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FAA-listed STC holder

Revo Inc STCs

The Jun 30, 2026 FAA DRS snapshot lists 13 selected supplemental type certificates with status Current under Revo Inc. The records span 5 public aircraft directories and 6 modification categories. This is a research directory, not a claim that any specific kit or service is currently offered.

13
listed Current at snapshot
5
aircraft directories
6
modification categories
Sep 30, 2004
latest recorded revision

Modification mix

Engine and powerplant5
Other aircraft modifications2
Cabin and interiors2
Fuel systems2
Aircraft structures1
Aircraft connectivity1

Aircraft represented

REVO Lake LA-4-20026 STCsREVO Lake LA-425 STCsREVO Lake LA-4A18 STCsREVO Lake Model 25017 STCsREVO Lake LA-4P16 STCs

Recently revised records

Showing the 13 most recently revised records. Category directories provide the complete paginated discovery path.

SA876EAFuel systems

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.

FAA holder: Revo Inc

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SA970NEAircraft connectivity

Installation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations: United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) ___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47. CONFIGURATION 1: Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows: Option 1: Radome In accordance with drawings 150017, 190011, 190018 and 190019. Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing 190019. This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system compatibility. Option 2: Dual Alternator System In accordance with drawings 4-7781 and 4-7782. Option 3: Bow Compartment Covers In accordance with drawing 4-3501. Option 4: Upper Fin Revision In accordance with drawing 4-2652, Revision C. Option 5: Disassembly Provisions In accordance with drawing 300015. Option 6: Dual Rudder/Aileron Electric Trim System In accordance with drawing 4-3519 and STC SA1142SO. CONFIGURATION 2: Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003.

FAA holder: Revo Inc

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