N319FE

Service difficulty reports · 234

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 = 'N319FE' 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 FDEA200811034676Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Floor PanelSDR FDEA200811034675Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Floor PanelSDR FDEA200811034674Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10- 0600C210-1JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Floor PanelSDR 08FDEA04676Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA04675Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA04674Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.Nov 3, 2008 · N319FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200810304625Skin · crackedDURING U/S INSP OF HORIZ STB, FOUND UPPER INTERIOR SKIN PANELS PN 7229-1, PN 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS, INSP FINDING FORM FOR DETAIL. ACCOMPLISHED EA NR 8-5510-125425.Oct 30, 2008 · N319FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR 08FDEA04625Skin · crackedDURING U/S INSP OF HORIZONTAL STAB, FOUND UPPER INTERIOR SKIN PANELS P/N 7229-1, P/N 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS,Oct 30, 2008 · N319FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR FDEA200810174387Bulkhead Web · crackedDURING INSP NLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 2-3 VOL I.Oct 17, 2008 · N319FE · Doug DC1030F · Fuselage Main, BulkheadSDR 08FDEA04387Pressure Panel · crackedDURING INSPECTION NLG W/W FOUND CRACK ON VERTICAL WEB.Oct 17, 2008 · N319FE · Doug DC1030F · Fuselage Main, BulkheadSDR FDEA200810154353Skin · dentedLOWER FUSELAGE DENT ON EXT SKIN DIM: 2" X 2" DEPTH 0.09". REPAIRED DENT IAW SRM 53-20-01 FIG 13 SHT 2A VOL I.Oct 15, 2008 · N319FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200810154352Skin · crackedLT WING L/E CRACK ON EXT LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.Oct 15, 2008 · N319FE · Doug DC1030F · Trailing Edge FlapsSDR 08FDEA04353Skin · dentedLOWER FUSELAGE DENT ON EXT SKIN DIM, 2 INCH BY 2 INCH DEPTH 0.09 INCH.Oct 15, 2008 · N319FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 08FDEA04352Skin · crackedLT WING L/E CRACK ON EXT LOWER SKIN.Oct 15, 2008 · N319FE · Doug DC1030F · Wing, Plate/SkinSDR 07FDEA01547Seat Track · wornMCD SEAT TRACK FROM STA 1099 TO STA 1321 RBL 47 HAS 6 AREAS WITH WORN LUGS. FOUND DURING C CHECK AT MAE, REMOVED AND REPLACED DAMAGED SEAT TRACKApr 23, 2007 · N319FE · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03142Handle · pulledDESCENDING THRU 4000 FT GOT BOTH LEFT AND RIGHT CABIN DOOR ANNUNCIATOR LIGHTS ILLUM. PRESSURIZATION WENT TO ZERO DIFF PRESS AND CABIN ALT= ACFT ALT. LANDED EWR WITHOUT INCIDENT. FOUND BOTH AFT DOORS OPEN ON WALKAROUND, TRIED TO ELECTRICALLY CLOSE DOORS NOAug 30, 2006 · N319FE · Doug DC1030 · Service DoorsSDR 06FDEA2265Door · openLEFT AFT NR 4 ENTRY PASS/CREW DOOR CAME OPEN IN FLIGHT. FOUND THAT THE LEFT AFT NR 4 PASS/CREW SERVICE DOOR -RED- EMERGENCY HANDLE WAS PULLED PRIOR TO DEPARTURE. SUSPECT HUB PERSONNEL LIFTED HANDLE TO RAISE DOOR WITH NO RESULTS, THEN RELEASED HANDLE WITH NOJun 11, 2006 · N319FE · Doug DC1030 · Passenger/Crew DoorsSDR 06FDEA0311Manifold · failedCLIMBING TO 1800 NR 2 MANIFOLD FAILURE. COMPLIED WITH QRH UNABLE TO REDUCE NR 2 PNEUMATIC PRESSURE .LANDED AT NEAREST SUITABLE AIRPORT. "MEL 36-01-A: NR 2 PNEUMATIC SUPPLY SYSTEM - INOP." INSTALLED NEW FLANGE, RETAINER & SEAL AT NR 2 ENG OVER PRESSURE VALVEJan 22, 2006 · N319FE · Doug DC1030 · Pneumatic Indicating SystemSDR 05FDEA02483Warning Light · intermittentDURING CRUISE FLIGHT, WE GOT THE AIR CONDITIONER DOOR OPEN LIGHT THAT CAME ON SEVERAL TIMES. GRADUALLY COMING ON FOR LONGER PERIODS RAN QRH & LANDED AT NEAREST FIELD,KIND. INSPECTED ALL THREE AC BAY DOOR SWITCHES IAW 52-42-01-2 FOUND ALL 3 DOOR SWITCHES TOAug 16, 2005 · N319FE · Doug DC1030 · Door Warning SystemSDR 04FDEA00559Pressure Switch · malfunctionedNR 3 MANIFOLD FAILURE LIGHT ILLUMINATED IN CRUISE AT FL 370. RED TABS FOLLOWED. T/S PER TAFI 36-23-00 FAULT CODE BC/YZ. PROBLEM DUPLICATED WITH OR WITHOUT PNEU SYS NR 3 PRESSURIZED. ACCOMPLISHED NR 3 PNEUMATIC SYSTEM DECAY CHECK PER DC-10 JRH TEST PASSEDMar 3, 2004 · N319FE · Doug DC1030 · Pneumatic Indicating SystemSDR 03FDEA00738Proximity Sensor · inoperativeUPON GEAR RETRACTION AFTER DEPARTURE, FRONT DISPLAY (F/O) LT MAIN GEAR LIGHT REMAINED RED, ALL OTHERS EXTINGUISHED. RECYCLED GEAR IAW RED TAB PROCEDURE- GEAR RETRACTED NORMALLY; ALL LIGHTS EXTINGUISHED. R/R PROX BOX.May 16, 2003 · N319FE · Doug DC1030 · Landing Gear Position and WarningSDR 02FDEA00925Beam · crackedCENTER CARGO DOOR COUNTER BALANCE BEAM CRACKED AT FORWARD BRACKET. REMOVED AND REPLACED COUNTER BALANCE BEAM ASSEMBLY IAW MM.Dec 5, 2002 · N319FE · Doug DC1030F · Cargo/Baggage DoorsSDR 02FDEA00249Mec · out of rigON TAKEOFF NR 3 ENG W/N ATTAIN MAX PWR. ADJUSTED NR 3 ENG MEC 1/2 TURN UPTRIM, RAN ALL ENG PER JRH CHAPTER 5 AND ACCOMPLISHED MAX. ALL ENGINES OPERATING OKAY.Apr 12, 2002 · N319FE · Doug DC1030F · Fuel Control/Turbine EnginesSDR 01FDEA00121Door · damagedSNRM N-1 A/C STRIKE MAIN CARGO DOOR AQS/LAX NOTE: A/C MAIN CARGO DOOR DAMAGED IN OAKLAND AND FERRIED TO LAX FOR REPAIRS. ** S/D ** R&R DOOR PER EA 8-5230-49684 AND SRM 51-31-01 VOL II.Feb 14, 2001 · N319FE · Doug DC1030F · Cargo/Baggage DoorsSDR 01FDEA00115Transformer · faultyDURING SAFETY CHECK FOUND OVERHEAD SWITCH PANEL LIGHTS (CB) POPPED. RESET NORM. BEGAN TO SMELL FUMES AND SMOKE FROM OVERHEAD PANEL. INSTALL TRANSFORMER T1-94, OPS NORM PER MM 33-11-07-2.Feb 13, 2001 · N319FE · Doug DC1030F · Flight Compartment EquipmentSDR 00FDEA00455Door · corrodedAVIONICS COMP DOOR NR 115AZ FOUND CORRODED INTERIOR. *S/D* REMOVED AND REPLACED PER DRAWING NR ACA 3777, MM 52-41-01-2.Jul 11, 2000 · N319FE · Doug DC1030F · Electrical/Electronic Compartment DoorsSDR 00FDEA00445Control Cable · brokenLT WING LEAD EDGE SLAT NR 7 EXTEND CABLE NR 65 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-13-4.Jul 7, 2000 · N319FE · Doug DC1030F · Leading Edge Slat Control SystemSDR 00FDEA00444Control Cable · brokenLT WING LEAD EDGE SLAT NR 6 EXTEND CABLE NR 63 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-11-4.Jul 7, 2000 · N319FE · Doug DC1030F · Leading Edge Slat Control SystemSDR 99FDEA00273Clip · crackedSNRM 308,309,310 LT WING TO FUSELAGE UPPER FAIRING SUPPORT RIBS ATTACH CLIP CRACKED AT BS 1225, BS 1289, BS 1300, BS 1310, BS 1341 AND BS 1375. L/H WING TO SELAGE FARIR BOTTOM SUPT RIBS CRACKED. CARRIED OUT REPAIRS PER AEA 0553, ANB 7140, ANB 7139, AEA 0552,Jul 19, 1999 · N319FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 97FDEA00719Connector · dirty97-0197 - WITH GEAR RETRACTED RED NOSE GEAR UNSAFE LIGHT ON F/E PANEL INTERMITTENT ON (NO LIGHT ON FWD PANEL) RECYCLED GEAR NO CHANGE. INSPECTED NOSE GEAR PROX SWITCHES FOR DAMAGE ALL OK PROX BOX. REMOVED AND CLEANED ELECTRICAL PINS GOOD BITE TEST NOW OK FOROct 8, 1997 · N319FE · Doug DC1030F · Landing Gear Position and WarningSDR 97FDEA00336Gear Light · failedON EXTENSION OF THE LANDING GEAR THERE WAS NO GREEN GEAR LIGHT FOR THE CENTER GEAR. RECYCLED GEAR TO NO AVAIL. RELAMPED BOTH F/E AND PILOT CENTER GEAR POSITION LIGHT, OPS CK'D GOOD.Jun 9, 1997 · N319FE · Doug DC1030 · Landing Gear Position and WarningSDR 96FDEA1020Hyd Pump · leakingTOTAL LOSS OF HYDRO SYSTEM NR 3 ON CLIMBOUT, PERFORMED RED TAB PROCEDURE AND LANDED 35/EXT 16L SEA WITHOUT INCIDENT. MAINTENANCE FOUND 2/3 REVIISABLE MOTOR PUMP LEAKING. REMOVED AND REPLACED 2/3 REVIISABLE MOTOR PUMP PER M/M 29-22-01, LEAK AND OPS CHECK GOODMay 22, 1996 · N319FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 96FDEA00683Uplock Sensor · malfunctionedAFTER TAKEOFF, A FEW MINUTES AFTER GEAR WAS RAISED THE LEFT MAIN REG LIGHT ON THE FWD PANEL ILLUMINATED. NO LIGHTS ON S/O'S PANEL. CYCLED THE GEAR AND ALL LIGHTS EXTINGUISHED. LIGHTS ILLUMINATED AGAIN DURING APPROACH PHASE. REPEAT WRITE-UP. REPLACED D1-81Mar 26, 1996 · N319FE · Doug DC1030 · Landing Gear Position and WarningSDR 96FDEA00682Gear Light · malfunctionedON TAKEOFF, RAISED GEAR AND ALL LIGHTS OUT, BUT AFTER A FEW SECONDS THE LEFT MAIN LIGHT ON FWD PANEL CAME ON. NO LIGHTS ON S/O PANEL. CYCLED THE GEAR AND ALL LIGHTS WENT OUT AND REMAINED OUT. LIGHTS CAME BACK ON BRIEFLY DURING DESCENT AND BACK OUT, SEVERAL Mar 26, 1996 · N319FE · Doug DC1030 · Landing Gear Position and Warning
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