# Service difficulty reports: N320FE

A list on [N320FE](https://openairdocs.org/aircraft/N320FE.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 · 183 reports

- [SDR FDEA202110062471](https://openairdocs.org/sdr/FDEA202110062471.md): Fuse · leaking · Oct 6, 2021 · N320FE · Doug MD1030F · Hydraulic System, Main
  > ON SHORT FINAL AT KIND WITH SLATS EXTENDED AND FLAPS 22 DEG WE EXTENDED THE LANDING GEAR. VERY SOON AFTER EXTENDING THE LANDING WHILE PERFORMING THE BEFORE LANDING CHECKLIST, WE RECEIVED A LEVEL 2 HYD 3 FAIL ALERT. WE IMMEDIATELY CALLED UP THE HYD SYNOPTIC A
- [SDR FDEA202007311734](https://openairdocs.org/sdr/FDEA202007311734.md): Warning Message · illuminated · Jul 31, 2020 · N320FE · Doug MD1030F · Pneumatic Indicating System
  > LEVEL 1 AIR SYS 3 OFF ILLUMINATED FOURTEEN MINUTES INTO FLIGHT AT FL 280. ASSOCIATED BLEED (3) AND PACK (3) OFF. RED DUCT LINE ILLUMINATED ON AIR SYNOPTIC. COMPLIED WITH QRH. REF MM 36-00-01-5, PERFORMED DECAY CHECK OF #3 PNEUMATIC SYSTEM, DECAY CHECK PA
- [SDR FDEA2020071091474](https://openairdocs.org/sdr/FDEA2020071091474.md): Warning Light · false activation · Jul 9, 2020 · N320FE · Doug MD1030F · Pneumatic Distribution System
  > LVL 1 AIR SYS OFF ALERT. AIR SYS AUTOMATICALLY SHUT OFF NR 3 BLEED AND NR 3 PACK. NR 3 DUCT WENT MOMENTARILY RED PRIOR TO AUTO SHUTDOWN OF NR 3 AIR SYS. CHECKED PNEUMATIC MANIFOLD FAULT INDICATOR IN CAC. NO FAULT BALLS ARE ILLUMINATED. CHECKED AIU'S,
- [SDR FDEA202006201300](https://openairdocs.org/sdr/FDEA202006201300.md): Warning Message · false activation · Jun 20, 2020 · N320FE · Doug MD1030F · Emergency Lighting
  > EMER LT BAT 1 LOW ON PREFLIGHT PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MD-10-30 AMM 33-50-00-5-0. OPS CHECK GOOD; OK FOR SERVICE.
- [SDR FDEA2020062301300](https://openairdocs.org/sdr/FDEA2020062301300.md): Battery · low voltage · Jun 20, 2020 · N320FE · Doug MD1030F · Emergency Lighting
  > EMER LIGHT BAT 1 LOW ON PREFLIGHT.
- [SDR FDEA202006161253](https://openairdocs.org/sdr/FDEA202006161253.md): Control Module · failed · Jun 16, 2020 · N320FE · Doug MD1030F · Trailing Edge Flap Control System
  > ON APPROACH SLATS EXTENDED, FLAPS WOULD NOT MOVE, HANDLE STUCK. EXECUTED A GO AROUND. SPENT SOME TIME WIGGLING THE HANDLE AND DIAL- AND-FLAP AND FINALLY GOT THEM TO MOVE. AFTER LANDING CLEANED UP THE WING AND ATTEMPTED TO EXTENDED FLAPS AGAIN. HANDLE STU
- [SDR FDEA2019112633066](https://openairdocs.org/sdr/FDEA2019112633066.md): Beam · corroded · Nov 23, 2019 · N320FE · Doug MD1030F · Fuselage Main, Structure
  > CORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK 0.045". OUT OF LIMITS. FABRICATED ANGLE ON T19/1450803. INSTALLED ANGLE IAW SRM 51-31-01 VOL
- [SDR FDEA2019111542960](https://openairdocs.org/sdr/FDEA2019111542960.md): Landing · cracked · Nov 14, 2019 · N320FE · Doug MD1030F · Horizontal Stabilizer, Plate/Skin
  > H-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO 8- 5310-T0350635 PT1 TITLE: FUSELAGE - MAIN F
- [SDR FDEA2019111542959](https://openairdocs.org/sdr/FDEA2019111542959.md): Stop · worn · Nov 14, 2019 · N320FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > LATCH STOPS WORN ACCESS PANEL 311AB RH SIDE. TITLE: FUSELAGE - PLATES AND SKINS - 311AB ACCESS DOOR CUTOUT LANDING SKIN RH FWD DAMAGE REPAIR WAS ACCOMPLISHED ON EA 8-5310-T0350318. MAJOR REPAIR
- [SDR FDEA2019111522935](https://openairdocs.org/sdr/FDEA2019111522935.md): Nut Plate · damaged · Nov 12, 2019 · N320FE · Doug MD1030F · Trailing Edge Flaps
  > LT I/B FLAP INBOARD HOIST FITTING HAS 2 EACH NUT PLATES STRIPPED OUT. REMOVED AND REPLACED 2 EA NUT PLATES ON LT I/B FLAP I/B HOIST FITTING IAW DWG ARC2369 AND SRM 51-31-01 VOL II. SKIN SPLICE REPAIR IAW SRM 57-10-00 FIG 86 VOL I. RSC TRACKING ON EA T8-5750
- [SDR FDEA2019102412717](https://openairdocs.org/sdr/FDEA2019102412717.md): Floor Panel · damaged · Oct 21, 2019 · N320FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL BETWEEN STA 595 AND STA 675 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 595 TO STA 675 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELERR T19/1448546 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2019102412716](https://openairdocs.org/sdr/FDEA2019102412716.md): Floor Panel · damaged · Oct 21, 2019 · N320FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL BETWEEN STA 765 AND STA 795 BETWEEN X91.5 AND X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 765 TO 795 BEWTEEN X91.5 AND X107.5 FABRICATED ON VTMAE TRAVELER T19/1448549 IAW SRZ-25-005 CAT "A" MAJOR REPAIR
- [SDR FDEA2019102412715](https://openairdocs.org/sdr/FDEA2019102412715.md): Floor Panel · damaged · Oct 21, 2019 · N320FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELER T19/1448544 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2019102412714](https://openairdocs.org/sdr/FDEA2019102412714.md): Floor Panel · damaged · Oct 21, 2019 · N320FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL BETWEEN STA 675 AND STA 735 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 675 - STA 735 BETWEEN X27.5 TO X47.5 FABRICATED ON VTMAE TRAVELER T19/1448545 IAW SRZ-25-005 CAT "A" MAJOR REPAIR
- [SDR FDEA2019102412713](https://openairdocs.org/sdr/FDEA2019102412713.md): Floor Panel · damaged · Oct 21, 2019 · N320FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL BWTWEEN STA 595 AND STA 675 BETWEEN -X75.5 AND -X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 595-675 AND BETWEEN -X75.5 AND -X107.5 FABRICATED ON MAE TRAVELER T19/1448049 IAW SRZ 25-005. CAT "A" MAJOR REPAIR.
- [SDR FDEA2018042601108](https://openairdocs.org/sdr/FDEA2018042601108.md): Light · malfunctioned · Apr 24, 2018 · N320FE · Doug MD1030F · Indicating/Recording System
  > DURING PREFLIGHT, WHEN SELECTING EMERGENCY PWR SWITCH TO ARM, THE ON LIGHT REMAINED ILLUMINATED. RESET FUEL LEVERS. ACFT HAD POWER DROP OFF DURING PREFLIGHT. COMPLIED WITH AN OPS TEST IAW AMM 24-00-00-5. OK FOR SERVICE.
- [SDR FDEA201712283460](https://openairdocs.org/sdr/FDEA201712283460.md): Transmitter · out of adjust · Dec 28, 2017 · N320FE · Doug MD1030F · Trailing Flap Position Indicating System
  > AT 121 KNOTS DURING TAKEOFF, RECEIVED AN AUDIBLE WARNING FOR THE FLAPS, FOLLOWED BY A WARNING FOR THE SLATS.. REJECTED TAKEOFF AT 130 KNOTS. PERFORMED A FLAP INDICATION TEST, FOUND TRANSMITTER IN LIMITS. LIB, RIB, & LOB ARE BELOW OR AT LOW END OF TOLERAN
- [SDR FDEA201711043166](https://openairdocs.org/sdr/FDEA201711043166.md): Bulkhead · cracked · Nov 4, 2017 · N320FE · Doug MD1030F · Fuselage Main, Bulkhead
  > NR 3 AC PACK COMPARTMENT STA 475 BULKHEAD WEB, A/C CHECK VALVE FASTENER HOLE AT 4:30 POSITION HAS A.5 INCH CRACK PROPAGATING THROUGH HOLE. REPAIRED PER EA 8-5310-T0336280.
- [SDR FDEA201710102886](https://openairdocs.org/sdr/FDEA201710102886.md): Panel · delaminated · Oct 10, 2017 · N320FE · Doug MD1030F · Wing, Plate/Skin
  > LT WING, PANEL 541 LB IS DELAMINATED/SPLIT. REPAIRED LT WING, PANEL 541 LB AT THE DELAMINATED/SPLIT AREA REF SRM 51-71-00 VOL 2 PG 1-47 AND DRAWING NUMBER ARC0357.
- [SDR FDEA201710042856](https://openairdocs.org/sdr/FDEA201710042856.md): Seat Track · worn · Oct 4, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK APPROX STA 1265, CENTER LINE X.8.5 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710042855](https://openairdocs.org/sdr/FDEA201710042855.md): Seat Track · worn · Oct 4, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 625, RBL 27.5 IS DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710042854](https://openairdocs.org/sdr/FDEA201710042854.md): Seat Track · damaged · Oct 4, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 1581, LBL 75 DAMAGED. REPAIRED IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710042853](https://openairdocs.org/sdr/FDEA201710042853.md): Seat Track · damaged · Oct 4, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK BS 565, LBL 8.5 SHOWS DAMAGE. REPAIRED IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710033020](https://openairdocs.org/sdr/FDEA201710033020.md): Channel · cracked · Oct 3, 2017 · N320FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > NR 3 A/C COMPARTMENT BS 555, LONGERON 34R FRAME J-CHANNEL HAS A 1.5 INCH CRACK. INSTALLED A TYPICAL FORMED CHANNEL REPAIR IAW SRM 53-00-01, FIG.8, SHEET 2, PAGE 30 & 31, VOL I.
- [SDR FDEA201710032846](https://openairdocs.org/sdr/FDEA201710032846.md): Seat Track · damaged · Oct 3, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPT APPROX STA 1601 RBL 75 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710032844](https://openairdocs.org/sdr/FDEA201710032844.md): Seat Track · worn · Oct 3, 2017 · N320FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, APPROX STA 1039 LBL 75 GROOVE/ GOUGE WORN INTO TRACK. SEAT TRACK IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710012877](https://openairdocs.org/sdr/FDEA201710012877.md): Frame · cracked · Oct 1, 2017 · N320FE · Doug MD1030F · Fuselage Main, Frame
  > CENTER CARGO BAY, APPROXIMATELY BS 1841, LBL 6 AND RBL 6, FRAME WEB IS CRACKED. REPAIRED THE FRAME IAW SRM 51-00-01, FIG 10, SHT 5, VOL I.
- [SDR FDEA201709303046](https://openairdocs.org/sdr/FDEA201709303046.md): Skin · cracked · Sep 30, 2017 · N320FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER SKIN HAS A.75 INCH CRACK AT XOF 572. 5 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709303045](https://openairdocs.org/sdr/FDEA201709303045.md): Skin · cracked · Sep 30, 2017 · N320FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A.4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709303044](https://openairdocs.org/sdr/FDEA201709303044.md): Skin · cracked · Sep 30, 2017 · N320FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER SKIN HAS A 2.0 IN. CRACK AT XOF 563. 12 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709283088](https://openairdocs.org/sdr/FDEA201709283088.md): Skin · cracked · Sep 28, 2017 · N320FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT UPPER AFT CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-T0336191.
- [SDR FDEA201709283087](https://openairdocs.org/sdr/FDEA201709283087.md): Skin · cracked · Sep 28, 2017 · N320FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT, AFT LOWER CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-0336191. MAJOR REPAIR.
- [SDR FDEA201709283028](https://openairdocs.org/sdr/FDEA201709283028.md): Door · cracked · Sep 28, 2017 · N320FE · Doug MD1030F · Air Conditioning Doors
  > LOWER FUSELAGE NR 3 ACM ACCESS DOOR UPPER FLANGE PREVIOUS REPAIR HAS CONTINUED TO CRACK. REPAIRED THE NR 3 ACM DOOR UPPER FLANGE CRACK IAW EA 8-5240-T0336127.
- [SDR FDEA201709273132](https://openairdocs.org/sdr/FDEA201709273132.md): Tee Fitting · cracked · Sep 27, 2017 · N320FE · Doug MD1030F · Fuselage Main, Bulkhead
  > BS 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH. CRACK EXTENDED THROUGH THE RADIUS. REPAIED THE BULKHEAD TEE CAP IAW EA T 8-5310-T0335740, PART 1 & 2.
- [SDR FDEA201709273003](https://openairdocs.org/sdr/FDEA201709273003.md): Bulkhead Web · cracked · Sep 27, 2017 · N320FE · Doug MD1030F · Fuselage Main, Bulkhead
  > NOSE WHEEL WELL RIGHT VERTICAL PANEL AT APPROX STA 480 HAS A CRACK APPROX 6 INCH LONG. INSTALLED WEB SECTION AND DOUBLERS REF. SRM 53-00-01 FIG.10 (SHEET 5) VOLI.
- [SDR FDEA201709272925](https://openairdocs.org/sdr/FDEA201709272925.md): Web · cracked · Sep 27, 2017 · N320FE · Doug MD1030F · Fuselage Main, Structure
  > NOSE WHEEL WELL LEFT VERTICAL WEB PANEL BS 315, HAS A CRACK BEHIND THE HYDRAULIC LINES. REMOVED AND REPLACED DAMAGED SECTION OF THE WEB IAW SRM 53-00-01, FIG 10, SHT 4, 5, 7, PGS 50, 51, 53, AND DWG NCA6046, AND ACA3837.
- [SDR FDEA201704201245](https://openairdocs.org/sdr/FDEA201704201245.md): Warning Message · false indication · Apr 20, 2017 · N320FE · Doug MD1030F · Pneumatic Indicating System
  > AT FL 350, HAD A LEVEL 3 AIR MANIFOLD 3 FAILURE. RAN QRH, ALERT WENT AWAY. DECLARED AN EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT. CHECKED MANIFOLD FAILURE INDICATORS IN CAC AND FOUND RT MANIFOLD PRESSURE SWITCH FAULTING IAW AMM 36-23-03-4-0, 36-0
- [SDR FDEA201701030027](https://openairdocs.org/sdr/FDEA201701030027.md): Warning Light · false activation · Jan 3, 2017 · N320FE · Doug MD1030F · Passenger/Crew Doors
  > R1 DOOR SLIDE LIGHT ILLUMITATED. PERFORMED OPERATIONAL CHECK OF THE R1 DOOR SLIDE BOTTLE PRESSURE LIGHT IAW AMM 25-61-03-5-0. TESTED GOOD SEVERAL TIMES. OK FOR SERVICE.
- [SDR FDEA201602140557](https://openairdocs.org/sdr/FDEA201602140557.md): Test Switch · faulty · Feb 14, 2016 · N320FE · Doug MD1030F · Emergency Equipment
  > R1 DOOR EVAC SLIDE, REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 24 FEB 16. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH
- [SDR FDEA201510263375](https://openairdocs.org/sdr/FDEA201510263375.md): Skin Panel · cracked · Oct 26, 2015 · N320FE · Doug MD1030F · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER SKIN PANEL 7281-1, HAS A.700" CRACK JUST FWD OF REAR SPAR CAP, FWD BARREL NUT HOLE. R & R SECTION OF SKIN PANEL, PLANK, IAW EA 8-5510-T0320816.
- [SDR FDEA201510263374](https://openairdocs.org/sdr/FDEA201510263374.md): Spar Cap · cracked · Oct 26, 2015 · N320FE · Doug MD1030F · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER, UPPER OUTER REAR SPAR CAP, FWD BARREL NUT HOLE HAS A.400" VERTICAL CRACK EXTENDING FROM BELOW THE BARREL NUT AT THE 5:00 POSITION. R & R SECTION OF REAR SPAR CAP IAW EA 8-5510-T0320816.
- [SDR FDEA201510233327](https://openairdocs.org/sdr/FDEA201510233327.md): Panel · delaminated · Oct 23, 2015 · N320FE · Doug MD1030F · Wing, Plate/Skin
  > LEFT WING HINGE PANEL 551DB HAS DELAMINATION. REPAIRED THE HINGE PANEL IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510223316](https://openairdocs.org/sdr/FDEA201510223316.md): Panel · delaminated · Oct 22, 2015 · N320FE · Doug MD1030F · Nacelle/Pylon, Plate/Skin
  > AFT ENG INLET DUCT, RT SIDE PANEL 364JR, LOWER SFT DELAMINATED. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510223315](https://openairdocs.org/sdr/FDEA201510223315.md): Panel · delaminated · Oct 22, 2015 · N320FE · Doug MD1030F · Nacelle/Pylon, Plate/Skin
  > AFT ENG INLET DUCT, RT SIDE PANEL 364JR DELAMINATED, LOWER FWD. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL. II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203292](https://openairdocs.org/sdr/FDEA201510203292.md): Fuel Door · damaged · Oct 20, 2015 · N320FE · Doug MD1030F · Wing, Plate/Skin
  > RIGHT WING REFUEL & DEFUEL DOOR, PUNCTURED ON UPPER MID SURFACE. REPAIR IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203291](https://openairdocs.org/sdr/FDEA201510203291.md): Panel · delaminated · Oct 20, 2015 · N320FE · Doug MD1030F · Spoilers
  > LEFT WING NR 5 SPOILER PANEL HAS DELAMINATION, UPPER SURFACE. REPAIR SPOILER IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203285](https://openairdocs.org/sdr/FDEA201510203285.md): Wire · damaged · Oct 20, 2015 · N320FE · Doug MD1030F · Electrical Power System Wiring
  > FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE OF ACFT. SPLICED IN A NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 29-12-01, AND E8-2810-7-5002 PT 1.
- [SDR FDEA201510203284](https://openairdocs.org/sdr/FDEA201510203284.md): Wire · damaged · Oct 20, 2015 · N320FE · Doug MD1030F · Electrical Power System Wiring
  > FOUND DAMAGED WIRE LOCATED AT BS 1346, RT SIDE OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 33-32-02, AND E8-2810-7-5002 PT1.
- [SDR FDEA201510203283](https://openairdocs.org/sdr/FDEA201510203283.md): Wire · damaged · Oct 20, 2015 · N320FE · Doug MD1030F · Electrical Power System Wiring
  > FOUND WIRE DAMAGED, LOCATED AT BS 1240, RT SIDE OF CENTERLINE OF ACFT. REPLACED WIRE IAW SWPM 20-10-03, 20-00-16, WDM 28-21-03, AND E8-2810-7-5002 PT1.
- [SDR FDEA201510203282](https://openairdocs.org/sdr/FDEA201510203282.md): Wire · damaged · Oct 20, 2015 · N320FE · Doug MD1030F · Electrical Power System Wiring
  > FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00- 16, WDM 52-33-01 AND E8-7-2810-5002 PT1.

Next page: https://openairdocs.org/aircraft/N320FE/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 = 'N320FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N320FE/reports

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