STC SA1618CE
Current · Amended · Aircraft · Single-Engine · Rev 12/01/1988 · FAA STC database
Installation redundant NASA type fuel vent system and modification of fuel vapor return system. View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (15)
- 3A21 The Cessna Aircraft Company · T210N
- 3A21 The Cessna Aircraft Company · T210K
- 3A21 The Cessna Aircraft Company · 210L
- 3A21 The Cessna Aircraft Company · T210L
- 3A21 The Cessna Aircraft Company · 210M
- 3A21 The Cessna Aircraft Company · T210M
- 3A21 The Cessna Aircraft Company · 210N
- 3A21 The Cessna Aircraft Company · 210H
- 3A21 The Cessna Aircraft Company · T210H
- 3A21 The Cessna Aircraft Company · 210J
- 3A21 The Cessna Aircraft Company · T210J
- 3A21 The Cessna Aircraft Company · 210G
- 3A21 The Cessna Aircraft Company · 210K
- 3A21 The Cessna Aircraft Company · T210G
- 3A21 The Cessna Aircraft Company · P210N
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120