Full copy of the NTSB Reno crash report

gunnergirl81

Sergeant
Full Member
Minuteman
Apr 2, 2008
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KCMO
Got a copy of the original prelim NTSB report. Its a PDF and I don't know how to post it here. If you want the original let me know and I'll email it to you. The cut and paste is hard to read. Anyone know how to post the PDF?

National Transportation Safety Board
PRELIMINARY REPORT
AVIATION
NTSB ID:
Occurrence Date:
Occurrence Type:
PRELIMINARY INFORMATION - SUBJECT TO CHANGE Page 1
Location/Time
Most Critical Injury:
Investigated By:
This space for binding
Nearest City/Place
Aircraft Information
Registration Number
State Zip Code
Aircraft Manufacturer
Local Time Time Zone
Model/Series Number
Serious Minor None
Amateur Built Aircraft?
Air Medical Transport Flight:
Fatal
Type of Aircraft:
Injury Summary:
Revenue Sightseeing Flight:
Narrative
Brief narrative statement of facts, conditions and circumstances pertinent to the accident/incident:
Printed on : 10/6/2011 9:17:47 PM
Airplane No
11 66
On September 16, 2011, about 1626 Pacific daylight time, an experimental North America P-51D,
N79111, impacted terrain following a loss of control while maneuvering at Reno Stead Airport, Reno,
Nevada. The airplane was registered to Aero-Trans Corp, Ocala, Florida, and operated by the pilot
as Race 177 under the provisions of 14 Code of Federal Regulations Part 91. The commercial pilot
sustained fatal injuries; the airplane sustained substantial damage. Casualties on the ground
included 10 fatalities and 74 injured. As of the time of this preliminary report, eight of the
injured remain hospitalized, some in critical condition. Visual meteorological conditions prevailed
at the time of the accident, and no flight plan had been filed for the local air race flight, which
departed from Reno Stead Airport about 10 minutes before the accident.
The airplane was participating in the Reno National Championship Air Races in the last event of the
day. The airplane had completed several laps and was in a steep left turn towards the home pylon
when, according to photographic evidence, the airplane suddenly banked momentarily to the left
before banking to the right, turning away from the race course, and pitching to a steep nose-high
attitude. Witnesses reported and photographic evidence indicates that a piece of the airframe
separated during these maneuvers. After roll and pitch variations, the airplane descended in an
extremely nose-low attitude and collided with the ground in the box seat area near the center of
the grandstand seating area.
Investigators from the National Transportation Safety Board (NTSB) and the Federal Aviation
Administration examined the wreckage on site. They documented the debris field and identified
various components of the airplane’s control system and control surfaces. The wreckage was removed
to a secure storage facility for detailed examination at a later date.
The airplane’s ground crew noted that the airplane had a telemetry system that broadcast data to a
ground station as well as recorded it to a box on board the airplane. The crew provided the ground
station telemetry data, which includes engine parameters and global positioning satellite system
data to the NTSB for analysis. The onboard data box, which sustained crush damage, was sent to the
NTSB’s Vehicle Recorder laboratory for examination. Investigators recovered pieces of a camera
housing and multiple detached memory cards from the airplane’s onboard camera that were in the
debris field. The memory cards and numerous still and video image recordings were also sent to the
Vehicle Recorders laboratory for evaluation.
The Federal Aviation Administration and the Reno Air Race Association are parties to the
investigation.
Updated on Sep 23 2011 11:18AM
No No
N79111 NORTH AMERICAN/AERO CLASSICS P-51D
NTSB
Fatal
Reno NV 89506 1626 PDT
Accident
09/16/2011
WPR11MA454
This space for binding
National Transportation Safety Board
PRELIMINARY REPORT
AVIATION
NTSB ID:
Occurrence Date:
Occurrence Type:
Registration Number Aircraft Manufacturer Model/Series Number
Other Aircraft Involved
Accident Information
Aircraft Damage: Accident Occurred During:
Crew Name Certificate No. Injury
Pilot
2
3
4
5
6
Operator Information
Name
Street Address
Operator Designator Code
City
Doing Business As
State Zip Code
Observation Time (Local):
Altimeter: "Hg
Page 2
-Type of Certificate(s) Held:
Air Carrier Operating Certificate(s):
Operating Certificate:
Regulation Flight Conducted Under:
Type of Flight Operations Conducted:
Operator Certificate:
Flight Plan/Itinerary
Type of Flight Plan Filed:
Last Departure Point
Destination
State Airport Identifier
State Airport Identifier
Weather Information
Investigator's Source:
Sky/Lowest Cloud Condition:
Facility ID:
Ft. AGL Visibility:
Ft. AGL
SM
PRELIMINARY INFORMATION - SUBJECT TO CHANGE
Lowest Ceiling:
On File On File Fatal
Broken 11000 10 29.92
Scattered 8500
Unknown KRNO 1555
Local Flight NV KRTS
Same as Accident/Incident Location KRTS
Unknown
Air Race/Show
Part 91: General Aviation
None
PO BOX 1476 OCALA FL 34478-1476
James K Leeward
Substantial
Accident
09/16/2011
WPR11MA454
This space for binding
National Transportation Safety Board
PRELIMINARY REPORT
AVIATION
NTSB ID:
Occurrence Date:
Occurrence Type:
Date
Wind Direction:
Weather Conditions at Accident Site:
Weather Information (Continued from page 2)
Temperature: °C Dew Point:
Wind Speed: Kts. Gusts:
Administration Data
Notification From
°C
Kts.
FAA District Office/Coordinator Investigator-In-Charge (IIC)
PRELIMINARY INFORMATION - SUBJECT TO CHANGE Page 3
FAA AVP - 100
Christine Soucy
NTSB
Howard D. Plagens
17 21 Visual Conditions
25 -2 280
Accident
09/16/2011
WPR11MA454
 
Re: Full copy of the NTSB Reno crash report

<div class="ubbcode-block"><div class="ubbcode-header">Originally Posted By: Wanderlust</div><div class="ubbcode-body">What's the NTSB ID#? </div></div>

WPR11MA454
 
Re: Full copy of the NTSB Reno crash report

Figured you guys would like to read this. I R/C planes and have a huge interest in full scale so I've been following this on about 4 different sites. Below is a report from a guy who knows what he is talking about.





Haven't seen any new news on this lately, but did just get an email from a friend in the aviation business with this narrative. I cannot vouch for the authenticity/accuracy of this so am posting with this caveat in mind.

Here's what the email stated;

"To my pilot friends, this is inside info from one of the L29 jet race pilots and may be the best info todate on the Reno Air Race tragedy:

INFO I RECENTLY RECEIVED
Good News for the future of air racing.

Our new crew member, Matt Jackson, is not only a race pilot, aircraft business owner and aircraft owner (he also takes care of Tom Cruises P-51) but he is also the VP of the Unlimited Racing Class and head of the Safety Committee.

We had a long talk about the Reno crash on the way to Mojave today.

Matt believes the cause of the crash was due to The Galloping Ghost having a CG too close to the aft limit which resulted in pitch instability. There are instructions on the P-51 regarding no combat missions with the aft fuel tank full resulting in an aft CG problem. Instructions specify to empty the aft fuel tank first in flight.

During qualifying Matt watched Galloping Ghost from inside the cockpit of Furias and could not believe how much trouble Leeward was having in keeping the Ghost in a stable pattern around the course.

Since Leeward lives in Florida and the Galloping Ghost was modified for racing in Calif., when Leeward picked up the Ghost for the Reno races at the last minute, a complete flight test program had not been done based on available information.

There is a video of the entire last lap of the Ghost before the crash which Matt showed me. As Leeward was coming around pylon #8 at about 480 mph after passing Rare Bear, he hit turbulence which pitched his left wing down, Leeward corrected with hard right rudder and aileron. Just as the aircraft was straightening out, he hit a second mountain of turbulence which caused the tail to 'dig in' resulting in a 10+ G climb rendering Leeward unconscious instantly and resulted in the tail wheel falling out. (broken tail wheel support structure was found on the course). As the Ghost shot upward the LH elevator trim tab broke loose. This can be heard on the tape, so the trim tab did not cause the accident.

Since the Ghost was racing at 480 mph with full right rudder and the stick full right, this is where everything stayed when Leeward blacked out. Cockpit camera film that was salvaged from the wreck shows Leeward slumped over to the right in the cockpit. As a result, the Ghost climbed up and to the right, rolled over on her back and then headed for the box seats. Most in the box seats never saw it coming because it came in from behind them.

Matt has had long conversations with the NTSB who call the accident a 'fluke'. They are not going to recommend canceling future races. He has also talked to the insurance companies covering the races for Reno and they also say they are not going to cancel their coverage of future races. Now we wait for the FAA to make a decision.

Ironically, Matt bought box seats tickets for his good friends who stayed with him for a few days before the races. They were the husband and wife who were killed."
 
Re: Full copy of the NTSB Reno crash report

One of ya'll let me know and I'll send you the PDF of the original NTSB Prelim. I've got an unfair advantage as I'm related by marriage to an NTSB cert accident investigator and retired avaition compliance inspector. They've got the cause of the crash already, but as those who know the NTSB, they don't make a statement until they can show the evidence to prove its a fact. The below is what my FIL has given us.

The short version is that those aircraft are trimmed to run in nose down pitch. The horiz. stab. trim tabs are under constant high load due to this. This witness statements and video show an item departing the aircraft, and then the pitch and roll. They believe it was the trim tab, or part of it. High speed analysis show the tab partially attached, but in a position that would have negated its effect on the attitude of the aircraft. The footage also shows the tailwheel in the down position, and no sign of Leeward in the cockpit. Some estimates put the initial g load as high as 10 G's peak during the pitch up, far more than needed to induce G-loc, break the tail wheel loose, and possibly collapse the seat (it should have been all but impossible for Leeward to be completely out of view). The most popular theory is Leeward was dead at this point, but without doubt was just cargo from there on.

Again, this is THEORY. But I trust the source, and he's backed by 40 years as a military and civilian aviation crash investigator.