020022152331](https://openairdocs.org/sdr/IPXA2020022152331.md): Floor Panel · damaged · Feb 21, 2020 · N410UP · Boeing 75724APF · Fuselage Floor Panel > INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 114N5410-5 DAMAGEDFABBED PANEL 114N5410-5 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K Next page: https://openairdocs.org/aircraft/N410UP/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 = 'N410UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N410UP/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.