14 CFR Part 25

E859301

14 CFR Part 25 is the U.S. Federal Aviation Administration’s airworthiness standards that govern the design and certification of transport category airplanes.

All labels observed (3)

Label Occurrences
FAA Part 25 2
14 CFR Part 25 canonical 1
FAA 14 CFR Part 25 1

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf FAA airworthiness standard ⓘ
U.S. federal aviation regulation ⓘ
transport category airplane certification standard ⓘ
administeredBy Federal Aviation Administration ⓘ
appliesIn type certification process ⓘ
appliesTo large cargo airplanes ⓘ
large passenger airplanes ⓘ
transport category airplanes ⓘ
turbine-powered transport airplanes ⓘ
codifiedIn Title 14 of the Code of Federal Regulations ⓘ
contains Subpart A – General ⓘ
Subpart B – Flight ⓘ
Subpart C – Structure ⓘ
Subpart D – Design and Construction ⓘ
Subpart E – Powerplant ⓘ
Subpart F – Equipment ⓘ
Subpart G – Operating Limitations and Information ⓘ
Subpart H – Electrical Wiring Interconnection Systems ⓘ
Subpart I – Ice Protection ⓘ
governs airworthiness standards for transport category airplanes ⓘ
design of transport category airplanes ⓘ
type certification of transport category airplanes ⓘ
harmonizedWith EASA CS-25 ⓘ
jurisdiction United States ⓘ
legalBasis 49 U.S.C. Subtitle VII ⓘ
partOf Federal Aviation Regulations ⓘ
U.S. civil aviation regulations ⓘ
regulator Federal Aviation Administration ⓘ
relatedTo 14 CFR Part 21 ⓘ
14 CFR Part 26 ⓘ
14 CFR Part 91 ⓘ
safetyObjective acceptable level of safety for transport category airplanes ⓘ
protection of occupants in normal and emergency conditions ⓘ
subject crashworthiness requirements ⓘ
emergency evacuation requirements ⓘ
fatigue and damage tolerance requirements ⓘ
fire protection requirements ⓘ
flight characteristics requirements ⓘ
flight crew compartment design requirements ⓘ
flight performance requirements ⓘ
icing protection requirements ⓘ
operating limitations ⓘ
passenger cabin safety requirements ⓘ
powerplant installation requirements ⓘ
pressurization requirements ⓘ
structural design requirements ⓘ
systems and equipment requirements ⓘ
usedFor amended type certification of modified transport airplanes ⓘ
type certification of new transport airplane designs ⓘ

How these facts were elicited

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

FAA Part 23 → relatedTo → FAA Part 25 ⓘ
linked to: 14 CFR Part 25
FAA Part 33 → relatedTo → FAA Part 25 ⓘ
linked to: 14 CFR Part 25
EASA CS-25 → comparableTo → FAA 14 CFR Part 25 ⓘ
linked to: 14 CFR Part 25