# TCDS 3A1: MICCO Aircraft Company

- Type: Type certificate data sheet
- Status: Current
- Holder: MICCO Aircraft Company
- Revision: 16
- Revised: September 1, 2006
- Product: Aircraft, Small Airplane
- Certification basis: Part 23, Part 36, CAR 4a
- Registered aircraft: 31, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/41/53/4153a4e04ced8a930f90359bd9a34e07f227359cf71fb0d3f64375c4eddad874
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CDF4FA2D7930459D862571FB0058FE38.0001
- Page: https://openairdocs.org/tcds/3A1

## Models (4)

As the data sheet lists them.

- MAC-145B
- MAC-125C
- MAC-145
- MAC-145A

## What the data sheet says

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

```text
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
3A1 
Revision 16 
MICCO AIRCRAFT CO., INC. 
(Meyers, LanShe) 
 
MAC-145 
MAC-125C 
MAC-145A 
MAC-145B 
September 1, 2006 
 
TYPE CERTIFICATE DATA SHEET NO. 3A1
 
Type Certificate Holder MICCO Aircraft Company, Inc. 
 407 NW Wiley Post Road 
 Frank Phillips Field, Hangar #7 
 Bartlesville, Oklahoma  74003 
 
Type Certificate Holder Record Meyers Aircraft Company transferred 3A1 to Interceptor Corporation on 
January 8, 1969 
 Interceptor Corporation transferred 3A1 to Interceptor Company on  
 December 31, 1974 
 Interceptor Company transferred 3A1 to Prop-Jets Incorporated on July 1, 1977 
 Prop-Jets Incorporated transferred 3A1 to Nydia Meyers Trust on  
 March 2, 1981 
 Nydia Meyers Trust transferred 3A1 to Ralph Haven May 8, 1981 
 Ralph Haven transferred 3A1 to The New Meyers Airplane Company on  
 March 21, 1994 
 The New Meyers Airplane Company transferred 3A1 to Estumkeda, Ltd. (d.b.a. 
Micco Aircraft Co.) on January 18, 1995 
 Estumkeda, Ltd. transferred 3A1 to LanShe Aerospace, LLC on  
 February 22, 2003 
 LanShe Aerospace, LLC transferred 3A1 to Aero Acquisitions, LLC on  
 September 12, 2005 
 Aero Acquisitions, LLC transferred 3A1 to Micco Aircraft Company, Inc. on 
 September 1, 2006 
 
I - Model MAC-145, 2 PCLM, Approved November 2, 1948
 
Engine C ontinental C145-2 
 
Fuel 80 Min. octane aviation gasoline 
 
Engine limits For all operations, 2700 rpm (145 hp) 
 
Propeller limits Static rpm at maximum permissible throttle setting: 
  (with Equipment Item 1)  Not over 2380, not under 2210. 
  No additional tolerance permitted. 
 Diameter:  Not over 76 in., not under 71.5 in. 
 
Page No. 1 2 3 4 5 6 7 8 9 10 
Rev.No. 16 11 11 11 13 13 15 11 13 13

3A1 Page 2 of 10 
 
 
Airspeed limits Glide or dive 200 mph True Ind. 
 Level flight or climb 155 mph True Ind. 
 Flaps extended 95 mph True Ind. 
 Gear extended 110 mph True Ind. 
 
C.G. range (+16.7) to (+19.0) at 1910 lbs. (See NOTE 4 for required modification) 
 (+15.0) to (+19.0) at 1735 lbs. 
 (+13.7) to (+19.0) at 1600 lbs. or less. 
 Straight line variation between points given. 
 
 
LBS.
2000
190 0
180 0
170 0
160 0
150 0
140 0
13 14 15 16 17 18 19 20
INCHES
(Fo r unmodified
airplanes)
FWD
LIM IT
REAR
LIMIT
 
 
Empty weight C.G. range (+10.5) to (+14.3).  When empty weight C.G. falls within this range, 
computation of critical force and aft C.G. positions is unnecessary.  Range is 
not valid for non-standard configurations.   
 
Datum  12 inches aft of forward face of firewall at centerline of airplane 
 
Leveling means  Lower door sill 
 
Maximum weight 1735 lbs. (1910 lbs. when modified in accordance with provisions of NOTE 4) 
 
No. of seats 2 (+26) 
 
Maximum baggage 100 lbs. (+54) (Main) 
 20 lbs. (+61) (Map shelf per Meyers Dwg. No. 43G027) 
 
Fuel capacity 32 gals. Main (+33).  (See Equipment Item 107 for auxiliary fuel system) 
 
Oil capacity 2 gals. (-40)

3A1 Page 3 of 10 
  
 
Control surface movements Elevator - Restricted Up 9°  Down 20° 
               Unrestricted Up 22°  Down 20° 
 Elevator trim tab  Up 14°  Down 50° 
 Ailerons  Up 22°  Down 9.5° 
 Rudder - Restricted Right 9.5°  Left 9.5° 
  Unrestricted Right 21°  Left 16° 
 Flaps  Up 0°  Down 45° 
 
Serial Nos. eligible 203 and up 
 
Export eligibility  Eligible for export to all countries subject to the provisions of MOP 2-4 except 
as follows: 
  (a)  Canada - Landplane – eligible,    Skiplane - not eligible 
 
Required equipment Equipment Items 1 (or 2 or 3 or 5 or 6), 101, 102, 104, 105, 106, 201, 202, 
 204, 301, 302, 303. 
 
II - Model MAC-125C, 2 PCLM 
(Same as Model MAC-145 except for engine and propeller installation). 
 
Engine C ontinental C125-2 
 
Fuel 80 min. octane aviation gasoline 
 
Engine limits For all operations,  2550 rpm (125 hp) 
 
Airspeed limits Glide or dive 200 mph True Ind. 
 Level flight or climb 155 mph True Ind. 
 Flaps extended 95 mph True Ind. 
 Gear extended 110 mph True Ind. 
 
Propeller limits See Equipment Item 4 
 
C.G. range (+16.7) to (+19.0) at 1735 lbs. 
 (+13.7) to (+19.0) at 1600 lbs. 
 Straight line variation between points given. 
 
LB S.
173 5
16 00
15 00
14 00
13 00
13 14 15 16 17 18 19 20
INCH ES
FW D
LI MIT
RE AR
LI MIT
12

3A1 Page 4 of 10 
 
 
Empty weight C.G. range (+10.6) to (+14.3).  When empty weight C.G. falls within this range, 
computation of critical fore and aft C.G. positions is unnecessary.  Range is 
not valid for non-standard arrangements. 
 
Datum  12 inches aft of forward face of  firewall at centerline of airplane 
 
Leveling means  Lower door sill 
 
Maximum weight 1735 lbs.  
 
No. of seats 2 (+26) 
 
Maximum baggage 50 lbs. (+41) 
 
Fuel capacity 32 gals. Main (+33).  (See Equipment Item 107 for auxiliary fuel system) 
 
Oil capacity 2 gals. (-40) 
 
Control surface movements Elevator - Restricted Up 9°  Down 20° 
               Unrestricted Up 22°  Down 20° 
 Elevator trim tab  Up 14°  Down 50° 
 Ailerons  Up 22°  Down 9.5° 
 Rudder - Restricted Right 9.5°  Left 9.5° 
  Unrestricted Right 21°  Left 16° 
 Flaps  Up 0°  Down 45° 
 
Serial Nos. eligible 203 and up 
 
Export eligibility  Eligible for e xport to all countries subject to the provisions of MOP 2-4 except 
as follows: 
  (a)  Canada - Landplane - eligible 
   Skiplane - not eligible 
 
Required equipment Equipment Items 4, 101, 102, 104, 105, 106, 201, 202, 204, 301, 302, 303. 
 
 
III - Model MAC-145A, 2 PCLM (Utility Category), Approved January 5, 2000 
 
Engine Textron Lycoming IO-360-C1E6 
 
Fuel 100/100LL minimum grade aviation gasoline 
 
Engine Limits  For all operations  2700 rpm (200 hp) 
 
Propeller and Propeller Limits McCauley B3D36C424-E/74SA-0 
 Avoid continuous operation below 15 inHG manifold pressure setting  
 between 1650 and 2250 rpm when above 85 KIAS  
 
Airspeed Limits (IAS) VNE (Never Exceed)   180 knots 
 V C (Maximum Structural Cruising)  138 knots 
 V A (Design Maneuvering)   120 knots 
 V FE (Flaps Extended)   110 knots 
 V LO (Maximum Gear Retraction/Extension) 118 knots 
 V LE (Maximum Gear Extended)  128 knots

3A1 Page 5 of 10 
  
 
C.G. Range (Utility) (+103.5) to (+105.5) at 2600 lbs. 
 (+101.5) to (+105.5) at 2000 lbs. or less 
 
 
LB S.
26 00
24 00
22 00
20 00
18 00
10 1 102 10 3 104 105 106
INCH E S AF T OF  DATUM
FW D
LIM IT
RE A R
LI M IT
10 0
 
 
Empty Weight C.G. Range None 
 
Datum  70.0 inches forward of front cabin bulkhead  
 
Leveling Means  2 screws at Station 72.7 and 83.2 at W.L. 101.3, located on left side of  
  cabin area 
 
Maximum Weight (Utility) 2600 lbs. Takeoff 
 2492 lbs. Landing 
 
No. of Seats 2 (+114.0 Fwd. seat position, +117.8 Aft seat position) 
 
Maximum Baggage 100 lbs. at (+137.5) 
 
Fuel Capacity 68 gallons usable at (+117.9), 4 gallons unusable fuel at (+116.0) 
 See NOTE 1 
 
Oil Capacity 2 gallons (+30.0) 
 
Control Surface Movements Elevator Up 28° Down 20° 
 El evator Trim Up 9° Down 20° 
 Elevator Trim*  Up 4° Down 24° 
 Ai lerons Up  22° Down 12° 
 R udder Right 22° Left 22° 
 Flaps Up 0° Down 30° 
 (Tolerance ± 2°) 
 * Elevator Trim travel for airplanes equipped with aileron servo tabs 
 
Maximum Operating Altitude 12,000 feet MSL 
 
Serial Numbers Eligible 304 and subsequent

3A1 Page 6 of 10 
 
 
 
IV - Model MAC-145B, 2 PCLM (Utility Category and Acrobatic Category*), Approved October 19, 2000 
  *Acrobatic Category approved March 4, 2002.  See NOTE 5 for Acrobatic modifications. 
 
Engine Textron Lycoming IO-540-T4B5 
 
Fuel 100/100LL minimum grade aviation gasoline 
 
Engine Limits  For all operations  2700 rpm (260 hp) 
 
Propeller and Propeller Limits Hartzell HC-C3YR-1RF/F7693F 
 See NOTE 3 for Acrobatic limitation. 
 
Airspeed Limits (IAS) VNE (Never Exceed)   195 knots 
 V C (Maximum Structural Cruising)  166 knots 
 V A (Design Maneuvering)   121 knots 
 V FE (Flaps Extended)   111 knots 
 V LO (Maximum Gear Retraction/Extension) 118 knots 
 V LE (Maximum Gear Extended)  128 knots 
 
C.G. Range  Utility Category
 (+103.5) to (+105.5) at 2850 lbs. 
 (+102.5) to (+105.5) at 2500 lbs. or less 
 
 Acrobatic Category 
 (+103.5) to (+104.5) at 2650 lbs. 
 (+102.5) to (+104.5) at 2500 lbs. or less 
 
 
LB S .
29 0 0
28 0 0
27 0 0
26 0 0
2 500
10 2 10 3 10 4 10 5 10 6
I N CH E S  AF T  OF  DAT U M
FW D
LI MIT
REA R
LI MIT
10 1
AC R O B A T IC
C A T E GOR Y
      U T IL IT Y
C A T E GOR Y
 
 
Empty Weight C.G. Range None 
 
Datum  70.0 inches forward of firewall

3A1 Page 7 of 10 
  
Leveling Means  2 screws at Station 72.7 and 83.2 at W.L. 101.3, located on left side of  
  cabin area 
 
Maximum Weight   Utility Category Acrobatic Category  
 Takeoff  2850 lbs.   2650 lbs. 
 Landing  2742 lbs.   2650 lbs. 
 
No. of Seats 2 (+114.0 Fwd. seat position, +117.8 Aft seat position) 
 
Maximum Baggage Utility Category - 100 lbs. at (+137.5) 
 
 Acrobatic Category - None 
 
Fuel Capacity Utility Category
  See NOTE 1 68 gallons usable at (+117.9), 4 gallons unusable fuel at (+116.0) 
 
 Acrobatic Category 
 28 gallons usable at (+119.93), 4 gallons unusable fuel at (+119.3) 
 (CAUTION:  Utility fuel tanks must be empty for acrobatic flight.) 
 
Oil Capacity 2 gallons (+39.6) 
 
Control Surface Movements El evator Up 28° Down* 20° 
 Elevator Trim  Up 4° Down 24° 
 Ailerons Up  22° Down 12° 
 Rudder Right 22° Left 22° 
 Flaps Up 0° Down 30° 
 (Tolerance ± 2°) 
 *For airplanes with acrobatic modification installed, Elevator Down 
 travel is 27°. 
 
Maximum Operating Altitude 14,000 feet MSL 
 
Serial Numbers Eligible 260001 and subsequent  (see NOTE 5) 
 
 
DATA PERTINENT TO ALL MODELS
 
Certification basis Type Certificate No. 3A1 issued November 2, 1948 
 
 Models MAC 125C and MAC-145 - CAR 4a 
 
Models MAC-145A and MAC-145B - 14 CFR Part 23 as amended by 23-1 through  
23-46 effective June 16, 1994; with the following rules at these listed amendment levels:  
23.179, 23.301, 23.305, 23.321, 23.351, 23.479, 23.485, 23.603, 23.605, 23.607, 23.611, 
23.613, 23.619, 23.621, 23.655, 23.675, 23.677, 23.679, 23.721, 23.723, 23.731, 
23.1331, 23.1351, 23.1353, 23.1357, 23.1365, 23.1385, 23.1387, 23.1389, 23.1391, 
23.1393, 23.1395, 23.1397, 23.1411, 23.1413, 23.1431 and 23.1507 effective February 
1, 1965;  23.75, 23.77, 23.333, 23.337, 23.341, 23.345, 23.349, 23.361, 23.415, 23.455, 
23.473, 23.572, 23.629, 23.733 and 23.1501 as amended by 23-7;  23.1587 as amended 
by 23-13;  23.173 as amended by 23-14;  23.335 as amended by 23-16;  23.145 and  
 23.1309 as amended by 23-17;  23.45, 23.175, 23.177 and 23.181 as amended by 23-21;  
23.853 as amended by 23-23;  23.397, 23.561 and 23.785 as amended by 23-34;

3A1 Page 8 of 10 
 
 23.371(for acrobatic only), 23.421, 23.423, 23.425, 23.427, 23.441 and 23.443 as  
 amended by 23-48 (Part 23, Appendix A); and 23.71 and 23.73 as amended by 23-50 
with Equivalent Safety Finding to 23.1143(g) throttle and mixture control cable 
attachment and CAR 04a.702 in lieu of 23.65. 
 MAC-145A - 14 CFR Part 36 as amended by 36-20. 
 MAC-145B - 14 CFR Part 36 as amended by 36-22. 
 
Production basis None.  Prior to orig inal certification of each aircraft an FAA representative must perform 
a detailed inspection for workmanship, material, and conformity with the approved 
technical data and a check of the flight characteristics. 
 
Equipment   The following equipment is for Models MAC-125C and MAC-145: 
   
(A plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change when that 
item is installed.) 
 
MAC-125C/MAC-145 Propellers and Propeller Accessories
1. Propeller - Lewis L-6FK-3-54, L-6FK-3-52, L-6FK-48 or any other fixed pitch wood  15 lbs. (-59) 
 propeller which is eligible for the engine power and speed and which meets the diameter  
 and static rpm limits given under "Propeller Limits" for Model MAC-145.   
 Eligible only with Continental C-145 engine with dampered crankshaft denoted by suffix  
 letter "D" after engine serial number.  
 
2. Propeller - McCauley 1A170-DM7657 or any other Model 1A170-DM propeller that  34 lbs. (-59) 
 meets the following limits:  Static rpm at maximum permissible throttle setting:  Not over  
 2230, not under 2110.  No additional tolerance permitted.  Diameter:  Not over 76 in.,  
 not under 72.5 in.   
 Eligible on Model MAC-145 only.   
 McCauley propeller spinner, Meyers Dwg. #47R032 optional. 
 
3. Propeller - Hartzell ground adjust able HA12UF/8032-6 Blade pitch setting 15° at 3/4  22 lbs. (-59) 
 of propeller radius or set to obtain following limits:  Static rpm at maximum permissible  
 throttle setting:  Not over 2210, not under 2110.   No additional tolerance permitted.   
 Diameter:  Not over 74 in., not under 72.5 in.  
 Eligible on Model MAC-145 only with Continental C-145 engine dampered crankshaft  
 denoted by suffix letter "D" after engine serial number.  
 
4. Propeller - Koppers Aeromatic F200/0074E Parts List assembly No. 4920, dated   33 lbs. (-60) 
 October 13, 1948.  Installa tion and operation must be accomplished in accordance with  
 Koppers "Installation Procedures and Opera ting Limitations No. 24," dated October 12,  
 1948.  Low pitch setting 13° at 24 in. sta.  Static  rpm at maximum permissible throttle setting:   
 Not over 2550, not under 2450.  No a dditional tolerance permitted.   
 Diameter:  Not over 74 in., not under 72.5 in.   
 Eligible on Model MAC-125C only. 
 
5. Propeller - Koppers Aeromatic F200H/00-74E Pa rts list assembly No. 4356H-1  34 lbs. (-61)  
 (Includes Altitude Control 4427)  6 lbs. (-46) 
 Adjustment and opera tion must be accomplished in accordance with  
 Koppers "Adjustment Instructions and Operating Limitations No. 45"   
 Low pitch setting 13° at 24 in. sta.   
 Static rpm at maximum permissible thro ttle setting:  Not over 2675, not under 2575.

3A1 Page 9 of 10 
  
 No additional tolerance permitted.   
 Diameter:  Not over 74 in., not under 72.5 in.  
 (Eligible on Model MAC-145 only with Continental C-145 engine dampered crankshaft  
 denoted by suffix letter "D" after engine serial number).   
 Hampton propeller spinner Model 1-B optional. 
 
6. Propeller - Sensenich M74DR, fixed pitch metal (Model MAC-145 only)  30 lbs. (-59) 
 Static rpm at maximum permissible thro ttle setting:  Not over 2380, not under 2210.   
 No additional tolerance permitted.   
 Diameter:  Not over 74 in., not under 72 in.  
 
MAC-125C/MAC-145 Engines and Engine Accessories - Fuel and Oil System
101. Carburetor air heater and mufflers (Meyers Dwg. No. 47R003) 14 lbs.  (-35) 
102. Carburetor air intake and filter assy .  (Continental No. A40692) 4 lbs.  (-42) 
103. Starter, Delco-Remy No. 1109656 (Continental No. 50309) 16 lbs.  (-25) 
104. Engine- driven fuel pump, AC No. 1539051 (Continental No. 40585) 2 lbs.  (-52) 
105. Hand fuel pump, AC No. 1539051 (Continental No. 40585) 2 lbs.  (-14) 
106. Cowl flaps and control (Meyers Dwg. No. 47R008) 2 lbs.  (-15) 
107. Auxiliary fuel system installation per Meyers Dwg. 47R004,   13 lbs. (+29) 
    R.H. and L.H. wing tanks, capacity 8½ gals. each  
 Fuel arm of auxiliary tanks (+29) 
108. Electric fuel pump, Bendix Model No. 476818, replacing  
   Item 05 (Model MAC-145 only).   2 lbs.  (-14) 
 
MAC-125C/MAC-145 Landing Gear
201. Two main wheel-brake assemblies, 6.00-6, Type III 13 lbs.  (+8) 
 (a) Goodrich (formerly Hayes) Model 600MD 
  Wheel Assembly No. D-3-47MD 
  Brake Assembly No. D-2-129  
 (b) Goodrich Model 601MD 14 lbs. (+8) 
  Wheel Assembly No. D-3-512-MD 
  Brake Assembly No. D-2-505  
202. Two main wheel 4-ply rating tires, 6.00-6, Type III (with regular tubes)  18 lbs.  (+8) 
204. Tail wheel assembly  
 (a) Meyers Dwg. No. 44B039   12 lbs.  (+166) 
 
MAC-125C/MAC-145 Electrical Equipment
301. Battery - 12 volt   31 lbs.  (-15) 
302. Engine driven generator (Cont. 40435)   10 lbs.  (-25) 
303. Voltage regulatory - Delco-Remy (Cont. 40483)   2 lbs.  (-14) 
 
MAC-125C/MAC-145 Interior Equipment
401. Wheel control, Meyers Dwg. No. 46A040   10 lbs.  (+20) 
402. Stick control, Meyers Dwg. No. 46R001     7 lbs.  (-20) 
 
 
For Models MAC-145A and MAC-145B - The basic required equipment as prescribed in the applicable  
airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification.  In addition, the 
following items of equipment are required: 
 
 1.  FAA Approved Airplane Flight Manual for the Micco MAC-145A, Document No. F-145A-3, dated 
January 5, 2000, or later FAA approved revision.

3A1 Page 10 of 10 
 
 
 2.  FAA Approved Airplane Flight Manual for the Micco MAC-145B, Document No. F-145B-3, dated 
October 19, 2000, or later FAA approved revision. 
 
 3.  FAA Approved Airplane Flight Manual Supplement for the Micco MAC-145B with Acrobatic Option, 
Document No. F-145B-3A, dated March 4, 2002, or later FAA approved revision. 
 
NOTE 1 A current weight and balance report including list of  equipment included in certificated weight empty, and 
loading instructions when necessary, must be in each aircraft at the time of original certification.  The 
certificated empty weight and corresponding center of gravity location must include unusable fuel  
 of 24 lbs. at (+116.0) for the MAC-145A and Utility Category MAC-145B and 24 lbs. at (+119.3) for the 
MAC-145B operating in Acrobatic Category. 
 
NOTE 2 For Models MAC-125C and MAC-145, the following placar ds must be displayed in front of and in clear 
view of the pilot: 
 
 "INTENTIONAL SPINNING PROHIBITED." 
  "DO NOT EXTEND FLAPS ABOVE 95 MPH." 
  "DO NOT EXTEND GEAR ABOVE 110 MPH." 
 
 For Models MAC-145A and MAC-145B, all placards required in the FAA Approved Airplane Flight 
Manual and any applicable Airplane Flight Manual Supplement must be installed in the appropriate 
locations. 
 
NOTE 3 For MAC-145A and MAC-145B, see FAA approved Airworthiness Limitations section of the  
 Instructions for Continued Airworthiness (Section 4 of Airplane Maintenance Manual) for mandatory 
inspections or retirement time limits. 
 
NOTE 4 Model MAC-145 aircraft are eligible at 1910 lb s. maximum weight when following is accomplished: 
 (a) Reinforcement of fuselage tail cone bulkhead  No. 4 as per Meyers Dwg. No. 43R001 change C or 
subsequent. 
 (b) Install propeller equipment item (2) or (5) as noted. 
 
NOTE 5. Model MAC-145B aircraft, S/N 260001 and subsequent, are eligible for multiple airworthiness 
certification in the Utility and Acrobatic Categories when modified in accordance with Micco Aircraft 
Acrobatic Drawing List 200005, dated March 4, 2002, or later FAA approved revision. 
 
 
...END...
```

## ADs (2, in force first)

- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005

## Registered aircraft by registry model (OpenAirDocs)

- [Meyers MAC-145](https://openairdocs.org/model/meyers-mac-145): 14 aircraft (registry code 5650104)
- [Estumkeda Ltd DBA Micco Acft MAC-145B](https://openairdocs.org/model/estumkeda-ltd-dba-micco-acft-mac-145b): 10 aircraft (registry code 5660002)
- [Estumkeda Ltd DBA Micco Acft MAC-145A](https://openairdocs.org/model/estumkeda-ltd-dba-micco-acft-mac-145a): 5 aircraft (registry code 5660000)
- [Lanshe Aerospace MAC-145B](https://openairdocs.org/model/lanshe-aerospace-mac-145b): 2 aircraft (registry code 5660005)
- [Estumkeda Ltd DBA Micco Acft MAC-125C](https://openairdocs.org/model/estumkeda-ltd-dba-micco-acft-mac-125c): 0 aircraft (registry code 5660001)
- [Lanshe Aerospace MAC-145](https://openairdocs.org/model/lanshe-aerospace-mac-145): 0 aircraft (registry code 5660003)
- [Lanshe Aerospace MAC-145A](https://openairdocs.org/model/lanshe-aerospace-mac-145a): 0 aircraft (registry code 5660004)
- [Meyers Industries MAC-125C](https://openairdocs.org/model/meyers-industries-mac-125c): 0 aircraft (registry code 5650102)

## STCs approved under this data sheet (85, first 50)

- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc.
- [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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [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 SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): 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 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 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 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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [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 SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [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 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 SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc.
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01768SE](https://openairdocs.org/stc/SA01768SE): Installation of an oil cooler system.. Steve's Aircraft
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc

All 85: https://openairdocs.org/tcds/3A1/stcs.md

---
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.