# Service difficulty reports: N445UP A list on [N445UP](https://openairdocs.org/aircraft/N445UP.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 · 213 reports - [SDR IPXA2026011477249](https://openairdocs.org/sdr/IPXA2026011477249.md): Flap System · faulted · Jan 13, 2026 · N445UP · Boeing 75724APF · Trailing Edge Flap Control System > FLAP/SLAT ELEC STATUS MESSAGE TRAILING EDGE FLAPS DISAGREE EICAS RAN CHECK LIST LANDED FLAP 20*. ACCOMPLISHED ADJUSTMENT OF FLAP SYSTEM IAW AMM 27-51-00-825-007.REMOVED AND REPLACED FLAP POSITION INDICATOR IAW AMM 27-58-02-004-001 DUE TO A FAULTY (L) NEEDLE - [SDR IPXA2026011377249](https://openairdocs.org/sdr/IPXA2026011377249.md): Warning Message · illuminated · Jan 13, 2026 · N445UP · Boeing 75724APF · Leading Edge Slat Control System > EMD, FLAP/SLAT ELEC STATUS MESSAGE TRAILING EDGE FLAPS DISAGREE EICAS RAN CHECK LIST LANDED FLAP 20* - [SDR IPXA2026010909847](https://openairdocs.org/sdr/IPXA2026010909847.md): Flap System · faulted · Jan 8, 2026 · N445UP · Boeing 75724APF · Trailing Edge Flap Control System > DIVERSION, EMERGENCY DECLARED, TE FLAP DISAGREE EICAS ON APPROACH PERFORMED CHECKLIST AND UNABLE TO EXTEND FLAPS TO EVEN 1 DEGREE. PERFORMED FSEU BITE FIM 27-51 FT 805. CODE 305 / 328 DISPLAYED ON FAULT HISTORY LAG 0. PER FT 805 FIG 104B, CONTINUE T/S PER FI - [SDR IPXA2025122202811](https://openairdocs.org/sdr/IPXA2025122202811.md): Fuel Sys · out of balance · Dec 12, 2025 · N445UP · Boeing 75724APF · Fuel Transfer Valve > FUEL CONFIG EICAS DURING APPROACH. AFTER USING CTR TANK FUEL FLOWS WERE EQUAL. LEFT TANK SHOWED 2000 LESS THAN RIGHT. WITH AP ON AILERON SHOWED MORE THAN 1 UNIT TO THE LEFT. AIRCRAFT ROLLED TO RIGHT WHEN AP WAS OFF. REPLACED VALVE 2 EA. REF. AMM 28-21-05-004 - [SDR IPXA2025121202811](https://openairdocs.org/sdr/IPXA2025121202811.md): Fuel Sys · faulted · Dec 12, 2025 · N445UP · Boeing 75724APF · Aircraft Fuel Distribution System > FUEL CONFIG EICASDURINGAPPROACH AFTER USING CTRTANK FUEL FLOWS WERE EQUAL. LEFT TANK SHOWED 2000 LESS THAN RIGHT.WITH AP ON AILERON SHOWEDMORE THAN1UNIT TO THELEFT. AIRCRAFT ROLLED TO RIGHT WHEN AP WAS OFF DEFERRED AMM 28-21-00-702-001 PAR B,2 - [SDR IPXA2025052917198](https://openairdocs.org/sdr/IPXA2025052917198.md): Bracket · corroded · May 16, 2025 · N445UP · Boeing 75724APF · Aerodynamic Fairings > R/H WING TO BODY PANEL 194CR LOWER NUTPLATE BRACKET HAS CORROSION. 33-032. INSTALLED PARTS R/H WING TO BODY IAW B757-200 SRM 51-70-12-0G-0. VERIFIED INSTALLED PARTS ON R/H WING TO BODY PANEL 194CR STRUCTURE. - [SDR IPXA2025052717502](https://openairdocs.org/sdr/IPXA2025052717502.md): Channel · cracked · May 16, 2025 · N445UP · Boeing 75724APF · Fuselage Miscellaneous Structure > FAULT-STR-Z143-LH MLG W/W AFT BULKHEAD AT STA 1180 LBL 11 CHANNEL CRACKED-DOT 139-20, MR-139. INSTALLED NEW CHANNEL ON LH MLG W/W AFT BULKHEAD AT STA 1180 LBL 11 IAW B757-200 SRM 51-40-02-0G-0 MATERIAL USED: P/N:04-001-0109 BTCH:0004371371 P/N:BACB30NX6K4 BTC - [SDR IPXA2025052803409](https://openairdocs.org/sdr/IPXA2025052803409.md): Support · corroded · May 15, 2025 · N445UP · Boeing 75724APF · Aerodynamic Fairings > WING TO BODY FAIRING SUPPORT STRUCTURE PANEL AR STA1040 HAS CORROSION. INSTALLED NEW SUPPORT STRUCTURE PANEL 195AR STA1040. IAW.51-40-02. - [SDR IPXA2025053087153](https://openairdocs.org/sdr/IPXA2025053087153.md): Frame · dented · May 14, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > AFT CARGO COMPARTMENT, FRAME STA 1280, BETWEEN STR 23 TO STR 24 L/H HAS A DENT. INSTALLED FRAME REPAIR AT AFT CARGO COMPARTMENT, FRAME STA 1280, BETWEEN STR 23 TO STR 24 L/H IAW 51-40-02-0G. - [SDR IPXA2025052891223](https://openairdocs.org/sdr/IPXA2025052891223.md): Floorbeam · corroded · May 14, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Floor Beam > FAULT Z-200 STR: FLOOR BEAM STA 1200 BETWEEN LBL 60.0 TO RBL 45 HAS CORROSION. INSTALLED FLOOR PANELS 241XMF,241XLF,241XKF,242XKF,242XLF,242XMF I.A.W AMM53-01-01-424-023. ACCOMPLISH REPAIR PER EO-93994-REQ1 AND VT-MAE EA 757-5360-27-A3971, REV. -, PRIOR TO F - [SDR IPXA2025052986923](https://openairdocs.org/sdr/IPXA2025052986923.md): Frame · dented · May 14, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > MAJOR REPAIR, AFT CARGO COMPARTMENT, FRAME STA 1480, STR 26 L/H HAS A DENT LOCATED AND DRILLED NEW FRAME IAW B757-200PF, SRM 51-40-05, SRM REV 122 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R. - [SDR IPXA2025052985498](https://openairdocs.org/sdr/IPXA2025052985498.md): Frame · dented · May 14, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > MAJOR REPAIR, AFT CARGO COMPARTMENT, FRAME STA 1320, STR 26 L/H HAS A DENT INSTALLED FRAME REPAIR AFT CARGO COMPARTMENT, FRAME STA 1320, STR 26 L/H IAW B757-200PF SRM 53-00-07-2R-5. PERFORMED COLD WORK AT FRAME REPAR IAW B757-200PF SRM 51-40-09. - [SDR IPXA2025053185240](https://openairdocs.org/sdr/IPXA2025053185240.md): Frame · dented · May 14, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > AFT CARGO COMPARTMENT, FRAME STA 1260 BETWEEN STR 25 TO STR 26 L/H HAS A DENT. INSTALLED FRAME REPAIR (01EA) AND CLIPS (02EA) ON AFT CARGO COMPARTMENT, FRAME STA 1260 BETWEEN STR 25 TO 26 L/H, IAW B757-200PF SRM 53-00-07-2R-6, REPAIR 6 AND SRM 51-40-02. PERFO - [SDR IPXA2025061067748](https://openairdocs.org/sdr/IPXA2025061067748.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > FWD CARGO COMPARTMENT FRAME AT STA 680 BETWEEN STR 22 TO STR 24 R/H HAS A DENT. INSTALLED FRAME REPAIR AT FWD CARGO COMPARTMENT FRAME AT STA 680 BETWEEN STR 22 TO STR 24 R/H IAW B757-200PF SRM 53-00-07-2R-5. - [SDR IPXA2025061068154](https://openairdocs.org/sdr/IPXA2025061068154.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > FWD CARGO COMPARTMENT FRAME AT STA 820 BETWEEN STR 23 TO STR 25 R/H HAS A DENT. INSTALLED FRAME REPAIR AT FWD CARGO COMPARTMENT FRAME AT STA 820 BETWEEN STR 23 TO STR 25 R/H IAW B757-200PF SRM 53-00-07-2R-5. - [SDR IPXA2025061068228](https://openairdocs.org/sdr/IPXA2025061068228.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > FWD CARGO COMPARTMENT FRAME AT STA 700 BETWEEN STR 22 TO STR 24 L/H HAS A DENT. VERIFIED INSTALLED REPAIR FRAME AT FWD CARGO COMPARTMENT FRAME AT STA 700 BETWEEN STR 22 TO STR 24 R/H. - [SDR IPXA2025052967941](https://openairdocs.org/sdr/IPXA2025052967941.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > MAJOR REPAIR, FWD CARGO COMPARTMENT FRAME AT STA 780 BETWEEN STR 22 TO STR 25 R/H HAS DOUBLE DENTS INSTALLED FRAME REPAIR AT FWD CARGO COMPARTMENT FRAME AT STA 780 BETWEEN STR 22 TO STR 25 R/H IAW B757-200PF SRM 53-00-07-2R-5. PERFORMED COLD WORK AT FRAME REPA - [SDR IPXA2025052859121](https://openairdocs.org/sdr/IPXA2025052859121.md): Strap · corroded · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Miscellaneous Structure > MAJOR REPAIR, APU INLET DOOR AFT STRAP STA 1825 HAS CORROSION INSTALLED ALL REPAIR PARTS (3EA STRAPS AND 2EA FILLERS) IAW B757-200PF SRM 51-40-02-0G-0 FOR ACCOMPLISH TO SRM 53-80-15-2R-1 DETAIL II. - [SDR IPXA202506047748](https://openairdocs.org/sdr/IPXA202506047748.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > STR FWD CARGO COMPARTMENT FRAME AT STA 680 BETWEEN STR 22 TO STR 24 R/H HAS A DENT REVIEWED - [SDR IPXA2025060368154](https://openairdocs.org/sdr/IPXA2025060368154.md): Stringer · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer > STR FWD CARGO COMPARTMENT FRAME AT STA 820 BETWEEN STR 23 TO STR 25 R/H HAS A DENT. - [SDR IPXA2025060368228](https://openairdocs.org/sdr/IPXA2025060368228.md): Frame · dented · May 13, 2025 · N445UP · Boeing 75724APF · Fuselage Main, Frame > STR FWD CARGO COMPARTMENT FRAME AT STA 700 BETWEEN STR 22 TO STR 24 L/H HAS A DENT. - [SDR IPXA2025053137890](https://openairdocs.org/sdr/IPXA2025053137890.md): Skin · corroded · May 12, 2025 · N445UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin > MAJOR REPAIR NR 2 ENGINE PYLON OUTBD INTERNAL SKIN, AFT OF THE MID SPAR FITTING HAS EXFOLIATION CORROSION. DOT 8-001. INSTALLED FITTING AFT HINGE REMOVED ON STEP 4 IAW SRM 51-40-02. AND REQUEST OK TO REINSTALL UPPER SILL ANGLE REMOVED ON STEP 27 FOR FOM. INSTA - [SDR IPXA2024050611839](https://openairdocs.org/sdr/IPXA2024050611839.md): Flap System · faulted · May 4, 2024 · N445UP · Boeing 75724APF · Trailing Flap Position Indicating System > **EMERGENCY DECLARED** TE FLAP DISAGREE. FLAP INDICATION BETWEEN 20 AND 25. REVIEWED FAULT HISTORY W/ NO DEFECTS NOTED IN THE LAST 3 MONTHS. TESTED ALL 3 FLAP FSEU'S, NO FAULTS NOTED REF AMM 27-51-01-722-005. SUSPECT STICKY FLAP/SLAT POSITION IND. R&R FLAP/SLA - [SDR IPXA2023070577973](https://openairdocs.org/sdr/IPXA2023070577973.md): Cusp Web · corroded · Jun 8, 2023 · N445UP · Boeing 75724APF · Fuselage Miscellaneous Structure > FAULT: THE R/H CUSP WEB AT STA 1674 HAS EXFOLIATING CORROSION TREATED AND PRIMED NEW RETAINER IAW SRM 51-20-01. INSTALLED NEW RETAINER IAW SRM 51-40-02-0G PARAGRAPH 4. VERIFIED NEW RETAINER INSTALLED JOB COMPLETE. REVIEWED - [SDR IPXA2023070548429](https://openairdocs.org/sdr/IPXA2023070548429.md): Seat Track · corroded · Jun 6, 2023 · N445UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings > FAULT: MCD AT STA 290 BL 0, SEAT TRACK SHOWS SIGNS OF CORROSION INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G PARAGRAPH 4 AND 7. INSTALLATION OF FLOOR PANEL 211XAF TO BE ACCOMPLISHED ON THE ACCESS BOOK ZONE 200. INSTALLED SIDE PANEL 417UB240-9 I.A.W. SRM 51-40- - [SDR IPXA2023070571657](https://openairdocs.org/sdr/IPXA2023070571657.md): Seat Track · corroded · May 31, 2023 · N445UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings > FAULT: R/H O/B SEAT TRACK HAS CORROSION INSTALLED 5 E/A NUT PLATES AT NEW SEAT TRACK I.A.W. SRM 51-40-02-0G. FINAL INSPED NEW SEAT TRACK I.A.W. SRM 51-40-02-0G. REVIEWED - [SDR IPXA2023070565771](https://openairdocs.org/sdr/IPXA2023070565771.md): Door Frame · corroded · May 31, 2023 · N445UP · Boeing 75724APF · Doors > FAULT: LOWER DOOR FRAME ON THE FWD CARGO DOOR SHOWS SIGNS OF EXFOLIATED CORROSION. INSTALLED THE NEW REPAIR T-CHORDS AND LOWER ANGLES TO THE LOWER AREA OF THE #1 CARGO DOOR IAW SRM 51-40-02-0G. RESTORED THE SELF LEVELING COMPOUND ON THE INTERNAL AREA OF THE #1 - [SDR IPXA2023070579713](https://openairdocs.org/sdr/IPXA2023070579713.md): Frame · unknown · May 25, 2023 · N445UP · Boeing 75724APF · Standard Practices/Structures > *MAJOR REPAIR* FAULT: PREVIOUS REPAIR AT FRAME 1300 L/H ALL WORK ACCOMPLISHED PER UPS EO, EO-34655-REQ3 AND VT MAE EA, 757-5360-27-A3240. REVIEWED. - [SDR IPXA2023070579587](https://openairdocs.org/sdr/IPXA2023070579587.md): Frame · unknown · May 25, 2023 · N445UP · Boeing 75724APF · Standard Practices/Structures > *MAJOR REPAIR* FAULT: PREVIOUS REPAIR AT 1320 ACCOMPLISHED WORK PER UPS EO: EO-86206-REG1 AND VTMAE EA 757-5360-27-A3241. REVIEWED. - [SDR IPXA2023070379633](https://openairdocs.org/sdr/IPXA2023070379633.md): Frame · unknown · May 25, 2023 · N445UP · Boeing 75724APF · Standard Practices/Structures > FAULT: PREVIOUS REPAIR AT FRAME 1280 VERIFIED ALL WORK ACCOMPOLISHED PER UPS E.O.-44339-REQ3 AND VTMAE E.A. 757-5360-27-A3239 REV. JOB COMPLETED. - [SDR IPXA2023061479633](https://openairdocs.org/sdr/IPXA2023061479633.md): Unknown · unknown · May 25, 2023 · N445UP · Boeing 75724APF · Standard Practices/Structures > *SDR FILED OPEN* FAULT: PREVIOUS REPAIR AT FRAME 1280 VERIFIED ALL WORK ACCOMPOLISHED PER UPS E.O.-44339-REQ3 AND VTMAE E.A. 757-5360-27-A3239 REV. JOB COMPLETED. - [SDR IPXA201912169978](https://openairdocs.org/sdr/IPXA201912169978.md): Stringer · damaged · Nov 21, 2019 · N445UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:757MAIN CABIN LH STRINGER 15 BETWEEN STA660-STA780 HAS BEEN CUTOUT DUE TO IMPACT DAMAGEREPAIR OF MAIN CABIN STRINGER 15L,PN143N3110-376 ACCOMPLISHED PER UPS FINAL EO NO B757-5300-74701-A - [SDR IPXA2019101047761](https://openairdocs.org/sdr/IPXA2019101047761.md): Control System · out of adjust · Oct 10, 2019 · N445UP · Boeing 75724APF · Engine Controls > AFTER STARTING BOTH ENGINES, THE LEFT ENGINE IDLED 10% HIGHER THAN THE RIGHT. LEFT ENG N1 WS 31.7 %. RIGHT N1 WAS 21.7 %, LEFT ENGINE APPEARED TO BE STUCK IN FLIGHT IDLE. ADJUSTED THE LEFT ENGINE CONTROLS IAW AMM 76-11-00-825, AND T/C 5001, STEPS 61-62. OP - [SDR IPXA2019100747640](https://openairdocs.org/sdr/IPXA2019100747640.md): Engine · failed · Oct 3, 2019 · N445UP · Boeing 75724APF · Engine (Turbine/Turboprop) > ON SHORT FINAL, THE LEFT ENGINE FAILED AND APPEARED TO BE SEIZED. RAN ENG FIRE SEVERE DAMAGE CHECK LIST & SHUT IT DOWN. CONTINUED SINGLE ENG LANDING. EMERGENCY DECLARED. LANDED SAFELY ON RWY AFTER WITH NO FURTHER. INCIDENT. NO EMERG EQUIP WAS USED. ACFT TAK - [SDR IPXA2019062843857](https://openairdocs.org/sdr/IPXA2019062843857.md): Support Channel · chafed · Jun 28, 2019 · N445UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors > INSPECTION TYPE:SEG1 AGING INSPECTION RIGHT HAND APU DOOR FIRE LOOP SUPPORT CHANNEL CHAFED AT AFT END. WORKED PER EA# 757-2615-27-A2353 REV - AND EO B757-5240-73037-A. - [SDR IPXA2019062864779](https://openairdocs.org/sdr/IPXA2019062864779.md): Structure · corroded · Jun 26, 2019 · N445UP · Boeing 75724APF · APU Cowling/Containment > INSPECTION TYPE: SEG1, AFT APU TAIL CONE HAS EXFOLIATING CORROSION AT 5:00 POS.REMOVED AND REPLACED BONDED TAILCONE PANEL IAW SRM 51-40-02-OG. - [SDR IPXA2019062643697](https://openairdocs.org/sdr/IPXA2019062643697.md): Panel · delaminated · Jun 24, 2019 · N445UP · Boeing 75724APF · Fuselage Miscellaneous Structure > INSPECTION TYPE: CP13. DAMAGE TO DRY BAY PANEL DELAMINATION. REPAIRED PANEL IAW B757 SRM 51-70-07, PER SRM 57-20-09-2R-1, FIG 201, TABLE 1, 250 DEGREE CURE - [SDR IPXA2019062643696](https://openairdocs.org/sdr/IPXA2019062643696.md): Panel · delaminated · Jun 24, 2019 · N445UP · Boeing 75724APF · Fuselage Miscellaneous Structure > INSPECTION TYPE:CP13, DAMAGE TO DRY BAY PANEL, DELAMINATION. REPAIRED PANEL IAW B757 SRM 51-70-07 PER 57-20-09-2R-1, FIG 201, TABLE 1, 250 DEGREE CURE - [SDR IPXA2019050441731](https://openairdocs.org/sdr/IPXA2019050441731.md): Light · inoperative · May 3, 2019 · N445UP · Boeing 75724APF · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY LIGHT HAS THREE INOP BULBS. RELAMPED EMERGENCY LIGHT THREE BULBS PER AMM 33-51-01-1. - [SDR IPXA2018092864444](https://openairdocs.org/sdr/IPXA2018092864444.md): Circuit Card · unknown · Sep 26, 2018 · N445UP · Boeing 75724APF · Fire Detection > LEFT ENGINE FIRE WARNING DURING SHUTDOWN. MECHANIC CONFIRMED NO FIRE. COMPLETED FIM 26-11-00-815-802, MESSAGE RESET. COMPLETED VISUAL CHECK OF ENGINE, NO EVIDENCE OF OVERHEAT OR FIRE. REPLACED M10224 FIRE, OVERHEAT CARD 1 IAW AMM 26-10-01-401. ALL TESTS N - [SDR IPXA2018080872568](https://openairdocs.org/sdr/IPXA2018080872568.md): Bulb · inoperative · Aug 7, 2018 · N445UP · Boeing 75724APF · Emergency Lighting > EMERGENCY LIGHT HAD TWO INOPERATIVE BULBS. REPLACED THE TWO BULBS IAW AMM 33-51-01. - [SDR IPXA2017090721459](https://openairdocs.org/sdr/IPXA2017090721459.md): Bulb · inoperative · Sep 7, 2017 · N445UP · Boeing 75724APF · Emergency Lighting > EMERGENCY EXIT LIGHT HAS FOUR INOPERATIVE BULBS. REPLACED THE BULBS IAW AMM 33-51-01-2. - [SDR IPXA2017072219610](https://openairdocs.org/sdr/IPXA2017072219610.md): Skin · dented · Jul 12, 2017 · N445UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin > INSPECTION TYPE: C-12, NR 2 PYLON INBD SIDE SKIN PANEL DENTED. REPAIRED IAW EO B757-5430-64999-A - [SDR IPXA2017071619338](https://openairdocs.org/sdr/IPXA2017071619338.md): Structure · corroded · Jul 7, 2017 · N445UP · Boeing 75724APF · Elevator Structure > INSPECTION TYPE: C12, RT ELEVATOR WING TIP T/E WEDGE CORRODED. REPAIRED THE ELEVATOR T/E WEDGE IAW REO-G20920. - [SDR IPXA2017072219611](https://openairdocs.org/sdr/IPXA2017072219611.md): Door Frame · gouged · Jul 2, 2017 · N445UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE: C-12, FWD NOSE AREA DOOR 113AL FWD CUTOUT FRAME GOUGED. REPAIRED IAW EO B757-5310-64993-A - [SDR IPXA2017071319261](https://openairdocs.org/sdr/IPXA2017071319261.md): Structure · corroded · Jul 1, 2017 · N445UP · Boeing 75724APF · Elevator Structure > INSPECTION TYPE: C-12, LEFT ELEVATOR TIP CORRODED, FOUND AFTER REMOVAL. REMOVED CORROSION IAW REO-620929. - [SDR IPXA2017071319246](https://openairdocs.org/sdr/IPXA2017071319246.md): Skin · dented · Jun 30, 2017 · N445UP · Boeing 75724APF · Horizontal Stabilizer, Plate/Skin > INSPECTION TYPE: C-12, LEFT HORIZONATL STAB UPPER SURFACE INBD L/E DENTED. REPAIRED THE DAMAGE IAW 51-70-10, REPAIR 2, AND 51-70-10-2R. - [SDR IPXA2017071319244](https://openairdocs.org/sdr/IPXA2017071319244.md): Skin · dented · Jun 30, 2017 · N445UP · Boeing 75724APF · Horizontal Stabilizer, Plate/Skin > INSPECTION TYPE:C-12, LEFT HORIZONTAL STAB UPPER SURFACE INBD L/E DENTED. REPAIRED THE DAMAGE IAW 51-70-10, REPAIR 2, AND 51-70-10-2R - [SDR IPXA2017072019564](https://openairdocs.org/sdr/IPXA2017072019564.md): Wedge · chafed · Jun 28, 2017 · N445UP · Boeing 75724APF · Leading Edge Devices > INSPECTION TYPE: C-12, LEFT WING NR 3 SLAT LOWER TRAILING EDGE CHAFED. REPAIRED THE DAMAGE IAW EO B757-5750-64988-A AND REO-G20909, REV IR. - [SDR IPXA2016101009200](https://openairdocs.org/sdr/IPXA2016101009200.md): Escape Reel · misinstalled · Oct 9, 2016 · N445UP · Boeing 75724APF · Emergency Equipment > EMERGENCY DESCENT REELS INCORRECTLY INSTALLED. REMOVED AND INSTALLED THE DECENT DEVICES IAW AMM 25-61-02-201. Next page: https://openairdocs.org/aircraft/N445UP/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 = 'N445UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N445UP/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.