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WPR17CA001 · Cessna R172K K

2 Oct 2016 · Rosamond, CA, United States

Cessna R172K K · Accident: flight control system malfunction/failure during takeoff

From Rosamond Skypark Airport (L00) to Camarillo International Airport (CMA)

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Event

NTSB case
WPR17CA001
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Cessna R172K K

Aircraft type
Cessna 172
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N736LZ
Operator
Unknown
Onboard fatalities
Unknown
Route
From Rosamond Skypark Airport (L00), Rosamond, CATo Camarillo International Airport (CMA), Camarillo, CA
Aircraft age
About 39 years (built 1977)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Takeoff
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Flight control system malfunction/failure
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Personnel issues › Action/decision
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The pilot/owner and three non-pilot acquaintances decided to use the airplane to fly to another airport for lunch. The pilot had owned and operated the airplane about 10 years, and reported a total time of about 550 hours in that make and model. His normal procedures included hangaring the airplane, and using a yoke-mounted iPad "mini" for in-flight information. The outbound flight was uneventful. After landing, the pilot installed the flight control lock in the pilot-side yoke shaft. After lunch, the four persons returned to the airplane for the return trip. The pilot reported that the preflight inspection and taxi out to the run-up area were normal, but during the before-takeoff check process there, he noticed that the two fuel tank gauges indicated different quantities from one another, which was unusual for the high wing airplane. The pilot decided to interrupt the before-takeoff check process, shut down the engine, and physically "stick" the tanks to accurately determine the total fuel quantity. After the pilot measured the fuel quantities, which he determined were satisfactory, he re-boarded the airplane, re-started the engine, and taxied from the run-up area onto the runway for departure. The airplane lifted off about half-way down the 3,600 foot runway, but when it was at an altitude of about 20 feet above the ground, it stopped climbing. The pilot "immediately recognized something was wrong," aborted the departure, and the airplane landed on the remaining runway. The pilot was unable to stop the airplane on the runway, and it sustained substantial damage to the fuselage as a result. None of the occupants were injured. After the accident, the pilot determined that he had left the control lock in for the takeoff. The pilot reported that he normally used the airplane manufacturer's checklists on all his flights, including this one, but the evidence in this event contradicts that account. The manufacturer's checklists explicitly specified that the flight controls be checked for freedom of travel during two separate pre-departure phases; the walk-around preflight inspection, and the before-takeoff operational checks. For undetermined reasons, the pilot omitted those items from both of those phases, and deprived himself of two opportunities to detect the presence of the control lock. Investigation revealed that the manufacturer-issued control lock had been installed backwards by the pilot, which prevented it from accomplishing one of its primary design functions, that of inhibiting pilot access to the ignition switch. Further investigation revealed that the pilot rarely used the control lock due to the fact that he hangared his airplane, and that he was unaware that he had installed it backwards. The yoke-mounted iPad limited the pilot's view of the installed control lock, which reduced the potential for visual detection. The pilot reported that the winds were "light," which reduced the likelihood of the need for flight control inputs on the ground during taxi, and thus deprived the pilot of another opportunity for detection of the locked controls. Finally, after his impromptu physical check of the fuel quantity, the pilot did not re-commence the interrupted before-takeoff checklist from the beginning, and thus missed another opportunity to detect the locked flight controls.

Probable cause

The pilot's improper use of the control lock, combined with his incomplete execution of two pre-departure procedures, which resulted in a takeoff with the control lock installed.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR17CA001
Event ID
20161003X35157
Case number
WPR17CA001
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: f1ad98b379e52de9c77c75407eaa7a72ce05daaab6a372422d57a624bef70d0b; retrieved 2026-09-16T04:20:34.004Z.