CEN09LA281

NTSB accident investigation · Cessna 551 · Stillwater, OK · May 5, 2009

Accident · No injuriesLimited investigationFinal report
Date
May 5, 2009, 14:49 local (19:49 UTC)
Place
Stillwater, OK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N740JBCessna 551
Defining event
Enroute-cruise: Loss of control in flight
Weather
Instrument (IMC) · Day
Status
Completed · report June 27, 2011
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration FSDO, Cessna Aircraft Company
FAA report
20090505008649A
Case key
73790

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot's loss of control for undetermined reasons.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Not determinedNot determined › Not determined · Unknown/Not determinedCessna 551: 1 caseAll aircraft: 2,247 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported that after leveling off at 16,000 feet with the autopilot engaged, he began to review his charts preparing for landing. When he went back to a visual scan of the instruments, he noted that the flight director was flagged off and that both the pilot and co-pilot attitude indicators were off. The pilot declared an emergency with air traffic control, reduced the throttles to idle, and pulled back on the controls. After the airplane came out of the bottom of the clouds and the pilot regained visual contact with the ground, the airplane was in a 60-degree left turn at approximately 80 knots of airspeed. After the pilot regained control, the flight director and all instruments began working again. The pilot then re-engaged the autopilot and continued to his destination, where he landed without further incident. Examination of the flight director system, gyros, and attitude indicators at the aircraft manufacturer’s facilities failed to identify a failure or malfunction with the flight instruments.

Factual narrative

On May 5, 2009 at 1449 central daylight time a Cessna Citation model 551, N740JB experienced temporary loss of control while in cruise flight at 16,000 feet. The airline transport pilot (ATP) and passenger were not injured. The airplane sustained substantial damage during the loss of control. The airplane and operated by Ballard Aviation, Incorporated under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Instrument flight rules (IFR) conditions prevailed, which operated on an IFR flight plan. The flight originated at Stillwater Regional Airport (SWO), Stillwater, Oklahoma, at 1430, with a destination of Wichita Mid-Continent Airport (ICT), Wichita, Kansas. In a written statement provided to the NTSB the pilot reported that after leveling at 16,000 feet with the autopilot engaged he began to review his charts preparing for landing at ICT. When he scanned the instruments, he noted the flight director was flagged off; and both the pilot and co-pilot attitude indicators were off. He declared an emergency with air traffic control (ATC), reduced the throttles to idle, and pulled back on the controls. The pilot added that as the airspeed approached 200 knots, he lowered the landing gear. When the airplane broke through the bottom of the clouds, the airplane was in a 60-degree left turn and approximately 80 knots of airspeed. The ATP managed to regained control of the airplane and level the airplane at approximately 6,100 feet. The flight director and all instruments began working again and he ATP re-engaged the autopilot and continued to ICT where he landed without further incident. The airplane was recovered to the Cessna aircraft company facilities in Wichita, Kansas for examination. Inspection of the airframe revealed that structural damage to the airplane’s fuselage and wings, during the recovery from the rapid decent. Flight instruments including the flight director system, gyros, and attitude indicators were removed and examined for evidence of failure or malfunction. No anomalies were found and the described failures could not be duplicated.

Aircraft

Registration
N740JB
Reported as
Cessna 551
Category
Airplane
Serial number
551-0359
Airframe hours
5,125
Engines
P&W Canada JT15D-4, turbo jetP&W Canada JT15D-4, 2,500 lbs thrust, turbo jet
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Ballard Aviation Inc, doing business as Personal Part 91 flight
Registered owner
Ballard Aviation Inc
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · April 29, 2009
Departed
KSWO · Stillwater, OK
Destination
KICT · Wichita, KS
Flight plan
IFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Weather

Conditions
Instrument (IMC) · Day
Wind
120° at 5 knots
Visibility
10 statute miles
Lowest ceiling
1,400 ft overcast
Temperature
63 °F, dew point 59 °F
Altimeter
29.87 inHg
Observed at
KSWO, 25 nm away

Docket · 14

The files NTSB released with the investigation on May 2, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 7.3 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.