# Service difficulty reports: N296UP, cancelled Dec 18, 2023

A list on [N296UP, cancelled Dec 18, 2023](https://openairdocs.org/deregistered/N296UP-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 8 · 378 reports

- [SDR IPXA2023053193349](https://openairdocs.org/sdr/IPXA2023053193349.md): Aileron · inoperative · May 31, 2023 · N296UP · Doug MD11F · Aileron Control System
  > ATB, AILERAON DEFLECT DISAG RESULTING IN SIGNIFICANT AILERON DISPLACEMENT. AFTER REPLACEMENT OF KOB AILERON DEFLECTED ACTUATOR, AILERON DEFLECTION SYSTEM OPS CHECK GOOD. PLACARD REMOVED.
- [SDR IPXA2023051093183](https://openairdocs.org/sdr/IPXA2023051093183.md): Door · inoperative · May 9, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > LH CREW DOOR WILL NOT OPEN. R/R L1 DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06. OPS CHECK NORMAL.
- [SDR IPXA2023050693137](https://openairdocs.org/sdr/IPXA2023050693137.md): Door · inoperative · May 6, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NALT 1 DOOR W/ NOT OPEN W/ GND PWR @ SDF POSTFLT R1 IS NORMAL. ITEM PLACARD ON DI M808083 PER MEL 52-10-3-1-2-1 PLACARD INSTALLED NO DMPR&R RELAY R2-5324 PER SOPM 20-11-04 & WDM 52-1101 PG. 6 OPS CHECK NORMAL THIS CEALRS M808083 PLACARD REMOVED
- [SDR IPXA2023042392964](https://openairdocs.org/sdr/IPXA2023042392964.md): Door · stuck · Apr 23, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > DOOR 1L WOULD NOT OPEN AFTER TAXI IN DOOR WAS DISARMED DOOR 1R OPERATES NORMALLY. DEF IN REF TO MEL 52-10-1-2-0-1 DEF# M 807390 PLACARD INSTALLED DMP C/W. PERFORMED OPS CK ON L-1 PASSENGER DOOR NORMAL MODE IAW AMM 52-10-700-801. OPS CK OKAY BOTH USING INTERNA
- [SDR IPXA2023032192110](https://openairdocs.org/sdr/IPXA2023032192110.md): Housing · broken · Mar 21, 2023 · N296UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NAL1 DOOR FWD EMERGENCY LIGHT HOUSING BROKEN. CPW.R&R L1 DOOR EMER LIGHT OP CK GOOD. REF SWPM 20-10-11 & MM 20-50-02
- [SDR IPXA2023032192109](https://openairdocs.org/sdr/IPXA2023032192109.md): Door · discharged · Mar 21, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR PNEUMATIC RESERVOIR DISCHARGED. REQUIRE SERVICE.SERVICE L1 PNEUMATIC RESERVOIR REF MM 12-25-04.
- [SDR IPXA2023031491843](https://openairdocs.org/sdr/IPXA2023031491843.md): Door · inoperative · Mar 14, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > MAIN CABIN DOOR 1L BINDING WHEN CLOSING UNABLE TO ARM. L1 DOOR DEFERRAL IN CLOSED POSITION REF MEL 52-10-3-1-2-1-2 PLACARD INSTALLED ON LOG PAGE 530195 ITEM # 1 M-804609INSPECTED L1 DOOR, FOUND BROKEN SHIM COVER TOP AFT SIDE. UPON FURTHER NOTICE DOOR NEEDED FU
- [SDR IPXA2023031091716](https://openairdocs.org/sdr/IPXA2023031091716.md): Cover · inoperative · Mar 10, 2023 · N296UP · Doug MD11F · Passenger/Crew Doors
  > LEFT ENTRY DOOR PLASTIC SLIDE COVER ON DOOR NOT SECURE. DEFERRED PER MEL 52-10-3-1-2-1-2. NO MX ACTION REQ. PLACARD INSTALLED. OPENED M804609INSPECTED L1 DOOR, FOUND BROKEN SHIM COVER TOP AFT SIDE. UPON FURTHER NOTICE DOOR NEEDED FURTHER T/S FOR BAD BOOGIES OR
- [SDR IPXA2023011389510](https://openairdocs.org/sdr/IPXA2023011389510.md): Power Supply · inoperative · Jan 3, 2023 · N296UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY LOW MESSAGE DISPLAYED. R & R EMERGENCY LIGHTING POWER SUPPLY PER AMM 33-51-01-400-802 & AMM 33-51-01-000-802. ACCOMPLISHED OPERATIONAL TEST AMM 33-51-01-700-802. FUNCTIONAL TEST AMM 33-50-00-700-801 AND AMM 33-50-00-700-802 ALL PASSED.
- [SDR IPXA2023010438910](https://openairdocs.org/sdr/IPXA2023010438910.md): Warning Message · illuminated · Jan 3, 2023 · N296UP · Doug MD11F · Emergency Lighting
  > REF ITEM 1 THIS LOGPAGE EMERG. LT BAT LO MESSAGE DISPLAYED. FWD TO MEL 33 50 4, PLAC INSTALLED M PROC C/W AMC ISSUED M799426. OPEN
- [SDR IPXA2022053182680](https://openairdocs.org/sdr/IPXA2022053182680.md): Battery · inoperative · May 31, 2022 · N296UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:NA**SUPPLEMENTAL SDR** EMER LT BATT 1 LO ON PREFLIGHT.REPLACED POWER SUPPLY IAW MM 33-51-01-400-802. OPS CHECK GOOD. THIS CLEARS 782460.
- [SDR IPXA2022052882597](https://openairdocs.org/sdr/IPXA2022052882597.md): Door · inoperative · May 27, 2022 · N296UP · Doug MD11F · Doors
  > INSPECTION TYPE:NAL1 DOOR WAS ON DEFERAL CREW OPENED DOOR UNABLE TO CLOSE BOTH FWD AND AFT LOWER CABLES BROKENINSTALLED FWD & AFT LOWER CABLES ON L1 DOOR PER AMM 52-11-03-400-801 OPS CHECK GOOD
- [SDR IPXA2022052582527](https://openairdocs.org/sdr/IPXA2022052582527.md): Cable · broken · May 25, 2022 · N296UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR AFT CABLE BROKE.INSTALLED FWD & AFT LOWER CABLES ON L1 DOOR PER AMM 52-11-03-400-801. OPS CHECK GOOD.
- [SDR IPXA2021101074798](https://openairdocs.org/sdr/IPXA2021101074798.md): Skin · none · Oct 10, 2021 · N296UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/ART AC DOOR SKIN CUTOUT CRACKED.REPAIRED IAW EO MD11-5330-81636
- [SDR IPXA2021091073772](https://openairdocs.org/sdr/IPXA2021091073772.md): Doubler · chafed · Aug 31, 2021 · N296UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:S/VINTERNAL DOUBLER HAS DAMAGED HOLES AND CHAFE DAMAGE BETWEEN STA. 1958 TO 1997 AND BETWEEN L48L TO 50L.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. AGA7167 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2021090973746](https://openairdocs.org/sdr/IPXA2021090973746.md): Shear Tie · corroded · Aug 30, 2021 · N296UP · Doug MD11F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:SVAFT FUSELAGE SHEAR CLIP HAS EXFOLIATED CORROSION AT STA. Y=1996.75 BETWEEN LON 48R AND LON 50RREMOVED,FABRICATED AND REPLACED CORRODED SHEAR CLIP AT STA. Y=1996.75 BETWEEN LON 48R AND 50R IAW SRM 51-35-01 (MINOR)
- [SDR IPXA2021090973749](https://openairdocs.org/sdr/IPXA2021090973749.md): Doubler · damaged · Aug 30, 2021 · N296UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SVAFT FUSELAGE SKIN DOUBLER HAS 3EA ELONGATED HOLES BETWEEN STA.1975-1986 LON 48L-49L.REPAIRED 3EA ELONGATED HOLES AT AFT FUSELAGE SKIN DOUBLER BETWEEN STA.1975-1986 LON 48L-49L IAW VT-SAA EA 011-5330-01-A9341 REV I/R AND UPS EO MD11-5330-81536
- [SDR IPXA2021090983722](https://openairdocs.org/sdr/IPXA2021090983722.md): Tear Strap · damaged · Aug 30, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV, TEAR STRAP AT STA 1921 BETWEEN LONGERONS 50L & 52 IS CREASED.REPAIRED CREASED TEAR STRAP AT STA 1921 BETWEEN LONGERONS 50L & 52 IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021091093758](https://openairdocs.org/sdr/IPXA2021091093758.md): Shear Tie · damaged · Aug 23, 2021 · N296UP · Doug MD11F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:SVAFT FUSELAGE SHEAR TIE HAS AN EXTRA DAMAGE FASTENER HOLE AT STA.1926 BETWEEN LON 51L AND LON 52.REMOVED,FABRICATED AND REPLACED AFT FUSELAGE DAMAGED SHEAR TIE AT STA.1926 BETWEEN LON 51L AND LON 52 IAW SRM 51-33-01 (MINOR).
- [SDR IPXA2021090983720](https://openairdocs.org/sdr/IPXA2021090983720.md): Tear Strap · broken · Aug 23, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SVTEAR STRAP AT STA 1942 BETWEEN LONGERONS 50L & 52 IS BROKEN.REPAIRED BROKEN TEAR STRAP AT STA 1942 BETWEEN LONGERONS 50L & 52 IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)
- [SDR IPXA2021091373852](https://openairdocs.org/sdr/IPXA2021091373852.md): Bulkhead Web · deflection · Aug 20, 2021 · N296UP · Doug MD11F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:S/VAFT PRESSURE BULKHEAD WEB HAS DEFLECTION DAMAGE COMMON TO AN EXISTING REPAIR AT STA. 2007 AND BETWEEN X= -10 TO X=10.REPAIRED DAMAGED AFT PRESSURE BULKHEAD WEB AT STA. 2007 AND BETWEEN X= -10 TO X=10 IAW VT-SAA EA 011-5310-01-A9340 REV. I/R
- [SDR IPXA2021091373848](https://openairdocs.org/sdr/IPXA2021091373848.md): Doubler · chafed · Aug 19, 2021 · N296UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:S/VAFT FUSELAGE INTERNAL PRODUCTION DOUBLER HAS CHAFE DAMGE BETWEEN STA. 2007 TO 2033 AND BETWEEN LONG. 45L TO 45R.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. AJC7207 AND SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021091373849](https://openairdocs.org/sdr/IPXA2021091373849.md): Filler · chafed · Aug 19, 2021 · N296UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:S/VAFT FUSELAGE SKIN FILLER HAS CHAFE DAMAGE AT STA. 2007 AND BETWEEN LONG. 45L TO 45R.REMOVED, FABRICATED AND REPLACED FILLER IAW DWG. AJC7204 AND SRM 51-33-001 & 51-35-01. (MINOR)
- [SDR IPXA2021090973752](https://openairdocs.org/sdr/IPXA2021090973752.md): Shear Tie · damaged · Aug 19, 2021 · N296UP · Doug MD11F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:SVAFT FUSELAGE SHEAR CLIP DAMAGE AT STA. Y=1942.00 BETWEEN LON 51L AND LON 52L.REPAIRED AFT FUSELAGE DAMAGED SHEAR CLIP AT STA. Y=1942.00 BETWEEN LON 51L AND LON 52L IAW SRM 53-00-06 REPAIR 1 FIG 201 REV 68 (MAJOR)
- [SDR IPXA2021090273454](https://openairdocs.org/sdr/IPXA2021090273454.md): Longeron · damaged · Aug 19, 2021 · N296UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SVAFT CARGO COMPARTMENT LON 51L HAS CHAFE DAMAGE BETWEEN STA.1937.50 TO STA.1959.REPAIRED CHAFED LON 51L BETWEEN STA.1937.50 TO 1959 IAW VT-SAA EA 011-5310-01-A9316 REV I/R AND UPS EO MD11-5310-81418-A (MINOR).
- [SDR IPXA2021071371625](https://openairdocs.org/sdr/IPXA2021071371625.md): Former · cracked · Jul 2, 2021 · N296UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:2CRT WING FIXED L/E FORMER AT XOS 912 IS CRACKED.REMOVED AND REPLACED CRACKED RT WING FIXED L/E FORMER AT XOS 912 IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021071371624](https://openairdocs.org/sdr/IPXA2021071371624.md): Tee Fitting · cracked · Jul 1, 2021 · N296UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:2CRT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021070971464](https://openairdocs.org/sdr/IPXA2021070971464.md): Doubler · cracked · Jul 1, 2021 · N296UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:2CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA. XOS. 906.5607.REMOVED AND REPLACED CRACKED R/H WING FIXED L/E LOWER STRINGER REPAIR DOUBLER AT STA. XOS. 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021071371623](https://openairdocs.org/sdr/IPXA2021071371623.md): Doubler · cracked · Jun 30, 2021 · N296UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CRT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 906.561 IS CRACKED.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 906.561 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021071471673](https://openairdocs.org/sdr/IPXA2021071471673.md): Floorbeam · cracked · Jun 29, 2021 · N296UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:2CFWD LOWER CARGO FLOOR BEAM AT STA 6-70 & X= 57.50 IS CRACKED.REPAIRED CRACKED FWD LOWER CARGO FLOOR BEAM AT STA 6-70 & X= 57.50 IAW VT-SAA EA 011-5340-01-A9215 REV. IR AND UPS EO MD11-5310-80984-A. REF. FAA FORM 8100-9 SIGNED BY: STEPHEN KANG
- [SDR IPXA2021071071498](https://openairdocs.org/sdr/IPXA2021071071498.md): Floorbeam · cracked · Jun 29, 2021 · N296UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:2CFORWARD CARGO COMPARTMENT FLOOR BEAM CRACK AT STA.Y= 6-70,X= -57.5 AND Z= -98.REPAIRED CRACKED FWD CARGO COMPT FLOOR BEAM IAW SRM 53-40-51,REPAIR 1,FIG 202,REV 67
- [SDR IPXA2021070971463](https://openairdocs.org/sdr/IPXA2021070971463.md): Stringer · cracked · Jun 28, 2021 · N296UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 908.REPAIRED CRACKED R/H WING FIXED L/E UPPER STRINGER BETWEEN STA. XOS. 901.5 TO 912.0 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)
- [SDR IPXA2021071071499](https://openairdocs.org/sdr/IPXA2021071071499.md): Floor Panel · delaminated · Jun 25, 2021 · N296UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CAVIONICS COMPARTMENT FLOOR PANEL DELAMINATED AT AFT CENTER.REMOVED,FABRICATED AND REPLACED AVI COMPT DELAMINATED FLOOR PANEL IAW VT-SAA EA 011-5330-01-A9207 REV I/R AND UPS EO MD11-5330-80933-A (MAJOR).
- [SDR IPXA2021070971462](https://openairdocs.org/sdr/IPXA2021070971462.md): Stringer · cracked · Jun 24, 2021 · N296UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:2CCENTER WING BOX STRINGER #49 IS CRACKED AT STA. XCW= 17.0.REPAIRED CRACKED CENTER WING BOX STRINGER #49 BETWEEN STA. XCW= 3 TO XCW= 32 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021070971460](https://openairdocs.org/sdr/IPXA2021070971460.md): Stringer · cracked · Jun 24, 2021 · N296UP · Doug MD11F · Wing Main, Frame Structure
  > INSPECTION TYPE:2CCENTER WING BOX STRINGER # 50 IS CRACKED AT STA. XCW -17.REPAIRED CRACKED CENTER WING BOX STRINGER #50 BETWEEN STA. XCW= -5.0 TO 29.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)
- [SDR IPXA2021071471668](https://openairdocs.org/sdr/IPXA2021071471668.md): Ventilator Panel · cracked · Jun 23, 2021 · N296UP · Doug MD11F · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:2C#1 PYLON PANEL 437CR VENTILATOR ASSY IS CRACKED.REPAIRED CRACKED #1 PYLON VENTILATOR ASSY IAW VT-SAA EA 011-5430-01-A9223 REV. IR AND UPS EO MD11-5460-80982-A. REF. FAA FORM 8100-9 SIGNED BY: STEPHEN KANG (AR-605677) DATED 07/12/2021. (MAJOR)
- [SDR IPXA2021071371622](https://openairdocs.org/sdr/IPXA2021071371622.md): Stiffener · corroded · Jun 23, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CAFT AVI COMPT VERTICAL STIFFENER AT STA 470 BULKHEAD BELOW SERVICE DOOR IS CORRODED.REMOVED AND REPLACED CORRODED AFT AVI COMPT VERTICAL STIFFENER AT STA 470 BULKHEAD BELOW SERVICE DOOR IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021070971484](https://openairdocs.org/sdr/IPXA2021070971484.md): Floor Panel · corroded · Jun 23, 2021 · N296UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION TYPE:2CFLOOR PANEL WSP0785-501 HAS CORROSION AT POS 4 BETWEEN STA.475-500 AND X=19 TO X=27.REPAIRED CORRODED FLOOR PANEL IAW VT-SAA EA 011-5310-01-A9206 REV I/R AND UPS EO MD11-5310-80887-A (MINOR).
- [SDR IPXA2021070671320](https://openairdocs.org/sdr/IPXA2021070671320.md): Floorbeam · corroded · Jun 23, 2021 · N296UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:2CFWD MAIN CABIN LAV FLOOR SUPPORT HAS HEAVY CORROSION AT STA Y=421.578 BETWEEN X=-65 & X=-81.REMOVED,FABRICATED AND REPLACED CORRODED FLOOR SUPPORT IAW SRM 51-31-01 (MINOR).
- [SDR IPXA2021063071149](https://openairdocs.org/sdr/IPXA2021063071149.md): Doubler · chafed · Jun 23, 2021 · N296UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:2CTAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER IS CHAFED.REPAIRED CHAFED TAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-B APPENDIX A. (MINOR)
- [SDR IPXA2021071671767](https://openairdocs.org/sdr/IPXA2021071671767.md): Flap · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Trailing Edge Flap Control System
  > INSPECTION TYPE:2CRT WING O/B FLAP I/B AFT HINGE INTERNAL FITTING HAS A 3" CRACK.REMOVED AND REPLACED CRACKED RT WING FLAP ASSY IAW AMM 27-50-30. (MINOR)
- [SDR IPXA2021071371637](https://openairdocs.org/sdr/IPXA2021071371637.md): Skin · corroded · Jun 22, 2021 · N296UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2C, RT WING UPPER SURFACE BETWEEN XORS 97 - XORS 130.4 AND BETWEEN STRINGER 11 & 15 IS CORRODED AROUND FASTENERS.REPAIRED CORRODED RT WING UPPER SURFACE BETWEEN XORS 97 - XORS 130.4 AND STRINGER 11 & 15 IAW EA 011-5730-01-A9216 REV. IR AND UPS
- [SDR IPXA2021071371621](https://openairdocs.org/sdr/IPXA2021071371621.md): Frame Angle · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:2CCENTER CARGO FRAME ANGLE AT STA 1541 AND LONGERON 41L IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO FRAME ANGLE AT STA 1541 AND LONGERON 41L IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021071371620](https://openairdocs.org/sdr/IPXA2021071371620.md): Frame Angle · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:2CCENTER CARGO FRAME ANGLE AT STA 5-113 AND LONGERON 41L IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO FRAME ANGLE AT STA 5-113 AND LONGERON 41L IAW SRM 51-33-01 & 51-35-01. (MINOR)
- [SDR IPXA2021070971481](https://openairdocs.org/sdr/IPXA2021070971481.md): Stiffener · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 STRINGER 46R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR).
- [SDR IPXA2021070871403](https://openairdocs.org/sdr/IPXA2021070871403.md): Skin · corroded · Jun 22, 2021 · N296UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:2CRT WING UPPER SURFACE T/E SKIN CORRODED BETWEEN XORS =779.5-XORS =819.5.REPAIRED CORRODED RT WING UPPER T/E SKIN IAW EA 011-5730-01-A9221 REV I/R AND UPS EO MD11-5710-80892-A (MINOR).
- [SDR IPXA2021070671322](https://openairdocs.org/sdr/IPXA2021070671322.md): Support Angle · corroded · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CAFT CARGO STEP UP BULKHEAD SUPPORT ANGLE CORRODED AT STA.1841 BETWEEN STR 43L &STR 43R.REPAIRED CORRODED SUPPORT ANGLE IAW VT-SAA EA 011-5100-01-A9205 REV I/R AND UPS EO MD11-5100-80871-A (MINOR).
- [SDR IPXA2021070171200](https://openairdocs.org/sdr/IPXA2021070171200.md): Rib · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:2CRH MLG W/W CUT-OUT RIB CRACK AT FWD O/B JAMB.REMOVED,FABRICATED AND REPLACED CRACKED RIB IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2021070171186](https://openairdocs.org/sdr/IPXA2021070171186.md): Stiffener · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CAFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 49R IS CRACKED.REMOVED AND REPLACED CRACKED AFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 49R IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2021070171185](https://openairdocs.org/sdr/IPXA2021070171185.md): Stiffener · cracked · Jun 22, 2021 · N296UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CAFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 47R IS CRACKED.REMOVED AND REPLACED CRACKED AFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 47R IAW SRM 51-33-01. (MINOR)

Next page: https://openairdocs.org/deregistered/N296UP-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 = 'N296UP' AND deregistration_id = 'N296UP-2023-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N296UP-2023-12-18/reports

---
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