# Service difficulty reports: N383FE, cancelled Mar 2, 2024

A list on [N383FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N383FE-2024-03-02.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 · 223 reports

- [SDR FDEA202009222296](https://openairdocs.org/sdr/FDEA202009222296.md): Balance Weight · corroded · Sep 22, 2020 · N383FE · Doug MD1010F · Rudder Structure
  > UPPER FWD RUDDER, UPPER WEIGHT CORRODED. REMOVED AND REPLACED UPPER FWD RUDDER, IAW AMM 27-20-02-4.
- [SDR FDEA202009182330](https://openairdocs.org/sdr/FDEA202009182330.md): Splice Plate · corroded · Sep 18, 2020 · N383FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN-DECK AT STA-1371 LT SLANT PANELS "T" CORD HAS ONE AREA WITH MILD CORROSION. CORROSION REMOVAL PERFORMED ON ANGLE APB7080-1 (REFER JPF ITEM 1) AND SPLICE PLATE ANB7011-1 (REFER JPF ITEM 2). REWORK ON ANGLE APB7080-1 AND SPLICE PLATE ANB7011-1 REVIEWED AN
- [SDR FDEA202009172294](https://openairdocs.org/sdr/FDEA202009172294.md): Rib · cracked · Sep 17, 2020 · N383FE · Doug MD1010F · Vertical Stabilizer, Spar/Rib
  > RT HORIZ INBOARD LEADING EDGE SECTION, THE LEADING EDGE CAP OUTBOARD FORMED RIB, IS CRACKED AT BOTTOM AREA, MARKED. REPAIRED FORMER, REFERENCE SRM 22-00-01 FIG 7 SH 1 VOL 1.
- [SDR FDEA202009092164](https://openairdocs.org/sdr/FDEA202009092164.md): Doubler · cracked · Sep 9, 2020 · N383FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING FIXED LEADING EDGE APPROX AT STA XOS 664. INTERNAL BEADED DOUBLER HAS CRACKS AROUND TWO (2) FASTERNERS, MARKED. FABRICATED AND INSTALLED REPAIR DOUBLER, REF MD-10 SRM 57-10-00 FIG 71 P 222 VOL 1.
- [SDR FDEA2020090932086](https://openairdocs.org/sdr/FDEA2020090932086.md): Drive Chain · missing · Sep 3, 2020 · N383FE · Doug MD1010F · Passenger/Crew Doors
  > L-1 DOOR DRIVE CHAIN FOR EMERGENCY PNEUMATIC SYSTEM WAS MISSING. INSTALLED NEW CHAIN PER M/M 52-11-08-2.
- [SDR FDEA202008302447](https://openairdocs.org/sdr/FDEA202008302447.md): Former · cracked · Aug 30, 2020 · N383FE · Doug MD1010F · Wing Main, Frame Structure
  > LT WING LEADING EDGE, PER WIP EA NR 8-5710-T0356192 P1 STEP NR 2, FOUND CRACK INDICATION WITH HFEC APPROXIMATELY.25" IN LENGTH OF FORMER AT XOS 643, EMANATING FROM RADIUS TO FASTENER HOLE AREA ACCESSIBLE AFTER TRIMOUT OF CRACKED INBOARD FLANGE. REPAIRED LEFT
- [SDR FDEA202008302445](https://openairdocs.org/sdr/FDEA202008302445.md): Former · cracked · Aug 30, 2020 · N383FE · Doug MD1010F · Wing Main, Frame Structure
  > LT WING LEADING EDGE, PER WIP EA NR 8-5710-T0356192 P1 STEP NR 2, FOUND CRACK INDICATION WITH HFEC, APPROX.25" IN LENGTH OF FORMER AT XOS 643, EMANATING FROM RADIUS TO FASTENER HOLE, AREA ACCESSIBLE AFTER TRIMOUT OF CRACKED INBOARD FLANGE. THIS SDR ENTERED I
- [SDR FDEA202008292316](https://openairdocs.org/sdr/FDEA202008292316.md): Drag Angle · worn · Aug 29, 2020 · N383FE · Doug MD1010F · Vertical Stabilizer
  > LOWER AFT LT SIDE VERICAL STAB DRAG ANGLE WORN AT STA 2163. REPAIRED, PER EA 8-5530-T0356709 "STABILIZERS-VERTICAL STABILIZER LT DRAG ANGLE AND SKIN PANEL."
- [SDR FDEA202008252295](https://openairdocs.org/sdr/FDEA202008252295.md): Attach Angle · cracked · Aug 25, 2020 · N383FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > INSIDE LT MLG WW, AFT OUTBOARD LOWER CORNER, GUSSET TO INBOARD FLAP WELL, UNDER SIDE ATTACH ANGLE IS CRACKED. PREVIOUS REPAIR FAILURE. MAY NOT BE PER SRM, MARKED. REMOVED AND REPLACED CRACKED ANGLE P/N FX ANB7175-57 AS REQ, REF DAC DWG ANB7175 AND SRM 51-31
- [SDR FDEA2020082722046](https://openairdocs.org/sdr/FDEA2020082722046.md): Skin · corroded · Aug 22, 2020 · N383FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE AT MLG DOUBLER-APPROX XORS 281 BETWEEN STRG 1-2, CORROSION. REMOVED CORROSION, MATERIAL LOSS APPROXIMATELY.050" FOUND TO BE WITHIN LIMITS, PER SRM 57-00-01 FIG 8 SH 2 V1.
- [SDR FDEA202008212229](https://openairdocs.org/sdr/FDEA202008212229.md): Seat Track · corroded · Aug 21, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CTR WING AREA, CORROSION ON SEAT TRACK, CLIP NUT LOCATIONS, STA 1159-1229 RBL 78 (MARKED NR 3). R&R SEAT TRACK, PER SRM 53-70-00 FIG 1 VOL 1 AND DWG SR 10-53-002.
- [SDR FDEA202008212010](https://openairdocs.org/sdr/FDEA202008212010.md): Floorbeam · corroded · Aug 21, 2020 · N383FE · Doug MD1010F · Fuselage Main, Floor Beam
  > CTR WING AREA CORROSION ON FLOOR SUPPORT STA 1219 RBL 78-106 (MARKED NR 1). MAIN DECK FLOOR SUPPORT AT STA 1219 RBL78-106 (PNR WSP0711-509). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT, IAW MD10-10 SRM 51-35-01 VOL 2 (REFER JPF FOR FABRICATION OF FLOOR SUPPO
- [SDR FDEA2020082812049](https://openairdocs.org/sdr/FDEA2020082812049.md): Seat Track · damaged · Aug 21, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 1381 RBL 8 HAS A DAMAGED LOBE, REQUIRES REPAIR. REPLACED DAMAGE SEAT TRACK AT STA 1381 RBL 8 REF SRM 53-70-00, FIG 1, VOL 1. INSTALLED REF SRM 51-31-01, VOL II.
- [SDR FDEA202008192448](https://openairdocs.org/sdr/FDEA202008192448.md): Former · cracked · Aug 19, 2020 · N383FE · Doug MD1010F · Wing Main, Frame Structure
  > LT WING LEADING EDGE AT FUEL DOOR CUT-OUT APPROXIMATELY XOS 643 AFT OUTBOARD CORNER OF CUT-OUT LANDING/SUPPORT IS CRACKED. REPAIRED LEFT WING LEADING EDGE FORMER AT XOS643, IAW EA NR 8-5710-T0356192. MAJOR REPAIR.
- [SDR FDEA202008192444](https://openairdocs.org/sdr/FDEA202008192444.md): Former · cracked · Aug 19, 2020 · N383FE · Doug MD1010F · Wing Main, Frame Structure
  > LT WING LEADING EDGE AT FUEL DOOR CUT-OUT APPROXIMATELY XOS 643, AFT OUTBOARD CORNER OF CUT-OUT. LANDING/SUPPORT IS CRACKED. THIS SDR ENTERED IN ERROR.
- [SDR FDEA202008192356](https://openairdocs.org/sdr/FDEA202008192356.md): Frame · corroded · Aug 19, 2020 · N383FE · Doug MD1010F · Fuselage Main, Frame
  > LT FUSELAGE AT STA 1581 FILLET FRAME AFT SIDE HAS EXFOLIATION CORROSION, MARKED. NR 5 CUT OUT DAMAGED AREAS AND INSTALLED REPAIR ANGLES AND STRAP, PER EA 8-5320-T0356455 P1.
- [SDR FDEA202008192302](https://openairdocs.org/sdr/FDEA202008192302.md): Doubler · cracked · Aug 19, 2020 · N383FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING FIXED LE AT APPROX XOS 646 OUTBOARD OF FUEL PANEL, INTERNAL BEADED DOUBLER HAS CRACKS AROUND TWO (2) FASTENERS, MARKED. 0000829504: MARTINEZ, MARK A - 23-SEP-2020 03:04. INSTALLED DOUBLER AS REQUIRED, PER MD10 SRM NR 57-10-00 VOL-I FIG-71.
- [SDR FDEA202008192263](https://openairdocs.org/sdr/FDEA202008192263.md): Doubler · cracked · Aug 19, 2020 · N383FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING FIXED LEADING EDGE AT APPROX XOS 664-INTERNAL BEADED DOUBLER HAS CRACKS AROUND TWO (2) FASTENERS, MARKED. INSTALLED DOUBLER AS REQUIRED, REF MD 10 SRM 57-10-00 VOL 1 P 222.
- [SDR FDEA202008192222](https://openairdocs.org/sdr/FDEA202008192222.md): Skin · cracked · Aug 19, 2020 · N383FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > NR 3 PACK DOOR CUT OUT. UPPER AFT CORNER STA 535, CRACK EMINATING FROM FASTENER, INDICATION CONFIRMED WITH HFEC. REPAIRED NR 3 PACK DOOR CUT OUT UPPER AFT CORNER AT STA 535, REF MD10 SRM CH 53-50-00 FIG 3A SHEET 3 VOL 1.
- [SDR FDEA202009118172](https://openairdocs.org/sdr/FDEA202009118172.md): Skin · cracked · Aug 18, 2020 · N383FE · Doug MD1010F · Cargo/Baggage Doors
  > AFT CARGO DOOR INTERIOR SKIN JUST ABOVE AND BETWEEN NR 3 & NR 4 HOOK LATCHES, SKIN IS CRACKED. (MKD) INSTALLED REPAIR DOUBLERS AND ANGLE PER EA NR T8-5230-T0356217.
- [SDR FDEA2020090972140](https://openairdocs.org/sdr/FDEA2020090972140.md): Skin · dented · Aug 17, 2020 · N383FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZ STAB, LEADING EDGE (CENTER INBOARD SECTION) HAS MULTIPLE DENTS. INSTALLED REPAIR DOUBLER, REF SRAM 55-10-00 FIG 13 SH 1-3 VOL 1.
- [SDR FDEA2020082672025](https://openairdocs.org/sdr/FDEA2020082672025.md): Structure · corroded · Aug 17, 2020 · N383FE · Doug MD1010F · Fuselage Main, Structure
  > AFT FUSELAGE WASTE TANK COMPARTMENT AT STA 1997 & LBL 51 TO RBL 51. WEB TO LONGERON ATTACHMENT EXFOLIATED (MARKED), BLENDED CORROSION AREA FOUND TO BE BEYOND LIMITS. FABRICATED REPAIR ANGLE REF SRM 53-30-00 FIG. 8 AND DWG AGA3784 AND INSTALLED REF SRM 51-3
- [SDR FDEA2020090962084](https://openairdocs.org/sdr/FDEA2020090962084.md): Skin · damaged · Aug 16, 2020 · N383FE · Doug MD1010F · Trailing Edge Flaps
  > LT WING, OUTBOARD FLAP OUTER SKIN APPROX I/B MIDDLE OF FLAP. PREVIOUS SHEET METAL REPAIR STRIP IS MISSING, MARKED. INSTALLED NEW REPAIR STRIP ON LT WING OUTBOARD FLAP OUTER SKIN APPROX I/B MIDDLE OF FLAP, REF SRM 57-20-00 FIGURE 11 VOL I.
- [SDR FDEA202008152303](https://openairdocs.org/sdr/FDEA202008152303.md): Bracket · missing · Aug 15, 2020 · N383FE · Doug MD1010F · Ailerons
  > RIGHT WING, BEAM INST CLOSURE, INBOARD AILERON BRACKET (ARC0472-41) IS MISSING A FASTENER AND IS CRACKED, AREA MARKED. INSTALLED ARC0472-42 TEE, REF DWG ARC0472 AND SRM 51-31-01 VOL 2.
- [SDR FDEA202008152053](https://openairdocs.org/sdr/FDEA202008152053.md): Rib · cracked · Aug 15, 2020 · N383FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE, SUSPECT RIB CRACKED, NEXT TO UPPER SPAR CAP AT APPROX STA XORS 220. (MARKED. FIRE BOTTLE AND HEAT DUCT PREVENT CLOSE EXAMINATION) REPAIRED R/H WING L/E CRACKED RIB AT STA. XORS 220 WITH REPAIR DOUBLER PER SRM 57- 20-00 FIG.1 SH
- [SDR FDEA2020082642022](https://openairdocs.org/sdr/FDEA2020082642022.md): Rib · cracked · Aug 14, 2020 · N383FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE RIB CRACKED NEXT TO UPPER SPAR CAP AT APPROX STA XORS 714 (MARKED). REPAIRED RT WING FIXED LEADING EDGE CRACKED RIB AT STA. XORS 714 NEXT TO UPPER SPAR CAP PER SRM 57-20-00 FIG. 1 SHT. 6 V 2.
- [SDR FDEA202008132313](https://openairdocs.org/sdr/FDEA202008132313.md): Panel · leaking · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage Main, Structure
  > DURING FUSELAGE PRESSURIZATION LEFT W/W OUTBOARD SLANT PANEL LOWER OUTBOARD CORNER LEAKING AIR.
- [SDR FDEA202008132244](https://openairdocs.org/sdr/FDEA202008132244.md): Seat Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 1005 RBL 24 SEAT TRACK HAS SHARP BURRS MARKED NR 22. REPLACED DAMAGED SEAT TRACK FROM EXISTING REPAIR FROM STA 970 TO STA 1050 (APPROX) RBL 24, REF SRM 53-70-00 FIGURE 1 SHEET 1 VOL I DRAWING SR10-53-002, SRM 51-31-01 VOL II, SEALED R
- [SDR FDEA202008132011](https://openairdocs.org/sdr/FDEA202008132011.md): Seat Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 1381-1391 LBL 12 SEAT TRACK LOBES BURRED & OBLONG. REPLACED DAMAGED SEAT TRACK FROM STATION 1371 TO STATION 1391, REF SRM 53-70-00 FIG 1 VOL 1 INSTALLED PER SRM 51-31-01 VOLII FDX DRAWING SR10-53-002 AND SRM 51-41-01 VOL II. MX#3748
- [SDR FDEA202008131962](https://openairdocs.org/sdr/FDEA202008131962.md): Seat Track · worn · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 625 RBL 48 SEAT TRACK IS DAMAGED MARKED NR 32 0003893740: 21-AUG-2020 02:30. REMOVED AND INSTALLED NEW SEAT TRACK SECTION IN MAIN CARGO FROM STA 625 TO STA 690 AT RBL 48, REF SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR.
- [SDR FDEA2020081432175](https://openairdocs.org/sdr/FDEA2020081432175.md): Cargo Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 1029 RBL 24 SEAT TRACK HAS 2 LOBE SECTIONS OUT OF LIMITS, MARKED NR 18 NR 19. REPLACED DAMAGED SEAT TRACK FROM EXISTING REPAIR FROM STA 970 TO STA 1050 (APPROX) RBL 24, REF SRM 53-70-00 FIGURE 1 SHEET 1 VOL I DRAWING SR10-53-002, SRM
- [SDR FDEA2020091032165](https://openairdocs.org/sdr/FDEA2020091032165.md): Floor Panel · dented · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK: FLOOR PANEL UPPER SURFACE DAMAGED BETWEEN LBL X=75.25 TO LBLX=107.25 NEAR STA 1741 0005202524: HAZEMI, AL-19-AUG-2020 00:33. REPAIRED THE FLOOR PANEL'S SMALL DENT LIMITED TO SKIN SURFACE PER SRM 53-60-00 VOL-I.
- [SDR FDEA2020009092071](https://openairdocs.org/sdr/FDEA2020009092071.md): Seat Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 900 RBL 48 SEAT TRACK IS DAMAGED MARKED NR 16. REPLACED DAMAGED SEAT TRACK AT STA 900 RBL 48 REF SRM 53-70-00 FIG.1 VOL I.
- [SDR FDEA2020083132071](https://openairdocs.org/sdr/FDEA2020083132071.md): Seat Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 900 RBL 48 SEAT TRACK IS DAMAGED. REPLACED DAMAGED SEAT TRACK AT STA 900 RBL 48 REF. SRM 53-70-00 FIG.1 VOL.I
- [SDR FDEA2020082632028](https://openairdocs.org/sdr/FDEA2020082632028.md): Floorboard · delaminated · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN CARGO AT APPROXIMATELY STA 550 RBL 8 FLOOR BOARD IS DAMAGED MARKED NR 29 0005202524. FABRICATED FLOOR BOARD AT MAIN CARGO AT STA 550 RBL 8 PER FEDEX DWG SRZ - 25-005; 0005202524, 0005202524. FABRICATED FLOOR BOARD AT MAIN CARGO AT STA 550 RBL 8 PER FEDE
- [SDR FDEA2020082632026](https://openairdocs.org/sdr/FDEA2020082632026.md): Seat Track · worn · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 1371-1381 LBL 72 SEAT TRACK LOBES OBLONG. REMOVED AND REPLACED SEAT TRACK AT STA 137-1381 LBL 72 REF SRM 53-70-00 FIG 1, VOL 1.
- [SDR FDEA2020082632011](https://openairdocs.org/sdr/FDEA2020082632011.md): Seat Track · damaged · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 1381-1391 LBL 12. SEAT TRACK LOBES BURRED & OBLONG. REPLACED DAMAGE SEAT TRACK FROM STATION 1371 TO STATION 1391, REF 53-70-00, FIG 1, VOL 1. INSTALLED PER SRM 51-31-01, VOL II.
- [SDR FDEA2020082631979](https://openairdocs.org/sdr/FDEA2020082631979.md): Seat Track · worn · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN AT LBL X=47.50 NEAR STA 1635, MARKED RED. MAIN DECK SEAT TRACK AT STA 1621-1661 LBL 47.5, SPLICE REPAIR PERFORMED IAW SRM 53- 70-00 FIG 1 VOL1, DRWG SR10-53-501, SRM 51-31-01 VOL2, THEN SEALED IAW SRM 51-41-01 VOL2. (NOTE: REPAIR
- [SDR FDEA202008131943](https://openairdocs.org/sdr/FDEA202008131943.md): Seat Track · worn · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN, AT LBL X=47.50 NEAR STA 1640 MARKED RED MAIN DECK SEAT TRACK AT STA 1621-1661 LBL47.5, SPLICE REPAIR PERFORMED IAW SRM 53-70- 00 FIG 1 VOL1 AND DRWG SR10-53-501, THEN SEALED IAW SRM 51-41-01 VOL 2. (NOTE: REPAIR ALSO DONE TOGETHE
- [SDR FDEA2020082131962](https://openairdocs.org/sdr/FDEA2020082131962.md): Seat Track · worn · Aug 13, 2020 · N383FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO AT APPROX STA 625 RBL 48 SEAT TRACK IS DAMAGED MARKED #32 0003893740: CORAL, CHRISTOPHER - 21-AUG-2020 02:30 REMOVED AND INSTALLED NEW SEAT TRACK SECTION IN MAIN CARGO FROM STA 625 TO STA 690 AT RBL48 REF SRM 53-70-00 FIG 1A VOL I. (MAJOR REPA
- [SDR FDEA202008122441](https://openairdocs.org/sdr/FDEA202008122441.md): Skin · chafed · Aug 12, 2020 · N383FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE TO TAILCONE MATING SURFACE, TOP LEFTHAND SIDE (WHERE TAILCONE MATES TO FUSELAGE), LAND IS WORN AND CRACKED. REPAIRED PER EA 8-5530-T0356709 "STABILIZERS-VERTICAL STABILIZER LT DRAG ANGLE AND SKIN REPAIR."
- [SDR FDEA202007231632](https://openairdocs.org/sdr/FDEA202007231632.md): Valve · leaking · Jul 23, 2020 · N383FE · Doug MD1010F · Hydraulic System, Main
  > WHILE TAXING RECEIVED LEVEL 2 HYD 2 FAIL AND QUANTITY SHOWED ZERO. ENGINES AND PUMPS WERE RUNNING WHILE QUANTITY AT ZERO. ENGINES AND PUMPS WERE RUNNING WHILE QUANTITY AT ZERO, FOUND HYD LEAK AT 2-1 NON REV MOTOR PUMP SHUTOFF VALVE. R & R SHUTOFF VALVE, R
- [SDR FDEA2019021100330](https://openairdocs.org/sdr/FDEA2019021100330.md): Switch · out of adjust · Feb 10, 2019 · N383FE · Doug MD1010F · Passenger/Crew Doors
  > PDIS 383 52-10 7066 08FEB19 MEM FACT U LOGPAGES:3071704 DOOR L1 WILL NOT CLOSE ALL THE WAY LIGHT SHOWING AT THE TOP MEL 08FEB19 15:43 MEM U RELEASED FOR SERVICE PER MEL: 52-10-01 CATEGORY: C EXPIRATION: 18FEB19 "MEL 52-10-01: L1 ELECT
- [SDR FDEA201810052792](https://openairdocs.org/sdr/FDEA201810052792.md): Skin · cracked · Oct 5, 2018 · N383FE · Doug MD1010F · Ailerons
  > DURING LT WING O/B AILERON INSTALL L/E FORWARD I/B SKIN IS CRACKED. ACCOMPLISHED EA 8-5750-T0342670, WINGS - FLIGHT SURFACES - LT WING, O/B AILERON, L/E I/B SKIN CRACK - PARTIAL SKIN REPLACEMENT REPAIR - COVER EA MAJOR REPAIR.
- [SDR FDEA201810022765](https://openairdocs.org/sdr/FDEA201810022765.md): Skin · dented · Oct 2, 2018 · N383FE · Doug MD1010F · Elevator, Plate/Skin
  > RT INBD ELEVATOR LWR SURFACE HAS (1 EACH) DENTS. EVALUATED DENT RT I/B ELEVATOR LWR SURFACE, FOUND TO BE OUT OF LIMITS IAW SRM 55-00-01 FIG 1A. REPAIRED DENT IAW SRM 55-00-01 FIG NR 3. REF EA 8-5520-T0342588. STABILIZERS - ELEVATORS - RT I/B ELEVATOR, LWR SUR
- [SDR FDEA201809212650](https://openairdocs.org/sdr/FDEA201809212650.md): Support · damaged · Sep 21, 2018 · N383FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT FLOOR STRUCTURAL SUPPORT IS BROKEN LOCATED AT BODY STATION 1259 AT RH SIDE X82 AT AREA LOCATED UNDERNEATH MAIN CARGO COMPT. FLOOR PANELS 252LF AND 262BF. REMOVED CRACKED ANGLE FLOOR SUPPORT IAW MD-10 SRM 51-31-01. RECEIVED FABBED F
- [SDR FDEA201809202633](https://openairdocs.org/sdr/FDEA201809202633.md): Frame · corroded · Sep 20, 2018 · N383FE · Doug MD1010F · Fuselage Main, Frame
  > AFT CARGO AT STA 1787 RBL 10 BELOW FLOOR PNL, FRAME LOWER AREA HAS CORROSION. REMOVED AND REPLACED LOWER J-ANGLE AT AFT CARGO PIT STA 1781 RBL 10 BELOW FLOOR PNL FRAME IAW SRM 51-33-01. MAJOR REPAIR.
- [SDR FDEA2018091852550](https://openairdocs.org/sdr/FDEA2018091852550.md): Skin Panel · gouged · Sep 15, 2018 · N383FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FWD CARGO DOOR CUT OUT AFT LOWER SECTION PREVIOUS REPAIR SKIN EDGE HAS GOUGED. REMOVED EXISTING REPAIR DOUBLER LWR FWD CARGO DOOR CUT OUT IAW SRM 51-31-00. INSTALLED REPAIR DOUBLER LWR FWD CUTOUT IAW SRM 53-20-00. THIS IS A CLASS 2 REPAIR. MAJOR REPAIR
- [SDR FDEA201807141713](https://openairdocs.org/sdr/FDEA201807141713.md): None · none · Jul 14, 2018 · N383FE · Doug 600N · Fuel Indicating System
  > TANK 3 TIP TRAPPED & TNK 3 FUEL QTY LO ALERT AT CRUISE FUEL QTY- 21.0K, QRH COMPLIED WITH. ELECTED TO PUT FUEL SYSTEM MANUAL AND TRANSFER FUEL FROM TANK NR 2. ALERT WENT AWAY. FUEL SYSTEM BACK TO AUTO. ALERTS RETURN DURING ARRIVAL AND APPROACH. FUEL QTY 16K.
- [SDR FDEA201805221271](https://openairdocs.org/sdr/FDEA201805221271.md): Heat Exchanger · failed · May 22, 2018 · N383FE · Doug MD1010F · Engine Oil Temperature
  > DURING CLIMBOUT, THE NR 2 ENGINE OIL TEMP PEAKED AT 184 DEGREES IN THE RED BAND AND ALSO RECEIVED A LEVEL 2 ALERT FOR NR 2 ENG OIL TEMP HIGH. SHUTDOWN THE NR 2 ENGINE ALL OTHER ENGINE PARAMETERS NORMAL. NO VIBRATIONS. COMPLETED INSTALLATION OF THE NR 2

Next page: https://openairdocs.org/deregistered/N383FE-2024-03-02/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 = 'N383FE' AND deregistration_id = 'N383FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N383FE-2024-03-02/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.