WPR24LA125

NTSB accident investigation · Cessna 195B · Portales, NM · April 8, 2024

Accident · Minor injuriesClass 3 · LimitedFinal report
Date
April 8, 2024, 16:15 local (22:15 UTC)
Place
Portales, NM
Injuries
1 minor, 2 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N2147CCessna 195B
Defining event
Takeoff: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report November 13, 2025
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Western Pacific Region
Parties
FAA FSDO
FAA report
20240408007729A
Case key
194089

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

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Probable cause

The pilot’s decision to take off with a quartering tailwind and his subsequent failure to maintain directional control. Contributing to the accident was the pilot’s improper elevator control inputs during takeoff.

Findings · 5

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.

Wind: crosswindEnvironmental issues › Conditions/weather/phenomena · Response/compensationCessna 195B: 3 casesAll aircraft: 1,008 casesProbable cause
Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedCessna 195B: 13 casesAll aircraft: 3,958 casesProbable cause
Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Decision related to conditionCessna 195B: 1 caseAll aircraft: 594 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotCessna 195B: 8 casesAll aircraft: 9,295 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 during takeoff there was a left crosswind and he applied controls to counter the crosswind; the takeoff roll was normal, and the airplane remained on the runway centerline until just before it became airborne. He said the airplane then veered to the right and exited the right side of the runway, where he moved the throttle to idle and applied maximum braking. Witnesses observed the airplane taxiing to takeoff and noted there would be a left quartering tailwind during takeoff. They videoed the takeoff, and the recording showed the airplane accelerating on the runway with the elevator near the full trailing-edge-up position, forcing the tail onto the runway during the takeoff roll. The video also captured the windsock by the runway, indicating the quartering tailwind. The video showed the airplane became airborne in a somewhat nose-high attitude and it climbed about 5 ft above the ground to the right of the runway when the pilot brought the throttle to idle. The airplane subsequently descended, resulting in a hard landing beside the runway. The landing gear collapsed, and the right wing struck the ground, resulting in substantial damage. The Airplane Flying Handbook, Transition to Tailwheel Airplanes, states “as the airplane accelerates, the pilot smoothly decreases the pitch attitude and adjusts aileron and rudder control pressures to maintain the appropriate crosswind correction. If the pitch attitude remains excessively steep or if it is too flat, crosswind control during the ground roll becomes more difficult.” It also states that although tailwheel airplanes can be lifted off in a three-point attitude, this technique results in an unusually high pitch attitude and an angle of attack excessively close to stall. The pilot’s decision to maintain the tailwheel on the runway throughout the takeoff roll likely made directional control more difficult with the quartering tailwind.

Factual narrative

On April 8, 2024, about 1615 mountain daylight time, a Cessna 195B, N2147C, was substantially damaged when it was involved in an accident near Portales, New Mexico. The pilot and two passengers received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, he had landed at Portales Municipal Airport (PRZ), Portales, New Mexico, to refuel during a cross-country flight. After refueling, he proceeded to take off on runway 19 with controls applied to counter the left crosswind. He reported that the takeoff roll was normal, and the airplane remained on the runway centerline. He stated that just before the airplane becoming airborne, it veered to the right. When the airplane exited the right side of the runway he brought the throttle to idle and applied maximum braking. A pilot-rated witness observed the pilot refuel the airplane and believed the pilot topped off the fuel. He also stated there was “a lot” of baggage in the airplane, making the airplane heavy with the 3 occupants. He and another witness observed the airplane taxi to the departure runway and observed most of the takeoff and the accident. The pilot-rated witness stated the windsock indicated there was a quartering tailwind gusting to about 20 knots, and he and another witness commented to each other that the pilot should not takeoff from [rwy 19] because of the tailwind. The pilot-rated witness stated the elevator was “pinned full aft” in the full trailing edge up position during the takeoff The second witness captured most of the airplane’s takeoff roll and the accident on video. The video matches the witnesses’ recollection of events. The airplane can be seen accelerating, and the engine can be heard operating at a high power setting for about 9 seconds before the airplane goes out of sight behind large fuel tanks located between the witnesses and the runway. The elevator position can be seen in the trailing edge up position as the airplane goes out of sight behind the fuel tanks. The engine can be heard until the airplane reappears from behind the fuel tanks about 3 seconds later. When the airplane reappears, it is in a wings-level, nose-high attitude about 5 ft above the ground. The engine rpm can be heard rapidly decreasing as the airplane comes into view and descended. The left wing dropped momentarily before the airplane's wings leveled. The airplane then made a hard landing off the right side of the runway. The airplane bounced once and then nosed over into the ground before stopping upright. The right main landing gear collapsed and the right wing struck the ground, resulting in substantial damage. An FAA inspector noted the airplane’s ailerons did not move together during an on-scene examination of the airplane. After the airplane was lifted off the ground, wreckage recovery personnel verified flight control continuity and proper flight control movement before disassembling the airplane for transportto a repair facility. Personnel at the repair facility also examined the disassembled airplane and found no anomalies with the flight control system. According to the automated weather report, the wind was from 120° at 12 knots. The windsock, as seen in the witness video, corresponded to the witnessed left quartering tailwind. The Airplane Flying Handbook (Chapter 14: Transition to Tailwheel Airplanes Takeoff) states the following: LIFTOFF “When the appropriate pitch attitude is maintained throughout the takeoff roll, liftoff occurs when the AOA and airspeed combine to produce the necessary lift without any additional “rotation” input. The ideal takeoff attitude requires only minimum pitch adjustments shortly after the airplane lifts off to attain the desired climb speed. All modern tailwheel aircraft can be lifted off in the three-point attitude. That is, the AOA with all three wheels on the ground does not exceed the critical AOA, and the wings will not be stalled. While instructive, this technique results in an unusually high pitch attitude and an AOA excessively close to stall, both inadvisable circumstances when flying only inches from the ground.” CROSSWIND “It is important to establish and maintain proper crosswind corrections prior to liftoff; that is, application of aileron deflection into the wind to keep the upwind wing from rising and rudder deflection as needed to prevent weathervaning. Takeoffs made into strong crosswinds are the reason for maintaining a positive AOA (tail-low attitude) while accelerating on the runway. Because the wings are making lift during the takeoff roll, a strong upwind aileron deflection can bank the airplane into the wind and provide positive crosswind correction soon after the takeoff roll begins. The remainder of the takeoff roll is then made on the upwind main wheel while the pilot uses rudder to maintain the alignment of the longitudinal axis with the runway. As the airplane accelerates, the pilot smoothly decreases the pitch attitude and adjusts aileron and rudder control pressures to maintain the appropriate crosswind correction. If the pitch attitude remains excessively steep or if it is too flat, crosswind control during the ground roll becomes more difficult. As the aircraft leaves the runway, the wings can be leveled as appropriate drift correction (crab) is established.”

Aircraft

Registration
N2147C
Reported as
Cessna 195B
Category
Airplane
Serial number
16132
Built
1954
Airframe hours
3,688
Engine
Jacobs R755B2, 275 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 22, 2024 · 11.4 hours before
Destination
CEZ · Cortez, CO
Flight plan
IFR
Airport
PRZ · Portales Muni, runway 01/19, 5,700 × 60 ft, asphalt
Equipment
Electronic flight bag or handheld device, Electronic multifunction display, Electronic primary flight display, Onboard weather, Stall warning system, Angle of attack indicator, Auto-pilot, ADS-B

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
69
Injuries
Minor
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
November 29, 2023
Seat
Left
Restraint
Lap only
Flight hours
16,674 total · 116.1 in this make and model · 12,362 as pilot in command · 11.4 in the last 90 days · 11.4 in the last 30 days · 3.5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 12 knots, gusting 20
Visibility
10 statute miles
Lowest ceiling
21,000 ft broken
Temperature
66 °F, dew point 19 °F
Altimeter
29.85 inHg
Observed at
KCVS, 15 nm away
METAR
KCVS 082155Z COR AUTO 09012G20KT 10SM SCT160 BKN210 19/M07 A2985 RMK AO2 SLP076 T01911073 $ COR 2200

Docket · 5

The files NTSB released with the investigation on November 14, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 9.6 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.