19981118045709I

Incident

FAA incident report · Beech A36 · Carlsbad, CA · November 18, 1998

Date
November 18, 1998 · 07:56 local
Place
Carlsbad, CA
Airport
Mcclellan-Palomar
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N2024Q
Reported as
Beech A36
Reported engine
Continental IO520B
People aboard
2
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On November 18, 1998, at approximately 0756, the pilot of N2024Q, a Beechcraft A36, noted smoke in the cockpit and elected toland at the closest available airport. The aircraft was not damaged and there were no injuries. The aircraft was being operated under federal aviation regulation 91 when the incident occurred. The flight originated at san diego, California, VFR conditions prevailed at the time of the incident, and no VFR flight plan was filed. Investigation disclosed that the exhaust pipe had departed the aircraft, and excessive heat was directed into the engine compartment aft of the turbocharger. The exhaust clamp failed allowing the exhaust pipe to depart. The clamp was forwarded to NTSB Washington, DC for further testing.

As the FAA filed it

ON NOVEMBER 18, 1998, AT APPROXIMATELY 0756, THE PILOT OF N2024Q, A BEECHCRAFT A36, NOTED SMOKE IN THE COCKPIT AND ELECTED TOLAND AT THE CLOSEST AVAILABLE AIRPORT. THE AIRCRAFT WAS NOT DAMAGED AND THERE WERE NO INJURIES. THE AIRCRAFT WAS BEING OPERATED UNDER FEDERAL AVIATION REGULATION 91 WHEN THE INCIDENT OCCURRED. THE FLIGHT ORIGINATED AT SAN DIEGO, CALIFORNIA, VFR CONDITIONS PREVAILED AT THE TIME OF THE INCIDENT, AND NO VFR FLIGHT PLAN WAS FILED. INVESTIGATION DISCLOSED THAT THE EXHAUST PIPE HAD DEPARTED THE AIRCRAFT, AND EXCESSIVE HEAT WAS DIRECTED INTO THE ENGINE COMPARTMENT AFT OF THE TURBOCHARGER. THE EXHAUST CLAMP FAILED ALLOWING THE EXHAUST PIPE TO DEPART. THE CLAMP WAS FORWARDED TO NTSB WASHINGTON, DC FOR FURTHER TESTING.

Other reports on N2024Q · 1

Matched to the same aircraft by N-number and date.