1 - The Black Vault
1 - The Black Vault
1 - The Black Vault
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0428 local, made its tactical landing at Cubi Point<br />
NAS at 0506, onloaded its personnel, and departed<br />
at 0508. <strong>The</strong> AFSOB ground radio station received<br />
an operational normal call at 0514 local. <strong>The</strong> last<br />
transmission received from the aircraft was at 0521<br />
and did not indicate that the crew was having any<br />
problems. At 0523, 15 minutes after the second<br />
takeoff, local fishermen near Capones Island, located<br />
northwest of Cubi Point NAS, observed the<br />
aircraft impact the water and explode. After approximately<br />
10 minutes, the wreckage sank in 240<br />
feet of water. Twenty-three people were killed on<br />
impact, with Lieutenant Blohm, the electronic warfare<br />
officer and lone survivor, being thrown from<br />
the aircraft and rescued by local fisherm en. 38<br />
Postaccident investigation could not determine<br />
the exact cause of the crash, but the most probable<br />
explanation was thought to be fatigue brought on by<br />
the stress of the previous year’s activities. <strong>The</strong> op -<br />
eration’s tempo during preparations for the Iranian<br />
rescue mission coupled with the recent move to<br />
Clark AB had taken its toll on the squadron. <strong>The</strong><br />
administrative flight on the 25th of February also<br />
had interrupted the crew’s circadian rhythm cycle,<br />
thus resulting in degraded crew rest before the mission.<br />
A second possible cause of the accident was a<br />
malfunctioning terrain-following radar system. <strong>The</strong><br />
system was designed to convert to a “radar override”<br />
condition when the aircraft was over water,<br />
and there were no returns from the water’s surface.<br />
Engineers theorized that if the system did not enter<br />
the override mode, the radar could fly the aircraft<br />
into the water without any radar reference available<br />
to determine the aircraft’s altitude.* One of<br />
several modifications made to the Combat Talon<br />
stemming from the accident provided a warning<br />
light that told the crew when the aircraft was in<br />
radar override. Personnel from the 1st SOS killed in<br />
the 26 February 1981 crash of aircraft 64-0564 were<br />
Maj James M. Kirk, Capt Norman L. Martel, Capt<br />
Thomas D. Patterson, Capt Gregory S. Peppers, TSgt<br />
Stephen A. Blyler, TSgt Barry R. Chumbley, TSgt<br />
Gary W. Logan, and SSgt John T. Felton. 39 **<br />
Post–Desert One<br />
Advancements for Combat Talon<br />
Since the failed Desert One rescue attempt, the<br />
special operations community had made huge advancements<br />
in both hardware procurement and<br />
tactics development. During Honey Badger both<br />
USAF and US Army rotary-wing capabilities<br />
PROJECT HONEY BADGER AND CREDIBLE SPORT<br />
received the most attention, thus resulting in a<br />
much superior helicopter capability than the US<br />
military had in November 1979. For Combat Talon<br />
the advancements made before Desert One continued<br />
during Honey Badger, and important tactics<br />
were developed and refined to allow the weapons<br />
system to better accomplish the difficult counterterrorism<br />
mission.<br />
<strong>The</strong> tactic of determining if a runway were clear<br />
using the Combat Talon FLIR was perfected early<br />
in the Desert One training period, but the ability<br />
to clear the runway if something heavy were<br />
blocking it still needed to be solved. A solution was<br />
found by developing drop procedures to deliver<br />
either a 15,000-pound or 25,000-pound bulldozer<br />
to be used to remove any runway obstruction. If<br />
the FLIR pass determined that the runway were<br />
blocked, a Combat Talon could air-drop the bulldozer<br />
and a combined team of US Army rangers<br />
and USAF CCT personnel. <strong>The</strong> rangers would use<br />
the bulldozer to clear runway obstructions. Once<br />
the runway was clear, the CCT would provide air<br />
traffic control for follow-on aircraft to la nd. 40<br />
Another challenge for planners was to airland as<br />
many aircraft as quickly as possible on an airfield<br />
so that the maximum number of soldiers could be<br />
inserted in the shortest time. A tactic known as<br />
dual-runway operations was developed that fulfilled<br />
this requirement. 41 Flying in formation the Combat<br />
Talon lined up on the primary runway in pairs and,<br />
at a preplanned point, would spread apart so that<br />
the wingman was aligned with the parallel runway.<br />
Both aircraft would touch down on each runway at<br />
the same time. Follow-on aircraft would employ the<br />
same tactic, with a 30-second spacing between landings<br />
on the same runway. Thus, within a 60-second<br />
span as many as six aircraft could land on two parallel<br />
runways. To arrive in formation at the prescribed<br />
time and with the proper spacing, proce -<br />
dures were refined that allowed the aircraft to use<br />
its air-to-air TACAN and the SST-181 beacon to<br />
maintain spacing, whether in weather or in the<br />
clear. Complex procedures were also developed to<br />
allow for lead change and formation breakup/rejoin<br />
should the situation arise.<br />
A unique tactic that was also developed during<br />
Honey Badger was the transport of a small helicopter<br />
that was off-loaded from the Combat Talon,<br />
assembled, and flown away to support the ground<br />
force tactical plan. Six OH-58s were originally<br />
modified with short struts to allow rotor-head<br />
__________<br />
*<strong>The</strong> theory was confirmed two years later when an LAS Ontario test crew observed a continual fly-down command by the TF radar while flying<br />
over water. <strong>The</strong> test was terminated when the aircraft descended to 100 feet.<br />
**Peppers and Felton flew to Desert One on 24 April 1980.<br />
249