# Service difficulty reports: N270UP, cancelled Jan 21, 2025

A list on [N270UP, cancelled Jan 21, 2025](https://openairdocs.org/deregistered/N270UP-2025-01-21.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 7 · 302 reports

- [SDR IPXA2023092994293](https://openairdocs.org/sdr/IPXA2023092994293.md): Engine · inoperative · Sep 26, 2023 · N270UP · Doug MD11F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* *IFSD* ENGINE 3 SURGE ON TO
- [SDR IPXA2023082293980](https://openairdocs.org/sdr/IPXA2023082293980.md): Bottle · low pressure · Aug 22, 2023 · N270UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAR1 DOOR EMERGENCY PNEUMATIC BOTTLE PRESSURE LOWSVC'D BOTTLE AS REQ'D TO ACCEPTABLE PRESSURE REF AMM 12-25-04/301
- [SDR IPXA2023070993625](https://openairdocs.org/sdr/IPXA2023070993625.md): Door · broken · Jul 9, 2023 · N270UP · Doug MD11F · Service Doors
  > R1 DOOR AFT RETAINER AND VIEWING WINDOW IS BROKE. DEFERRED R1 DOOR GIRT BAR AFT RETAINER/VIEWING WINDOW IAW EO MD11-5210-87587-A LINKED TO M810223.R&R R1 DOOR AFT RETAINER & VIEWING WINDOW IAW AMM 25-23-07-400-802. THIS CLEARS D810224 PLACARD REMOVED.
- [SDR IPXA2023042192945](https://openairdocs.org/sdr/IPXA2023042192945.md): Sign · broken · Apr 20, 2023 · N270UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/AL1 EXIT DOOR EXIT SIGN FELL DOWNINSTALLED EXIT SIGN PE AMM 33-27-05.
- [SDR IPXA2023033092444](https://openairdocs.org/sdr/IPXA2023033092444.md): Bottle · inoperative · Mar 29, 2023 · N270UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAR1 SLIDE ASSIST BOTTLE DEPLETEDSERVICED R1 SLIDE ASSIST BOTTLE IAW AMM 12-25-04
- [SDR IPXA2023020390577](https://openairdocs.org/sdr/IPXA2023020390577.md): Not Entered · not entered · Feb 2, 2023 · N270UP · Doug MD11F · Pneumatic Indicating System
  > INSPECTION TYPE:NA**DIVERSION** DURING CLIMB OUT OF PHX CREW RECIEVED LEVEL 1 AIR SYS OFF MESSAGE. RED MANF FAIL LIGHT ON OVERHEAD PANEL ILLUMITED FOR APPROX. 10 SEC. AND WENT OUT. BLEED AIR VALVE # 1 CLOSED. SYSTEM IS DEPRESSURIZED.ACCOMPLISHED FIM 36-23-02 F
- [SDR IPXA2023011990046](https://openairdocs.org/sdr/IPXA2023011990046.md): Support Angle · cracked · Jan 18, 2023 · N270UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:C-1, RH UPPER WING TO BODY FAIRING ATTACH ANGLE CRACKED AT APPX. STA. 1239. REMOVED. FABBED AND INSTALLED RT WING TO BODY FAIRIHG SUPPORT ANGLE IAW SRM 51-31-01 AND DRAWING ANB7142
- [SDR IPXA2023012090089](https://openairdocs.org/sdr/IPXA2023012090089.md): Spar Cap · corroded · Jan 10, 2023 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CL/H WING REAR UPPER AFT SPAR AT STA XORS=720.000 HAS CORROSION.REMOVED AND REPAIRED THE CORRORED L/H WING REAR UPPER AFT SPAR AT STA XORS=720.000 IAW VT-SAA EA 011-5700-01-A9808 IR AND UPS EO MD11-5710-85675-A (MINOR)
- [SDR IPXA2023012690291](https://openairdocs.org/sdr/IPXA2023012690291.md): Stringer · cracked · Jan 3, 2023 · N270UP · Doug MD11F · Fuel Storage
  > INSPECTION TYPE:C3, MAJOR REPAIR, UPPER CENTER AUX TANK EXISTING REPAIR IS CRACKED LOCATED BETWEEN STA X-81 AND X-46 AT STRINGER 48.REPAIRED THE CRACKED EXISTING REPAIR STRINGER 48 LOCATED BETWEEN STA X-81, X-46 IAW EA 011-5710-01-A9806 REV I/R & EO MD11-57
- [SDR IPXA2023012690289](https://openairdocs.org/sdr/IPXA2023012690289.md): Stringer · cracked · Jan 3, 2023 · N270UP · Doug MD11F · Fuel Storage
  > INSPECTION TYPE:C3, MAJOR REPAIR, UPPER CENTER AUX TANK EXISTING REPAIR IS CRACKED LOCATED BETWEEN STA X-17 AND X17 STR 47.REPAIRED CRACKED EXISTING REPAIR STRINGER 47 BETWEEN STA X-17 AND X17 IAW EA 011-5710-01-A9807 REV I/R & EO MD11-5710-85669-A.
- [SDR IPXA2023012490215](https://openairdocs.org/sdr/IPXA2023012490215.md): Stringer · cracked · Jan 3, 2023 · N270UP · Doug MD11F · Fuel Storage
  > INSPECTION TYPE:3C, MAJOR REPAIR, UPPER CENTER AUX TANK HAS CRACKED STRINGER 48 LOCATED BETWEEN X17 AND X46. REPAIRED THE CRACKED STRINGER 48 AT THE UPPER CENTER AUX TANK IAW SRM 57-10-03, REPAIR 1, FIG 201, REV 69.01.
- [SDR IPXA2023012690282](https://openairdocs.org/sdr/IPXA2023012690282.md): Spar · corroded · Jan 2, 2023 · N270UP · Doug MD11F · Wing Spar
  > INSPECTION TYPE:C3L/H UPPER WING T/E REAR SPAR HAS CORROSION AT STA XORS=718. REPAIRED UPPER REAR SPAR ON THE L/H WING AT STA XORS=718 IAW SRM 57-00-00 FIG 202, DWG ARB7413. (MINOR)
- [SDR IPXA2023011789997](https://openairdocs.org/sdr/IPXA2023011789997.md): Doubler · cracked · Dec 30, 2022 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: C3, MAJOR REPAIR. RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPX. STA XOS-635. REMOVED, FABRICATED, REPAIRED THE CRACKED BEADED DOUBLER AT STA XOS-635 IAW SRM 57-40-02 REPAIR 15 FIG 205, REV 69.01. (MAJOR)
- [SDR IPXA2023011789994](https://openairdocs.org/sdr/IPXA2023011789994.md): Seat Track · corroded · Dec 28, 2022 · N270UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C3BULGE UNDER MOONMAT CENTER OF COURIER AREA AT STA X=0.00 BETWEEN Y=411 - Y=441.REMOVED, REPAIRED CORROSION AT SEAT TRACK AT STA X=0.00 AND BETWEEN Y=411 - Y=441 IAW EA 011-5320-01-A9799 IR, DATED 01/10/2023 AND UPS EO MD11-5310-85649-A.
- [SDR IPXA2022072184404](https://openairdocs.org/sdr/IPXA2022072184404.md): Light · inoperative · Jul 20, 2022 · N270UP · Doug MD11F · Emergency Equipment
  > INSPECTION TYPE:NAR1 DOOR PRESSURE LIGHT DOES NOT ILLUMINATE DURING PREFLIGHT TEST. DEFERRED SLIDE PRESSURE TEST INDICATIONS SYSTEM PER MEL 25-61-2 DMP C/WRELAMPED THE PTT SWITCH REF AMM 25-61-04. OPS TEST OK, PLACARD REMOVED.
- [SDR IPXA2022071884279](https://openairdocs.org/sdr/IPXA2022071884279.md): Door · inoperative · Jul 16, 2022 · N270UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NA** SDR FILED OPEN** R1 DOOR SLIDE REMOTE PRESSURE TEST BUTTON INOP. DEFERRED REMOTE R1 SLIDE PRESSURE TEST FUNCTION IAW MEL 25-61-2. ASSIGNED M786461 PLACARD INSTALLED & DMP C/W.
- [SDR IPXA2022021679064](https://openairdocs.org/sdr/IPXA2022021679064.md): None · none · Feb 15, 2022 · N270UP · Doug MD11F · Pneumatic Distribution System
  > INSPECTION TYPE:NA** ATB SDR FILED** NO EMERGENCY DEC'D**A/C LANDED W/OUT INCIDENT** LEVEL 2 "AIR SYS 3 PRES LO" AIR TURN BACK DUE TO ICING COND AT DEST.R&R HIGH STAGE MANIFOLD PRESSURE SENSOR PER AMM 36-12-04-000-801, OPS CHECK, SYSTEM CHECK NORMAL, FOB BEFO
- [SDR IPXA2021112876382](https://openairdocs.org/sdr/IPXA2021112876382.md): None · inoperative · Nov 27, 2021 · N270UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/ATEST LT. ON R1 ENTRY DOOR INOP.DEFERRED PER MEL 25-61-2 & ACCOMPLISHED DMP 25-61-2 R1 SLIDE PRESS. OK. ASSIGNED M-764325. EACH FLT RE-INSP. REQ. REPLACED BATTERIES REF 25-61-04 OPS NML.
- [SDR IPXA2021081672780](https://openairdocs.org/sdr/IPXA2021081672780.md): Skin · cracked · Aug 16, 2021 · N270UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/AFUSELAGE SKIN CRACK AT RIGHT SIDE AIR CONDITIONING DOOR OPENINGACCOMPLISH FUSELAGE SKIN REPAIR IAW EO 80909-B
- [SDR IPXA2021060370143](https://openairdocs.org/sdr/IPXA2021060370143.md): Cable · broken · Jun 3, 2021 · N270UP · Doug MD11F · Passenger/Crew Doors
  > WHILE CLOSING THE LEFT SIDE CREW ENTRANCE DOOR, ONE OF THE CABLES BROKE. R&R L1 DOOR AFT LOWER DRIVE CABLE PER MM 52-11-03, PRIOR TO RIG/ OPS CHECK FOUND DAMAGED SPRING AND FRAYED CABLE. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1 M746276 ASSIGNED, PLACARD INSTALL
- [SDR IPXA2021040567775](https://openairdocs.org/sdr/IPXA2021040567775.md): Sensor · failed · Apr 3, 2021 · N270UP · Doug MD11F · Airfoil Anti/De-ice System
  > INSPECTION TYPE:NA**ATB - SDR FILED OPEN - NO EMERG DECLARED - NO EQUIP USED.** LVL 1 ANTI -ICE SENSOR FAIL AT FL240 ON CLIMBOUT. MEL 36 10 2 1 DEFER PNEU SUPPLY 1 DMP C/W.
- [SDR IPXA2021013165105](https://openairdocs.org/sdr/IPXA2021013165105.md): Case · cracked · Jan 12, 2021 · N270UP · Doug MD11F · Turbine Engine Air Inlet Section
  > INSPECTION TYPE: 2 C NR 1 ENGINE FAN CASE IS CRACKED AT 5 O'CLOCK POSITION JUST AFT OF NOSE COWL ANTI-ICE VALVE. REPAIRED CRACKED NR 1 ENGINE FAN CASE AT 5 O'CLOCK POSITION IAW UPS EO 4000-7230-79031-A. MINOR
- [SDR IPXA2021012865014](https://openairdocs.org/sdr/IPXA2021012865014.md): Hinge · corroded · Jan 11, 2021 · N270UP · Doug MD11F · Trailing Edge Flap Control System
  > INSPECTION TYPE: C2 LT WING OUTBOARD FLAP OUTBOARD HINGE BORE HAS CORROSION. REPAIRED CORRODED LT OUTBOARD FLAP OUTBOARD HINGE BORE, IAW VT-SAA EA 011-5740-01-A8829 REV I/R AND UPS EO MD11-5740-79149-A. (MINOR)
- [SDR IPXA2021012865027](https://openairdocs.org/sdr/IPXA2021012865027.md): Hinge · corroded · Jan 11, 2021 · N270UP · Doug MD11F · Trailing Edge Flap Control System
  > INSPECTION TYPE: C2 RT WING OUTBOARD FLAP INBOARD HINGE LOWER LUG BORE CORRODED. REPAIRED CORRODED RT OUTBOARD FLAP INBOARD HINGE LUG BORE, IAW VT-SAA EA 011-5740-01-A8834 REV I/R AND UPS EO MD11-5740-79170-A. (MINOR)
- [SDR IPXA2021012364803](https://openairdocs.org/sdr/IPXA2021012364803.md): Lug · gouged · Jan 9, 2021 · N270UP · Doug MD11F · Ailerons
  > INSPECTION TYPE: 2C RT OUTBOARD AILERON ACTUATOR ATTACH FITTING LUGS ARE GOUGED. REPAIRED GOUGED RT OUTBOARD AILERON ACTUATOR ATTACH FITTING LUGS, IAW VT-SAA EA 011-5751-01-A8822 REV IR AND UPS EO MD11-5750-79096-A. (MINOR)
- [SDR IPXA2021020265227](https://openairdocs.org/sdr/IPXA2021020265227.md): Longeron · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:2CCENTER CARGO LONGERON 52 IS CORRODED AT STA. 5-11.REPAIRED CORRODED LONGERON 52 BETWEEN STA. 5-0 TO 5-32 IAW VT-SAA EA 011-5310-01-*A8818 REV. I/R AND UPS EO MD11-5310-79192-A. (MAJOR)
- [SDR IPXA2021020265226](https://openairdocs.org/sdr/IPXA2021020265226.md): Floorbeam · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:2CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 AND X= -57.5.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70 AND X= -57.5 IAW VT-SAA EA 011-5310-01-A8835 REV. I/R AND UPS EO MD11-5340-79191-A. (MAJOR)
- [SDR IPXA2021013065083](https://openairdocs.org/sdr/IPXA2021013065083.md): Floor Support · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2 C CENTER CARGO FLOOR SUPPORT IS CRACKED AT STA 1521 BETWEEN LBL 25 & RBL 25. R & R CRACKED CENTER CARGO FLOOR SUPPORT AT STA 1521 BETWEEN LBL 25 - RBL 25 IAW MD-11 SRM 51-35-01. MINOR
- [SDR IPXA2021013065082](https://openairdocs.org/sdr/IPXA2021013065082.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2 C FLOOR PANEL NR WSP0790-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 62.1 - X= 73.3 IAW VT-SAA EA 011-5320-01-A8807 REV IR AND UPS EO MD11-5310-79067-A. MINOR
- [SDR IPXA2021013065081](https://openairdocs.org/sdr/IPXA2021013065081.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0789-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 47.5 - X= 62.1 IAW VT-SAA EA 011-5320-01-A8812 REV IR AND UPS EO MD11-5310-79073-A. MINOR
- [SDR IPXA2021013065080](https://openairdocs.org/sdr/IPXA2021013065080.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0788-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 36 - X= 47.5 IAW VT-SAA EA 011-5320-01-A8824 REV IR AND UPS EO MD11-5310-79107-A. MINOR
- [SDR IPXA2021013065079](https://openairdocs.org/sdr/IPXA2021013065079.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0785-502 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= 27.5 - X= 36 IAW VT-SAA EA 011-5310-01-A8809 REV. IR AND UPS EO MD11-5310-79066-A. MINOR
- [SDR IPXA2021013065078](https://openairdocs.org/sdr/IPXA2021013065078.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE: 2 C FLOOR PANEL WSP0785-501 HAS CORROSION. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X= -27.5 - X= -36 IAW VT-SAA EA 011-5310-01-A8810 REV IR AND UPS EO MD11-5320-79065-A. MINOR
- [SDR IPXA2021013065077](https://openairdocs.org/sdr/IPXA2021013065077.md): Floor Panel · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE: 2 C FLOOR PANEL NR WSP0785-502 IS CORRODED. REPAIRED CORRODED MAIN CABIN FLOOR PANEL BETWEEN STA 475 - 488.8 & X=0 - X= -8.50 IAW VT-SAA EA 011-5320-01-A8814 REV IR AND UPS EO MD11-5310-79059-A. MINOR
- [SDR IPXA2021012764972](https://openairdocs.org/sdr/IPXA2021012764972.md): Tee Fitting · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2 MAIN CABIN LONGERON 15L TEE ANGLE IS CRACK AT STA 1341. REMOVED,FABRICATED AND REPLACED CRACKED LONG 15L TEE ANGLE, IAW SRM 51-33-01, 51-35-01 AND DWG AEA7568-21 (MINOR).
- [SDR IPXA2021012764975](https://openairdocs.org/sdr/IPXA2021012764975.md): Seat Track · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C2 MAIN CABIN SEAT TRACK CORRODED AT STA 421-443 RBL X-27.50. REMOVED, FABRICATED AND REPLACED CORRODED SEAT TRACK, IAW SRM 51-31-01, 51-33-01 VT-SAA EA 011-5310-01-A8808 I/R AND UPS EO MD11-5310-79153-A. (MINOR)
- [SDR IPXA2021012764974](https://openairdocs.org/sdr/IPXA2021012764974.md): Longeron · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: 2C LONGERON 47 LT HAS CORROSION AT STA 6-90 AND 6-100. REPAIRED CORRODED LONGERON 47 LT BETWEEN STA. 6-70 TO 6-100, IAW SRM 53-00-05 REPAIR 1 FIG 201 & 202. (MAJOR)
- [SDR IPXA2021012764967](https://openairdocs.org/sdr/IPXA2021012764967.md): Intercostal · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C LOWER FWD CARGO INTERCOSTAL IS CRACKED AT STA 6-50 AND LONG 43L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021012664888](https://openairdocs.org/sdr/IPXA2021012664888.md): Skin · dented · Jan 7, 2021 · N270UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE: 2C RT WING INBOARD FLAP NR 2 ROLLER ACCESS COVER IS DENTED AND GOUGED AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0. REPAIRED DENTED RT INBOARD FLAP NR 2 ROLLER ACCESS COVER AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0, IAW SRM
- [SDR IPXA2021012364796](https://openairdocs.org/sdr/IPXA2021012364796.md): Floor Support · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C FLOOR PANEL SUPPORT UNDER LAV HAS HEAVY CORROSION. REMOVED AND REPLACED CORRODED FLOOR PANEL SUPPORT UNDER LAV BETWEEN STA 392-440 AND BETWEEN X= -8.5-X= -27.5, IAW MD-11 SRM 51-33-01. (MINOR)
- [SDR IPXA2021012164710](https://openairdocs.org/sdr/IPXA2021012164710.md): Seat Track · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: 2C COURIER AREA SEAT TRACK IS CORRODED BETWEEN STA 459.277 & 515.00 AND BETWEEN X=68 TO X=77.58. REMOVED, FABRICATED AND REPLACED SEAT TRACK, IAW DWG WSP0826-509 AND SRM 53-20-52. (MINOR)
- [SDR IPXA2021012164709](https://openairdocs.org/sdr/IPXA2021012164709.md): Seat Track · corroded · Jan 7, 2021 · N270UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: 2C COURIER AREA SEAT TRACK IS CORRODED BETWEEN STA 400.34 TO 481.0 AND X= -36. REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA 400.34 TO 481.0 AND X= -36, IAW DWG WSP0826 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021011664479](https://openairdocs.org/sdr/IPXA2021011664479.md): Doubler · chafed · Jan 7, 2021 · N270UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE: 2C TAIL CONE RT UPPER PRODUCTION DOUBLER REPAIR FILLER HAS DEEP CHAFE DAMAGE. REMOVED AND REPLACED CHAFED TAIL CONE RT UPPER PRODUCTION DOUBLER REPAIR FILLER, IAW UPS EO MD11-5350-66790-A. (MINOR)
- [SDR IPXA2021011664487](https://openairdocs.org/sdr/IPXA2021011664487.md): Access Panel · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C RT WING LOWER SKIN FUEL ACCESS PANEL 636AB LANDING HAS 2 EA CRACKS. REPAIRED 2 EA CRACKS ON RT WING LOWER SKIN FUEL ACCESS PANEL 636AB LANDING, IAW MD-11 SRM 57-20-02, REPAIR 5, FIGURE 201. (MINOR)
- [SDR IPXA2021011664486](https://openairdocs.org/sdr/IPXA2021011664486.md): Access Panel · cracked · Jan 7, 2021 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C LT WING LOWER SKIN FUEL ACCESS PANEL 536AB LANDING HAS 4 CRACKS. REPAIRED 4 EA CRACKS ON LT WING LOWER SKIN FUEL ACCESS PANEL 536AB LANDING, IAW MD-11 SRM 57-20-02, REPAIR 5, FIGURE 201. (MINOR)
- [SDR IPXA2021012664889](https://openairdocs.org/sdr/IPXA2021012664889.md): Skin · cracked · Jan 6, 2021 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE LOWER SKIN IS CRACKED AT STA XOS 500.00. REPAIRED CRACKED LT WING FIXED LEADING EDGE LOWER SKIN AT STA XOS 500.00, IAW SRM 57-40-01 REPAIR 17 FIG 201. (MAJOR)
- [SDR IPXA2021012364802](https://openairdocs.org/sdr/IPXA2021012364802.md): Former · cracked · Jan 6, 2021 · N270UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE FORMER IS CRACKED INBOARD OF NR 9 SLAT TRACK. REMOVED AND REPLACED CRACKED LT WING FIXED LEADING EDGE FORMER INBOARD OF NR 9 SLAT TRACK, IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)
- [SDR IPXA2021012364795](https://openairdocs.org/sdr/IPXA2021012364795.md): Support · cracked · Jan 6, 2021 · N270UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE: 2C RT WING FIXED LEADOMG EDGE SUPPORT ANGLE OUTBOARD SIDE OF REFUELING CONTROL PANEL IS CRACKED INSIDE ACCESS PANEL 619CB. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE SUPPORT ANGLE OUTBOARD SIDE OF REFUELING CONTROL PANEL INSIDE A
- [SDR IPXA2021012364801](https://openairdocs.org/sdr/IPXA2021012364801.md): Stiffener · cracked · Jan 6, 2021 · N270UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE RIB STIFFENER IS CRACKED AT OUTBOARD END OF ACCESS PANEL 618FB. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE RIB STIFFENER AT OUTBOARD END OF ACCESS PANEL 618FB, IAW MD-11 SRM 51-33-01 AND 51-35-01. (M
- [SDR IPXA2021012164707](https://openairdocs.org/sdr/IPXA2021012164707.md): Doubler · cracked · Jan 6, 2021 · N270UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 661.71 TO 667.67. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 661.71 TO 667.67, IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Next page: https://openairdocs.org/deregistered/N270UP-2025-01-21/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 = 'N270UP' AND deregistration_id = 'N270UP-2025-01-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N270UP-2025-01-21/reports

---
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