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1 - The Black Vault

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PRAETORIAN STARSHIP<br />

that everyone in front of the navigator’s curtain<br />

use NVGs. <strong>The</strong> right-seat pilot flew the approach<br />

with panel lights turned out, while the flight engineer<br />

monitored the engine instruments and the<br />

right-seat pilot’s approach. Both the right-seat pilot<br />

and the flight engineer focused their NVGs<br />

inside the cockpit. To prevent any light bleeding<br />

forward from the navigators’ station, heavy blackout<br />

curtains were installed in place of the thin<br />

dividing curtain used on standard C-130 aircraft.<br />

All lights forward of the curtain were either<br />

turned off or taped to prevent illuminating the<br />

interior of the cockpit. Throughout the approach<br />

the left-seat pilot and the third pilot (safety pilot)<br />

focused their NVGs outside the aircraft and<br />

scanned for the runway environment. At one to<br />

four miles out from landing, the left-seat pilot acquired<br />

the landing lights, the safety pilot confirmed<br />

them, and the left-seat pilot began flying<br />

the aircraft. Airspeed, absolute altitude, and<br />

vertical-velocity information were read to the leftseat<br />

pilot by the right-seat pilot and the left navigator<br />

until the aircraft touched down on the runway.<br />

If no lights were on the runway, the left-seat<br />

pilot usually acquired the runway within a mile of<br />

the approach end, depending on moon illumination<br />

and the brightness of the runway striping. As<br />

the aircraft decelerated through 40 knots after<br />

landing, the landing lights were turned off, and<br />

the aircraft rolled out to its predetermined offload<br />

location. Covert taxi lights were used sparingly<br />

and usually only during turns or in congested<br />

areas. 1<br />

For NVG takeoffs the left-seat pilot maintained<br />

runway alignment with visual reference to the<br />

runway centerline while still using NVGs. <strong>The</strong><br />

right-seat pilot read off the airspeeds as the aircraft<br />

accelerated. On rotation the right-seat pilot<br />

provided the left-seat pilot with the number of<br />

degrees nose-up attitude and the aircraft’s airspeed<br />

on climb out. With the introduction of the<br />

IR filters for the aircraft lights and for the portable<br />

runway lights, Vaught’s requirement for total<br />

blacked-out landings (to the naked eye) was<br />

achieved. 2<br />

Fuel-Cell (Blivet) Airdrop<br />

<strong>The</strong> 8th SOS had initially identified the need<br />

to air-drop fuel to helicopters during the October<br />

1979 Red Flag exercise held at Nellis AFB, Nevada.<br />

When the requirement to refuel helicopters<br />

arose in late November, JTF planners turned to<br />

the air-drop method as their first solution to the<br />

refueling problem. <strong>The</strong> initial blivet drop was<br />

conducted using rigging similar to the CRRC,<br />

with two G-12D parachutes to support a rigged<br />

weight of 3,500 pounds (500 gallons of fuel). As<br />

the number of helicopters were expanded to six,<br />

then later to eight, the number of blivets to be<br />

dropped by each C-130 increased to five. Between<br />

December 1979 and February 1980, the blivet<br />

drop was refined to include all equipment required<br />

to position the blivets and then to pump<br />

fuel to the waiting helicopters. Thus, the standard<br />

five-blivet airdrop included two petroleum,<br />

oil, and lubricant pumps (A-22s) and a small<br />

tractor, called a mule, to move the blivets into<br />

position. <strong>The</strong> total weight of the load was approximately<br />

20,000 pounds. 3<br />

Testing was done on the five blivet loads at<br />

Fort Bragg and at Yuma, Arizona, in December<br />

and in early 1980. Testing confirmed that CDS<br />

procedures provided were the most accurate and<br />

effective means to deliver the heavy load. <strong>The</strong> following<br />

modifications were made to the Combat<br />

Talon to allow for successful CDS air-drops:<br />

1. Additional intermediate rails were installed.<br />

2. A dual CDS gate (strap with cutter blade)<br />

was developed.<br />

3. Retractable VanZelm ratchets were installed.<br />

4. Individual gates were used for each blivet.<br />

Although the fuel blivet air-drop procedure<br />

was not used for the actual mission, the air-drop<br />

option remained the JTF’s first choice until<br />

shortly before mission execution. A secondary<br />

airland method of delivering the blivets also was<br />

developed. Called the blivet combat off-load, it<br />

included modification of the ground-loading<br />

ramps with skate wheels to allow the aircraft to<br />

taxi with the loading ramps deployed. After the<br />

aircraft had landed and taxied to its off-load loca -<br />

tion, each blivet would be released from its restraints<br />

one at a time as the aircraft taxied forward.<br />

After the first blivet was downloaded, the<br />

aircraft would stop, the loadmaster would cut the<br />

second blivet loose, and the aircraft would<br />

resume taxi while the blivet exited the rear of the<br />

aircraft. <strong>The</strong> procedure was repeated until all<br />

blivets were unloaded. At Desert One Fleming’s<br />

crew downloaded three fuel blivets using the<br />

combat off-load procedure. 4<br />

Fuel-Bladder Refueling System<br />

Although airdrop of the fuel blivets proved to<br />

be a viable delivery technique, the Delta Force<br />

commander, Col Charlie Beckwith, did not like<br />

the idea of having to depend on air-dropped<br />

236

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