# STC SA2114CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Central Air Charter, United States
- Description: Installation of Electro Delta VR300-28-50 Central Air Charter VR-0015, or Central Air Charter GR2850VI voltage regulator as a replacement for original Delco Remy 1119656 voltage regulator.
- Applied: January 10, 1985
- Status date: September 2, 1988
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 6A1](https://openairdocs.org/tcds/6A1)
- Certificate PDF: https://openairdocs.org/files/sha256/52/5f/525f12405235731805a7ed67827e2fbe6868ecaeefaee360b70c529f92277613
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4193E34AC2F6176985256CC2000159C9.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2114CE

## ADs that name it (0)

None.

## Approved models (1)

- Twin Commander Aircraft Corporation 500-B ([TCDS 6A1](https://openairdocs.org/tcds/6A1))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA211408 This certificate issued to: Central Air Charter 411 Lou Holland Drive sansas City, MO 64117 Purt 3 the CIVII Air Regulations.

Original Product - Type bortificale Numbon: 6A1 Make: Gulfstream American Model: 500-B Description of Type Design Change: Installation of Electro Delta, Inc., VR300-28-50, Central Air Charter VR-0015, or Central Air Charter GR2850V1 voltage regulator as a replacement for original Delco Remy 1119656 voltage regulator in accordance with Central Air Charter Document "V.R. Installation in 500B Commanders" dated January 9, 1985 (for VR300-28-50), Central Air Charter Drawing List "V.R. Installation in 500B Commanders" dated December 15, 1987 (for either VR300-28-50 or VR-0015), or Central Air Charter Drawing List 'GR2850V1 Solid State Voltage Regulator Installation in 500B Commanders" dated August 18, 1988 (for GR2850V1), or later FAA approved revisions.

Limilalions andbindilions: 1. Incorporation of other modifications on these airplanes should not be approved unless it is determined that the interrelationship between this change and those being incorporated will introduce no adverse effect upon the airworthiness of the airplane. 2. This approval is limited to those airplanes incorporating 50-Amp generators. 3. This modification is compatible with STC SA2113CE.

Daledapplicatim: January 10, 1985 Jule wissued:

Date of Issuance: June 6, 1985 Vale unended: December 22, 1987 FEDERAL AVIATIO By direction of hear 3l1.988 Laurence A. Hesson (Signature) TONIN STRANDE Wichita Aircraft Certification Office Lawrence A. Herron, Manager (Title)

47.

FAA FoR 6110-2 (10-68)

## Every issue (1)

- September 2, 1988: Amended, Current. [certificate](https://openairdocs.org/files/sha256/52/5f/525f12405235731805a7ed67827e2fbe6868ecaeefaee360b70c529f92277613)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.