F-106 DELTA DART

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Lineage History F-106B 572529

Convair
F-106B
572529
1957
95
340 (277 A, 63 B)
1959-07-01
1959-12-28
1966-04-21
unknown
539th
AFFTC,AFSC,SA-AMC
Jul 1959 - 95th F-106 produced by Convair at San Diego CA
13 Aug 59 - To 539th FIS McGuire AFB NJ (Later deployment to Tyndall AFB FL)
31 Aug 62 - To 6515th Organizational Maintenance Squadron, AF Systems Command, Edwards AFB CA
30 Sep 64 - To AF Flight Test Center (AFSC), Edwards AFB CA
28 Apr 66 - To NF-106B
30 Mar 67 - To Martin Company, Baltimore MD
07 May 68 - To AF Flight Test Center (AFSC), Edwards AFB CA
21 Oct 71 - To 552nd Airborne Early Warning Wing (ADC), McClellan AFB CA
13 Feb 72 - To Sacramento Air Logistics Area, McClellan AFB CA
14 Sep 76 - Dropped from inventory as surplus

While at the Martin Company in Baltimore, both F-106B 57-2519 and F-106B 57-2529 supported a flight simulation program designed to replicate flight characteristics (for the back seat pilot) of different kinds of aircraft, like the Martin X-23, X-24A & X-24B lifting bodies and space re-entry vehicles. In March 2004 I got confirmation e-mails from two retired Convair Reps, Jim Day & Joe Sylvia. On 09 Jan 2007 I got an e-mail from Don Ward, a pilot involved with the flight simulation program.

Both 57-2519 and 57-2529 were put in storage as NF-106Bs at McClellan AFB CA in the early 70s. In the mid 70s, it was decided to use the two NFs to repair crash damaged aircraft, so the NFs were declared surplus.
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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
07-10-2022