Regulatory Text
14 C.F.R. § 25.489 — Ground handling conditions.
§ 25.489 Ground handling conditions. Unless otherwise prescribed, the landing gear and airplane structure must be investigated for the conditions in §§ 25.491 through 25.509 with the airplane at the design ramp weight (the maximum weight for ground handling conditions). No wing lift may be considered. The shock absorbers and tires may be assumed to be in their static position. [Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-23, 35 FR 5673, Apr. 8, 1970]
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-D1080C
Entity Class
REGULATION / FEDERAL-CFR-SECTION
Domain Signature
boisestandard.org
Citation
14 C.F.R. § 25.489
Corpus
CFR — Code of Federal Regulations
Status
✓ ACTIVE
Source
PRIMARY-SOURCE
Source Verified
✓ TRUE
Content Hash
8a99942c4ac699bd...
Semantic Edges
Pending — corpus passes queued
The regulatory text of 14 C.F.R. § 25.489 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