# Service difficulty reports: N406UP

A list on [N406UP](https://openairdocs.org/aircraft/N406UP.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 · 285 reports

- [SDR IPXA2026081930589](https://openairdocs.org/sdr/IPXA2026081930589.md): Flap System · warning message · Aug 18, 2026 · N406UP · Boeing 75724APF · Trailing Edge Flap Control System
  > EMD ON CLIMB OUT AT APPROX 3K' WE GOT A LE SLAT DISAGREE EICAS. MAINTAINED 230 KT OR LESS FOR ENTIRE FLIGHT. AFTER QRH PROCEDURE, MSG WENT OUT. PERFORMED BITE PROCEDURE IAW FIM 27-51 FAULT TREE 805 FLAP/SLAT ELECTRONIC UNIT (FSEU) BITE PROCEDURE. FOUND ALTERNA
- [SDR IPXA2026042809227](https://openairdocs.org/sdr/IPXA2026042809227.md): Light · inoperative · Apr 27, 2026 · N406UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHT INOP FOUND THE EMERGENCY LIGHT WERE ON FOR MORE THAN 10 MINS. WHICH REQUIRES 16 HOURS OF CHARGING. R&R EMERGENCY BATTERY PACK REF. AMM. 33-51-07-902-001. OPS CKD NORMAL AT THIS TIME
- [SDR IPXA2025092269443](https://openairdocs.org/sdr/IPXA2025092269443.md): Valve · faulted · Sep 21, 2025 · N406UP · Boeing 75724APF · Turbine Engine Oil System
  > ATB, CLIMB OUT PASSING 24000€™ L OIL TEMP WAS IN THE AMBER RANGE (165°) QRH COMPLETED ACCOMPLISHED AIR TURNBACK. REMOVED AND REPLACED L/H ENG AIR/OIL HEAT EXCHANGER VALVE IAW AMM 79-21-08. OPS AND LEAK CHECKS PERFORMED IAW AMM 71-00-00 NO LEAKS NOTED AND OP
- [SDR IPXA2025091564404](https://openairdocs.org/sdr/IPXA2025091564404.md): Tail Cone · damaged · Aug 20, 2025 · N406UP · Boeing 75724APF · Aerodynamic Fairings
  > MAJOR REPAIR, DAMAGE ON TOP OF TAILCONE AREA BELOW RUDDER ALL STEPS OF EO-94785-REQ2 COMPLETED. THIS DEFERRAL IS NOW CLOSED.
- [SDR IPXA2025011359796](https://openairdocs.org/sdr/IPXA2025011359796.md): Angle · faulted · Jan 7, 2025 · N406UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: REFERANCE FRAME REPAIR T3F18E005ERCC, CORRECTIVE ACTION 6 & 7 SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1500 IN AFT PIT REQUIRES RII AUTHERIZATION. ACCOMPLISH REPAIR PER EA 757-5360-27-A3758, REV- PRIOR TO FURTHER FLIGHT. VERIFIED RECEIVING OF FINAL E
- [SDR IPXA2025011349181](https://openairdocs.org/sdr/IPXA2025011349181.md): Frame · damaged · Jan 6, 2025 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT: Z100 STR OPEN UP FLOOR PANELS, MBA SYSTEM, SIDEWALLS, AND TRANSITION PANEL TO F.O.M FS 1500 FRAME REPAIR AT STR 26R. INSTALLED SIDEWALL PANELS 162BW, 154JW IAW B757-200 SRM 51-40-02 AND INSTALLED LOWER AFT MBA SYSTEM AFT/AFT #8 AND #9, IAW B757-200 AMM
- [SDR IPXA2025010522565](https://openairdocs.org/sdr/IPXA2025010522565.md): Frame · not reported · Jan 4, 2025 · N406UP · Boeing 75724APF · Standard Practices/Structures
  > *SDR FILED OPEN* REF FRAME REPAIR T3F18E005ERBT, CORRECTIVE ACTION 7. - SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1460 RH SIDE IN AFT PIT REQUIRES RII AUTHORIZATION ACCOMPLISH REPAIR PER EA 757-5360-27-A3756, REV- PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2024112840807](https://openairdocs.org/sdr/IPXA2024112840807.md): Tee Angle · corroded · Nov 7, 2024 · N406UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STA 1680 HAS CORROSION ON UPPER AND LOWER SURFACE OF UPPER T-CHORD
- [SDR IPXA2024120260414](https://openairdocs.org/sdr/IPXA2024120260414.md): Tee Angle · damaged · Oct 30, 2024 · N406UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WTB LOWER STRUCTURE, T-CHORD STA 1142, LBL 60 WITH CORROSION. INSTALLED T CHORD AT STA 1142, LBL 60 IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024120232048](https://openairdocs.org/sdr/IPXA2024120232048.md): Seat Track · corroded · Oct 29, 2024 · N406UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SUPPORT STRUCTURE, STA 1195 RBL 24 SEAT TRACK CORRODED. DOT 28-100 REVIEWED
- [SDR IPXA2024103131000](https://openairdocs.org/sdr/IPXA2024103131000.md): Floor Panel · broken · Oct 29, 2024 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > FLOOR PANEL 252XBF BROKEN STA 1200. FABRICATED FLOOR PANEL 252XBF USING MATERIAL P/N:5024N400001SS-G BATCH#:0000096292 I.A.W. SREO-B757-5320-9692-K.
- [SDR IPXA2024120240326](https://openairdocs.org/sdr/IPXA2024120240326.md): Skin · delaminated · Oct 24, 2024 · N406UP · Boeing 75724APF · Trailing Edge Flaps
  > LEFT INBOARD FLAP UPPER OUTBOARD SURFACE IS DELAMINATED IN TWO AREAS. DOT AA014. REVIEWED
- [SDR IPXA2025010310527](https://openairdocs.org/sdr/IPXA2025010310527.md): Floorbeam · corroded · Oct 23, 2024 · N406UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FAULT-STR-100-AGING ACFT INSP.- FLOOR BEAM AT STA 1200, FORWARD SIDE, HAS EXFLOIATION CORROSIN AROUND NUT PLATE.. DOT AA10. ACCOMPLISHED REPAIR PER VT-MAE EA 757-5360-27-A3717, REV- AND EO-91891-REQ1. REVIEWED
- [SDR IPXA2024112010471](https://openairdocs.org/sdr/IPXA2024112010471.md): Frame · dented · Oct 23, 2024 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > FRAME 1500 RIGHT SIDE IN AFT PIT IS DENTED. DOT AA007. REQUIRED SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF, REV 121, 53-00-07-2R-5, TABLE #3 FOR ZONE #1.
- [SDR IPXA2024112510405](https://openairdocs.org/sdr/IPXA2024112510405.md): Frame · dented · Oct 23, 2024 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > FRAME 1460 RIGHT SIDE BETWEEN S-25R AND S-27R, IN AFT PIT IS DENTED. DOT AA006. CORRECTION TO LAST STATEMENT REPAIR PER DETAIL #1
- [SDR IPXA2024120286460](https://openairdocs.org/sdr/IPXA2024120286460.md): Skin · delaminated · Oct 22, 2024 · N406UP · Boeing 75724APF · Landing Gear Doors
  > LEFT MLG STRUT MOUNTED DOOR LOWER AFT TRAILING EDGE IS DELAMINATED. DOT AA002. REVIEWED
- [SDR IPXA2024062459694](https://openairdocs.org/sdr/IPXA2024062459694.md): Unknown · missing · Jun 21, 2024 · N406UP · Boeing 75724APF · Emergency Equipment
  > FO'S EVAS TEST TOOL MISSING. INSTALLED FO'S EVAS TEST TOOL AS REQUIRED
- [SDR IPXA2024050811638](https://openairdocs.org/sdr/IPXA2024050811638.md): Landing Gear · warning message · May 4, 2024 · N406UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY FOUND LEFT SYSTEM RETURN CHECK VALVE P/N BACV10CD13 FOR THE NLG EXTENSION & RETRACTION BYPASSING. R&R BOTH LEFT SYSTEM RET
- [SDR IPXA2024050611638](https://openairdocs.org/sdr/IPXA2024050611638.md): Warning Message · false activation · May 4, 2024 · N406UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > **SDR FILED OPEN** GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY VERIFIED VALVE INPUT ARM ON LANDING GEAR SELECTOR VALVE INSTALLED PROPERLY PER AMM 32-31-02. <BR>CAPPED
- [SDR IPXA2023022191199](https://openairdocs.org/sdr/IPXA2023022191199.md): Door · warning message · Feb 21, 2023 · N406UP · Boeing 75724APF · Passenger/Crew Doors
  > INSPECTION TYPE:N/AON LANDING WE RECIEVED A LEFT FORWARD ENTRY DOOR MESSAGEINSPECTED CREW ENTRY DOOR INDICATION PROXIMITY SWITCH AND FOUND LOWER PORTION OF SHIM TO NOT BE PROPERLY ATTACHED. RE-ATTACHED LOWER PORTION OF SHIM IAW AMM 52-71-00-420-017. OPS CHECK
- [SDR IPXA2022102487481](https://openairdocs.org/sdr/IPXA2022102487481.md): Battery Pack · inoperative · Oct 24, 2022 · N406UP · Boeing 75724APF · Emergency Lighting
  > FLT DECK INTERIOR EMERGENCY LIGHTS OVER ENTRY DOOR INOP. R & R EMERGENCY EXIT LIGHT BATTERY ENTRY DOOR. OPS CK GOOD IAW AMM 33-51-01-012-002, 33-51-01-402-003. OPS CK GOOD. THIS CLEARS M793866
- [SDR IPXA2022101587153](https://openairdocs.org/sdr/IPXA2022101587153.md): Frame · dented · Oct 15, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1360 STRINGER 26L NEEDS AN ALTERNATIVE METHOD TO INSPECT EXISTNG REPAIR PER EO# B757-5310-73926-A APPENDIX A STEP #4FOLLOWED INSPECTION METHOD PER VT MAE EA# 757-5360-27-A3047 REV- UPS EO NO: B757-5310-28011-B
- [SDR IPXA2022101487137](https://openairdocs.org/sdr/IPXA2022101487137.md): Skin · dented · Oct 14, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEG1FUSELAGE SKIN AT STA 434 BETWEEN S23L AND 25L HAS 2 DENTS DENT 1 IS L-1.0" W=1.030" DEPTH=.046" AND DENT 2 L=.632" W=.621" AND DEPTH=.048" MAKING THE SKIN OUT OF LIMITS PER SRM 53-00-01-1A-1 DET 3.REPAIRED SKIN PER EA# B757-5310-27-A3062 PR
- [SDR IPXA2022100886960](https://openairdocs.org/sdr/IPXA2022100886960.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1560 BETWEEN STRINGERS S25R AND S26R HAS TWO DENTS ON THE UPPER FLANGE OF FRAME 1560 NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1560 PER SRM 53-00-07-2R-5 DETAIL 1
- [SDR IPXA2022100886958](https://openairdocs.org/sdr/IPXA2022100886958.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1480 AT STRINGERS 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 1
- [SDR IPXA2022100886957](https://openairdocs.org/sdr/IPXA2022100886957.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1520 BETWEEN STRINGERS 23R AND 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3
- [SDR IPXA2022100886956](https://openairdocs.org/sdr/IPXA2022100886956.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1INCOMING REPAIR ACCOMPLISHED ON FS 1300 BETWEEN STRINGERS S23L AND S26L WAS DONE PER SRM 51-70-11. CUSTOMER REQUEST TO REMOVE REPAIR AND INSTALL REPAIR PER SRM 53-00-07-2R-5 DETAIL 3REPAIRED FRAME 1300 LH PER SRM 53-00-07-2R-5 DETAIL 3 AND
- [SDR IPXA2022100886955](https://openairdocs.org/sdr/IPXA2022100886955.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1460 BETWEEN STRINGERS S25L AND S26L THERE IS A.420" LONG BY.032" DEEP DENT ON THE UPPER FLANGE NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3
- [SDR IPXA2022100886954](https://openairdocs.org/sdr/IPXA2022100886954.md): Frame · dented · Oct 8, 2022 · N406UP · Boeing 75724APF · Fuselage Main, Frame
  > INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1540 1.2" O/B OF STRINGER S26R HAS A.70" LONG BY.45" WIDE BY.50" DEEP GOUGE ON THE UPPER PART OF WEB INTO THE FRAME FLANGEREPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 2
- [SDR IPXA2022090485888](https://openairdocs.org/sdr/IPXA2022090485888.md): Skin · punctured · Sep 4, 2022 · N406UP · Boeing 75724APF · Elevator Structure
  > INSPECTION TYPE:N/ARIGHT ELEVATOR LOWER SKIN PUNCTUREDREPAIRED DAMAGED SKIN IAW EO B757-5520-84504-A
- [SDR IPXA2022051181990](https://openairdocs.org/sdr/IPXA2022051181990.md): None · broken · May 11, 2022 · N406UP · Boeing 757 · Emergency Lighting
  > INSPECTION TYPE:N/AEMERGENCY LIGHT SWITCH GUARD IS BROKENREPLACED SWITCH GROUND. OPS TEST GOOD IAW AMM CH 33-51-08
- [SDR IPXA2021060470179](https://openairdocs.org/sdr/IPXA2021060470179.md): Radome · damaged · Jun 4, 2021 · N406UP · Boeing 75724APF · Aerodynamic Fairings
  > EMERG DECLARED-NO EQUIP USED - LANDING UNEVENTFUL. DURING DESCENT THROUGH APPROX 15000 FT LOUD NOISE AND MULTIPLE EICAS MSG DISPLAYED DUE TO RADOME DAMAGE IAS DISAGREED AND LEFT SIDE AIR DATA SW ENGAGEDREMOVED NOSE RADOME PER MM 53 12 01 902 008 TAF 0558016
- [SDR IPXA2021021265622](https://openairdocs.org/sdr/IPXA2021021265622.md): Stringer · corroded · Feb 12, 2021 · N406UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SEG4AFT CARGO STRINGER 30 STA 1200 HAS CORROSIONREPAIRED IAW 53-00-03-2R-1 REMOVED DAMAGED SECTION SPLICED IN NEW SECTION
- [SDR IPXA2021020365305](https://openairdocs.org/sdr/IPXA2021020365305.md): Floor Panel · damaged · Feb 3, 2021 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XCF DAMAGEDFABBED PANEL 242XCF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2021020365304](https://openairdocs.org/sdr/IPXA2021020365304.md): Floor Panel · damaged · Feb 3, 2021 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT, FLOOR PANEL 242XDF DAMAGEDFABBED PANEL 242XDF FROM 5024M400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2021020365302](https://openairdocs.org/sdr/IPXA2021020365302.md): Floor Panel · damaged · Feb 3, 2021 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XGF DAMAGEDFABBED PANEL 242XGF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2020020551852](https://openairdocs.org/sdr/IPXA2020020551852.md): Frame · bent · Feb 5, 2020 · N406UP · Boeing 75724APF · Fuselage Main, Bulkhead
  > INSPECTION TYPE:SPVCHORD ON RIGHT SIDE PRESSURE BULKHEAD HAS SLIGHT BENT AT STA200 RBL37 WL200REMOVED DAMAGED AREA AND INSTALLED NEW SECTION AND REPAIRED SPLICE
- [SDR IPXA2020020551851](https://openairdocs.org/sdr/IPXA2020020551851.md): Bulkhead Web · dented · Feb 5, 2020 · N406UP · Boeing 75724APF · Fuselage Main, Bulkhead
  > INSPECTION TYPE:SPVFWD PRESSURE BULKHEAD WEB PART #141N2800-164 DENTED BLKHD STA199 RBL30 WL200REMOVED DAMAGE, INSTALLED FILLER AND REPAIR DOUBLER
- [SDR IPXA2019041941214](https://openairdocs.org/sdr/IPXA2019041941214.md): Guard · broken · Apr 19, 2019 · N406UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHT GUARD HAD A BLACK PIECE BREAK OFF. R&R THE SWITCH GUARD IAW SWPM 20-83-11, OPS CHECKED GOOD.
- [SDR IPXA2019041214957](https://openairdocs.org/sdr/IPXA2019041214957.md): Shutoff Valve · failed · Apr 10, 2019 · N406UP · Boeing 75724APF · Compressor Bleed Valve
  > DIVERSION - L ENG BLEED OFF ILLUMINATED AFTER EAI WAS SELECTED ON DURING FLIGHT AT CRUISE FL 300. L ENG WAS FOLLOWED BY R ENG. L AND R PACK OFF. ACCOMPLISHED CHECKLIST AND DESCENDED TO 10,000 AFTER LOSS OF PRESSURE.REPLACED LT ENG HI PRESS SHUTOFF VALVE REF 36
- [SDR IPXA2019022539412](https://openairdocs.org/sdr/IPXA2019022539412.md): Skin · dented · Feb 25, 2019 · N406UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1, DENT STA 520 S-22L DOT18-13FOUND TO BE OUT OF LIMITS DUE TO LOCATION, DENT MUST BE MORE THAN 0.5" REPAIRED PER EA #B757-5330-27-A2331
- [SDR IPXA2019022099223](https://openairdocs.org/sdr/IPXA2019022099223.md): Floor Panel · delaminated · Feb 19, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1MCD FLOOR PNL 252 XTF DELAMINATEDFABBED PNL 252 XTF FROM 5024N400001SS-G, BATCH # 0003384848 PER SREO B757-5320-9692-K
- [SDR IPXA2019022099210](https://openairdocs.org/sdr/IPXA2019022099210.md): Floor Panel · delaminated · Feb 19, 2019 · N406UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1MCD FLOOR PANEL 231XFJ DELAMINATEDFABRICATED NEW FLOOR PANEL 231XJF FROM 5024N400001SS-G, BATCH #3350636 PER SREO B757-5320-9692-K
- [SDR IPXA2019022099209](https://openairdocs.org/sdr/IPXA2019022099209.md): Floor Panel · delaminated · Feb 19, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1MCD FLOOR PNL 232 XJF DELAMINATEDFABRICATED NEW PNL 232XJF FROM 502N400001SS-G BATCH#0002379150 & 0003418355
- [SDR IPXA2019022099208](https://openairdocs.org/sdr/IPXA2019022099208.md): Floor Panel · delaminated · Feb 19, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1MCD FLOOR PNL 221XBF DELAMINATEDFABRICATED NEW PNL FROM 5024N400001SS-G, BATCH#33550626 PER SREO B757-5320-9692 K
- [SDR IPXA2019022099207](https://openairdocs.org/sdr/IPXA2019022099207.md): Floor Panel · delaminated · Feb 19, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1MCD FLOOR PANEL 231XFF DELAMINATEDFABRICATED NEW FLOOR PANEL 231XFF FROM 5024N400001SS-G BATCH# 3350636 PER SREO B757-5320-9692-K
- [SDR IPXA2019021839166](https://openairdocs.org/sdr/IPXA2019021839166.md): Floor Panel · damaged · Feb 18, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1, PANEL 232XCF REQUIRES FAB. FABBED PANEL 232XCF FROM 5024N40000-G BATCH# 33550636 AND STEP CUT PER SREO B757-5320-9692-K.
- [SDR IPXA2019021839164](https://openairdocs.org/sdr/IPXA2019021839164.md): Floor Panel · damaged · Feb 18, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1, PANEL 252XSF REQUIRES FAB. FABBED PANEL 252XSF FROM 5024N40000-G BATCH 33550636 PER SREO B757-5320-9692-K
- [SDR IPXA2019021839163](https://openairdocs.org/sdr/IPXA2019021839163.md): Floor Panel · damaged · Feb 18, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1, PANEL 231XCF REQUIRES FAB. FABBED PANEL 231XCF FROM 5024N40000-G BATCH 33550636 AND STEP CUT PER SREO B757-5320-9692-K
- [SDR IPXA2019021839162](https://openairdocs.org/sdr/IPXA2019021839162.md): Floor Panel · damaged · Feb 18, 2019 · N406UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1, MAIN CABIN FLOOR PANEL 211XAF REQUIRES FAB. FABBED PANEL 211XAF FROM 5024N40000-SS-G BATCH 33550636 PER SREO B757-5320-9692-K.

Next page: https://openairdocs.org/aircraft/N406UP/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 = 'N406UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N406UP/reports

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