- Date
- October 27, 2017, 17:50 local (21:50 UTC)
- Place
- Tallahassee, FL
- Injuries
- 3 uninjured
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N211WSmith Aerostar 600A
- Defining event
- Initial climb: Loss of control in flight
- Weather
- Visual (VMC) · Day
- Status
- Completed · report February 21, 2018
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA/ FSDO
- FAA report
- 20171027021289A
- Case key
- 96277
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 incorrect pitch control and premature landing gear retraction during the initial climb.
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.
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 of the multiengine, retractable-landing-gear airplane reported that, during the initial climb, he "noted 105 IAS [indicated airspeed] as normal and reached down to retract the gear." He added that he "glanced down" to make sure he had grabbed the landing gear selector, and when he looked back outside, the airplane was "near the runway." He further added that he "pulled back hard on the yoke," but the propellers struck the runway, and the airplane then settled on the runway and skidded into the grass to the left. The pilot reported in the National Transportation Safety Board Form 6120.1 Pilot/Operator Aircraft Accident/Incident Report Safety Recommendation section that the airplane was "not high enough above [the] ground to raise the gear," and he may have "relaxed back-pressure on the yoke after rotation," and when leaning slightly forward for the gear handle, the yoke may had been pushed forward slightly. The airplane sustained substantial damage to the fuselage. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The Federal Aviation Administration's Airplane Flying Handbook stated, in part: Avoid premature landing gear retraction and do not retract the landing gear until a positive rate of climb is indicated on the flight instruments. If the airplane has not attained a positive rate of climb, there is always the chance it may settle back onto the runway with the gear retracted. This is especially so in cases of premature lift-off. Remember that leaning forward to reach the landing gear selector may result in inadvertent forward pressure on the yoke, which causes the airplane to descend.
Factual narrative
The pilot of the multi-engine, retractable landing gear airplane reported that, during the initial climb, he "noted 105 IAS [indicated airspeed] as normal and reached down to retract the gear." He added that he "glanced down" to make sure he had grabbed the landing gear selector, and when he looked back outside, the airplane was "near the runway." He further added that he "pulled back hard on the yoke," but the propellers struck the runway, the airplane settled on the runway, and skidded into the grass to the left. The pilot reported additional factors related to the accident on the National Transportation Safety Board Form 6120.1 Pilot/Operator Aircraft Accident/Incident Report Safety Recommendation section. He added that the airplane was "not high enough above [the] ground to raise the gear," and he may have "relaxed back-pressure on the yoke after rotation," and when leaning slightly forward for the gear handle, the yoke may had been pushed forward slightly. The airplane sustained substantial damage to the fuselage. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The Federal Aviation Administration's Airplane Flying Handbook stated in part: Avoid premature landing gear retraction and do not retract the landing gear until a positive rate of climb is indicated on the flight instruments. If the airplane has not attained a positive rate of climb, there is always the chance it may settle back onto the runway with the gear retracted. This is especially so in cases of premature lift-off. Remember that leaning forward to reach the landing gear selector may result in inadvertent forward pressure on the yoke, which causes the airplane to descend.
Aircraft
- Registration
- N211W
- Reported as
- Smith Aerostar 600A (600)
- Category
- Airplane
- Serial number
- 60-0460-153
- Built
- 1977
- Airframe hours
- 5,931.5
- Engines
- Lycoming IO-540-K1J5, 300 horsepower, reciprocatingLycoming IO-540-K1J5, 300 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · August 11, 2017
- Departed
- TLH · Tallahassee, FL
- Destination
- 06A · Tuskegee, AL
- Flight plan
- IFR
- Airport
- TLH · Tallahassee Intl, runway 09, 8,000 × 150 ft, asphalt
- Equipment
- Auto-pilot, Angle of attack indicator, Stall warning system, Onboard weather, Handheld GPS, Electronic primary flight display, Electronic multifunction display, Electronic flight bag or handheld device
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.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 57
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 3, With waivers/limitations
- Last flight review
- October 27, 2016
- Seat
- Left
- Restraint
- 3-point
- Flight hours
- 1,955 total · 204 in this make and model · 1,947 as pilot in command · 42 in the last 90 days · 14 in the last 30 days · 1 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 180° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- 25,000 ft broken
- Temperature
- 72 °F, dew point 50 °F
- Altimeter
- 30.00 inHg
- Observed at
- KTLH
Docket · 3
The files NTSB released with the investigation on January 25, 2018, on NTSB’s docket system: statements, records, photos and specialists’ reports. 8.8 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.