N254UP

Service difficulty reports · 345

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N254UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2025080145238Proximity Sensor · faultedDESCENDING THROUGH 17000 W/SPEED EXTENDED, THE RIGHT GEAR HANDLE RED WARNING LIGHT CAME ON,AND STAYED ON. RE-ADJUSTED RH MLG GEAR UP AND DOOR LATCHED PROXIMITY SENSOR IAW AMM 32-61-15. PERFORMED BITE TEST IAW AMM 32-61-15-741-802. TEST GOOD.Aug 1, 2025 · N254UP · Doug MD11F · Landing Gear Position and WarningSDR IPXA2025070795201Skin · crackedLEFT WING / FOUND CRACKED LE SKIN AT SLAT TRACK #14. 040-28 , ATA 51-00.HFEC SURFACE INSP. (ASST.#20-1204, CAL. DUE: 12/11/25) OF LH WING LE SKIN AT SLAT TRACK #14 CUTOUT PER NDT SPM 06-10-01.001. CRACK DETECTED AT IB EDGE OF TRACK CUTOUT TO NEAR EDGE AFT.FABRJun 24, 2025 · N254UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2025070534130Fuel Tank · corrodedFOUND CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA 1239 XCW=-81.00 ATA 53-10.REMOVED 6EA FASTENERS AND REMOVED CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA. 1239 XCW=-81.00 PER MD11 SRM 57-10-01-1A-1 FIG. 101. ACCOMPLISHED ON E.A.# 011-5730-01-B0525 REV. PJun 20, 2025 · N254UP · Doug MD11F · Fuel StorageSDR IPXA2025070734130Fuel Tank · corrodedFOUND CORROSION AT FUEL TANK UPPER SKIN M. CABIN STA 1239 XCW=-81.00 ATA 53-10 VERIFIED STEP 27 VERIFIED REPAIR ACCOMPLISHED IN ACCORDANCE WITH EO-94206-REQ1 AND VT-SAA EA 011-5730-01-B0525 REV IRJun 20, 2025 · N254UP · Doug MD11F · Fuel StorageSDR IPXA2025070873830Doubler · crackedRIGHT WING LE COVE HAS A CRACKED BEADED DOUBLER AT APPROX XOS=740.8 TO XOS=734.75 49-075. CUT OUT DAMAGED BEADED DOUBLER AT RH WING LE AT APPROX STA XORS 633 IAW MD-11 SRM 57-40-02-2R-15 REPAIR 15 DIMENSIONS CUT OUT 12.25" X 6.2".LOCATED AND DRILLED BEADED DOJun 17, 2025 · N254UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2025070771804Seat Track · crackedMAIN CARGO SEAT TRACK CRACKED AT BOTTOM SIDE VEIWED FROM CENTER CARGO STA 1681 LBL 8.5. FABRICATED 2 EA SEAT TRACK SPLICES REPAIR REF SRM 53-00-52-2R-1.FABRICATED 2EA REPAIR SPLICE PLATES REF SRM 53-00-52-2R-1. INSTALLED EWIS AT MAIN CARGO STA 1681 LBL8.5 REJun 17, 2025 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025070751852Longeron Splice · corrodedCORROSION FOUND AT CENTER CARGO BLIGE AREA RH LONGERON 48 SPLICE BETWEEN STA 5-53 TO 5-73. REMOVED DAMAGE SPLICE FROM CTR CGO BLIGE AREA RH LONGERON 48 BETWEEN STA 5-53 TO 5-73 IAW SRM 51-33-01. FABRICATED SPLICE PN AEA7653-1SAAU FOR LONGERON 48 RT CTR CARGOJun 16, 2025 · N254UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2025070742098Beam · crackedRIGHT OVER WING DOOR HAS A CRACK BEAM P/N ADA3750-1. REMOVED THE DAMAGED DOOR BEAM ON R-3 OVERWING DOOR REF SRM 51-33-01-0G-0 AND SRM 51-35-01-0G-0.FABRICATED BEAM EA011-5212-01-B0519-1 FOR RT WING DOOR, PLATE WITH 10% PART THICKNESS IN ALL DIRECTIONS WHILE Jun 16, 2025 · N254UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2025070835259Intercostal · crackedSTR- RH A/C BAY HAS A CRACKED INTERCOSTAL JUST AFT OF A/C BAY DOOR APPROX STRINGER S31. <BR>49-032 ATA 53-00.REMOVED INTERCOSTAL AT A/C R/H COMP APPROX STRINGER S31 REF MD11 SRM 51-35-01 AND 51-33-01.FABRICATED INERCOSTAL WEB PN ACA3804-27SAAU FOR RH AC BAY DOJun 15, 2025 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2025040275223Stick Shaker · inoperative**ATB** CAPT/S STICK SHAKER, PLI SHOWING STALL FO STICK SHAKER PLI NORMAL. REMOVED AND REPLACED #1 AOA VANE PER AMM 27-35-02. OPS CHECK NORMAL.Apr 1, 2025 · N254UP · Doug MD11F · Stall Warning SystemSDR IPXA2025012221486Handle · out of positionL1 EXTERNAL DOOR HANDLE ROTATED TO THE EMERGENCY POSITION BY DE-ICE EMPLOYEE. DOOR IS STUCK IN THE PARTIALLY OPENED POSITION. DOOR HANDLE STUCK IN THE EMERGENCY POSITION. RESET L1 DOOR PNEUMATIC SYSTEM IAW AMM 52-11-04-700-801.<BR>SERVICED L1 DOOR PNEUMATIC BOJan 22, 2025 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024112792263Skin · dentedENTRY DOOR DENT/BENT TOP LEFT APPROX. 2 1/4 IN BY 1 1/4 IN. INSTALLED L1 DOOR IAW AMM 52-11-02. OPS CHECK GOOD. DOOR SLIDE PIN REMOVED AND STOWED.Nov 25, 2024 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024112692263Skin · dentedENTRY DOOR DENT/BENT TOP LEFT APPROX. 2 1/4 IN BY 1 1/4 INNov 25, 2024 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024102909839Battery · no testLOW LVL 1EMERGANCYLT BATTERY LOW WON€™T PASS TEST PERFORMED OPS CHECK PER AMM: 33-51-01, NO FAULTOct 28, 2024 · N254UP · Doug MD11F · Emergency LightingSDR IPXA2024102286629Battery · dischargedLVL1 EMERGENCY LT BAT LOW ON PREFLIGHT R/R EMERGENCY POWER SUPPLY BATTERY REF AMM 33-51-01. OPS CHECK GOOD. REVERSED DMP. REMOVED PLACARD. THIS CLEARS DEFERRAL.Oct 22, 2024 · N254UP · Doug MD11F · Emergency LightingSDR IPXA2024092129171Battery Pack · inoperativeL1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR NOT ILLUMINATING. REMOVED AND REPLACED BATTERY AND LIGHT BULBS IAW AMM 25-61-04. OPS. CHECK GOOD. THIS CLEARS DEFERRAL.PLACARD REMOVED. NO DISABLING DMP APPLIED.Sep 21, 2024 · N254UP · Doug MD11F · Escape SlideSDR IPXA2024091007025Slide · unsecureCREW ENTRY L1 DOOR EVACUATION SLIDE NOT SECURED. COMPLETED L1 EVACUATION SLIDE INSTALL REF AMM 25-62-02-400 THIS CLEARS MEL PLACARD REMOVEDSep 10, 2024 · N254UP · Doug MD11F · Escape SlideSDR 2024F00181Door Frame · crackedUPPER LEFT CORNER AFT PACK NO.3 ACCESS 114AR VISUAL CRACK FOUND APPROX. .75 IN PICS ATTACHED. VERIFIED ALL INSP STEPS COMPLIED WITH ON EO-90589-PRELIM1 RIGHT-SIDE AIR-CONDITIONING DOOR JAMB CORNER SKIN CRACK- PRELIMINARY REPAIR NO. 1Jul 31, 2024 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2024030591110Battery · dischargedEMERG LIGHTS BATT 1 LO R/R EMERG POWER SUPPLY BATTERY PER AMM33-51-01-400-802 OPS CHECKS GOODMar 5, 2024 · N254UP · Doug MD11F · Emergency LightingSDR IPXA2023121528319Unknown · unknown*SDR FILED OPEN* CENTER PIT CEILING DAMAGE, UPPER GILLINER ATTACH ANGLE INBOARD OF THE FWD DOOR ACTUATOR ARM. INSTALLED CTR CARGO COMPT CEILING LINER IAW AMM 25-56-07Dec 15, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023083194060Cover · missingINSPECTION TYPE:NAR1 DOOR EMERGENCY LT COVER MISSING ABOVE GALLEY.INSTALLED GROMMETS AND BEZEL ADDY REF IPC 33-52-55-01-05,20.Aug 30, 2023 · N254UP · Doug MD11F · Emergency LightingSDR IPXA2023071093629Aileron Sys · warning messageINSPECTION TYPE:NA*SDR FILED OPEN* *ATB* EMERGENCY DECLARED* AFT START CONFIGURED ACFT & RCVD LVL 2 AIL DEFLECT DISAG MSG RAN CK LIST & SYS RESET AFT TKOFF MSG RTRND FO SLATED AC WANTED TO ROLL LEFT BUT MAINTAINED ACFT CONTROL RAN CK LIST AND LIGHT REMAINED ILJul 9, 2023 · N254UP · Doug MD11F · Aileron Control SystemSDR IPXA2023062693523Spar · corrodedINSPECTION TYPE:C3CORROSION FOUND R/WING ON LOWER SPAR CAP VERTICAL FLANGE STA XW 486REMOVED CORROSION AND REPAIRED IAW VT-SAA EA 011-5710-01-A9978 I/R AND UPS EO MD11-5710-87379-A. MINOR REPAIRJun 26, 2023 · N254UP · Doug MD11F · Wing SparSDR IPXA2023062893530Seat Track · corrodedINSPECTION TYPE:C3*MAJOR REPAIR* MAIN CABIN SEAT TRACK AT STA Y=6.70 AND Y=6.80, X=27.50 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN STA Y=6.70 AND STA Y=6.80, X=27.50 IAW 53-00-52-2R FIG 201 REPAIR 1. (MAJOR)Jun 16, 2023 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023062893534Tee Angle · crackedINSPECTION TYPE:3CR/H WING O/B FLAP O/B HINGE LWR TEE SUPPORT ANGLE IS CRACKED.REPLACED CRACKED TEE AT THE R/H WING O/B FLAP O/B HINGE LWR SUPPORT ANGLE IAW SRM 51-31-01 (MINOR)Jun 14, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023063093551Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #3 LUG BORE HAS CORROSION ATSTA XW=486.403.REPAIRED CORRODED HINGE ASSY. #3 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87Jun 13, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023062693516Splice · unknownINSPECTION TYPE:3C*MAJOR REPAIR* FOUND EXISTING REPAIR SPLICE FITTING AT STA Y=6-80 LONGERON 46L WITH NO HISTORY.REPLACED EXISTING REPAIR SPLICE FITTING AT STA Y= 6-80 LONGERON 46L IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)Jun 13, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023062893535Hinge · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #2 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DATJun 9, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023062893536Hinge · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #3 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DATJun 9, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023063093549Hinge · corrodedINSPECTION TYPE:3CL/H WING O/B FLAP I/B FWD HINGE AFTER REMOVAL OF BUSHING FOUND INCOMING #1 LUG BORE OUT OF LIMITS.REPAIRED HINGE ASSY. #1 LUG BORE AT THE L/H WING O/B FLAP I/B FWD HINGE IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DATED 06Jun 8, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023062993544Longeron · corrodedINSPECTION TYPE:3C*MAJOR REPAIR* FOUND CORROSION UNDERNEATH OF THE END SPLICE OF LONGERON 50 R/H CTR CARGO AT STA Y=5-2.21 - Y=5-11.00.REPAIRED CORRODED LONGERON 50R AT THE R/H SIDE CTR CARGO STA Y=5-2.21 - Y=5-11.00 IAW VTSAA EA 011-5310-01-A9976 I/R AND UPSJun 6, 2023 · N254UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2023062693515Longeron · corrodedINSPECTION TYPE:3C*MAJOR REPAIR* CAC COMP. BILGE AREA LONGERON 46L HAS CORROSION AT STA Y=6-75.REPAIRED CORRODED LONGERON 46L SECTION AT THE CAC COMP. BILGE AREA AT STA Y=6-75 IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)Jun 4, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023062993545Beam · crackedINSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R3 DOOR LWR HORIZONTAL BEAM FWD SIDE IS CRACKED BETWEEN STA Y=793 - Y=838.REPAIRED CRACKED HORIZONTAL BEAM AT THE MAIN CABIN R3 DOOR FWD SIDE BETWEEN STA Y=793 - Y=838 IAW VTSAA EA 011-5210-01-A9970 I/R AND UPS EO MDJun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2023062093483Web · crackedINSPECTION TYPE:C3MAIN CABIN R/H FLOOR WEB IS CRACKED AT STA 1986.REMOVED, FABRICATED AND REPLACED CRACKED FLOOR WEB IAW SRM 51-35-01 AND DWG AGA7145. (MINOR)Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023062093488Skin · corrodedINSPECTION TYPE:3CEMPENNAGE R/H FUSELAGE BODY FAIRING SKIN HAS SURFACE CORROSION AT STA 1941-2122.REPAIRED CORRODED SKIN AT THE EMPENNAGE R/H FUSELAGE AREA AT STA 1941-2122 IAW SRM 51-21-01 DWG AJC7060. (MINOR)Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2023062093486Tee Fitting · crackedINSPECTION TYPE:3CUPPER CENTER AUXILIARY TANK FWD BULKHEAD TEE BRACKET IS CRACKED BETWEEN STA XCW=46 AND XCW=81.REMOVED, FABRICATED AND REPLACED CRACKED TEE BRACKET AT THE UPPER CENTER AUXILIARY TANK FWD BULKHEAD BETWEEN STA XCW=46 AND XCW=81 IAW SRM 51-33-01 Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023061693454Stringer · crackedINSPECTION TYPE:3C*MAJOR REPAIR* UPPER CENTER AUXILIARY TANK HAS A CRACKED EXISTING REPAIR BETWEEN STA XCW=-17 AND XCW=-46.REPAIRED CRACKED EXISTING REPAIR AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=-17 AND XCW=-46 IAW SRM 57-10-03 FIG 201 REPAIR 1. (Jun 3, 2023 · N254UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2023063093553Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=638.305.REPAIRED CORRODED HINGE ASSY. #3 LUGE BORE AT THE L/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=638.305 IAW VTSAA EA 011-5740-01-A9986 I/R AND UPS EO MD11-5740-Jun 2, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023063093552Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=486.403.REPAIRED HINGE ASSY. #2 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DAJun 2, 2023 · N254UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023063093555Stringer · crackedINSPECTION TYPE:3C*MAJOR REPAIR* R/H WING #3 TANK UPPER STRINGER 1 IS CRACKED BETWEEN STA XORS=1012.55 AND 1042.350.REPAIRED CRACKED STRINGER 1 AT THE R/H WING #3 TANK UPPER SIDE BETWEEN STA XORS=1012.55 AND XORS=1042.350 IAW VTSAA EA 011-5710-01-A9977 I/R ANDJun 2, 2023 · N254UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2023062893533Stiffener · crackedINSPECTION TYPE:3CAFT CARGO COMP STA 1841 R/H SIDE 1EA STIFFENER HAS A CRACKED.REPLACED CRACKED STIFFENER AT THE AFT CARGO COMP AT STA 1841 IAW SRM 51-33-01 (MINOR)Jun 1, 2023 · N254UP · Doug MD11F · Cargo CompartmentsSDR IPXA2023062893532Angle · brokenINSPECTION TYPE:3CR/H WING FUEL QUANTITY CONTROL UNIT HAS A BROKEN O/B ATTACHMENT ANGLE.REPLACED BROKEN ANGLE AT THE R/H WING FUEL QUANTITY CONTROL UNIT ATTACHMENT IAW 51-33-01 AND DWG ARB2382. (MINOR)Jun 1, 2023 · N254UP · Doug MD11F · Leading Edge DevicesSDR IPXA2023062693513Splice · corrodedINSPECTION TYPE:3CCTR CARGO BILGE AREA AT STA Y=1701 - Y=1721 SPLICE ON LONGERON 52 HAS CORROSION.REPAIRED CORRODED SPICE AT THE CTR CARGO BILGE AREA AT STA Y=1701 - Y=1721 ON LONGERON 52 IAW SRM 51-33-01 AND DWG AFA7102. (MINOR)Jun 1, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023062093485Angle · corrodedINSPECTION TYPE:3CCTR CARGO STA 1721-1741 LONGERON 52 INTERCOSTAL WEB ANGLE SUPPORT HAS CORROSION.REMOVED, FABRICATED AND REPLACED THE CORRODED SUPPORT TEE AT THE CTR CARGO STA 1721-1741, LONGERON 52 IAW SRM 51-33-01 AND DWG ACA7673. (MINOR)Jun 1, 2023 · N254UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023061693455Spar Cap · corrodedINSPECTION TYPE:C3*MAJOR REPAIR* R/H WING REAR SPAR AREA ABOVE O/B FLAP O/B HINGE FITTING HAS CORROSION BETWEEN STA XORS=724 AND XORS=730.REPAIRED CORRODED R/H WING REAR SPAR AREA ABOVE O/B FLAP O/B HINGE FITTING BETWEEN STA XORS=724 AND XORS=730 IAW VTSAA EA May 31, 2023 · N254UP · Doug MD11F · Wing SparSDR IPXA2023062093484Stiffener · crackedINSPECTION TYPE:3CVERTICAL STIFFENER FROM FRONT OF R/H WHEEL WELL AFT CUTOUT IS CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER AT THE R/H WHEEL WELL AFT CUTOUT IAW SRM 51-35-01 AND DWG ANB7203. (MINOR)May 30, 2023 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023032792290Door · inoperativeINSPECTION TYPE:NAL1 "DOOR DISARM') LIGHT SWITCH BROKENREMOVED & REPLACED LENS ASSY IAW MD11 AMM 20-30-10Mar 25, 2023 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023032492198Door · inoperativeINSPECTION TYPE:NADOOR 1R DISARM LIGHT INOP.SECURED DISARM LIGHT IAW AMM, 52-10-00.Mar 23, 2023 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2022112288349Girt Bar · out of positionL1 ENTRY DOOR WILL NOT ARM PHYSICAL BLOCK, WHEN TRYING TO MOVE ARMING LEVER AFTER CLOSING. FOUND GORT BAR OUT OF POSITION REST REF AMM 52 10 01Nov 21, 2022 · N254UP · Doug MD11F · Emergency EquipmentSDR IPXA2022110887971Door · malfunctionedUNABLE TO ARM L1 DOOR AFTER CLOSING REPOSITIONED QIRT BW ON L1 DOOR OPENED THE SEVERAL CYCLES REF MD11 MM 25-61-01 OPENEDS NORMALLYNov 7, 2022 · N254UP · Doug MD11F · Passenger/Crew Doors
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