F-106 DELTA DART

Logo

Lineage History F-106B 590152

Convair
F-106B
590152
1959
271
340 (277 A, 63 B)
1960-06-01
1960-07-01
1991-07-24
unknown
119th,318th,498th,84th,87th
ADWC
Jun 1960 - 271st F-106 produced by Convair at San Diego CA
29 Jul 60 - To 318th FIS, 325th FW, McChord AFB WA
15 Sep 66 - To 498th FIS, 57th FG, Paine Field WA
17 Oct 66 - To 318th FIS, 325th FW, McChord AFB WA
14 Nov 66 - To 498th FIS, 57th FG, Paine Field WA
13 Dec 66 - To 318th FIS, 325th FW, McChord AFB WA
01 Jul 68 - To 318th FIS McChord AFB WA
20 Dec 68 - To 84th FIS, 78th FW, Hamilton AFB CA (TDY/Loan?)
17 Jun 71 - Lightning strike on test hop at 318th FIS McChord AFB WA
16 Dec 71 - In commission after repair by Sacramento ALC CA
30 Dec 71 - To 318th FIS McChord AFB WA
18 Nov 72 - To ADWC Tyndall AFB FL (TDY)
22 Dec 72 - To 318th FIS McChord AFB WA
27 Apr 73 - To 119th FIS/177th FIG Atlantic City NJ (ANG)
16 Jul 73 - To 318th FIS McChord AFB WA (ADC)
21 Aug 74 - To 87th FIS KI Sawyer AFB MI (Loan?)
10 Jan 75 - To 318th FIS McChord AFB WA
01 Oct 79 - Command change from ADCOM to TAC
17 Oct 83 - To 87th FIS KI Sawyer AFB MI
06 May 85 - To Davis Monthan AFB AZ for storage FN087
14 Aug 86 - To Tracor Flight Systems, Mojave CA for drone test/eval
01 Sep 89 - To Tyndall AFB FL as QF-106 AD101 (First drone serial number)
24 Jul 91 - Crashed on 1st NULLO (Dual Hyd failure, lost back-up flight controls)
06-05-1985
FN087
AD101
-
1
No Pilot - Drone Crash
-
-
-
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