Lineage History F-106A 590125

Manufacturer:

Convair

Model:

F-106A

USAF S/N:

590125

Production Year:

1959

Production C/N No.:

311

No. Built

340 (277 A, 63 B)

Production Date:

1960-09-01

Delivery Date:

1960-10-01

Ended Service:

1971-11-07

Airframe Hours:

unknown

Units Assigned:

456th,498th,84th

History Lineage:

Sep 1960 - 311th F-106 produced by Convair at San Diego CA
30 Nov 60 - To 456th FIS Castle AFB CA
08 May 63 - To 498th FIS, 325th FW, McChord AFB WA
14 Jun 66 - To 498th FIS, 57th FG, Paine Field WA
30 Sep 68 - To 84th FIS, 78th FW, Hamilton AFB CA
01 Jan 70 - To 84th FIS, 1st FW, Hamilton AFB CA
01 Oct 70 - To 84th FIS Hamilton AFB CA
07 Nov 71 - Crashed after mid-air with an F-4, pilot Maj. Clifford L. Lowrey ejects eight miles NE of base, survived.

Crashed near Nellis AFB NV. A USAF McDonnell Douglas F-4 Phantom II and F-106A 59-0125, of the 84th FIS, Hamilton AFB, California, suffer mid-air and crash in isolated areas near Nellis AFB, Nevada. All three crew eject and survive. F-4 crew, Maj. Henry J. Viccellio and Maj. James A. Robertson, okay. Phantom comes down 35 miles from Caliente, Nevada, Delta Dart attempts recovery to Nellis but pilot Maj. Clifford L. Lowrey ejects eight miles NE of base

AMARC Storage PCN ID No.:

QF Drone Conversion:

QF Drone ID No.:

QF Drone Shotdown:

Shotdown By:

QF Drone Lost on Nullo No.:

Deployed to Osan AB Korea:

B-1B Chase Plane:

Crash

Crew Ejected:

Crew Survived:

Crew Killed:

Pilot Front / Pilot Rear:

Pilot Rear:

Accident Report No:

Destroyed:

Written-Off:

Survivor:

Static Display Painted As:

Instruments - TAC Conventional:

TAC Conventional: Models produced with Tactical 'Round Eye' instruments.

Instruments - Conventional:

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

Instruments - TEST-to-TACTICAL:

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..

Instruments - Vertical, 1st Produced:

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

Instruments - Tactical Vertical:

Last Update:

31-05-2021

Back to list

F-106 DELTA DART

Lineage History F-106A 590125