- Date
- July 4, 2015, 11:15 local (16:15 UTC)
- Place
- Newton, KS
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Approach
- Aircraft
- N7985PPiper PA 24-250
- Defining event
- Approach-VFR pattern final: Sys/Comp malf/fail (non-power)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report September 11, 2015
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- Wichita FSDO (FAA)
- FAA report
- 20150704010039A
- Case key
- 91552
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 the right main landing gear down-lock micro switch, which resulted in a landing gear collapse during landing, and the pilot/owner's unfamiliarity with the emergency landing gear extension procedure. Contributing to the accident was the flight instructor's lack of experience in this make and model airplane and unfamiliarity with the emergency landing gear extension procedure.
Findings · 3
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
During a local instructional flight, the flight instructor reported that while on final approach at their destination airport, the landing gear did not illuminate down and locked. He reported that he tried to cycle the gear with the electric landing gear handle, but the down and locked green light would not illuminate. When the power was reduced to idle, the flight instructor reported that the audible gear unsafe horn sounded as well. The flight instructor performed a go-around, and the pilot receiving instruction reported that he began the manual gear extension checklist according to the "SureCheck" checklist. During the manual gear extension procedure, both pilots reported that a "spring tension" prevented the emergency gear handle from extending to the full forward position. Subsequently, the flight instructor reported that he reset the motor release arm and attempted to extend the landing gear again with the electric gear handle, but the landing gear electric motor circuit breaker popped and the motor release arm jammed. After receiving confirmation from ground personnel that the landing gear was only partially extended, the flight instructor performed an emergency landing. During touchdown, the landing gear collapsed and the airplane skidded to a stop on the runway. The fuselage was substantially damaged in the accident. During a postaccident examination, a Federal Aviation Administration aviation safety inspector found that the right main landing gear down-lock micro switch was operating intermittently within the electrical actuating system. According to the inspector, an intermittent micro switch on this landing gear can result in gear unsafe warnings and continuous electrical motor operation. Additionally, the SureCheck checklist used did not include instructions provided in the Pilot's Operating Handbook stating, "Do not re-engage landing gear operating motor in flight." The SureCheck checklist does contain a warning stating "this product is not a substitute for any operation manual which coincides with each specific aircraft." The flight instructor reported that he had two hours of flight time in this make and model airplane, and the pilot receiving instruction reported that he had no previous experience in this make and model airplane.
Factual narrative
During a local instructional flight, the flight instructor reported that while on final approach at their destination airport, the landing gear did not illuminate down and locked. He reported that he tried to cycle the gear with the electric landing gear handle, but the down and locked green light would not illuminate. When the power was reduced to idle, the flight instructor reported that the audible gear unsafe horn sounded as well. The flight instructor performed a go-around, and the pilot receiving instruction reported that he began the manual gear extension checklist according to the "SureCheck" checklist. During the manual gear extension procedure, both pilots reported that a "spring tension" prevented the emergency gear handle from extending to the full forward position. Subsequently, the flight instructor reported that he reset the motor release arm and attempted to extend the landing gear again with the electric gear handle, but the landing gear electric motor circuit breaker popped and the motor release arm jammed. After receiving confirmation from ground personnel that the landing gear was only partially extended, the flight instructor performed an emergency landing. During touchdown, the landing gear collapsed and the airplane skidded to a stop on the runway. The fuselage was substantially damaged in the accident. During a postaccident examination, a Federal Aviation Administration aviation safety inspector found that the right main landing gear down-lock micro switch was operating intermittently within the electrical actuating system. According to the inspector, an intermittent micro switch on this landing gear can result in gear unsafe warnings and continuous electrical motor operation. Additionally, the SureCheck checklist used did not include instructions provided in the Pilot's Operating Handbook stating, "Do not re-engage landing gear operating motor in flight." The SureCheck checklist does contain a warning stating "this product is not a substitute for any operation manual which coincides with each specific aircraft." The flight instructor reported that he had two hours of flight time in this make and model airplane, and the pilot receiving instruction reported that he had no previous experience in this make and model airplane.
Aircraft
- Registration
- N7985P
- Reported as
- Piper PA 24-250 (250)
- Category
- Airplane
- Serial number
- 24-3223
- Built
- 1962
- Airframe hours
- 4,443
- Engine
- Lycoming O-540 SERIES, 250 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · June 30, 2014
- Departed
- 3AU · Augusta, KS
- Destination
- EWK · Newton, KS
- Airport
- EWK · Newton-City-County, runway 17, 7,003 × 100 ft, asphalt
- Equipment
- Stall warning system
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 · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Flight instructor
- Age
- 59
- Injuries
- None
- Certificates
- Commercial, Flight instructor, Airline transport
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Last flight review
- April 25, 2015
- Seat
- Right
- Restraint
- Lap only
- Flight hours
- 4,800 total · 2 in this make and model · 4,150 as pilot in command · 9 in the last 90 days · 6 in the last 30 days · 1 in the last 24 hours
- Role
- Pilot
- Age
- 57
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, With waivers/limitations
- Last flight review
- June 10, 2010
- Seat
- Left
- Restraint
- Lap only
- Flight hours
- 170 total · 0 in this make and model · 100 as pilot in command
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 150° at 6 knots
- Visibility
- 10 statute miles
- Temperature
- 79 °F, dew point 63 °F
- Altimeter
- 30.04 inHg
- Observed at
- KEWK
Docket · 6
The files NTSB released with the investigation on September 8, 2015, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.0 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.
Other investigations on N7985P · 2
Matched to the same aircraft by N-number and date.