N801NK, cancelled Jun 16, 2005

Service difficulty reports · 150

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 = 'N801NK' AND deregistration_id = 'N801NK-2005-06-16'
  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 GTIA040794Slide · unsecureL1 SLIDE PACK CAME OFF DOOR. RESECURED SLIDE PACK.Oct 2, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA040789Strut · damagedACY - FLT 1174 - AFTER TAKEOFF FELT RUMBLE WHICH FELT LIKE NOSE GEAR DOOR NOT CLOSING. RECYCLED NOSE GEAR AND UNSAFE LIGHT ILLUMINATED. PER MNCTL DIRECTION, RECYCLED GEAR AGAIN, LIGHT CAME ON AND THEN WENT OUT. CONTINUED FLIGHT. SERVICED NOSE STRUT. ALL OSep 27, 2004 · N801NK · Doug DC982 · Main Landing Gear Strut/Axle/TruckSDR GTIA040799Turbine Blades · looseDURING NOTCH CK IW SB A6224, TABLE 3, FOUND MORE THAN ONE - 4TH STAGE BLADES WITH LESS THAN OR EQUAL TO 5 IN LBS (6 BLADES LOOSE). REPLACED WITHIN 20 HOURS OR CYCLES. REMOVED AND REPLACED ENGINE.Sep 21, 2004 · N801NK · Doug DC982 · Turbine SectionSDR GTIA040705Warning Light · illuminatedTPA - FLT 642 - RIGHT GEAR LIGHT 'RED' STAYS ON AFTER GEAR IS UP. NO GEAR DOOR OPEN LIGHT RECYCLE GEAR ALL NORMAL. SEE LOG PGS 291781-1N 2, 3 AND 291782-1, 2 AND 3 FOR FINDING AND CORRECTIONS. CYCLED MAIN GEAR SEVERAL TIMES. NO DISCREPANCY NOTED. GEAR PINAug 5, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040704Rod · out of adjustAFTER GEAR RETRACTION RT MAIN RED INDICATOR LIGHT STAYED ON 15 SECOND LONGER THAN THE OTHER GEAR INDICATOR LIGHTS. RT HYD PRESSURE MOMENTARILY DROPPED TO 1500 PSI. ALL PUMPS ON HI/ON CRUISE ALT, FL 350, WHEN LEVELING OFF THE GEAR DOOR OPEN LIGHT FLICKERED ONAug 4, 2004 · N801NK · Doug DC982 · Landing Gear Door Retract SectionSDR GTIA040698Position Switch · malfunctionedRIGHT RED GEAR UP AND LOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. RECYCLED GEAR PER QRH. LIGHT WENT OUT ABOUT 45 SECONDS AFTER RETRACTION. LUBRICATED RT MAIN GEAR UPLOCK MECH. REMOVED AND REPLACED RT MLG POSITION SWITCH. REMOVED AND REPLACED SENSJul 31, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040695Uplock Sensor · malfunctionedTHE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYDRAULIC PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PLUMBING, GEAR, DOOR MECH'S. ON RIGHT GEAR NO DEFECTS NOTED. REMOVED AND REPLACED TRJul 29, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040699Uplock Sensor · malfunctionedTHE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYD PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PUMPING, GEAR AND DOOR MECH ON RIGHT GEAR. NO DEFECTS NOTED REMOVED AND REPLACED RIGHT GEARJul 29, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040659Latch · dirtyR1 GIRT BAR SPRING LOADED LATCHES HAVE TO BE MANUALLY MANIPULATED TO LOCK GIRT BAR IN PLACE. CLEANED AND LUBED R1 DOOR GIRT BAR LATCHES. OPS CHECK GOOD. (M)Jul 13, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA040585Slide · dislodgedRSW - FLT 670 - FOUND FORWARD CABIN SLIDE PACK FELL OUT. REINSTLALED L1 SLIDE PACK ASSEMBLY. (M)Jun 19, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA040465Proximity Sensor · inoperativeRT MLG UNSAFE LIGHT ON AFTER GEAR RETRACTION. RECYCLE GEAR. LIGHT OUT. REMOVED AND REPLACED MLG UPLOCK PROXIMITY SENSOR. OPS CHECK NORMAL.May 17, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040463Proximity Switch · inoperativeGEAR DOOR OPEN LIGHT ILLUMINATED. DURING CRUISE. EXT AFTER 30 MIN. ADJ. RT AND LT DOOR PROXIMITY SWITCHES. OPS CHECK GOOD WITH GEAR SWING. MONITIORED DOOR LIGHT WITH NO PRESSURE AND GEAR UP. ALL INDICATIONS NORMAL.May 14, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040450Proximity Switch · inoperativeON TAKEOFF, GEAR RETRACTION RT MAIN GEAR UNSAFE LIGHT, RECYCLED GEAR LIGHT WENT OUT. ON CLEANED RT MAIN PROXIMITY SWITCH. PERFORMED PROXIMITY BOX CHECK SYSTEM OPS CHECK.May 11, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040440Warning Light · illuminatedAFTER T/O NOSE GEAR UNSAFE LIGHT ON FOLLOWED QRH AND LANDED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION OPERATIONAL CK. OPS CK OK.May 8, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040337Support · brokenDTW - FOUND AFT GALLEY SERVICE DOOR, ONE GIRT BAR SUPPORT TAB BROKEN. INSTALLED NEW GIRT BAR SUPPORT TAB ON AFT GALLEY SERVICE DOOR. (M)Apr 23, 2004 · N801NK · Doug DC982 · Fuselage Main, Attach FittingsSDR GTIA040333Connector · looseFOUND TAIL COMPARTMENT EMERGENCY EXIT IDENTIFIER IS NOT LIGHT ON TEST. SECURED CONNECTOR, OPS CHECK. (M)Apr 15, 2004 · N801NK · Doug DC982 · Electrical ConnectorsSDR GTIA040273Cover · looseFLT 223 - ORD - FOUND L1 SLIDE PACK AND COVER CAME LOOSE FROM ENTRY DOOR. NO DAMAGE NOTED, REINSTALLED L1 SLIDE PACK AND COVER. (M)Apr 9, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA040259Lanyard · misroutedFLL - FOUND L1 DOOR ESCAPE SLIDE LANYARD IS ROUTED INCORRECTLY. REROUTED L1 DOOR ESCAPE SLIDE LANYARD. (M)Apr 1, 2004 · N801NK · Doug DC982 · Emergency EquipmentSDR GTIA040242Control Valve · defectiveAFTER TAKEOFF RIGHT RED GEAR LIGHT STAYED ON. AMBER DOOR LIGHT WAS OUT, A/C PRESS NORMAL QRH PROCEDURE AFTER APPROX 10 MINUTES GEAR DOOR OPEN LIGHT CAME ON REF QRH. CABIN PRESS STILL NORMAL AFTER 20 MINUTES DOOR LIGHT OUT AT 1200 FT AND 260 KNOTS RED GEAR LIMar 27, 2004 · N801NK · Doug DC982 · Landing Gear SelectorSDR GTIA040243Slide · out of positionLGA - FLT 1174 - L1 DOOR SLIDE PACK FELL OFF OF DOOR WHEN DOOR WAS CLOSED. REINSTALLED FORWARD CABIN DOOR SLIDE ASSEMBLY AND COVER. (M)Mar 26, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA040219Proximity Switch · faultyFTW - FOUND DOOR MLG LIGHT CAME ON DURING CLIMB FOR APPROX 2 MINUTES STAYED OFF THE REST OF FLIGHT. FOUND LEFT MAIN GEAR DOOR PROX SWITCH D1-30. REMOVED AND REPLACED LEFT MAIN GEAR OPEN PROX SWITCH, OPS CHECK GOOD. (M)Mar 23, 2004 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA040252Clip · corrodedFTW - FOUND MID PIT JAM BEAM FORWARD END CLIP CORRODED AT FS 598 AROUND FASTENER. FABRICATED MID PIT JAM BEAM FORWARD END CLIP. (M)Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Miscellaneous StructureSDR GTIA040212Longeron · corrodedFTW - FOUND MIDPIT LONGERON 30 CORRODED AT FS 664 AROUND FASTENER HOLE. REMOVED LONGERON SECTION L30 FROM STATION 585-665. FABRICATED LONGERON. LONGERON REPAIR PER SPIRIT EA 5310-0403. INSTALLED LONGERON, INSTALLED SPLICE AT STATION 665. (M)Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040231Longeron · corrodedFTW - FOUND MIDPIT LONGERON 28R CORRODED AT FS 617 AROUND FASTENER HOLE. REMOVED LONGERON 28R STATION 588 TO 628. FABRICATED LONGERON. INSTALLED LONGERON. (M)Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040172Floorboard · damagedFTW - FOUND MAIN CABIN FLOORBOARD FS 200-256 LEFT INBOARD CENTER HAS MISSING AND DAMAGED INSERTS AND DAMAGED ON END. FABRICATED NEW CABIN FLOORBOARD STATION 200-256. (M)Feb 21, 2004 · N801NK · Doug DC982 · Fuselage Floor PanelSDR GTIA040211Hook · crackedFTW - FOUND L2 DOOR HAS SEVERAL CRACKS AT SLIDE COVER AND LINER/GIRT BAR HOOK IS BROKEN. INSTALLED NEW GIRT BAR HOOK. (M)Feb 19, 2004 · N801NK · Doug DC982 · Emergency EquipmentSDR GTIA040227Doubler · corrodedFTW - FOUND LEFT ALTERNATE STATIC PORT INTERNAL DOUBLER CORRODED. REMOVED INTERNAL DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED INTERNAL DOUBLER. (M)Feb 19, 2004 · N801NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA040186Panel · crackedFTW - FOUND DORSAL FIN PANEL FORWARD 9 EACH FASTENER HOLES CRACKED, CHAFED, AND BROKEN OUT. FABRICATED DOUBLER. BLENDED OUT CRACKED AREAS. INSTALLED DOUBLER. (M)Feb 19, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Plate/SkinSDR GTIA040185Door · crackedFTW - FOUND RIGHT THRUST REVERSER UPPER DOOR INBOARD SIDE CRACKED AND BENT. REMOVED DOUBLER. STOP DRILLED END OF CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)Feb 17, 2004 · N801NK · Doug DC982 · Engine Thrust ReverserSDR GTIA040184Thrust Reverser · corrodedFTW - FOUND RIGHT THRUST REVERSER UPPER SIDE PITTED HEAVILY. FOUND CRACK IN THE TOP SIDE UPPER DOOR. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)Feb 17, 2004 · N801NK · Doug DC982 · Engine Thrust ReverserSDR GTIA040226Beam · corrodedFTW - FOUND MID PIT DOOR JAMB IS CORRODED STATION 636 TO 623 ON EDGE AND AROUND FASTENERS. REMOVED JAMB BEAM. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M)Feb 16, 2004 · N801NK · Doug DC982 · Fuselage Main, StructureSDR GTIA040170Panel · corrodedFTW - FOUND LEFT WING PANEL 1163C SCRATCHED LIGHT SURFACE CORRODED. REMOVED CORROSION FROM LEFT PANEL 1163C. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)Feb 16, 2004 · N801NK · Doug DC982 · Wing, Plate/SkinSDR GTIA040183Attach Angle · crackedFTW - FOUND RIGHT SIDE DORSAL FIN ATTACH ANGLE CRACKED THROUGH VERTICAL LEG AND INTO 1ST ROW OF FAST ON HORIZONTAL LEG AND GOUGED AND BROKEN FAST. DYE PEN INSPECTION SHOWS NO CRACKS. REMOVED RIGHT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND RFeb 16, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Attach FittingsSDR GTIA040182Attach Angle · crackedFTW - FOUND LEFT SIDE DORSAL FIN ATTACH ANGLE CRACKED AND GOUGED THROUGH VERTICAL LEG INTO 1ST ROW OF HORIZONTAL. REMOVAL LEFT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND INNER ATTACH ANGLE LEFT SIDE CRACKED SEVERAL PLACES. REMOVED LEFT INNERFeb 16, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Attach FittingsSDR GTIA040187Nose Cowl · damagedFTW - NR 2 NOSE COWL LIP RING HAS OVERHEAT INDICATIONS. MEASUREMENTS OBTAINED EXCEEDED UPPER LIMIT FOR 2024-T42 MATERIAL. NR 2 ENGINE NOSE COWL S/N 099-362. REMOVED AND REPLACED SAS WO B00127-11N-00001. (M)Feb 13, 2004 · N801NK · Doug DC982 · Turbine Engine Compressor SectionSDR GTIA040032Slide · looseFLL - FLT 679 - L1 DOOR SLIDE NOT ATTACHED AT BOTTOM SIDE. REINSTALLED L1 DOOR SLIDE. (M)Jan 26, 2004 · N801NK · Doug DC982 · Escape SlideSDR GTIA031039Controller · failedAIRCRAFT WOULDN'T HOLD CABIN PRESSURE. CABIN WARNING VOICE FLOW LIGHT ON. LEFT VALVE TEMP FULL HOT (AUTO) REDUCED TEMP BOTH PACKS LEFT PACK ON 30 SEC FLOW LIGHT ON MASK DROPPED. MANUAL MODE ON OUTFLOW VALVE. PERFORMED TEST ON TEMP CONTROLLER SYSTEM WITH TESDec 11, 2003 · N801NK · Doug DC982 · Cabin Temperature ControllerSDR GTIA030864Slide · dislodgedDTW - FOUND L1 DOOR SLIDE PACK FELL OFF. INSTALLED L1 DOOR EVACUATION SLIDE. NO DISCERPANCIES NOTED. (M)Oct 24, 2003 · N801NK · Doug DC982 · Escape SlideSDR GTIA030713Slide · out of positionLGA - FLT 705 - SLIDE PACK FELL OFF L-1. FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN OPENING DOOR AT ARRIVAL GATE. GIRT BAR LATCH ON THE FLOOR IS VERY DIRTY AND STICKY. REINSTALLED L1 DOOR SLIDE AND CHECKED GIRT BAR LATCHES FOR OPERATION, OPS NORMAL. (M)Sep 24, 2003 · N801NK · Doug DC982 · Escape SlideSDR GTIA030623Blade · damagedON PREFLIGHT INSPECTION, FOUND FOD DAMAGE TO THE NR 2 ENGINE C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE. (M)Aug 9, 2003 · N801NK · Doug DC982 · Turbine Engine Compressor SectionSDR GTIA030486Line · leakingRT ENGINE WAS LOSING OIL PRESSURE AND QUANTITY. FOLLOWED QRH PROCEDURES SHUT DOWN ENGINE. OIL PRESSURE AT SHUTDOWN 30 PSI OIL TEMP AT SHUTDOWN 135 DEGREES, OIL QTY AT SHUTDOWN 5 QUARTS, OIL PRESSURE WINDMILLING 2 PSI, OIL QUANTITY WINDMILLING 4 QUARTS. FOUNJun 27, 2003 · N801NK · Doug DC982 · Engine Oil Distribution (Airframe Furnished)SDR GTIA030279Liner · damagedNR 2 ENGINE INLET HAS TWO CUTS ON ACCOUSTIC LINING AT 4 AND 6 O`CLOCK POSITION. REPAIRED NR 2 ENGINE INLET ACCOUSTIC LINING. NO OTHER DEFECTS NOTED AT THIS TIME.Apr 28, 2003 · N801NK · Doug DC982 · Engine Air Intake SystemSDR GTIA040339Proximity Switch · inoperativeMYR - FLT 1582 - RIGHT MAIN LANDING GEAR INDICATION ON DEPARTURE. QRH ACCOMPLISHED AND LANDING GEAR RECYCLED GEAR DOOR OPEN LIGHT INTERMITTENTLY ON WITH NO VIBRATION NOTED. RIGHT MLG LIGHT EXTINGUISHED WHEN REACHING 10000 FT ON DESCENT. TROUBLESHOT SYSTEM, Apr 22, 2003 · N801NK · Doug DC982 · Landing Gear Position and WarningSDR GTIA021163Striker · defectiveACY - FLT 311 - UPON SLAT RETRACT, THE SLAT DISAGREEMENT LIGHT CAME ON AND SLAT OVERSPEED WARNING IN FLIGHT. FOLLOWED QRH PROCEDURES RETURNED TO KACY THERE WAS NO ROLL ASYMMETRY, AIRCRAFT WAS STABLE IN FLIGHT. REMOVED AND REPLACED NR 4 SLAT DRIVE DISAGREE PRNov 1, 2002 · N801NK · Doug DC982 · Leading Edge Slat Position Indicating SystemSDR GTIA020889Wire · cutFTW - FOUND ONE AFT STAIRWAY EMERGENCY LIGHT IS INOPERATIVE. TROUBLESHOT FOUND EMERGENCY LIGHT WIRES CUT AT SPLICE POINTS. RESPLICED WIRES. (M)Aug 3, 2002 · N801NK · Doug DC982 · Light System WiringSDR GTIA020875Contactor · bentFTW - FOUND LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE, UPPER SIGNS ONLY. FOUND BATTERY PACK CONTACT BENT. REALIGNED CONTACT. (M)Jul 30, 2002 · N801NK · Doug DC982 · Emergency LightingSDR GTIA020846Blade · nickedNR 1 ENGINE C1 FAN BLADES ARE ROUGH AND HAVE NICKS. NR 1, SN 718528, FAILED BORESCOPE INSPECTION , C-7 DISK 10 BLADES WITH NICKS AND MISSING MATERIAL. 2 BLADES DAMAGED NEAR TIP (1) MEASURES .140 INCH LONG (2) MEASURES .165 INCH LONG WITH A CRACK PROPAGATINGJul 14, 2002 · N801NK · Doug DC982 · Turbine Engine Compressor SectionSDR GTIA020835Longeron · gougedFTW - AFT ACCESSORY COMP GOUGE ON LONGERON 22L FLANGE, STATION 1380. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER. (M)Jul 13, 2002 · N801NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA020845Skin · damagedFTW - FOUND STATION 546-552 BETWEEN LONGERON 17R AND 18R, 6 INCHES LONG CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE. FORMED FINGER DOUBLER. FORMED SKIN DOUBLER. INSTALLED FINGER DOUBLER AND FILLER. (M)Jul 11, 2002 · N801NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA020851Skin · puncturedFTW - FOUND RUDDER TAB HAS PUNCTURE MARK (HOLE) APPROX .25 INCH DIAMETER 3 INCHES ABOVE FIXED TAB. RUDDER TRIM TAB FIXED TAB DEBONDED. THIS TAB REPLACED. (M)Jul 10, 2002 · N801NK · Doug DC982 · Rudder, Tab Structure
Back to N801NK, cancelled Jun 16, 2005