# Service difficulty reports: N321FE

A list on [N321FE](https://openairdocs.org/aircraft/N321FE.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 4 · 193 reports

- [SDR FDEA202211182822](https://openairdocs.org/sdr/FDEA202211182822.md): Vane · delaminated · Nov 18, 2022 · N321FE · Doug MD1030F · Trailing Edge Flaps
  > L/H O/B FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED L/H O/B FLAP VANE AT #5 RUBSTRIP AS REQUIRED PER SRM 51-71-00, VOL.II, PARA. #17 PG. 75-80, INADDITION WITH SRM 57-00-01, VOL.I, PG. 11, FIG.#4 REF. JPF STEPS ON BACK 4-11. MAJOR REPAIR.
- [SDR FDEA202211172813](https://openairdocs.org/sdr/FDEA202211172813.md): Rub Strip · delaminated · Nov 17, 2022 · N321FE · Doug MD1030F · Wing Miscellaneous Structure
  > DELAMINATED RUBSTRIP. R & R THE RUB STRIP IAW DWG ARC1455.
- [SDR FDEA202211162828](https://openairdocs.org/sdr/FDEA202211162828.md): Vane · delaminated · Nov 16, 2022 · N321FE · Doug MD1030F · Trailing Edge Flaps
  > LH OUTBD FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED PER SRM 57-00-01 FIG.4, SHEET 1
- [SDR FDEA2021083062136](https://openairdocs.org/sdr/FDEA2021083062136.md): Frame · corroded · Aug 26, 2021 · N321FE · Doug MD1030F · Fuselage Main, Frame
  > INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & # 2 ACM AT STATION 541.667 BOTTOM OF ACA3348-3 FRAME HAS CORROSION AT LOWER FLANGE. REPAIRED INBOARD LOWER FLANGE OF ACA 3348-3 WEB. REF SRM 53-00-01 FIG. 8 VOL. 1 AND DAC DWG ACA 3348.
- [SDR FDEA202108252115](https://openairdocs.org/sdr/FDEA202108252115.md): Angle · corroded · Aug 25, 2021 · N321FE · Doug MD1030F · Fuselage Main, Structure
  > INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & #2 ACM APPROX. STA 540 AT BOTTOM OF BULKHEAD VERTICAL FLANGE OF CHORD ANGLE HAS EXFOLIATION CORROSION APPROX. FOUR SQUARE INCHES. (MKD) 0003748737: KOTSOGLOU, CHRISTOPHER - 28-AUG-2021 03:26 REMOVED, FA
- [SDR FDEA2021083042114](https://openairdocs.org/sdr/FDEA2021083042114.md): Rib · cracked · Aug 24, 2021 · N321FE · Doug MD1030F · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB L/E - PNL #371CLE HAS CRACKED RIB - 7TH FROM BOTTOM L/H SIDE TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER REFERENCE SRM 55-00-01 FIG. 7 SHEET 1 VOL. 1. "MAJOR REPAIR"
- [SDR FDEA202108232076](https://openairdocs.org/sdr/FDEA202108232076.md): Skin · cracked · Aug 23, 2021 · N321FE · Doug MD1030F · Rudder Structure
  > LOWER AFT RUDDER, BOTTOM RHS AFT SECTION HAS AN APPROX 1" CRACK, MARKED. REMOVED AND REPLACED LOWER AFT RUDDER. REF AMM 27-20-01-4 INSTALLED P/N: NMC6015- 505 S/N: 48450.
- [SDR FDEA202108212055](https://openairdocs.org/sdr/FDEA202108212055.md): Skin · delaminated · Aug 21, 2021 · N321FE · Doug MD1030F · Elevator, Plate/Skin
  > R/H O/B ELEVATOR TRAILING EDGE DELAM. (MARKED) REPAIRED O/B TRAILING EDGE ELEVATOR ENVELOPE PER SRM 55-30-00 VOL.1 PGS 1-9. "MAJOR REPAIR"
- [SDR FDEA202108092002](https://openairdocs.org/sdr/FDEA202108092002.md): Skin · dented · Aug 9, 2021 · N321FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN DENT/CREASE - AFT OF CENTER CARGO AT APPROX STA.1850 BETWEEN LONGS 38-39. CUT OUT DAMAGED SKIN AT STA. 1850 BETWEEN LONGERONS 38R AND 39R AND INSTALLED REPAIR PER SRM 53-20-00 FIG. 6 SH.12-15 VOL.1. "MAJOR REPAIR"
- [SDR FDEA202107241851](https://openairdocs.org/sdr/FDEA202107241851.md): Skin · damaged · Jul 24, 2021 · N321FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING O/B FLAP UPPER I/B T/E SPLIT AT CONNECTION AND DAMAGED AT CORNER. (DOT 6) REMOVED, FABRICATED AND INSTALLED L/H WING O/B FLAP UPPER I/B T/E DAMAGED SECTION REF SRM 57-20-00 VOL 1 PARAGRAPH 13 STEPS A-E.
- [SDR FDEA202107211829](https://openairdocs.org/sdr/FDEA202107211829.md): Floorboard · damaged · Jul 21, 2021 · N321FE · Doug MD1030F · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL ADA0241-51(127WF) FABRICATED NEW FLOOR REF FEDEX DWG SRZ-25-005
- [SDR FDEA202107131969](https://openairdocs.org/sdr/FDEA202107131969.md): Lock · sheared · Jul 13, 2021 · N321FE · Doug MD1030F · Wing Main, Frame Structure
  > L/H WING TOP SURFACE - TAPER LOCK STICKING UP FROM TOP SURFACE OF WING - APPROXIMATE STA XORS 275 ON GROSS WEIGHT MOD DOUBLER AFT OF REAR SPARE 0003748737: KOTSOGLOU, CHRISTOPHER - 14-AUG-2021 04:01 REMOVED AND REPLACED L/H WING TOP SURFACE FASTENER PER
- [SDR FDEA202107131848](https://openairdocs.org/sdr/FDEA202107131848.md): Frame · worn · Jul 13, 2021 · N321FE · Doug MD1030F · Fuselage Main, Frame
  > CENTER CARGO COMPT FUSE FRAM SECTION REMOVED TO FOM STA 1787 L47R-L49R. INSTALLED STA. 1787 FRAME SECTION FROM LONGERON 47R TO 49R REF DOUGLAS DRAWING AFA 7112. INSTALLED FRAME REPAIR CHANNELS AND REPAIR STRAP BETWEEN L45R-L46R REF EA 8-5310-T0363372 " FU
- [SDR FDEA202107131919](https://openairdocs.org/sdr/FDEA202107131919.md): Frame · damaged · Jul 13, 2021 · N321FE · Doug MD1030F · Fuselage Main, Frame
  > CENTER CARGO COMPT FUSE FRAME SECTION REMOVED TO FOM STA 1801 L47L-L45R. INSTALLED STA. 1801 FRAME SECTION FROM LONGERON 47L AT B/P SPLICE TO 45R REF.DOUGLAS DRAWING AFA7166. INSTALLED FRAME SPLICE AT LONGERON 45R REF. EA 8- 5310-T0363251 "FUSELAGE-MAIN F
- [SDR FDEA202107131847](https://openairdocs.org/sdr/FDEA202107131847.md): Longeron · worn · Jul 13, 2021 · N321FE · Doug MD1030F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO COMPT L47R HAS EXFOLITATION CORROSION ON INBOARD SIDE STA 1775. INSTALLED NEW SECTION OF LONGERON 47R FROM EXISTING SPLICE LOCATION AT STA. 1775 TO REPAIR SPLICE AT STA. 1811. REF. SRM 53-10-00 FIG. 2 VOL.1 AND DOUGLAS DRAWING AGA7027.
- [SDR FDEA202107131772](https://openairdocs.org/sdr/FDEA202107131772.md): Floor Panel · delaminated · Jul 13, 2021 · N321FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR BOARD AT STATION 1039 L/H SIDE WITH 5/L MARKING FOUND TO BE SPONGE/SOFT FABRICATED NEW FLOOR PANEL MAIN DECK AT STATION 1039 L/H SIDE WITH 5/L MARKING REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202107101939](https://openairdocs.org/sdr/FDEA202107101939.md): Support · corroded · Jul 10, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT LAV SUPPORT AGA7087-504 STATION 1891-2007 RBL-24 EXFOLIATION CORROSION EXISTS UNDER DOME NUTS. INSTALLED NEW/FABRICATED AFT LAV SUPPORT ON MAIN CABIN AT STATION 1891-2007 RBL 24 REF, DOUGLAS DWG NO. AGA7087 AND MD10-30 SRM 51-31-01 VOL 2.
- [SDR FDEA202107091846](https://openairdocs.org/sdr/FDEA202107091846.md): Rib · cracked · Jul 9, 2021 · N321FE · Doug MD1030F · Wing, Rib/Bulkhead
  > R/H WING UPPER FILLET PANEL SUPPORT RIB ANB7142-10 AT STATION 1341 CRACKED LOWER END. REMOVED AND REPLACED RIGHT HAND WING UPPER FILLET PANEL SUPPORT RIB ANB7142- 10 AT STATION 1341 I.A.W DAC DWG ANB7102 AND SRM 51-31-01 VOL. 2.
- [SDR FDEA202107082023](https://openairdocs.org/sdr/FDEA202107082023.md): Bulkhead Web · worn · Jul 8, 2021 · N321FE · Doug MD1030F · Fuselage Main, Bulkhead
  > MAIN CARGO STATION 2007 LBL 30 HOLE DAMAGED ON PRESSURE BULKHEAD AT FLOOR BOARD SUPPORT TEE REPAIRED HOLE PER SRM 51-39-01 VOL II. REF. E.A # 8-5310-T0363077 TITTLE: FUSELAGE-MAIN FRAME- AFT PRESSURE BULKHEAD WEB AND DOUBLER DAMAGED AT FASTENER HOLE. "MA
- [SDR FDEA202107061942](https://openairdocs.org/sdr/FDEA202107061942.md): Support · corroded · Jul 6, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT LAV SUPPORT AGA7544-1 STATION 1891-2007 LBL 24 EXFOLIATION CORROSION EXISTS ON FOWARD END BEYOND LIMITS INSTALLED NEW/FABRICATED AFT LAV SUPPORT ON MAIN CABIN AT STATION 1891-2007 LBL 24 REF, DOUGLAS DWG NO. AGA7087 AND MD10-30 SRM 51-31-01
- [SDR FDEA202106301622](https://openairdocs.org/sdr/FDEA202106301622.md): Vane · worn · Jun 30, 2021 · N321FE · Doug MD1030F · Trailing Edge Flaps
  > R/H INB'D T/E FLAP VANE INB'D L/E AREA SHOWING RUBBING DAMAGE. REPAIRED R/H INB FLAP VANE I/B L/E PER SRM 51-71-00 VOL II PAR 16 PG 64. I.A.W. SRM 57-00-01 FIG 4 SHEET 1. RSC TRACKING E.A. 8-5750-T-0362626 FLT. SURFACES - R/H I/B FLAP VANE STRUCTURE R
- [SDR FDEA202106221811](https://openairdocs.org/sdr/FDEA202106221811.md): Longeron · corroded · Jun 22, 2021 · N321FE · Doug MD1030F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO COMP. APPROX. STA 1750 TO 1781 LONG 46R FOUND SEVERAL AREAS OF CORROSION INSIDE HAT SECTION OF LONGERON. (MKD) REMOVED CORRODED SECTIONS AND INSTALLED NEW SECTIONS OF LONGERON 46R FROM STA. 1671 AT EXISTING SPLICE LOCATION TO STA. 1831. REPA
- [SDR FDEA202106221647](https://openairdocs.org/sdr/FDEA202106221647.md): Frame · cracked · Jun 22, 2021 · N321FE · Doug MD1030F · Wing Spar
  > LEFTHAND WING; XORS=570 LEADING EDGE INTERNAL FRAME STRAP HAS 6" CRACKS @ UPPER OUTBOARD SECTION. REMOVED AND REPLACED LEFT WING XORS 570 LEADING EDGE INTERNAL FRAME STRAP UPPER OUTBOARD SECTION REF DWG ARB3954.
- [SDR FDEA202106221592](https://openairdocs.org/sdr/FDEA202106221592.md): Angle · cracked · Jun 22, 2021 · N321FE · Doug MD1030F · Leading Edge Devices
  > L/H WING #2 SLAT OUTBOARD CAP CRACKED AT THE ANGLE #2 SLAT OUTBOARD CAP ANGLE REPAIR PER SRM 57-00-01 FIG 10 VOL 1. "MAJOR REPAIR"
- [SDR FDEA202106211812](https://openairdocs.org/sdr/FDEA202106211812.md): Longeron Splice · corroded · Jun 21, 2021 · N321FE · Doug MD1030F · Fuselage Main, Longeron/Stringer
  > CENTER GARGO COMPARTMENT BILGE - APPROX STA.1808 46R - EXFOLIATION CORROSION ON LONG AND SPLICE. REMOVED CORRODED LONGERON SECTIONS AND INSTALLED NEW SECTIONS OF LONGERON 46R FROM STA. 1671 AT EXISTING SPLICE LOCATION TO STA. 1831. REPAIR SPLICES INSTALL
- [SDR FDEA202106211626](https://openairdocs.org/sdr/FDEA202106211626.md): Web · dented · Jun 21, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPT STA 1841 AT FLOOR LEVEL WEB IS DENTED FROM CONTAINER CONTACT. MRKD LBL 15 TO RBL 5. REMOVED AND REPLACED DAMAGED WEB AGA7170-3 IAW DAC DWG AGA7170 AND SRM 51-31- 01 VOL. 2.
- [SDR FDEA202106192025](https://openairdocs.org/sdr/FDEA202106192025.md): Floor Support · corroded · Jun 19, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. LBL24, (MARKED #13) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SRM 51-33-01 VOL. 2. AND DAC DWG NJC6040.
- [SDR FDEA202106192024](https://openairdocs.org/sdr/FDEA202106192024.md): Floor Support · corroded · Jun 19, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. RBL24, (MARKED #12) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SRM 51-33-01 VOL. 2. AND DAC DWG NJC6040.
- [SDR FDEA202106191783](https://openairdocs.org/sdr/FDEA202106191783.md): Floor Support · corroded · Jun 19, 2021 · N321FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPT MAIN DECK FLOORBOARD SUPPORT CORRODED STA 1741 RBL 55. MRKD REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA. 1741 RBL 55 CTR CARGO COMPT. PER SRM 51-31-01 VOL 2 AND DWG NO. S2929169
- [SDR FDEA202106181665](https://openairdocs.org/sdr/FDEA202106181665.md): Skin · corroded · Jun 18, 2021 · N321FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > AFT FUSE WASTE TANK COMPT, CORROSION ON INTERIOR OF FUSELAGE SKIN, AT EXISTING EXTERIOR DOUBLER AREA, AT STA 2000 BETWEEEN L-45 AND L-45 R/H. (MARKED #11) REMOVED CORROSION FOUND TO BE WITHIN LIMETS REF SRM 53-20-00 FIG 4 SHT 2 NOTE 16 VOL 1.
- [SDR FDEA202106171699](https://openairdocs.org/sdr/FDEA202106171699.md): Door Frame · worn · Jun 17, 2021 · N321FE · Doug MD1030F · Fuselage Main, Structure
  > MAIN CARGO DECK, LH SIDE, STA. 535, LONG 23, FRAME GOUGED BY LOWER HINGE HARDWARE OF CARGO NET BRACKET. DOT #10. REMOVED DAMAGED PREVIOUS "L" ANGLE REPAIR AND INSTALLED NEW REPAIR AT STA. 535 LONGERONS 22 TO 25 REF. MD10-30 SRM 53-30-00 FIG. 13 SHEET 1 VOL
- [SDR FDEA202106171698](https://openairdocs.org/sdr/FDEA202106171698.md): Door Frame · damaged · Jun 17, 2021 · N321FE · Doug MD1030F · Fuselage Main, Structure
  > MAIN CARGO DECK, LH SIDE, STA. 535, LONG 20, FRAME GOUGED BY UPPER HINGE HARWARE OF CARGO NET BRACKET. DOT #9. REMOVED PREVIOUS "L" ANGLE REPAIR AND INSTALLED NEW REPAIR AT STA.535 LONGERON 18 TO 21 REF. MD10-30 SRM 53-30-00 FIG. 14 SHEET 1 VOL.1
- [SDR FDEA202106161814](https://openairdocs.org/sdr/FDEA202106161814.md): Seat Track · worn · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN, NEAR STA 1501 LBL 8.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 8.5 FROM STA 1501-1551 REF SRM 53-70-00 FIG 1 VOL 1, AND SRM 51-31-01 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002
- [SDR FDEA202106161813](https://openairdocs.org/sdr/FDEA202106161813.md): Seat Track · worn · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 LBL 47.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 47.5 FROM STA 1129-1149 REF SRM 53-70-00 FIG 1 VOL 1, AND SRM 51-31-01 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002
- [SDR FDEA202106161795](https://openairdocs.org/sdr/FDEA202106161795.md): Seat Track · worn · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN, NEAR STA 1370 RBL 47.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 47.5 FROM STA 1313-1411 REF SRM 53-70-00 FIG 1 PAGE 3 VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002.
- [SDR FDEA202106161794](https://openairdocs.org/sdr/FDEA202106161794.md): Seat Track · worn · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 RBL 8.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 8.5 FROM STA 1129-1069 REF SRM 53-70-00 FIG 1 PAGE 3 VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002
- [SDR FDEA202106161792](https://openairdocs.org/sdr/FDEA202106161792.md): Seat Track · worn · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, GOUGES ON SEAT TRACK LOBES AT STA 1039 LBL 78 (MARKED #18) INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 78 FROM STA 1009-1089 REF SRM 53-70-00 FIG 1 PAGE 6A VOL 1, AND SRM 51-31-01 PAGE 37 VOL 2 AND FEDEX EXPRESS DWG SR10-53-002 REF SR
- [SDR FDEA202106161713](https://openairdocs.org/sdr/FDEA202106161713.md): Skin · dented · Jun 16, 2021 · N321FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > LH FUSELAGE APPROX STA.1894 BETWEEN L43-L44 - DENT ON SKIN. REPAIRED DAMAGED SKIN REF SRM 53-20-00 FIG.6 SHEETS 12-13 VOL. 1 AND SRM 51-31-01 VOL. 2.
- [SDR FDEA202106151769](https://openairdocs.org/sdr/FDEA202106151769.md): Floorboard · damaged · Jun 15, 2021 · N321FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202106151768](https://openairdocs.org/sdr/FDEA202106151768.md): Floorboard · damaged · Jun 15, 2021 · N321FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202106151770](https://openairdocs.org/sdr/FDEA202106151770.md): Floorboard · damaged · Jun 15, 2021 · N321FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202103160657](https://openairdocs.org/sdr/FDEA202103160657.md): Engine · failed · Mar 16, 2021 · N321FE · Doug MD1030F · Turbine Engine Reduction Gear
  > APPROXIMENTELY 30 MINUTES IN TO FLIGHT (FL350) CREW HEARD A VERY LOUD BANG WITH SIGNIFICANT AIRCRAFT YAW. OBSERVED ENGINE NO 1 N1 ROLL BACK WITH CONFIRM ENG OUT ON FMS. DETERMINED N1 ON ENG 1 HAD SEIZED AND EXECUDED PHASE 1. COMPLIED AND COMPLETED ENGING 1
- [SDR FDEA2020050860906](https://openairdocs.org/sdr/FDEA2020050860906.md): Boot · defective · May 6, 2020 · N321FE · Doug MD1030F · Cabin Cooling System
  > JUST AS BEGAIN DESCENT ONTO MEM RECEIVED LEVEL ONE AIR SYST 3 OFF ALERT AT APPROX IMATELY FL370 ASSOCIATED RED MANF LT NEXT TO #3 BLEED ALSO ILLUMINATED CORRESPONDING PNEUMATIC LINE FROM #3 BLEED TO #3 PACK REMAINED ILLUMINATED FOR APPOXIMATELY 5=10 MINUT
- [SDR FDEA2020043090841](https://openairdocs.org/sdr/FDEA2020043090841.md): Adiru · failed · Apr 29, 2020 · N321FE · Doug MD1030F · Inertial Guidance System
  > AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN QRH. IT APPEARED CAPTAINS AIRSPEED WAS IN ERROR. TRIED TO SELECT AUX CADC. THIS DID NO FIX IT.
- [SDR FDEA2020043090840](https://openairdocs.org/sdr/FDEA2020043090840.md): Adc · failed · Apr 29, 2020 · N321FE · Doug MD1030F · Air Data Computer
  > AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN QRH. IT APPEARED CAPTAINS AIRSPEED WAS IN ERROR. TRIED TO SELECT AUX CADC. THIS DID NO FIX IT.
- [SDR FDEA2020010640019](https://openairdocs.org/sdr/FDEA2020010640019.md): Power Supply · failed · Jan 4, 2020 · N321FE · Doug MD1030F · Emergency Lighting
  > MDIS 321 33-50 6660 04JAN20 MEM OPEN U LOGPAGES:3133468 EMERGENCY LT BATT 1 LOW VOLTS FACT 05JAN20 22:09 MEM REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPLY
- [SDR FDEA201910142639](https://openairdocs.org/sdr/FDEA201910142639.md): Dimmer · failed · Oct 14, 2019 · N321FE · Doug MD1030F · Flight Compartment Lighting
  > DURING CLIMB ABOVE 18,000 FT, OVERHEAD PANEL WENT COMPLETELY DARK. NO INDICATION LIGHTS OF ANY KIND EXCEPT ENGINE IGNITION WERE ILLUMINATED. ON PREFLIGHT THE NR 4 & 5 DISPLAY UNITS BLANKED OUT FOR ABOUT 30 SECONDS & THE HYD PANEL SAID SELECT MANUAL. THOSE
- [SDR FDEA201909162254](https://openairdocs.org/sdr/FDEA201909162254.md): Seat · faulty · Sep 16, 2019 · N321FE · Doug MD1030F · Flight Compartment Equipment
  > CREW REPORTS CAPTAINS SEAT WILL NOT MOVE AFT MANUALLY WHEN POSITIONED FWD ALL THE WAY. REMOVED AND REPLACED CAPTAINS SEAT PER AMM 25-11-01-4, FUNCTION CHECK GOOD.
- [SDR FDEA201906301468](https://openairdocs.org/sdr/FDEA201906301468.md): Seat Track · damaged · Jun 30, 2019 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN DECK SEAT TRACK STA 735 LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 705 TO 725 REF. SRM 53-70-00 FIG. 1 VOL. 1, SRM 51-31-01 VOL. 2 AND SR10-53-002.
- [SDR FDEA201906301467](https://openairdocs.org/sdr/FDEA201906301467.md): Seat Track · damaged · Jun 30, 2019 · N321FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN DECK SEAT TRACK STA 645, LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 645 TO STATION 664, LBL 107 REF. SRM 53-70-00 FIG. 1 VOL. 1. AND DWG SR10-53-002.

Next page: https://openairdocs.org/aircraft/N321FE/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 = 'N321FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N321FE/reports

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