N986HA
Registered owner: 645 AERONAUTICAL SYSTEMS GROUP (AESG), OH (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.
17 reports on file, 1996-08-12 – 2003-11-17.
Part: RELAY — DEFECTIVE (AUTOFEATHER) · airframe 18,438 hrs · 20,905 cycles
AUTOFEATHER DID NOT ARM AT 97 PERCENT, 60 KTS, ABORTED TAKEOFF. REPLACED AUTOFEATHER CONTROL RELAY.
Part: SOCKET — BURNED (CABIN LIGHT) · airframe 18,278 hrs · 20,732 cycles
STRONG ELECTRICAL BURNING ODOR AROUND ROW 7.
Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 9,050 hrs · 9,855 cycles
Lav smoke detector went off shortly after departure. Captian returned to field, no smoke was detected. Lav smoke detector was replaced proir to this flight for same problem. MEL lav smoke detector, generated EO to pull and collar circuit breaker. Smoke detector replaced 1 MARCH 2003.
Earlier reports · 1996–2002 · 14 reports
2002
Part: FAN — OVERHEATED · airframe 14,600 hrs · 17,067 cycles
A BURNING SMELL WAS REPORTED COMING FROM THE GALLEY/COAT CLOSET AREA OF THE CABIN. AIRCRAFT DIVERTED TO AVL. REPLACED AVIONICS BAY COOLING FAN.
2001
Part: BRAKE — SMOKE (RT MLG)
ON LANDING ROLLOUT ATC REPORTED HEAVY SMOKE OFF RIGHT MLG. INSPECTED AND CLEANED RIGHT MAIN LANDING BRAKES, LEAK CHECKED WITH PARKING BRAKE APPLIED AND DURING TAXI. NO DEFECT FOUND ALL OPERATION NORMAL IAW AIRCRAFT MM 32-40-00. (M)
2000
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,762 hrs · 13,032 cycles
MID CABIN OVERHEAD WHITE DOWN EMERGENCY LIGHT OUT. MAINTENANCE RELAMPED, NO FIX. ALLOWED EMERGENCY BATTERIES TO CHARGE OFF AIRCRAFT POWER. RELATCHED EMERGENCY LIGHT BATTERY DISABELING CIRCUIT PER MAINTENANCE MANUAL 33-35-00. OPS CHECK GOOD.
Part: PIPE — CRACKED (DORSAL FAIRING) · airframe 9,539 hrs · 11,725 cycles
CREW REPORTED THE CABIN CEILING BECAME VERY HOT FROM ROW 4 THRU ROW 7 WITH A HOT BLEED AIR SMELL. FOUND BLEED PIPE IN DORSAL FAIRING CRACKED. REPLACED PIPE AND PERFORMED CONDUCTIVITY TEST ON ADJACENT STRUCTURE.
1999
Part: LIGHT — MALFUNCTIONED (CABIN)
F/A'S EMERGENCY CALL AND ATT LIGHTS STAY ON ALL THE TIME. FLIGHT DECK EMERGENCY AND CALL LIGHTS STAY ON. SYSTEMS WORK BUT LIGHT STAYS ON. REF: LOG PAGE 37752. REMOVED AND REPLACED PA ELECTRONICS UNIT, OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN)
NR 1 AND NR 3 OVHD EMERGENCY CEILING AISLE LIGHTS ARE INOP. REMOVED AND REPLACED BATTERIES PS1 AND PS2, OPS CHECK GOOD.
Part: SWITCH — FAILED (NR 1 & 2 ENGINE)
TORQUE FLUX ON BOTH ENGINES FOLLOWED BY AN OIL SMELL. SHUT BOTH BLEEDS OFF AND IT STABILIZED FOR APPROXIMATELY 5 MINUTES, THEN NR 2 TORQUE DECREASED TO 45 PERCENT. REPLACED NR 1 AND NR 2 HP BLEED SWITCHES (P/N 7G899) (S/N 356), (S/N 272) OFF. ALSO, FOUND NR 2 HP BLEED VALVE GASKET BLOWN. REPLACED GASKET.
1998
Part: FUEL PUMP — FAILED (NR 2 ENGINE)
FLT 3464 - MCO-MIA - AFTER TAKEOFF, WHILE CLIMBING AT 13,000 FT, THE NR 2 ENGINE FAILED. THE CREW DECLARED AND EMERGENCY AND RETURNED TO MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 FUEL PUMP AND MECHANICAL FUEL CONTROL (MFC). (M)
Part: FUEL PUMP — FAILED (NR 2 ENGINE)
FLT 3464 - MCO-MIA - AFTER TAKEOFF, WHILE CLIMBING AT 13,000 FT, THE NR 2 ENGINE FAILED. THE CREW DECLARED AND EMERGENCY AND RETURNED TO MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 FUEL PUMP AND MECHANICAL FUEL CONTROL (MFC). (M)
1997
Part: CONTROL BOX — FAILED (CABIN)
FLT 3410 - TLH-TPA - DURING PREFLIGHT CHECKS, FOUND SEVERAL INTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY LIGHTS CONTROL BOX. (M)
Part: TQ SIGNAL COND — FAILED (NR 1 ENGINE)
FLT 3005 - CLT-TLH - AFTER TAKEOFF, UPTRIM ADVISORY LIGHT FLICKERED ON AND OFF AND NR 1 ENGINE UPTRIMMED. THE A/C CONTINUED ON TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU). ON SUBSEQUENTLY FLIGHT, AFTER T/O, 3087 TLH TO TPA, THE NR 2 TORQUE ROLLED BACK, BOTH ANALOG AND DIGITAL, UPTRIM ADVISORY LIGHT WAS ON. THE AIRCRAFT RETURNED TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 TSCU. (M)
Part: TQ SIGNAL COND — FAILED (NR 2 ENGINE)
FLT 3005 - CLT-TLH - AFTER TAKEOFF, UPTRIM ADVISORY LIGHT FLICKERED ON AND OFF AND NR 1 ENGINE UPTRIMMED. THE A/C CONTINUED ON TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU). ON SUBSEQUENTLY FLIGHT, AFTER T/O, 3087 TLH TO TPA, THE NR 2 TORQUE ROLLED BACK, BOTH ANALOG AND DIGITAL, UPTRIM ADVISORY LIGHT WAS ON. THE AIRCRAFT RETURNED TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 TSCU. REFERENCE HNAA9798634.
1996
Part: TSCU — FAILED (NR 2 ENGINE)
TLH/TPA - FLT 3240 - ON CLIMB-OUT AT 300 FEET, AUTOFEATHER SELECTED ON, NR 1 ENGINE UP-TRIM LIGHT FLICKERED, AND ENGINE ATTEMPTED TO UP-TRIM. THE AIRCRAFT TURNED BACK TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU) AND TIGHTENED NR 2 TORQUE PROBE CANNON PLUG. (X)
Part: VALVE — STUD BROKEN (HI PRESS SOV)
SHUT-OFF VALVE STUD FOUND BROKEN DURING POST-FLIGHT INSPECTION. NO IN-FLIGHT INDICATIONS WERE OBSERVED. CAUSE UNKNOWN. VALVE ASSY WAS REPLACED AND ALL SYSTEMS FUNCTIONED NORMALLY.