# Service difficulty reports: N271UP, cancelled Dec 18, 2023

A list on [N271UP, cancelled Dec 18, 2023](https://openairdocs.org/deregistered/N271UP-2023-12-18.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 · 294 reports

- [SDR IPXA2023051693239](https://openairdocs.org/sdr/IPXA2023051693239.md): Light · inoperative · May 16, 2023 · N271UP · Doug MD11F · Emergency Lighting
  > EMERG LOGHT BAT 110 DMAG TEST FUNCTION. DEFERRED EMERGENCY LIGHTING SYSTEM IAW MEL 33-50-4 DMP CW PLACARD INSTALLED THIS OPEN M 808559THIS AIRCRAFT HAS BEEN SCRAPPED.
- [SDR IPXA2023021490989](https://openairdocs.org/sdr/IPXA2023021490989.md): Light · inoperative · Feb 14, 2023 · N271UP · Doug MD11F · Emergency Lighting
  > DURING PREFLIGHT EMERGENCY LIGHTS WILL NOT TEST. DEFERRED EMER LIGHT TEST FUNCTION IAW MEL 33-50-2 DMP COMPLIED WITH PLACARD INSTALLED.PERF OPERATIONAL TEST OF THE EMER LIGHTING SYSTEM IAW AMM 33-50-00-700-802. OPS CHECK GOOD. THIS CLEARS M802738.
- [SDR IPXA2023020290533](https://openairdocs.org/sdr/IPXA2023020290533.md): Light · inoperative · Feb 2, 2023 · N271UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA*** SUPPLEMENTAL SDR *** EMERGENCY LIGHTING SYSTEM TEST FUNCTION INOP. DEFERRED IAW MEL 33-50-2. CONTROL NO. M-801800 ASSIGNED, PLACARD INSTALLED. DMP COMPLIED WITH.R&R PER AMM 33-51-01-700-802. OPS CHECK GOOD. DEFERRAL CLEARED AND PLACARD RE
- [SDR IPXA2023011789982](https://openairdocs.org/sdr/IPXA2023011789982.md): Power Supply · no test · Jan 16, 2023 · N271UP · Doug MD11F · Emergency Lighting
  > EMERGENCY BATTERY 1 LOW MESSAGE DURING LIGHT TEST. R/R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-401.
- [SDR IPXA2023010289483](https://openairdocs.org/sdr/IPXA2023010289483.md): Line · stripped · Jan 1, 2023 · N271UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAWHILE PERFORMING TC# 8325 R1 DOOR PNEUMATIC BOTTLE ASSEM. FOUND BETWEEN BOTTLE AND OUT LINE STRIPPED THREADS. REQ # 428503REPLACED UNION BETWEEN BOTTLE AND OUT LINE ON R1 DOOR PNEUMATIC STORAGE RESERVOIR WITH A SERVICEABLE UNION. LEAK CHECK G
- [SDR IPXA2022102487473](https://openairdocs.org/sdr/IPXA2022102487473.md): Access Panel · gouged · Oct 24, 2022 · N271UP · Doug MD11F · Vertical Stabilizer, Plate/Skin
  > RIGHT SIDE LOWER VERTICAL STAB AFT ACCESS PANEL DAMAGEDREPAIRED DAMAGED AREA IAW EO MD11-5530-84606-C
- [SDR IPXA2022062783543](https://openairdocs.org/sdr/IPXA2022062783543.md): None · none · Jun 25, 2022 · N271UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA** SDR FILED OPEN**EMERG BATT 1 LO MESSAGE ON EICAS DURING PREFLIGHT CHECK. DEFERRED IAW MEL 33-50-4 DMP 33-50-4 ACCOMPLISHED. REF # M784711 PLACARD APPLIED
- [SDR IPXA2021060870280](https://openairdocs.org/sdr/IPXA2021060870280.md): Support Bracket · cracked · Jun 7, 2021 · N271UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:CL/H I/B WING #2 SLAT TRACK SLOT DOOR AFT SUPPORT BRACKET IS CRACKEDREMOVED FABBED AND INSTALLED SUPPORT BRACKET IAW SRM 51-31-01 DWG ARB1602 AND SRM 51-35-01
- [SDR IPXA2021060870279](https://openairdocs.org/sdr/IPXA2021060870279.md): Stiffener · chafed · Jun 7, 2021 · N271UP · Doug MD11F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:C#1 PYLON FAIRING ATTACH T ANGLE DEEPLY CHAFED AFT OF PRECOOLERREMOVED, FABBED, AND INSTALLED STIFFNER IAW SRM 51-31-01 DWG AUB7564 AND SRM 51-31-01
- [SDR IPXA2021060870274](https://openairdocs.org/sdr/IPXA2021060870274.md): Web · cracked · Jun 7, 2021 · N271UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CR/H AC BAY HAS A CRACKED WEB AT L-34 AT FS 595REMOVED FABBED AND INSTALLED NEW WEB IAW SRM 51-31-01, DRAWING # ACA3804 AND SRM 51-35-01
- [SDR IPXA2021060870303](https://openairdocs.org/sdr/IPXA2021060870303.md): Skin · cracked · May 26, 2021 · N271UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:2CR/H I/B FLAP LOWER SKIN HAS A CRACK XIFH= 134.REPAIRED CRACKED R/H I/B FLAP LOWER SKIN BETWEEN STA. XIFH=133.9 TO 147.3 AND BETWEEN STA. YIFH= 34 TO 78 IAW SRM 57-50-01 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021061170439](https://openairdocs.org/sdr/IPXA2021061170439.md): Floor Panel · corroded · May 24, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IS CORRODED.REPAIRED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IAW VT-SAA EA 011-5310-01-A9155 REV IR AND UPS EO MD11-5320-8
- [SDR IPXA2021061170438](https://openairdocs.org/sdr/IPXA2021061170438.md): Floor Panel · corroded · May 24, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IS CORRODED.REPAIRED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IAW VT-SAA EA 011-5310-01-A9162 REV. IR AND UPS EO MD11-5320-80651-A
- [SDR IPXA2021061070373](https://openairdocs.org/sdr/IPXA2021061070373.md): Mount · corroded · May 24, 2021 · N271UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:C2RH O/B HOR STAB #6 HINGE FITTING O/B LUG BUSHING HAS CORROSION.REPAIRED CORRODED HINGE FITTING O/B LUG IAW VT-SAA EA 011-5523-01-A9154 REV I/R AND UPS EO MD11-5520-80624-A (MINOR).
- [SDR IPXA2021061070372](https://openairdocs.org/sdr/IPXA2021061070372.md): Mount · corroded · May 24, 2021 · N271UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:C2RH I/B ELEVATOR #3 BEARING MOUNT FITTING O/B BUSHING HAS CORROSION.REPAIRED CORRODED MOUNT FITTING IAW VT-SAA EA 011-5523-01-A9153 REV I/R AND UPS EO MD11-5520-80625-A (MINOR).
- [SDR IPXA2021061070377](https://openairdocs.org/sdr/IPXA2021061070377.md): Floor Panel · corroded · May 24, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475-500.175 & BETWEEN X= -73.3 AND X= -107.250 HAS CORROSION.REPAIRED CORRODED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9167 REV. I/R AND UPS EO MD11-5320-80613-A. (MINOR)
- [SDR IPXA2021060970339](https://openairdocs.org/sdr/IPXA2021060970339.md): Skin · gouged · May 24, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:C2LH WING L/E SKIN IS GOUGE O/B OF #1 PYLON.REMOVED,FABRICATED AND REPLACED LT L/E SKIN IAW SRM 51-35-01 (MINOR).
- [SDR IPXA2021060470167](https://openairdocs.org/sdr/IPXA2021060470167.md): Floorbeam · corroded · May 24, 2021 · N271UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:2CFWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2021061470509](https://openairdocs.org/sdr/IPXA2021061470509.md): Support · damaged · May 23, 2021 · N271UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CFWD. CARGO CEILING SUPPORT HAS DAMAGED FASTENER HOLES BETWEEN STA. 909 TO 1009 AT X= -14.REPAIRED DAMAGED CEILING SUPPORT BETWEEN STA 909 TO 1009 AT X= -14 IAW VT-SAA EA 011 5320-01-A9158 REV. I/R AND UPS EO MD11-5320-80668-A. (MAJOR) REF 810
- [SDR IPXA2021060870291](https://openairdocs.org/sdr/IPXA2021060870291.md): Seat Track · cracked · May 23, 2021 · N271UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CFWD. CARGO CEILING AREA SEAT TRACK IS CRACKED AT STA. 635 AND X= -27.5.REPAIRED CRACKED SEAT TRACK BETWEEN STA. 625.0 TO 645.0 AND X= -27.5 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021060470161](https://openairdocs.org/sdr/IPXA2021060470161.md): Stringer · cracked · May 22, 2021 · N271UP · Doug MD11F · Wing, Longeron/Stringer
  > INSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 667.679.REPAIRED CRACKED R/H WING FIXED L/E UPPER STINGER AT STA. XOS. 667.679 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)
- [SDR IPXA2021060470166](https://openairdocs.org/sdr/IPXA2021060470166.md): Longeron Splice · cracked · May 22, 2021 · N271UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021060370113](https://openairdocs.org/sdr/IPXA2021060370113.md): Stringer Splice · cracked · May 22, 2021 · N271UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON 44R SPLICE FITTING IS CRACKED AT STA. 5-123.REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG. A5A7116 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021061170437](https://openairdocs.org/sdr/IPXA2021061170437.md): Spar Cap · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:2CLT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IS CORRODED.REPAIRED CORRODED LT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IAW VT-SAA EA 011-5710-01-A9159 REV. IR AND UPS EO MD11-5710-80646-A.
- [SDR IPXA2021061170434](https://openairdocs.org/sdr/IPXA2021061170434.md): Skin · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IS CORRODED.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IAW VT-SAA EA 011-5730-01-A9147 REV. IR AND UPS EO MD11-5730-80654-A. REF. FAA FORM 8100
- [SDR IPXA2021061470507](https://openairdocs.org/sdr/IPXA2021061470507.md): Support Angle · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C2RH O/B WING LOWER SUPPORT ANGLE HAS CORROSION AT LWR T/E.REMOVED,FABRICATED AND REPLACED CORRODED SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).
- [SDR IPXA2021061470506](https://openairdocs.org/sdr/IPXA2021061470506.md): Skin · gouged · May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:C2RT WING ACCESS PANEL 616ET GOUGE AT UPPER FWD SURFACE.REMOVED,FABRICATED AND REPLACED GOUGED PANEL(SKIN) IAW SRM 51-35-01 AND 51-31-01 (MINOR).
- [SDR IPXA2021061470512](https://openairdocs.org/sdr/IPXA2021061470512.md): Spar Cap · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:2CR/H WING REAR SPAR CAP UPPER FLANGE HAS CORROSION BETWEEN STA. XORS. 1042.35 TO 1054.REPAIRED CORRODED R/H WING REAR SPAR CAP UPPER FLANGE BETWEEN STA. XORS. 1042.35 TO 1054 IAW VT-SAA EA 011-5710-01-A9137 REV. I/R AND UPS EO MD11-5710-80666-
- [SDR IPXA2021061170411](https://openairdocs.org/sdr/IPXA2021061170411.md): Cap · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:2CR/H WING LOWER CAP HAS CORROSION AT STA. XW= 320.REPAIRED CORRODED R/H WING LOWER CAP BETWEEN STA. XW= 275.230 & XW= 326.730 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)..
- [SDR IPXA2021060870300](https://openairdocs.org/sdr/IPXA2021060870300.md): Spar Cap · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:2CRT WING REAR SPAR UPPER CAP BELOW #3 SPOILER HAS CORROSION.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AT STA XORS 653.100 IAW VT-SAA EA 011-5700-01-A9140 REV. IR AND UPS EO MD11-5710-80599-A. (MINOR)
- [SDR IPXA2021060470165](https://openairdocs.org/sdr/IPXA2021060470165.md): Skin · corroded · May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 & BETWEEN STRINGER 17 AND FWD SPAR HAS 5 EA AREAS OF CORROSION.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 7 BETWEEN STRINGER 17 AND FWD SPAR 5 EA AREAS IAW VT-SAA EA 011
- [SDR IPXA2021060470159](https://openairdocs.org/sdr/IPXA2021060470159.md): Skin · cracked · May 21, 2021 · N271UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:2CR/H WING I/B FLAP CENTER BOX UPPER SKIN IS CRACKED AT STA.XIFH=147.3.REPAIRED CRACKED R/H WING UPPER SKIN AT STA. XIFH= 147.3 AND BETWEEN YIF= 26 TO YIFH= 28 IAW SRM 57-00-01 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021060270078](https://openairdocs.org/sdr/IPXA2021060270078.md): Vane · delaminated · May 21, 2021 · N271UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:2CL/H I/B FLAP VANE I/B LOWER SURFACE IS DELAMINATEDREPAIRED DELAMINATED L/H I/B FLAP VANE LOWER SURFACE IAW SRM 57-50-80 REPAIR 2 FIG. 201 & SRM 51-62-01 GENERAL. (MAJOR)
- [SDR IPXA2021061170436](https://openairdocs.org/sdr/IPXA2021061170436.md): Seat Track · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:2CFWD CABIN SEAT TRACK BETWEEN STA 480 - 488 AT LBL 27.5 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN SEAT TRACK BETWEEN STA 421.578 - 625 AT LBL 27.5 IAW SRM 51-31-01 & 51-33-01. (MINOR)
- [SDR IPXA2021061170435](https://openairdocs.org/sdr/IPXA2021061170435.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500 AND BETWEEN LBL 74 - LBL 107 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500 AND BETWEEN LBL 74 - LBL 107 IAW SRM 51-31-01 & 51-35-01. (MINOR)
- [SDR IPXA2021061470517](https://openairdocs.org/sdr/IPXA2021061470517.md): Skin · gouged · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CL/H WING FIXED L/E SKIN IS GOUGED BETWEEN STA. XOS= 1031.669 TO 1044.27.REPAIRED GOUGED L/H WING FIXED L/E SKIN BETWEEN STA. XOS.= 1031.669 TO 1044.27 IAW VT-SAA EA 011-5730-01-A9139 REV. I/R AND UPS EO MD11-5750-80664-A. (MAJOR) REF 8100-9 B
- [SDR IPXA2021061070385](https://openairdocs.org/sdr/IPXA2021061070385.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475 AND 500 AND BETWEEN X=0 TO X= 8.5 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9160 REV. I/R AND UPS EO MD11-5320-80626-A. (MINOR)
- [SDR IPXA2021061070383](https://openairdocs.org/sdr/IPXA2021061070383.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CRCB FLOOR PANEL HAS CORROSION BETWEEN STA. 475.0 TO 500.0 AND BETWEEN X= -27.5 TO X= -36.0.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9161 REV. I/R AND UPS EO MD11-5320-80627-A. (MINOR)
- [SDR IPXA2021061070382](https://openairdocs.org/sdr/IPXA2021061070382.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475.0 TO 500.175 AND BETWEEN X= 62.190 AND 73.340 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5310-01-A9156 REV. I/R AND UPS EO MD11-5320-80633-A. (MINOR)
- [SDR IPXA2021061070379](https://openairdocs.org/sdr/IPXA2021061070379.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CMAIN CABIN FLOOR PANEL BETWEEN STA. 475.0 & 500.0 AND BETWEEN X= 27.5 TO X= 36.0 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9164 REV. I/R AND UPS EO MD11-5320-80632-A. (MINOR)
- [SDR IPXA2021060870289](https://openairdocs.org/sdr/IPXA2021060870289.md): Skin · gouged · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CL/H WING LOWER L/E SKIN HAS GOUGES BETWEEN STA. XW= 332 TO 344 & YW= 273 TO 280.REPAIRED GOUGED L/H WING LOWER L/E SKIN BETWEEN STA. XW= 332 TO 344 & YW= 273 TO 280 IAW SRM 57-40-01 REPAIR 12 FIG. 201. (MAJOR)
- [SDR IPXA2021060470164](https://openairdocs.org/sdr/IPXA2021060470164.md): Floor Panel · corroded · May 20, 2021 · N271UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 503 & BETWEEN LBL 19 - LBL 27.5 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 503 & BETWEEN LBL 19 - LBL 27.5 IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2021060370112](https://openairdocs.org/sdr/IPXA2021060370112.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CR/H WING FIXED L/E SPLICE DOUBLER IS CRACKED AT STA. XOS. 667.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. ARB3954 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021060370111](https://openairdocs.org/sdr/IPXA2021060370111.md): Former · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:2CR/H WING FIXED L/E SPLICE/FORMER IS CRACKED AT STA. XOS. 639.REMOVED, FABRICATED AND REPLACED SPLICE/FORMER IAW DWG. ARB2931 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021060370110](https://openairdocs.org/sdr/IPXA2021060370110.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692 TO 703.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DPOUBLER BETWEEN STA. XOS. 692 TO 703.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021060370109](https://openairdocs.org/sdr/IPXA2021060370109.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 636 TO 643.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 636 TO 643 IAW SRM 57-40-01 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021060370108](https://openairdocs.org/sdr/IPXA2021060370108.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 589.88 TO 594.88.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 589.88 TO 594.88 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021060370107](https://openairdocs.org/sdr/IPXA2021060370107.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.667.62 TO 673.76.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 667.62 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021060170013](https://openairdocs.org/sdr/IPXA2021060170013.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 661 TO 667.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 661 TO 667 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2021060170016](https://openairdocs.org/sdr/IPXA2021060170016.md): Doubler · cracked · May 20, 2021 · N271UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 633 TO 636.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 633 TO 636 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Next page: https://openairdocs.org/deregistered/N271UP-2023-12-18/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 = 'N271UP' AND deregistration_id = 'N271UP-2023-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N271UP-2023-12-18/reports

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