# STC SA876EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Revo Inc, United States
- Description: 1.  Models LA-4-200, LA-4, LA-4A, LA-4P:

     Installation of Auxiliary Fuel System in accordance with Aerofab Drawings No. 180004, Rev. G, dated June 8, 1971,    
     and 180009, Rev. D, dated February 10, 1971.

2.  Model LA-4-200:  Increase of Gross Weight to 2690 pounds.

Limitations and Conditions (Continued):
(b)	       Aerofab Inc. Airplane Flight Manual Supplement:

(i)	No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4-200 Flight Manual  Dated July 11, 1960, revised April 11, 1973, or:
     
(ii)	No. 4, FAA approved December 28, 1973, revised July 18, 1975, for Lake LA-4-200 Flight Manual reissued  December 28, 1973.

      is required for operations at 2690 lb. Gross Weight.
- Applied: October 28, 1969
- Status date: September 30, 2004
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1A13](https://openairdocs.org/tcds/1A13)
- Certificate PDF: https://openairdocs.org/files/sha256/08/8a/088a5b6544a5b042f27d1f3f429d5eb46f964a3ea397635170102ba11ae75181
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A49E985B29C5943886256F86006A024B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA876EA

## ADs that name it (1)

- [AD 76-02-01](https://openairdocs.org/ad/76-02-01): Engine Power · Revo Lake LA-4 and Lake LA-4-200 with STC SA876EA. Effective Jan 30, 1976. Named in the applicability

## Approved models (4)

- REVO Incorporated Lake LA-4 ([TCDS 1A13](https://openairdocs.org/tcds/1A13))
- REVO Incorporated Lake LA-4-200 ([TCDS 1A13](https://openairdocs.org/tcds/1A13))
- REVO Incorporated Lake LA-4A ([TCDS 1A13](https://openairdocs.org/tcds/1A13))
- REVO Incorporated Lake LA-4P ([TCDS 1A13](https://openairdocs.org/tcds/1A13))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES Number SA876EA This certificate issued to Revo, Incorporated 1396 Grandview Boulevard Kissimmee, Florida 34744

Part 03 of the Civil Air Regulations.

Original Product--Type Certificate Number : 1A13 Make : REVO Model : Lake LA-4-200, Lake LA-4, Lake LA-4A, Lake LA-4P

1. Models LA-4-200, LA-4, LA-4A, LA-4P:

Installation of Auxiliary Fuel System in accordance with Aerofab Drawings No. 180004, Rev. G, dated June 8, 1971, and 180009, Rev. D, dated February 10, 1971.

2. Model LA-4-200:

Increase of Gross Weight to 2690 pounds.

1. Model LA-4-200:

(a) Aerofab Inc. Airplane Flight Manual Supplement No. 5, FAA approved June 24, 1971 for Lake LA-4-200 Flight Manual dated July 11, 1960, revised April 11, 1973, is required for operations at 2600 lb. gross weight.

Date of application : October 28, 1969

Date of issuance : June 24, 1971 Date reissued : October 06, 1989; November 20, 2002;

Septem ber 30, 2004 Date amended : May 09, 1975; July 18, 1975;

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number SA876EA Date of Issuance: June 24, 1971 Date Amended: May 09, 1975

(b) Aerofab Inc. Airplane Flight Manual Supplement:

(i) No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4- 200 Flight Manual Dated July 11, 1960, revised April 11, 1973, or:

(ii) No. 4, FAA approved December 28, 1973, revi sed July 18, 1975, for Lake LA-4-200 Flight Manual reissued December 28, 1973.

is required for operations at 2690 lb. Gross Weight.

2. Models LA-4, LA-4A, LA-4P:

Aerofab Inc. Airplane Flight Manual Supplement No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4-200 Flight Manual dated July 11, 1960, revised April 11, 1973 is required for operations at 2400 lb. Gross Weight.

3. Models LA-4-200, LA-4, LA-4A, LA-4P:

(a) Placards required are installed in accordance with Aerofab Drawing No. 180004, Rev. G and the AFMS.

(b) This approval should not be extended to other airc raft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

## Every issue (1)

- September 30, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/08/8a/088a5b6544a5b042f27d1f3f429d5eb46f964a3ea397635170102ba11ae75181)

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