F-106 DELTA DART
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Convair
F-106A
572484
1957
89
340 (277 A, 63 B)
1959-07-01
1959-12-28
1961-09-14
unknown
498th
Jul 1959 - 89th F-106 produced by Convair at San Diego CA
29 Jul 59 - To 498th FIS Geiger Field WA 01 Dec 60 - To 498th FIS. 84th FG, Spokane IAP WA 14 Sep 61 - Crashed on second approach near Geiger having been waved off during the first approach due to conflicting traffic on the runway. 1st Lieutenant Russell C. Wood, 28, ejected at low altitude (700 ft) Parachute did not have time to fully deploy and was killed. On the morning of September 14, 1961, First Lieutenant Russell C. Wood briefed for a routine target mission. This would likely have been an intercept of a B-52 training in the area. Given the location of SAC bases, the B-52 could have been from Larson AFB, Fairchild AFB, or any number of other bases in the Northwest (Idaho, Montanna...etc.). It could have also been an intercept of an EB-57 , which was used to test the Air Defenses of the Continental US, though, I believe that to be unlikely. From what I understand the EB-57s were used for training and checking the radar systems and operators, not necessarily the ADC fighters. Airman second class Kenneth D. Hintz accompanied Wood on his walk around of F-106A #57-2484. There were no discrepancies and Hintz secured the access panels while Wood strapped in. One combustion start was attempted with no success, but a pneumatic start worked at 0915. The MA-1 power system timed in and they made various checks, then Wood taxied to the ramp. He was airborne a 0926, 6 minutes after the proposed time. Estimated fuel on-board was 8900 pounds. Wood made a left turn out of traffic and began his climb on a heading of 326. The proposed flight plan was "Geiger direct 52 degrees N. 122 degrees W. (William's Lake B.C.) direct Larson TACAN, direct Spokane VORTAC." That looks like a trip to the North East to British Columbia, a turn to the South West back to Larson, then a turn to the East to end up back at Spokane. The F-106 on the same flight profile and plan 1/2 hour behind heard his check-ins via radio, but no ground stations did. It was not until he was over the Larson TACAN at 1038 at FL480 (48,000 feet) that Spokane Center heard from him. He then contacted Spokane Approach Control and was positively identified on radar (No difficult feat considering there probably were not many other aircraft at FL480) and "he was cleared to the 35 mile fix of the Spokane VORTAC, report inbound." (VORTAC stands for: VHF Omnidirectional Range/Tactical Aircraft Control) He reported over the fix at FL200. He was instructed to report once he passed FL70. At 24 miles he was advised of traffic, a DC-6, at 14 miles West of VORTAC. At 15 miles he was devised to begin his landing cockpit check. He reported when he passed through 7000 feet, and requested a "surveillance approach to runway 03." He was told to level off at 4000 feet and he acknowledged. Again he was advised of traffic, and told to "prepare to start his descent in 4 miles." He then told RAPCON (Radar Approach Control) that he would have to break off this approach, but they did not respond. He continued his approach, then was told to start his descent. Twelve seconds later he was told to maintain 4000 feet and turn right to 150 because of traffic. He reported steady on 150, and then was told to turn to 205 and maintain 4000. 30 seconds later the tower observed him continue turning past 205. They asked if he was continuing this approach on his own, to which he replied, "Negative, I would like a surveillance approach to runway 03." They told him to stop his turn and then proceeded to give him a "no-gyro" approach. At 5 miles he was told to begin his descent. Radar contact was lost at three miles, which was normal considering ground clutter. The aircraft crashed 2.4 miles from the runway on a heading of 063 degrees true. The smoke was observed from Spokane Tower at 1102. Wood ejected, but unsuccessfully from an altitude of 200-500 feet above the ground. The report ends with the summation that there was no indication of emergency from Wood. It does not state what caused the crash. It does not go into anything else. Simply the flight description. This, in the my world of aircraft accident reports, is annoying, since others generally have a page where a determination of cause is surmised if it isn't known. As an unqualified observer from almost 50 years on, I offer my supposition that it may have been possible for his J-75 to flame out. I don't know what would have caused a flame-out, though. Perhaps he retarded the fuel flow for a moment or there was a stuck valve. Did he suffer a bird strike? Until the rest of the report is released or someone comes forward with a better idea, that is what we are left with. The picture of the crash site and this ground track are all that is included with this report. On the map you can make out the B-52 and KC-135 shapes to the left where Fairchild is, and the F-106 and civil aircraft shapes at Spokane International.
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1Lt Russell C. Wood
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610914003
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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.. Tactical Vertical: Models factory produced w/Tactical Vertical instruments: late 1957 and all 1958, 1959.. F-106 Specifications
31-05-2021
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