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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

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