# Service difficulty reports: N284UP

A list on [N284UP](https://openairdocs.org/aircraft/N284UP.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 5 · 244 reports

- [SDR IPXA2025091628055](https://openairdocs.org/sdr/IPXA2025091628055.md): Coalescer Bag · odor · Sep 16, 2025 · N284UP · Doug MD11F · Humidity Control System
  > NOTICED 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 O
- [SDR IPXA2025081222186](https://openairdocs.org/sdr/IPXA2025081222186.md): Battery · no test · Aug 12, 2025 · N284UP · Doug MD11F · Emergency Lighting
  > PRE 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.
- [SDR IPXA2025080154641](https://openairdocs.org/sdr/IPXA2025080154641.md): Skin · cracked · Jul 16, 2025 · N284UP · Doug MD11F · Wing, Plate/Skin
  > LH 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.
- [SDR IPXA2025080217947](https://openairdocs.org/sdr/IPXA2025080217947.md): Support · cracked · Jul 14, 2025 · N284UP · Doug MD11F · Trailing Edge Flaps
  > STR- 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 ARB00
- [SDR IPXA2024121868366](https://openairdocs.org/sdr/IPXA2024121868366.md): Sign · detached · Dec 18, 2024 · N284UP · Doug MD11F · Emergency Lighting
  > WHEN 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.
- [SDR IPXA2024082633027](https://openairdocs.org/sdr/IPXA2024082633027.md): Handle · unknown · Aug 24, 2024 · N284UP · Doug MD11F · Passenger/Crew Doors
  > R1 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 207
- [SDR IPXA2024080869614](https://openairdocs.org/sdr/IPXA2024080869614.md): Battery Pack · warning message · Aug 8, 2024 · N284UP · Doug MD11F · Emergency Lighting
  > DURING 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 REVERSED
- [SDR IPXA2024051311197](https://openairdocs.org/sdr/IPXA2024051311197.md): Slat System · malfunctioned · May 10, 2024 · N284UP · Doug MD11F · Leading Edge Slat Control System
  > **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
- [SDR IPXA2024021724615](https://openairdocs.org/sdr/IPXA2024021724615.md): Door · unknown · Feb 17, 2024 · N284UP · Doug MD11F · Passenger/Crew Doors
  > L1 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.
- [SDR IPXA2023112909334](https://openairdocs.org/sdr/IPXA2023112909334.md): Unknown · unknown · Nov 29, 2023 · N284UP · Doug MD11F · Passenger/Crew Doors
  > L1 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.
- [SDR IPXA2023092694250](https://openairdocs.org/sdr/IPXA2023092694250.md): Battery · discharged · Sep 25, 2023 · N284UP · Doug MD11F · Emergency Lighting
  > LVL1 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
- [SDR IPXA2023081293886](https://openairdocs.org/sdr/IPXA2023081293886.md): Seat Track · corroded · Aug 8, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2023081293885](https://openairdocs.org/sdr/IPXA2023081293885.md): Seat Track · corroded · Aug 8, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2023081293884](https://openairdocs.org/sdr/IPXA2023081293884.md): Seat Track · corroded · Aug 7, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2023081293883](https://openairdocs.org/sdr/IPXA2023081293883.md): Seat Track · corroded · Aug 7, 2023 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2023080593805](https://openairdocs.org/sdr/IPXA2023080593805.md): Stiffener · cracked · Jul 26, 2023 · N284UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION 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 DW
- [SDR IPXA2023080593803](https://openairdocs.org/sdr/IPXA2023080593803.md): Seat Track · corroded · Jul 22, 2023 · N284UP · Doug MD11F · Fuselage Structure (General)
  > INSPECTION 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)
- [SDR IPXA2023081193878](https://openairdocs.org/sdr/IPXA2023081193878.md): Hinge Bracket · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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 011-5740
- [SDR IPXA2023081193877](https://openairdocs.org/sdr/IPXA2023081193877.md): Hinge Bracket · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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 011-5740-0
- [SDR IPXA2023081093866](https://openairdocs.org/sdr/IPXA2023081093866.md): Hinge Bracket · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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 011-5740-0
- [SDR IPXA2023080993860](https://openairdocs.org/sdr/IPXA2023080993860.md): Flap · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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 F
- [SDR IPXA2023080993858](https://openairdocs.org/sdr/IPXA2023080993858.md): Flap · worn · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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
- [SDR IPXA2023080593801](https://openairdocs.org/sdr/IPXA2023080593801.md): Bracket · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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)
- [SDR IPXA2023080493793](https://openairdocs.org/sdr/IPXA2023080493793.md): Bracket · corroded · Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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)
- [SDR IPXA2023081093870](https://openairdocs.org/sdr/IPXA2023081093870.md): Hinge Bracket · corroded · Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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
- [SDR IPXA2023081093869](https://openairdocs.org/sdr/IPXA2023081093869.md): Hinge Bracket · corroded · Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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/
- [SDR IPXA2023080993859](https://openairdocs.org/sdr/IPXA2023080993859.md): Flap · corroded · Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION 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 08
- [SDR IPXA2023072893757](https://openairdocs.org/sdr/IPXA2023072893757.md): Angle · cracked · Jul 19, 2023 · N284UP · Doug MD11F · Nacelle/Pylon Structure
  > INSPECTION 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)
- [SDR IPXA2023072893756](https://openairdocs.org/sdr/IPXA2023072893756.md): Bracket · cracked · Jul 19, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION 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. (M
- [SDR IPXA2023080593806](https://openairdocs.org/sdr/IPXA2023080593806.md): Tee Angle · cracked · Jul 18, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2023080493795](https://openairdocs.org/sdr/IPXA2023080493795.md): Doubler · cracked · Jul 16, 2023 · N284UP · Doug MD11F · Leading Edge Devices
  > INSPECTION 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. (MAJ
- [SDR IPXA2023080193769](https://openairdocs.org/sdr/IPXA2023080193769.md): Stringer · cracked · Jul 16, 2023 · N284UP · Doug MD11F · Wing, Longeron/Stringer
  > INSPECTION 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.201
- [SDR IPXA2023060893396](https://openairdocs.org/sdr/IPXA2023060893396.md): Door · inoperative · Jun 7, 2023 · N284UP · Doug MD11F · Service Doors
  > R-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.
- [SDR IPXA2023042793001](https://openairdocs.org/sdr/IPXA2023042793001.md): Door · inoperative · Apr 27, 2023 · N284UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION 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 CLEAR
- [SDR IPXA2023040592617](https://openairdocs.org/sdr/IPXA2023040592617.md): Sign · damaged · Apr 4, 2023 · N284UP · Doug MD11F · Emergency Lighting
  > INSPECTION 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.
- [SDR IPXA2023030791649](https://openairdocs.org/sdr/IPXA2023030791649.md): Door · inoperative · Mar 6, 2023 · N284UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION 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
- [SDR IPXA2023030791621](https://openairdocs.org/sdr/IPXA2023030791621.md): Door · inoperative · Mar 6, 2023 · N284UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION 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. PERFORM
- [SDR IPXA2023030191443](https://openairdocs.org/sdr/IPXA2023030191443.md): Door · inoperative · Mar 1, 2023 · N284UP · Doug MD11F · Passenger/Crew Doors
  > L1 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.
- [SDR IPXA2022122289213](https://openairdocs.org/sdr/IPXA2022122289213.md): Light · crew error · Dec 21, 2022 · N284UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY 1 LOW ON PREFLT. LAST CREW LEFT EMERGENCY LIGHTS ARMED. PERFORMED OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD.
- [SDR IPXA2022091286143](https://openairdocs.org/sdr/IPXA2022091286143.md): None · inoperative · Sep 9, 2022 · N284UP · Boeing 737 · Fuel Quantity Indicator
  > INSPECTION 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
- [SDR IPXA2022082385519](https://openairdocs.org/sdr/IPXA2022082385519.md): Angle · inoperative · Aug 22, 2022 · N284UP · Boeing 737 · Emergency Lighting
  > INSPECTION TYPE:N/AEMERG LIGHTING LO BATT 1R&R EMERG LIGHTING POWER SUPPLY PER MM 33-51-01--401 OPS CHECKS GOOD
- [SDR IPXA2022031580140](https://openairdocs.org/sdr/IPXA2022031580140.md): None · none · Mar 14, 2022 · N284UP · Doug MD11F · Emergency Equipment
  > INSPECTION 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.
- [SDR IPXA2021091573938](https://openairdocs.org/sdr/IPXA2021091573938.md): Anti-Ice System · faulted · Sep 12, 2021 · N284UP · Doug MD11F · Engine Anti-Icing System
  > **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 NORMA
- [SDR IPXA2021090473550](https://openairdocs.org/sdr/IPXA2021090473550.md): Bracket · corroded · Aug 25, 2021 · N284UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2021090173383](https://openairdocs.org/sdr/IPXA2021090173383.md): Attach Angle · cracked · Aug 19, 2021 · N284UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2021083173367](https://openairdocs.org/sdr/IPXA2021083173367.md): Attach Angle · cracked · Aug 19, 2021 · N284UP · Doug MD11F · Fuselage Main, Attach Fittings
  > INSPECTION 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)
- [SDR IPXA2021083173366](https://openairdocs.org/sdr/IPXA2021083173366.md): Floor Panel · corroded · Aug 18, 2021 · N284UP · Doug MD11F · Fuselage Floor Panel
  > INSPECTION 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 MD1
- [SDR IPXA2021091073782](https://openairdocs.org/sdr/IPXA2021091073782.md): Skin · corroded · Aug 17, 2021 · N284UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION 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
- [SDR IPXA2021090473549](https://openairdocs.org/sdr/IPXA2021090473549.md): Rib · cracked · Aug 17, 2021 · N284UP · Doug MD11F · Elevator, Spar/Rib
  > INSPECTION 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. LA
- [SDR IPXA2021090273477](https://openairdocs.org/sdr/IPXA2021090273477.md): Floor Support · cracked · Aug 17, 2021 · N284UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION 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)

Next page: https://openairdocs.org/aircraft/N284UP/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 = 'N284UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N284UP/reports

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