Lieutenant James H. Doolittle, Air Service, United States Army, with the Curtiss R3C-2 Schneider Trophy winner, 1925. (U.S. Air Force)
26 October 1925: Lieutenant James Harold Doolittle, Air Service, United States Army, won the Coupe d’Aviation Maritime Jacques Schneider (commonly called the Schneider Trophy) when he placed first flying his Curtiss R3C-2 float plane over a 217-mile (349 kilometer) course near Bay Shores on Chesapeake Bay, Maryland.
Doolittle’s average speed for the seven laps around the triangular race course was 232.57 miles per hour (374.29 kilometers per hour). The second-place airplane, a Gloster-Napier III flown by Captain Hubert Broad, averaged 199.16 miles per hour (320.52 kilometers per hour).
Doolittle also set two Fédération Aéronautique Internationale (FAI) world records during the race: World Record for Speed Over 100 Kilometers, with an average speed of 377.83 kilometers per hour (234.77 miles per hour);¹ World Record for Speed Over 200 Kilometers, 377.16 kilometers per hour (234.36 miles per hour).² On the following day, Doolittle set a third FAI record: World Record for Speed Over a 3 Kilometer Course, 395.5 kilometers per hour (245.75 miles per hour).³
Lieutenant James H. Doolittle (left) and Lieutenant Cyrus Bettis with the Curtiss R3C-2. (NARA 31758AC)
A contemporary news article commented on Jimmy Doolittle’s performance:
Gloster III Schneider Cup racer, powered by a 700 horsepower Napier Lion VII “broad arrow” W-12.
“. . . according to reports Lieut. Doolittle’s cornering was superb, and must have been to a great extent responsible for the excellent performance. Reports from America—coming, it is thought, from a reliable source—indicate that one particular engine out of the 12 built for the Pulitzer and Schneider Trophy races proved exceptionally good, as will often happen in a batch of engines, and it is believed that this engine was fitted in Doolittle’s Curtiss-Army Racer. This fact, taken in conjunction with the masterly handling of the machine, would seem to account for the wholly unexpected average speed maintained, which was, of course, far and away ahead of the speeds of the British and Italian competitors.”
—FLIGHT, The Aircraft Engineer & Airships, No. 879 (No. 44, Vol. XVII.) October 29, 1923 at Page 703
“The triangular Schneider race course stretched from Bay Shore Park to Gibson Island to the south and across Chesapeake Bay to Huntingfield Point. Contestants had to fly the 50-kilometer (31-mile) course seven times.” Smithsonian National Air and Space MuseumThe Curtiss R3C-2 Racer on display at the National Air and Space Museum. (Photo by Eric Long, National Air and Space Museum, Smithsonian Institution)
The R3C-2 was a single-engine, single-seat, single-bay biplane, equipped with pontoons for taking off and landing on water. It was built especially for air racing. Two R3Cs were built for the United States Navy and one for the Army. (The Army aircraft is identified by a Navy Bureau of Aeronautics serial number (“Bu. No.”) A-7054. It does not seem to have been assigned an Air Service serial number.) The airplane and its V-1400 engine were both built by the Curtiss Aeroplane and Motor Company, which had been founded by Glenn Hammond Curtiss. The R3C-2 was converted from the R3C-1, the land plane configuration which had been flown by Lieutenant Cyrus Bettis, AS, USA, to win the Pulitzer Trophy Race just two weeks earlier.
The RC3-2 is 22 feet long (6.706 meters), an increase of 2 feet, 3.5 inches (0.698 meters) over the R3C-1 configuration, resulting from the replacement of the fixed wheeled landing gear with the single-step pontoons. The upper wing span is 22 feet (6.706 meters), with a chord of 4 feet, 8¼ inches (1.429 meters). The lower wing span is 20 feet (6.096 meters) with a chord of 3 feet, 3¾ inches (1.010 meters). Weight empty was 2,135 pounds (968 kilograms) and maximum takeoff weight was 2,738 pounds (1,242 kilograms).
Constructed of wood, the fuselage has four ash longerons and seven birch vertical bulkheads. The framework is covered with two layers of 2-inch (51 millimeter) wide, 3/32-inch (2.38 millimeter) thick spruce strips. These were placed on a 45° diagonal from the fuselage horizontal centerline, with the second layer at 90° to the first. These veneer strips were glued and tacked to the frame. The fuselage was then covered with doped fabric. The wings and tail surfaces are also of wood, with spruce ribs and a covering of spruce strips.
Lieutenant Cyrus Bettis, USAAS, with the Curtiss R3C-1 racer at Mitchel Field, Long Island, New York, 12 October 1925. The surface radiators on the wings can be seen. (Curtiss Aeroplane and Motor Co.)
The single-bay wings are wire braced and contain surface radiators made of thin brass sheeting. The radiators contained 12 gallons (45.4 liters) of water, circulating at a rate of 75 gallons (283.9 liters) per minute. By using surface radiators to cool the engine, aerodynamic drag was reduced.
The Curtiss V-1400 engine was developed from the earlier Curtiss D-12. It was a water-cooled, normally aspirated, 1,399.91-cubic-inch-displacement (22.940 liter), dual overhead cam (DOHC) 60° V-12, with a compression ratio of 5.5:1. The V-1400 was rated at 510 horsepower at 2,100 r.p.m., and could produce 619 horsepower at 2,500 r.p.m. It was a direct-drive engine and turned a two-bladed duralumin fixed-pitch propeller with a diameter of 7 feet, 8 inches (2.337 meters). The propeller was designed by Sylvanus Albert Reed, Ph.D. The V-1400 engine weighed 660 pounds (299 kilograms).
The R3C-2 had a fuel capacity of 27 gallons (102 liters). Its range was 290 miles (467 kilometers).
The Coupe d’Aviation Maritime Jacques Schneider at the Science Museum, London. (Wikipedia, edit by Eric Menneteau)
Jimmy Doolittle was one of America’s foremost pioneering aviators. He set many records, won air races, tested and developed new flying equipment and techniques.
He was a highly-educated military officer, having earned his Bachelor of Arts from the University of California Berkeley School of Mines, and M.S and D.Sc. degrees in Aeronautical Engineering from the Massachusetts Institute of Technology.
During World War II, Colonel Doolittle planned and led the famous Halsey-Doolittle Raid against Japan, 18 April 1942, for which he was awarded the Medal of Honor.
As a brigadier general, he commanded 12th Air Force in North Africa. Promoted to major general, he was given command of the 15th Air Force in the Mediterranean Theater, and commanded 8th Air Force as a lieutenant general, 1943–1945.
After the war, Lieutenant General Doolittle was placed on the inactive list. On 4 April 1985, by Act of Congress, James H. Doolittle was promoted to General. General Doolittle is the only person to have been awarded both the Congressional Medal of Honor and the Presidential Medal of Freedom.
First Lieutenant James Harold Doolittle, Air Service, United States Army
Henry Farman winning the Archdeacon Cup with his Voisin-Farman I. (Wright Brothers Aeroplane Co.)Coupe d’Aviation Ernest Archdeacon
26 October 1907: At Issy-les-Moulineaux, France, Henry Farman flew his Voisin-Farman I airplane a distance of approximately 771 meters (2,530 feet) in 52 seconds to win the Coupe d’Aviation Ernest Archdeacon (Ernest Archdeacon Cup) for the longest flight of the year.
The single-place single-engine biplane was built by brothers Charles and Gabriel Voisin, and was very similar to the Voisin-Delagrange I which they had built several months earlier. Henry Farman had requested some slight modifications. He first flew the airplane 30 September 1907.
The Voisin-Farman I was 44 feet, 2 inches (13.462 meters) long, with a wingspan of 35 feet, 5 inches (10.795 meters) and weighed 705 pounds (319.8 kilograms) and gross weight of 1,213 pounds (550 kilograms).
The airplane was powered by a steam-cooled, direct-injected, 487.14 cubic-inch-displacement (7.983 liter) Société Antoinette 8V 90° V-8 direct-drive engine producing 53 horsepower at 1,100 r.p.m. The engine turned a two-bladed pusher propeller. It was designed by Léon Levavasseur. The engine was 1.120 meters (3 feet, 8 inches) long, 0.630 meters (2 feet, 1 inch) wide and (0.540 meters (1 foot, 9 inches) high. It weighed 95 kilograms (209 pounds).
Charles Voisin and Henry Farman, 1907. (Unattributed)
The prototype Bell Model 430, C-GBLL, in flight, circa 1994. (Bell Helicopter TEXTRON)
A “dog ship” is an aircraft retained by a manufacturer for engineering development testing.
25 October 1994: At Bell Helicopter Textron’s plant at Mirabel, Quebec, Canada, the prototype Bell Model 430, registered C-GBLL, made its first flight.
The Bell Model 430 (“Four-Thirty”) is a twin-engine intermediate-weight helicopter, operated by one or two pilots, and which can be configured to carry from 6 to 11 passengers. It has advanced avionics. The standard helicopter is equipped with skid landing gear, and retractable tricycle gear is optional. The 430 was the first helicopter to be certified for instrument flight with a single pilot, without a stability augmentation system. The aircraft is also certified for Category A operations, meaning that if one engine were to fail during takeoff, the helicopter could continue to fly with the remaining engine.
Bell 430 instrument panel with some optional equipment. (Bell Helicopter TEXTRON)
The 430 was developed from the preceding Model 230 (and the 230 from the 222). It was lengthened 1 foot, 6 inches (0.457 meters) and uses a four-bladed semi-rigid main rotor. Instead of a mechanical rotor head of trunnions, bearings and hinges, the 430 has a “soft-in-plane” fiberglass rotor yoke that is flexible enough to allow the blades to flap, feather and lead/lag.
The Bell 430 is 50 feet, 0.6 inches (15.248 meters) long, with rotors turning. The fuselage is 44 feet, 1 inch (13.437 meters) long. Overall height 12 feet, 1.6 inches (3.697 meters). The span of the stub wings is 11 feet, 6.0 inches (3.454 meters). The fixed horizontal stabilizer has a spa of 11 feet, 5.9 inches (3.453 meters) and a -9° angle of incidence. The vertical fin is canted slightly to the right to unload the tail rotor during high speed flight.
The main rotor mast is tilted 5° forward and 1.15° to the left. The forward tilt helps to keep the passenger cabin level during forward flight, while the left tilt counteracts the translating tendency caused by tail rotor thrust while in a hover.
Bell 430 prototype at Mirabel, Quebec, Canada, December 1995. (Vertiflite)
The main rotor is 42 feet, 0 inches (12.802 meters) in diameter and rotates counter-clockwise as seen from above. (The advancing blade is on the right.) The rotor turns at 348 r.p.m., resulting in a blade tip speed of 765 feet per second (233 meters per second). The blades are of composite construction. They use an asymmetrical airfoil and have a chord of 1 foot, 2.2 inches (0.361 meters). The blades are pre-coned 2° 30′.
The tail rotor is mounted on the left side of the tail boom, with the rotor disc offset 1 foot, 9.5 inches (0.572 meters) to the left of the aircraft centerline. Seen from the helicopter’s left, the tail rotor turns clockwise (the advancing blade is below the axis of rotation). The tail rotor is 6 feet, 10.5 inches (2.098 meters) in diameter, with a chord of 10.0 inches (0.254 meters). The blades are constructed of a stainless steel spar, with a bonded stainless steel skin over an aluminum honeycomb. The tail rotor turns 1,881 r.p.m.
Three-view drawing of the Bell Model 430 with retractable tricycle landing gear. (Bell Helicopter TEXTRON)
In standard configuration, the wheel-equipped Model 430 has an empty weight of 5,364 pounds. Its maximum gross weight is 9,300 pounds (4,218 kilograms).
The 430 is powered by two Rolls-Royce Series IV M250 C40B FADEC turboshaft engines. (The engine was previously known as the Allison 250-C40B. Rolls-Royce acquired Allison in 1995). The engine has full digital electronic controls. The 250-C40B uses a single-stage centrifugal compressor, reverse-flow combustion chamber, and a 4-stage axial-flow turbine section (2-stage gas producer turbine, N1, and 2-stage power turbine, N2.) At 100% N1, the gas producer rotates at 51,000 r.p.m. and the power turbine turns 30,908 r.p.m. The output drive speed is 9,598 r.p.m.
The engines have a Maximum Continuous Power rating of 695 shaft horsepower, and 808 s.h.p. for takeoff (5-minute limit). If an engine fails, the remaining engine can be operated at 940 s.h.p. for 30 seconds; 880 s.h.p for 2 minutes; and 835 s.h.p. for 30 minutes.
At Sea Level, the Bell Model 430 has a cruise speed of 133 knots (153 miles per hour/246 kilometers per hour), and maximum cruise of 147 knots (169 miles per hour/272 kilometers per hour). VNE is 150 knots (173 miles per hour/278 kilometers per hour). The helicopter’s service ceiling is 20,000 feet (6,096 meters). At its maximum gross weight, the 430 can hover in ground effect (HIGE) at 10,400 feet (3,170 meters) and out of ground effect (HOGE) at 6,200 feet (1,890 meters).
The fuel capacity of the 430 is 187.5 U.S. gallons (708 liters). This gives the helicopter a range of 286 nautical miles (329 statute miles/530 kilometers). A 48 gallon (182 liter) auxiliary fuel tank can be installed in the baggage compartment. With skid landing gear, the fuel capacity is increased to 247 gallons (935 liters), increasing the range to 353 nautical miles (406 statute miles/654 kilometers).
The Bell Model 430 received its Transport Canada certification on 23 February 1996, with the first production aircraft delivered the following month. Production continued for 12 years. The final 430 was delivered in May 2008.
This helicopter is an early production Bell Model 222, sometimes unofficially called a “222A”. (Wikipedia)
C-GBLL was originally built as the sixth Model 222, serial number 47006, and registered by the Federal Aviation Administration as N2759D. The aircraft was used as the prototype of the Bell 222B, which upgraded the engines from the original 618-shaft horsepower Lycoming LTS-101-650C3 turboshaft engines to 680 s.h.p. LTS-101-750Cs. The diameter of the main rotor was increased from 40 feet to 42 feet.
In 1983, N2759D was next used as the prototype for the Model 222UT, which replaced the retractable tricycle landing gear with fixed skids constructed of tubular aluminum. This simplified the helicopter, decreased its empty weight and allowed for an increased fuel capacity. N2759D was transferred to Bell Helicopter Textron Canada at Mirabel. Its U.S. registration cancelled by the FAA on 17 October 1990, and it was re-registered C-GBLL by Transport Canada.
The skid-equipped Bell Model 222UT is often used as an emergency medical transport helicopter. This aircraft, operated by Mercy Air Service Inc., is standing by at Mohave Airport (MHV) in the high desert of southern California. (Unattributed)
Early problems with the Lycoming LTS-101 adversely affected sales of the Bell 222. Bell designed a new variant equipped with Allison 250-C30G engines. This helicopter was designated the Model 230. The first prototype, C-GEXP, with skid gear, made its first flight on 12 August 1991, followed by the second prototype—C-GBLL—on 3 October 1991.
Bell 230 prototype C-GBLL, minus main rotor and mast, and tail rotor, circa 1993. Compare the exhaust stacks to those of the 222UT in the image above. (Fiveprime)
The 430 prototype was given a new serial number, s/n 43901.
McDonnell Douglas F-4E-67-MC Phantom II, 78-0744, the last of 5,057 Phantoms built at St. Louis, 25 October 1979. (McDonnell Douglas Corporation)
25 October 1979: The 5,057th and very last Phantom II—an F-4E-67-MC, U.S. Air Force serial number 78-0744—was rolled out at the McDonnell Douglas Corporation plant, Lambert Field (STL), St. Louis, Missouri, and the production line was closed.
78-0744 was transferred to the Republic of Korea Air Force (ROKAF) under the Foreign Military Sales program Peace Pheasant II and assigned to the 17th Tactical Fighter Wing based at Cheongju International Airport (CJJ). One source says that it was “written off” but details are lacking.
McDonnell Douglas F-4E-67-MC Phantom II 78-0744 in United States Air Force markings. (U.S. Air Force)
The Shikishima Kamikaze unit is offered a toast of water as a farewell, 25 October 1944. At left is Lieutenant Yukio Seki (with cup in his hands). Commander Asaiki Tamai, with his back to the camera, is next to him. At center, also facing away from the camera, is Vice Admiral Takjiro Onishi.
25 October 1944: During The Battle of Leyte Gulf, the Divine Wind Special Attack Unit (Shinpū Tokubetsu Kōgekitai, or 神風特別攻撃隊) carries out its first mission, an attack on two task groups of United States Navy escort aircraft carriers near the island of Samar in the Philippine Sea.
Prior to the Kamikaze attack of 25 October 1944, there had been other suicide attacks by Japanese pilots, possibly beginning as early as the attack at Pearl Harbor, Hawaii, 7 December 1941. But the idea of intentional suicide attacks was proposed by Captain Motoharu Okamura, IJN, and studies began 15 June 1944.
Midshipman Yukio Seji, IJN,1939.
The first unit of 23 pilots, Unit Shikishima, was selected by Commander Asaichi Tamai. Lieutenant Yukio Seki (29 September 1921–25 October 1944) was appointed the unit’s commanding officer.
At 7:40 a.m., 25 October, six Japanese airplanes from Davao, Mindanao, attacked three Sangamon-class escort carriers of Task Group 77.4.1 (called “Taffy 1”), under the command of Rear Admiral Thomas Lamison (“Tommy”) Sprague, USN.
One airplane struck USS Santee (CVE-29) on the forward port side of the flight deck and continued through, blowing a 15 foot × 30 foot (4.6 × 9.1 meters) hole in the hangar deck. Fortunately eight 1,000 pound (454 kilogram) bombs located there did not explode. The resulting fire was extinguished by 7:51 a.m. In addition to the airplane’s pilot,16 sailors were killed and 27 wounded.
Five minutes later, at 7:57 a.m., Santee was hit on the starboard side by a torpedo launched by the Japanese Type B3 submarine, I-56.
USS Santee (CVE-29) being hit by a torpedo fired from the Japanese submarine I-56, 0757, 25 October 1944. (Naval History and Heritage Command NH 71526)
Immediately after the crash aboard Santee, another Kamikaze circled USS Suwanee (CVE-27). It was hit by antiaircraft gunfire and headed toward USS Sangamon (CVE-26). A 5-inch shell fired by Suwanee brought it down short of Sangamon. At the same time, another Kamikaze nearly hit USS Petroff Bay (CVE-80), a Casablanca-class escort carrier, but was shot down by antiaircraft fire.
Suwanee shot down a second Zero and damaged a third. This airplane rolled over, and trailing smoke, hit the escort carrier’s flight deck forward of the aft elevator. Its bomb exploded between the flight and hangar decks.
“Effect of a crash dive on Suwanee flight deck. A 250 kilogram (551 pound) bomb has just exploded between flight and hangar decks and fire billows out, 25 October 1944. (Naval History and Heritage Command NH 71528)
Within two hours the flight deck damage had been repaired, though the elevator remained inoperative. Flight operations resumed at 10:09 a.m.
Five Mitsubishi A6M2 Type 0 Model 21 Reisen fighters (commonly referred to as the “Zero”, and also known by the Allied reporting name Zeke) led by Lieutenant Seki departed Malabacat, Luzon, and headed toward Task Force 77.4.3 (“Taffy 3”), under the command of Rear Admiral Clifton Albert Frederick (“Ziggy”) Sprague, USN. (Ziggy Sprague was not related to Tommy Sprague.)
Prior to this mission, Lieutenant Seki was interviewed by war correspondent Masashi Onoda. Seki is reported to have said, “Japan’s future is bleak if it is forced to kill one of its best pilots. I am not going on this mission for the Emperor or for the Empire. . . I am going because I was ordered to!”
Most of Taffy 3 had just survived an attack by the Imperial Japanese Navy’s overwhelming Center Force, consisting of the Japanese super battleship Yamato, battleships Nagato, Kongo, Haruna, cruisers Haguro, Chokai, Kumano, Suzuya, Chikuma, Tone, and two destroyer squadrons, in The Battle off Samar.
The Kamikazes approached the task group at very low altitude, avoiding radar, then climbed to 5,000–6,000 feet (1,524–1,829 meters). They appeared so suddenly that the fleet’s combat air patrol was unable to intercept. At 10:50 a.m., the first Zero attacked USS Kitkun Bay (CVE-71), apparently aiming for the carrier’s bridge. It missed, but passed over the island, crashed the port catwalk, and bounced into the sea. The bomb it carried exploded and seriously damaged the ship.
“A Japanese kamikaze pilot in a Mitsubishi A6M5 Model 52 Reisen (“Zero,” or “Zeke”) crash dives on the U.S. Navy escort carrier USS White Plains (CVE-66) on 25 October 1944. The aircraft missed the flight deck and impacted the water just off the port quarter of the ship.” (Naval History and Heritage Command 80-G-288882)
Two Zeros attacking USS Fanshaw Bay (CVE-70) were shot down. Two more dived on USS White Plains (CVE-66) but were driven off by the carrier’s 40 millimeter Bofors antiaircraft guns. One, smoking from a hit, turned away and dived toward the escort carrier USS St. Lo (CVE-63). At 10:51, St. Lo‘s guns opened fire, but this fighter, identified as a Mitsubishi A6M5 Type 0 Model 52 Reisen, crashed through the flight deck and exploded in flames.¹
An explosion aboard USS St. Lo (CVE-63), immediately after being hit by a kamikaze, 10:51 a.m., 25 October 1944. Photograph taken from USS Kitkun Bay (CVE-71). (National Archives and Records Administration 80-G-270513)
In his classic 15-volume History of United States Naval Operations in World War II, Rear Admiral Samuel Eliot Morison, USNR, describes what followed:
“Quickly there followed seven explosions of torpedoes and bombs on the hangar deck. Great sections of the flight deck and elevator and entire planes were hurled hundreds of feet into the air. The ship blazed from stem to stern, and at 1125 the unluckily renamed ² St. Lo foundered under a cloud of dense smoke.
“The second member of this pair partly circled the formation, turned, and started a run on White Plains, which maneuvered to evade with hard left rudder. The plane came weaving under fire of all after guns; a torrent of blazing tracers could be seen entering its fuselage and wing roots. When only a few yards astern, it rolled over and dove, missing the port catwalk by inches and exploding between that level and the water. The flight deck was showered with debris and fragments of the pilot, and eleven men were injured.
RADM S. E. Morison, USNR, ca. 1953
“As Kitkun Bay was steaming on course 200° at 1110, she sighted 15 Judys [Yokosuka D4Y Suisei dive bombers]approaching the formation from astern, distant about five miles. She launched twoWildcats by catapult for combat air patrol, but not in time. She and the three remaining carriers, Fanshaw Bay, White Plains and Kalinin Bay were without screen, owing to rescue work. One of the three Kamikazes got through the C.A.P. and dove at Kitkun Bay from astern. Its wings were shot off as it neared the ship, and just in time, for the bomb struck the water 25 yards on the starboard bow and parts of the plane hit the forecastle. Kalinin Bay received a crash dive on her flight deck which damaged it badly, but the fires then started were quenched in less than five minutes. A second plane crashed after her stack and two others dove but missed. AdmiralSprague’s flagship, the lucky “Fannie Bee,” alone alone sustained no damage in this assault.”
—History of United States Naval Operations in World War II, Volume XII, Leyte—June 1944–January 1945, by Rear Admiral Samuel Elliot Morison, USNR. Chapter XIII, Section 3, at Page 302. Little, Brown and Company, Boston, 1988
“10:55 a.m. A major explosion occurs on USS St. Lo (CVE 63).” (National Archives and Records Administration 80-G-27051)
Of St. Lo‘s crew of 889 men, 113 were killed or missing, and another 30 later died of wounds.
Taffy 3’s remaining screening ships,³ the Fletcher-class destroyer USS Heerman (DD-531), with the Butler-class destroyer escorts USS John C. Butler (DE-339), USS Dennis (DE-405) and USS Raymond (DE-341), searched for survivors of the sunken St. Lo. They recovered 754 men.
USS St. Lo (CVE-63) burning in Leyte Gulf, 25 October 1944. (National Archives and Records Administration 80-G-47041)The remains of a Yokosuka D4Y Suisei dive bomber aboard USS Kitkun Bay (CVE-71), 25 October 1944. (United States Navy)Damage to the flight deck of USS Kalinin Bay (CVE-68), 25 October 1944. (National Archives and Records Administration 80-G-270510)
Just after noon on 26 October, another group of Kamikazes attacked Taffy 1. The task group’s combat air patrol saved Santee from 12 Judys. Sangamon and Petroff Bay were narrowly missed.
A Zeke crashes into the flight deck of USS Suwanee (CVE-27), 1240 hours, 26 October 1944. (National Archives and Records Administration 80-G-270613)
At 12:40 p.m., a Zero crashed onto Suwanee‘s flight deck and hit a torpedo bomber which had just landed. Both airplanes exploded. Nine more of Suwannee‘s airplanes caught fire. 85 sailors were killed, 58 were missing and 102 wounded, some of whom later died of their injuries.
USS Midway (CVE-63) at San Diego, California, April 1944. It is painted in a three color disruptive camouflage. The ship would be renamed USS St. Lo three months later. (National Archives and Records Administration 80-G-47028)
USS St. Lo (CVE-63) was a Casablanca-class escort aircraft carrier. Originally designated an auxiliary aircraft carrier, USS Chapin (ACV-63), the ship was laid down by the Kaiser Shipbuilding Co., Vancouver, Washington, 23 January 1943, under a Maritime Commission contract (M.C. Hull 1100). Chapin was renamed USS Midway (CVE-63) on 3 April 1943.
Midway was launched 17 August 1943, and commissioned 23 October 1943. Captain Francis Joseph McKenna, USN, was in command. The ship cost $6,033,429.05.
On 10 October 1944, Midway was renamed USS St. Lo (CVE-63), just 15 days before she was sunk.
St. Lo had an overall length 512 feet, 3 inches (156.14 meters), beam of 65 feet, 2 inches (19.86 meters) and maximum draft of 22 feet 4 inches (6.81 meters). The extreme width of the flight deck was 108 feet, 1 inch (32.95 meters). The ship had a full load displacement of 10,902 long tons (11,077 metric tons). It was powered by four Babcock & Wilcox boilers of 9,000 shaft horsepower (6,700 kilowatts), feeding two Skinner Unaflow vertical reciprocating steam engines, which turned two screws capable of driving it at 19 knots (22 statute miles per hour/35 kilometers per hour). The carrier had an unrefueled range of 10,240 nautical miles (11,784 statute miles/18,965 kilometers) at 15 knots (17 statute miles per hour/28 kilometers per hour).
“St. LO (CVE-63) slows to a stop as she is abandoned in an orderly manner. Note the men going down lines into the water.” (National Archives and Records Administration 80-G-270511)
The flight deck was equipped with one steam catapult and two elevators.
St. Lo was armed by one 5-inch, 38-caliber (127 millimeter) dual purpose naval gun, sixteen 40 millimeter Bofors automatic antiaircraft guns, and twenty 20 millimeter Oerlikon autocannon. She carried 672 rounds of 5-inch, 3,298 rounds of 40 millimeter cannon shells, and 7,440 rounds of 20 millimeter shells. The carrier also carried 1,350 rounds of .45 ACP small arms ammunition.⁴
St. Lo carried 27 aircraft, including Grumman F4F or General Motors/Eastern Aircraft FM Wildcat fighters and Grumman TBF or General Motors TBM Avenger torpedo bombers.
The wreck of USS St. Lo is located near N. 11° 1′ 12″, E. 126° 2′ 24″.
¹ Historian John Toland named Lieutenant Seki as the pilot of this airplane, but Lieutenant Junior Grade Hiroshi Nishizawa, IJN, flying one of the A6M5 escorting fighters, reported that Seki’s airplane bounced off the deck of the carrier and its bomb did not explode. It crashed into the sea. He observed a second plane crash onto St. Lo, and its bomb did explode. Nishizawa was killed the following day, 26 October 1944.
² It is an old sailors’ superstition that it is unlucky to rename a ship. USS St. Lo had been laid down as USS Chapin Bay in January 1943. On 3 April 1943, it was renamed USS Midway. In order to free the name Midway for the new large aircraft carrier CVB-41, as well to commemorate the Battle of Saint-Lô, USS Midway was renamed USS St. Lo on 10 October 1944.
³ Along with USS Gambier Bay (CVE-73), Taffy 3’s escorting Fletcher-class destroyers, USS Hoel (DD-503) and USS Johnston (DD-557) and the Butler-class destroyer escort, USS Samuel B. Roberts (DE-413), were sunk several hours earlier by enemy naval gunfire during The Battle off Samar, when they heroically counterattacked the Center Force.
⁴ Naval History and Heritage Command, “Midway II (CVE-63)”