STC SA4378WP
Current · Reissued · Aircraft · Small/Large Airplane · Rev 10/02/2014 · FAA STC database
Installation of hydraulic landing gear retraction system. View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (13)
- A24CE Beechcraft Corporation · 200
- A24CE Beechcraft Corporation · 200C
- A24CE Beechcraft Corporation · 200CT
- A24CE Beechcraft Corporation · 200T
- A24CE Beechcraft Corporation · A100-1 (U-21J)
- A24CE Beechcraft Corporation · A200 (C-12A)
- A24CE Beechcraft Corporation · A200 (C-12C)
- A24CE Beechcraft Corporation · A200C (UC-12B)
- A24CE Beechcraft Corporation · A200CT (C-12D)
- A24CE Beechcraft Corporation · B200
- A24CE Beechcraft Corporation · B200C
- A24CE Beechcraft Corporation · B200CT
- A24CE Beechcraft Corporation · B200T
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120
- § 21.47