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WPR11LA287 · Cessna 177RG

26 Jun 2011 · St Johns, AZ, United States

Cessna 177RG · Accident: loss of control in flight during initial climb

From St Johns Industrial Air Park (SJN) to Mesquite Metro Airport (HQZ)

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Event

NTSB case
WPR11LA287
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 177RG

Aircraft type
Cessna 177
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
N2725V
Operator
Unknown
Onboard fatalities
Unknown
Route
From St Johns Industrial Air Park (SJN), St Johns, AZTo Mesquite Metro Airport (HQZ), Mesquite, TX
Aircraft age
Not recorded
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
Initial climb
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
Loss of control in flight
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

  • Aircraft › Aircraft oper/perf/capability
  • Personnel issues › Task performance

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

NTSB narrative

The airplane arrived at the airport after a 3-hour flight. The pilot serviced the airplane to capacity with fuel and departed about 1 hour later. Turbulent crosswind and high density altitude conditions (9,369 feet) existed at the time of departure. A witness saw the airplane taxi along the 3,400-foot-long departure runway for about 1/3 of its length before beginning to accelerate. The passengers reported that, compared to previous flights, the airplane accelerated slower and took off farther down the runway, as would be expected due to the high density altitude. The pilot reported that the takeoff progressed normally until the airplane reached an altitude of about 200 feet above ground level. At that point, the airplane would no longer climb, and, certain that they would not be able to return to the airport, the pilot attempted to maneuver the airplane for landing in the field ahead. The passengers reported that, once airborne, the airplane rocked from side-to-side, and the stall warning horn operated continuously. The witness observed the airplane in an unusually nose-high attitude throughout the flight until it suddenly descended out of her view. The airplane impacted the ground in a flat attitude, sustaining crush damage in the vertical plane. Although the horizontal stabilizer sustained tree-strike damage, the wings did not; this damage pattern was consistent with the nose-high attitude observed by the witness. The airplane was loaded within its center of gravity envelope and was about 125 pounds below maximum gross weight. No evidence of preimpact mechanical malfunction or failure was noted during the postaccident examination of the airframe and engine. Review of recorded engine monitor data revealed that an appropriate level of power was being produced, and all engine parameters were normal. Although the mixture control was found in the full rich position, the pilot recalled that he leaned the mixture during taxi, and the power output determined from the engine monitor data was consistent with an appropriately leaned mixture. The pilot did not recall the extended runway taxi reported by the witness, however, performance calculations indicated that the remaining runway length would still have allowed for takeoff and adequate terrain clearance.

Probable cause

The pilot did not attain and maintain an adequate airspeed during the takeoff initial climb, which resulted in an aerodynamic stall.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR11LA287
Event ID
20110627X41846
Case number
WPR11LA287
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: 90e112483c6702e6cac08d7470a4e4fa8981f33190ad369f2569ff10e0c003e2; retrieved 2026-09-15T16:21:22.711Z.