N314FE, cancelled Jul 9, 2013
Service difficulty reports · 45
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 = 'N314FE' AND deregistration_id = 'N314FE-2013-07-09' 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.
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 = 'N314FE' AND deregistration_id = 'N314FE-2013-07-09' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201203020739Anti-Ice Valve · failedON CLIMB OUT, RECEIVED LT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED TO SEA. R & R LSDR FDEA201203020738Anti-Ice Valve · failedON CLIMB OUT, RECEIVED LEFT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED. R & R LEFT WING SDR FDEA201109093812Support Fitting · crackedMAIN CARGO DOOR FRAME, CENTERING GUIDE, LOWER AFT SUPPORT FITTING CRACKED. FABRICATED & INSTALLED SUPPORT FITTING.SDR FDEA201101070067Static Inverter · inoperativeEMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-24-00 FAULT D. FOUND STATIC INVERTER BAD. R & R STATIC INVERTER IAW AMM 24-24-01-2, OK FOR SERVICE.SDR FDEA201005121519Wire Harness · damagedON CLIMB OUT OF ANC - NR3 ENGINE EGT GAGE FLUCTUATED WILDLY OUT OF 20,000 FT HIT 1020 GOT "ENG 3 EXCEEDANCE ALL ENG 3 OIL, TEM, PRESSURE SHOWED NORMAL DUMPED FUEL RETURNED TO DEPARTURE. ANC R EGT INDICATION NORMAL AFTER SHUTDOWN, VISUAL INSP OF HARNESS ASDR FDEA201003040649Warning Light · illuminatedAT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-01-4.AS PRECAUTIONARY PERFORMED DECAY CHECK ON ALL 3 MANIFOLDS PER AMM 36-00-01-5.ALL MANIFOLDSSDR FDEA201002230494Clamp · looseBASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOWSDR FDEA201001080044Throttle · malfunctionedAFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OFF, THE THROTTLES WOULD NOT STAY ADVANCED PROBABLY DUE TO THE AIRPLANE TRYING TO PROTECT ITSELF DUE TSDR FDEA200911143954Spar Cap · crackedLT HORIZ STABILIZER L/E, FOUND 1EA CRACK 1,5" LONG ON UPPER FRONT SPAR CAP AT XE 115 REPAIRED IAW SRM 55-20-00 VOL 1, FIG9.SDR FDEA200910063482Skin · dentedDURING INSP EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN OF CTR CARGO DOOR 4"X2" DEEP .120". REPAIRED DENT IAW SRM 52-10-00, FIG 6, VOL I.SDR FDEA200909233370Skin · dentedRT WING INBD FLAP UPPER SKIN FOUND DEEP DENT AND OIL CANING 2.50 INCH X 1.50 INCH DEEP .055 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1-4 VOL I.SDR FDEA200908313170Door Frame · corrodedINSPECTED UPPER CARGO DOOR JAMB STRUCTURE CORROSION ON UPPER DOOR JAMB. ACCOMPLISHED EA NR 8-5310-129649.SDR FDEA200908102964Channel · corrodedCTR CARGO COMPT REF EO 8-2550-7-2354 P2 STEP "E1" AFTER REMOVAL PARTS FOUND DEEP CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.SDR FDEA200907282794Skin · crackedLT WING L/E FOUND CRACKED ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.SDR FDEA200907282793Skin · crackedLT WING EXT STRUCTURE FOUND CRACKED ON LWR EXT SKIN L/E SLAT NR 4. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 & SRM 57-10-00 FIG 43 VOL I.SDR FDEA200907202671Beam · crackedCTR CARGO BILGE INSP FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I.SDR FDEA200907202670Hinge · nickedLT WING INBD FLAP FOUND ON OUTBD HINGE "ON WING" INBD SIDE DEEP NICKS. REPAIRED AREA IAW SRM 57-20-00 FIG 17 SHT 1 VOL I.SDR FDEA200907202668Angle · crackedUPPER INT. FUSELAGE COMPT "ZONE 312" DURING REPAIR ASSESSMENT WITH EO 8-5100-7- 5001-P2. FOUND CRACK ON ANGLE UPPER SIDE AFT VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 2B VOL I.SDR FDEA200907132601Skin · crackedRT WING EXT SURFACE FOUND CRACK ON UPPER EXT SKIN OTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.SDR FDEA200907112584Skin · dentedLT WING EXT FOUND 2 EA DENTS ON INBD FLAP LOWER EXT. SKIN LWR PNL. 1): 0.75 INCH X 0.50 INCH MAX DEEP 0.070 INCH. 2): 0.50 INCH X 0.50 INCH MAX DEEP 0.060 INCH. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200907112583Skin · dentedLT WING EXT FOUND 1 EA DENT .75 INCH X 1 INCH MAX DEEP .060 INCH ON INBD FLAP LWR EXT. SKIN LWR PANEL. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200907012435Skin · looseRT WING EXT SURFACE FOUND NR 180 EA LOOSE FASTENERS ON UPPER EXT SKIN OUTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 & SRM 57-20-00 FIG 2 VOL I.SDR FDEA200906262319Skin · crackedRT WING LWR EXT SURFACE FOUND CRACKS AND NR 100 EA LOOSE FASTENERS ON LWR EXT SKIN OTBD FLAP. REPAIRED AREA IAW SRM 57-10-00 FIG 7, SHT 3, VOL I.SDR FDEA200906262318Frame · wornDURING INSP LT AIR COND FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & 4A VOL I.SDR FDEA200906262317Frame · crackedDURING INSPECTION LT AIR COND FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.SDR FDEA200906262316Frame · wornDURING INSP AVIONIC COMPT BILGE AREA FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4, VOL I.SDR FDEA200906232239Membrane · crackedAFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200906232238Membrane · crackedAFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.SDR FDEA200906122044Skin · crackedDURING INSP OF COSTANT SECTION STB, FOUND UP PANEL, INSP POSITION 3, WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-129688.SDR 08FDEA03885Line · leakingCENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTENSION HANDLE WAS PULLED. ON LANDING ROLLOUT HYD QUE ILLUMINATED, HYD SYS 3 ELEV ILLUMINATED. FOUND HYD LINE TO CENTER GEAR UNLOCK CYLINDESDR FDEA200807182982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM - INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUSDR 08FDEA02982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUSSDR 03FDEA00337Anti-Ice System · inoperativeRIGHT WINDSHIELD ANTI/ICE INOPERATIVE LIGHT ILLUMINATED SHORTLY AFTER TAKE OFF. REMOVED AND REPLACED RIGHT WINDSHIELD IAW M.M. 56-11-00-2. REMOVED AND REPLACED WINDSHIELD ANTI/ICE CONTROLLER IAW MM 30-41-01-2. GROUND OPS CHECK NORMAL.SDR 02FDEA00383Transmitter · leakingAFTER 2+15 OF FLT HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PERFORMED RED TABS, WITH FLUID DOWN TO 4.5 GALS. WHEN ENG 3 HYD PUMPS TURNED BACK ON, STARTED TO SLOWLY DECREASE TO 3.5 GALS. ENG HYD PUMPS TURNED OFF WITH QTY HOLDING AT 3.5 GALS. ON LANDING APPROX, SDR 02FDEA00355Seal · splitHYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PRESSURE WAS NORMAL, QTY ABOUT 4.5 GALS. RAN RED TABS. LANDED AT TJSJ. HYD LEAK CONFIRMED BY COMPANY MX AFTER LANDING. UPON EXAMINATION, FOUND LEAK TO BE COMING FROM NR 3 HYD PRESSURE XMITTER. REMOVED XMITTER AND FOUSDR 02FDEA00219Periseal · failedAFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP.SDR 01FDEA00025Sensor · damagedAFT T/O AND LAND GEAR UP S/O PNL IND RED UNSAFE NOSE GEAR. RECYCLED LG AND NOSE RED UNSAFE LIGHT ON EXT AND RETRACTION. *S/D* REPLACED DAMAGED NOSE GEAR LOCKED SENSOR PER A/W/D 32-61-04 PG 1 D1-79 AND S/M/P CHAP 20 MM 32-61-03-2. OPS CK NORMAL.SDR 00FDEA00782Tire · disintegrated00-317 NR 3 & 4 TIRE REQUIRES REPLACEMENT DUE TO DISINTEGRATION ON T/O OUT OF CDG. R&R NR 3, 4, 7, 8 TIRES, & DAMAGED PANELS 152PT, 152MT, 152NT, PER MM 20-21-01-2.SDR 00FDEA00729Controller · malfunctionedDURING CLIMB HAD UNCOMMANDED AUTO SLAT EXTENSION.SDR 00FDEA00307Valve · failedLOUD BANG FROM REAR OF A/C PRESS BUMP FELT. REMOVED AND REPLACED AIR CONDITIONING SYS AIR CK VALVE IN REF TO AMM 21-22-03-2. OPS CK NORM.SDR 00FDEA0025Connector · failedNR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE.SDR 00FDEA00025Connector · failedNR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. REPLACED WIRE HARNESS, PLUG CONNECTOR PER WD/M 29-21-01, 29-21-02. REPLACED HYD PUMP AND ELECT MOTOR PER MM 29-21-01-2. OPS AND LEAK SDR 99FDEA00013Transmitter · failed99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SIDE. FOUND LT OTBD FLAP POS TRANSMITTER BAD. REMOVED AND REPLACED SAME PER MM 27-54-03-2. OPS CK GOOD. FOUND DUPLEX ACTUATOR INOP MM 27-5SDR 98FDEA00692Temp Gauge · inopNR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AND REPLACED HYDRAULIC GAUGE AFTER TROUBLESHOOTING, RAN SYS, OK FOR SERVICE MM 29-33-01.SDR 97FDEA00907Control Unit · failed97-0260 - ON T/O CTR AND RT GEAR RED LIGHTS WERE SLOW TO EXTINGUISH, LEFT GEAR LIGHT WENT FROM EXTINQUISHED TO RED RECYCLE GEAR AND ALL LIGHTS EXTINGUISHED. ON LANDING, ALL GEAR LIGHTS AND WARNING HORNS INDICATED UNSAFE, RECYCLED GEAR AND INITIALLY LEFT AND R
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