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B-26
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Span
- 65 feet Wing area - 602 square feet Length
- 56 feet Height - 19 feet & 10 inches Powerplants
- (2) 1,850 horsepower 18-cylinder Pratt &
Whitney double Wasp R-2800-5 engines Empty weight
- 21,375 pounds Gross weight - 27,200 pounds
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B-26A
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- 41-7345
to 41-7365 (21)
- 41-7368
(1)
- 41-7431
(1)
- 41-7477
to 41-7483 (7)
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Externally
identical to the B-26, the B-26A had additional Dural
armor plate. Goodyear rubber self-sealing fuel tanks
replaced the original Mareng ones. Other changes included:
24-volt electrical system, provision for a second releasable
250-gallon gas tank in the forward bomb bay, low pressure
oxygen system, and a 100-amp generator. These changes
added nearly 2,000 pounds to the weight.
The
B-26A retained the R-2800-5s, although these were now
the Ford license-built version. The AAF ordered that
all B-26s off the production line without the changes
specified for the B-26A variant be modified to include
them. This was accomplished and the B-26 and B-26A became
virtually identical in service.
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B-26A-1
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- 41-7366
to 41-7367 (2)
- 41-7369
to 41-7430 (62)
- 41-7432
to 41-7476 (45)
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Because
of the critical shortage of R-2800-5 engines for the
B-26As, in late October, 1941, the AAF ordered Pratt
& Whitney to divert 200 R-2800 S1A4Gs ("A"
engine of 1,850 hp) and 222 R-2800 2SB-Gs ("B"
engines of 2,000 hp) from an RAF order to Martin. These
converted engines were redesignated by the AAF as R-2800-39s
and R-2800-41s respectively.
The
switch to the -39 engines was made on the Baltimore
assembly line starting with aircraft 41-7366. These
Marauders were designated B-26A-1s and were otherwise
identical to the B-26As.
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B-26B
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- 41-17544
to 41-17624 (81)
- 41-17626
to 41-17644 (19)
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B-26Bs
were the first in the series with noticeable external
differences. The tail gun position was completely redesigned,
with the single .30-caliber machine gun replaced by
two 0.50-caliber guns in a new "stepped"
tail arrangement. Overall length increased to 58'-3''.
Two other visible changes: torpedo racks under the fuselage
were to be fitted as factory standard, and the oil cooler
air scoop under the cowling was enlarged. Engines were
switched from the R-2800-39s of the B-26A-1s back to
the R-2800-5s.
A
total of 100 "pure" B-26Bs were manufactured.
The first example was accepted and delivered April 5,
1942.
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"B-26B-1"
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- 41-17645
to 41-17851 (207)
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Starting
in July, 1942, an eventual total of 207 Baltimore-built
B-26Bs, most destined as "final equipment"
for North African bound groups, were flown from Middle
River to Martin's Omaha Modification Center and reworked
there under AAF instructions. So many modifications
were made to these planes that unofficially they became
known as "B-26B-1s"
Nose
Plexiglas was structurally strengthened to accommodate
a center-line mounted flexible .50-caliber gun. A fixed
forward-firing . 50-caliber machine gun was installed
in the lower right-hand side of the nose. The two .30-caliber
waist guns and the .30-caliber tunnel gun were replaced
by flexible Browning . 50-calibers. Two circular scanning
lenses were added above each waist gun position.
Provisions
were made for two more 250-gallon ferry tanks to be
fitted in the rear bomb bay. This increased fuel capacity
to 1,962 gallons, extended maximum ferry range to 2,850
miles, and raised takeoff weight considerably. The air
intakes on top of each engine cowling were changed to
much larger ones that would accommodate sand filters.
The Plexiglas windows on both sides of the fuselage,
next to the radio operator and navigator table, were
replaced with "bulged" ones to permit a view
downwards. To improve engine cooling--and lessen maintenance
difficulties--the large propeller spinners were deleted.
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B-26B-2
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- 41-17852
to 41-17946 (95)
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Pratt
& Whitney began delivering its upgraded 2,000 hp
takeoff-rated "Double Wasp" R-2800-41 engine
("B" series) from the British order to Martin-Baltimore
during May, 1942. Marauders built with this powerplant
were designated B -26B-2s. Ninety-five were so equipped.
The first was accepted June 17, 1942.
A
"whip" antenna for the new VHF radio was fitted
to the underside of the B-2 and on subsequent Marauders
just aft of the nose wheel door.
A
number of overseas-bound B-26B-2s received the same
modifications at Martin-Omaha as the "B-26B-1s"
had.
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B-26B-3
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- 41-17625
(1)
- 41-17947
to 41-17973 (27)
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First
examples of the slightly-modified Pratt & Whitney
R-2800-43 engine (2,000 hp takeoff-rated) became available
in the fall of '42, and the Army ordered them installed
on 28 Marauders, designated B-26B-3s.
Most
of the B-26B-3s destined for overseas were also modified
at Martin-Omaha as the "B-26B-1s" had been.
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B-26B-4
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- 41-17974
to 41-18184 (211)
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Production
of the B-26B-4 variant commenced at Baltimore with the
431st aircraft of the "B" series in September,
1942. Two hundred eleven were built.
The
most significant and noticeable change was an attempt
to improve takeoff performance by lengthening the nose
wheel strut six inches. This gave the B-26B-4 a distinct
"nose-up" attitude on the ground. A "bump"
had to be built into the nose gear doors to the front
to clear the repositioned retracting mechanism.
Mechanically
operated main wheel landing gear doors were incorporated
starting with this variant. Built in three sections,
two were closed when the landing gear was extended to
cut drag. Retractable circular air ventilators were
added beside pilot and co-pilot positions.
Weight
of the Marauder had been steadily rising with the addition
of more equipment and armament. Wing loading, which
had been high with the original design, went even higher--to
a nearly unsafe 63 lb./sq. ft. The B-26B-4's wing loading
was exceeded only by the German Do 217 (64 lb./sq. ft.),
highest of all the medium bombers of World War II.
Martin-
Omaha likewise modified many of the North African-bound
B-26B-4s just as It had the "B-26B-1s". In
addition, four forward-firing .50-caliber fixed guns
in "blisters" were mounted on each side of
the fuselage below the radio operator and navigator's
compartment. Armament now totaled twelve Colt-Brownings,
giving the Marauder as much firepower as a fighter!
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B-26C-5-MO
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- 41-34673
to 41-34680 (8)
- 41-34682
to 41-34688 (7)
- 41-34694
(1)
- 41-34696
to 41-34701 (6)
- 41-34743
to 41-34776 (34)
- 41-34788
to 41-34847 (60)
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For
the "long wing" Marauder, Martin was ordered
to increase wing area to 713 sq. ft. by broadening the
chord and lengthening the span to 71 feet. This dropped
wing loading to 51.5. A larger tail was also fitted.
Overall, the plane was 58'-3" long and sat 21'-6"
off the ground. Tread width was nearly 22'. Due to the
larger, and heavier, wing and tail assembly, and the
additional armament and armor, weight increased by 1,500
pounds to 26,300 pounds basic, 31,200 normal (DGW) and
37,000 loaded.
Because
of its greater weight and drag, top speed of a "long
wing" at 15,000 feet declined to 282 mph and cruising
speed dropped to 214 mph. With a load of 4,000 pounds
of bombs and 962 gallons of fuel (no bomb bay tanks),
the "long wing" had an operating range of
550 miles.
A
50-inch tire on a larger wheel replaced the 47-inch
one on the main landing gear. A streamlined "bump"
in wheel well door covers appeared to accommodate the
increased diameter tire. The hydraulic system was improved.
Exhaust flame dampers were added. Generators were upped
from 100 to 200 amps. Easier access was provided to
the nose compartment by reducing the height of the co-pilot's
seat.
The
armament changes Initially done on "B-26B-1s",
plus the package guns of the B-26B-4, were made standard.
In addition, side waist gun doors were enlarged and
moved one station aft to improve the angle of fire down
and to the front. Each would slide up and lock open.
A single larger circular scanning window, replacing
the two smaller ones, was located above each waist door
to give the gunner a better view. Bomb racks, bomb hoisting
equipment and the bombardiers' position were changed.
The optically flat glass In the lower nose transparency
was enlarged and elongated.
Marauders
built at Omaha were now to have the suffix "MO".
The original B-26Cs from the Nebraska plant were subsequently
redesignated B -26C-05-MOs. One hundred seventy-five
examples were built. Main and nose landing gear doors
(all but one section) were made to close when the gear
was extended from the 61st article on.
Fifty-nine Omaha-built
B-26C-5-MOs were substantially
lightened and redesignated B-26C-6-MOs (see next).
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B-26C-6-MO
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- 41-34681
(1)
- 41-34689
to 41-34693 (5)
- 41-34695
(1)
- 41-34702
to 41-34742 (41)
- 41-34777
to 41-34787 (11)
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A
unique Marauder weight reduction modification experiment
was ordered early in 1943 by the AAF In an attempt to
improve landing and takeoff performance. Fifty-nine Omaha-built
B-26C-5-MOs, to be assigned as original equipment for
the England-bound 323rd Bombardment Group, were substantially
lightened. Redesignated B-26C-6-MOs, these Marauders
had no co-pilot; his control column, seat, and armor
plate were removed, as was some equipment such as the
liaison radio set.
After
the first two Squadrons of the 323rd had ferried these
modified Marauders to the U. K. and flown some combat
missions, commanders there objected so strenuously to
the lack of a co-pilot that the experiment was abandoned.
All "single pilot" B-26C-6-MOs were eventually
converted back to two-pilot configuration.
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B-26B-10-MA/B-26C-10-MO
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- 41-18185
to 41-18334 (150 "B" models)
- 41-34848
to 41-34907 (60 "C" models)
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The
last 150 "B" model Marauders (642nd to 791st
articles, 41-18185 through 41-18334) from Middle
River were made as B-26B-10-MAs, Identical to the B-26C-5-
MOs. The first B-10 was accepted January 15, 1943.
The suffix "MA" indicated the planes were
built at Baltimore.
By
March, 1943, Martin-Omaha had made the changes required
by Martin-Baltimore's Engineering Department and began
producing Its B-26C-10-MO model, Identical to the B-26B-10-MA. Sixty were built serialed 41-34848 through 41-34907.
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B-26B-15-MA/B-26C-15-MO
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- 41-31573
to 41-31672 (100 "B" models)
- 41-34908
to 41-34997 (90 "C" models)
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The
block of 100 Baltimore-built Marauders serialed 41-31573
through 41-3 1672 were designated B-26B-15s. They differed
from the B-26B-10 only in having the fixed oxygen system
Type A-9 regulator deleted and improved IFF equipment
(SCR-595A) fitted.
Martin-Omaha
also incorporated these same changes in aircraft 41-34908
through 41-34997, designated B-26C-15-MOs.
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B-26B-20-MA/B-26C-20-MO
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- 41-31673
to 41-31772 (100 "B" models)
- 41-34998
to 41-35172 (175 "C" models)
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Starting
with the B-26B-20-MA and B-26C-20-MO, the hand-held
twin-fifty tall gun position was redesigned and fitted
with a power-operated electro -mechanical Bell type
M-6 turret. The blunt, rounded-off installation visibly
changed the Marauder's tail profile and reduced overall
length to 56 ft. 1 in. Another noticeable external change
was the shorter chord rudder.
One
hundred B-26B-20-MAs were built along with 175 B-26C-20-MOs.
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B-26B-25-MA/B-26C-25-MO
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- 41-31773
to 41-31872 (100 "B" models)
- 41-35173
to 41-35372 (200 "C" models)
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The
one hundred B-26B-25-MAs and 200 equivalent B-26C-25-MOs
featured more armor plate on the Martin 250CE turret.
Some
of these aircraft destined for Stateside training and
other non-combat uses were not fitted with the Bell
tail turret. On the C-25-MOs headed for the MTO, Martin-Omaha
fitted a shell collector pan beneath the tail guns.
Three
B-26C-25-MOs, serials 41-35370 through 41-35372, were
converted to AT-23Bs.
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B-26B-30-MA/B-26C-30-MO
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- 41-31873
to 41-31972 (100 "B" models)
- 41-35373
to 41-35572 (200 "C" models)
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Starting
with this model, a curved piece of armor plate was mounted
externally to the left side of the fuselage to protect
the pilot. Armor was also added behind the bombardier
and around vital mechanical parts of the plane in several
locations.
One
hundred B-26B-30-MAs were built at Baltimore while 200
B-26C-30-MOs were made by Martin-Nebraska.
Forty-eight
of the B-26C-30-MOs were converted to AT-23Bs, serialed
41-35525 through 41-35572. And 100 C-30s were furnished
to the RAF as Marauder IIs, FB 418-517.
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B-26B-35-MA/B-26C-35-MO
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- 41-31973
to 41-32072 (100 "B" model)
- 41-35573
to 41-35772 (200 "C" models)
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The
carburetor alcohol de-icing system was eliminated and
that was the only change in this block of 100 B-26B-35-MAs
and 200 identical B-26C-35-MOs.
23
aircraft, 41-35598 through 41-35620, were converted
from B-26C-35-MOs to AT-23Bs at Martin-Omaha.
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B-26B-40-MA/B-26C-40-MO
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- 42-43260
to 42-43459 (200 "B" models)
- 41-35773
to 41-35872 (100 "C" models)
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A
torpedo -firing switch was added to the pilot's control
column with this version and the type B-2 Torpedo Director
was discontinued. The carburetor air duct was revised
for hot air de-icing from the middle of this block (42-43320)
forward. One external change on this model was noticeable:
"shark nose" ailerons were fitted from 42-43310
on.
Martin-Baltimore
built 200 B-26B-40-MAs. A total of 141 of these planes
were converted to AT-23As, serials 42-43319 through
42-43459.
Martin-Nebraska
manufactured 100 B-26C-40-MOs and all were subsequently
converted to AT-23Bs.
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B-26B-45-MA/B-26C-45-MO
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- 42-95629
to 42-95828 (200 "B" models)
- 42-107497
to 42-107855 (359 "C" models)
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On
this block of Marauders, the pilot was provided with
a ring-and-head sight for his package guns. Increased
strength bomb hooks for the B-10 shackles were fitted.
IFF radio equipment SCR-695 was supplied and the new
SCR-522 VHF Command radio set with accessories was added.
The engine fire extinguisher was reinstated as standard.
A remote heading compass was fitted.
With
the requirement for carrying thirty 100-pound bombs
dropped by the AAF as a result of combat experience,
the Marauder's aft bomb bay was sealed up from this
variant on. That bay hereafter held tail gun ammo. A
special track was installed to carry the .50-caliber
bullets some 30 feet back to the tail gun position.
The
fixed .50-caliber machine gun In the nose was deleted
in the middle of the production run (from 42-95979).
A
total of 200 B-26B-45-MAs were built. One hundred nine
of these aircraft, 42-95629 through 42-95737, were subsequently
converted to AT-23As. All told, 359 B-26C-45-MOs were
built. The last 26 in the block, serials 42-107856 through
42-107881, were made as AT-23Bs.
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B-26B-50-MA
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- 42-95829
to 42-96028 (200)
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An
emergency mechanical bomb bay door closing arrangement
was provided from this block on IFF gear was revised.
Lycoming propeller blades began to be fitted from a/c
42-95942.
Two
hundred B-26B-50-MAs were built at Baltimore.
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B-26B-55-MA
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- 42-96029
to 42-96228 (200)
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The
D-8 bombsight was discontinued with this model and the
M-series was fitted instead. Specification changes in
the Martin CE 250 top gun turret (optical sight, etc.)
were incorporated from a/c 42-96079 on. In a major change,
camouflage paint was completely deleted by Martin-Baltimore
from 42-96129 on. Two hundred B-26B-55-MAs were manufactured.
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B-26F-1-MA
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- 42-96229
to 42-96328 (100)
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The
B-26F- 1 -MA, which started to come off the Middle River
line in February, 1944, featured the last major structural
change in the Marauder: wing Incidence (angle to the
fuselage) was Increased by 3 1/2 degrees to 7 degrees.
The "twisted wing" (besides giving greater
propeller ground clearance) Improved lift characteristics,
reducing takeoff run length and lowering landing speed.
In the air the "F" flew fairly level--the
tail was up slightly- -and the plane no longer gave
pilots the feeling that It was riding "nose high".
Disadvantages: top speed was lowered some to 277 m.p.h.
and the new model didn't handle quite as well.
Torpedo
shackles were deleted from this model on. An all-electric
bomb release system was now furnished. Starting with
a/c 42-96231, a revised oil cooler with thermostatic
control and surge valve was fitted, along with wing
bottom panels redesigned for easier removal. Instrument
panel changes were made; trailing antenna was made removable.
The
B-26F-1-MA had provisions for a revised fuel transfer
system. Gasoline tanks were redesigned to permit inter-connection,
although this system was not actually hooked up on this
variant. Up to this time emergency extension of the
main landing gear had been left to gravity, but this
didn't always work. The "F" was fitted with
a mechanical means of lowering the main gear in an emergency.
In
all, 100 B-26F-1-MAs were built for the USAAF by Martin-Baltimore.
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B-26F-2-MA/B-26F-6-MA
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- 42-96329
to 42-96428 (100)
- 42-96429
to 42-96528 (100)
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These
two identical blocks of 100 aircraft each were built
for the RAF and SAAF as Marauder IIIs, serialed HD
402 through HD 601.
The
Bell M-6 power-boost tail turret was deleted from this
block forward, replaced by the M-6A, a modified version
with a flexible canvas cover over the end of the gun
position. Provision was made for fitting optical gun
sights on flexible machine guns. The T-1 bombsight was
installed instead of the M-series. Provisions for British
nose and tail bomb fusing and B-9 shackles were made.
Radio equipment was changed to British standards.
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B-26G-1-MA
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- 43-34115
to 43-34214 (100)
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The
B-26G series began being built at Baltimore in March,
1944. It differed from the B-26F only in equipment details.
Externally they were identical. An armor "blanket"
was added to protect the fuselage from the blast of
the package guns. Marauders of this block, at the request
of the Ninth Air Force (a/c 43-34190 on) were equipped
with the C-1 Automatic Pilot.
Partial
top-surface camouflage paint was applied at the factory.
Inboard and outboard wing fuel tanks were, hereafter,
interconnected. Universal "Army/Navy" instead
of "Air Corps" equipment was fitted. A larger
life raft compartment was provided in the top section
of the forward fuselage of the B-26G-1-MA. This compartment
took an A-3 or E-2 rubber dinghy, and offered stowage
for all required provisions, including a dinghy radio.
One
hundred B-26G-1-MAs were built.
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B-26G-5-MA
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- 43-34215
to 43-34414
(200)
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The
two hundred B-26G-5-MAs built had only minor hydraulic
system changes.
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B-26G-10-MA/B-26G-11-MA
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- 43-34415
to 43-34539 (125 G-10 models)
- 43-34540
to 43-34614 (75 G-11 models)
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One
hundred twenty-five of the B-26G-10-MA variant were
built for the USAAF while an additional 75 B-26G-11-MAs,
went to the RAF as Marauder Ills, HD 602-676.
A
tail gun shell collector pan was fitted as standard
below the position on the bottom of the fuselage. The
lock valve cowl flap system was deleted from 43-34575
on. Some planes were furnished with Lycoming prop blades.
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B-26G-15-MA/TB-26G-15-MA
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- 44-67805
to 44-67954 (150)
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With
this model, the C-1 Automatic Pilot was deleted, along
with the portable system outlets. The radio compass
was changed. One hundred fifty B-26G-15-MAs were built.
The last ten of these aircraft (44-67945 through 44-67954),
were designated TB-26-15-MAs after being modified in
November, 1944, for training and target-tow duties.
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B-26G-20-MA/TB-26G-20-MA/B-26G-21-MA
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- 44-67970
to 44-67989 & 44-68065
to 44-68104 (60
B-26G-20-MA)
- 44-67955
to 44-67969 (15 TB-26G-20-MA)
- 44-67990
to 44-68064 (75
B-26G-21-MA)
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Whip-type
static dischargers were the only additions to this model,
150 examples of which were made.
Fifteen
planes of this block (44-67955 through 44-67969) were
built as TB-26G-20-MAs. And 75 were designated B-26G-21-MAs
(44-67990 through 44-68064) and turned over to the RAF
where they were serialled HD 677-751 and called Marauder
IIIs.
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B-26G-25-MA/TB-26G-25-MA
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- 44-68105
to 44-68254 (150)
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Last
variant off the line, the B-26G-25-MA had only a few
minor changes to distinguish it from its immediate predecessors.
Of the 150 examples, thirty-two (44-68222 through 44-68253)
were stripped of armament and operational equipment
in March, 1945, to serve as TB-26G-25-MA trainers and
target tugs.
The
last Marauder built left Martin April 18, 1945. It was
B-26G-25-MA 44-68254 named "Tail End Charlie"
and "30".
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Text
from The
Martin Marauder
B-26 by Victor C. Tannehill
Copyright(c) 2008 320th History Preservation. All rights reserved.
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