F-106 DELTA DART

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Lineage History F-106A 572457

Convair
F-106A
572457
1957
52
340 (277 A, 63 B)
1959-03-01
1959-03-28
1969-04-22
unknown
437th,456th,460th,539th
AFFTC
Mar 1959 - 52nd F-106 produced by Convair at San Diego CA
15 Apr 59 - To Air Force Flight Test Center, Edwards AFB CA as a test bird
18 May 59 - To 539th FIS McGuire AFB NJ
05 Dec 66 - Burn Damage
25 Apr 67 - To 456th FIS Castle AFB CA
01 Jul 68 - To 437th FIS, 414th FG, Oxnard AFB CA
30 Sep 68 - To 460th FIS, 414th FG, Oxnard AFB CA
22 Apr 69 - Crashed on landing. Pilot, a Maj but name unknown, ejected and survived. The right gear was stuck and after several tries at bouncing it loose the pilot decided to use the cable barrier. Unfortunately the tail hook caught the runway lights and ripped off so he had to set it down on one main gear. Aircraft pieces were strewn over several fields next to Oxnard AFB, Camarillo, CA. Aircraft carted off on a flatbed.
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TAC Conventional: Models produced with Tactical 'Round Eye' instruments.


Conventional: Models were originally committed as TEST or BAILMENT aircraft..


TEST-to-TACTICAL: Models returned to Convair and upgraded from TAC Conventional to Vertical
instruments in 1961. Fuselage cut in half at station 412 (Aft bulkhead missile bay) and a new fuselage, cockpit section,
and nose section was installed with the latest production avionics, the same as the last F-106A 590148 and F-106B 590165.
A total of 35 aircraft (28 "A" models and 7 "B" models) were converted and reassigned to various ADC units..


Vertical, 1st Produced: First 'A' and 'B' models produced with vertical instruments.
Tactical Vertical: Models factory produced w/Tactical Vertical instruments: late 1957 and all 1958, 1959..


F-106 Specifications
Role/Function  Fighter-Interceptor
Manufacturer  Convair Division of General Dynamics
Country  United States
Crew  'A' Model 1, 'B' Model 2
Power plant  Pratt & Whitney J-75-P-17 Turbojet
Thrust  24,500 lbs. in Afterburner
Max Speed  1,525 mph (Mach 2.31) @ 40,000 ft
Service Ceiling  53,000 ft
Wing Span  38 ft. 3½ in. 
Length  70 ft 8.78in
Height  20 ft 3.3in
Weight  23,646 lb. empty, 41,831 lb max
Cost USD  $3,305,435 Initial, $4.7M after MODS
Range  2,700 mi. max fuel w/ext tanks
No. Built  340 (277 'A', 63 'B') 
Armament  AIR-2A (1) AIM-4 (4) M61A1 (1) 
Fire Control System  Hughes MA-1 / IBM Semi-Automatic Ground Environment (SAGE) System
Ejection Seats  
1st Seat  Weber Aircraft Corporation Interim seat, not Zero-Zero, inadequate for supersonic speed ejections. 
2nd Seat  Convair/ICESC (Industry Crew Escape System Committee) Supersonic Rotational B-seat, called the supersonic 'Bobsled'. 
3rd Seat Final  Weber Aircraft Corporation Zero-Zero ROCAT (Rocket Catapult), Zero-Zero, High-altitude supersonic ejections, retro-fitted to all aircraft. 
Mfr. Model #  MK No. 8-24
31-05-2021