N284UP

Service difficulty reports · 244

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 = 'N284UP' 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 IPXA2025091628055Coalescer Bag · odorNOTICED AN ODOR AT 11,000 FT DISSIPATED AT 15,000 FT FO SAID IT SMELLED LIKE BURNING RUBBER. REMOVED AND REPLACED NR 2 PACK WATER SEPARATOR CONICAL COALESCER IAW AMM 21-54-04, LEAK CHECK GOOD. DURING ENGINE RUN ISOLATED NR 2 PACK FOR 5 MINS WITH NO NOTABLE OSep 16, 2025 · N284UP · Doug MD11F · Humidity Control SystemSDR IPXA2025081222186Battery · no testPRE FLIGHT, DURING EMER LIGHT TEST GOT €Œ L1 EMER LT BAT 1 LO. ? REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. REVERSED DMP 33-50-4. OPS CHECK GOOD PER AMM 33-51-01.Aug 12, 2025 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2025080154641Skin · crackedLH WING SLAT TRACK #10 LE TRACK CUT OUT HAS A CRACK AT RADIUS.040-19, ATA-51-00. ACCOMPLISH REPAIR PER SRM 57-40-02-2R-7 REPAIR 7 REV 71. INSTALLED REPAIR FILLER AND DOUBLER AT L/H WING SLAT TRACK #10 LE TRACK CUT OUT PER MD11 SRM 57-40-02-2R-7 REPAIR 7 FIG. Jul 16, 2025 · N284UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2025080217947Support · crackedSTR- LH O/B FLAP , I/B FLAP HINGE HAS A CRACKED SIDE BRACE AT O/B SIDE. .REMOVED THE DAMAGED SIDE BRACE FITTING IN LH WING O/B FLAP O/B SIDE OF I/B HINGE FITTING REF SRM 51-33-01-0G-0.FABRICATED SIDE BRACE FLAP HINGE TENSION STRAP P/N ARB0029-509 IAW DWG ARB00Jul 14, 2025 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2024121868366Sign · detachedWHEN OPENING THE MAIN ENTRY DOOR THE EMERGENCY EXIT SIGN FELL OFF REMOVED AND REPLACED L1 EMERGENCY EXIT SIGN IAW MD-11 AMM 33-27-05. OPS CHECK GOOD.Dec 18, 2024 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2024082633027Handle · unknownR1 DOOR SLIDE/EMER DOOR OPENING LEVER (RED) IS IN DIFFERENT POSITION THAN L1 DOOR LEVER. L1 DOOR MECHANISM IS AT A DIFFERENT ANGLE DUE TO ARTICULATING CREW REST. BOTH R1 AND L1 EMERGENCY INSIDE HANDLE ARE IN CORRECT POSITIONS. REF AMM 52-10-01 FIG 207Aug 24, 2024 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024080869614Battery Pack · warning messageDURING PREFLIGHT RECIEVED THE LVL1 EMER LT BAT 1 LO ALERT. R/R BATTERY EMERGENCY POWER SUPPLY PER AMM 33-51-01-401 OPS CHECK GOOD THIS CLEAR DEFERRAL PLACARD REMOVED DMP REVERSEDAug 8, 2024 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2024051311197Slat System · malfunctioned**EMERGENCY DECLARED** **ATB** DURING CLIMB, AFTER SLATS RETRACT COMMAND, THE AIRCRAFT BEGAN AN UNCOMMANDED ROLL TO THE LEFT. WAS UNABLE TO LEVEL THE WING WITH THE YOKE INPUTS. MAINTAINED AN APPROXIMATE 20* BANK UNTIL SLATS WERE RE PERFORMED FIM SLAT DISAGREE May 10, 2024 · N284UP · Doug MD11F · Leading Edge Slat Control SystemSDR IPXA2024021724615Door · unknownL1 DOOR WILL NOT OPEN. L1 DOOR OPS CHECKS GOOD AT THIS TIME. REF AMM 52-10-01. THIS CLEARS MEL 52-10-3-2-1-2. PLACARD REMOVED.Feb 17, 2024 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023112909334Unknown · unknownL1 DOOR DOES NOT OPEN WITH ELECTRIC FROM INSIDE AIRCRAFT (INTERMITTENT) C/W PERFORMED AMM TASK 52-10-01-700-801 OPERATIONAL CHECK OF L1 DOOR NORMAL MODE. UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. NO RELEVANT LOG HISTORY 90 DAYS. DEFERRAL CLOSED PLAC RMVD.Nov 29, 2023 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023092694250Battery · dischargedLVL1 EMER LT BAT 1 LO DURING PREFLIGHT CHECK. DEFERRED EMERGENCY LIGHTING SYSTEM PER MD11 MEL 33-50-4. DMP COMPLIED, CONTROL# M812709 ASSIGNED, PLACARD INSTALLEDR&R EMERG LIGHTING BATT POWER SUPPLY PER MM TASK 33-51-01 REVERSED DMP 33-50-4. PERFORMED OPER CHK Sep 25, 2023 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2023081293886Seat Track · corrodedINSPECTION TYPE:4C*** MAJOR REPAIR *** MAIN CABIN HAS A SEAT TRACK AT STA 710 TO 745 RBL -8.5 WITH CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN STA 710 TO 745 RBL -8.5 IAW SRM 53-00-52 FIG. 201 REPAIR 1. (MAJOR)Aug 8, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023081293885Seat Track · corrodedINSPECTION TYPE:4C*** MAJOR REPAIR *** MAIN CABIN HAS A SEAT TRACK THAT IS CRACK AT STA 740 TO STA 745 AND LBL 8.5.REPAIRED CRACKED SEAT TRACK AT THE MAIN CABIN AT STA Y=740 TO Y=745 AND LBL 8.5 IAW SRM 53-00-52 FIG 201 REPAIR 1. (MAJOR)Aug 8, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023081293884Seat Track · corrodedINSPECTION TYPE:4C*** MAJOR REPAIR *** MAIN CABIN SEAT TRACK HAS CORROSION AT STA 745 AND LBL 27.5.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN STA 745 AND LBL 27.5 IAW SRM 53-00-52 FIG. 201 REPAIR 1. (MAJOR)Aug 7, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023081293883Seat Track · corrodedINSPECTION TYPE:4C*** MAJOR REPAIR *** MAIN CABIN SEAT TRACK HAS CORROSION AT STA 745 RBL -8.5.REPAIRED CORRODED SEAT TRACK AT STA 745 AND RBL -8.5 IAW SRM 53-00-52 FIG. 201 REPAIR 1. (MAJOR)Aug 7, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2023080593805Stiffener · crackedINSPECTION TYPE:4CL/H WHEEL WELL 3RD VERTICAL STIFFENER AFT OF CUTOUT IS CRACKED AT LOWER SECTION AT STA Y=1474.000REMOVED, FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER AT THE L/H WHEEL WELL THE 3RD AFT OF CUTOUT AT STA Y=1474.000 IAW SRM 51-35-01 AND DWJul 26, 2023 · N284UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023080593803Seat Track · corrodedINSPECTION TYPE:4C*MAJOR REPAIR* MAIN CABIN BETWEEN STA 775 TO STA 791 LBL 8.5 SEAT TRACK HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN BETWEEN STA 775 TO STA 791 LBL 8.5 IAW SRM 53-00-52 FIG.201 REPAIR 1 (MAJOR)Jul 22, 2023 · N284UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023081193878Hinge Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG I/B FACE HAS CORROSION AT STA XW=-254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE AT STA XW=-254, YW=495.961 IAW VTSAA EA 011-5740Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081193877Hinge Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG O/B FACE HAS CORROSION AT STA XW=254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE AT STA XW=254, YM=495.961 IAW VTSAA EA 011-5740-0Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081093866Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG I/B FACE HAS CORROSION AT STA XW=254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE AT STA XW=254, YW=495.961 IAW VTSAA EO 011-5740-0Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993860Flap · corrodedINSPECTION TYPE:4CR/H WING I/B FLAP SIDE O/B HINGE #6 LUG BORE HAS PITTING AT STA XW=-254.REPAIRED HINGE AT THE R/H WING I/B FLAP SIDE O/B HINGE #6 LUG BORE AT STA XW=-254 IAW VTSAA EA 011-5740-01-B0054 I/R AND UPS EO MD11-5750-87788-A DATED 08/07/23 AND FAA FJul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993858Flap · wornINSPECTION TYPE:4CR/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE IS WORN AT STA XW=-486.403.REPAIRED WORN HINGE AT THE R/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE AT STA XW=-486.403 IAW VTSAA EA 011-5740-01-B0060 I/R AND UPS EO MD11-5750-87840-A DATED 08/07/23 Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080593801Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE O/B FLAP O/B HINGE BRACKET #1 LUG BORE HAS CORROSION AT STA XW=-638.3059.REPLACED CORRODED HINGE BRACKET ASSY. AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.3059 IAW AMM 57-53-01 (MINOR)Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080493793Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE O/B FLAP I/B HINGE BRACKET #1 LUG BORE HAS PITTING AT BETWEEN STA XW= -486.403, YW=589.366.REPLACED R/H WING A/C SIDE O/B FLAP I/B HINGE BRACKET BETWEEN STA XW=-486.403, YW=589.366 IAW AMM 57-53-01-400-801. (MINOR)Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081093870Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING I/B FLAP SIDE O/B HINGE BRACKET #6 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING I/B FLAP O/B HINGE #6 LUG BORE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0052 I/R AND UPS EO Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081093869Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING I/B FLAP SIDE O/B HINGE BRACKET #7 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING I/B FLAP SIDE O/B HINGE BRACKET #7 LUG BORE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0052 I/Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993859Flap · corrodedINSPECTION TYPE:4CL/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE HAS CORROSION AT STA XW=486.403.REPAIRED CORRODED HINGE AT THE L/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE AT STA XW=486.403 IAW VTSAA EA 011-5740-01B0061 I/R AND UPS EO MD11-5750-87789-A DATED 08Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023072893757Angle · crackedINSPECTION TYPE:4C#3 PYLON UPPER WIRE HARNESS SUPPORT HAS A CRACKED ANGLE AT THE AFT SIDE ABOVE PRECOOLER.REMOVED, FABRICATED AND REPLACED ANGLE AT THE #3 PYLON AT THE AFT SIDE ABOVE PRECOOLER IAW SRM 54-05-41 AND DWG AUB7564. (MINOR)Jul 19, 2023 · N284UP · Doug MD11F · Nacelle/Pylon StructureSDR IPXA2023072893756Bracket · crackedINSPECTION TYPE:4CCAC COMP. RADIO RACK SHELF AT O/B LOWER SIDE IF SHELF JUST O/B OF THE FLASHER TIMING UNIT HAS A CRACKED BRACKET.REMOVED, FABRICATED AND REPLACED BRACKET AT THE CAC COMP. JUST O/B OF THE FLASHER TIMING UNIT IAW SRM 51-53-01 AND DWG AAN7185. (MJul 19, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2023080593806Tee Angle · crackedINSPECTION TYPE:4CFWD CARGO COMPARTMENT HAS A CRACKED T-CLIP BRACKET AT FS 6-60 LBL 55 ON AFT SIDE OF FLOOR BEAM.REMOVED, FABRICATED AND REPLACED CRACKED T-CLIP AT THE FWD CARGO COMPARTMENT AT FS 6-60 LBL 55 ON AFT SIDE OF FLOOR BEAM IAW SRM 51-33-01. (MINOR)Jul 18, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2023080493795Doubler · crackedINSPECTION TYPE:4C*MAJOR REPAIR* R/H WING L/E HAS A BEADED DOUBLER THAT IS CRACKED JUST I/B OF SLAT TRACK #12 AT STA XOS=755.REPAIRED CRACKED BEADED DOUBLER AT THE R/H WING L/E JUST I/B OF SLAT TRACK #12 AT STA XOS=755 IAW SRM 57-40-02 FIG. 205 REPAIR 15. (MAJJul 16, 2023 · N284UP · Doug MD11F · Leading Edge DevicesSDR IPXA2023080193769Stringer · crackedINSPECTION TYPE:4CR/H WING L/E LWR STRINGER HAS A CRACKED ON EXISTING DOUBLER JUST O/B OF SLAT TRACK #14 AT STA XOS=906.5607.REPAIRED EXISTING CRACKED DOUBLER AT THE R/H WING L/E LWR STRINGER JUST O/B OF SLAT TRACK #14 STA XOS=906.5607 IAW SRM 57-40-03 FIG.201Jul 16, 2023 · N284UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2023060893396Door · inoperativeR-1 DOOR DISARMED LT INOP. DEFERRED R-1 DOOR SLIDE PER MEL 52-10-3-1-2-1. OK TO CONTINUE UNDER CONTROL # M809295. PLA INSTALLED. R&R LIGHT ASSY IAW MD11 AMM 20-30-00. OP CHECK GOOD. M809295 CLEARED PLACARD REMOVED.Jun 7, 2023 · N284UP · Doug MD11F · Service DoorsSDR IPXA2023042793001Door · inoperativeINSPECTION TYPE:N/A**SDR FILED OPEN** L 1 CREW ENTRY DOOR STUCK HALF OPEN. PLACED L1 DOOR ON DEFERRAL PER MD11 MEL 52 10 3 1 2 1. CONTROL NUMBER M 807635 ASSIGNED PLACARD INSTALLED. R&R L1 DOOR LOCK RELEASE SOLENOID PER AMM 52-10-06, OPS CHECK GOOD THIS CLEARApr 27, 2023 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023040592617Sign · damagedINSPECTION TYPE:NADAMAGED EMER EXIT SIGN DAMAGED (AFT PIN BROKEN OFF).REMOVED AND REPLACED AFT PIN PER 00-INTRO-PAR.2.B INSTALLED L1 EMER EXIT SIGN.Apr 4, 2023 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2023030791649Door · inoperativeINSPECTION TYPE:NA*SDR FILED OPEN* ADDITIONAL ACTIONS REQUIRED FOR L1 DOOR DEFERRAL. LINK TO M804260. PULLED AND COLLARED L1 DOOR POWER AND CONTROL CB'S (B1-1028 & B1-1835) PER GMM 3-5-1-1. RESET C/BS LINKED TO M804260 REF LP 570998 ITEM 1 OPCKS GOOD IAW AMM Mar 6, 2023 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023030791621Door · inoperativeINSPECTION TYPE:NA*SDR FILED OPEN* L1 DOOR INTERMITTENLY WORKING ELECTRICALLY. C/W DMP. DEFERRED L1 DOOR PER MEL 52-10-1-2-0-1. R&R LEFT FWD DOOR ACTUATOR RELAY (R2-177) AND LH FWD DOOR LOCK PWR RELEASE RELAY (R2-5324) IAW WDM 52-11-01, SWPM 20-20-03. PERFORMMar 6, 2023 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023030191443Door · inoperativeL1 DOOR INTERMITTENTLY INOP. DEFERRED L1 DOOR PER MEL 52-10-1-2-0-1 VERFIED BOTTLE PRESSURE ASSIGNED DMI# PLACARD INSTALLEDREVERSED DMP. R&R L1 DOOR ELECTRICAL ACTUATOR REF MM 52-11-01. OPS CHECK OK. DEFERRAL CLEARED, PLACARD REMOVED.Mar 1, 2023 · N284UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2022122289213Light · crew errorEMERGENCY LIGHT BATTERY 1 LOW ON PREFLT. LAST CREW LEFT EMERGENCY LIGHTS ARMED. PERFORMED OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD.Dec 21, 2022 · N284UP · Doug MD11F · Emergency LightingSDR IPXA2022091286143None · inoperativeINSPECTION TYPE:N/A**ATB** - **EMERGENCY DECLARED** LEVEL AT 33,000' RECEIVED A LEVEL 1 TNK 1 TIP TRAPPED AND LEVEL 1 TNK 1 FUEL QTY LO. 5600 LBS TRAPPED IN TIPTANK AIR TURN BACKTRBLSHT FUEL TRANSFER SCHEDULED REF MD11 FIM 28 14 16 00 SHT 1 REMOVED & REPALCED Sep 9, 2022 · N284UP · Boeing 737 · Fuel Quantity IndicatorSDR IPXA2022082385519Angle · inoperativeINSPECTION TYPE:N/AEMERG LIGHTING LO BATT 1R&R EMERG LIGHTING POWER SUPPLY PER MM 33-51-01--401 OPS CHECKS GOODAug 22, 2022 · N284UP · Boeing 737 · Emergency LightingSDR IPXA2022031580140None · noneINSPECTION TYPE:NAFIRST OFICER IS UNABLE TO READ THE SLIDE RAFT PRESSURE ON L1 DOOR.ADJUSTED SLIDE SO THAT GAUGE IS VISABLE IN WINDOW W/REF TO M/M 25-61-15.Mar 14, 2022 · N284UP · Doug MD11F · Emergency EquipmentSDR IPXA2021091573938Anti-Ice System · faulted**ATB** - AFTER TAKEOFF RECEIVED LVL 1 ENG 1 A-ICE 1 DISAGREE AND ENG 3 A-ICE 3 DISAG. DURING DESCENT, MESSAGES EXTINGUISHED. TRANSFERRED TO NR 456456 FOR PERMANENT REPAIRFOUND ENGINE 1 & 3 ANTI-ICE LOCK IN THE OPEN POSITION, REPOSITIONED ANTI-ICE IN THE NORMASep 12, 2021 · N284UP · Doug MD11F · Engine Anti-Icing SystemSDR IPXA2021090473550Bracket · corrodedINSPECTION TYPE:3CRT WING O/B FLAP I/B HINGE BRACKET ASSY. HOLE #7 IS CORRODED.REPAIRED CORRODED RT WING O/B FLAP I/B HINGE BRACKET ASSY. XW 486.403 HOLE #7 IAW VT-SAA EA 011-5740-01-A9326 REV. IR AND UPS EO MD11-5740-81500-A. (MINOR)Aug 25, 2021 · N284UP · Doug MD11F · Wing, Attach FittingsSDR IPXA2021090173383Attach Angle · crackedINSPECTION TYPE:3CCENTER LOWER FUSELAGE R/H FRAME ATTACH ANGLE AT STA 1278 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER LOWER FUSELAGE R/H FRAME ATTACH ANGLE AT STA 1878 IAW SRM 51-33-01. (MINOR)Aug 19, 2021 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2021083173367Attach Angle · crackedINSPECTION TYPE:3CCENTER FUSELAGE L/H FRAME ATTACH ANGLE AT STA 1278 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER FUSELAGE L/H FRAME ATTACH ANGLE AT STA 1278 IAW SRM 51-33-01. (MINOR)Aug 19, 2021 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2021083173366Floor Panel · corrodedINSPECTION TYPE:3CFWD CABIN FLOOR PANEL WSP0785-501 BETWEEN STA 475 TO 500 AND X= -8.8 TO X= -17 IS CORRODED.REPAIRED CORRODED FWD CABIN FLOOR PANEL WSP0785-501 BETWEEN STA 475 TO 500 AND X= -8.8 TO X= -17 IAW VT-SAA EA 011-5320-01-A9310 REV. IR AND UPS EO MD1Aug 18, 2021 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2021091073782Skin · corrodedINSPECTION TYPE:3CR/H AFT FUSELAGE SKIN BETWEEN STA 2103 TO 2163.685 AND BETWEEN LONGERONS 33R TO 35R IS CORRODED.REPAIRED CORRODED R/H FUSELAGE SKIN BETWEEN STA 2103 TO 2163.685 AND BETWEEN LONGERONS 33R TO 35R IAW VT-SAA EA 011-5330-01-A9311 REV. IR AND UPS Aug 17, 2021 · N284UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2021090473549Rib · crackedINSPECTION TYPE:3CRT I/B ELEVATOR I/B L/E RIB UPPER FLANGE AT XE= 125.8 IS CRACKED.REPAIRED CRACKED RT I/B ELEVATOR I/B L/E RIB UPPER FLANGE AT XE= 125.8 IAW VT-SAA EA 011-5520-01-A9301 REV. IR AND UPS EO MD11-5520-81471-A. REF. FAA FORM 8100-9 SIGNED BY P. LAAug 17, 2021 · N284UP · Doug MD11F · Elevator, Spar/RibSDR IPXA2021090273477Floor Support · crackedINSPECTION TYPE:3CCOCKPIT FLOOR SUPPORT ANGLE AT STA 366 AND RBL 20 IS CRACKED.REMOVED AND REPLACED CRACKED COCKPIT FLOOR SUPPORT ANGLE AT STA 366 AND RBL 20 IAW SRM 51-33-01. (MINOR)Aug 17, 2021 · N284UP · Doug MD11F · Fuselage Miscellaneous Structure
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