N388FE, cancelled Jul 29, 2013

Service difficulty reports · 19

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201008032782Clamp · looseDURING 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. Aug 3, 2010 · N388FE · Doug MD1010F · Pneumatic Indicating SystemSDR FDEA201003271019Spar Cap · crackedRT 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 NMar 27, 2010 · N388FE · Doug MD1010F · Wing SparSDR FDEA200909183328Insulation · damagedAFT 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 VENSep 18, 2009 · N388FE · Doug MD1010F · Pneumatic Distribution SystemSDR 08FDEA04660Spar Cap · damagedCOMPLY 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.Oct 31, 2008 · N388FE · Doug MD1010F · Wing SparSDR 08FDEA00408Cap · crackedLT 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.Feb 12, 2008 · N388FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00361Seat Track · wornMCD SEAT TRACK AT BS 650-730 LBL 107 IS WORN. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.Feb 6, 2008 · N388FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0721Duct · failedPASSING 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. Feb 17, 2006 · N388FE · Doug MD1010F · Pneumatic Distribution SystemSDR 05FDEA02045Landing Gear · malfunctionedAFTER 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 Jul 22, 2005 · N388FE · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR 04FDEA03193Hinge · corrodedRIGHT 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 OUTBNov 23, 2004 · N388FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA03127Hinge · corrodedRIGHT 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 HANDNov 16, 2004 · N388FE · Doug MD1010F · Trailing Edge FlapsSDR 04FDEA01657Panel · corrodedLEFT 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.Jun 10, 2004 · N388FE · Doug DC1010 · Wing, Plate/SkinSDR 04FDEA00333Pressure Switch · malfunctionedDURING 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 SWITCHFeb 6, 2004 · N388FE · Doug DC1010 · Ice/Rain Protection SystemSDR 02FDEA00597Landing Gear · failedIN 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 EVACUATEAug 14, 2002 · N388FE · Doug DC1010 · Landing Gear Retraction/Extension SystemSDR 00FDEA00520Mount · corrodedNR 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.Aug 5, 2000 · N388FE · Doug DC1010F · Engine Mount SectionSDR 00FDEA00216Control Box · inoperative00-108 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.Apr 11, 2000 · N388FE · Doug DC1010F · Landing Gear Position and WarningSDR 00FDEA00096Throttle · frozenPRIOR 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.Feb 19, 2000 · N388FE · Doug DC1010F · Power LeverSDR 99FDEA00247Uplock Target · bentRIGHT 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.Jun 29, 1999 · N388FE · Doug DC1010F · Landing Gear Position and WarningSDR 99FDEA00235Prox Target · inoperativeLEFT 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.Jun 23, 1999 · N388FE · Doug DC1010F · Landing Gear Position and WarningSDR 98FDEA00478Spar · corrodedSTA-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.Jul 22, 1998 · N388FE · Doug DC1010 · Wing Spar
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