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B-17 E-Z Goin’ and the Sonderkommando Elbe – Buchen Raid

Laurence J. Lazzari Crew
Kneeling L to R: Sgt. Laurence W. Donnelly (BTG), T/Sgt. Robert J. Steele (ROG), 2nd Lt. Charles W. Staiger (NAV)Sgt. Joseph G. Allen.  Standing L to R: Sgt. Richard H. Heritage (NG/TOG), T/Sgt. Charles A. Weiss (TTE), 2nd Lt. Laurence J. Lazzari (P),
2nd Lt. Guiher G. Greenwood (CP), 2nd Lt. Daniel J. O’Connell, Jr. (TG).
100th BG Photo Archives

This website recently received a comment from USAF Colonel Guiher G. Greenwood (retired) who served with the 351st Bomb Squadron, 100th Bomb Group, regarding a picture posted in our gallery. He identified the plane pictured as that of the B-17 E-Z Goin’ piloted by Joe Martin with co-pilot Henry Cervante on the Buchen raid of April 7, 1945. Interestingly, Col Greenwood and Joe Martin lived through one of the more infamous “suicide” attacks by the Germans in their last desperate days of the war.

The Sonderkommando Elbe was a special squadron of the German Luftwaffe, a Luftwaffe task force assigned to bring down Allied bombers by ramming German aircraft into the Allied bombers. Sonderkommando means special command, and Elbe is a river that runs through Germany to the North Sea. The Sonderkommando Elbe was formed at Reichmarschall Hermann Goering’s insistence that the Reich’s defense units should start ramming bombers as a last resort. This group of fighters was not solely tasked with ramming bombers, but that was their last ditch option. In theory this was not a suicide mission, they were only supposed to ram an Allied bomber if there was a chance to bail out alive. Unlike the Japanese kamikaze pilots, the inexperienced German pilots brought a parachute with them while flying their striped-down Messerschmitt Bf 109′s, if the pilot survived the collision, he could use the parachute.

The only documented mission, often called Rammkommando Elbe (ramming) or Werewolf, was on April 7, 1945 when a total of 120 pilots took off in their fighters and attacked several formations of U.S. bombers heading towards the Germany heartland. These young German pilots were motivated to destroy Allied bombers by any means necessary, they had seen their country decimated by the relentless Allied bombing campaign. Although the Luftwaffe had an amply supply of airplanes, even in April 1945, they lacked trained pilots and aviation fuel. Many of the Sonderkommando pilots had only 50 hours of training, and their lack of experience was as likely to get them killed as the P-51 Mustangs that protected the Bomber Armada.

This last ditch effort of the mighty Luftwaffe resulted in only 15 Allied bombers attacked with eight successfully destroyed. Several planes barely limped back to base, these included the E-Z Goin’ flown by Joe Martin’s crew. Their left stabilizer was ripped off, and the rudder substantially damaged. In addition to having little control of the plane, they also lost engine #1. Somehow the crew was able to return to England, and landed successfully.

Related Articles:

Rammkommando – German Kamikaze, WWII
TARGET: BUCHEN GERMANY, 7 APRIL 1945- G. GENE GREENWOOD
Rammkommando “ELBE”
The Boeing B-17 Flying Fortress

Lockheed Martin F-16 Fighting Falcon

The U.S. Air Force officially named the F-16 “Fighting Falcon” on July 21st, 1980, during a ceremony at Hill AFB in Utah.

The F-16 Fighting Falcon is a compact, multi-role fighter aircraft. In the air combat role, the F-16′s maneuverability and combat radius exceed that of all potential enemy fighter aircraft. It can locate targets in all weather conditions and detect low flying aircraft in radar ground clutter. In the air-to-surface role, the F-16 can fly over 500 miles, deliver its weapons accurately, defend itself, and return to base. An all-weather capability allows it to accurately deliver ordnance during bad weather or at night. With a full load of internal fuel the F-16 can withstand up to 9G’s, it’s likely the pilot will fail before the airframe does.. The bubble cockpit canopy gives the pilot unobstructed vision forward and upward and much improved vision over the side and rear.

The F-16 first flew in December 1976. The first operational F-16A was delivered to the 388th TFW at Hill AFB, Utah in January 1979. The two-seat version, the F-16B, has two cockpits each about the same size as the single ‘A’ version cockpit. To make room for the second cockpit the forward fuselage fuel tank and avionics growth space is reduced.

The Falcon was one of the first to use the now standard fly-by-wire control system whereby no direct mechanical link is provided, instead the pilot’s controls communicate with the F-16 ‘s electronics which in turn move the aircraft’s flying surfaces. This system requires a side-mounted control stick instead of the conventional between the knees joystick that came as standard with combat planes since the beginning, needed for better control during the high-G maneuvers the plane can fly.

To simplify and cut the cost of development and production of the Falcon, some existing and proven systems from other USAF aircraft were adapted for it’s use. Parts used in the earlier F15 Eagle and the old swing wing F111 fighter bomber found a home in the aircraft. Unusually the F16 Falcon has a single engine instead of two. While cutting the cost of the aircraft and also maintenance time it does always increase the chance of a ‘dead stick landing’, however the F16 has proven reliable in the field.

The Lockheed Martin F-16 Fighting Falcon, the first of the US Air Force multi-role fighter aircraft, is the world’s most prolific fighter with more than 2,000 in service with the USAF and 2,000 operational with 23 other countries.

Lockheed Martin F-16 Fighting Falcon

Specifications
Primary Function Multi-role fighter
Builder Lockheed Martin Corp.
Power Plant F-16C/D:
one Pratt and Whitney F100-PW-200/220/229 or
one General Electric F110-GE-100/129
Thrust F-16C/D, 27,000 pounds(12,150 kilograms)
Length 49 feet, 5 inches (14.8 meters)
Height 16 feet (4.8 meters)
Wingspan 32 feet, 8 inches (9.8 meters)
Speed 1,500 mph (Mach 2 at altitude)
Ceiling Above 50,000 feet (15 kilometers)
Maximum Takeoff Weight 37,500 pounds (16,875 kilograms)
Combat Radius [F-16C] 740 nm (1,370 km) w/
2 2,000-lb bombs + 2 AIM-9 + 1,040 US gal external tanks
340 nm (630 km) w/
4 2,000-lb bombs + 2 AIM-9 + 340 US gal external tanks
200 nm (370 km) + 2 hr 10 min patrol
w/ 2 AIM-7 + 2 AIM-9 + 1,040 US gal external tanks

Range Over 2,100 nm (2,425 mi; 3,900 km)
Armament One M-61A1 20mm multibarrel cannon with 500 rounds; external stations can carry up to six air-to-air missiles, conventional air-to-air and air-to-surface munitions and electronic countermeasure pods.

Fabrica Militar de Aviones IA 58 Pucará

FMA IA 58 Pucará
The FMA IA 58 Pucará (Quechua: Fortress) is a two-seat light attack aircraft powered by two turboprop engines. It was designed for the COIN (counterinsurgency) and CAS (close air support) roles for the Argentine Air Force. A low-wing monoplane of all-metal construction, with a retractable landing gear, it was manufactured by the Fabrica Militar de Aviones. It has narrow fuselage and tail section and a tandem seat cockpit with a steep sloping nose. Although heavily armed the weapons are unguided and visually aimed by the crew. The IA 58 only needs a minimum of ground support to operate; it is able to operate from unprepared rough terrains.

Named after a form of South American stone hill fortress, the Pucara’s origins can be traced back to the mid-1960′s when Argentina’s Fabrica Militar de Aviones ( Military Aircraft Factory ) was requested to develop a new combat aircraft capable of performing COIN, CAS and reconnaissance missions. The first flight of the prototype AX-2 Delfin, powered by a pair of Garrett TPE331-U-303 turbo props, took place on 20 August 1969. Subsequent prototypes were re-engined with French Turbom Eca Astazou XVIG turboprops.

The Pucara was designed to operate from rough field and unprepared sites with the minimum of ground support – a point it proved to good effect during the Falklands War of 1982. Operations are possible by night, but not in adverse weather conditions, and weapons aiming is achieved visually by the pilot making full use of the excellent forward visibility over the Pucara’s downward sloping nose.

The IA 58A is the main production variant of the Pucará design. About 108 aircraft were built for Argentina of which 6 were sold to Uruguay. About 3 aircraft were captured by the United Kingdom during the Falkland War, they are now preserved by the RAF. The production standard IA 58A first flew on 8 November 1974, with deliveries to the Argentinean Air Force commencing just over a year later.

The IA 58B is basically a IA 58A with 30mm cannons in place of the 20mm cannons present in the A model. Although a prototype has been developed, none were produced.

The IA 58C is a multi-role single-seat version of the Pucará. The changes included the addition of a Head-up Display, IFF (identification friend of foe), 30-mm DEFA 553 cannons in the nose, two extra hard points for Magic 2 Air-to-Air missiles and additional weapons capability, including Martin Pescador anti-ship missiles.

The IA 66 prototype was a IA 58A model fitted with 1,000-shp Garrett TPE331-11-601W turboprops, none were produced.

However, overall production figures have been modest at best, with exports to Uruguay, Sri Lanka and Colombia accounting for less than 20 aircraft in total

Specifications
Country of Origin Argentina
Wing Span 14.5m ( 47 ft 7 in )
Length 15.25 m ( 46ft 9in)
Height 5.36m ( 17ft 7 in )
Weight empty, equipped 4,037 kg ( 8,900 lb );
MTOW 6,800 kg ( 14,991 lb )
Engine two 988 shp Turbomeca Astazou XVIG turboprops
Maximum speed 500 km/h ( 311 mph ) at 3,000 m ( 9,840 ft )
Cruising speed 430 km/h ( 267 mph )
Service Ceiling 9,700 m ( 31, 825 ft )
Armament two Hispano HS804 20mm cannon each with 270 rpg, four FN Browning 7.62 mm cannon with 900 rpg; up to 1500 kg ( 3,307lb ) of free fall bombs, napalm tanks, 70 mm ( 2.75 in ) rockets, cannon pods, two auxiliary fuel tanks.
Role: counter insurgency, close air support, light attack
Builder: Fabrica Militar de Aviones (FMA)
Variants: IA 58A, IA 58B, IA 58C, IA66
Operators: Argentina, Colombia, Sri Lanka, and Uruguay

Click the picture for even more great Pucará pictures!
FMA IA 58 Pucará

Lockheed Martin F-22 Raptor

F-22 Raptor

The F-22A Raptor is a next-generation fighter/attack aircraft that features the latest stealth technology to reduce detection by radar. Using more advanced engines and avionics than the current F-15 Eagle, the F-22A is intended to maintain U.S. Air Force capabilities against more sophisticated enemy aircraft and air defenses in the 21st century.

The Raptor combines stealth, maneuverability and the ability to fly long distances at supersonic speeds — or “super cruise” — in performance of air superiority and air-to-ground missions. Furthermore, it requires less maintenance than older fighters. These capabilities represent an exponential leap in war fighting capabilities.

In 1981 the U.S. Air Force needed a new air superiority fighter that would take advantage of new technologies in fighter design including composite materials, lightweight alloys, advanced flight control systems, higher power propulsion systems and stealth technology. Lockheed Martin’s F-22 won the design competition in April 1991, and the rollout ceremony for the first F-22 Raptor occurred in April 1997.

The Raptor successfully completed its initial operational and test evaluation in 2004, and the program received approval for full rate production. In December 2005 operational aircraft were designated F-22As.

Production of the F-22A is a partnership between Lockheed Martin, Boeing and Pratt & Whitney. Boeing builds the Raptor’s wings and aft-fuselage; the engines come from Pratt & Whitney, and Lockheed Martin builds the forward fuselage and assembles the subsections in Marietta, Ga.

On May 12, 2005, the Raptor program achieved a historic milestone with the delivery of the first combat-capable Raptor to the 27th Fighter Squadron, 1st Fighter Wing, at Langley Air Force Base, Va. In January 2006 the 27th Fighter Squadron flew the first operational mission with the F-22 in support of Operation Noble Eagle (the official name given to the defense of U.S. borders).

A combination of sensor capability, integrated avionics, situational awareness, and weapons provides first-kill opportunity against threats. The F-22A possesses a sophisticated sensor suite allowing the pilot to track, identify, shoot and kill air-to-air threats before being detected. Significant advances in cockpit design and sensor fusion improve the pilot’s situational awareness. In the air-to-air configuration the Raptor carries six AIM-120 AMRAAMs and two AIM-9 Sidewinders.

The F-22A has a significant capability to attack surface targets. In the air-to-ground configuration the aircraft can carry two 1,000-pound GBU-32 Joint Direct Attack Munitions internally and will use on-board avionics for navigation and weapons delivery support. In the future air-to-ground capability will be enhanced with the addition of an upgraded radar and up to eight small diameter bombs. The Raptor will also carry two AIM-120s and two AIM-9s in the air-to-ground configuration.

Advances in low-observable technologies provide significantly improved survivability and lethality against air-to-air and surface-to-air threats. The F-22A brings stealth into the day, enabling it not only to protect itself but other assets.

The F-22A engines produce more thrust than any current fighter engine. The combination of sleek aerodynamic design and increased thrust allows the F-22A to cruise at supersonic airspeeds (greater than 1.5 Mach) without using afterburner — a characteristic known as super cruise. Super cruise greatly expands the F-22A ‘s operating envelope in both speed and range over current fighters, which must use fuel-consuming afterburner to operate at supersonic speeds.

The sophisticated F-22A aero design, advanced flight controls, thrust vectoring, and high thrust-to-weight ratio provide the capability to outmaneuver all current and projected aircraft. The F-22A design has been extensively tested and refined aerodynamically during the development process.

From the very beginning, the F-22A exceeded the USAF’s expectations, and during exercises and deployments, it proved to be more than a match for any fighter opposing it.

During the highly realistic Exercise Northern Edge 2006, the F-22 proved itself against as many as 40 “enemy aircraft” during simulated battles. The Raptor pilots achieved a 108-to-zero “kill” ratio against the best F-15, F-16 and F-18 “adversaries.” The stealthy F-22A also proved that it could avoid and destroy enemy surface to air missiles, and recorded an impressive 97 percent mission capability rate.

Specifically noting the Raptor’s performance at Northern Edge, the National Aeronautic Association (NAA) awarded its 2006 Robert J. Collier Trophy, considered America’s most prestigious award for aeronautical and space development, to the Lockheed Martin Corp.-led F-22 Raptor aircraft team “for designing, testing and operating” the Raptor. Team members included Lockheed Martin, Boeing, Pratt & Whitney, Northrop Grumman, Raytheon and BAE Systems. This amazing aircraft was described as “the most efficient and effective fighter in history, through exceptional performance and outstanding safety features.”

The F-22A will have better reliability and maintainability than any fighter aircraft in history. Increased F-22A reliability and maintainability pays off in less manpower required to fix the aircraft and the ability to operate more efficiently.

Specifications
Primary Function: Air dominance, multi-role fighter
Contractor: Lockheed-Martin, Boeing
Power Plant: Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles.
Thrust: 35,000-pound class (each engine)
Wingspan: 44 feet, 6 inches (13.6 meters)
Length: 62 feet, 1 inch (18.9 meters)
Height: 16 feet, 8 inches (5.1 meters)
Weight: 43,340 pounds (19,700 kilograms)
Maximum Takeoff Weight: 83,500 pounds (38,000 kilograms)
Fuel Capacity: Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms)
Payload: Same as armament air-to-air or air-to-ground load outs; with or without 2 external wing fuel tanks.
Speed: Mach 2 class with super cruise capability
Range: More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles)
Ceiling: Above 50,000 feet (15 kilometers)
Armament: One M61A2 20-millimeter cannon with 480 rounds, internal side weapon bays carriage of two AIM-9 infrared (heat seeking) air-to-air missiles and internal main weapon bays carriage of six AIM-120 radar-guided air-to-air missiles (air-to-air load out) or two 1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided air-to-air missiles (air-to-ground load out)
Crew: One
Unit Cost: $142 million
Initial operating capability: December 2005
Inventory: Total force, 91