N315FE

Service difficulty reports · 212

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 = 'N315FE' AND registry_match = 'registration'
  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 08FDEA00264Skin · dentedRIGHT WING TRAILING EDGE LOWER SKIN SURFACE DENTED INBD OF OUTBD MAIN FLAP INBD END. REMOVED PANELS TO FOM IAW MD/DC10 SRM 51-31-01 VOL II, CUTOUT DAMAGE AREA IAW MS/DC10 SRM 57-00-01 VOL I. MATERIAL ID FOR DOUBLER REPAIR 2024 T-3, .090 PO NR 575582.1, IJan 24, 2008 · N315FE · Doug DC1030F · Wing, Plate/SkinSDR 08FDEA00260Skin · dentedRT WING, NR 5 L/E SLAT HAS DENTS 5EA ON L/E SKIN. CUT OUT DAMAGED AREA, FABERICATED DOUBLERS, SPLICE PLATE, BAFFLES, SEAL, FILLER AND INSTALLED REPAIR IAW SRM 57-10-00 FIG.II, VOL I, SRM51-21-01 VOL II AND SRM 51-35-02 VOL II.Jan 24, 2008 · N315FE · Doug DC1030 · Leading Edge DevicesSDR 08FDEA00242Skin · dentedCENTER CARGO DOOR FWD LOWER EDGE IS DENTED. REPAIRED CENTER CARGO DOOR FWD LOWER EDGE IAW DC10 SRM 52-10-00 VOL I FIG 17 SHEET 1.Jan 23, 2008 · N315FE · Doug DC1030 · Cargo/Baggage DoorsSDR 05FDEA01227Switch · defectiveNR 3 MANIFOLD FAIL ILLUMINATED IN FLT. C/W QRH PROCEDURES, LIGHT EXTINGUISHED. PERFORMED DECAY CHECK OF NR 3 PNEU SYS IAW JRH AND PASSED ITERROGATED FAULT INDICATOR IN CAC AND FOUND RIGHT WING PRESS SWITCH FAULTED WITH APU AIR CHECKED ALL ANTI-ICE TUBING ANDMay 7, 2005 · N315FE · Doug DC1030 · Pneumatic Indicating SystemSDR 04FDEA001104Support · brokenON TAKEOFF AT 1200 FT AGL THE EGT ON NR 1 ENG WENT TO 960 DEGREES INDICATED VERY RAPIDLY. TOOK 4 THROTTLE WIDTHS TO BRING THE EGT BACK INTO PARAMETERS AND ENG RUNNING SMOOTLY. DUMPED APPROX 20K LBS OF FUEL. INITIAL VISUAL INSPECTION REVEALED SEVERAL BROKENApr 26, 2004 · N315FE · Doug DC1030 · Nacelle/Pylon, Main FrameSDR 04FDEA00969Access Panel · missingDURING MAINT WALKAROUND FOUND CTR CARGO DOOR PRESSURE RELIEF ACCESS PANEL MISSING FROM A/C. INSTALLED PANEL PER MM 53-53-00.Apr 15, 2004 · N315FE · Doug DC1030 · Cargo/Baggage DoorsSDR 01FDEA00296Hydraulic Line · leakingEVIDENCE OF HYD LEAK COMING FROM AFT CARGO COMPARTMENT. *S/D* REPAIRED PIPE ASSY AGK7002-553 PER MM 20-10-01-2 AND REPLACED PNEU DUCT INSULATION BLANKETS.Apr 24, 2001 · N315FE · Doug DC1030F · Hydraulic System, AuxiliarySDR 01FDEA00283Angle · crackedNR 3 RT LEAD EDGE ASSY FOR HORIZONTAL HAS 7 INCH STRESS CRACK, RUNNING THRU HOLES ON UPPER FLANGE. *S/D* REMOVED AND REPLACED T-ANGLE REF SRM 55-10-00. RE-INSTALLED NR 3 RT LEADING EDGE ASSY.Feb 23, 2001 · N315FE · Doug DC1030F · Horizontal Stabilizer StructureSDR 00FDEA00359Skin · damagedFWD CARGO DOOR CUTOUT FWD SIDE FOUND EXTERIOR SKIN AT L 39-40 DAMAGED. *S/D* REMOVED DAMAGED AREA PER SRM 53-50-00 FIG 9 SHEET 3 VOL 1 AND 51-21-01 VOL II. REPAIRS ARE REPAINTED PER SRM 51-21-02 VOL II. FASTENERS INSTALLED PER 51-33-01 VOL II.May 29, 2000 · N315FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 98FDEA00429Hydraulic Sys · high temp98-0167 STA-DXB: DURING TAXI OUT HYD SYS NR 2 READ 50-50 DEG AFTER APPROX 8 MIN OF FLT TEMP NR 2 HAD INCREASE TO 60 DEG TMP SHORTLY INCREASE TO 70 DEG RED TABS REFER TO ND TEMP INCREASE WITHIN 5 MIN TO 90 CONT RED TAB PROC WITH NR 2 SYS SHUT DOWN. WHEN TMP AJun 28, 1998 · N315FE · Doug DC1030F · Hydraulic System, MainSDR 98FDEA00148Fire Bottle · dischargedON PRE FLT CK, FOUND NR 2 ENG FIRE AGT 2 LOW LIGHT CAME ON. ON CK FOUND NR 2 ENG NR 2 BOTTLE DISCHARGE CARTRIDGE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE AND CARTRIDGE AS PER M/M 26-21-02 AND M/M 26-21-01. ALSO, WIRING AND AGENT DISCHARGE S/W (S1-1Mar 3, 1998 · N315FE · Doug DC1030F · Extinguishing SystemSDR 96FDEA01690Piccolo Tube · leakingAIRCRAFT WING ANTI-ICE SET UP FOR USE ON TAKEOFF, ABOUT 10 TO 15 SECONDS AFTER LIFT OFF. NR 1 MANIFOLD FAIL LIGHT ILLUMINATED. TURNING OFF WING ANTI-ICE TURNED OFF MANIFOLD FAIL LIGHT. TROUBLESHOT SYSTEM FOUND NR 5 LEFT HAND SLAT PICCOLO TUBE OUTBOARD END LNov 22, 1996 · N315FE · Doug DC1030F · Airfoil Anti/De-ice System
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