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STC SE1753CE

Current · Reissued · Engine · Rev 12/03/1991 · FAA STC database

Removal of manifold pressure relief valve, modification of engine oil pump and scavenge oil pump, and replacement of tuborcharger with later model unit. View PDF on drs.faa.gov ↗

The STC PDF is authoritative: installation instructions, ICA requirements and limitations.

Applicable aircraft (1)

Certification basis — 14 CFR

Specific sections

  • Sec. 111
  • Sec. 113
  • Sec. 115
  • Sec. 117
  • Sec. 119
  • Sec. 120