ERA13LA288

NTSB accident investigation · Hagerty RV-7A · Altoona, PA · June 15, 2013

Accident · Serious injuriesLimited investigationFinal report
Date
June 15, 2013, 13:13 local (17:13 UTC)
Place
Altoona, PA
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N954CHHagerty RV-7A
Defining event
Landing-flare/touchdown: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report July 30, 2014
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO, NTSB
FAA report
20130615013809A
Case key
87228

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 pilot's improper recovery from an encounter with a wind gust during landing, which resulted in a hard landing on, and displacement of, the nose landing gear and a subsequent runway excursion and noseover.

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.

Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedHagerty Charles J RV-7A: 1 caseAll aircraft: 1,269 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 the airplane maintained 80 mph on final approach and slowed to 70 mph at touchdown. Upon touchdown on the main landing gear, the pilot reported that a wind gust occurred, and the airplane subsequently climbed and then landed hard on the nose landing gear, which bent under. The airplane then rolled off the runway onto grass and nosed over. The pilot reported no preimpact failure or malfunction that would have precluded normal operation. Both occupants reported having their lapbelts "snug" but not as tight as they could have been. Postaccident examination revealed that the nose landing gear was displaced and that a person's head with a similar sitting height as both occupants would have been about 1 inch below a crush line between the vertical stabilizer and the engine cowling. When the airplane inverted, both occupants struck their heads and sustained neck injuries that likely resulted from proximity of their heads to the canopy and might have been exacerbated by any slack in their restraints. Although postaccident measurements of the restraints confirm the occupants' statements that they were less than tight, anthropomorphic data for both occupants was not obtained, therefore; the amount of slack in either seat restraint was not conclusively determined.

Factual narrative

On June 15, 2013, about 1313 eastern daylight time, an amateur built Hagerty RV-7A, N954CH, registered to and operated by a private individual, nosed over during landing at Altoona-Blair County Airport (AOO), Altoona, Pennsylvania. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 Code of Federal Regulations (CFR) Part 91 personal flight from Falwell Airport (W24), Lynchburg, Virginia, to AOO. The airplane sustained substantial damage and the private pilot and one passenger sustained serious injuries. The flight originated from W24 about 1150.The pilot stated that he announced his position on the common traffic advisory frequency when he was 10 miles from the destination airport and heard the pilot of an airplane announce the flight was departing runway 30. He asked the pilot of that airplane what runway the winds favored and continued his straight-in approach to runway 03. On final for the runway, with a mountain range on the right and the wind from the right, he encountered turbulence. As the flight descended closer he noticed the windsock and it showed a 7 to 10 knot wind and was extended ½ way out with some gusts. He maintained 80 mph on final slowing to 70 mph at touchdown. On touchdown on the main landing gear a wind gust occurred and the airplane climbed, and then came down hard on the nose landing gear which bent under. The airplane rolled a good distance, riding on metal, and he thought about fire. The airplane started pulling to the left, and he reached over and pulled the mixture control and may have also turned off the electric thinking if he was off the runway and on grass there would be no sparks. The airplane went off the runway onto grass, and the nose landing gear dug in and the airplane nosed over. While hanging upside down he undid his 4-point restraint and an individual from the airport helped pull the canopy out of the way. He was able to crawl through a hole in the canopy and reached in and released his wife's 4-point restraint. She was able to get on her back, and he helped her out. By that time, the first responders arrived. The pilot further stated that his restraint was "snug", but it could have been tighter meaning it was not as snug as it could have been, while the passenger (his wife) reported her restraint was not loose but not too tight. His sitting height is 34.5 inches and his wife's sitting height is 35 inches. He also stated there was no mechanical failure or malfunction that caused the accident. A witness who is the pilot's brother reported the touchdown appeared smooth with no wobble or sway, but the airplane became airborne then, "came down very quickly" and veered to the left side of the runway. He reported seeing the nose-over and ran inside the terminal building where he called 911. Inspection of the airplane following recovery by the FAA-IIC revealed the nose landing gear tire pressure was 37 psi, while the left and right main landing gear tire pressures were47 psi each. The FAA-IIC also reported no apparent damage to the roll structure or seat restraints. The airplane was recovered for further examination. Examination of the airplane following recovery was performed by several NTSB personnel. The inspection determined that a person with a sitting height ½ inch more than the pilot and the same as the passenger would have about 1 inch of clearance between the top of the subjects head and a line extending between the top of the vertical stabilizer to the engine cowling. The on-board GPS receiver was retained for read-out. Read-out of the GPS receiver was performed by the NTSB Vehicle Recorder Division located in Washington, DC. The results of the read-out indicate that the entire accident flight was recorded. With respect to the final approach, at 1313:19, the airplane was about 474 feet past runway 03 threshold at 70 knots groundspeed. The successive GPS recorded data indicates that the while continuing over the runway the altitude increased slightly (agreed with pilot statement) while the groundspeed decreased to the lowest value (40 knots), then the altitude decreased and the groundspeed decreased to 11 knots with the location on the grass to the left side of the runway. According to the current president of the designer of the airplane, the roll structure for airplanes with slider or tip-up type canopies is considered dual purpose in that it was designed to provide a support structure for the plexi-glass canopy and also to provide a degree of protection in the event of a nose-over. The president also reported that both structures were designed for the RV-6 and RV-6A airplanes in the '80's and have changed very little for the RV-7, RV-7A, RV-9 and RV-9A airplanes. The original designer did not recall doing any testing on either design, but both have proven to have very good track records in the field. An aviation surface observation report taken at the accident airport at 1253, or approximately 20 minutes before the accident indicates in part that the wind was from 330 degrees at 8 knots; no gusts were reported.

Aircraft

Registration
N954CH
Reported as
Hagerty RV-7A
Category
Airplane, amateur-built
Serial number
71991
Built
2012
Airframe hours
50
Engine
Superior IO-360-A1LD2, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Charles J. Hagerty
Registered owner
Charles J. Hagerty
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · March 16, 2013
Departed
W24 · Lynchburg, VA
Destination
AOO · Altoona, PA
Airport
AOO · Altoona-Blair County Airport, runway 03, 5,645 × 100 ft, asphalt
Equipment
Handheld GPS

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
56
Injuries
Serious
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
December 18, 2012
Seat
Left
Restraint
4-point
Flight hours
137 total · 46 in this make and model · 25 in the last 90 days · 9 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
330° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 45 °F
Altimeter
30.09 inHg
Observed at
AOO

Docket · 8

The files NTSB released with the investigation on May 30, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 9.2 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.