178.44—Specification 3HT seamless steel cylinders for aircraft use.

Table 1—Authorized Materials
Designation AISI 4130(percent)
Carbon 0.28/0.33
Manganese 0.40/0.60
Phosphorus 0.040 maximum
Sulfur 0.040 maximum
Silicon 0.15/0.35
Chromium 0.80/1.10
Molybdenum 0.15/0.25
Table 2—Check Analysis Tolerances
Element Limit or maximum specified (percent) Tolerance (percent) over the maximum limit or under the minimum limit
Under minimum limit Over maximum limit
Carbon Over 0.15 to 0.40 incl .03 .04
Manganese To 0.60 incl .03 .03
Phosphorus1 All ranges .01
Sulphur All ranges .01
Code of Federal Regulations 842
Silicon To 0.30 incl .02 .03
Over 0.30 to 1.00 incl .05 .05
Chromium To 0.90 incl .03 .03
Over 0.90 to 2.10 incl .05 .05
Molybdenum To 0.20 incl .01 .01
Over 0.20 to 0.40 incl .02 .02
1 Rephosphorized steels not subject to check analysis for phosphorus.

Code of Federal Regulations

S = [P(1.3D2 0.4d2)] / (D2 − d2)
Where:
S = Wall stress in psi;
P = Minimum test pressure prescribed for water jacket test;
D = Outside diameter in inches;
d = Inside diameter in inches.
(s) Inspector's report. In addition to the requirements of § 178.35, the inspector's report must indicate the rejection elastic expansion (REE), in cubic cm (cc).
[Amdt. 178-114, 61 FR 25942, May 23, 1996, as amended at 62 FR 51561, Oct. 1, 1997; 65 FR 58631, Sept. 29, 2000; 66 FR 45385, Aug. 28, 2001; 67 FR 51652, Aug. 8, 2002; 68 FR 75748, 75749, Dec. 31, 2003]