Regulatory Text
14 C.F.R. § 27.321 — General.
§ 27.321 General. (a) The flight load factor must be assumed to act normal to the longitudinal axis of the rotorcraft, and to be equal in magnitude and opposite in direction to the rotorcraft inertia load factor at the center of gravity. (b) Compliance with the flight load requirements of this subpart must be shown— (1) At each weight from the design minimum weight to the design maximum weight; and (2) With any practical distribution of disposable load within the operating limitations in the Rotorcraft Flight Manual. [Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-11, 41 FR 55468, Dec. 20, 1976]
Source: ecfr.gov · govinfo.gov — public domain
Official Source ↗
Root-LD Entity Data
◈ Machine-Readable Provenance Record
Root-LD v1.0 · boisestandard.org
Federation ID
BS-CFR14-SEC-376492
Entity Class
REGULATION / FEDERAL-CFR-SECTION
Domain Signature
boisestandard.org
Citation
14 C.F.R. § 27.321
Corpus
CFR — Code of Federal Regulations
Status
✓ ACTIVE
Source
PRIMARY-SOURCE
Source Verified
✓ TRUE
Content Hash
5c2cc27eeb84e666...
Semantic Edges
Pending — corpus passes queued
The regulatory text of 14 C.F.R. § 27.321 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
Navigate Corpus — Title 14 C.F.R.
Title 14 — Aeronautics and Space
14 C.F.R. § 1.114 C.F.R. § 1.214 C.F.R. § 1.314 C.F.R. § 3.114 C.F.R. § 3.514 C.F.R. § 3.20014 C.F.R. § 3.20514 C.F.R. § 5.114 C.F.R. § 5.314 C.F.R. § 5.514 C.F.R. § 5.2114 C.F.R. § 5.2314 C.F.R. § 5.2514 C.F.R. § 5.2714 C.F.R. § 5.5114 C.F.R. § 5.5314 C.F.R. § 5.5514 C.F.R. § 5.7114 C.F.R. § 5.7314 C.F.R. § 5.7514 C.F.R. § 5.9114 C.F.R. § 5.9314 C.F.R. § 5.9514 C.F.R. § 5.9714 C.F.R. § 11.114 C.F.R. § 11.314 C.F.R. § 11.514 C.F.R. § 11.714 C.F.R. § 11.914 C.F.R. § 11.11
14 C.F.R. — public domain
← All Legislation