|
|
|
|
|
|
|
|
|
|
|
3rd
January 1961 |

USN |
Crusader YF-8C |
147040 |
NATC PAX |
in US |
LCDR W. F. Whalen ejected |
|
Vought |
|
11th
January 1961 |

USMC |
Crusader F-8B
[F8U1] |
145447 |
VMF-312 |
Ejected over Mt. Fuji
in Japan
during tactics flight |
1/LT Gene R. Merritt ejected |
|
One was a Martin-Baker seat the
other was a Vought seat - which was which |
|
11th
January 1961 |

USN |
Crusader F-8C |
147017 |
VF-103, CVA-59 |
|
LTJG D. M. Brookes ejected |
|
|
17th January 1961 |
|
Vought F8U-1 Crusader |
14367
NF |
VA-51 |
x |
x |
x |
x |
|
30th January 1961 |
|
Vought F8U-2 Crusader |
146927 |
VF-142 |
x |
x |
x |
x |
|
31st January 1961 |
|
Vought F8 Crusader |
143808 |
x |
x |
x |
x |
x |
|
1st
February 1961 |

USN |
Crusader F-8A |
145366 |
VF-51 |
in US |
Lt. Cdr. A. C. O'Neal ejected |
|
Martin-Baker |
|
22nd
February 1961 |

USN |
Crusader F-8C |
146923 |
VF-103, CVA-59 |
|
DETAILS OF THIS LOSS NOT CLEAR
DID IT HAPPEN ??? |
|
|
|
23rd
February 1961 |

USN |
Crusader F-8C |
146988 |
VF-124 |
in US |
LTJG K. J. Jackson ejected |
|
Vought |
|
4th March 1961 |

USN |
F8U-1
Crusader |
|
|
|
LTJG R. E. Jacobsen ejected at less than 100 feet.
He died three hours later |
|
Martin-Baker |
|
27th
April 1961 |

USMC |
Crusader F-8B
[F8U-1
Crusader] |
145428 |
VMF-312, CVA-41, USS Midway |
hitting round down on USS Midway |
CAPT M. P. Cady ejected |
|
Vought |
|
28th
April 1961 |

USMC |
Crusader F-8A |
145377 |
VMF-333 |
in US |
2/LT R. S. Welz ejected
outside envelope of the seat and was killed |
|
Martin-Baker |
|
1st
May 1961 |

USN |
Crusader F-8B |
145452 |
VF-154
???? |
in Philippine Islands |
MAJOR R. S. Rash ejected
[F8U-1E]CAPT P. L.
Elliott
USMC ejected
[F8U-1]
CONFUSION as to who was in which aircraft |
|
Vought |
|
1st
May 1961 |

USMC |
Crusader F-8B |
145427
DR |
VMF-312,
CVA-43,
USS Coral Sea |
|
|
Vought |
|
2nd May 1961 |

USN |
Vought F8U-1 Crusader |
145367
NF |
VF-124 |
x |
x |
x |
x |
|
6th
May 1961 |

USN |
Crusader F-8B |
145424 |
VF-124 |
in US. |
Ensign P. D. Farley ejected |
|
Martin-Baker |
|
8th
May 1961 |

USN |
F-8 Crusader |
|
|
|
Lt. Cdr. P. Montilardi ejected |
|
Martin-Baker |
|
22nd
May 1961 |

USN |
Crusader RF-8A |
146839 |
VFP-62, CVA-42, USS Franklin D. Roosevelt |
|
LT W. G. Offerman ejected |
|
Martin-Baker |
|
2nd June 1961 |
|
Vought F8 Crusader |
146923 |
x |
x |
x |
x |
x |
|
12th
June 1961 |

USN |
Crusader F-8C |
147003 |
VF-124 |
in US |
LCDR J. A. Schneider ejected |
|
Martin-Baker |
|
22nd
June 1961 |

USN |
F8U-2 Crusader |
|
|
|
LT P. J. Brown
ejected safely |
|
Martin-Baker |
|
17th
August 1961 |

USN |
Crusader F-8C |
145570 |
VF-191
Barbers Point Naval Air Station, Oahu |
engine suffered catastrophic failure during take
in Hawaii. |
Lt. Kenneth Corica
ejected successfully |
|
Martin-Baker |
|
26th
August 1961 |

USN |
Crusader F-8A |
BuNo 143708 |
VF-211
 |
Punched out over Crater Lake, OR and
actually landed in the lake, being fished out soon after by rangers |
Lt. (jg) William Boardman
ejected
[second ejection, see also
15th April 1959 when he ejected from a TV-2]
[personal testimony]
|
 |
Vought |
|
30th August 1961 |
|
Vought F8 Crusader |
145439 |
x |
x |
x |
x |
x |
|
30th
August 1961 |

USN |
F8U-1P
RF-8A Crusader |
145618 |
VFP-62
Cecil
Field
Jacksonville, Florida
|
Over
the Okeefenokee swamp. |
LTJG Gerald L. "Jerry" Coffee
ejected[Also ejected from RA-5C Vigilante 3rd February 1966,
captured. POW] |
 |
Martin-Baker |
|
9th September 1961 |

USMC |
Crusader F-8C |
146982 |
VMF334 |
RAG training. Material
failure, wing broke at fold on a gunnery hop out of Yuma
in US |
Lt. William H. Juvonen
ejected
Controlled ejection |
|
Martin-Baker |
|
19th September 1961 |

USN |
Crusader F-8C |
145578 |
VF-194
CVA-61
USS Ranger |
|
LCDR G. H. Holloman ejected |
|
Martin-Baker |
|
20th September 1961 |

USMC |
Crusader F-8C |
146912 |
VMF-323 |
in US. |
Capt. L H.Holmes
ejected |
|
Martin-Baker |
|
6th October 1961 |

USN |
RF-8A Crusader |
needed |
VFP-62 |
After the pilot's ejection the
aircraft continued in flight for over one hour and had to be brought down over
the water by
a Sidewinder missile fired from another fighter |
LCDR C. H. Price ejected |
|
Vought |
|
|
 |
|
|
16th October 1961 |

USN |
Crusader F-8A |
144452 |
VF-211 |
in US. |
LTJG William M Boardman
[third ejection, see also
15th April 1959 when he ejected from a TV-2]
and second ejection
on 26th
August 1961][personal testimony] |
 |
Martin-Baker |
|
16th October 1961 |

USMC |
F-8C Crusader |
147033 |
VMF-333 |
in US. |
1st Lt. James E.
Strawn ejected at high speed |
 |
Martin-Baker |
|
17th October 1961 |

USMC |
Crusader F-8C |
16949 |
VMF-334 |
in US. |
Major R. B.Haines ejected |
|
Martin-Baker |
|
21st October 1961 |

USN |
Crusader F8U-1 |
145375
AB 212 |
VF-11
CVA-42
USS Franklin D. Roosevelt |
|
Lt. J. Terry Kryway
[2nd ejection also ejected from an F-8 on 20th February 1959] ejected after he directed the aircraft off the
deck due to fire
caused by heavy landing
broke wheel strut. Famous sequence of photographs [by photographer mate L.
J. Cera] |
LOOKING FOR PHOTO OF LT KRYWAY _ CAN ANYONE HELP ??? |
Martin-Baker |
 
Stills from the famous film sequence
Visit Rod Rogers
web site
for the complete set |
|
23rd October 1961 |

USN |
Crusader F-8A |
143794 |
VF-191 |
in Japan. |
Lt. C. D. Metzler ejected |
|
Martin-Baker |
|
2nd November 1961 |

USN |
Crusader F-8C |
146926 |
VF-194 |
in Japan |
LTJG R. L. Martin
ejected |
|
Martin-Baker |
|
2nd November 1961 |

USMC |
Crusader F-8A |
147024 |
VMF-333 |
in US |
1/LT. Joseph "Joe" P. McDonald
ejected |
|
Martin-Baker |
|
FEEDBACK |
I am listed as
ejecting on November 2nd 1961 while with VMF-333 in U.S. (actually,
within two miles of base at Beaufort, S.C.) under name 1st Lt. J.P.
MacDonald (actually, I'm J. (for Joseph, better "Joe") F. McDonald. I popped out
some two weeks ahead of 1st Lt. C. W. Vogt (November 15,1961), a member of the
same group (who later served as Chairman of the U.S. National
Transportation Safety Board from 1992 - 1994).
I was two weeks behind 1st Lt. James E. Strawn's supersonic ejection
on October 16, 1961, when he was my wingman in the manoeuvres described
in his amazing account linked to your write-up of his ejection. I am in
sporadic contact with him through a larger group of mostly former VMF-333 F8
jocks.
Love to help. . . .
Joe
in email 28th October 2009
[name spelling corrected 28/10/09]
|
|
12th November 1961 |

USN |
Crusader F-8D |
148653 |
VF-154, CVA-43, USS Coral Sea |
??? |
Lt. (jg) J. A. James
ejected |
|
Martin-Baker |
|
15th November 1961 |

USMC |
Crusader F-8C |
146922 |
VMF-323 |
Engine failure,
in Hawaii |
1st LT C. W. Vogt
ejected |
|
Martin-Baker |
|
30th November 1961 |

USN |
Crusader RF-8A |
146850 |
VFP-63 |
in US |
LT L. K. Dalrymple
ejected |
|
Martin-Baker |
|
4th
December 1961 |

USMC |
Crusader F-8B |
145448 |
VMF-312
Atsugi |
Wing failure during tactic flight
in Japan.
Landed after coming through thatched roof of
Japanese police station |
Capt. Allen Leroy Frucci
ejected NW of Tokyo
No injuries
[Allen Frucci also ejected on
29th October 1962 from a USAF F-100D while on a tour of exchange] |
 |
Martin-Baker |
|
FEEDBACK |
"Bail out on 4 Dec
61. Pilots name -Allen Leroy Frucci - Flying out of Atsugi while
a member of VMF-312 ( the best and wildest crusader squadron of
them all) He was in a hassle with some of our other folks and
pulled the wing off. Ejected safely and came down through the
roof of a Japanese police station. Just another day in dear old
312."
Bob Wiedemann |
|
5th December 1961 |
|
Vought F8U-2N Crusader |
146845
NH |
VF-211 |
x |
x |
x |
x |
|
7th December 1961 |

USMC |
Vought F8U-1E Crusader |
145529
WT |
VMF-232 |
x |
x |
x |
x |
|
10th
December 1961 |

USN |
Crusader F-8D |
147915 |
VF-32, CVA-60 |
|
LCDR R. W. Paige ejected |
|
Martin-Baker |
|
13th December 1961 |
|
Vought F8U-1P Crusader |
146859 |
VFP-63 |
x |
x |
x |
x |
|
15th
December 1961 |

USN |
Crusader F-8D |
147900 |
VF-174 |
in US |
LT W. A. Updike ejected |
|
Martin-Baker |
|
25th
January 1962 |

USMC |
Crusader F-8A |
144442 |
???
|
in US |
1st Lt. H. M. Spann ejected |
|
Martin-Baker |
|
8th
February 1962 |

USMC |
Crusader F-8B |
145493 |
VMF-232
CVA-19 |
|
I.Lt. D. G. Doherty
ejected |
|
Martin-Baker |
|
16th
February 1962 |

USN |
Crusader RF-8A |
146887 |
VFP-62, CVAN- 65 |
|
Lt. H. H. Love ejected |
|
Martin-Baker |
|
27th
February 1962 |

USN |
Crusader F-8A |
145396 |
VF-124 , CVA- |
collided during join up in US |
Lt.(jg) R. G. Bengston
ejected
1st Lt. C. P Jackson
ejected
Who was in which
aircraft??? |
|
Martin-Baker |
|
27th
February 1962 |

USMC |
Crusader F-8A |
146975
???? |
|
collided during join up in US |
|
Martin-Baker |
|
5th March 1962 |

USMC |
Vought F8 Crusader |
146896
FM |
VMCJ-1 |
x |
Lt. (jg) T. H. Godber
ejected
From which
Aircraft ?? |
x |
x |
|
5th
March 1962 |

USN |
Crusader F-8A |
145388 |
VU-4 |
in US |
|
Martin-Baker |
|
|
 |
|
8th
March 1962 |

USN |
Crusader F-8C |
146906 |
VF-103 |
in US |
LCDR A. E. Westmoreland ejected |
|
Martin-Baker |
|
9th
March 1962 |

USN |
Crusader F-8A |
145403 |
VF-191 |
in US |
LCDR J. L. Snyder
ejected |
|
Martin-Baker |
|
16th March 1962 |

USN |
Vought F8U-1 Crusader |
145323
NM |
VF-191 |
x |
x |
x |
x |
|
26th
March 1962 |

USN |
Crusader F-8C |
146962 |
VMF-334
CVA-34 |
in US. |
1/Lt. B. J. Bertram
ejected |
|
Martin-Baker |
|
28th
March 1962 |

USMC |
Crusader RF-8A |
146822 |
VMCJ-2 |
in US |
CAPT R. W. Tucker ejected |
photo in file - I think |
Martin-Baker |
|
2nd
April 1962 |

USN |
Crusader RF-8A |
146857 |
VFP-63 |
in US |
LTJG S. W. Betts ejected |
|
Martin-Baker |
|
3rd April 1962 |

USN |
Vought F8U-1 Crusader |
143774
JF |
VU-4 |
Damaged beyond repair |
x |
x |
x |
|
13th
April 1962 |

USMC |
Crusader RF-8A |
146875 |
VMCJ-3 |
in US |
Col. H Williams
ejected
landed in 3 feet of water and separated from seat |
|
Martin-Baker or Vought
??? |
|
21st
April 1962 |

USMC |
Crusader F-8B |
145485 |
VMF-122 |
in US |
2/LT K. L. Weller
ejected |
|
Martin-Baker |
|
24th
April 1962 |

USN |
Crusader F-8A |
143709 |
|
in US |
LCDR W. T. Harvey ejected |
|
Martin-Baker |
|
25th April 1962 |

USN |
Vought F8U-2E Crusader |
148709
AE-201 |

VF-132
USS Constellation
Link |
Ramp strike,during night landing, Diverted to Guantanamo Bay Cuba
- carsh landed |
Lt
R. Loomis
OK |
x |
x |
|
|
US Navy Photo courtesy Bruce Nason via Ken Jack,
webmaster
www.vfp62.com |
|
30th
April 1962 |

USN |
Crusader F-8D
[F8U‑2N] |
148683
AE 2 |
VF‑132
CVA-64 |
Caribbean, damaged in night bolter |
Cdr. G. C.Watkins
ejected
immediately and was picked up by destroyer |
|
Martin-Baker |
|
3rd May 1962 |

USMC |
Vought F8U-2 Crusader |
146924
WU |
VMF-334 |
x |
x |
x |
x |
|
7th
May 1962 |

USN |
F8U-2 Crusader |
145567 |
VF-194 |
in US |
LTJG Otto Burgdorf ejected |
|
Martin-Baker |
|
8th
May 1962 |

USN |
F-8C Crusader |
147013 |
VF-24 |
CVA-41 |
LTJG Barry E. Kunkel
ejected
[personal testimony] |
need photo |
Martin-Baker |
|
|
web bio |
|
22nd
May 1962 |

USN |
Crusader F-8A |
145375 |
VF-62 |
in US |
LT W. F. Heiss ejected |
|
Martin-Baker |
|
23rd May 1962 |

USMC |
Vought F8U-1E Crusader |
145464
WT |
VMF-232 |
x |
x |
x |
x |
|
22nd
June 1962 |

USN |
F-8B Crusader |
145541 |
VMF-312 |
Ejection in US |
Major L. A. Seipp ejected |
|
Martin-Baker |
|
26th
June 1962 |

USN |
F-8A Crusader |
143705 |
VC-4. |
Ejection in US |
Lt. G. E.Custer
ejected |
|
Martin-Baker |
|
27th June 1962 |
|
Vought F8U-2NE Crusader |
149162
NJ |
VF-124 |
x |
x |
x |
x |
|
1st
July 1962 |

USN |
Crusader F-8D |
149188 |
VF-33,
CVAN-65
USS Enterprise |
Catapult failure |
LT Edward Frances "Sully" Sullivan
ejected
Body not recovered
[see below] |

photo via Gregory Sullivan |
Martin-Baker |
|
|
|
|
1st July 1962 |

USN |
Vought F8U-2N Crusader |
147052
NU |
VF-124
USS Ranger |
Off
California, USA |
|
x |
x |
|
1st
July 1962 |

USMC |
Crusader F-8C |
146964 |
VMF-33 |
in US |
|
|
Martin-Baker |
|
2nd July 1962 |

USN |
Vought F8U-2N Crusader |
147053
NH |
VF-111 |
x |
x |
x |
x |
|
4th
July 1962 |

USN |
Crusader F-8C |
146967 |
VF-174 |
in US |
Lt. jg R. N. Super
ejected |
|
Martin-Baker |
6th
July 1962
also seen as 7th |

USN |
RF-8A Crusader |
145644 |
VFP-62 |
in US |
ENSIGN G. M. Burton ejected |
|
Martin-Baker |
|
10th July 1962 |

USN |
F-8C Crusader |
146946 |
VMF-174 |
in US |
LTJG Robert "Bob" C. Smith ejected
killed on impact |
|
Martin-Baker |
|
11th July 1962 |

USMC |
Vought F8U-2 Crusader |
146964
WU |
VMF-334 |
|
1/Lt. M. M. Bomis ejected |
x |
x |
|
11th
July 1962 |

USMC |
F8U-1E Crusader |
145522
WT |
VMF-232 |
in Philippine Islands |
1/Lt. N. R. Driscoll ejected |
|
Martin-Baker |
|
14th
August 1962 |

USN |
Crusader F-8C |
146934 |
VF-84, CVA-62 |
|
Lt. (jg) H. E. Shephard
ejected |
|
Martin-Baker |
|
25th
August 1962 |

USN |
Crusader F-8B |
145517 |
VF-62
Cecil Field |
Took off from
Cecil Field, near Jacksonville, heading for Guantanamo Bay, Cuba
Flamed out
Crashed in US |
Cdr. John G. Brozo
[Skipper - 'Diamond Flight']
ejected
Was found two days after the
accident by an
Air Force rescue crew, flying an amphibious aircraft. They landed in
very rough seas and retrieved CDR Brozo from his one-man life raft. He
had suffered a broken back due to the ejection |
|
Martin-Baker |
|
25th
August 1962 |

USN |
Crusader F-8B |
???? |
VF-62
Cecil Field |
Took off from
Cecil Field, near Jacksonville, heading for Guantanamo Bay, Cuba
Flamed out
Crashed in US |
LTJG Tom Malloy
['Diamond Two']
believed to have ejected
never found |
|
Martin-Baker |
|
|
THUNDERSTORM FLIGHT
It was a beautiful Florida Saturday morning, in August 1962, when a
flight of seven F-8 Crusaders from Fighter Squadron 62 . I
well remember LTJG Tom Malloy laughing and pointing to his new flight
suit as we briefed for the long flight that morning. He had been
issued the flight suit the day before and had not tried it on. It was
about three sizes too big and he looked lost in that tent size
costume. There was no way to exchange it for another one since it was
Saturday and the supply office was closed. Tom had a wonderful sense
of humor and accepted our kidding with a big smile. That is the way I
remember him until this day.
As you will recall this time and date was just prior to the ‘Cuban
Missile Crisis’. Our mission was to demonstrate a ‘show of force’ at
the small Naval Base on the southeastern side of Cuba. I had joined
VF-62 just a few weeks earlier and this was my first major deployment
with the squadron. I was a ‘Nugget’ as they call the new pilots fresh
out of flight school. Two Divisions, eight airplanes, were scheduled
to deploy that morning but one of the airplanes had mechanical
problems. LCDR Paul Gillcrist was scheduled to be the second Division
leader but he never got airborne due to a radio problem as I recall.
Therefore, we had a flight of 4 and a flight of
3 F-8’s heading for Cuba.
We went "Feet Wet" (over water) just north of Miami. About 150 miles
southeast from Miami, over the Caribbean, we entered an area of very
low visibility at our cruising altitude of 39,000 feet. Our forward
visibility was one mile or less. We had no weather radar. In fact the
radar on board the F-8B had a maximum range of 16 miles and most of
them never worked. The weather briefing we received before the flight
made no mention of severe weather along our route of flight. We were
unaware that huge thunderstorms were hidden in the haze ahead.
Nevertheless these cumulonimbus demons were in our flight path and
were about to inflect major damage to our flight.
The Skipper, John Brozo (Diamond Flight) was leading the first
division of 4 airplanes. His flight consisted of LTJG Tom Malloy,
Diamond two, LT Dick Oliver, Diamond three, and LTJG Ben Walker,
Diamond four. In my flight of three airplanes were LT Al Wattay,
Division leader, LT John Nichols (Pirate) right wing and myself flying
left wing position. LT Wattay positioned our flight about 5 miles aft
and two miles abeam Diamond Flight. Although the visibility was low
the ride was fairly smooth as I recall.
Everything was going great until I heard the Skipper say in a very
loud and frantic voice, "DIAMOND ONE FLAMED OUT!" And as my heart was
elevating up into my throat I heard his wingman LTJG Tom Malloy saying
with even more fear in his voice, "DIAMOND TWO FLAMED OUT." Before I
could suck up more oxygen I heard the Skipper say, "DIAMOND ONE
EJECTING - STAY WITH ME IF YOU CAN!" Just seconds later I heard LT
Dick Oliver say, "DIAMOND THREE FLAMING OUT." Almost instantaneously
another call came into my headset, "DIAMOND TWO EJECTING." Nothing was
heard from Diamond Four. We thought he went down as well.
WOW! This was my first major cross-country with the squadron and the
airplanes were falling out of the sky. I was anxiously waiting for my
engine to quit as well. We were only seconds away from their position.
I was very tense to say the least. My heartbeat was louder than the
jet engine. However our flight of three flew through the same area,
basically at the same time, without any problems. It took many months
and numerous accident investigations to determine how our flight made
it through this area without any problems. I’ll explain why later.
The F-8 was a great fighter as long as the engine was running.
However, an engine flameout causes instant electrical and hydraulic
power loss. In addition, at the higher altitudes, the canopy fogs over
almost immediately. We were at 39,000 feet and the pilots who lost
engine power experienced all of the above instantaneously. This makes
the great fighter not too ‘user-friendly’ to say the least. All flight
instruments go ape, the airspeed decreases rapidly and the flight
controls freeze since there is no hydraulic power. In a situation like
this the pilot is just along for the ride, but he is frantically
trying to regain control of that hunk of metal falling through space
by instant recall of his emergency procedures. All the while he is
being slammed around in the cockpit like a sock in a washing machine.
The Navy had a term called ‘Over Learning.’ All pilots had to go over
and over emergency procedures time and time again until they could
respond automatically, in any situation, without thinking. This rote
memory of learning saved a lot of pilots and planes.
One of the undesirable characteristics of the F-8 is that when the
indicated airspeed reduces below 170 KIAS it will automatically enter
into a spin with just a little aileron or spoiler input. Due to the
conditions of this flight, listed above, these flamed- out Crusaders
automatically entered into a spin. It was very tough to recover the
F-8 from a spin in day VFR conditions. Add a big bad thunderstorm to
the equation, with the engine flamed out, the flight controls frozen,
the airplane spinning, and the canopy iced over makes recovery nothing
short of a miracle.
The F-8 was equipped with an emergency air driven generator that also
provided emergency hydraulics for primary flight controls. This Ram
Air Turbine (RAT), when extended into the air stream, was designed to
recover part of the electrical power and part of the hydraulic power
as well. The emergency generator switch had to be turned on after
dropping the RAT, or no electrical power would be supplied to the
aircraft. This procedure was easy to omit. The RAT restored hydraulic
power necessary for spin recovery and electrical power for a re-light
of the engine in this big bad cumulonimbus cloud.
It takes a few seconds for the RAT to come up to speed after
deployment. Sometimes, like in this case, those few seconds can feel
like an eternity. As I recall LT Oliver said in the accident report,
"The airplane was spinning before the RAT became effective." This is
kind of like the parachute riggers jokingly saying, "If it don’t work
bring it back and we will give you another one!"
Yet, with all this adversity Diamond Three, LT Dick Oliver, did
recover from the spin, and got his engine running again. This was by
no means an easy task. He first had to extend the RAT to regain flight
control and then he had to recover from the spin. A spinning F-8 may
go from 10 degrees nose up to 190 degrees nose down, while pulling
from plus 4 to minus 3 G’s, all the while rotating rapidly like a west
Texas twister. This short paragraph does not do justice for the superb
airmanship that Lt Oliver demonstrated that dreadful day.
Spin recovery procedures in the F-8 were very different and extremely
difficult. While experiencing the violent maneuvers noted above the
pilot had to move both hands to the left console and unlock the
pneumatic switch for emergency extending the leading edge landing
droop. This extended droop changed the aerodynamics of the wing and
served to get the stalled wing producing lift again. In addition, full
aft stick, and full aileron into the rotation of the spin was
required. At the same time full opposite rudder into the spin was
essential. This condition was held until the rotation stopped and only
then could the nose be brought up to pull out of the dive. If the
airplane was in un-controlled flight at 10,000 AGL the pilot was
required to eject. After recovering from a spin the leading edge
landing droop could not be retracted in the air. This placed speed and
‘G’ restrictions on the airplane. In addition the maximum range was
reduced consequentially as well. Needless to say that spins were to be
avoided and when one developed it left you with a crippled airplane.
The emergency engine air start procedure was a lengthy process. A lot
of altitude was lost during the re-start procedure. During this time
you were falling out of the sky like a rock. The pilot had to insure
that the RAT had been deployed and the emergency generator switch was
ON in order to supply electrical power to the igniters, which was
required to start the jet engine. If I remember correctly you tried to
establish airspeed around 200 KIAS, plus or minus 30 KIAS. This speed
supplied enough ram air through the engine intake to windmill the
engine from 17% to 30% RPM. Once these parameters were met the
throttle and ignition could be selected. If you got fuel flow of at
least 750 Pounds Per Hour the engine should relight. If not repeat the
procedures again, if you had enough altitude. Last choice was to make
a nylon descent via the ejection system.
When my flight leader, LT Al Wattay, heard the radio transmissions
from Diamond flight he advanced power by selecting the afterburner,
accelerated to MACH ONE and we climbed to 50,000 feet. LT Nichols
(Pirate) and I were hanging on his wing as best we could. Little did
we know at the time that the extra speed and altitude is what saved
our flight and possibly our lives. It was brought out in the accident
report that the Skipper of Diamond flight had let his formation slow
to below Mach .70, which is very slow at that altitude. They also
determined that it was a good possibility that vertical wind shears
could cause a flame out during such conditions due to reduced air
through the intake to the engine. In addition the older models F-8’s
were not equipped with engine anti-ice. This was also a factor in the
accident. Due to the fact that LT Wattay accelerated our flight to a
much higher airspeed the wind shear had no effect on our engines. In
addition climbing to a higher altitude removed us out of the icing
area. Thanks LT Wattay for great airmanship that day.
We proceeded on to Guantanamo after making "MAYDAY" calls and
reporting the crash site position on guard to the search and rescue
Air Force squadron in Miami. There was no way for us to locate the
downed pilots since the weather was clogged in all the way to the
deck. And besides that we just barely had enough fuel to fly to
Guantanamo. There were no Texaco Tankers available that day.
After landing in Cuba we assumed that three aircraft had been lost. We
still had no word from Diamond Four. All of sudden we heard an F-8
coming into the area at the speed of heat. We were very thrilled to
see Diamond Four, Lt Ben Walker, overhead. Later he told us that he
had lost his generator in the midst of all the excitement, dropped his
RAT for electrical power, but never regained his radio. All that he
knew was that his flight had disappeared in the clag.
Diamond One, the Skipper, was found two days after the accident by an
Air Force rescue crew, flying an amphibious aircraft. They landed in
very rough seas and retrieved CDR Brozo from his one-man life raft. He
had suffered a broken back due to the ejection. The F-8 had an
explosive cartridge in the ejection system that hit you in the butt
with mega ‘Gs’ when ejecting. A spin produces a lot of negative ‘Gs’.
The Skipper said that he was in a negative ‘G’ flight when he ejected.
This could explain his broken back due to the extra hit in the rear by
the ejection seat. He was later relieved of his command for taking his
flight through a thunderstorm. Yet, he had no way of knowing that
severe weather was in his flight path.
Diamond Two, Tom Malloy, was never found. About three years later his
helmet washed ashore on one of the small islands in the Caribbean. He
was reported missing until that time. We never really knew what happen
to him after he called "Ejecting." The Skipper said that his ejection
was very rough. After landing in the water he almost drowned by his
parachute pulling him under. The wind on the surface was very strong.
Under those conditions a parachute in the water can be deadly. If Tom
was injured during ejection, as the Skipper was, his survival would
have been in jeopardy.
The following is what a pilot may experience when ejecting from a fast
flying airplane at high altitude. As you can imagine it is a hazardous
experience to say the least. As stated above the explosive charge in
the ejection seat can give you quite a kick in the butt. This big kick
is necessary to insure that the pilot clears the vertical tail of the
airplane during an ejection. The first sequence in an ejection is for
the canopy to separate from the airplane. If it does not separate the
pilot is shot through the canopy. If the pilot ejects at 40,000 feet
he is quick to feel the cold rushing wind hitting his body at the
speed at which he ejected; let’s say 400 KTS for example. It may be 60
degrees below zero at that altitude and with very little oxygen to
breathe. This is not too good for the boys in summer flying suits. The
pilot cannot survive in that environment very long because he would
freeze to death and or die from hypoxia (lack of oxygen). The ejection
system is designed so that a small drogue parachute, about the size of
an umbrella, extends immediately after ejecting. This small chute
prevents the pilot from tumbling during descent, but he is still
falling like a brick. The ejection seat is equipped with an emergency
oxygen bottle that will last about 10 minutes for just such high
dives. This system can be used under water as well. That is if your
mask has not been ripped from your face during the high-speed exit of
the airplane.
The pilot, still strapped in the ejection seat, will free-fall, in
this case 30,000 feet, before the main chute opens. He is traveling at
the ‘speed of heat’ straight down. This sequence is supposed to open
the main parachute automatically by a barometric release, which is
normally set for operating at 10,000 feet above ground level. When
that altitude is reached a bladder in the seat inflates pushing the
pilot out of the seat and then the main parachute deploys. If the
automatic system does not work then the pilot can manually push the
ejection seat aside and pull the ‘D-Ring’ for the chute to open. How
does the pilot know when he reaches 10,000 feet? He can only estimate
his altitude by visual references. In a thunderstorm that is
impossible. In a storm such as this there would be limited visibility,
which would make it impossible to estimate your altitude. In addition
the pilot is in heavy rain, or hail, severe turbulence, and possible
heavy lightning.
Presume that the pilot gets a good parachute opening at 10,000 feet
and floats gracefully down to the waiting ocean. He still has a lot of
emergency procedures to accomplish to insure his survival. First, and
most importantly, he must unhook from the life saving parachute, which
becomes a death trap once it hits the water. When a parachute is
filled with water it will sink like a rock taking the pilot down as
well. If the pilot’s hands or arms are injured it may be impossible to
release the parachute. This quickly turns into a very serious
condition. In addition, once the parachute is released from the
pilot’s harness shroud lines from the chute may entangle the pilot.
These lines may snare him and take him under. For that reason all Navy
pilots carried an open knife, with a hook blade, attached to their
harness to cut the shroud lines if necessary.
If all of the above was accomplished without incident, the pilot still
had a lot of work to do. He must inflate his life vest to keep him
afloat since he is burdened with about 50 pounds of flight gear. At
this time he needs to deploy and inflate his one-man life raft that is
stored in a packet, which is attached to his harness. In this parcel
are such items as shark chaser, dye marker, signal mirror, fishing
hooks, a small salt-water distillery to convert seawater to fresh
drinking water, and a host of other small things.
Boarding the one-man life raft is no easy task in a swimming pool and
it becomes even more difficult in rough seas or if he is injured. Once
on board the little rubber raft a big wave can dump you back in the
water very quickly and totally mess up your command at sea. You must
re-board the little ‘private yacht’ or the sharks may eat you for
dessert. This could go on for days. These are the conditions that
Diamond One and Diamond Two were faced with that dreadful day.
The news media in our city broadcasted that all planes in our flight
were lost at sea. Of course that placed undue and unnecessary stress
on our families and friends. Communications back then were very
antiquated. It took hours for the facts, as we knew them, to get back
to our home base.
Thereafter this story was told many times in pilot training. The
point was made loud and clear to never fly into a thunderstorm.
I record this account in tribute to my fallen comrades. CDR John
(Diamond) Brozo, deceased; LT Dick (Smooooth One) Oliver, deceased
killed with the Blue Angels; LTJG Tom Malloy, killed on this flight;
LT Ben (Bugger) Walker (deceased); LT John (Pirate) Nichols, deceased.
As far as I know LT Al Wattay is still living. Note: The rank
indicated is the rank these officers held at the time of this
accident.
In this narrative I was amazed at how many emergency procedures I
could recall after 40 years. This information is 100% from my memory
and not from documents or other sources. This again proves the point
that the military drilled unto all pilots the ‘Over Learning’ process.
Most pilots could do the same. God bless.
Ron Knott 5/2005
sourcehttp://www.airtalk.org/image-vp229594.html |
|
14th September 1962 |

USMC |
Crusader F-8D |
148685 |
VMF-235
NAS Dallas |
iDallas, US |
1/LT A. Phil Longdon Jr, ejected
when attitude was inverted
killed |
|
Martin-Baker |
|
|
"Phil was number 2 in a 4-plane echelon
entering the break at NAS Dallas. The leader broke for landing and just
before Phil broke, an Air Guard F-86 that was shooting touch and goes,
pulled up through the entry altitude and collided with Phil. The F8
was struck at the wing root and the wing separated from the fuselage. The F8
continued sans wing and rolled. Phil ejected, but when the
seat actually fired he was inverted and was ejected into the ground at the
edge of the lake. The Air Guard pilot was killed when his cockpit struck
Phil's plane."
Tom O'Rorke
in email 25th
November 2008
|
|
20th September 1962 |

USN |
F-8 Crusader |
|
|
|
Lt. Gurg K. Webb ejected |
|
Martin-Baker |
|
10th October 1962 |

USN |
Vought F-8A Crusader |
145406
NM-106 |
VF-191
CVA-31 USS Bonhomme Richard |
Barricade stop - but went over the side |
Ltjg Don Jordan
egressed safely |
x |
x |
|
|
On Oct. 10th, 1962, on board the
Bonnie Dick, CVA-31, a pitching deck off the coast of Hong Kong caused the left
main wheel to separate & a
bolter followed. All other A/C were recovered & the barricade erected. 2nd pass
was an OK 2 wire with the hook releasing the wire after about
30' of travel. Barricade cable did not release from the top of the stanchions
allowing the A/C to "eat" it's way thru. The A/C left the angle deck with full
power at about 100 kts. & hit the water flat. It broke into several pieces,
wing, fuselage & cockpit. Canopy was gone so pilot proceeded to unbuckle the
shoulder fittings. Cockpit then rolled inverted & sank. One Hartman fitting
had broken, so mask had to be held in order to get oxygen. The two waist buckles
were released, only to discover the left foot jammed under the rudder petal.
Pilot stood on the seat & lunged, releasing foot, & also disconnecting O2 hose
at a depth of about 40'. Swimming to the surface he saw parts of the A/C
sinking around him. The bridge had incorrectly called for full right rudder,
throwing the stern toward the crash site, so the pilot also saw one of the huge
props throwing bubbles as it churned past. Made it the surface after remembering
to actuate the Mae West. Chopper was right there & deposited pilot on the
flight deck. Slight injuries, cut on chin & elbow, flew two days later.
CVA-31 Capt. Bullard VF-191
Skipper Merl Gorder, XO Jack Snyder, Safety
Officer John Harker CAG LSO Ken Wiley VF-191 LSO Wayne Williams
Pilot
Ltjg Don Jordan A/C F-8A Don't have access to my log book in storage
so can't confirm BuNo. |
|
15th
October 1962 |

USMC |
Crusader F-8C |
145591 |
VMF-333 |
in Puerto Rico |
2/LT J. D. Carroll ejected |
|
Martin-Baker |
|
16th
October 1962 |

USN |
Crusader
RF8U |
145604 |
DET65
VFP-62
CVAN65 Enterprise
|
in US |
Lt Cmdr W. Newby Kelt
[1st ejection from an F-8
see also
16th April 1963] |
 |
Martin-Baker |
|
17th
October 1962 |

USN |
Crusader F-8C |
145586 |
VF-174 |
in US |
Lt. J. F. Ruchala
or
Lt. (jg) C. K. Dosch ejected who was in which aircraft ??? |
|
Martin-Baker |
|
17th
October 1962 |

USN |
Crusader F-8D |
149156 |
VF-11, CVA-42 |
|
|
Martin-Baker |
|
25th October 1962 |

USN |
Vought RF-8A Crusader |
146837 |
VTF-64 Det C
USS Kitty Hawk |
Lost during mission |
x |
x |
x |
|
7th
November 1962 |

USN |
Crusader RF-8A |
146829 |
VFP-62 |
in US |
Lt. J. McDonnell ejected |
|
Martin-Baker |
|
15th
November 1962 |

USN |
Crusader F-8A |
143728 |
VF-124 |
in US |
Lt. Cdr. J. F. Sullivan
ejected |
|
Martin-Baker |
|
25th November 1962 |

USN |
Vought F-8E Crusader |
149178
AF |
VF-33
USS Enterprise |
Lost during mission |
x |
x |
x |
|
4th
December 1962 |

USMC |
Crusader F-8C |
146914 |
VMF-334 |
in US |
Lt. Col. Walter Panchison
ejected |
|
Martin-Baker |
|
26th December 1962 |

USMC |
Vought F-8C Crusader |
146940
DN |
VMF-333
NAS Roosevelt Roads, PR, USA |
Lost during mission |
x |
x |
x |
|
11th
December 1962 |

USN |
Crusader F-8D |
149144 |
VF-11, CVA-42 |
|
Lt. Cdr. F. G. Fellowes Jr.
ejected |
|
Martin-Baker |
|
5th January 1963 |

USMC |
Crusader F-8B |
145434 |
VMF-312 |
in US |
1.Lt. W.D.Bethea ejected |
|
Martin-Baker Mk.F5 |
|
24th January 1963 |

USMC |
Crusader F-8B |
145480
DW |
VMF-251 |
|
Major K. C. Palmer ejected |
|
Martin-Baker Mk.5A |
|
24th January 1963 |

USN |
Vought F-8A Crusader |
141355
UH |
VU-7 |
x |
x |
x |
x |
|
25th January 1963 |

USN |
Crusader F-8D |
147066 |
VF-124
CVA-19 |
|
LT W. S. Fields III ejected |
|
Martin-Baker Mk.F5 |
|
1st February 1963 |

USN |
Vought RF-8A Crusader |
146851 |
VFP-63
USS Kitty Hawk |
Lost during mission |
x |
x |
x |
|
5th February 1963 |

USN |
Vought F-8C Crusader |
145551
AJ-2?? |
VF-103 |
x |
x |
x |
x |
|
15th February 1963 |

USN |
Crusader RF-8A |
145640
PP-928 |
VFP-63
CVA-43
USS Coral Sea |
rolled over to the left when it
became airborne. after launching and he ejected with the aircraft inverted into
the sea |
LT Delmar D. Young ejected
killed.
His body was not recovered |
|
Martin-Baker Mk.F5 |
|
18th February 1963 |

USN |
Vought F-8C Crusader |
146928
NG-1?? |
VF-91 |
x |
x |
x |
x |
|
25th February 1963 |

USN |
Vought DF-8A Crusader |
143711
UA |
VC-1 |
x |
x |
x |
x |
|
10th March 1963 |

USMC |
Vought F-8C Crusader |
147032 |
VMF-333 |
x |
x |
x |
x |
|
11th March 1963 |

USMC |
Vought RF-8A Crusader |
144621
TN |
VMCJ-3 |
Damaged beyond repair |
x |
x |
x |
|
19th March 1963 |

USN |
Vought F-8D Crusader |
147920
AC-2?? |
VF-32
"Swordsmen"
CV-60
USS Saratoga |
Crashed on the flight deck during night time air operation. |
CDR Ed J. Clayton
[VF-32 Skipper]
killed |
 |
|
|
These details need confirming |
|
25th
March 1963 |

USMC |
 |
Capt. Donald E. Cathcart
ejected |
 |
Martin-Baker Mk.5A |
|
F-8D Crusader |
148655 |
VMF-451 |
MCAS Beaufort, South Carolina
USA |
|
26th
March 1963 |

USN |
RF-8A Crusader |
146862 |
VFP-62 |
in US |
LT W. L. Taylor ejected |
|
Martin-Baker Mk.5A |
|
27th March 1963 |

USN |
Vought RF-8A Crusader |
146877 |
VFP-63
Det. D |
x |
x |
x |
x |
|
8th April 1963 |

USN |
Vought F8 Crusader |
144612 |
VFP-62 |
Aircraft went into the water while attempting to photograph a
Russian trawler |
LTJG John Richard Richardson
killed |
 |
x |