GAA16CA074

NTSB accident investigation · Cessna 177 · Palm Springs, CA · November 14, 2015

Accident · No injuriesData collectionFinal report
Date
November 14, 2015, 09:30 local (17:30 UTC)
Place
Palm Springs, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N2112QCessna 177
Defining event
Landing: Sys/Comp malf/fail (non-power)
Weather
Visual (VMC) · Day
Status
Completed · report March 14, 2016
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
Riverside FSDO (FAA)
FAA report
20151114019279A
Case key
92424

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 failure of a shaft seal at the nose gear retraction/extension actuator, which resulted in a loss of hydraulic fluid and a main landing gear collapse during landing.

Findings · 2

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The pilot reported that during the takeoff initial climb, after the landing gear was retracted, the landing gear's hydraulic pump electric motor continued to run, even though the landing gear appeared to be fully retracted, as viewed in the landing gear mirror. The pilot then attempted to extend the landing gear normally, but the landing gear would not indicate down and locked. Subsequently, for over an hour, the pilot attempted to manually extend the landing gear, using the emergency manual gear extension hand pump, but he could see in the mirror that the landing gear was only partially extended. During the subsequent emergency landing, the main landing gear collapsed and the airplane skidded to a stop on the runway. The right stabilator sustained substantial damage. A postaccident examination revealed that the landing gear system was empty of hydraulic fluid. After the system was serviced with hydraulic fluid and operated, a leak was found at the nose gear actuator due to the failure of a shaft seal. The tests revealed that the landing gear extension process could not be completed, and the manual landing gear pump did not have sufficient fluid remaining to extend all three landing gear. The airplane logbooks revealed no records of service to the nose gear actuator and shaft seal and each were the original manufactured parts.

Factual narrative

The pilot reported that during the takeoff initial climb, after the landing gear was retracted, the landing gear's hydraulic pump electric motor continued to run, even though the landing gear appeared to be fully retracted, as viewed in the landing gear mirror. The pilot then attempted to extend the landing gear normally, but the landing gear would not indicate down and locked. Subsequently, for over an hour, the pilot attempted to manually extend the landing gear, using the emergency manual gear extension hand pump, but he could see in the mirror that the landing gear was only partially extended. During the subsequent emergency landing, the main landing gear collapsed and the airplane skidded to a stop on the runway. The right stabilator sustained substantial damage. A postaccident examination revealed that the landing gear system was empty of hydraulic fluid. After the system was serviced with hydraulic fluid and operated, a leak was found at the nose gear actuator due to the failure of a shaft seal. The tests revealed that the landing gear extension process could not be completed, and the manual landing gear pump did not have sufficient fluid remaining to extend all three landing gear. The airplane logbooks revealed no records of service to the nose gear actuator and shaft seal and each were the original manufactured parts.

Aircraft

Registration
N2112Q
Reported as
Cessna 177 (RG)
Category
Airplane
Serial number
177RG0512
Built
1974
Airframe hours
3,289
Engine
Lycoming IO-360-A1B6D, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · October 17, 2015
Departed
UDD · Palm Springs, CA
Destination
HMT · Hemet, CA
Airport
PSP · Palm Springs Intl, runway 31R, 4,952 × 75 ft, asphalt
Equipment
Onboard weather, Stall warning system, Electronic primary flight display, ADS-B, Auto-pilot, 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
70
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
September 22, 2015
Seat
Left
Restraint
3-point
Flight hours
3,596 total · 603 in this make and model · 3,132 as pilot in command · 13 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 21 °F
Altimeter
30.00 inHg
Observed at
KPSP

Docket · 3

The files NTSB released with the investigation on March 7, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.4 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.