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E-2A / E-2C Hawkeye


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For a straight E-2C (Group 0, 1, 2 or 2+): Shape of the nose, flat antenna's on the outer vertical stabs and the tail, canoe faring on the lower right side of the fuselage, radio antenna configuration. Depending on the time frame, SATCOM nipple on the dome and a stormscope antenna under the tail.

For an E-2C G2/G2+: GPS puck on top of cockpit

For and E-2C Hawkeye 2000: all of the above, except the refractometer is deleted (bong looking thing on the cockpit roof), radio antenna configuration is changed again, added the "trashcan" antenna under the fuselage, the trailing wire HF antenna is deleted and the SATCOM nipple is upgraded to a Fez looking thing.

HTH

Spongebob

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Lower?

Yep. It seemed a good idea in 1960 when there were fewer big carriers around. E-2As could do it, the feature was deactivated when they were converted to E-2Bs and deleted in the E-2C.

How'd it work? The upper section of the pylon fairing was built in left and right sections. To stow, the sections folded down, and the radome was hydraulically lowered. No more difficult than folding the wings. The movable section of the pylon fairing was only the upper two or so feet of the assembly - about where you see the black leading edge on the E-2B photo that Dave posted above. That brought the top of the radome below the tips of the vertical stabilizers, which was all that was needed.

HTH,

Craig

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So, the differences are in nipples, trashcans, pucks, bongs, and Fezs?
In other words kinda like choosing a stripper for a lapdance...
I thought I remember hearing something once about it squatting slightly for stowage clearance issues

Another quality to look for.... ;)

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How exactly does the rotodome lower, BTW?

Like so much other stuff, it's a result of the original RFP. It stated that the aircraft had to be able to operate from SCB-27C modified Essex class carriers and newer. Because of the limited Hangar overhead, the dome needed to be lowered by 3 ft. In addition, the limited elevator size necessitated the wing-fold system, the deck strength and aircraft weight of no more than 52k lbs and the less-than-aerodynamically-stable correct length (the E-2 is 10ft short of ideal which causes a divergent pitch oscillation in the approach configuration (gear/flaps down)). During testing, initial CQ for the E-2A was done on the Lexington.

After the E-2A proved to be a useless hunk of FOD operationally, "they" made the decision to place the E-2B squadrons onto Midway and newer carriers, so the rotodome system was sort-of removed (it was still listed in the E-2C NATOPS as of 2003 along with the Essex class clearance.)

HTH

Spongebob

Edited by Spongebob
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Aha! I knew I had this filed.

E-2A BuNo 149818, July 1964. Spongebob might recognize this corner of Pt. Mugu's Hangar 553. (Navy Photo)

It turns out that the fairing splits into four sections, two per side.

12img329.jpg

Of course you could just go topless over Long Island...

W2F-1 BuNo 149149 (aircraft #2) January 1962 (Grumman Photo)

12img330.jpg

It is very difficult to see, but this aircraft is trimmed with da-glo orange.

HTH,

Craig

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