N435KD
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
38 reports on file, 2014-08-17 – 2019-11-04.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 76,268 hrs · 15,794 cycles
CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 50L F.S.1621-1721. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 52 F.S. 1561-1601. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 48R F.S.1561-1581. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 51L F.S.1601-1621.CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 49R F.S. 1629.CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 50R F.S. 1649.CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 51R F.S. 1629.
Part: ENGINE — FAILED (NR 1) · airframe 76,206 hrs · 15,727 cycles
#1 ENGINE FAILURE @ FL200 ENG 1 FADEC MAINT LEVEL 1 ALERT - INTERMITTENT ROUGH VIBRATION EVERY 10-15 SECONDS WITH NO INDICATION ON SYNOPTIC PAGE
Earlier reports · 2014–2017 · 36 reports
2017
Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 74,966 hrs · 14,977 cycles
CORROSION ON THE UPPER SURFACE OF THE ARP7264-1 DOUBLER ON THE LOWER WING SKIN XORS 264 LEFT WING PLATING AFT OF THE REAR SPAR.
Part: CHANNEL — CRACKED (RT WING) · airframe 74,966 hrs · 14,977 cycles
RIGHT WING LEADING EDGE AT XORS 795 ACCESS PANEL LOWER SIDE OF LEADING EDGE ACCESS PANEL FORWARD CHANNEL IS CRACKED.
Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 74,966 hrs · 14,977 cycles
LOWER FRAME ANGLE OF THE AFT SIDE OF THE BULK CARGO DOOR OPENING IS CORRODED
Part: SKIN — CRACKED (LT WING LE) · airframe 74,966 hrs · 14,977 cycles
LEFT WING DROOPED LEADING EDGE SKIN HAS 2 CRACKS NEAR THE OUTBOARD FLEX SKIN ATTACH BOLT.
Part: RIB — CRACKED (RT WING LE) · airframe 74,966 hrs · 14,977 cycles
RIGHT WING FIXED LEADING EDGE RIB AT WING STATION 725 IS CRACKED IN THE LOWER AFT RADIUS.
Part: RIB — CRACKED (RT WING LE) · airframe 74,966 hrs · 14,977 cycles
RIGHT WING LEADING EDGE RIB IS CRACKED AT WING STATION 800
Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 74,966 hrs · 14,977 cycles
AFT LOWER CORNER OF THE AFT CARGO DOOR FRAME IS CORRODED.
Part: SKIN — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 74,966 hrs · 14,977 cycles
NR 1 L/E SLAT SKIN ON THE OUTBOARD END UNDER THE STAINLESS RUB STRIP HAS A CORRODED HOLE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,966 hrs · 14,977 cycles
RIGHT FORWARD DOOR HANDLE EMERGENCY LIGHT IS INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,966 hrs · 14,977 cycles
RIGHT FORWARD DOOR EMERGENCY LIGHTS L2-480 & L2-481 ARE INOPERATIVE.
Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 74,966 hrs · 14,977 cycles
STATION 5-0 LONGERON 7L SPLICE FITTING IS CRACKED. FOUND DURING X-RAY INSPECTION.
Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 74,966 hrs · 14,977 cycles
STATION 5-0 LONGERON 3L SPLICE FITTING CRACKED. FOUND DURING X-RAY INSPECTION.
Part: SPAR — DAMAGED (LT WING) · corrosion level 2 · airframe 74,966 hrs · 14,977 cycles
ZONE 518, LEFT WING LEADING EDGE SPAR AREA HAS SCRAPES AND CORROSION ON THE LEADING EDGE OF THE SPAR
2016
Part: ENGINE — LEAKING (NR 3) · airframe 74,068 hrs · 14,734 cycles
SMOKE IN UPPER CARGO COMPARTMENT AND COURIER COMPARTMENT, UNABLE TO GET RID OF IT, TO THE POINT IT WAS IRRITATING TO THROAT. CLOSE TO WEAR OXYGEN MASK. SUSPECT NR 3 ENGINE OIL LEAKING INTO BLEED AIR SYS.
Part: COALESCER BAG — DIRTY (ZONE 100) · airframe 74,063 hrs · 14,732 cycles
DIVERTED, DUE TO SMOKE DEVELOPED, LOOKED LIKE ORIGINATING FROM MAIN CARGO DECK. COULD NOT DUPLICATE SMOKE ON THE GROUND. DEFERRED NR 2 AIR CONDITIONING PACK AS MOST PROBABLE CAUSE. REPLACED COALESCER BAG IN ALL 3 AIR CONDITIONING SYSTEMS.
2015
Part: AIR DUCT — BLOWN (NR 3 ENGINE) · airframe 73,263 hrs · 14,538 cycles
PASSING 9500 FEET, NOTICED AMBER HYD ALERT NR 4 DU. LEVEL 3 ALERT FOR FIRE ENG NR 3 WENT OFF WITH FIRE BELL & ALL LIGHTS. THROTTLE NR 3 RETARDED, ALERT REMAINED PRESENT. SHUT OFF FUEL VLV, ALERT DISAPPEARED. DISCHARGED FIRE BOTTLE & DIVERTED FLIGHT. DISCOVERED BLOWN DUCT FROM HIGH PRESSURE TURBINE COOLING SYS.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION AT STATION 1690 TO 1701 STRINGER 42R TO 43R ON INNER SKIN DOUBLER.
Part: SKIN — CHAFED (RT WING) · airframe 72,688 hrs · 14,398 cycles
RIGHT WING, UPPER SURFACE SKIN OF LE AT APPROX STATION 1180 SKIN IS CHAFED & WORN FROM SLAT SEAL.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
AFT SIDE OF STATION 2007 BULKHEAD 2" BELOW APU BLEED DUCT HAS CORROSION ON DOUBLER.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
EVIDENCE OF CORROSION IN FWD LOWER CARGO PIT STRINGER 48L BETWEEN STATION 1129 6-50 & 1129 6-70.
Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 72,688 hrs · 14,398 cycles
NUMBER 1 PYLON INBD PANEL NR 437, FRAME HAS FASTENERS PULLING THROUGH SKIN.
Part: SKIN — CRACKED (LT WING) · airframe 72,688 hrs · 14,398 cycles
LEFT WING LOWER SKIN AT FUEL PANEL ACCESS DOOR CUT OUT AT STATION XORS 696.730 HAS 10 EACH FASTENER HOLES WITH CRACK INDICATION.
Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
OUTBOARD HINGE FITTING ON RT OTBD TE FLAP HAS EVIDENCE OF CORROSION ON OTBD LOWER MOUNT BOLT.
Part: HINGE — BROKEN (CARGO DOOR) · airframe 72,688 hrs · 14,398 cycles
MAIN CARGO DOOR FWD HINGE IS BROKEN & AFT HINGE PIN IS SEIZED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,688 hrs · 14,398 cycles
EVIDENCE OF A CRACK AT STATION 1129 6-100 APPROX STRINGER 38L.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION ON SUPPORT FITTING ON PRESS DECK UNDER MD FLOOR STATION 1360, RBL 50.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION ON PRESS DECK UNDER MAIN DECK FLOOR AT STATION 1350 AT LBL 110.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION ON PRESS DECK UNDER MAIN DECK FLOOR AT STATION 1340 AT LBL 110.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION IN CTR CARGO COMPARTMENT STATION 1665, LONGERON 45R.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
CORROSION IN CTR CARGO COMPARTMENT STATION 1685 AT LONGERON 43R.
Part: SKIN — CRACKED (RT WING) · airframe 72,688 hrs · 14,398 cycles
RIGHT WING LOWER SKIN AT FUEL PANEL ACCESS DOOR CUT OUT AT STATION XORS 696.730 HAS 20 EACH FASTENER HOLES WITH CRACK INDICATIONS.
Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
LEFT WING ROOT REAR SPAR TO TRAPEZOIDAL PANEL SPLICE PLATE HAS CORROSION AROUND SEVERAL FASTENERS.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,688 hrs · 14,398 cycles
FUSELAGE FRAME AT STATION 410.580 BILGE AFT OF LAVATORY SERVICE TUBE CORROSION ON FRAME.
2014
Part: FUEL FILTER — DIRTY (NR 2 ENGINE) · airframe 71,720 hrs · 12,201 cycles
NR 2 ENGINE FUEL FILTER OFF LIGHT DURING TAKE OFF ROLL. REMOVED, CLEANED AND REINSTALLED FUEL FILTER. PERFORMED ENGINE RUNS. SYSTEM OPERATIONALLY CHECKED NORMAL.
Part: WIRE — BURNED (LT FUEL PUMP) · airframe 71,714 hrs · 14,179 cycles
LEFT PUMP OFF ALERT. TROUBLESHOOTING REVEALED SEVERAL BURNED AREAS OF WIRING HARNESS ABOVE TAIL FUEL TANK.
Part: UNKNOWN — MULTIPLE FAIL (INDICATORS) · airframe 71,709 hrs · 14,178 cycles
DURING CLIMB, LOSS OF MULTIPLE INDICATIONS, LOST BOTH ADCS, AIR DATA COMPUTER NR 1 AND 2. LOST FCC NR 2 AFTER TAKEOFF. STANDBY ALTIMETER/AIRSPEED UNRELIABLE.