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The Aircraft

UH-1e's

List of known aircraft Bureau Numbers and Serial numbers

 

Phu Bai... Summer of 68  Photos Courtesy of Gary Zimmerman

 

The Armed UH-IE

  Even before the first UH-IE was delivered to the Marine Corps, suggestions had been made to equip it as an armed helicopter. The Army versions were being manufactured with modifications suitable for a full system of armament. "Bell Helicopter, rather than re-tool, found it cheaper and more advantageous to assemble the Marine UH-IE with identical modifications as those required on the armed version of [the UH- IB/Dl Army helicopters."

  In November 1963, DC/S (Air) reported that "the Army is very enthused with the [UH-IB/Dl as a light weapons fire system," and suggested that 12 aircraft in each VMO should be converted into armed helicopters. The idea, however, became enmeshed in controversy on the role of helicopters as attack air- craft and little progress was made at the time.

  A year later, as SHUFLY continued to report difficulties in conducting assaults without conventional fixed-wing escort aircraft, another attempt to arm the UH-IE was made. The CNO sent a letter on 19 September 1964 to BuWeps stating:

  ... The Marine Corps has an urgent requirement for six Ground Fire Suppression Armament Kits to be in- stalled on the Assault Support Helicopter [UH-IE within the next 60 to 90 days.

  Then, in very precise language, which reflected the difference of opinion within the Marine Corps, he spelled out the reason for his request:

Tactical doctrine requires these helicopters to perform observation, reconnaissance, and rescue missions forward of friendly lines without armed escort. There is no present system of self-defense against ground fire for these helicopters.

  The armament was to be used only for self-defense. No mention was made of escorting assault troop helicopters. The letter went on to request BuWeps to “select equipment, determine the technical feasibility of the complete system and install the selected equipment in six UH-IE helicopters."

  The actual design was to be the responsibility of HMX-1 at Quantico. It had just completed the fabrication of the TK-1 for the UH-34 and had gained experience in modifying guns to fire on helicopters. On 13 October, CMC directed a high priority project to "develop, evaluate, and service test a readily install- able weapons kit for the UH-IE helicopter to provide armed helicopter support for transport helicopters."  The official concept now had been expanded to include escort missions.

 

 

 

   Three different kits were tested. The first, and that which eventually was adopted, was very much like the TK-1. Among the armament features installed in the UH-IE as a result of Bell's common manufacturing process with the Army versions were attaching points to which the Marines fastened a platform on each side of the aircraft. Two electrically fired M-60C machine guns were mounted on each platform, unlike the TK-1, which had guns only on one side. Two bomb racks were bolted on to the bottom of the platforms. Normally 2.75-inch rocket pods were suspended from the bomb racks, though other items could be carried.

  A simple ring and post type of sight was provided which swung up to the top of the cockpit when not needed. To provide the forward point of the sight, a small piece of black tape was placed on the windshield. While the sight seemed crude, it was effective and simple. "Many more elaborate types of sights exist," HMX-1 reported, "but all require major modification of the UH-IE cockpit, introduce added maintenance requirements, or block the pilot's vision."

  The kits, dubbed TK-2, were assembled by the Overhaul and Repair Activity, Jacksonville, Florida, under the technical direction of HMX-1 and the Marine Corps Landing Force Development Center (MCLFDC). A total of 15 were made.

   Test firing at NAS, Patuxent River revealed only minor problems. The most serious was that the expended cartridge links ejected from the left guns could endanger the tail rotor. (The same problem was one of the reasons the UH-34 had no guns on the left side.) The guns were slightly repositioned and later deflector plates were added.

  This apparently solved the ejected link problem. However, on the last day of test firing, several additional nicks in the tail rotor were received. It was decided, in view of the time element, to go ahead with the fabrication of the other kits and continue efforts to solve the ejection problem after the kits were completed and delivered to Fleet Marine Force units. The alternative was to hold up delivery to a deploying squadron."

  On 15 January 1965 the completed armament sets were shipped to VMO-6 at Camp Pendleton. Once in- stalled on the UH-lE’s, they were an immediate success. So much so that on 31 March, CNO requested BuWeps to provide kits for 33 more aircraft. Delivery was promised in July.

  Simultaneously with the development of this TK-2, HMX-1 was experimenting with other kits. Two General Electric .50 caliber SM-14 gun pods were evaluated "with excellent results, providing primarily greater effective range." The added weight made the heavier machine guns suitable only for specialized missions.

   Also tested were two Stoner 63 machine gun pods on temporary loan from the U.S. Air Force. The installation proved unsatisfactory for the UH-IE.

   In addition to the rockets and machine guns mounted on the sides of the helicopter, tests were con- ducted on a rotating turret mounted below the nose of the aircraft. The Emerson Electric TAT-101 turret contained two M-60 machine guns and could be aimed and controlled by the pilot.'14 Beginning in April 1967, UH-lE's were modified to incorporate the turret. A total of 94 kits were purchased. By April 1972, other armament conversions were available which were more suited for the task, and the TAT-101 was removed from those aircraft in which they were installed.

   While the TK-1 on the UH-34 was undergoing final testing at HMX-1 and efforts were under way to have approved a similar kit for the UH-IE, General Krulak at FMFPac sent CMC his estimate of the results, which could be expected. "The proposed arming of the UH- 34 will not provide equivalent protection to replace U.S. Army UH-IB's." The TK-1s, however, should be provided and "the assignment of Marine UH-IE helicopters to the 1st Marine Air Wing be expedited for employment in armed escort as required."  As soon as the pilots at Pendleton finished training, six of the armed UH-lE's were shipped in April to Futenma. These six aircraft of Lieutenant Colonel George Bauman's VMO-2 arrived at Da Nang on 3 May 1965. They immediately began to take over the role of escorting the Marine assault troop helicopters.

   The introduction into Vietnam of Marine armed helicopters did nothing to still the proponents or opponents of the concept. The situation was not helped by a controversy, which during 1964 was becoming increasingly public, between the Air Force and the Army over their respective roles. For airborne fire- power, the Army placed almost total reliance on its armed helicopters. The Air Force held that only its fixed-wing aircraft were suitable for close air support and helicopter escort.

   The Marine Corps occasionally got dragged into the controversy between the two other services. General Greene made a speech at the National Press Club in Washington, D.C. on 26 March 1964. In it, he once again stated his position on armed helicopters. Press accounts, unfortunately, were written stressing that the "Marines Join Air Force in Opposing Helicopters Ground Support"

   He had made no such statement. What General Greene told the reporters was the same thing he had been telling and would continue to tell the Marines-

   “This service [armed helicopters in South Vietnam has been carried out under peculiar circumstances which has led many people to question the Marine Corps' position and has resulted in some misunderstanding of it.   The special situation in South Vietnam has not caused us to modify our belief .  In South Vietnam, Marine Corps tactical fixed wing aircraft have not been available because of political considerations.”

   He summed up. "We consider this capability (armed helicopters] must be complementary, rather than competitive with the primary fire support provided by fixed wing aircraft.

   Marine attack aircraft, after they were introduced into Vietnam, were used to protect and escort the assault helicopters. So were armed helicopters. Each in its way performed a vital mission. Throughout the conflict in Vietnam, the Marine Corps continued to maintain a balance of weapons which were capable of performing anywhere in the world under almost any conceivable circumstance. The armed helicopter and fixed-wing attack aircraft were just two of them. Much of the credit belongs to General Greene. He, at least, had not forgotten the lessons of previous wars. ("Marines and Helicopters 1962-73" Lt Col. William R. Fails   USMC")

Photo courtesy Jim Kennedy VMO-3

 

COBRAS

 

 

 

AH-1G

Photo courtesy of Dennis Bevis

 

UH-1N

Here is one of the first UH-1N's in 367. This is a photo of one of the Hueys on final to landing in mainland Japan in 1977. Photo Courtesy Steve Hornberger

Specifications

Primary function Utility helicopter
Manufacturer Bell Helicopter Textron
Power plant Pratt and Whitney T400-CP-400
Power Burst: 1290 shaft horsepower (transmission limited)
Continuous: 1134 shaft horsepower (transmission limited)
Length 57.3 feet (17.46 meters)
Height 14.9 feet (4.54 meters)
Rotor Diameter 48 feet (14.62 meters)
Speed 121 knots (139.15 miles per hour) at sea level
Ceiling 14,200 feet (4331 meters)
(limited to 10,000 feet (3050 meters) by oxygen requirements)
Maximum takeoff weight 10,500 pounds (4,767 kilograms)
Range 172 nautical miles (197.8 miles)
Crew Officer: 2
Enlisted: 2
Armament
  1. M-240 7.62mm machine gun or
  2. GAU-16 .50 caliber machine gun or
  3. GAU-17 7.62mm automatic gun
    All three weapons systems are crew-served, and the GAU-2B/A can also be controlled by the pilot in the fixed forward firing mode.
  4. The helicopter can also carry two 7-shot or 19-shot 2.75" rocket pods.
Introduction date 1971
Unit Replacement Cost $4,700,000
Marine Corps Inventory 107

 

 

 

AH-IW

VT-35 on UDP in Okinawa. 27 Aug 1998  Photo Courtesy Steve Hornberger

 

Specifications

Contractor: Bell Helicopter TEXTRON, Inc. (Prime), General Electric, Kollsman Inc.
Power Plant:
  1. Two General Electric T700-GE-401 Turboshaft engines
  2. Each engine delivers 1,690 horsepower.
Accommodations:
  1. Two seats, in tandem (pilot in rear, copilot/gunner in front)
Performance:
  1. Climb rate: 1,925 feet per minute
  2. Maximum altitude: 14,750 feet
  3. Maximum attainable speed: 170 knots (195 mph)
  4. Maximum cruising speed: 152 knots (173 mph)
Countermeasures:
  1. AN/ALE-39 Chaff system and SUU-4/1 Flare dispensers
Armament:
  1. One M197 three barrel 20 mm gun (mounted under the nose with 750 round ammo container)
  2. Underwing attachments for four TOW missiles, eight Hellfire missiles, or one AIM-9L Sidewinder missile
  3. Can also be equipped with Zuni rocket launchers

External Dimensions

Main rotor diameter 14.63 m
Main rotor blade chord 00.84 m
Tail rotor diameter 02.97 m
Tail rotor blade chord 00.305 m
Distance between rotor centers 08.89 m
Wing span 03.28 m
Wing aspect ratio 03.74
Length: overall, rotors turning 17.68 m
Length: fuselage 13.87 m
Width overall 03.28 m
Height (to top of rotor head) 04.11 m
Overall height 04.44 m
Ground clearance, main rotor, turning 02.74 m
Elevator span 02.11 m
Width over skids 02.24 m

Areas

Main rotor blades (each) 006.13 m2
Tail rotor blades (each) 000.45 m2
Main rotor disc 168.11 m2
Tail rotor disc 006.94 m2
Vertical fin 002.01 m2
Horizontal tail surfaces 001.41 m2

Weights and Loadings

Weight empty 004.634 kg
Mission fuel load (usable) 946 kg
Maximum useful load (fuel and disposable ordinance) 002.065 kg
Maximum Takeoff and landing weight 006.690 kg
Maximum disc loading 039.80 kg/m2
Maximum power loading 004.42 kg/kW

Performance (At Maximum T-O weight, ISA)

Never exceed speed (Vne) 190 knots
Maximum level speed at S/L 152 knots
Rate of climb at S/L, OEI 244 m/minute
Service ceiling More than 4,720 m
Service ceiling, OEI More than 3,660 m
Hovering ceiling
IGE
4, 495 m
OGE
915 m
Range at S/L with standard fuel, no reserves 317 nm

If any of you guys have data for these aircraft let us know.

Known Bureau Numbers (and ARMY Serial Numbers for the Cobra’s) in VMO-3 and HML-367 in Vietnam Help!

1966-1971

Bureau Numbers MODEX Squadron Last Seen Notes
151879   HML-776, HT-18 1986 Aberdeen Ranges as Target
152426     1993 AMARC
152438 VT-12 HML-367 10/10/1969 Combat Loss (KIA)
152476        
153371        
153742   VMO-3 01/18/1968 Combat Loss at sea (KIA)
153743        
153745     1986 Stockton, CA
153750 VT-4      
153751        
153754   HML-367, HT-18 1979  
153757   VMO-3 11/14/1967 Combat Loss (KIA)
153758        
153764     10/10/69 Combat Loss
153765       N67RF Civil Registry (not today)
154337        
154699        
154751        
154752        
154754   HML-771 (QK-413) May-90 AMARC 5/90
154756        
154757   HML-367, HT-18 1979 AMARC 5/90
154762     01/12/1969 Lost in denied area west of K sahn
154765        
154766        
154770        
154773        
154774     May-90 AMARC 5/90
154775   HML-367 (UV-19)   AMARC
154778     Jun-86 GRD Instruction Chanute TTC 6/86
154780        
154954        
154955        
154963   HML-367 09/17/1968 Combat Loss (KIA)
154966        
154969        
155339   HML-367 08/09/1969 Combat Loss (KIA)
         
UH-1E's Built By BN    
151266  to 151299 33    
151840  to 151887 47    
152416  to 152439 23    
153740  to 153767 27    
154730  to 154749 19    
154750  to 154780 30    
154943  to 154969 26    
    205    
         
         
         
AH-1G Serial's MODEX Squadrons Last Seen Notes