N569JA
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.
12 reports on file, 1995-01-25 – 2001-05-21.
Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE)
LEFT ENGINE SHUTDOWN IN CRUISE DUE TO POWER DROPPING OFF, POWER LEVER ADVANCE HAD NO EFFECT. MADE UNEVENTFUL LANDING ANC. REPLACED NR 1 ENGINE FUEL CONTROL UNIT. GROUND OPERATIONAL CHECK GOOD. (M)
Part: CLAMP — BROKEN (EXHAUST TAILPIPE)
RIGHT E-HANDLE PULLED AFTER TAKEOFF DUE TO FIRE WARNING ZONE 1. FOUND NR 2 ENGINE U-JOINT TO INTERMEDIATE PIPE CLAMP BROKEN. REMOVED AND REPLACED SAME. (X)
Part: FIRE LOOP — SHORTED (NR 2 ENGINE)
ZONE 1 FIRE WARNING ILLUMINATED WITH WARNING BELL ON NR 2 ENGINE. NO VISIBLE SIGN OF FIRE. SHUT DOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT ANC. NO PHYSICAL EVIDENCE OF FIRE. REPLACED FORWARD ZONE 1 FIRE DETECTION LOOP ON NR 2 ENGINE. GROUND OPS CHECK GOOD. (M)
Part: FIRE LOOP — SHORTED (NR 2 ENGINE)
ZONE 1 FIRE WARNING ILLUMINATED WITH WARNING BELL ON NR 2 ENGINE. NO VISIBLE SIGN OF FIRE. SHUT DOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT ANC. NO PHYSICAL EVIDENCE OF FIRE. REPLACED FORWARD ZONE 1 FIRE DETECTION LOOP ON NR 2 ENGINE. GROUND OPS CHECK GOOD. (M)
Part: GENERATOR — FAILED (LT ENGINE)
LOST BOTH AIRSPEED INDICATORS ON APPROACH TO CDV IN HEAVY ICING. PITOT HEAT SELECTED ON AND FUNCTIONING. SELECTED ALTERNATE STATIC SOURCE ON BOTH SIDES. LEFT GEN DROPPED OFF LINE. RETURNED TO ANC AND MADE UNEVENTFUL LANDING. REPOSITIONED STATIC SWITCHES TO NORMAL.. PURGED PITOT STATIC SYSTEM OF MOISTURE. REPLACED CRACKED PILOTS DRAIN CAP. CHECKED PITOT TUBE HEATERS, SYSTEM GROUND CHECKS GOOD. REPLCED LEFT DC GENERATOR. (M)
Part: BEARING — DESTROYED (RT MLG)
RIGHT MLG OUTBOARD WHEEL ASSY DEPARTED AIRCRAFT ON LANDING ANC BOTH WHEEL BEARINGS HAD DISINTIGRATED. NO EVIDENCE OF HEAT DISTRESS. GREASE WAS FOUND IN BEARING CAVITY AND ON REMAINING ROLLERS. BEARINGS INSTALLED NEW TWO MONTHS EARLIER. SUSPECT DAMAGED OR DEFECTIVE BEARING.
Part: SCREW — MISSING (RT WING TE)
LOOSE PANEL ON WING FLAP PULLEY COVER. RETURNED TO ANC, MADE UNEVENTFUL LANDING. REPLACED COVER SCREWS. NO OTHER DAMAGE NOTED.
Part: AIR DISTRIBUTION — SMOKE (CABIN)
SMOKE DETECTED IN CABIN ON LANDING. PERFORMED ENGINE RUN, PRESSURIZATION SYSTEM ON, CABIN HEAT FULL HOT, SUPPLEMENTAL HEATER ON, AND COMPLETED ENVIRONMENTAL SYSTEM TEST. NO SMOKE DETECTED, ALL SYSTEMS OPERATE NORMAL. VISUAL INSPECTION OF ENGINE DRIVEN COMPRESSOR OUTLET DUCT PERFORMED, NO OIL DETECTED AIRCRAFT RELEASED.
Part: SWITCH BRACKET — LOOSE (LT MLG)
LEFT GEAR DOWN LIGHT WOULD NOT ILLUMINATE. RETURNED TO ANC AND MADE UNEVENTFUL LANDING. TIGHTENED AND RERIGGED LOOSE LT MLG DOWNLOCK SWITCH BRACKET IAW CV580 M/M 32-61-31 PG 501 AND 502. RETRACT TEST SUCCESSFUL.
Part: UPLOCK LEVER — CRACKED (NLG)
NOSE LANDING GEAR WOULD NOT RETRACT. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE.
Part: UPLOCK LEVER — CRACKED (NLG)
GEAR UNLOCK LIGHT WOULD NOT GO OUT AFTER DEPARTURE. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE. RE-RIGGED NOSE LANDING GEAR AND PERFORMED RETRACT TEST.
Part: BATTERY PACK — DISCHARGED (CABIN EEL)
INTERIOR EMERGENCY EXIT LIGHT ON RT SIDE ROW 3 INOP. REPLACED BATTERY PACK.