CORSNING
Tech Sergeant
I am attempting to put together a quick reference operational performance timeline
for the Mustang. I am hoping to get the help needed to complete this reference. I
have found that the more I researched and put it down on paper, the less I actually
knew. What I have been able to put together looks like this:
NA-73X: First flight 26 October 1940: V-1710-39/3,000 rpm: 1,050 hp./S.L.,
1,095 hp./5,000 ft., 1,140 hp./10,000 ft.
ACC: RAF forms the Army Cooperation Command on 1 December 1940. They are
the first to fly the Mustang.
Mustang I (Mk.I/NA-73): 25 April 1941: First flight piloted by Louis Wait.
MK.I AG346: 24 October 1941: The first Mustang I arrives in Liverpool, England.
AG346 is sent to Boscombe Down for test trials.
Mk.I: 10 May 1942: No.26 Sqn.(ACC), F/Officer Graham Dawson flew 1st combat
operational flight. V-1710-F3R: Same as V-1710-39. Armament: 4 x 0.3in. +
4 x 0.5in. machine guns.
Mk.I:......Four sent to USSR..................V-1710-39: 8,8:1 supercharger gear ratio
Mk.I:......date?.............RAF unit?..........V-1710-F21R: 7.48:1 supercharger gear ratio
Mk.IA: September 1942: First Mk.IAs arrive in England V-1710-F3R. Armament:
4 x 20 mm / 125 rpg.
Mk.IA: 22 June 1943: No.268 Squadron are issued the first Mustang IAs.
Mk.IA: 13 August 1943: No.268 Sqdn. fly first operation sortie.
Mustang X (converted Mk.I A/C No.AL 975/G): First flight 13 October 1942:
Merlin 65: 1,315 hp. (First Rolls Royce version).
12 December 1942: Letter from Allison Division dated concerning the V-1710-F3R
(-39) and V-1710-F4R(-73).
1. 60"Hg boost has been agreed on by Allison: ~1,570 hp./3,000 rpm.
2. 66"Hg boost is the boost control setting used in the Middle East: ~1,745 hp./S.L.,
1,770 hp./2,000 ft.
3. 70"Hg boost has been used by some pilots for prolonged periods in Australia:
1,780 hp./S.L.
P-51:..9 April 1943....154th Observation Sdn....V-1710-39/3,000 rpm: 1,150 hp./T.O./
44.5"Hg, 1,150 hp./10,800 ft./43.9"Hg.
27 August 1943: Letter from Headquarters, Northwest African Strategic Air Force
APO 520, to Commanding General APO 650 concerning the Mk.I and Mk.Ia with
V-1710-39: "The British have operated at full throttle at sea level (72"Hg) for as
much as 20 min. at a time without hurting the engines. According to them, the
Allison is averaging 1500 hours between bearing failures as compared to 500 to
600 hours for the Merlin. The Allison, they have found will drag them home even
with the bearing ruined."
A-36A production deliveries begin October 1942. Armament: 6 x 0.5 in. / 200 rpg.
Engine: Allison V-1710-87 @ 3,000 rpm: 1,325 hp./47"Hg/T.O., 1,500 hp./52"Hg.
A-36A: 6 June 1943: The 23rd FG/14th AF & 27th Fighter-Bomber Group become
operational.
P-51A: production deliveries begin March 1943. Engine: Allison V-1710-81: 1,200 hp./
52"Hg/3,000 rpm. @ 57"Hg and 3,000 rpm: 1,480 hp./5,000-10,400 ft., 1,330 hp./11,800 ft.
Armament: 2 x 0.5 in./350 rpg + 2 x 0.5 in./280 rpg.
P-51A: June 1943: Fifty Mk.IIs and one A-36A join the RAF.
P-51A: July 1943: The 311th FG in India receive P-51As.
P-51A: September 1943: The 23rd FG/14th AF in Kweilin, China receive P-51A and use
them on fighter missions.
Mk.II: May 1944: No.II (2) Sqdn. receive the first Mustang IIs and a limited number
are operational by 6 June 1944 (D-Day).
P-51B-1 production deliveries begin May 1943.
ACC is disbanded on 1 June 1943. The RAF Mustangs go to 2 Tactical Air Force (2TAF).
P-51B: 1 December 1943: 354th F.G./9th A.F. become operational. Engine: Rolls Royce
V-1650-3/3,000 rpm/61"Hg. military power: 1,380 hp./T.O. & S.L., 1,490 hp./13,750 ft.,
1,210 hp./25,800 ft.
Date ?: Rolls-Royce V-1650-3/67"Hg/3,000 rpm: 1,600 hp./15,600 ft., 1,330 hp./29,000 ft.
P-51B-5:...date?...unit?...V-1650-3
P-51B-7 (Mid-run P-51B-5): December 1943 V-1650-3...85 gallon fuselage fuel tank
installation begins at the factory.
Mk.III: RAF begin operations in February 1944. They will be allotted 308 P-51Bs and
636 P-51Cs under Lend-Lease.
P-51B-10: Late March/Early April 1944 arrive in the ETO...unit?...V-1650-?
P-51B-15: (Late April 1944?)...ETO Sdn.?...V-1650-7/3,000 rpm: 1,490/T.O./61"Hg.,
@ 67"Hg: 1,720 hp./6,250 ft., 1,505 hp./19,250 ft.
P-51B: April 1944 arrive in the MTO.
P-51C-1: Production deliveries begin September 1943.
P-51D-5: Production deliveries begin March 1944.
P-51D-5: Late May 1944 arrive at 354th & 4th F.G./9th A.F. under command of the
8th A.F. Engine: R/R V-1650-7 / 67"Hg. Armament: 6 x 0.5 in. machine guns.
100/150 Grade fuel: Deliveries begin to the 8th A.F. on 10 June 1944. Boost levels for
V-1650-7 are raised to 72-75"Hg.
Mk.III / V-1650-7 used as interceptors in defense of England use up to +25 psi.(80.8"Hg)
boost: 1,940 hp./S.L., 1,810 hp./12,000 ft.
XP-51F: 14 February 1944: First flight.
XP-51G: First flight 9 August 1944. Note: First flight was with a 5-blade propeller. Three days
later the aircraft is flown with a 4-blade Aeroproducts propeller.
P-51K: August 1944: Production deliveries begin.
P-51K: September 1944.....ETO unit?.....V-1650-7
P-51D/K: November 1944 arrive in the PTO.
P-51D/K: December 1944 they enter combat.....PTO unit?.....V-1650-7
F6D:.........November 1944....82nd Recon. Sdn........V-1650-7
P-51H: 3 February 1945: First flight of production aircraft. Engine Packard V-1650-9:
1,335 hp./T.O., 2,220 hp./9,000 ft., 1,790 hp./22,700 ft.
P-51H: A few sorties were flown in a combat area during the last two weeks according to
some pilots in the squadron(s) that were gearing up for operational status at the end of WW2.
P-51M: August 1945: Only Dallas production P-51H.
15 August 1945 Mustang production ceases with 15,484 US built and 1,000 Australian built
or in production.
Special Note: 8th Fighter Command was among the first to wear anti-g suits which inflated
automatically around the calves, thighs and lower body during tight turns and when pulling
out from a dive. The G-suit restricted the blood from draining from the head and trunk of the
body which delayed the onset of blacking out. The downside, the suit allowed pilots to be able
to take more punishment than their aircraft. This resulted in deformed wings and popped rivets.
Any corrections or additions to the reference are greatly appreciated, Jeff.
for the Mustang. I am hoping to get the help needed to complete this reference. I
have found that the more I researched and put it down on paper, the less I actually
knew. What I have been able to put together looks like this:
NA-73X: First flight 26 October 1940: V-1710-39/3,000 rpm: 1,050 hp./S.L.,
1,095 hp./5,000 ft., 1,140 hp./10,000 ft.
ACC: RAF forms the Army Cooperation Command on 1 December 1940. They are
the first to fly the Mustang.
Mustang I (Mk.I/NA-73): 25 April 1941: First flight piloted by Louis Wait.
MK.I AG346: 24 October 1941: The first Mustang I arrives in Liverpool, England.
AG346 is sent to Boscombe Down for test trials.
Mk.I: 10 May 1942: No.26 Sqn.(ACC), F/Officer Graham Dawson flew 1st combat
operational flight. V-1710-F3R: Same as V-1710-39. Armament: 4 x 0.3in. +
4 x 0.5in. machine guns.
Mk.I:......Four sent to USSR..................V-1710-39: 8,8:1 supercharger gear ratio
Mk.I:......date?.............RAF unit?..........V-1710-F21R: 7.48:1 supercharger gear ratio
Mk.IA: September 1942: First Mk.IAs arrive in England V-1710-F3R. Armament:
4 x 20 mm / 125 rpg.
Mk.IA: 22 June 1943: No.268 Squadron are issued the first Mustang IAs.
Mk.IA: 13 August 1943: No.268 Sqdn. fly first operation sortie.
Mustang X (converted Mk.I A/C No.AL 975/G): First flight 13 October 1942:
Merlin 65: 1,315 hp. (First Rolls Royce version).
12 December 1942: Letter from Allison Division dated concerning the V-1710-F3R
(-39) and V-1710-F4R(-73).
1. 60"Hg boost has been agreed on by Allison: ~1,570 hp./3,000 rpm.
2. 66"Hg boost is the boost control setting used in the Middle East: ~1,745 hp./S.L.,
1,770 hp./2,000 ft.
3. 70"Hg boost has been used by some pilots for prolonged periods in Australia:
1,780 hp./S.L.
P-51:..9 April 1943....154th Observation Sdn....V-1710-39/3,000 rpm: 1,150 hp./T.O./
44.5"Hg, 1,150 hp./10,800 ft./43.9"Hg.
27 August 1943: Letter from Headquarters, Northwest African Strategic Air Force
APO 520, to Commanding General APO 650 concerning the Mk.I and Mk.Ia with
V-1710-39: "The British have operated at full throttle at sea level (72"Hg) for as
much as 20 min. at a time without hurting the engines. According to them, the
Allison is averaging 1500 hours between bearing failures as compared to 500 to
600 hours for the Merlin. The Allison, they have found will drag them home even
with the bearing ruined."
A-36A production deliveries begin October 1942. Armament: 6 x 0.5 in. / 200 rpg.
Engine: Allison V-1710-87 @ 3,000 rpm: 1,325 hp./47"Hg/T.O., 1,500 hp./52"Hg.
A-36A: 6 June 1943: The 23rd FG/14th AF & 27th Fighter-Bomber Group become
operational.
P-51A: production deliveries begin March 1943. Engine: Allison V-1710-81: 1,200 hp./
52"Hg/3,000 rpm. @ 57"Hg and 3,000 rpm: 1,480 hp./5,000-10,400 ft., 1,330 hp./11,800 ft.
Armament: 2 x 0.5 in./350 rpg + 2 x 0.5 in./280 rpg.
P-51A: June 1943: Fifty Mk.IIs and one A-36A join the RAF.
P-51A: July 1943: The 311th FG in India receive P-51As.
P-51A: September 1943: The 23rd FG/14th AF in Kweilin, China receive P-51A and use
them on fighter missions.
Mk.II: May 1944: No.II (2) Sqdn. receive the first Mustang IIs and a limited number
are operational by 6 June 1944 (D-Day).
P-51B-1 production deliveries begin May 1943.
ACC is disbanded on 1 June 1943. The RAF Mustangs go to 2 Tactical Air Force (2TAF).
P-51B: 1 December 1943: 354th F.G./9th A.F. become operational. Engine: Rolls Royce
V-1650-3/3,000 rpm/61"Hg. military power: 1,380 hp./T.O. & S.L., 1,490 hp./13,750 ft.,
1,210 hp./25,800 ft.
Date ?: Rolls-Royce V-1650-3/67"Hg/3,000 rpm: 1,600 hp./15,600 ft., 1,330 hp./29,000 ft.
P-51B-5:...date?...unit?...V-1650-3
P-51B-7 (Mid-run P-51B-5): December 1943 V-1650-3...85 gallon fuselage fuel tank
installation begins at the factory.
Mk.III: RAF begin operations in February 1944. They will be allotted 308 P-51Bs and
636 P-51Cs under Lend-Lease.
P-51B-10: Late March/Early April 1944 arrive in the ETO...unit?...V-1650-?
P-51B-15: (Late April 1944?)...ETO Sdn.?...V-1650-7/3,000 rpm: 1,490/T.O./61"Hg.,
@ 67"Hg: 1,720 hp./6,250 ft., 1,505 hp./19,250 ft.
P-51B: April 1944 arrive in the MTO.
P-51C-1: Production deliveries begin September 1943.
P-51D-5: Production deliveries begin March 1944.
P-51D-5: Late May 1944 arrive at 354th & 4th F.G./9th A.F. under command of the
8th A.F. Engine: R/R V-1650-7 / 67"Hg. Armament: 6 x 0.5 in. machine guns.
100/150 Grade fuel: Deliveries begin to the 8th A.F. on 10 June 1944. Boost levels for
V-1650-7 are raised to 72-75"Hg.
Mk.III / V-1650-7 used as interceptors in defense of England use up to +25 psi.(80.8"Hg)
boost: 1,940 hp./S.L., 1,810 hp./12,000 ft.
XP-51F: 14 February 1944: First flight.
XP-51G: First flight 9 August 1944. Note: First flight was with a 5-blade propeller. Three days
later the aircraft is flown with a 4-blade Aeroproducts propeller.
P-51K: August 1944: Production deliveries begin.
P-51K: September 1944.....ETO unit?.....V-1650-7
P-51D/K: November 1944 arrive in the PTO.
P-51D/K: December 1944 they enter combat.....PTO unit?.....V-1650-7
F6D:.........November 1944....82nd Recon. Sdn........V-1650-7
P-51H: 3 February 1945: First flight of production aircraft. Engine Packard V-1650-9:
1,335 hp./T.O., 2,220 hp./9,000 ft., 1,790 hp./22,700 ft.
P-51H: A few sorties were flown in a combat area during the last two weeks according to
some pilots in the squadron(s) that were gearing up for operational status at the end of WW2.
P-51M: August 1945: Only Dallas production P-51H.
15 August 1945 Mustang production ceases with 15,484 US built and 1,000 Australian built
or in production.
Special Note: 8th Fighter Command was among the first to wear anti-g suits which inflated
automatically around the calves, thighs and lower body during tight turns and when pulling
out from a dive. The G-suit restricted the blood from draining from the head and trunk of the
body which delayed the onset of blacking out. The downside, the suit allowed pilots to be able
to take more punishment than their aircraft. This resulted in deformed wings and popped rivets.
Any corrections or additions to the reference are greatly appreciated, Jeff.
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