# Service difficulty reports: N281UP

A list on [N281UP](https://openairdocs.org/aircraft/N281UP.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 · 277 reports

- [SDR IPXA2023110167359](https://openairdocs.org/sdr/IPXA2023110167359.md): Unknown · unknown · Nov 1, 2023 · N281UP · Doug MD11F · Service Doors
  > R1 DOOR PNEUMATIC DOOR ASSIST BOTTLE PRESSURE BELOW GREEN GAUGE. SERVICED R1 DOOR ASSIST BOTTLE AS REQ, LEAK CKS OK. REF AMM 12-25-04 THIS CLEARS DMI 2802094 DMP REVERSED.
- [SDR IPXA2023092094216](https://openairdocs.org/sdr/IPXA2023092094216.md): Gauge · out of position · Sep 20, 2023 · N281UP · Doug MD11F · Emergency Equipment
  > BOTH L&R SLIDE INFLATION CYLINDER GAUGES ON CABIN DOORS NOT VISABLE FROM CABIN. TRANSFER TO M812572 PER MEL 52-10-3-1-2-2 PLACARD INSTALLEDR&R L1&R1 FWD ENTRY DOOR SLIDE ESCAPES REF MD-11 AMM 25-61-15. THIS CLEARS DEFERRAL M812572, PLACARD REMOVED.
- [SDR IPXA2023081893953](https://openairdocs.org/sdr/IPXA2023081893953.md): Light · no test · Aug 17, 2023 · N281UP · Doug MD11F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FAIL TEST. "MAIN BAT 1 LO". DEFERRED PER MEL 33-50-4 C/W DMP 33-50-4. R&R EMERGENCY BATTERY SUPPLY IAW AMM 33-51-01 REVERSED DMP 33-50-4 OF CHECK GOOD REMOVED PLACARD THIS CLEARS M811555 MD11 IPC 33-51-01-05
- [SDR IPXA2023071093635](https://openairdocs.org/sdr/IPXA2023071093635.md): Bottle · low · Jul 9, 2023 · N281UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAR1 DOOR PNEUMATIC BOTTLE IS LOW.SERVICED R1 PNEUMATIC STORAGE BOTTLE IAW MD11 AMM 12-25-04.
- [SDR IPXA2023063093550](https://openairdocs.org/sdr/IPXA2023063093550.md): Door · inoperative · Jun 29, 2023 · N281UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAWHEN OPENING L1 DOOR SOMETHING. SOME THING IS LITTING AND MAKING A WAS NOISE *DOES NOT MEET SDR CRITERIA*READJUSTED MAIN PAX DOOR. IAW AMM 25-23-07 NO FAULT AT THIS TIME
- [SDR IPXA2023060193355](https://openairdocs.org/sdr/IPXA2023060193355.md): Door · inoperative · Jun 1, 2023 · N281UP · Doug MD11F · Passenger/Crew Doors
  > LEFT MAIN ENTRY DOOR WILL NOT OPEN ELECTRICALLY FROM EITHER SIDE. DEFERRED LEFT MED IAW MEL 52-10-3-1-2-1-2. R/R L1 FWD PASS DOOR LOCK PIN RELEASE SOLENOID PER AMM 52-10-06. OPS CHECK GOOD REF AMM 52-11-02. THIS CLEARS M809103. PLACARD REMOVED. IPC 52-11-07.
- [SDR IPXA2022110387808](https://openairdocs.org/sdr/IPXA2022110387808.md): Accumulator · discharged · Nov 3, 2022 · N281UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR PNEUMATICALLY OPENED BY CREW, DOOR RESERT AND DOOR ACCUMULATOR SERVICED PER MD11 AMM 52-10-01-201 AND 12-25-04-600-801.
- [SDR IPXA2022102687539](https://openairdocs.org/sdr/IPXA2022102687539.md): Cable · broken · Oct 26, 2022 · N281UP · Doug MD11F · Service Doors
  > R 1 DOOR FWD CABLE BROKEN/OFF OF DRUM. R1 DOOR. R/R R1 FWD LOWERING CABLE PER AMM 52-11-03. OPS CHECK GOOD PER AMM 52-11-02.
- [SDR IPXA2022081685312](https://openairdocs.org/sdr/IPXA2022081685312.md): Solenoid · inoperative · Aug 16, 2022 · N281UP · Doug MD11F · Service Doors
  > R1 DOOR INOP. R/R PASS DOOR LOCK PIN RELEASE SOLENOID REF AMM 52-10-06 PB 401. R/R R1 CLOSE-LIMIT SWITCH REF AMM 52-11-02 PB 501 830-805. DOOR OPERATES NORMALLY.
- [SDR IPXA2022042581451](https://openairdocs.org/sdr/IPXA2022042581451.md): Longeron · corroded · Apr 12, 2022 · N281UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:1CCENTER CARGO COMPARTMENT AFT INTERMEDIATE FUSELASE LON 51L CORRODED BETWEEN STA. 1701 AND STA, 1721.REPAIRED CORRODED LONGERON 51L BETWEEN STA. 1701 AND STA. 1721 IAW VT-SAA EA 011-5310-01-A9542 REV I/R AND UPS EO MD11-5310-83450-A BY P.LAU (
- [SDR IPXA2022042181353](https://openairdocs.org/sdr/IPXA2022042181353.md): Splice · cracked · Apr 8, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CFOUND LONGERON 49R PRODUCTION SPLICE FITTING CRACKED BETWEEN STA 5-113 AND 1541.REPLACED PRODUCTION SPLICE P/N A5A7114-511 IAW MD11 SRM 51-31-01. (MINOR)
- [SDR IPXA2022042581436](https://openairdocs.org/sdr/IPXA2022042581436.md): Longeron · corroded · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:2CCENTER CARGO LONGERON 49R HAS CORROSION AT STA. 5-93/1541.REPAIRED CORRODED CENTER CARGO LONGERON 49R BETWEEN STA. 5-103 TO 5-123 IAW VT-SAA EA 011-5310-01-A9540 REV. I/R AND UPS EO MD11-5310-83411-A. (MAJOR) REF FAA FORM 8100-9 BY. S. KANG (
- [SDR IPXA2022042181352](https://openairdocs.org/sdr/IPXA2022042181352.md): Longeron · corroded · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CEXTERIOR FUSELAGE LONGERON 28R P/N AEA7545-2 HAS CORROSION BETWEEN STA Y=1207 - Y=1305.5.REPAIRED CORRODED LONGERON 28R P/N AEA7545-2 IAW EA 011-5300-01-A9541 REV I/R AND UPS EO MD11-5310-83430-A (MINOR)
- [SDR IPXA2022042081326](https://openairdocs.org/sdr/IPXA2022042081326.md): Stiffener · cracked · Apr 6, 2022 · N281UP · Doug MD11F · Aerodynamic Fairings
  > INSPECTION TYPE:4CLOWER FUSELAGE R/H WING TO BODY HAS A STIFFENER P/N AYB7104-526 WITH A CRACK AT STA 1298.REMOVED,FAB AND REPLACED THE CRACK STIFFENER P/N AYB7104-526 IAW DWG AYB7104 AND MD11 SRM 51-33-01. (MINOR)
- [SDR IPXA2022041881255](https://openairdocs.org/sdr/IPXA2022041881255.md): Stiffener · cracked · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:1CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 LON 49R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-33-01 AND 51-35-01 (MINOR).
- [SDR IPXA2022041681208](https://openairdocs.org/sdr/IPXA2022041681208.md): Stiffener · cracked · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-11 HAS A CRACK AT STA 1841.REMOVED, FAB AND REPAIRED THE CRACKED STIFFENER P/N AGA7170-11 IAW MD11 51-31-01 AND 51-35-01 (MINOR)
- [SDR IPXA2022041681207](https://openairdocs.org/sdr/IPXA2022041681207.md): Stiffener · cracked · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-9 THAT IS CRACKED AT STA 1841.REMOVED,FAB AND REPLACED THE CRACKED STIFFENER P/N AGA7170-9 IAW MD11 SRM 51-31-01 AND 51-35-01 (MINOR)
- [SDR IPXA2022041681206](https://openairdocs.org/sdr/IPXA2022041681206.md): Longeron · corroded · Apr 6, 2022 · N281UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:4CEXTERIOR FUSELAGE, LONGERON 28L P/N AEA7545-1 HAS CORROSION BETWEEN STA 1304-1309.REPAIRED CORRODED LONGERON 28L P/N AEA7545-1 IAW EA 011-5300-01-A9539 I/R AND UPS EO MD11-5310-83429-A (MINOR)
- [SDR IPXA2022041381125](https://openairdocs.org/sdr/IPXA2022041381125.md): Beam · cracked · Apr 6, 2022 · N281UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:2CR-3 DOOR PLUG UPPER HORZ. BEAM IS CRACKED AT THE FWD. END.REMOVED AND REPLACED BEAM IAW SRM 51-31-01 & 51-35-01. (MINOR)
- [SDR IPXA2022042281385](https://openairdocs.org/sdr/IPXA2022042281385.md): Web · cracked · Apr 5, 2022 · N281UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:4CMAIN CARGO R3 DOOR TORQUE BOX LWR AFT WEB IS CRACKED AT STA Y=1313 AND Z=-16.REMOVED, FAB AND REPAIRED CRACKED AFT WEB P/N AEA0112-2 AT STA Y=1313 AND Z=-16 IAW MD11 SRM 53-40-15 FIG 201 REPAIR 3 (MAJOR)
- [SDR IPXA2022042281383](https://openairdocs.org/sdr/IPXA2022042281383.md): Stringer · cracked · Apr 5, 2022 · N281UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:4CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA XOS=906.5607.REMOVED, FAB AND REPLACED CRACK REPAIR DOUBLER AT STA XOS=906.5607 IAW MD11 SRM 57-40-03 FIG 201 REPAIR 1 (MAJOR)
- [SDR IPXA2022042281392](https://openairdocs.org/sdr/IPXA2022042281392.md): Brace · cracked · Apr 5, 2022 · N281UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:4CL/H WING T/E REAR SPAR HAS A BRACE THAT IS CRACKED.REMOVED,FAB REPLACED THE CRACKED BRACE IAW MD11 DWG ARC0295 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2022041981297](https://openairdocs.org/sdr/IPXA2022041981297.md): None · cracked · Apr 5, 2022 · N281UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:4CR/H I/B FLAP I/B TRACK THE 2ND FITTING FROM THE BOTTOM IS CRACKED.REMOVED, REPLACED R/H I/B FLAP ASSY P/N NRC6055-508 IAW MD11 AMM 27-50-20-400-801 (MINOR)
- [SDR IPXA2022041581180](https://openairdocs.org/sdr/IPXA2022041581180.md): Doubler · cracked · Apr 5, 2022 · N281UP · Doug MD11F · Leading Edge Devices
  > INSPECTION TYPE:C4R/H O/B WING FIXED LEADING EGDE BEADED DOUBLER IS CRACKED AT STA XOS=661.7 -XOS=667.62.REMOVED, FAB AND REPAIRED THE CRACK BEADED DOUBLER AT STA XOS=661.7 - XOS=667.62 IAW DWG ARB2893-2 AND MD11 SRM 57-40-02 REPAIR 15, FIG 205 REV 68.01 (MAJ
- [SDR IPXA2022041581179](https://openairdocs.org/sdr/IPXA2022041581179.md): Floor Panel · corroded · Apr 5, 2022 · N281UP · Doug MD11F · Passenger Compartment Equipment
  > INSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0788-502 AT STA Y=475.0 - Y=503.175 AND X=-36.000 - X=-47.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL WSP0788-502 IAW DWG WSP0788 AND DWG SP11530078, SRM 51-31-01 (MINOR)
- [SDR IPXA2022042281387](https://openairdocs.org/sdr/IPXA2022042281387.md): Skin · damaged · Apr 4, 2022 · N281UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:4CCENTER FUSELAGE LOWER SKIN PANEL HAS EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L.REMOVED, REPAIRED EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L IAW VTSAA EA 011-5340-01-A9535 REV I/R AND UPS EO MD11-5330-83452-A FAA FORM 810
- [SDR IPXA2022041581177](https://openairdocs.org/sdr/IPXA2022041581177.md): Floor Panel · corroded · Apr 3, 2022 · N281UP · Doug MD11F · Passenger Compartment Equipment
  > INSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0786-501 AT STA Y=475.0 -Y=503.175 AND X=-17.000 - X=-27.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL IAW DWG WSP0786 AND DWG SP11530078, SRM 51-31-01 (MINOR)
- [SDR IPXA2022041181076](https://openairdocs.org/sdr/IPXA2022041181076.md): Stiffener · cracked · Apr 3, 2022 · N281UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:2CR/H MLG W/W 3RD STIFFNER AT O/B WEB IS CRACKED.REMOVED AND REPLACED STIFFNER IAW SRM 51-35-01. (MINOR)
- [SDR IPXA2021081872893](https://openairdocs.org/sdr/IPXA2021081872893.md): Status Message · illuminated · Aug 18, 2021 · N281UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE:N/ALEVEL 1 EMER LT BAT 1 LO MESSAGE DISPLAYEDR&R #1 EMER LT BAT IAW MD 11 AMM 33-51-01. PERFORMED OPS CHECK IAW AMM 33-51-01-700-802. BATTERY TEST PASSED
- [SDR IPXA2021072672071](https://openairdocs.org/sdr/IPXA2021072672071.md): Actuator · inoperative · Jul 25, 2021 · N281UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AWHILE RIGGING L1 DOOR ELEC. DOOR ACT BRAKE NOT HOLDING DOOR IN CUTOUT.R&R L1 DOOR ELEC ACTUATOR PER MM 52-11-01-400-801, L1 DOOR OPS CK GOOD.
- [SDR IPXA2021011464423](https://openairdocs.org/sdr/IPXA2021011464423.md): Cable · detached · Jan 13, 2021 · N281UP · Doug MD11F · Passenger/Crew Doors
  > L DOOR, CABLE CAME OFF TRACK. DEFERRED L1 DOOR. INSTALLED L/H AFD TOP CABLES PER 52-11-03. OPS TES GOOD.
- [SDR IPXA2021011464437](https://openairdocs.org/sdr/IPXA2021011464437.md): Indication Sys · inoperative · Jan 13, 2021 · N281UP · Doug MD11F · Emergency Equipment
  > L1 DOOR ALERT SYSTEM INOP. NEEDS BRACKET REPLACED TO SWITCH. EAD DOOR OPEN ALERT SYSTEM DEFERRED REF MD11 MEL 52-40-1-1-0-1 ITEM PLACARDED.REPLACED CLOSED SENSOR TARGET. OPS TEST GOOD REF 52-70-04. M732653 CLEARED. PLACARD REMOVED.
- [SDR IPXA2021012264765](https://openairdocs.org/sdr/IPXA2021012264765.md): Outflow Valve · malfunctioned · Jan 2, 2021 · N281UP · Doug MD11F · Pressure Regulator/Outflow Valve
  > INSPECTION TYPE: NA ATB EMERGENCY DECLARED, NO EQUIP USED- LANDING UNEVENTFUL. DURING CLIMB OUT ZTIME GOT LEVEL 1 CABIN RATE MESSAGE APPROXIMATELY 12000' MESSAGE NOTICED CAB ALT 8000 FT CLIMBING REQUIRED LEVEL OFF AT 17500 FT CAB ALT ABOVE 1000 MAX CABIN ALT
- [SDR IPXA2020122663810](https://openairdocs.org/sdr/IPXA2020122663810.md): Control Switch · failed · Dec 26, 2020 · N281UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE: N/A, SUPPLEMENTAL SDR, EMERGENCY LIGHTS WILL NOT ILLUMINATE. DEFERRED EMERGENCY LIGHT SYSTEM, IAW MEL 33-50-4. REPLACED BATTERY SUPPLY FOR T/S PURPOSES, NO HELP, SUSPECT FAULTY SWITCH. PLACARD INSTALLED. DMP C/W. REPLACED RELAY R2-5700 E
- [SDR IPXA2020111862525](https://openairdocs.org/sdr/IPXA2020111862525.md): Sign · loose · Nov 18, 2020 · N281UP · Doug MD11F · Emergency Lighting
  > INSPECTION TYPE: N/A 1R EXIT DOOR SIGN LOOSE. INSTALLED 1R EMERGENCY EXIT IDENTIFIER SIGN, IAW AMM 33 52 05. OPERATIONS CHECK GOOD.
- [SDR IPXA2020101961444](https://openairdocs.org/sdr/IPXA2020101961444.md): Computer · malfunctioned · Oct 17, 2020 · N281UP · Doug MD11F · Autopilot System
  > INSPECTION TYPE: N/A ATB, NO EMERGENCY DECLARED. LANDED UNEVENTFUL. AT LEVEL 2 FCC 2B DATA FAULT AT CRUISE FL 360 LEVEL SEL YAW UPR AA OFF LEVEL 1 LSAS LOB OFF. R & R FCC 2, PER AMM 22-01-03. PERFORMED AUTO FLIGHT SYSTEM CATT111B FCC-2 RTS, REF AMM 22-00-0
- [SDR IPXA2020071097588](https://openairdocs.org/sdr/IPXA2020071097588.md): Fitting · worn · Jul 9, 2020 · N281UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:3CLH I/B ELEVATOR O/B CAM FITTING IS WORN. REMOVED,REPAIRED AND INSTALLED LH I/B ELEVATOR O/B CAM FITTING IAW EA #011-5520-01-A8384 I/R AND UPS EO # MD11-5520-77027-A. (MINOR)
- [SDR IPXA2020071097587](https://openairdocs.org/sdr/IPXA2020071097587.md): Fitting · worn · Jul 9, 2020 · N281UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:3CLH O/B ELEVATOR CAM FITTING I/B OF #7 BEARING IS WORN.REMOVED,REPAIRED AND INSTALLED LH O/B ELEVATOR CAM FITTING I/B OF #7 BEARING IAW VT SAA EA #011-5520-01-A8384 I/R AND UPS EO #MD11-5520-77027-A. (MINOR)
- [SDR IPXA2020071097586](https://openairdocs.org/sdr/IPXA2020071097586.md): Fitting · worn · Jul 9, 2020 · N281UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE:3CR/H DETACHABLE ELEVATOR O/B CAM FITTING IS WORN.REMOVED,REPAIRED AND INSTALLED RH DETACHABLE ELEVATOR O/B CAM FITTING IAW EA #011-5520-01A8384 I/R AND UPS EO #MD11-5520-77027-A. (MINOR)
- [SDR IPXA2020070957584](https://openairdocs.org/sdr/IPXA2020070957584.md): Fitting · worn · Jul 9, 2020 · N281UP · Doug MD11F · Ailerons
  > INSPECTION TYPE:3CL/H DETACHABLE ELEV I/B CAM FITTING IS WORN.REMOVED,REPAIRED AND INSTALLED LH DETACHABLE ELEV I/B CAM FITTING IAW EA #011-5520-01-A8384 I/R AND UPS EO # MD11-5520-77027-A. (MINOR)
- [SDR IPXA2020071097582](https://openairdocs.org/sdr/IPXA2020071097582.md): Fitting · worn · Jul 9, 2020 · N281UP · Doug MD11F · Elevator Control System
  > INSPECTION TYPE:3CR/H I/B ELEVATOR O/B CAM FITTING IS WORNREMOVED,REPAIRED AND INSTALLED WORN RH I/B ELEV O/B CAM FITTING IAW VT SAA EA # 011-5520-01-A8384 I/R AND UPS EO MD11-5520-77027-A. (MINOR)
- [SDR IPXA2020071097591](https://openairdocs.org/sdr/IPXA2020071097591.md): Skin · corroded · Jul 9, 2020 · N281UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3C. LT WING UPPER CENTER SKIN CORRODED BETWEEN STA. XORS 514 TO XORS 521 ABOVE STRINGER 10.REPAIRED CORRODED LH WING UPPER CENTER SKIN BET. STA. XORS 514 TO XORS 521 ABOVE STRINGER 10 IAW VT SAA EA #011-5730-01-A8397 I/R AND UPS EO #MD11-5730-
- [SDR IPXA2020070357287](https://openairdocs.org/sdr/IPXA2020070357287.md): Skin Panel · cracked · Jul 3, 2020 · N281UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3C RT WING SKIN FUEL ACCESS PANEL 636AB 9EA FASTENER HOLES CRACKED. REPAIRED CRACKED RT WING SKIN ACCESS PANEL 636AB 9EA FASTENER HOLES IAW SRM 57-20-02 REPAIR 5. (MINOR)
- [SDR IPXA2020070357286](https://openairdocs.org/sdr/IPXA2020070357286.md): Skin Panel · cracked · Jul 3, 2020 · N281UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3C LT WING SKIN FUEL ACCESS PANEL 536AB 9EA FASTENER HOLES CRACK. REPAIRED LT WING SKIN FUEL ACCESS PANEL 536AB 9EA FASTENER HOLES IAW SRM 57-20-02 REPAIR 5 (MINOR).
- [SDR IPXA2020071317648](https://openairdocs.org/sdr/IPXA2020071317648.md): Longeron Splice · cracked · Jun 28, 2020 · N281UP · Doug MD11F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:3C, MAIN CABIN LONGERON 6R SPLICE AT BS 1531/5-123 IS CRACKED.REMOVED AND REPLACED MAIN CABIN CRACKED LONGERON 6R SPLICE AT BS 1531/5-123 IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2020071557815](https://openairdocs.org/sdr/IPXA2020071557815.md): Angle · cracked · Jun 25, 2020 · N281UP · Doug MD11F · Wing Miscellaneous Structure
  > INSPECTION TYPE:3C RT WING T/E ABOVE PANEL 641JB, VERTICAL STIFFNER ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED TEE ANGLE IAW DWG ARC0472 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2020071457783](https://openairdocs.org/sdr/IPXA2020071457783.md): Support Bracket · cracked · Jun 25, 2020 · N281UP · Doug MD11F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:3C **SUPPLEMENTAL SDR** NR 1 PYLON "V" RIB SUPPORT BRACKET IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT BRACKET IAW DWG AUB7517 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2020071317647](https://openairdocs.org/sdr/IPXA2020071317647.md): Hinge Fitting · worn · Jun 25, 2020 · N281UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CRT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG BUSHING IS LOOSE.REPAIRED RT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG WORN BUSHING BORE IAW VT-SAA EA 011-5740-01-A8394 REV. IR AND UPS EO MD11-5740-77054-A. (MINOR)
- [SDR IPXA2020070657409](https://openairdocs.org/sdr/IPXA2020070657409.md): Skin · corroded · Jun 25, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)
- [SDR IPXA2020070657407](https://openairdocs.org/sdr/IPXA2020070657407.md): Skin · corroded · Jun 25, 2020 · N281UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3C EXTERIOR FUSELAGE HAS CORROSION BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)

Next page: https://openairdocs.org/aircraft/N281UP/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 = 'N281UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N281UP/reports

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