TM 9-1275

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I. Introduction
Data
II. Inspection
II. (Cont)
III. Tools
IV. Gen Maint
V. Bbl & Rcvr
3rd/4th Echelons
5th Echelon
VI. Trigger
VII. Stocks
VIII. Equipment
IX. Final Insp.
X. Malfunctions
Section V

Barrel And Receiver Group

19. Disassembly
a. General. Remove and disassemble barrel and receiver groups (figs. 24 and 25) as outlined in FM 23-5.
b. Removing Barrel From Receiver (fig. 26). The barrel should be removed from the receiver only when rebarreling is necessary and then only by fifth echelon organizations. To remove, pass the barrel into the fixture, muzzle end first, until rib on barrel stops against shoulder in fixture. Position wrench on receiver as near to the barrel as possible and unscrew the receiver (counterclockwise) from the barrel.

Note. Never place the wrench on the rear of the receiver, as this will cause distortion.

c. Follower And Slide Assembly. Disassemble follower and follower slide (fig. 24) only when repair or replacement of parts is necessary. If necessary to disassemble, insert the blade of a screw driver under the front end of the slide (fig. 27) pry upward and forward, unlocking slide from follower.
d. Gas Cylinder group. (1) Front sight screw. Loosen the front sight screw (fig. 25) before attempting to remove the gas cylinders which have been modified, that is, those having a cut extending from the front sight base dovetail downward to the lower splines. Unless the front sight screw is loosened, damage may result to the barrel and gas cylinder. The front sight screw may be so tight that binding action of the gas cylinder on the barrel will make it difficult to remove the gas cylinder by lightly tapping on the bayonet lug (as prescribed in FM 23-5).

(2) Front sight screw seal. To remove the front sight screw seal (fig. 25), file off its exposed surface, and with a 3/16-inch hexagonal socket head set screw wrench, back out the screw. Replace and tighten the screw.

Note. The seal is no longer required and is not to be replaced after it has once been removed.

(3) Gas cylinder lock. Gas cylinder locks which are extremely tight fitting may be removed by use of the gas cylinder lock assembling wrench. Fit wrench over contour of gas cylinder lock and unscrew (counterclockwise). (See fig. 28)
e. Removing And Installing Extractor Without Removing Bolt From Rifle (fig. 29). To remove or install the extractor without removing the bolt from the rifle proceed as follows, using bolt, wire brush, and screw driver combination tool:
(1) Retract the bolt and insert the wire brush into the chamber of the barrel until the shoulder bears against the breech end of the barrel.
(2) Allow the bolt to close slowly, turning the tool so that the lug is under the extractor.
(3) Force the operating rod forward, holding the bolt against the tool, and turn the combination tool counterclockwise so that the lug pushes the extractor out of its seat and out of engagement with the ejector.
(4) Retract the bolt slowly, thus allowing removal of the extractor spring plunger assembly and the cartridge ejector assembly. The firing pin can then be withdrawn from its well.
(5) To install, place ejector and ejector spring, extractor and extractor spring in the bolt. With the brush of the combination tool in the chamber, line up the notches of the firing pin and ejector and force the operating rod forward, compressing the ejector spring. While holding spring compressed, press extractor into position.

20. Inspection
a. General. Inspect all parts for damage, wear, burs, rust, foreign matter in recesses, deformation, and for function and free action with mating parts. Important points to be inspected are shown in figures 30 and 31. Test all springs for set, minimum free length, and fracture.
b. Follower Rod. Inspect follower rod (fig. 31) for a pinched or worm fork and for loose rivets. The follower rod should have a long fork; therefore, replace all rods having short forks. (See fig. 32) This is necessary to prevent the rod from disengaging when grenades are being launched, Dispose of the old type (short fork) follower rod in accordance with existing regulations for unserviceable equipment.
c. Operating Rod Spring. (fig. 24) Inspect the operating rod spring for free length and load in the following manner, using operating rod spring gage:
(1) Testing free length. Insert the operating rod spring in the tube of gage and raise rod until bottom of stop collar is flush with the top surface of gage. (See fig. 33) Note position of operating rod spring in regard to top face of tube. If spring does not protrude beyond top face of tube, the maximum free length of 20 1/4 inches is satisfactory and the spring is serviceable in regard to free length. With the spring still in the tube, allow the rod to return to its original position and test for load.
(2) Testing load. Insert the stem of the 5-pound weight in the tube of gage and allow its weight to compress the spring. It should compress between 16 3/4 and 17 3/4 inches which is indicated by the first 1-inch relief notch cut in the stem of the weight. Note position of this notch in regard to top face of tube. If top face of tube falls within limits of the relief notch (fig. 34), the load at 5 pounds is acceptable. Next position the 11-pound weight on top of the 5-pound weight and allow their combined weight to compress the spring. It should compress between 11 3/4 and 12 3/4 inches which is indicated by the second 1-inch long relief notch cut in the stem of the 5-pound weight. Note position of this notch in regard to top face of tube. If top face of tube falls within the limits of the notch (fig. 34) the load at 16 pounds is acceptable.
d. Operating Rod (fig. 30). Inspect for binding between the barrel and receiver group and the operating rod by installing the rod and bolt in the rifle. As the rifle is tipped up and down, the rod and bolt should be moved from closed to open position and back by their own weight. If there is binding, inspect tube for dents and the handle for deformation, which will cause binding of the under side of the lug on the cut in the receiver. Inspect the diameter of the piston using no-go piston gage. (See fig. 35) All no-go piston diameter gages, initially produced are being withdrawn from service for reworking since the dimension of these gages has proven unsatisfactory. Pending the correction of these gages, the piston diameter will be measured with a micrometer and pistons which measure 0.525 inches or more should be considered serviceable. If the piston diameter is below the minimum specified by the serviceability chart (fig. 23), the operating rod assembly should be disposed of as unserviceable and uneconomically reparable, since an undersized gas piston tends to reduce the power available to operate the weapon.
e. Follower And Follower Slide (fig. 30). Inspect slides on follower for correct angle. An angle of approximately 92° plus/minus 0° 20 minutes must be maintained. (See fig 36)
f. Rear Sight Pinion - Early Manufacture. Inspect the pinions visually. Pinions having cracks caused by staking will not be removed from service (fig. 37), provided they do not interfere with functioning.
g. Gas Cylinder Group (fig. 38). Check the inside diameter of gas cylinder with gas cylinder gage. When the threads are cut in the gas cylinder the metal tends to flow and the inside diameter of the threaded section is reduced; therefore, this section must be slightly reamed to allow the gage to be inserted. Use the reamer on one end of the gage to perform this operation. Only the wire edge on top of the threads is removed. Remove all chips after reaming; any chips remaining will cause galling between the gas cylinder and the gas cylinder lock screw, due to the nature of stainless steel. Insert the gage after reaming and if the cylinder is serviceable the index surface of the gage should be level with, or protrude above, the end of the gas cylinder. (See fig. 39)

Caution: No force must be applied to a gage when a cylinder is being checked. If the gage is forced in the cylinder and rotated it will act as a reamer and will render the gas cylinder unserviceable.

Insert a small rod in the screw driver end of the gas cylinder lock screw and raise the valve from its seat. Inspect for burs and foreign matter. This is an important check as gas allowed to escape through the valve will dissipate the force necessary to drive the operating rod to the rear, thus causing a short recoil malfunction. Inspect function of valve spring to see that it closes the valve tightly in its seat. Replace all gas cylinder lock screws which have burs on the valve face or seat, or where the spring tension is insufficient to seat the valve tightly. All gas cylinder lock screws of early manufacture should be replaced by gas cylinder lock screw with valve assembly.
h. Bolt Assembly (fig. 40). (1) Bolt. Test the bolt while it is free for freedom and smoothness of movement, and for locking.
(2) Firing pin. Check protrusion of firing pin beyond the face of the bolt using firing pin protrusion gage. (See fig. 41) In fired position, the nose of the pin should protrude from 0.044 inch minimum to 0.059 inch maximum. Remove all full round firing pins and discard in accordance with existing regulations.
(3) Extractor. Test the extractor for grip of the cartridge base, and the extractor spring for tension.
i. Barrel. Inspect the barrel as outlined in section II.
j. Telescope Mount And Bracket (U.S. Rifle, Cal. .30, M1C (Sniper's) Only) (figs. 42 and 43). Inspect telescope mount bracket for retention on receiver and for burs on male dovetail slides. Inspect slide for function in telescope mount bracket and locking action of slide clamp with locking screws. Check supports for looseness in slide. Inspect screws and screw holes for worn or stripped threads and all recesses for foreign matter.
k. Telescope Mount And Base (U.S. Rifle, Cal., .30, M1D (Sniper's) Only) (fig. 44). Inspect base for looseness on barrel, and for burs. Inspect dowel pin for burs, wear, and for looseness in base. Inspect knob for looseness on screw and for worn knurling. Inspect function of plunger and spring with knob. Inspect all screws and screw holes for stripped or worn threads.

 

TM 9-1275

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