Category And Colors

1942 The First Full Year of Combat

1942 The First Full Year of Combat

The beginning of 1942 was not much better for the USAAF as the Japanese pushed deeper into the Philippines, most of the US aircraft being destroyed on the ground or overwhelmed in the air. The islands were finally overrun in May, but a short while before, Gen. Doolittle led sixteen B-25 medium bombers on a daring raid on Japan, made from the deck of the US Navy carrier Hornet. This was a real morale booster at a time when it was badly needed. The battle of the Coral Sea in May, followed by that of Midway in June, marked the turning point of the war in the Pacific, and finally al­lowed the new Eighth Air Force to be sent to England to commence operations against Germany.

On the eastern front the Russians had launched their first ma­jor winter counter-attack at the beginning of 1942 against the Ger­man Army around Moscow, causing its first major retreat of the war.

Later in the year, in North Africa, British Gen. Montgomery’s victory at El Alamein, Libya, in October started the final Axis re­treat across North Africa and paved the way for the Allied opera­tion “Torch”, under Gen. Eisenhower, the invasion of Northwest Africa on November 8, 1942.

At the end of 1942, the German Army got mired down in Stalingrad, paving the way for more Russian winter offensives.

The USAAF emphasis on production and training began to show results and by June, its strength had more than tripled to a total of more than 21,00(1 aircraft, including more than 12,000 train­ers. More than 140 aircraft were lost in combat over Europe and North Africa, while nearly three times as many, 341, were lost in the war against Japan.

During 1942, the results of combat experience resulted in the following major changes in the marking and camouflaging of USAAF aircraft:

Anti-submarine white camouflage evolved.

Blue haze paint tested for use on F-4 reconnaissance aircraft. “U. S.ARMY” underwing markings deleted from combat aircraft, May.

Red center removed from cocarde, rudder stripes deleted from com­bat aircraft. May.

Medium Green patches added to wing and tail surfaces of combat aircraft, July.

Camouflage colors standardized for all USA produced Allied air­craft, July.

Red center dot removed from cocarde and rudder stripes deleted from all aircraft, July.

Blue and yellow finish for primary and basic trainers deleted, Sep­tember.

Yellow outer ring added to fuselage cocarde in Europe and North Africa, September.

“U. S.ARMY” underwing markings deleted from all aircraft, Octo­ber.

Spec. No.

Jan. Feb.

Mar. Apr.

May June

Jul. Aug.

Sep. Oct.

Nov. Dec.

T. O. 07-1-1

Markings, Insignia, & Camouflage

New Issue |

A В | |

Bulletin 41

Colors for

Camouflage

Finishes

1

|

A

|

Bulletin 48

Colors for Temporary Camouflage Finishes

Issued May. 1

A-N

Porcelain Color Plates

Spec. 3-1

Color Card

24102

National

Insignia

3

|

4

|

L

|

24105

Markings for Airplanes

f

24113

Color for Army Air Corps Airplanes

6

|

24114

Camouflage Finishes for Aircraft

A

|

US Army Air Forces specifications in use, revised, or issued, by date and version,

during 1942. The letters indicate a letter revision of a spec., such as T. O. 07-1-1 A. The numbers indicate an amendment to an earlier version of a spec., such as Amendment No. 6 to Spec. 24114.

image89

Curtiss P-40-CU used as a training aircraft by the 54PG, at Hamilton Field, California, in early 1942. It is interesting to note that the cocarde underthe left wing and the old designator markings have been painted out, though very thinly, and that the neutral gray paint sweeps up to the horizontal stabilizer, identifying this as one of the original camouflaged P-40s. (USAF)

* * *

AAF Eastern Theater Of Operations orders camouflage paint to be applied immediately on all aircraft, January 1,1942.

Gen. Krogstad, commander of the First Air Force, requested that the First Bomber Command, Langley Field, VA„ take immediate action to have the prescribed camouflage applied to all of its aircraft immediately. This memo went to the 34th Bomb Gp, Westover Field, MA, the 43rd Bomb Gp, Bangor, ME, the 13th Reconn. Sq, Bangor, ME, and the 2nd Bomb Gp, Langley Field, VA.

Spec. No. 9S-24102-L, issued on November 10,1942, revises requirements for star insignia

The latest version of the “Insignia for Aircraft” spec, required that the material for the insignia should be paint, dope, lacquer, or enamel, consistent with the general finish of the aircraft. Decalcomania transfers could be used if approved by the USAAF. On the wings, it was specified that one star-insignia was to be placed on the upper left wing surface, and one on the under right wing surface with a point forward. For application to wood surfaces it was required that the wood surface be properly sealed, as detailed in Spec. 24115. Finally, it was pointed out that the insignia required by the spec, had been known by various names such as “cocarde” and” wing insignia”. It was now to be referred to as the “star-insignia”.

image164

Republic RP-47B-REs, 41-6002, 41-5999, 41-6001, etc. White aircraft numbers 1, 24, 25,32, are visible. The nearest aircraft has the squadron leader bands in red, yellow, and dark blue on the rear fuselage, and on the engine cowl. They are from the 56th PG, originally formed to defend the Republic plant on Long Island. Lt. Col. Zemke is flying number “1" aircraft. (USAF via Gerry R. Markgraf)

Dir. of Mil. Req. (Wash.) orders discrepancies in Tech Orders covering camouflage to be corrected, November 13, 1942.

Gen. Fairchild wrote to the CG, Mat. Com., (Wash.) on November 13,1942, that there were several discrepancies in the existing Techni­cal Orders that needed to be corrected. He then issued a revised 11-1111, Addition No. 1, dated November 20, 1942, directing that changes were necessary in existing Technical Orders to meet the current camouflage requirements. These were:

Existing Technical Orders did not prescribe the method of eliminating the boundary line between colors on camouflaged aircraft.

There was no indication that any action had been taken regarding the use of infra-red camouflage paint as recommended by Dir. of Mil. Req.

Aircraft delivered from the factories were camouflaged in the prescribed method, but those re-finished by subdepots did not meet speci­fications.

Current instructions from Mat. Com. indicated that there was no longer a requirement for haze paint for AAF aircraft.

Methods for camouflage of anti-submarine aircraft should be covered in Technical Orders.

MARKINGS AND INSIGNIA

3. MARKINGS

a. Each part and assembly will be permanently and legibly marked the same number as the drawing number in such location that it can be read after assembly in the unit. (See Specification No. 98-24105Q.)

b. Various detail and code markings for the cockpit, fuselage, oil lines, etc., as required in Specification No. 98-241050, will be maintained.

c. Radio call letters of not less than four numbers, utilizing both sides or each outboard side, as applicable, of vertical stabilizer and rudder assembly, will be maintained on all Army Air Forces aircraft. (See figures 8 and 10.) Call letters, or designators, will be derived by deletion of the first numeral of serial number (4) and the hyphen, and the combination of the remaining four or more numerals. In case of serial numbers of type 41-7, use zero as necessary to make four numerals, as 1007. Decalcomanias may be used in all cases where available. Standard sizes 8 x 12 inches and 6×9 inches may be used when present stocks are depleted. Colors will be yellow, shade No. 48, for dark camou­flage, and black, shade No. 44, for light surfaces.

d. Under no condition will the letters “U. S. Army” be applied to any airplane lower wing surface.

4. STANDARD INSIGNIA.

Cocardes, the five-point white star within a blue circle, will be placed and maintained on each Army Air Forces aircraft as indicated in the following paragraphs, Decalcomanias will be used in all cases where available

WARNING

Under no condition will the red circle within the white star be used.

a. WINGS.—Insignia of a size 80 to 90 percent of available width of wing at location specified herein will be maintained on top surface of left wing and lower surface of right wing with point forward. The center will be located inboard from each wing tip one-sixteenth of the total wing span on wings not tapered, but with outside edge not nearer

image204

FIGURE 7 FIGURE 8

 

than 6 inches to end, and one-eighth of span on tapered wing. The cocarde will be located tangent to the aileron cut­out or midway of the wing width on those on which aileron cut-out is not a factor. (See figures 7 and 8.)

b. FUSELAGE.—One star insignia approximately 75 percent of height of fuselage will be applied to each side with point upward near-midway between the trailing edge of the wing and the leading edge of the horizontal stabilizer. (See figure 8.)

c. Подпись: FIGURE 10
RUDDER STRIPES.—The use of rudder stripes is prohibited.

FIGURE 9

5. ORGANIZATIONAL INSIGNIA.

a. The placing of organizational markings or design (approved by the War Department as outlined in Army Air Forces Regulation 35-32) will be the responsibility of the organization itself. Depots will not be required to reproduce this insignia.

b. No specific locations are mandatory but points between wing and tail surfaces on opposite sides of the fuselage are considered most desirable. In no case will size of insignia exceed 75 percent of height of fuselage at point of application. Similar planes in the same organization will have the same size insignia.

c. If applied to other than smooth surfaces, insignia may be painted on thin aluminum sheet and bolted or screwed securely to rigid members of the airplane.

6. DECALCOMANIAS.

The use of decalcomanias for standard or organizational insignia (T, O. No. 01-1-21), and markings is authorized. Instructions for application should be printed on the reverse side of the various types; however, in event of any confusion the Commanding General, Air Service Command, Patterson Field, Fairfield, Ohio; Attention: Chief, Miscellaneous Equipment Section, will be notified giving Purchase Order number, type, and

size.

SECTION III

Deletion of camouflage on A-20 aircraft leads to considerable detail changes, detailed in AAF-Douglas Aircraft correspondence, December 8-20, 1943

The AAF Material Command wrote to Douglas Aircraft Co., Santa Monica, on December 8,1943, concerning the deletion of camouflage on A-20G, A-20J, A-20H, and A-20K aircraft. This letter stated that higher authority had directed that camouflage was to be deleted from all of these versions, at the earliest possible date without delaying production. Only aircraft destined for Russia were to be camouflaged; this was to be applied to aircraft at the Douglas plant if possible, however, it could be done at the Modification Center.

It was also required to delete camouflage from all spares shipped with uncamouflaged aircraft (except for the Russian aircraft). Basically, exterior surfaces of fabric, plywood, wood, magnesium and unclad dural were to be treated with primer and aluminized finishes, while exterior alclad and stainless steel surfaces would not need any finish. Black anti-glare paint was required on top of the fuselage to cover forward areas seen by the pilot.

Douglas were to deliver all aircraft with a uniform color of finish, i. e., no aircraft were to be delivered with some assemblies camouflaged and some not. No existing camouflaged parts or assemblies were to be scrapped. Propellers were to remain black with yellow tips. If existing camouflaged parts in stock would cause a marked delay in carrying out these orders, Douglas was to remove the camouflage or refinish them to an aluminum color without delaying aircraft deliveries.

Douglas was also told to not irrevocably convert its camouflaging facilities to other uses (presumably in case it became necessary to use camouflage finishes at a later date). They were asked to let the Material Command know when they could deliver completely uncamouflaged aircraft so that the necessary contract changes could be issued.

Enclosed with the letter was a sheet containing instructions for the removal of the camouflage. This agreed with the details in the letter, except for two areas. The instruction sheet called for the use of “Dark Green” anti-glare paint on the top of the forward fuselage, whereas the letter had asked for “Black” paint, and it also required the removal of camouflage from spinners (apparently, even higher authorities got their signals crossed!).

This anti-glare paint disagreement was resolved by a letter from Wright Field, dated December 13, 1943, which directed that all A – 20G and A-20H aircraft having camouflage deleted required Olive Drab No. 613 anti-glare paint on top of the fuselage and inboard side of nacelles, forward of the wing leading edge, to cover forward and lateral vision areas seen by the pilot. It also stated that in addition to “Moth” (P-70) aircraft, it was still necessary to camouflage all Lease-Lend aircraft.

The general confusion over details of camouflaging production aircraft continued, and Douglas Aircraft found it necessary to ask the Material Center to clarify the situation in a letter dated December 15, 1943, This stated that an AAF letter directed that standard A-20 camouflage should be applied to all P-70 aircraft. Other AAF directives stated that Lend-Lease and “Moth” aircraft only should be camouflaged. They received a reply from Material Command on December 17,1943, stating that camouflage was required on all the P­70 night fighter versions. In turn, on December 20, 1943, they acknowledged the directives received, stated that they were determining the effective dates for deletion of camouflage on the A-20G, H, J, and К versions. They also requested immediate official contract authority for the change, so that they could implement it without delay.

This correspondence clearly shows the time involved in contract changes at that time, due to transit times for mail, even with the use of teletypes.

image253

North American B-25H-5-NA, 43-4550, is seen in the new natural metal finish, without camouflage, as ordered in September 1943. (Nick Williams)

 

Revised ANA Bulletin No. 157a, lists AAF, Navy, and British equivalent or superseded colors, and changes color 619 to “Bright Red” from “Insignia Red,” March, 1944

On March 24,1944, a revised ANA Bulletin No. 157a, Standard Aircraft Camouflage Colors, added atable showing the AAF and Bureau of Aeronautics colors equivalent to or superseded by these standard camouflage colors. The British nearest equivalent colors were also listed and were those for which the AN standard colors could be substituted. The name of color 619 was changed to read “Bright Red” in place of “Insignia Red”. A paragraph titled “Color Match” was also added and read as follows:

In order to determine color matches the subject standards shall be compared with the dry paint film under test by viewing un­der diffuse daylight illumination. The illumination shall be equivalent to International Commission on Illumination Illuminant “C” obtained from north sky light or suitably filtered artificial sources. The line of sight should be normal to the plane of the specimen and the standard. No water, oil or other means of moistening the surfaces shall be used. Color standards should be handled by the edges and suitable precautions taken to minimize drift due to exposure, soil, rubbing or other cause.

The added table read as follows:

A-N Aircraft Standard

Nearest Equivalent

or Superceded

Color

ARMY AIR FORCES (1)

Bureau of Aeronautics

British (2)

601 Insignia White

602 Light Gray

Insignia White 46

Insignia White Light Gray

White

Neutral Gray 43

Extra Dark Sea

603 Sea Gray

Gray, Dark Sea Gray and Ocean Gray

604 Black

Black 44

Black

Black

605 Insignia Blue

606 Semi-Gloss Sea Blue

Insignia Blue 47

Insignia Blue Semi-Gloss Sea Blue

Dull Blue

607 Non-Specular Sea Blue

608 Intermediate Blue

Non-Specular Sea Blue, Dark Blue and Blue Gray Intermediate Blue

609 Azure Blue

610 Sky

Light Blue

Azure Blue and Deep Sky Sky

(3)

Medium Green 42

(3)

Light Green

611 Interior Green

612 Medium Green

(3)

613 Olive Drab

Dark Olive Drab 41

Dark Slate Gray and Dark Green

614 Orange Yellow

615 Middlestone

Identification Yellow 48

Orange Yellow

Yellow

Middlestone

Sand 49

616 Sand

Dark Earth

617 Dark Earth

618 Dull Red

Insignia Red 45

Insignia Red

Red

619 Bright Red {formerly

Insignia Red (4)

called Insignia Red)

NOTES: (1) AAF Bulletin No. 41

(2) Ministry of Aircraft Production Color Standards.

(3) 611 Interior Green is intended for standardization of the product obtained by tinting zinc chromate primer, Spec. AN-TT-P-656, for shop coat or interior finish purposes.

(4) 619 Bright Red (formerly called Insignia Red) is intended for use as specified by the Bureau of Aeronautics.

Boeing B-17G-75-BO, 42-37938, aircraft OR-E of the 323rd BS, 91st BG, at Bassing bourne, England, on June 6,1944, awaiting its next mission. Note that most of the aircraft behind are now in natural metal finish. (USAF)

image297

Consolidated B-24J-180-CO, 44-40791, aircraft “Playmate”, of the 867th BS, 494th BG, Seventh AF, was in natural metal finish. Note the slight kink in the fuselage bottom line with introduction of the nose turret on the B-24. (USAF via Gerry R, Markgraf)

Conservation of Alkyd Resin Paint Materials ordered, February 1945

Anew technical order, T, 0.07-1-13, was issued on February 1,1945. It stated that due to the strategic nature of the following alkyd resin paint materials, their use was to be kept to a minimum and restricted to aircraft, and aircraft accessories and parts. The list which followed included the aircraft camouflage enamels, gloss enamels, heat resisting enamels, zinc chromate primers, glyceryl phthalate varnishes, and all aircraft lacquers.

These materials were required for use on aircraft and aircraft parts and were not to be used on equipment, vehicles and buildings. Large stocks of these materials were not to be accumulated at any supply or maintenance activity. Lacquer could be applied over old lacquer with no zinc chromate primer as long as the surfaces were properly cleaned.

Spec. 98-24113-B revised to add new requirements for the interior finish of all aircraft, April 1945.

Amendment No. 2 to spec. 98-24113-B was issued on April 6,1945, and added three new paragraphs containing new requirements for the interior finishes of all AAF aircraft. They read as follows (paraphrased to shorten the official verbiage):

E-la. All interior parts of airplanes, which by reflection may be seen in the glass of windshields, cockpit enclosures, turrets, armor glass, etc., shall have one coat of zinc chromate primer, and are then to have two coats of camouflage lacquer or one coat of camouflage enamel. The color is to be black, shade no. 604 of Bulletin No. 157.

E-lb. All interior portions of cockpits, enclosure decks, turrets, engineers’, bombardiers’,and navigators’ stations, etc,, of air­planes (which are visible to crew members in flight, and are subject to direct rays of the sun) shall have one coat of zinc chromate primer, followed by two coats of camouflage lacquer or one coat of camouflage enamel. The color shall be medium green, shade no. 612 of Bulletin No. 157

image387

North American P-51B-5-NA, 44-13693, aircraft FT-1 “Angels Playmate” of the 353rd FS, 354th FG, Ninth Air Force, at strip A-98, Rosieres – en-Haye, France in February 1945. This was the aircraft of Lt. Bruce W. Carr, leading Ninth Air Force Ace w ith 14 victories. Spinner and nose band were yellow. (William L. Swisher)

 

image388

image389

Very rare photograph of a Martin AT-23B-MO, 41*35768, complete with camouflage and somewhat modified invasion stripes on fuselage. Seen in February 1945, at strip Y-32, Ophaven, Belgium, it was a gunnery training/’tow target version of the B-26C-MO. 375 were built, of which 225 went to the Navy as JM-ls. (William L. Swisher)

E-lc. The requirements in the above paragraphs for supplemental finishes on the interior of airplanes do not apply to electrical cables or other equipment whose operational functionality or reliability may be affected by overpainting.

DESIGN REQUIREMENTS

D-l. Markings for Large Seaplanes and Amphibians.

D-la. Wing Tips.-

D-la(l). Wing tip floats and struts shall be painted orange-yellow.

D-la(2). Upper and lower surfaces of both wing tips shall be painted orange-yellow from the wing tip inboard a distance equal to 7 percent of the total wing span (float excluded). A black border 6 inches in width shall be added inboard.

D-lb. Wing, Center Section (Upper Surface Only).

D-lb(l). The upper surface of the center section, including the rear projection portion of the engine nacelles, shall be painted orange-yellow to a distance just outboard of the two inboard engine nacelles, A black border 6 inches in width shall be added outboard.

image438

Lockheed P-80A-1-LO, 44-85004, was the thirteenth one built and was significant as being the first jet fighter to enter service with the AAF. The initial jet fighters for the AAF were puttied all over and finished with a very smooth ANA 602 light gray finish to improve performance. However, this finish quickly became chipped and scarred in service and was soon discarded. (March AFB Museum)

D-lb(2). On the upper surface, the word “RESCUE” shall be superimposed in black. Centered aft of the word “RESCUE”, the appropriate identification numerals and/or letters shall be added. Letters and numerals shall be of the modified vertical block type, uniform in shape and size, and shall be 36 inches high, 27 inches wide, and the width of the individual strokes forming them shall be 6 inches. The spacing between letters shall be 12 inches.

D-lc. Hull.-

D-lc(l). Hull (Rear Section).- A 36-inch orange-yellow band, approximately three feet forward of the leading edge of the hori­zontal stabilizer, shall encircle the aft portion of the hull, but not extend onto the last step or keel. Two 6-inch black stripes shall be added as borders.

D-lc(2). Hull (Forward Section).- On each side of the forward part of the hull and centered between the leading edge of the wing and the bow, an orange-yellow rectangle, whose length shall be equal to three times its height, shall be painted. Atwo-inch black stripe shall border the rectangle. The height of the rectangle shall be 33 percent of the vertical dimension of the projection of the fuselage side at the point of application, except that the height of this rectangle shall be not greater than 36 nor less than 20 inches excluding the border. The rectangle shall be located as near as possible to the center of the vertical projection of the fuselage at the point of application. The national aircraft insignia, which normally would occupy this space, shall be located aft on the hull to clear this marking.

D-lc(2)a. Identification Numbers.- The Air-Sea-Rescue identification numbers and/or letters shall be of the modified vertical block type, uniform in shape and size, and shall be approximately 2/3 of the height of the orange-yellow rectangle. The width of the letters and numerals shall be 3/4 of the height and the width of the individual strokes forming them shall be 1/6 of the height. The letters’and numerals shall be appropriately spaced.

D-lc(3). Hull (Bottom Section).- On the bottom of the hull, between the bow and the main step, and extending from chine to chine, the Air-Sea-Rcscue identification numerals and/or letters shall be painted. The top of the letters and/or numerals shall be at the port chine of the hull. Letters and numerals shall be orange-yellow, bordered by a two-inch black stripe. The width of the letters and numerals shall be 3/4 of the height, and the width of the individual strokes forming them shall be 1/6 of the height. The letters and numerals shall be appropriately spaced.

D-2. Markings for Other Aircraft.- The markings, as specified above, shall be used as appropriate to the size and shape of the aircraft.

Lockheed P-80A-1-LO, 44-85168, 44-85154, 44-85167, 44-85093, 44-85089, and 44-85160 of the 1st FG, being serviced on the ramp at March Field, California, in the summer ofl 946. Two others are flying overhead. The first unit to be equipped with the P-80, it moved to George AFB in July, 1950. (March AFB Museum)

image439

image440

Boeing B-29-55-MO, aircraft 6383 of the famous 509th Composite Group, attached to the 3I3th Wing, Twentieth Air Force, in June 1945. It has black and red bands around the rear fuselage. This aircraft is marked with the group’s arrowhead marking. It is finished in Jet 622 Gloss Black on all lower surfaces. Note the atomic explosion insignia on fuselage. Seen after August, 1945. (USAF via Gerry R. Markgraf)

White and Haze Paints tested on Pursuit Aircraft, January 1942

Exp. Eng. Sect. (WF), investigated the method for camouflaging pursuit aircraft which were being used in studies of photographic installations. Two kinds of paint were used for the tests, namely:

(1) Cabot Haze Paint, which was a colloidal dispersion of zinc oxide in oil. The plane had a bluish appearance (sky) when the paint was applied in a thin coating over a black background.

(2) A pinkish white and a micaceous paint procured from the Lowe Bros. Paint Co, Dayton, Ohio (hereafter Lowe Bros.) The tentative conclusions were that a flat white camouflage paint was most suitable for camouflage against clouds and the haze paint was preferable for blue-sky conditions. Exp. Eng. Sect, stated that further tests would be conducted to ascertain satisfactory results.

image90

North American B-2SA-NA, one of forty buiit before production shifted to the improved B-25B-NA version. The beam and ventral gun posi­tions of the B-25A were replaced on the B-25B by dorsal and ventral gun turrets with two 0.5 inch guns each. (March AFB Museum)

Permanent Camouflage Paints tested in Florida, January 1942.

Suitable finishes for permanent camouflage of aircraft were discussed in a report prepared by WF. Laboratory tests of applications and removal, adhesion, durability and optical reflection characteristics were included in the investigation. WF concluded that, after five months of Florida exposure, permanent materials, of low gloss, color retention and satisfactory adhesion, had been developed, A method of measuring the specular gloss of camouflage finishes had also been developed.

image91

Six of the sixteen B-25B-NAs on (he deck of the USS Hornet, Only visible radio call number is 40-2283. (USAF)

image92Two of the B-25B-NA* of Col. Jimmy Doolittle’s Tokyo strike force on the deck of the carrier CSS Hornet, on April 18,1942. The right aircraft is 40-2282. Note how crammed the aircraft were on the deck. (USAF)

Nose art on one of the Doolittle B-25B-NAS, appears to be painted in vvhitc. This attack achieved little in damage to Japan, but it came as a tremendous morale booster at a sorely needed time, and showed the Japanese that they were also now susceptible to attack by LIS forces. (1ISAF)

 

image93

image94

Douglas B-18B-DO, 37-530, in Theater 5, the Caribbean and British West Indies area. It is fitted with a very early MAD {Magnetic Anomaly Detection) boom, which appears to have its cover installed upside down. Although it has the post May 1942 cocarde without the red center circle, it is still in dark olive drab and neutral gray finish, despite the drive for a white anti-submarine aircraft finish. (USAF)

Request by the RAF for standardization of B-I7E camouflage, January 28,1942.

The RAF requested that the JAC make another effort to standardize the camouflage being applied to B-17Es at the modification centers, commenting that the previous differences of location of operational units of the two countries did not now apply, so it should be possible to find a common camouflage scheme for each class of aircraft. Under the aircraft allocation pooling then in force, it was difficult to paint different patterns at the manufacturing plants.

Technical Sub-Committee On Camouflage decides that the AAF basic camouflage scheme and the U. S. Navy basic camouflage scheme be accepted as the production standard for all aircraft produced in the U. S. March 5, 1942.

The Technical Sub-Committee on Camouflage met on March 5, 1942, to discuss the problems raised by the British Air Committee requiring that British camouflage schemes be painted at the factory on all aircraft destined for the RAF and FAA. This was to be applied

image95

A Curtiss P-40E, ‘585’, being towed in Alaska. It has the famous Aleutian Tiger markings, plus white stripes on the fuselage and rudder. Note the blue and gray PBY in the background. (USAF)

image96

Convair B-24E-DTs on the new production line at the Douglas Tulsa plant in 1942. Ten B-24Ds and 167 B-24Es were built on this line before shifting to the later B-24H version. This photo is a graphic reminder of the enormous production capacity of the US aircraft industry, built up by joint planning between the ЛАТ and civilian industry. More B-24s were built than any other US aircraft in World War 11, but it was taken out of service almost overnight at the end of the war. (Harry Gann)

either before the aircraft left the U. S. or after it reached the British theater of war. The British also stated that it was impossible for them to accept the U. S. camouflage schemes operationally.

The Sub-Committee decided that it was impracticable to adopt the British schemes as standard, because that system was based on the Service being able to anticipate the aircraft’s operational theater or role while it was being completed at the manufacturer.

They then considered camouflage schemes which could be used as a basis for all aircraft and could be converted to other services requirements with the least difficulty. It was agreed that this consideration could be converted into two standard basic schemes, (1) camouflage for land based aircraft, (2) camouflage for ship based aircraft, this to also include flying boats.

The British representative stated that 70% of the British camouflage schemes used a “Dark Green,” which was very similar to the Army dark olive drab, thus they could accept this in lieu of the Dark Green throughout the camouflage programs. For ship based aircraft, the British stated that the U. S, Navy colors would be acceptable.

The current policy of pooling all aircraft production was given as a very strong reason to accept the two basic camouflage schemes, and this was accepted by all present. It was also recommended that the requirements for insignia and markings of a particular Service be accomplished as follows:

a. When the allocation of aircraft was determined before production was complete, the insignia and markings of a particular Service would be applied at the factory.

b. When an aircraft was diverted from one service to another, the change of insignia and markings would be made at the modification centers.

In conclusion, the British representatives at the meeting agreed to submit the U. S. Navy camouflage system to the authorities in Great Britain for a decision as to whether or not it was acceptable. It was also agreed that the British would submit to the U. S. Army their specific requirements for camouflage on all types of Army aircraft in production in the US.

image97

One North American B-25C-NA, 41-12848, with two B-25Ds, operating in the anti-submarine role. B-2SD-1-NC, 41-29917, has no ventral turret, while B-25D-20-NC, 41-30583 has both ventral and dorsal turrets. The latter aircraft were the Kansas city built version of the B-25C. Note the white anti-submarine finish on the B-25C. (Harry Gann)

Responsibility for Aircraft Camouflage development defined, April 1942,

At this time, the Chief of Engineers was the War Dept. Agency responsible for the development of protective coloration and camouflage of all items of equipment, supplies and materials except aircraft. The Air Corps Board had held that responsibility for aircraft since 1940, while the Exp. Eng. Sect. (WF) was responsible for the material necessary for the camouflage.

The Director of Base Services (Washington) on April 2,1942, recommended that;

The Air Corps Board continue their responsibility for the development of means and methods for the camouflage of aircraft in flight and on the ground.

image98

North American B-25G-1-NA, 42-64809, was the eighth B-25G of 400 built, all at the North American, El Segundo, plant. It was armed with one 75mm cannon and two 0.5 inch guns in the nose, plus the turrets. Note the three P-51As, two Mustang Mk. Is, and 13 B-25Cs in the background.(March AFB Museum)

 

image100

image101

A training unit Curtiss P-40A, 39-1804, from Luke Field, Arizona, as designated by the X-804 on fuselage side. The band under the nose and the aircraft field number are yellow, (USAF)

Chief of Engineers continue development of all materials for camouflage of aircraft on the ground.

The Dir. of Mil. Req. (Wash.) be responsible for the approval and execution of camouflage schemes.

The Dir. of Mil. Req. pointed out on April 8, 1942, that the Air Corps Board had been inactivated as such, and functions were being handled by the AAF Proving Ground Command, Eglin Field, Florida, operating under Dir. of Mil. Req. That Directorate would now be accountable for the approval of camouflage schemes for aircraft developed by Material Command or Air Service Command. (Note: this points out how difficult it had been for Gen. Arnold to get a complete grip on the responsibilities and authority of the recently formed USAAF).

Gen. Arnold directs that “summer” camouflage be put immediately on all aircraft leaving U. S., March 14,1942.

Gen. Arnold caused some confusion by directing that “summer” camouflage be painted immediately on all aircraft leaving the U. S. He ordered that machinery was to be established so that camouflaging would be automatic as soon as it was determined for which theater the plane was destined. Brig. Gen. Fairchild, Dir. of Mil. Req. (Wash.), on April 7,1942, pointed out that there was no summer camouflage, but that the Joint Aircraft Committee (JAC) had approved the following camouflage for all land-based aircraft produced in the U. S.:

a. Surfaces seen from above to be painted the Army olive drab; surfaces seen from below to be painted a neutral gray. For night operations, a flat black color was to be used.

Prior to this, on March 19,1942, the Eng. Sec.(WF) had been told of Arnold’s order by the Prod. Eng. Sec., Washington. They replied on March 25, 1942, that after Study 42 had been conducted, it had been decided that all tactical aircraft should be camouflaged with a uniform design and color. They therefore recommended that all aircraft leave the country with the standard camouflage finish and that the special colors be applied in the combat zone to suit the particular terrain. This recommendation was based on the difficulty presented by the ever changing military situation.

Lockheed reports on problems with Haze Painting F-4 and F-5A aircraft, November 18,1942

In a letter to the AAF Resident Representative at Burbank, dated November 18,1942, Lockheed summarized data regarding the camou­flaging of F-4 and F-5A aircraft. Cabot haze paint had been used, as instructed by WF. This had proved unsatisfactory due to the difficulties in obtaining timely deliveries, the experimental stage of development, roughness of surfaces finished with this paint and the length of drying time. Lockheed had requested that they be allowed to use a Lowe Bros, lacquer type haze camouflage or Sherwin – Williams Kern-Haze enamel. These paints were not acceptable to Mat. Center (WF) because the permissible reflective values were exceeded by these paints. After a thorough inspection of the aircraft and test flights, the haze camouflage had to be “touched-up”, which produced a whiter surface than desired.

Summarizing, Lockheed’s investigation and experience to date in the use of the various haze camouflage materials, they felt that this type of camouflage scheme was extremely impractical for permanent applications, since it was impossible, underproduction conditions, to apply a finish which presented the desired camouflage effects.

Lockheed requested that they be allowed to revert to the standard camouflage on the remaining F-5A aircraft. (This report did not result in any changes to the existing haze camouflage requirements for the F-5As for some considerable time. See continuation in Chapter 2 – author).

TRAINING AND LIGHTER-THAN-AIR AIRCRAFT

7. TRAINERS,

a. The following types of aircraft are considered to be trainers:

(1) Primary Trainers (PT).

(2) Basic Trainers (ВТ).

(3) Advance Trainers (AT).

(4) Training Gliders (TG).

(5) Aircraft of other types regularly used for training purposes by the Flying Training Command.

(6) Ail types of aircraft not regularly assigned to, or normally located in, theaters of operation.

b. FINISHES,—All trainer aircraft will have aluminized finish, except those being by construction having an Alclad alloy finish. (See figure 8.)

c. APPLICATION OF FINISHES.

(1) Подпись:
image206Anodized alloy and miscellaneous steel parts may have two coats of aluminized lacquer, if neces­sary to match surrounding parts.

image207

Vultce ВТ-13, school aircraft “Y-295”, in natural metal finish, shows the lack of a fuselage insignia. The cowl is finished in red and while horizontal hands, below the black anti-glare panel. (USAF via Gerry R. Markgrafl

(2) All other exterior metal surfaces will be finished with one coat of zinc chromate primer, Specifi­cation No. AN-TT-P-656, and two coats of aluminized lacquer consisting of lacquer, cellulose nitrate, class A, clear, Specification No. AN-TT-L-51, with 6 to 8 ounces per gallon of bronze aluminum pigment paste, type B, Specification No. TT-A-468 or AN-TT-A-461.

(3) Exterior plywood surfaces will be finished in accordance with manufacturers’ instructions except that two or more finish coats will be pigmented with 8 ounces per gallon of bronze aluminum, pigment paste, Specification No. TT-A-468 type B, or Specification No. AN-TT-A-461.

(4) All exterior fabric parts will have four coats of clear nitrate dope, Specification No. AN-TT-D – 514. (Aluminized dope vehicle AN-TT-D-551 is not a suitable substitute as it does not have the tautening qualities of AN-TT-D-514.)This will be followed by two or more coats of aluminized dope prepared by adding 6 to 8 ounces per gallon of bronze, aluminum pigment paste, type B, Specification No. TT-A-468 or AN-TT-A461, to dope, cellulose nitrate, clear, Specification No. AN-TT-D-551.

(5) Patching will be accomplished with clear dope, Specification No. AN-TT-D-514 applied in same manner as semipigmented dope previously used.

(6) EMERGENCY REJUVENATOR FOR OLD FABRIC,—To one gallon of 2 to 1 mix of clear dope, Specification No. AN-TT-D-514, and blush retarding thinner, Specification No. AN-TT-T-258, add one fluid ounce each of tricresyl phosphate and castor oil. Apply one coat by brush to clean surface, followed by one spray coat. After several hours’ drying, spray one coat aluminized dope prepared as specified in para­graph 7.a.(4).

(7) For removal of all types of paint material from metal surfaces, use paint and varnish remover, Specification No. 14119. For removal of dope from fabric surfaces, use nitrate dope and lacquer thinner, Specification No. AN-TT-T-256.

d. MARKINGS.

(1) Each part and assembly will be permanently and legibly marked with the same number as the drawing number in such location that it can be read after assembly in the unit. (See Specification No. 98- 24105-Q.)

(2) Various detail and code markings for the cockpit, fuselage, oil lines, etc., as required in Specifi­cation No. 98-24105-Q will be maintained. Use of one coat of varnish, Specification No. TT-V-121 orAN-TT – V-116, for protection of fuselage legend is authorized.

(3) Radio call letters will be used as prescribed in paragraph 3.c.

(4) Painting of ring cowls is authorized in colors as directed by the CommandingGeneral of the Flying Training Command.

(5) Field numbers are authorized as designated by the Commanding General of the Flying Training Command for use in Army Air Forces Training Centers and Civil Flying Schools. They will be of contrasting color, preferably block type, and will be applied to opposite sides of the fuselage between the trailing edge of the wing and the leading edge of the horizontal stabilizer directly in front of the star insignia. The height will be approximately 75 percent of the height of fuselage at that point. (See figure 8.)

e. Standard insignia will be used as prescribed in paragraph 4.

image208

Vultee BT-13,42-42817, aircraft “31?", is seen after the fuselage insignia has been applied. The cowl is yellow’ with a centered insignia blue ring. Note the blue and yellow aircraft next in the lineup. (USAF via Gerry R. Markgraf)

/. All markings and insignia will be made with enamel, Specification No. AN-E-3, insignia colors in oil. Specification No. 3-120, or lacquer, Specification No. AN-TT-L-51.