# Service difficulty reports: N387FE, cancelled Apr 13, 2024

A list on [N387FE, cancelled Apr 13, 2024](https://openairdocs.org/deregistered/N387FE-2024-04-13.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 2 · 64 reports

- [SDR FDEA201209253431](https://openairdocs.org/sdr/FDEA201209253431.md): Handle · malfunctioned · Sep 25, 2012 · N387FE · Doug MD1010F · Landing Gear Selector
  > ON DEPARTURE, RAISED THE GEAR AND THE RED UNSAFE INDICATIONS REMAINED ON AT THE GEAR HANDLE PANEL AND ON THE CONFIGURATION SYNOPTIC PAGE. RECYCLED THE GEAR IAW THE QRH AND GOT THE SAME RESULTS. (IAW CREW DEBRIEF ALL HYD PRESSURES NORMAL AND GEAR FELT LIKE IT
- [SDR FDEA201201260335](https://openairdocs.org/sdr/FDEA201201260335.md): Coalescer Bag · odor · Jan 26, 2012 · N387FE · Doug MD1010F · Humidity Control System
  > IN CRUISE, WITH PACK 1 & PACK 3 ON, SMELLED FUMES IN COCKPIT. TURNED ON PACK 2 AND TURNED OFF PACK 1, THE ODOR STOPPED. REPLACED COALESTER BAG ON NR1 PACK IAW MM-21-54-03-2-0. OK TO CONTINUE.
- [SDR FDEA201105171852](https://openairdocs.org/sdr/FDEA201105171852.md): Pressure Switch · failed · May 17, 2011 · N387FE · Doug MD1010F · Pneumatic Distribution System
  > AT FL 370, GOT AIR SYS 3 OFF WITH ILLUMINATED RED MFG LIGHT. RAN QRH. MOMENTARY LEVEL 3 AIR MFG 3 FAIL WITH TRI TONE, DIVERT. T/S IAW FIM 36-23 ITEM 3, CHECKED PNEUMATIC FAULT IND U1-240 FOUND RT PRESSURE SWITCH TRIPPED. PERFORMED NR 3 MANIFOLD LEAK DOW
- [SDR FDEA201009173519](https://openairdocs.org/sdr/FDEA201009173519.md): Pan · corroded · Sep 17, 2010 · N387FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AT APPROX FS 383 LAV SERVICE PANEL. THE LAV PAN HAS CORROSION AND CRACKED FLANGE. R & R PAN AND DOUBLER. REF SRM 51-35-01
- [SDR FDEA201009163510](https://openairdocs.org/sdr/FDEA201009163510.md): Bulkhead · corroded · Sep 16, 2010 · N387FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LT WHEEL WELL FWD BULKHEAD SLANT PANEL LWR OTBD CORNER HAS CORROSION. REPAIRED SLANT PANEL TO REAR SPAR CAP ANGLE. REF SRM 53-40-00
- [SDR FDEA200907202679](https://openairdocs.org/sdr/FDEA200907202679.md): Engine · malfunctioned · Jul 20, 2009 · N387FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > REJECTED T/O PDX 28L NR 2 ENGINE N2 EXCEEDENACE 90KTS. INSPECTED EXHAUST FOR PARTICLES NONE FOUND. ACFT OK FOR SERVICE. REMOVED BOROSCOPE PLUGS FOR INSPECTION AND INSTALLED AND SAFTIED PLUGS AFTER COMPLETION OF INSPECTION REF MM 72-00-00-6.
- [SDR FDEA200812025049](https://openairdocs.org/sdr/FDEA200812025049.md): Spar · cracked · Dec 2, 2008 · N387FE · Doug MD1010F · Nacelle/Pylon, Frame/Spar/Rib
  > NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS 4 INCH CRACK, REFERENCE INSPECTION OF PYLON S177 WORKCARD 54X1201ALI-P2. COMPLIED WITH HFEC. VERIFIED NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS CRACKED INDICATION PER NDTSPM. REMOVED AND FABRICATED NEW WEB REF DWG
- [SDR FDEA200811285002](https://openairdocs.org/sdr/FDEA200811285002.md): Skin · cracked · Nov 28, 2008 · N387FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB FRONT SPAR CAP AND UPPER PORTION OF THE SKIN CRACKED AT STA XF 88.834, (N/R 513 GENERATED WO 43105). INSTALLED RT HORIZONTAL STAB FRONT SPAR CAP REPAIR IN REF TO SRM 55-20-00 PG 42 FIGURE 8 CAT A REPAIR.
- [SDR 07FDEA02234](https://openairdocs.org/sdr/07FDEA02234.md): Skin · cracked · Jun 21, 2007 · N387FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > 1 CRACK LONG 1" ON EXT SKIN LOWER AT STA 485 RT SIDE DOOR FWD W/W REPAIRED IAW SRM 53-50-00 FIG 25 VOL 1.
- [SDR 07FDEA02233](https://openairdocs.org/sdr/07FDEA02233.md): Skin · misrepaired · Jun 21, 2007 · N387FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR EXT FUS FROM STA 1901 TO 1921 BETWEEN LONGERONS 37 LT AND 35 LT REPAIRED IAW SRM 53-20-00 FIG 6 VOL I.
- [SDR 07FDEA02141](https://openairdocs.org/sdr/07FDEA02141.md): Doubler · damaged · Jun 15, 2007 · N387FE · Doug DC1010 · Wing, Plate/Skin
  > EXISTING SKIN REPAIR RIGHT WING L/E SKIN AT STA XOS 800 REPAIRED IAW SRM 57-10-00 FIG 20 VOL 1.
- [SDR 07FDEA02140](https://openairdocs.org/sdr/07FDEA02140.md): Doubler · damaged · Jun 15, 2007 · N387FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > EXISTING SKIN REPAIR AT STA 322 X=-7 EXTERNAL SKIN REPAIRED IAW SRM 53-20-00 FIG 6.
- [SDR 07FDEA02139](https://openairdocs.org/sdr/07FDEA02139.md): Repair · damaged · Jun 15, 2007 · N387FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR EXT FUSELAGE AT SAT 339 X=31 REPAIR IAW 53-20-00 FIG 6 AND SRM 57-30-00.
- [SDR 07FDEA02138](https://openairdocs.org/sdr/07FDEA02138.md): Rib · cracked · Jun 15, 2007 · N387FE · Doug DC1010 · Wing, Rib/Bulkhead
  > LT WING STATION XORS 346 STRINGERS 42-43 AND 43-44 LWR RIB CHORD CRACKED IN TWO PLACES IN THE VERTICAL LEG REPAIRED IAW SRM 57-20-00 FIG 27 SHEET 3 VOL 1.
- [SDR 07FDEA02137](https://openairdocs.org/sdr/07FDEA02137.md): Skin · dented · Jun 15, 2007 · N387FE · Doug DC1010 · Elevator, Plate/Skin
  > RT O/B ELEVATOR FOUND DENT 1.25" BY 1.25 INCH DEEP 0.82" ON UPPER SKIN AT STA XE 280. REPAIR SKIN IAW SRM 55-10-00 VOL1 FIG 8.
- [SDR 07FDEA02136](https://openairdocs.org/sdr/07FDEA02136.md): Web · worn · Jun 15, 2007 · N387FE · Doug DC1010 · Nacelle/Pylon Miscellaneous Structure
  > ON PYLON, NR 3 DEEP WEAR ON UPPER SURFACE OF HORIZONTAL WEB AT STA YN 200. REPAIRED IAW SRM 54-20-00 FIG 5.
- [SDR 07FDEA02135](https://openairdocs.org/sdr/07FDEA02135.md): Structure · leaking · Jun 15, 2007 · N387FE · Doug DC1010 · Wing Main, Frame Structure
  > HEAVY LEAK ON LT WING REAR SPAR AREA AT M22 DOUBLERS REMOVE CLIP TO GAIN ACCESS AND RESEAL AREA IAW SRM 51-33-01 VOL II AND MM 28-11-01-2.
- [SDR 07FDEA02134](https://openairdocs.org/sdr/07FDEA02134.md): Doubler · cracked · Jun 15, 2007 · N387FE · Doug DC1010 · Fuselage Main, Bulkhead
  > CAC COMPT CRACK.50" ON DOUBLER OF BULKHEAD AT STA 1156 LONG 40 LT ACCOMPLISHED EA NR 8-5330-108092.
- [SDR 07FDEA01993](https://openairdocs.org/sdr/07FDEA01993.md): Bulkhead · cracked · May 29, 2007 · N387FE · Doug DC1010 · Fuselage Main, Bulkhead
  > CLG W/W SPACE 2 EA CRACKS ON LT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 10 VOL 1.
- [SDR 07FDEA01949](https://openairdocs.org/sdr/07FDEA01949.md): Skin · dented · May 23, 2007 · N387FE · Doug DC1010 · Elevator, Plate/Skin
  > LT INBOARD ELEVATOR FOUND DEEP DENT AND NICK 5.250" BY 2.25" DEEP.080" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 VOL 1 FIG 8.
- [SDR 07FDEA01936](https://openairdocs.org/sdr/07FDEA01936.md): Structure · cracked · May 22, 2007 · N387FE · Doug DC1010 · Wing Main, Frame Structure
  > RT WING STATION CHORD VERTICAL LEG CRACKED. CRACK TRIMMED OUT FOR RELIEF AND REPAIRED ANGLE INSTALLED IAW SRM 57-20-00 FIG 27 SHT 3 VOL 1.
- [SDR 07FDEA01935](https://openairdocs.org/sdr/07FDEA01935.md): Retainer · cracked · May 22, 2007 · N387FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > FWD CARGO CUTOUT DOOR 2 CRACKS ON RETAINER SEAL AND DEEP WEAR ON EXISTING REPAIR SKIN. SKIN REPAIRED IAW SRM 53-20-00 FIG 6 AND 53-50-00 FIG 26 VOL 1. SEAL RETAINER REPLACED IAW SRM 51-30-00 VOL 2.
- [SDR 07FDEA01934](https://openairdocs.org/sdr/07FDEA01934.md): Longeron · corroded · May 22, 2007 · N387FE · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > LT AIR CONDITIONING COMPT SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPLACED SECTION OF LONGERON P/N ACA3796-501 IAW SRM 53-10-00 VOL 1 FIG 6.
- [SDR 07FDEA01775](https://openairdocs.org/sdr/07FDEA01775.md): Channel · corroded · May 14, 2007 · N387FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LIGHT CORROSION ON CHANNEL. REPAIR CHANNEL IAW SRM 53-70-00 FIG 4, SHT 1 VOL 1 PAGE 17.
- [SDR 07FDEA01773](https://openairdocs.org/sdr/07FDEA01773.md): Skin · cracked · May 14, 2007 · N387FE · Doug DC1010 · Wing, Plate/Skin
  > LT WING LOWER EXT SKIN L/E SLAT TRACK NR 10 FOUND CRACK.50" LONG CUT OUT CRACK AREA AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM 57-10-00 FIG 68 VOL 1.
- [SDR 07FDEA01771](https://openairdocs.org/sdr/07FDEA01771.md): Door Frame · cracked · May 14, 2007 · N387FE · Doug DC1010 · Fuselage Main, Structure
  > MAIN CABIN CRACK LONG.25" ON WEB. REPAIRED JAMB WEB IAW SRM 53-50-00 VOL 1 FIG 19 SHT 2.
- [SDR 07FDEA01769](https://openairdocs.org/sdr/07FDEA01769.md): Angle · corroded · May 14, 2007 · N387FE · Doug DC1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT BILGE ON CAP ANGLES FOUND LIGHT SURFACE CORROSION. REPAIRED IAW SRM 53-30-00 VOL 1 FIG 9.
- [SDR 07FDEA01342](https://openairdocs.org/sdr/07FDEA01342.md): Bulkhead · cracked · Apr 4, 2007 · N387FE · Doug DC1010 · Fuselage Main, Bulkhead
  > LT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.
- [SDR 07FDEA01341](https://openairdocs.org/sdr/07FDEA01341.md): Bulkhead · cracked · Apr 4, 2007 · N387FE · Doug DC1010 · Fuselage Main, Bulkhead
  > RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1.
- [SDR 07FDEA01340](https://openairdocs.org/sdr/07FDEA01340.md): Skin · damaged · Apr 4, 2007 · N387FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > FWD AVIONIC COMPT LT SIDE 2 HOLES ON SKIN. REPAIRED IAW SRM 53-30-00 FIG 4 VOL 1.
- [SDR 07FDEA01337](https://openairdocs.org/sdr/07FDEA01337.md): Stiffener · worn · Apr 4, 2007 · N387FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > LT AIR COND COMPT DEEP WEAR ON VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1.
- [SDR 07FDEA01335](https://openairdocs.org/sdr/07FDEA01335.md): Bulkhead · cracked · Apr 4, 2007 · N387FE · Doug DC1010 · Fuselage Main, Bulkhead
  > RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.
- [SDR 07FDEA01343](https://openairdocs.org/sdr/07FDEA01343.md): Skin · cracked · Apr 4, 2007 · N387FE · Doug DC1010 · Wing, Plate/Skin
  > LT WING LWR EXT SKIN L/E FOUND CRACK 0.5" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1.
- [SDR 06FDEA03905](https://openairdocs.org/sdr/06FDEA03905.md): Sensor · faulty · Nov 5, 2006 · N387FE · Doug DC1010 · Stall Warning System
  > AT SLAT RETRACTION AFTER T/O THE STICK SHAKER ACTIVATED AND SLAT DISAGREE LIGHT STAYED ILLUMINATED AND ALSO SLAT RESET LIGHT CAME ON AND STAYED ON. RAN UNSCHEDULED STICK SHAKER QRH PROCEDURES AND STICK SHAKER STOPPED. MAINT ADVISED TO RETURN TO MEM AS IT WAS
- [SDR 06FDEA03892](https://openairdocs.org/sdr/06FDEA03892.md): Actuator · malfunctioned · Nov 5, 2006 · N387FE · Doug DC1010 · Leading Edge Slat Actuator
  > AFTER T/O AT KLAX, ON SLAT RETRACTION GOT THE STICK SHAKER AND AUTO SLAT EXTENSION. RAN QRH PROCEDURE AND STILL EXPERIENCED THE SAME. DUMPED FUEL TO LANDING WEIGHT (APPROX 30000 LBS) AND RETURNED TO KLAX. ACCOMPLISHED AUTOSLAT RESET. CONFIRMED SLAT CONTR
- [SDR 06FDEA03230](https://openairdocs.org/sdr/06FDEA03230.md): Warning System · activated · Sep 7, 2006 · N387FE · Doug DC1010 · Pneumatic Indicating System
  > AFTER TAKEOFF POWER WAS SET, MASTER WARNING LIGHT FLICKERED ON MOMENTARILY. NO OTHER LIGHTS NOTED. AFTER AIRBORNE, MASTER WARNING LIGHT STAYED ON BRIEFLY WITH NR 2 PNEUMATIC FAIL LIGHT AND SUMMARY LIGHT ALL PACKS AND BLEEDS WERE OFF. ACCOMPLISHED QRH PROCE
- [SDR 04FDEA01915](https://openairdocs.org/sdr/04FDEA01915.md): Support · cracked · Jul 2, 2004 · N387FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > CENTER CARGO CEILING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT S2922781-1 AT MAE.
- [SDR 04FDEA01913](https://openairdocs.org/sdr/04FDEA01913.md): Bulkhead · cracked · Jul 2, 2004 · N387FE · Doug DC1010 · Vertical Stabilizer
  > VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND
- [SDR 04FDEA01912](https://openairdocs.org/sdr/04FDEA01912.md): Bulkhead · gouged · Jul 2, 2004 · N387FE · Doug DC1010 · Vertical Stabilizer
  > VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND
- [SDR 04FDEA01910](https://openairdocs.org/sdr/04FDEA01910.md): Angle · worn · Jul 1, 2004 · N387FE · Doug DC1010 · Aerodynamic Fairings
  > FUSE TAIL CONE CENTER PLATFORM LT ANGLE SUPPORT WORN. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE.
- [SDR 04FDEA01909](https://openairdocs.org/sdr/04FDEA01909.md): Guide · worn · Jul 1, 2004 · N387FE · Doug DC1010 · Aerodynamic Fairings
  > RIGHT TAIL CONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW 51-33-01 AT MAE.
- [SDR 04FDEA01898](https://openairdocs.org/sdr/04FDEA01898.md): Guide · worn · Jun 30, 2004 · N387FE · Doug DC1010 · Aerodynamic Fairings
  > LEFT TAILCONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW SRM 51-33-01 AT MAE.
- [SDR 04FDEA01883](https://openairdocs.org/sdr/04FDEA01883.md): Bracket · damaged · Jun 30, 2004 · N387FE · Doug DC1010 · Aerodynamic Fairings
  > BOTH LEFT AND RIGHT FWD SUPPORT PIN BRACKETS HAVE ELONGATED HOLES ON TAIL CONE WORK PLATFORM. REMOVED AND REPLACED BRACKETS IAW SRM 51-35-01 AT MAE.
- [SDR 04FDEA01882](https://openairdocs.org/sdr/04FDEA01882.md): Angle · bent · Jun 30, 2004 · N387FE · Doug DC1010 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG I/B FAN COWL LWR EDGE ANGLE BENT. REMOVED AND REPLACED IAW SRM 51-31-01 AT MAE.
- [SDR 04FDEA01880](https://openairdocs.org/sdr/04FDEA01880.md): Doubler · gouged · Jun 29, 2004 · N387FE · Doug DC1010 · Nacelle/Pylon, Plate/Skin
  > NR 3 ENG PYLON AFT UPPER FAIRING ANGLES LT AND RT GOUGED AND CHAFED AT AFT FASTENER HOLES. REMOVED AND REPLACED WORN ANGLES LT AND RT IAW SRM 51-35-01 AT MAE.
- [SDR 04FDEA01878](https://openairdocs.org/sdr/04FDEA01878.md): Vane · corroded · Jun 29, 2004 · N387FE · Doug DC1010 · Trailing Edge Flaps
  > COMPLY WITH EA 8-5750-78235 WINGS OUTBOARD FLAP ARC 1537 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-78235 WINGS O/B FLAP ARC1537 FLAP VANE SUPPORT CORROSION REWORK AT MAE.
- [SDR 04FDEA01870](https://openairdocs.org/sdr/04FDEA01870.md): Rib · gouged · Jun 28, 2004 · N387FE · Doug DC1010 · Wing, Rib/Bulkhead
  > ACCOMPLISH EA 8-5710-78226, WINGS REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1086-1. COMPLIED WITH EA 8-5710-78226.
- [SDR 04FDEA01843](https://openairdocs.org/sdr/04FDEA01843.md): Rib · gouged · Jun 22, 2004 · N387FE · Doug DC1010 · Wing, Rib/Bulkhead
  > LT FIXED LEADING EDGE SLAT TRACK RIB GAUGE REPAIR XOS 427.4. COMPLIED WITH FED EX EA 8-5740-79537, LT FIXED LEADING EDGE SLAT TRACK RIB GOUGE REPAIR XOS 477.41.
- [SDR 04FDEA01841](https://openairdocs.org/sdr/04FDEA01841.md): Duct · broken · Jun 21, 2004 · N387FE · Doug DC1010 · Cabin Cooling System
  > COMPLY WITH EA 8-2150-78236, AIR CONDITIONING NR 2 AC PACK EXHAUST DUCT STIFFENER REPAIR P/N-ACM7019. COMPLIED WITH EA 8-2150-78236 FOR STIFFENER REPAIR.
- [SDR 04FDEA01803](https://openairdocs.org/sdr/04FDEA01803.md): Fitting · corroded · Jun 19, 2004 · N387FE · Doug DC1010 · Trailing Edge Flaps
  > RIGHT I/B FLAP SIDE LOAD ROLLER FITTING 3 EA ROLLER BORES AND FACES CORRODED. SIDE LOAD FITTING REMOVED AND REPLACED WITH NEW FITTING IAW CMM 57-55-22 AT MAE.

Next page: https://openairdocs.org/deregistered/N387FE-2024-04-13/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 = 'N387FE' AND deregistration_id = 'N387FE-2024-04-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N387FE-2024-04-13/reports

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