# TCDS 1A13: Revo Incorporated

- Type: Type certificate data sheet
- Status: Current
- Holder: Revo Incorporated
- Revision: 28
- Revised: December 12, 2013
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 23, Part 36, CAR 3
- Registered aircraft: 154, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/4b/84/4b84ac6b7046613d1d466c0c4877f6a8b173e41fc030ca9b37ad8bc737c61187
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AADEB25A7AC1489186257C3F0066CA2A.0001
- Page: https://openairdocs.org/tcds/1A13

## Models (7)

As the data sheet lists them.

- Lake Model 250 (Renegade)
- Lake LA-4A
- Lake LA-4
- Lake LA-4-200 (Buccaneer)
- Lake LA-4P
- Colonial C-1
- Colonial C-2

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2 3 4 5 6 7 8 9 
Rev. No. 28 28 28 28 25 24 25 27 28 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
1A13 
Revision 28 
Revo, Inc. 
 COLONIAL C-1 
 COLONIAL C-2 
 LAKE LA-4 
 LAKE LA-4A 
 LAKE LA-4P 
 LAKE LA-4-200 
 LAKE MODEL 250 
 
December 12, 2013 
TYPE CERTIFICATE DATA SHEET NO. 1A13 
 
Type Certificate Holder. Revo, Incorporated 
 1396 Grandview Boulevard 
 Kissimmee, FL  34744 
 
Type Certificate Holder Record Colonial Aircraft Company transferred TC 1A13 to Lake Aircraft Corporation on 
December 23, 1959. 
Lake Aircraft Corporation transferred TC 1A13 to Consolidated Aeronautics, Inc. on  
May 7, 1963. 
Consolidated Aeronautics, Inc. transferred TC 1A13 to Revo, Incorporated on 
October 29, 1986. 
Revo, Incorporated transferred TC 1A13 to Global Amphibians, LLC on  
 October 28, 2002. 
 Global Amphibians, LLC transferred TC 1A13 to Revo, Incorporated on  
 September 30, 2004 
 
I. Colonial Model C-1, 3 PCAmM (Normal Category), Approved 19 September 1955 
 
 Engine Lycoming O-320-A2A 
 
 Fuel 80/87 minimum grade aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (150 hp) 
 
 Propeller and Propeller Limits 1. Hartzell, hub HC82XG-6L, blades L8046-6 
   Diameter:    not over 74 in., not under 72.5 in. 
  Pitch setting at 30 in. sta.: 
       Normal operation 11.7° to 20.0° 
  2. Woodward hydraulic governor 210065 
 
 Airspeed Limits (CAS) Vne (never exceed) 142 mph (123 knots) 
  Vfe (flaps extended) 125 mph (109 knots) 
  Vle, Vlo (maximum landing gear 
    extended, operating) 125 mph (109 knots) 
  Vp (maneuvering) 113 mph   (98 knots) 
  Vno (maximum structural cruising) 113 mph   (98 knots) 
 
 C.G. Range (+105.0) to (+109.0) at 2150 lb. 
  (+105.0) to (+109.6) at 1980 lb. or less 
  Straight line variation in aft C.G. between weights shown.

1A13 2 of 9 
I. Colonial Model C-1  (cont’d) 
 
 Empty Wt. C.G. Range None 
 
 Datum Hull Sta. 0. (Hull Sta. 0 is 90.75 in. forward of the leading edge of the wing at side of hull).  
 
 Maximum Weight  2150 lb. 
 
 Minimum Crew 1 
 
 No. of Seats 3.   2 at (+74), 1 at (+97) 
 
 Maximum Baggage 200 lb. (+97) 
 
 Fuel Capacity 40 gal. (+118) 
 
 Oil Capacity 2 gal. (6 qt. usable) (+111) 
 
 Control Surface Movements Elevator Up 21.5°  Down  20° 
 Ailerons Up  29° Down  15° 
 Rudder   Right 25°  Left 25° 
 Flaps      Down  20° 
 
 Manufacturer’s Serial Numbers 1 through 14, 16 through 20, 22 through 25 
 
 Certification Basis Type Certificate No. 1A13 (CAR 03, 15 December 1946, and Amendments 3-1 and 3-2). 
 
 Equipment The basic required equipment as prescribed in the applicable airworthiness requirements 
(see Certification Basis) must be installed in the aircraft for certification including the 
FAA-approved Airplane Flight Manual with its latest revision and appropriate 
supplements.  Refer to the equipment portion of Aircraft Specification 1A13, Revision 17, 
for additional required equipment. 
 
II. Colonial Model C-2, 4 PCAmM (Normal Category), Approved 24 December 1957 
(Same as Model C-1 except for engine installation, cockpit arrangement, horizontal tail surfaces, longitudinal trim system, 
modified tip floats, and structural modifications to engine pylon and wing.) 
 
 Engine Lycoming O-360-A1A 
 
 Fuel 91/96 minimum grade aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (180 hp) 
 
 Propeller and Propeller Limits 1. Hartzell, hub HC92ZK-6DL-1, blades L8447-12A 
   Diameter:    not over 72 in., not under 70.5 in. 
  Pitch setting at 30 in. sta.: 
       Normal operation 11.5° to 23.4° 
 
  or 2. Hartzell, hub HC92WK-8L, blades LW8447-12A 
   Diameter:    not over 72 in., not under 70.5 in. 
  Pitch setting at 30 in. sta.: 
       Normal operation 11.5° to 23.4° 
 
  3. Woodward hydraulic governor C210105 
 
 Airspeed Limits (CAS) Vne (never exceed) 146 mph (127 knots) 
  Vfe (flaps extended) 125 mph (109 knots) 
  Vle, Vlo (maximum landing gear 
    extended, operating) 125 mph (109 knots) 
  Vp (maneuvering) 121 mph (105 knots) 
  Vno (maximum structural cruising) 122 mph (106 knots)

3 of 9 1A13 
II. Colonial Model C-2  (cont’d) 
 
 C.G. Range (+102.5) to (+106.0) at 2350 lb. 
  (+102.0) to (+108.0) at 1950 lb. or less 
  Straight line variation in aft C.G. between weights shown. 
 
 Empty Wt. C.G. Range None 
 
 Datum Hull Sta. 0. (Hull Sta. 0 is 90.75 in. forward of the leading edge of the wing at side of hull).  
 
 Maximum Weight  2350 lb. 
 
 Minimum Crew 1 
 
 No. of Seats 4.   2 at (+66), 2 at (+92) 
 
 Maximum Baggage 200 lb. (+97), 20 lb. (+118) 
 
 Fuel Capacity 40 gal. (+118) 
 
 Oil Capacity 2 gal. (6 qt. usable) (+111) 
 
 Control Surface Movements Elevator Up 26°  Down 23° 
 Ailerons Up  29° Down  15° 
 Rudder   Right 25°  Left 25° 
 Flaps   Down  20° 
 Trim Tab  Up 36° +2°,-1° Down 24° +2°,-1° 
 
 Manufacturer’s Serial Numbers 115, 126 through 243. 
 
 Certification Basis Type Certificate No. 1A13 (CAR 03, 15 December 1946, and Amendments 3-1 and 3-2). 
 
 Equipment The basic required equipment as prescribed in the applicable airworthiness requirements 
(see Certification Basis) must be installed in the aircraft for certification including the 
FAA-approved Airplane Flight Manual with its latest revision and appropriate 
supplements.  Refer to the equipment portion of Aircraft Specification 1A13, Revision 17, 
for additional required equipment. 
 
III. Lake Model LA-4, Approved 26 July 1960; Lake Model LA-4A, Approved 1 June 1960; Lake Model LA-4P,  
 Approved 21 June 1960; 4 PCAmM (Normal Category) 
 
Model LA-4 Same as Colonial Model C-2 except four feet added to wing span; each aileron lengthened by 1 ft., 17 inches 
added to bow; rear wing-to-fuselage attachment revised; gross weight increased; nose gear doors modified due to increase in bow 
extension; and reinforcement of wing and wing-to fuselage carry-through structure.  (See Note 4.) 
 
Model LA-4A Same as LA-4 except the bow is the same as the Colonial Model C-2.  
 
Model LA-4P (Prototype) Same as Model LA-4 except that rear  wing-to-fuselage attachment was not revised and 
reinforcement of wing and wing-fuselage carry-through structure was not added. 
 
 Engines Lycoming O-360-A1A or O-360-AID 
 
 Fuel 91/96 minimum grade aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (180 hp) 
 
 Propeller and Propeller Limits 1. Hartzell, hub HC92ZK-8, blades L8447-12A 
   Diameter:    not over 72 in., not under 70.5 in. 
  Pitch setting at 30 in. sta.:  Normal operation 11.5° to 23.4° 
  or 2. Hartzell, hub HC92WK-8L, blades LW8447-12A 
   Diameter:    not over 72 in., not under 70.5 in. 
  Pitch setting at 30 in. sta.:  Normal operation 11.5° to 23.4°

1A13 4 of 9 
III. Lake Model LA-4, Lake Model LA-4A, and Lake Model LA-4P (cont’d) 
 
  3. Woodward hydraulic governor C210105 
  or 4. Hartzell hydraulic governor F-2. 
 
 Airspeed Limits (CAS) Vne (never exceed) 146 mph (127 knots) 
  Vfe (flaps extended) 125 mph (109 knots) 
  Vle, Vlo (maximum landing gear 
    extended, operating) 125 mph (109 knots) 
  Vp (maneuvering) 121 mph (105 knots) 
  Vno (maximum structural cruising) 122 mph (106 knots) 
 
 C.G. Range (+102.5) to (+106.0) at 2400 lb. 
  (+102.5) to (+108.0) at 1950 lb. or less 
  Straight-line variation in aft C.G. between weights shown 
 
 Empty Wt. C.G. Range None 
 
 Datum Hull Sta. 0. (Hull Sta. 0 is 90.75 in. forward of the leading edge of the wing  
  at side of hull). 
 
 Maximum Weight  2400 lb. 
 
 Minimum Crew 1 
 
 No. of Seats 4.   2 at (+63), 2 at (+92) 
 
 Maximum Baggage 200 lb. (+118) 
 
 Fuel Capacity 40 gal. (+118) 
 
 Oil Capacity 2 gal. (6 qt. usable) (+117) 
 
 Control Surface Movements Elevator Up  26° ± 1°  Down 23° ± 1° 
 Ailerons Up  29° + 2°, -1° Down  15° ± 1°,  neutral ± 2° 
 Rudder  Right  25° ± 1° Left 25° ± 1° 
 Flaps    Down  20° ± 1° 
 Trim Tab Up  36°+ 2°, -1°  Down 24°+ 2°, -1° 
 
 Aileron Cable Rigging Tension 25 lb. ±  3 lb. 
 
 Manufacturer’s Serial Numbers Model LA-4: 246 through 421, 423 through 429, 445, and 446 
  Model LA-4A: 244 and 245 only 
  Model LA-4P: 121 only 
 
 Certification Basis Type Certificate No. 1A13 (CAR 03, 15 December 1946, and Amendments 3-1 and 2). 
 
 Equipment The basic required equipment as prescribed in the applicable airworthiness requirements 
(see Certification Basis) must be installed in the aircraft for certification including the 
FAA-approved Airplane Flight Manual with its latest revision and appropriate 
supplements.  Refer to the equipment portion of Aircraft Specification 1A13, Revision 17, 
for additional required equipment.

5 of 9 1A13 
IV. Lake Model LA-4-200; 4 PCAmM (Normal Category) Approved 26 May 1970 
 (Same as LA-4 except for engine installation.) 
 
 Engines Lycoming IO-360-A1B or Lycoming IO-360-A1B6 
 
 Fuel 100/130 minimum octane aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (200 hp) 
 
 Propeller and Propeller Limits 1. Hartzell, hub HC-C2YK-1BL, blades L7666A-2 or L7666-2 
   Diameter:    not over 74 in., not under 72 in. 
  Pitch setting at 30 in. sta.: 
       low 14° min., high 27° to 31° 
   NOTE:  Avoid continuous operations between 2000 and 2350 r.p.m. 
  or 2. Hartzell, hub HC-C2YK-1BLF, blades FL7666A-2 
   Diameter:    not over 74 in., not under 72 in. 
  Pitch setting at 30 in. sta.: 
       low 14° min., high 27° to 31° 
   NOTE:  Avoid continuous operations between 2000 and 2350 r.p.m. 
   
3. Woodward hydraulic governor C210105 
  or 4. Hartzell hydraulic governor F-2-6A. 
 
 Airspeed Limits (CAS) Vne (never exceed)  (See Note 5) 
      For aircraft: 
   S/N 422-1036 146 mph (127 knots) 
   S/N 1037-Subsequent 154 mph (134 knots) 
   *S/N 422-1036 154  mph (134 knots) 
      * With Consolidated Aeronautics Kit K-137 installed. 
  Vfe (flaps extended) 125 mph (109 knots) 
  Vle, Vlo (maximum landing gear 
    extended, operating) 125 mph (109 knots) 
  Vp (maneuvering) 121 mph (105 knots) 
  Vno (maximum structural cruising) 122 mph (106 knots) 
   
 C.G. Range (+102.5) to (+106.0) at 2600 lb. 
  (+102.5) to (+108.0) at 1950 lb. or less 
  Straight-line variation in aft C.G. between weights shown 
  (See Note 6 for 2690 lb. C.G. Range) 
 
 Empty Wt. C.G. Range None 
 
 Datum Hull Sta. 0. (Hull Sta. 0 is 90.75 in. forward of the leading edge of the wing  
  at side of hull). 
 
 Maximum Weight  2600 lb. (See Note 6) 
 
 Minimum Crew 1 
 
 No. of Seats 4.   2 at (+61), 2 at (+92) 
 
 Maximum Baggage 200 lb. (+118) 
 
 Fuel Capacity 40 gal. (+118) Main Tank 
  14 gal. (+118) Aux. Fuel Tanks Optional (See Notes 6 and 9)

1A13 6 of 9 
IV. Lake Model LA-4-200  (cont’d) 
 
 Oil Capacity 2 gal. (6 qt. usable) (+117) 
 
 Control Surface Movements Elevator Up  26° ± 1°  Down 23° ± 1° 
 Ailerons Up   29° + 2°, - 1° Down  15° ± 1° 
     
 Rudder   Right  25° ± 1° Left 25° ± 1° 
 Flaps     Down  20° ± 1° 
  Trim Tab Up 36° + 2°, - 1° Down 24° + 2°, - 1° 
         
 
 Aileron Cable Rigging Tension 25 lb. ±  3 lb. 
 
 Manufacturer’s Serial Numbers 422, 430 through 444, 447 and up. 
 
 Certification Basis Type Certificate No. 1A13 (CAR 03, 15 December 1946, and Amendments 3-1 and 3-2. 
 
 Equipment The basic required equipment as prescribed in the applicable airworthiness requirements 
(see Certification Basis) must be installed in the aircraft for certification including the 
FAA-approved Airplane Flight Manual with its latest revision and appropriate 
supplements.   
 
  Refer to the applicable equipment list for additional approved equipment. 
 
V. Lake Model 250; 4 PCAmM (Normal Category) Approved 30 June 1983; 6 PCAmM (Normal Category)  
 Approved 12 April 1984 
 
Lake Model 250, 4-place is the same as LA-4-200 except for engine installation, vertical and horizontal tail surface configuration, 
horizontal tail trim surface, rudder trim tab, hull length, cargo door, landing gear “footprint” geometry, structural modific ation to 
engine pylon and wing, and gross weight. 
 
Lake Model 250-6-place is the same as Model 250, 4-place except for rear seat, auxiliary fuel (wing float) tanks are optional, 
increase in nose ballast, and tail ballast compartment. 
 
 Engine Lycoming IO-540-C4B5 (See Note 8.) 
 
 Fuel Minimum grade:  aviation gasoline 100 or 100LL 
 
 Engine Limits For all operations, 2575 r.p.m. (250 hp) 
 
 Propeller and Propeller Limits 1. TRW Hartzell, hub HC-E3YR-1RLF, blades FL7663D-2Q 
   Diameter:    76 inches (no outoff allowed) 
  Pitch setting at 30 in. sta.: 
    low  10.5°  
    high 26.0°  
     36.6° optional 
   2. TWR Hartzell hydraulic governor F-2-6A, F-2-6AZ or V3-3; or  
    Woodward N210681. 
 
 Airspeed Limits (CAS) Vne (never exceed)  170 mph  (148 knots)  
  Vfe (flaps extended) 125 mph  (109 knots)   
  Vle, Vlo (maximum landing gear 
    extended, operating) 125 mph  (109 knots)  
  Va (maneuvering) 135 mph  (117 knots) 
  Vno (maximum structural cruising) 135 mph  (117 knots)

7 of 9 1A13 
V. Lake Model 250  (cont’d) 
 
 C.G. Range  
C.G. Gross Weight 
150 in. 2600 lb. or less 
152.5 in. 3050 lb. 
153 in. 3140 lb. 
155 in. 3050 lb. (Landing) 
155 in. 3140 lb. (Takeoff and Enroute) 
158 in. 2600 lb. or less 
   
  Straight Line Variation Between Points Shown. 
150 151 152 153 154 155 156 157 158
2600 2600
3050 152.5 155
153 155
Landing
Takeoff and Enroute
C.G. Location, Inches
Aft of Datum
Gross
Weight,
Pounds
3140
 
 Empty Wt. C.G. Range See Note 7. 
 
 Datum Hull Sta. 0. (Hull Sta. 0 is 140.75 in. forward of the leading edge of the wing  
  at side of hull). 
 
 Maximum Weight  Ramp:  3151 lb. 
  Takeoff and Enroute:  3140 lb.  
  Landing:  3050 lb. 
 
 Minimum Crew 1 
 
 No. of Seats 4-place:   2 at (+96), 2 at (+126) 
  6-place:   2 at (+96), 2 at (+126), 2 at (+147) (Total weight of rear seat occupants  
                 limited to 200 lb. maximum). 
 
 Maximum Baggage 200 lb. (+168) 
 
 Fuel Capacity Main tank (+168) : 40.5 gal. total; 40 gal. usable 
  Wing float tanks (optional on 6-place) (+168): 14.5 gal. total; 14 gal. usable.  
  (See Note 9.) 
 
 Oil Capacity 12 qt. (+172)

1A13 8 of 9 
V. Lake Model 250  (cont’d) 
 
 Control Surface Movements Rudder  Right    25° ± 1°        Left   20° ± 1°      
  Rudder Trim Tab    L/R    33° ± 3° 
  Elevator     Up    25° + 1°, -2°    Down   27° ± 1° 
    
 Trim Surface      Up    36° + 2°, -1°     Down    24° + 2°, -1° 
 Flaps        Down   20° ± 1° 
  Flaps Up: 1/2° min., 1° max. droop relative to bottom 
    surface of wing at wing sta. 39 3/4 
 Ailerons Up 29° + 2°, -1° Down  15° ± 1° 
 Ailerons Neutral:       Up 5/8 in. ± 1/8 in. from alignment with fixed  
        outboard portion of wing trailing edge 
 
 Aileron Cable Rigging Tension 25 lb. ±  3 lb. 
 
 Manufacturer’s Serial Numbers Model 250, 4-place:  1, 2, 3, and 4 
  Model 250, 6-place:  5 and up 
 
 Certification Basis 1. 14 CFR Part 23, 18 December 1964, Amendments 23-1 to and including 23-23,  
   Subparts A, B, D, E, F, and G. 
 
  2. CAR 03, 15 December 1946, Amendments 3-1 and 3-2 as follows: 
   a. 03.2 (03.20 to and including 03.254) with exception that Part 23.427(c)  
    be complied with for tail surfaces. 
   b. 03.02, Airplane Categories - Normal 
   c. 03.3811, Emergency Provisions - Protection 
 
  3. 14 CFR Part 36, Appendix F, 18 December 1964, Amendments 36-1 to and  
   including 36-10. 
 
DATA PERTINENT TO ALL MODELS 
 Leveling Means Base of canopy, left or right side. 
 
 Production Basis None.  Prior to original certification, an FAA representative must perform a detailed 
inspection for workmanship, materials, and conformity with the approved technical data, a 
final inspection of the completed aircraft, and a check of the flight characteristics.  
 
NOTES 
 
 NOTE 1. All Models:  Current weight and balance report, including list of equipment included in 
certificated empty weight, and loading instructions, must be in each aircraft at the time of 
original certification and at all times thereafter.  The loading instructions are contained in 
the FAA-approved Airplane Flight Manual. 
 
 NOTE 2. Models C-1, C-2, LA-4, LA-4A, LA-4P, LA-4-200 
   The following placards must be displayed in full view of the pilot: 
 
   “THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE  
     IN COMPLIANCE WITH THE APPROVED AIRPLANE FLIGHT MANUAL.” 
 
   “NO ACROBATIC MANEUVERS, INCLUDING SPINS, APPROVED.” 
 
   All placards required in the approved airplane flight manual must be installed in the  
   appropriate location.

9 of 9 1A13 
 NOTE 2. (cont’d) Model 250 
   The following placards must be displayed in full view of the pilot: 
 
   Operating Limitations: 
   “THE MARKINGS AND PLACARDS INSTALLED IN THIS AIRPLANE CONTAIN  
   OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN  
   OPERATING THIS AIRPLANE IN THE NORMAL CATEGORY.  OTHER  
   OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN  
   OPERATING THIS AIRPLANE IN THIS CATEGORY ARE CONTAINED IN THE  
   AIRPLANE FLIGHT MANUAL.” 
 
   “THIS AIRPLANE IS CERTIFICATED FOR DAY OR NIGHT VFR OPERATIONS,  
     AND MAY BE EQUIPPED FOR DAY OR NIGHT IFR OPERATIONS.” 
 
   “FLIGHT INTO KNOWN ICING CONDITIONS IS PROHIBITED.” 
 
   “NO ACROBATIC MANEUVERS, INCLUDING SPINS, APPROVED.” 
 
 All placards required in the approved airplane flight manual must be installed in the  
 appropriate location. 
 
 NOTE 3. Reserved. 
 
 NOTE 4. Model LA-4:  Seaplane version is a Lake LA-4 modified in accordance with  
  STC SA781EA approved 8 July 1969 and amended 28 November 1969, issued to  
  Revo, Inc., P.O. Box 312, Sanford, Maine 04073, now located at 1396 Grandview Blvd.,  
  Kissimmee, Florida 34744. 
 
 NOTE 5. Model LA-4-200:  No structural change to LA-4-200 Type Design required for increase of 
Vne speed.  Increase of Vne speed for aircraft S/N 422-1036 requires installation of 
Consolidated Aeronautics Kit K-137 and a compatibility investigation of previously 
approved modifications, alterations, or equipment installations, other than FAA- approved 
type certificate holder’s changes to the Type Design, in relation to the increase of V ne 
speed. 
 
 NOTE 6. Model LA-4-200:  Maximum gross weight up to 2690 pounds is permitted when auxiliary 
fuel tanks (optional) are installed in accordance with weight and center of gravity 
limitations specified in Consolidated Aeronautics Flight Manual Supplement No. 4, 
December 28, 1973, as revised. 
 
 NOTE 7. Model 250, 4-place:  No empty weight C.G. range. 
  Model 250, 6-place:  See Loading Instructions in approved airplane flight manual.   
  Maximum removable ballast structural limitation:  nose (+54.5) 130 lb.; tail (+284)  
  50 lb. 
 
 NOTE 8. Model 250:  Turbocharged version is a Lake Model 250 modified in accordance with  
  STC SA469NE approved September 19, 1986 and amended March 31, 1988, issued to  
  Revo, Inc., P.O. Box 312, Sanford, Maine 04073, now located at 1396 Grandview Blvd.,  
  Kissimmee, Florida 34744. 
 
 NOTE 9. 34 gal. total usable fuel available in wing tanks (17 gal. each) installed in a ccordance  
  with STC SA264NE approved May 23, 1984, and amended February 21, 1985, issued to  
  Revo, Inc., P.O. Box 312, Sanford, Maine 04073, now located at 1396 Grandview Blvd.,  
  Kissimmee, Florida 34744. 
 
 NOTE 10. 4-place version available for Lake Model 250, 6-place modified in accordance with STC 
SA745NE approved April 19, 1990, issued to Revo, Inc., P.O. Box 312, Sanford, Maine  
  04073, now located at 1396 Grandview Blvd., Kissimmee, Florida 34744. 
 
 
 
.....END.....
```

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- [AD 72-07-11](https://openairdocs.org/ad/72-07-11): Flap pushrod end bearings · Revo Colonial C-1, Colonial C-2, Lake LA-4 and 3 more. Effective Jan 5, 1973
- [AD 67-11-01](https://openairdocs.org/ad/67-11-01): Fuel Pressure Gage Instrument Line · Revo Colonial C-1, Colonial C-2, Lake LA-4 and 2 more. Effective Aug 5, 1967
- [AD 65-15-03](https://openairdocs.org/ad/65-15-03): Nose Gear Drag Strut Bolt · Revo Lake LA-4. Effective Jul 1, 1965
- [AD 64-17-05](https://openairdocs.org/ad/64-17-05): Engine Breather Tube · Revo Lake LA-4, Lake LA-4A and Lake LA-4P. Effective Aug 28, 1964
- [AD 60-22-01](https://openairdocs.org/ad/60-22-01): Engine Mount · Revo Colonial C-2. Effective Nov 29, 1960
- [AD 57-06-01](https://openairdocs.org/ad/57-06-01): Landing Gear Lock · Revo Colonial C-1
- [AD 57-13-01](https://openairdocs.org/ad/57-13-01): Engine Strut Fittings · Revo Colonial C-1
- [AD 59-12-05](https://openairdocs.org/ad/59-12-05): Plastic Control Surface Locks · Revo Colonial C-1 and Colonial C-2
- [AD 59-15-02](https://openairdocs.org/ad/59-15-02): Aluminum Throttle Control Handle to the Steel Bell Crank · Revo Colonial C-1 and Colonial C-2
- [AD 59-17-04](https://openairdocs.org/ad/59-17-04): Wing Spar Attaching Bolts · Revo Colonial C-1 and Colonial C-2
- [AD 2005-12-02](https://openairdocs.org/ad/2005-12-02) (historical): Horizontal stabilizer attachment · Revo Colonial C-2, Lake LA-4, Lake LA-4-200 and 2 more. Effective Jul 8, 2005
- [AD 98-10-12](https://openairdocs.org/ad/98-10-12) (historical): Attachment Fitting and the Horizontal Stabilizer Rear Beam · Revo Colonial C-2, Lake LA-4, Lake LA-4-200 and 2 more. Effective Jun 8, 1998

## Registered aircraft by registry model (OpenAirDocs)

- [Consolidated Aeronautics LAKE LA-4-200](https://openairdocs.org/model/consolidated-aeronautics-lake-la-4-200): 139 aircraft (registry code 2400108)
- [Consolidated Aeronautics LAKE LA-4](https://openairdocs.org/model/consolidated-aeronautics-lake-la-4): 15 aircraft (registry code 2400102)
- [Aerofab LAKE LA-4-200](https://openairdocs.org/model/aerofab-lake-la-4-200): 0 aircraft (registry code 5110324)
- [Consolidated Aeronautics LAKE MODEL 250](https://openairdocs.org/model/consolidated-aeronautics-lake-model-250): 0 aircraft (registry code 2400111)
- [Revo COLONIAL C-1](https://openairdocs.org/model/revo-colonial-c-1): 0 aircraft (registry code 2400510)
- [Revo COLONIAL C-2](https://openairdocs.org/model/revo-colonial-c-2): 0 aircraft (registry code 2400512)
- [Revo LAKE LA-4](https://openairdocs.org/model/revo-lake-la-4): 0 aircraft (registry code 2400502)
- [Revo LAKE LA-4-200](https://openairdocs.org/model/revo-lake-la-4-200): 0 aircraft (registry code 2400508)
- [Revo LAKE LA-4P](https://openairdocs.org/model/revo-lake-la-4p): 0 aircraft (registry code 2400506)

## STCs approved under this data sheet (219, first 50)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc.
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of  existing instrument panel lights dimmer control.. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc.
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc.
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc.
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS  (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc.
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd.
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc.
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA2270WE](https://openairdocs.org/stc/SA2270WE): Installation of Roto-Master (Rajay) Turbocharged Lycoming O-360-A1A or AID Engine (modified per STC SE154SO).. TALCO Aviation
- [STC SA2990WE](https://openairdocs.org/stc/SA2990WE): Installation of Turbocharged Lycoming IO-360-A1B engine. TALCO Aviation
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA1650NM](https://openairdocs.org/stc/SA1650NM): Installation of Lycoming IO-360-A1B engine, Hartzell HC-CZYK-1BLF/FL7666A-2 propeller, updated fuel system, strut fairings and horizontal/vertical stabilizer fairing.. Dale Turner
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc.
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc.
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04621NY](https://openairdocs.org/stc/SA04621NY): Installation of the LCA01917 Exhaust System. Lake Central Air Services
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA04570NY](https://openairdocs.org/stc/SA04570NY): Installation of the Lake Renegade Cabin Step Extension. Lake Central Air Services
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA2069CE-D](https://openairdocs.org/stc/SA2069CE-D): Install KAP-150 three axis or KFC-150 three axis flight control system with optional KAS-297B vertical speed and altitude selector.. Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc.

All 219: https://openairdocs.org/tcds/1A13/stcs.md

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