Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:legislation
|
| gptkbp:appliesTo |
helicopters
normal category rotorcraft |
| gptkbp:country |
gptkb:United_States
|
| gptkbp:covers |
gptkb:performance
design and construction equipment requirements structural requirements emergency provisions operating limitations powerplant requirements flight characteristics systems and equipment |
| gptkbp:enforcedBy |
gptkb:Federal_Aviation_Administration
|
| gptkbp:fullName |
Title 14 of the Code of Federal Regulations, Part 27
|
| gptkbp:issuedBy |
gptkb:Federal_Aviation_Administration
|
| gptkbp:language |
English
|
| gptkbp:locationInCFR |
gptkb:14_CFR_Part_27
|
| gptkbp:maxTakeoffWeight |
7,000 pounds (3,175 kg) or less
|
| gptkbp:purpose |
airworthiness standards for normal category rotorcraft
|
| gptkbp:regulates |
certification of normal category rotorcraft
|
| gptkbp:relatedTo |
FAA Part 29
|
| gptkbp:startDate |
February 1, 1965
|
| gptkbp:bfsParent |
gptkb:FAA_Part_25
gptkb:FAA_Part_23 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
FAA Part 27
|