N127NK

Service difficulty reports · 41

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 = 'N127NK' 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 WX0A02009ADuct · rupturedLAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MX DISCNov 2, 2002 · N127NK · Doug DC921 · Pneumatic Distribution SystemSDR WXOA02009ADuct · crackedTAIL COMP HIGH TEMP ANNUNCIATOR INDIC ILLUMINATED INFLIGHT. AC RETURNED TO STATION W/O INCIDENT. MAINT INSP TAIL COMP AND ASSOC PRESS DIST SYS FOR CAUSE OF HIGH TEMP INDICATION. MAINT DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN SOURCE IN THE RT AIR COND SYS. Nov 2, 2002 · N127NK · Doug DC921 · Air Distribution SystemSDR WXOA02009Duct · rupturedLAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MAINTENNov 2, 2002 · N127NK · Doug DC921 · Pneumatic Distribution SystemSDR WXOA02007Drive Gear · failedENROUTE, NR 1 ENGINE LOW OIL PRESSURE ANNUNCIATOR INDICATION ILLUMINATED. CREW COMPLIED WITH AOM EMERGENCY/ ABNORMAL PROCEDURES. PRECAUTIONARY INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED. AIRCRAFT CONTINUED TO STATION WITHOUT INCIDENT. THE ENGINE WAS REMOVED ANDSep 18, 2002 · N127NK · Doug DC921 · Turbine Engine Oil SystemSDR WX0A01003Pan · crackedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND AFT CARGO DOOR CRACKED AROUND RIVNUT FASTENER AT LOWER FORWARD CORNER. ROUTED OUT CRACK ON AFT CARGO DOOR, FORWARD LOWER JAMB. FORMED DOUBLER REPAIR AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-Jul 25, 2001 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WX0A01002Aileron · delaminatedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT AILERON INBOARD TAB DELAMINATION DETECTED ON LOWER OUTBOARD SIDE. DELAMINATION REPORTED TO BE AN AREA OF APPROXIMTELY 5 SQUARE INCHES. CUTOUT DELAMINATED AREA (APPROX 10 INCHES BY 3 INCHES). Jul 25, 2001 · N127NK · Doug DC921 · Wing StructureSDR WX0A01001Attach Fitting · crackedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKED DETECTED BY VISUAL INSPECTION AT VERTICAL STABILIZER LEFT DORSAL FIN ATTACH FITTING. HFEC INSPECTION CONFIRMED CRACKS EMANATING FROM EIGHT FASTENERS HOLES. REMOVED AND REPLACED DORSAL FIN Jul 25, 2001 · N127NK · Doug DC921 · Empennage StructureSDR WX0A01007Fuel Line · leakingLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, MAIN FUEL SUPPLY HOSE ASSEMBLIES ON RIGHT AND LEFT ENGINES TO FUEL CONTROL UNITS REPORTED LEAKING. FUEL LEAKAGE DETECTED DURING POST INSPECTION ENGINE RUNS. MAINTENANCE REMOVED AND REPLACED LEFT AJul 25, 2001 · N127NK · Doug DC921 · Engine Fuel DistributionSDR WX0A01008Wire · chafedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT ENGINE AC LOAD METER IN COCKPIT OVERHEAD PANEL TO HAVE CHAFED WIRES AT CONNECTOR MAINTENANCE REPAIRED AND DETERMINED AC LOAD METER WIRING AIW DPS 1.834-2.1. SYSTEM OPERATIONAL CHECK NOJul 25, 2001 · N127NK · Doug DC921 · AC Indicating SystemSDR WX0A01006Jackscrew · wornLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, HORIZONTAL STABILIZER JACKSCREW FAILED END PLAY CHECK PER WORK CARD 0855, SB 27A362 AND AD 2000-15-15. JACKSCREW END PLAY REPORTED AT .041 INCHES. REMOVED AND REPLACED HORIZONTAL STABILIZER JACKSCJul 25, 2001 · N127NK · Doug DC921 · Stabilizer Control SystemSDR WX0A01005Skin · corrodedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEVEL 1 CORROSION WAS FOUND IN LOWER AFT FUSELAGE SKIN AT AFT JACK PAD AREA. CORROSION DAMAGE TO FASTENERS IN AREA ALSO DETECTED. REMOVED INTERNAL AND EXTERNAL STRUCTURE IN LOWER FUSELAGE JACK PADJul 25, 2001 · N127NK · Doug DC921 · Fuselage Main, Plate/SkinSDR WX0A01004Skin · crackedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FORWARD CARGO DOOR INNER SKIN CRACKED IN THE RADIUS BELOW AFT LATCH COVER. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 51-10-4, 52-05 FIGURE 26A, 51-30-5, 51-30-2, Jul 25, 2001 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WXOA99031Slat · dentedAMA - BIRD STRIKE REPORTED TO LEFT WING AT 8500 FT DURING DESCENT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. BIRD STRIKE INSPECTION ACCOMPLISHED IAW DC-9 MM 05-56. FOUND LEFT WING NR 2 OUTBOARD LEADING EDGE SLAT TO HAVE SUSTAINED BIRD STRIKE DAMAGE. DENov 13, 1999 · N127NK · Doug DC921 · Leading Edge DevicesSDR WXOA99030Angle · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEVEL 1 CORROSION ON AFT STAIR ANGLE. REMOVED CORRODED ANGLE. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-9 SRM 51-10-2, 51-10-3 AND 51-30-2. (M)Oct 22, 1999 · N127NK · Doug DC921 · Fuselage Miscellaneous StructureSDR WXOA99029Beam · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN GALLEY SERVICE DOOR HORIZONTAL BEAM AFT EDGE. CRACK REPORTED APPROXIMATELY .240 INCH LONG, EXTENDING FROM FASTENER HOLE. FABRICATED DOUBLER PER DC-9 SRM 52-05 FIGURE 25, SHEET 7 ANDOct 22, 1999 · N127NK · Doug DC921 · Service DoorsSDR WXOA99028Frame · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND THREE CRACKES ON FUSELAGE FRAME STATION 718 AT STRINGER 17L. REMOVED DAMAGED MATERIAL. PERFORMED HFEC INSPECTION IAW OPS 4.751. NO EVIDENCE OF CRACKS EXTENDING FROM CUT OUT AREA. FABRICATEOct 22, 1999 · N127NK · Doug DC921 · Fuselage Main, FrameSDR WXOA99027Frame · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND 3.5 INCH CRACK IN RADIUS OF FUSELAGE FRAME STATION 737 AT LONGERON 17L. REMOVED DAMAGED SECTION OF FRAME. FABRICATED ANGLE, FILLER AND DOUBLER (RED W/C A134, B03, W063). INSTALLED REPAIR PAOct 22, 1999 · N127NK · Doug DC921 · Fuselage Main, FrameSDR WXOA99026Frame · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN AFT ACCESSORY COMPARTMENT RIGHT SIDE OF FRAME 859 AT LONGERON 13R NEAR LIGHTNING HOLE. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC-9 SRM 53-01, 51-10-2, 51-10Oct 22, 1999 · N127NK · Doug DC921 · Fuselage Main, FrameSDR WXOA99025Intercostal · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND INTERCOSTAL CRACKED AT FORWARD AREA OF AFT CARGO DOOR JAMB. REMOVED DAMAGED INTERCOSTAL AND REPLACED IAW EA M-7200-99-09504. (M)Oct 22, 1999 · N127NK · Doug DC921 · Fuselage Miscellaneous StructureSDR WXOA99024Doubler · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND INTERNAL DOUBLER EDGE OF RUDDER BROKEN AT REFERENCE ZR99. REMOVED DAMAGED INTERNAL DOUBLER. FABRICATED REPLACEMENT DOUBLER IAW DC-SRM 51-10-1. INSTALLED REPAIR DOUBLER IAW DC-9 SRM 51-30-2.Oct 20, 1999 · N127NK · Doug DC921 · Rudder StructureSDR WXOA99023Shear Tie · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED AND APPROXIMATE 2 INCH LONG CRACK ON SHEAR TIE BETWEEN LONGERON L14 AND L15 AT FUSELAGE STATION 766. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR SHEAR TIE (REF W/C A13Oct 16, 1999 · N127NK · Doug DC921 · Fuselage Miscellaneous StructureSDR WXOA99022Support · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION OF FORWARD CARGO DORO PER OPS 4.735 DETECTED CRACKED AT AFT SIDE OF INTERCOSTAL ANGLE SUPPORT LOCATED AFT SIDE OF FORWARD STOP. REMOVED CRACKED ANGLE SUPPORT. FABRICATED REPAIROct 16, 1999 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WXOA99021Shear Tie · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK OF APPROXIMATELY 2 INCH LONG ON SHEER CLIP BETWEEN LONGERON L15 AND L16 AT FUSELAGE STATION 766. FABRICATED REPAIR SHEER CLIP. REMOVED CRACKED SHEER CLIP AND INSOct 15, 1999 · N127NK · Doug DC921 · Fuselage Miscellaneous StructureSDR WXOA99020Skin · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED AT UPPER AFT AREA OF LEFT MLG DOOR NEAR HINGE. STOP DRILLED CRACK, INSTALLED DOUBLER P/N J060256-23 IAW SRM 52-05 AND EA HM-7200-99-09402. (M)Oct 15, 1999 · N127NK · Doug DC921 · Landing Gear DoorsSDR WXOA99019Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC DETECTED A CRACK ON ANGLE P/N 9912243-10 AT THE RIGHT PYLON BULKHEAD LOWER FRONT SPAR (F/S 786) EXTENDING FROM FASTENER HOLE APPROX .400 INCH LONG. REMOVED AND REPLACED ANGLE IAW DC-9 SRM Oct 15, 1999 · N127NK · Doug DC921 · Nacelle/Pylon StructureSDR WXOA99018Skin · dentedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, DENT DISCOVERED ON RIGHT SIDE OF RUDDER BETWEEN RIBS 23 AND 24, LOCATED APPROXIMATELY 18 INCH FROM TRAILING EDGE. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR EXTERNAL DOUBLER IAW DC-9 SRM 55003, POct 15, 1999 · N127NK · Doug DC921 · Rudder, Plate/SkinSDR WXOA99017Fitting · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTIN PERFORMED PER OPS 4.751 OF LEFT PYLON 'BATH TUB' FITTING. INDICATION OF CRACK NOTED AT FAIL/SAFE STRAP INBOARD UPPER RIVET. DIMENSION OF CRACK APPROXIMATELY 2.5 INCH IN LENGTH. Oct 15, 1999 · N127NK · Doug DC921 · Nacelle/Pylon StructureSDR WXOA99016Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION PERFORMED PER OPS 4.735 AT FORWARD CARGO DOOR. INDICATION OF CRACK NOTED ON INTERCOSTAL ANGLE FITTING, LOCATED AFT SIDE OF LOWER FORWARD DOOR STOP. REMOVED EXISTING ANGLE AND FOct 15, 1999 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WXOA99015Door Pan · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED AT PAN AND INTERCOSTAL INTERSECTION OF TOP FORWARD CORNER OF FORWARD CARGO DOOR. FABRICATED REPAIR DOUBLER, STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 51-10-2, 51-1Oct 14, 1999 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WXOA99014Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK INDICATION ON FORWARD CARGO DOOR AT FORWARD SIDE OF LOWER AFT DOOR STOP, FORWARD SIDE OF INTERCOSTAL FITTING. REMOVED CRACKED ANGLE, FABRICATED REPAIR ANGLE AND IOct 14, 1999 · N127NK · Doug DC921 · Cargo/Baggage DoorsSDR WXOA99013Longeron · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK INDICATION AT LONGERON 16, FUSELAGE STATION 786 RIGHT. CRACK EVIDENT ON LONGERON AT CONNECTION POINT OF 'L' BRACKET ON AFT SIDE OF BULKHEAD. REMOVED DAMAGED AREA Oct 14, 1999 · N127NK · Doug DC921 · Fuselage Main, Longeron/StringerSDR WXOA99012Panel · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER ACCESS PANEL 3806 HAS CRACK PROPOGATING FROM EXISTING STOP DRILL. STOP DRILLED NEW CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 51-10-2, 51-10-3, 51-30-2 Oct 14, 1999 · N127NK · Doug DC921 · Vertical Stabilizer, Plate/SkinSDR WXOA99011Duct · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER AIR INTAKE DUCT AT 12 O'CLOCK POSITION HAS A CRACK APPROXIMATELY .25 INCHES LONG. REPAIRED CRACK IAW BOEING EA M-7200-99-09364. (M)Oct 14, 1999 · N127NK · Doug DC921 · Vertical StabilizerSDR WXOA99010Frame · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION AT STATION 766 RIGHT SIDE, BETWEEN LONGERON 15 AND 16, DETECTED CRACK IN RADIUS AT 3RD FASTENER BELOW LONGERON 15. REMOVED DAMAGED SECTION OF FORMER, FABRICATED REPAIR FORMER ANOct 14, 1999 · N127NK · Doug DC921 · Fuselage Main, FrameSDR WXOA99009Support · corrodedMHV - DURING AIRCRAFT SCHEDULED INSPECTON AT REPAIR STATION, LEVEL 1 SURFACE CORROSION DETECTED AT THREE PLACES IN AFT RIGHT LAV FLOOR SUPPORT FRAME, STATIONS 786 TO 826, RBL PLUS/MINUS 16. REMOVED CORRODED PARTS FROM FLOOR SUPPORT FRAME. FABRICATED 2 'L' MEOct 14, 1999 · N127NK · Doug DC921 · Fuselage Miscellaneous StructureSDR WXOA99008Clips · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKS DETECTED IN TWO CLIPS ON RIGHT ENGINE LOWER APRON. REMOVED CRACKED CLIPS, FABRICATED REPAIR CLIPS PER DC-9 SRM 51-10-2 AND SAMPLE, ALODINE AND PRIMED CLIPS PER DC-9 SRM 51-10-3, AND INSTALLEOct 12, 1999 · N127NK · Doug DC921 · Nacelle/Pylon StructureSDR WXOA99007Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, PERFORMED NDT HFEC INSPECTION PER OPS 4.735. RESULTS OF INSPECTION DETECTED CRACK ON ANGLE P/N 9912243-9 AT THE LEFT PYLON LOWER FRONT SPAR STATION Y781/Z20. REMOVED CRACKED ATTACH ANGLE AND INSTAOct 11, 1999 · N127NK · Doug DC921 · Nacelle/Pylon StructureSDR WXOA99006Frame · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT ACCESSORY COMPARTMENT FRAME 859 AT LONGERON L13 IS CRACKED BY LIGHTNING HOLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-9 SRM 53-01 PAGE 9, 51-10-2, 51-10-3 AND 51-30-2. (M)Oct 6, 1999 · N127NK · Doug DC921 · Fuselage Main, FrameSDR WXOA99005Duct · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED IN COOLING EXHAUST DUCT AT FUSELAGE STATION 261 AND LONGERON L21. WELDED CRACKS TWO PER REPAIR STATION PROCEDURES IAW FAA AC 43.13 1A. (M)Oct 6, 1999 · N127NK · Doug DC921 · Air Distribution SystemSDR WXOA99004Bracket · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT WING SLAT TRACK NR 2 FORWARD LOWER PANEL BRACKET CRACKED AND OUTBOARD BRACKET HOLE ELONGATED. REMOVED TWO DAMAGED BRACKETS, FABRICATED REPAIR BRACKETS AND INSTALLED REPAIR BRACKETS IAW DC-9 SROct 6, 1999 · N127NK · Doug DC921 · Wing Miscellaneous StructureSDR WXOA98001Connector · failedFAT - DURING ACCOMPLISHMENT OF SCHEDULED AIRCRAFT MAINTENANCE, FOUND DAMAGED ELECTRICAL WIRING CONNECTOR AT PRODUCTION SPLICE FOR ROWS 9-10 (RT) CABIN INTERIOR OVERHEAD AND SIDEWALL LIGHTING. GROUND WIRE DISCOVERED LOOSE AT CONNECTOR CAUSING ELECTRICAL ARCINGOct 14, 1998 · N127NK · Doug DC921 · Passenger Compartment Lighting
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