N387HA
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.
6 reports on file, 1997-11-17 – 2019-10-18.
Part: PACKING — MISSING (DIP STICK FILLER) · airframe 10,693 hrs · 8,037 cycles
PILOTS NOTICED LOW OIL PRESSURE INDICATION AFTER CLIMBING THRU 30,000 FEEET ON LEFT ENGINE. WENT THRU OILPRESSURE CHECK LIST AND REDUCED POWER. LOW OIL PRESSURE LIGHT CAME ON. WENT THRU ENGINE SHUT DOWN CHECK LIST AND N2 WENT TO ZERO BEFORE ENGINE WAS SHUT DOWN.
Part: WARNING LIGHT — ILLUMINATED (CABIN PRESSURE) · airframe 10,610 hrs · 7,956 cycles
EMERGENCY PRESSURE CAME ON AFTER TAKE OFF. RESET LEFT, COULD NOT RESET RIGHT AT ANY ALTITUDE.
Part: TUBE — CHAFED (CABIN PRESSURE) · airframe 10,603 hrs · 7,947 cycles
PASSING 10,000 FT, CALLED FOR THE AFTER TAKEOFF CLIMB CHECKLIST. APPROXIMATELY, AT THAT TIME THE CABIN ALTITUDE LIGHT CAME ON. NOTICED THAT THE CABIN ALTITUDE WAS READING 10,000 FT. SHORTLY AFTER, THE EMERGENCY BLEEDS KICKED ON AND HEARD THE CABIN ALTITUDE HORN, CLIMBING THROUGH APPROXIMATELY 11,0000FT. DIRECT PMD AT THAT TIME AND TOLD ATC LEVELING OFF AT 12,000 FT, UNABLE TO PRESSURIZE, AND WANTED A DESCENT TO 10,000 FT AND VECTORS FOR THE ILS16R. CLEARED TO DESCEND. CO-PILOT RESET THE EMERGENCY PRESSURIZATION SYSTEM, LT & RT BLEED OFF THEN ON ONE AT A TIME, BUT DID NOT RUN THE QRH DUE TO OUR ALTITUDE AND PROXIMITY TO THE AIRFIELD. ONCE THE EMERGENCY PRESSURIZATION SYS WAS RESET, CONTINUED TO THE FIELD. RAN THE NORMAL CHECKLISTS AND LANDED UNEVENTFULLY. DID NOT DECLARE AN EMERGENCY.
Part: SENSOR — FALSE INDICATION (BLEED SYS) · airframe 10,211 hrs · 7,596 cycles
RT BLEED LIGHT CAME ON DURING CLIMBOUT. JETTISONED APPROX 1500 LBS FUEL. DIVERTED TO AND LANDED AT MX. FOUND RT BLEED AIR HIGH TEMP SENSOR, BAD.
Part: HEATER — SMOKE (CABIN) · airframe 10,139 hrs · 7,552 cycles
WHITE SMOKE AND FUMES FROM AFT RT PASSENGER OVERHEAD VENT. IMMEDIATELY RETURNED AND UNEVENTFUL LANDING AT DEPARTURE. FOUND AUX HEAT HEATER ODOR, PLACARDED AUX HEAT SWITCH INOPERATIVE IAW MEL 21-20.
Part: RIB — CRACKED (RUDDER)
UPON REMOVAL OF THE LEFT LOWER RUDDER CLOSEOUT SKIN, THE INTERSPAR RIB WAS FOUND CRACKED ACROSS THE ENTIRE WIDTH OF THE RIB. THE DAMAGE TO THE RIB WAS A CLEAR INDICATION OF A CRACK CAUSED BY FATIGUE. THE DECREASED INTEGRITY ALSO CAUSED THE ATTACHING RUDDER SKIN TO CRACK.