N158CA
Registered owner: OSAGE AVIATION LLC, KS (owner ≠ operator)
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.
22 reports on file, 1995-01-08 – 2015-12-26.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,140 hrs · 19,080 cycles
LOWER LT OVERWING EMER EXIT LIGHT OUT. REPLACED LIGHT BULB IAW AMM 33-51-15. OPERATIONS CHECKED GOOD.
Earlier reports · 1995–1996 · 21 reports
1996
Part: INDICATOR — DEFECTIVE (RT PROPELLER)
RIGHT PROPELLER RPM IS INDICATING 1150 AT GROUND IDLE. REPLACED THE RT PROPELLER INDICATOR. PART TOTAL CYCLES, 26,067.
Part: BULB — FAILED (CABIN)
EMERGENCY FLOOR LIGHTING AT MAIN CABIN DOOR IS INOP. REPLACED LIGHT BULB, ALL LIGHTING OPERATIVE.
Part: BATTERY PACK — DISCHARGED (CABIN)
FOUR EMERGENCY LIGHTS WERE INOP. REPLACED EMERGENCY LIGHT BATTERY PACK.
Part: ENGINE — FAILED (RIGHT)
RIGHT ENGINE FAILED DURING TAKEOFF. REPLACED RIGHT ENGINE.
Part: HYD PUMP ASSY — FAILED (LANDING GEAR)
LT AND RT MLG DID NOT DOWN LOCK WHEN SELECTED DURING LANDING APPROACH. REPLACED THE HYDRAULIC PUMP ASSY.
Part: EROSION GUARD — LOOSE (RT PROP)
EROSION GUARD ON ONE BLADE OF RT PROPELLER IS LOOSE AND PEELING. REBONDED EROSION GUARD.
Part: ACTUATOR — FAILED (LT PITCH TRIM)
THE MAIN PITCH TRIM IS INOP. REPLACED THE PITCH TRIM ACTUATOR.
Part: SHOULDER HARNESS — MALFUNCTIONED (COPILOTS)
COPILOTS SHOULDER HARNESS LOCK DOES NOT WORK. REPLACED SHOULDER HARNESS.
Part: INNER RACE — SPUN (RT MLG)
MECHANIC REMOVED WHEEL FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS.
Part: CONTROL BOX — DEFECTIVE (LANDING GEAR)
LANDING GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION. REPLACED THE LAND GEAR CONTROL BOX.
1995
Part: FLIGHT CONTROLS — VIBRATION (CONTROL YOKES)
DURING TAKEOFF, A FORE AND AFT VIBRATION WAS NOTED IN CONTROL YOKES. FLIGHT CONTROL SYSTEM WAS INSPECTED AND NO DEFECTS NOTED. ACFT RELEASED FOR FLIGHT CHECK WHICH WAS SATISFACTORY.
Part: COMPUTER — DEFECTIVE (NR 1 AHRS)
LEFT AND RIGHT HEADING COMPARATOR YELLOW FLAG DURING FLIGHT. REPLACED THE NR 1 AHRS COMPUTER.
Part: CONTL VALVE — DEFECTIVE (LT DUCT)
LEFT DUCT OVERHEAT WARNING DURING FLIGHT. REPLACED THE DUAL TEMPERATURE CONTROL VAVLE.
Part: CONNECTOR — DEFECTIVE (RT PGB)
RT PROPELLER GEAR BOX OIL PRESSURE INDICATOR WAS FLUCTUATING BETWEEN 30 AND 200 PSI. REPLACED THE PGB OIL PRESSURE TRANSDUCER WIRING CONNECTOR.
Part: BEARING — WORN (LT AILERON)
SHUDDER FELT THROUGH CONTROL YOKE DURING INFLIGHT TURNS. REPLACED LT AILERON BEARINGS.
Part: OIL PRESS TRANS — DEFECTIVE (RT PROP G BOX)
RIGHT PROPELLER GEARBOX INDICATED ZERO OIL PRESSURE. FLIGHT RETURNED TO CVG. REPLACED OIL PRESSURE TRANSDUCER.
Part: INNER RACE — SPUN (LT MLG WHEEL)
MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT.
Part: EEL BATTERY — DISCHARGED (CABIN)
EMERGENCY EXIT SIGN AT MAIN CABIN DOOR WILL NOT ILLUMINATE. REPLACED EMERGENCY BATTERY.
Part: EEL BATTERY — DISCHARGED (CABIN)
EMERGENCY LIGHTS AT LT EMERG EXIT AND 5A, 7A ARE INOP. REPLACED BATTERY PACKS.
Part: PROP — DAMAGED (LEFT)
LEFT PROPELLER HAS BLADE TIP DAMAGE. REPLACED PROPELLER.
Part: AIR VALVE — DEFECTIVE (RT ENGINE)
RT ENGINE AIR VALVE WARNING LIGHT IS ON. REPLACED RT AIR VALVE.