# Service difficulty reports: N388FE, cancelled Jul 29, 2013

A list on [N388FE, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N388FE-2013-07-29.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA201008032782](https://openairdocs.org/sdr/FDEA201008032782.md): Clamp · loose · Aug 3, 2010 · N388FE · Doug MD1010F · Pneumatic Indicating System
  > DURING CLIMB, PASSING APPROX FL280 HAD INDICATIONS OF MANIFOLD FAILURE INCLUDING 'AIR SYS 1 OFF' & 'AIR SYS 2 OFF'. MASTER CAUTION/WARNING EAD ALERTS LASTED ONLY SPLIT SECOND. DIVERTED. PERFORMED DECAY CHECK OF PNEUMATIC SYSTEMS 1 & 2. INDICATIONS NORMAL.
- [SDR FDEA201003271019](https://openairdocs.org/sdr/FDEA201003271019.md): Spar Cap · cracked · Mar 27, 2010 · N388FE · Doug MD1010F · Wing Spar
  > RT WING REAR SPAR REPAIR IAW EA 8-5710-138106, PART 1 INSTRUCTIONS. INTERIM REPAIR ACCOMPLISHED IAW EA NR 8-5710-138106 PART 1, REPETITIVE INSP AT 1650 FLT CYC INTERVALS AND FINAL RESTORATION TO BE ACCOMPLISHED PRIOR TO ACFT REACHING 39357 FLT CYC REF: EA N
- [SDR FDEA200909183328](https://openairdocs.org/sdr/FDEA200909183328.md): Insulation · damaged · Sep 18, 2009 · N388FE · Doug MD1010F · Pneumatic Distribution System
  > AFT CARGO - NR 2 SYS PNEU DUCT INSULATION BLANKET HEAVILY DAMAGED INSIDE LT SIDEWALL STA 1921-1941. NOTE: SEPERATE NR GENERATED TO VERIFY CORRECT INSTALLATION OF VENT TUBE ADJACENT DAMAGED AREA (N00384: AFT CARGO LT SIDEWALL-VERIFY CORRECT INSTALLATION OF VEN
- [SDR 08FDEA04660](https://openairdocs.org/sdr/08FDEA04660.md): Spar Cap · damaged · Oct 31, 2008 · N388FE · Doug MD1010F · Wing Spar
  > COMPLY WITH LT WING REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR, STA XORS 395 TO 446 PER EA 8-5710-118517 REV NR POS, SEQ NR 000007. COMPLIED WITH E.A. 8-5710-118917 WING-REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR.
- [SDR 08FDEA00408](https://openairdocs.org/sdr/08FDEA00408.md): Cap · cracked · Feb 12, 2008 · N388FE · Doug MD1010F · Fuselage Main, Structure
  > LT END CAP OF CAC DOMED PRESSURE BULKHEAD CRACKED. REMOVED AND REPLACED END CAP IAW SRM 51-31-01. END CAP FABRICATED ON MAE TRAVELER T8/725202. REMOVED AND REINSTALLED DOUBLER IAW SRM 51-31-01 FOR ACCESS. CLEANED AND RESEALED AREA IAW MM 20-60-08-2.
- [SDR 08FDEA00361](https://openairdocs.org/sdr/08FDEA00361.md): Seat Track · worn · Feb 6, 2008 · N388FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MCD SEAT TRACK AT BS 650-730 LBL 107 IS WORN. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR 06FDEA0721](https://openairdocs.org/sdr/06FDEA0721.md): Duct · failed · Feb 17, 2006 · N388FE · Doug MD1010F · Pneumatic Distribution System
  > PASSING FL 220 PILOTS BOTH HEARD A LOUD BANG UNDERNEATH OUR SEATS. PRESSURIZATION WENT ERRATIC FOR ABOUT 10 SECONDS, SHORTLY FOLLOWED BY A LEVEL 2 AIR SYS 1-2 OFF LIGHT. FOLLOWED QRH, ISOLATED NR 1 MANIFOLD WHICH SUSPECT WAS THE PROBLEM. DIVERTED TO ATL.
- [SDR 05FDEA02045](https://openairdocs.org/sdr/05FDEA02045.md): Landing Gear · malfunctioned · Jul 22, 2005 · N388FE · Doug MD1010F · Landing Gear Retraction/Extension System
  > AFTER T/O RW 22L JFK. LT MAIN GEAR FAILED TO RETRACT. INDICATIONS WRE LEFT UNSAFE LIGHT AND A RED DOT LEFT GEAR ON CONFIG PAGE. ALSO NOTICED YAW WITH 1GEAR STILL DOWN. R & R LT TRIM CYLINDER PER MM 32-37-01-2. REMOVED AND REPLACED NR 2 SYS BRAKE LINES ON NR
- [SDR 04FDEA03193](https://openairdocs.org/sdr/04FDEA03193.md): Hinge · corroded · Nov 23, 2004 · N388FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND OUT OF LIMITS. INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA NR 8-5750-83939, WING-RIGHT HAND OUTB
- [SDR 04FDEA03127](https://openairdocs.org/sdr/04FDEA03127.md): Hinge · corroded · Nov 16, 2004 · N388FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT, PIVOT ATTACH POINT, INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND TO BE OUT OF LIMITS, INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA 8-5750-83939, WING, RIGHT HAND
- [SDR 04FDEA01657](https://openairdocs.org/sdr/04FDEA01657.md): Panel · corroded · Jun 10, 2004 · N388FE · Doug DC1010 · Wing, Plate/Skin
  > LEFT MAIN LANDING GEAR, WING SUPPORT FITTING CORROSION IN THREE TAPER LOCK HOLES. CORROSION REMOVAL AND OVERSIZED TAPER LOKS INSTALLATION IAW FEDEX EA 8-5710-70153.
- [SDR 04FDEA00333](https://openairdocs.org/sdr/04FDEA00333.md): Pressure Switch · malfunctioned · Feb 6, 2004 · N388FE · Doug DC1010 · Ice/Rain Protection System
  > DURING CLIMBOUT WITH WING & ENGINE ANTI ICE ON GOT A NR 1 MANFOLD FAIL ALERT. COMPLIED WITH QRH AND RTB. TROUBLESHOT PER FIM CH 36-23 FOUND MANIFOLD FAULT INDICATOR SET (LEFT WING PRESSURE SW SHOWN) SWITCH WOULD NOT RESET. REMOVED AND REPLACED PRESS SWITCH
- [SDR 02FDEA00597](https://openairdocs.org/sdr/02FDEA00597.md): Landing Gear · failed · Aug 14, 2002 · N388FE · Doug DC1010 · Landing Gear Retraction/Extension System
  > IN LANDING PATTERN AT TPA AT GEAR EXTENSION HEARD LOUD BANG AND A/C SHUTTERED SERIOUSLY. NR 3 HYDRAULIC DEC TO ZERO. LEFT MLG READ UNSAFE LIGHTS ILLUMINATED ON BOTH FRONT AND ENGINEER'S PANEL. ACCOMPLISHED APPROPRIATE RED TAB PROCEDURES. LANDED AND EVACUATE
- [SDR 00FDEA00520](https://openairdocs.org/sdr/00FDEA00520.md): Mount · corroded · Aug 5, 2000 · N388FE · Doug DC1010F · Engine Mount Section
  > NR 14 CORROSION FOUND ON NR 3 ENGINE AT AFT MOUNT ASSY. *S/D* REPLACED PER MM 20-20-01-2 DAC BLUE PRINT AUB 7032.
- [SDR 00FDEA00216](https://openairdocs.org/sdr/00FDEA00216.md): Control Box · inoperative · Apr 11, 2000 · N388FE · Doug DC1010F · Landing Gear Position and Warning
  > 00-108 WHEN GEAR RETRACT AFT T/O RT MAIN MOUNT RED LIGHT ON FRONT PNL REMAIN ILLUM. R&R PROXIMITY CONTROL BOX & TESTED PER MM 32-61-01-2.
- [SDR 00FDEA00096](https://openairdocs.org/sdr/00FDEA00096.md): Throttle · frozen · Feb 19, 2000 · N388FE · Doug DC1010F · Power Lever
  > PRIOR TO DESCENT, NR 2 THROTTLE FROZE IN POS. PERFORMED IN FLT ENGINE SHUTDOWN CKLIST & APPRO RED TABS. REMOVED AND REPLACED NR 2 ENG THROTTLE PUSH-PULL CABLE WITH MM 76-11-01-2. RAN NR 2 ENG IAW DC10 JRH.
- [SDR 99FDEA00247](https://openairdocs.org/sdr/99FDEA00247.md): Uplock Target · bent · Jun 29, 1999 · N388FE · Doug DC1010F · Landing Gear Position and Warning
  > RIGHT MLG LIGHT REMAINED ILLUMINATED AT GEAR RETRACT, HYD WERE NORMAL. CYCLE LANDING GEAR PER ABNORMAL PROC. FOUND DOOR PROXIMITY TARGET BENT PER EA 8-3230-46724 C/W EO 8-3260-7-3304 PART 2 ONLY. REMOVED AND REPLACED RIGHT UPLOCK TARGET ASSY.
- [SDR 99FDEA00235](https://openairdocs.org/sdr/99FDEA00235.md): Prox Target · inoperative · Jun 23, 1999 · N388FE · Doug DC1010F · Landing Gear Position and Warning
  > LEFT MAIN GEAR IND UNSAFE UP AFTER T/O WITH HANDLE UP. BOTH PANELS INDICATE UNSAFE. REMOVED AND REPLACED PROX TARGET, OPS CK PER MM 32-61-03.
- [SDR 98FDEA00478](https://openairdocs.org/sdr/98FDEA00478.md): Spar · corroded · Jul 22, 1998 · N388FE · Doug DC1010 · Wing Spar
  > STA-GYR: WHILE WORKING EO 8-5710-7-3314 PARTS 5,6,7, AND 8 FOUND LEFT NR 2 AND RT NR 4 HOLES IN PYLON FITTINGS AND WING SPAR CORRODED. CORROSION WAS REMOVED AND HOLES ARE WITHIN BLUEPRINT TOLERANCE.

## 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 = 'N388FE' AND deregistration_id = 'N388FE-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N388FE-2013-07-29/reports

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