From att-mt!ihlpl.att.com!jfb Wed Jan 13 12:18:08 1993
Path: cbnewsd!att-out!pacbell.com!ames!agate!usenet.ins.cwru.edu!gatech!hubcap!ncrcae!ncrhub2!ciss!law7!military
From: jfb@ihlpl.att.com
Newsgroups: sci.military
Subject: Number Forty-Three in the Series--Republic P-43 Lancer
Keywords: Thunderbolt prececessor
Message-ID: <C0syq8.60H@law7.DaytonOH.NCR.COM>
Date: 13 Jan 93 17:18:08 GMT
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Organization: AT&T Bell Laboratories -  Naperville, Illinois
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>From jfb@ihlpl.att.com


The Republic P-43 Lancer was a progressive development of the Seversky 
P-35.  It can be regarded as an "intermediate" between the P-35 and 
the superlative P-47.  

During 1938, the Seversky Aircraft Corporation initiated work on two 
developments of the P-35.  One was the AP-2, a conversion of an 
existing P-35 airframe with a Pratt and Whitney R-1830-19 radial 
containing an integral, medium altitude supercharger.  The other was 
the AP-4, with a similar engine but with a turbosupercharger mounted 
in the rear fuselage aft of the cockpit.  The airframes of the AP-2 
and AP-4 were almost identical to each other, and both featured 
inward-retracting main undercarriage members.  

The AP-2 was eventually delivered to the USAAC as the XP-41.  It was 
unsuccessful in attracting any production orders.  Initially, the AP-4 
featured a close-fitting engine cowling and an inordinately large 
propeller spinner in an attempt to reduce drag.  However, this 
arrangement caused cooling problems and a more orthodox radial cowling 
was fitted at an early stage.  Initially, the AP-4 looked a lot like 
its P-35 predecessor--the cockpit was raised quite high and there was 
a large area of transparency behind the pilot.  

On March 12, 1939, thirteen service test models of the AP-4 were 
ordered by the Army under the designation YP-43.  Serial numbers were 
39-704/716.  The YP-43 differed from the original AP-4 in several 
respects.  The cockpit was lowered in an attempt to reduce drag, the 
rear fuselage upper decking was raised, and the transparent area 
behind the cockpit greatly reduced.  The tailwheel leg was made 
longer.  The air intake for the turbosupercharger was moved from the 
port wing root and was mounted underneath the engine inside the 
deeper, oval-shaped cowling.  The two 0.5-inch machine guns in the 
engine cowling were supplemented by a pair of wing-mounted 0.3-inch 
machine guns.  The Pratt and Whitney R-1830-35 engine was adopted, 
offering 1200 hp for takeoff and 1100 hp at 20,000 feet.  

The first YP-43s were delivered to the Army in September 1940.  By 
this time, Major de Seversky had been ousted as president of Seversky, 
and his company had changed its name to Republic Aviation Corporation.  
The last YP-43 was delivered by April 1941, the type being given the 
name *Lancer*.  Maximum speed was 349 mph at 25,000 feet.  Initial 
climb rate was 2850 feet per minute.  Service ceiling was 38,000 feet, 
and range was 800 miles.  Wingspan was 36 feet, length was 27 feet 11 
inches, height was 14 feet, and wing area was 223 square feet Weights 
were 5656 pounds empty and 7300 pounds gross.  Although the weight of 
the YP-43 was excessive, the turbosupercharger gave the new aircraft a 
considerable advantage in both speed and operational ceiling over the 
earlier P-35.  

However, by 1941, the Lancer was already outdated by the rapid 
advances in air combat technology that had taken place in Europe.  It 
suffered from poor maneuverability and climbing performance, and 
lacked such modern innovations as armor protection for the pilot and 
self-sealing fuel tanks.  Consequently, the Army did not anticipate 
ordering any more P-43s beyond the initial service-test contract.  In 
fact, on September 13, 1939, the Army had already ordered eighty 
examples of the more advanced AP-4J from Republic under the 
designation P-44.  However, combat reports coming out of Europe in the 
spring of 1940 indicated that even the P-44 would not be up to the 
task, and Alexander Kartveli began to consider the successor which was 
eventually to emerge as the P-47 Thunderbolt.  On September 13, 1940, 
all work on the P-44 was cancelled in favor of the P-47.  

It would seem, therefore, that the P-43 would have a rather bleak 
future.  However, since the R-2800 Double Wasps that were to power the 
P-47 would not be available for some time, the Army felt that 
Republic's Farmingdale production lines needed to be kept busy in the 
interim.  Consequently, the P-43 was ordered into production as a 
stop-gap measure.  

Fifty-four P-43 Lancers were ordered by the Army in late 1940.  Serial 
numbers were 41-6668/6721.  They were virtually identical to the 
YP-43.  The engine was the turbosupercharged Pratt & Whitney 
R-1830-47, delivering 1200 hp.  The first P-43 was delivered on May 
16, 1941, the last example being delivered on August 28, 1941.  
Maximum speed was 349 mph at 25,000 feet.  Initial climb rate was 2850 
feet per minute.  Service ceiling was 38,000 feet, and range was 800 
miles.  Wingspan was 36 feet, length was 28 feet 6 inches, height was 
14 feet, and wing area was 223 square feet Weights were 5654 pounds 
empty and 7810 pounds gross.  Maximum takeoff weight was 7935 pounds.  
Armament consisted of two 0.50-inch and two 0.30-inch machine guns.  

The P-43 was immediately followed by the P-43A, 80 examples of which 
were ordered.  Serials were 40-2891/2970.  Deliveries began in 
September of 1941.  The P-43A was essentially the same as the earlier 
P-43, but differed in having the turbosupercharged R-1830-49 which 
afforded its full 1200 hp at 25,000 feet.  Armament was increased to a 
full four 0.50-in machine guns, two in the fuselage and two in the 
wings.  Deliveries began in September 1941.  Maximum speed was 356 mph 
at 25,000 feet.  An altitude of 15,000 feet could be reached in 6 
minutes.  Service ceiling was 36,000 feet, and range was 650 miles.  
Wingspan was 36 feet, length was 28 feet 6 inches, height was 14 feet, 
and wing area was 223 square feet Weights were 5996 pounds empty and 
7435 pounds gross.  Maximum takeoff weight was 8480 pounds.  

In the USAAF, the P-43 went to the 1st Pursuit Group at Selfridge 
Field, Michigan, to the 55th Pursuit Group at Portland Field, and then 
to the 14th Pursuit Group at March Field, California.  Their service 
life with these groups was quite brief, and they were soon replaced by 
P-38 Lightnings as soon as they became available.  

On June 30, 1941, 125 further examples were ordered with Lend-Lease 
funds for supply to the Chinese Air Force, although their primary 
purpose was still to keep the Farmingdale production lines occupied 
until the Thunderbolt could be ready.  The Chinese Lend-Lease P-43s 
were designated P-43A-1.  Serial numbers were 41-31448/31572.  The 
P-43A-1 differed from the P-43A by having a Pratt and Whitney 
R-1830-57 engine with the same power.  The four 0.50-inch machine guns 
were all concentrated in the wings.  Some attempt was made to make the 
design more combat-worthy by adding such modern features as armor and 
self-sealing fuel tanks.  Provision was made for the carrying of a 
41.6 Imp.  gall.  drop tank, one 200-pound bomb, or six 20-pound 
bombs.  maximum speed was 356 mph at 10,000 feet, service ceiling was 
36,000 feet, and maximum ferry range was 1450 miles.  Weights were 
5996 pounds empty, 7435 pounds loaded, and 8480 pounds maximum.  
Wingspan was 36 feet 0 inches, length was 28 feet 6 inches, height was 
14 feet 0 inches, and wing area was 223 square feet.  

Production of the P-43A-1 was completed in March of 1942, and 108 of 
these aircraft were ultimately transferred to China.  They saw a 
certain amount of action there, but they proved uniformly unequal to 
the task at hand.  They were handicapped by poor maneuverability and 
inefficient self-sealing fuel tanks and achieved little success 
against the Japanese.  

The USAAF always viewed the P-43 as only an interim type and 
considered it unfit for any combat role.  None of the USAAF P-43s ever 
saw any action, being used strictly for advanced training in Stateside 
units.  In 1942, most of the surviving USAAF P-43 and P-43A Lancers 
were converted as specialized photographic reconnaissance aircraft and 
redesignated P-43B.  These were fitted with cameras in the rear 
fuselage.  Most of these were used to train squadrons until Lockheed 
F-4s became available.  

Conversions to P-43B standards also included those P-43A-1s which did 
not get sent to China, and these planes were supplied to the Royal 
Australian Air Force in 1942.  I am unaware of the RAAF serial numbers 
of the type, and I am uncertain if any of them ever saw any combat.  A 
total of 150 Lancers were eventually converted to P-43B standards.  

Two other P-43As (serials 40-2894 and 40-2897) were modified as P-43C 
photographic reconnaissance aircraft, which were similar to the P-43B 
but with different photographic fixtures.  Yet another set of 
modifications of existing P-43s (serials 41-6685, 41-6687, 41-6692, 
41-6695, 41-6707, 41-6718) took place to produce the P-43D 
photographic version, which differed only in minor details from the 
P-43C.  

The designation P-43E was applied to a projected but unbuilt photo- 
reconnaissance version of the P-43A with different types of fixtures.  

In October 1942, surviving P-43s were redesignated RP-43, the R 
standing for "restricted from combat use".  

Sources: 

  War Planes of the Second World War, Fighters, Volume 4, William Green, 
  Doubleday, 1964.  

  The American Fighter, Enzo Angelucci and Peter Bowers, Orion Books, 
  1987.  

  United States Military Aircraft Since 1909, Gordon Swanborough and 
  Peter M.  Bowers, Smithsonian, 1989.  

  American Combat Planes, Ray Wagner, Doubleday, 1982.  

Joe Baugher       AT&T Bell Laboratories    2000 North Naperville Road 
		  Naperville, Illinois 60566-7033.   (708) 713-4548



