Cirrus SR22T N227RR

Summary

On 28 November 2014 at about 16:58 local time, a Cirrus SR22T registered N227RR, operated by Header Bug LLC, was involved in an accident near Hampton, South Carolina, United States. 4 people were on board and one was seriously injured, 3 had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

28 November 2014 at 16:58

Classification

Accident

Location

Hampton, South Carolina, United States

Nearest airport

Hampton-Varnville (3J0)

Coordinates

32.8606, -81.0617

Aircraft

Cirrus SR22T

Registration

N227RR

Category

Airplane

Year built

2014

Engines

1

Operator

Header Bug LLC

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Sarasota → Orangeburg

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

ERA15LA062

1 person was seriously injured.

The pilot’s improper decision to descend the airplane at an airspeed greater than the published best glide speed following an erroneous oil pressure indication, which resulted in an off-airport landing. Contributing to the erroneous oil pressure indication was the faulty oil pressure transducer. Contributing to the severity of the accident was the pilot’s late deployment of the ballistic parachute system.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The private pilot was conducting a personal cross-country flight with three passengers on board. The pilot reported that, during the preflight inspection, he checked the quantity of engine oil and verified that there was an adequate supply of engine oil on board. During cruise flight, about 9,000 ft mean sea level (msl), the oil pressure indication decreased to 0, which resulted in both audible and visual warnings. The engine power then reduced to idle, and the pilot's attempts to restore engine power by moving the throttle were not successful. The pilot subsequently diverted to a nearby airport about 7.5 nautical miles (nm) away. He stated that he descended the airplane slightly faster than the published best glide airspeed. When the airplane was at 800 ft msl and he realized it would not be able to land at the intended runway, he deployed the ballistic parachute. The airplane descended under the canopy, hit trees, descended to the ground, and then came to rest about 3/4 nm from the approach end of the intended runway. A postaccident examination and test run of the engine revealed no evidence of preimpact mechanical failures or malfunctions. Further, normal engine oil pressure was noted during the engine run; however, subsequent examination of the oil pressure transducer revealed that it was faulty and would have resulted in an erroneous oil pressure indication, as reported by the pilot. Further, although the pilot indicated that the engine lost power following the loss of oil pressure indication, which was supported by data downloaded from the onboard recording devices that showed decreased readings for fuel flow, exhaust gas temperature, and cylinder head temperature, the loss of engine power was consistent with the pilot's operation of the engine controls not with a mechanical malfunction or failure of the engine. Although the pilot reported that he descended the airplane slightly above the published best glide speed after first locating the alternate airport, the recorded data indicated that he descended at an indicated airspeed far greater than the published best glide speed for the majority of the descent. If the pilot had slowed to and maintained the published best glide speed either at the time of the first abnormal indication or after first locating the alternate airport, it is likely that the airplane would have been able to reach the intended runway and land successfully. Further, although the pilot reported that he deployed the parachute at 800 ft msl, it was actually deployed when the airplane was at 453 ft msl, or about 340 ft above ground level (agl), excluding the treetop heights. Although the successful deployment of the parachute has been demonstrated at less than 400 ft agl, the low-altitude deployment likely contributed to the severity of the accident by not allowing the parachute to fully deploy and adequately decelerate the airplane into an approximately level attitude.

Quoted verbatim from the NTSB record.