# TCDS A7EA: NZSkydive Limited

- Type: Type certificate data sheet
- Status: Current
- Holder: NZSkydive Limited
- Revision: 11
- Revised: March 30, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 23, Part 36
- Registered aircraft: 34, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/c2/6e/c26ecf1f63e76440e1ab76d54f1cc15bda43e7bf27d6acaaa659f0772be1de4c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8EF761197F76D19E8625883D004593D6.0001
- Page: https://openairdocs.org/tcds/A7EA

## Models (7)

As the data sheet lists them.

- FBA-2C4T
- FBA-2C
- FBA-2C2
- FBA-2C3
- FBA-2C4
- FBA-2C1
- FBA-2C3T

## 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 
 
TYPE CERTIFICATE DATA SHEET NO. A7EA 
 
This data sheet which is a part of type certificate No. A7EA prescribes conditions and limitations under which the product for which the 
type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. 
 
Type Certificate Holder  NZSkydive Limited 
  Trading as Pacific Aerospace 
  333 Airport Road  
  Hamilton 3282 
  New Zealand  
 
     Type Certificate Holder Record  Pacific Aerospace Ltd. transferred TC A7EA to NZSkydive Limited on November 29, 2021. 
Found Aircraft Canada, Inc. transferred TC A7EA to Pacific Aerospace Ltd on November 23, 2017. 
 
I - Model FBA-2C, 5 PCLM (Normal Category), Approved June 23, 1965 by the FAA and February 19, 1964 by the 
Canadian Department of Transport (DOT) 
 
Engine Lycoming O-540-A1C5 
 
Fuel 91-96 minimum grade aviation gasoline 
 
Engine limits Maximum for all operations, 250 hp. at 2575 r.p.m. 
Full throttle at sea level 
 
Propeller and McCauley variable pitch Model 2D36C28/80MM-6 
Propeller limits Diameter:  Maximum 74 inches, minimum 73 inches 
No reduction in minimum size allowed 
Pitch setting at Station 30.0: low 15.7°, high 32.0° 
Constant speed governor Woodward 210395 
Hartzell Constant Speed HC-927K-1D/8847-0 70 lb. (-63.0 in.) 
Diameter:  maximum 88 inches, minimum 88 inches 
Pitch setting at Station 30.0 inches: low 12°, high 26.4° 
Woodward constant speed governor B210340 
Airspeed limits Vne (never exceed) 155.3 m.p.h.  (135 knots) 
(CAS) Vno (max. structural cruising) 123.3 m.p.h.  (107 knots) 
 VA (maneuvering) 130   m.p.h.   (112.5 knots)  
 Vfe (flaps extended) 108.0 m.p.h.  (93.5 knots) 
 
C.G. range Landplane and Skiplane  (See Note 4 for Ski Installations) 
(Landing Gear Fixed) 
Gross Weight Forward Limit Aft Limit  
2850 lb. +17.0 in. +24.5 in.  
2250 or less +15.3 in. +24.5 in. 
 
Seaplane  (See Note 5 for Float Installations) 
 
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 
Rev. No. 11 11 8 8 11 8 8 8 8 11 8 10  8 8 8 8 8 
A7EA 
Revision 11 
NZSkydive 
Limited 
FBA-2C, FBA-2C1 
FBA-2C2, FBA-2C3 
FBA-2C4, FBA-2C3T 
FBA-2C4T 
March 30, 2022

A7EA Page 2 of 17 
 
 
 
  
 
Serial Nos. eligible     3 to 27 inclusive.   
 
 
II - Model FBA-2C1, (Bush Hawk) (Normal Category), Approved March 3, 2000 by the FAA and March 5, 1999 by 
the Canadian Department of Transport (DOT) 
 
Engine Lycoming I0-540-D4A5 (260 HP) or 
Lycoming I0-540-L1C5 (300 HP) 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
Engine limits Maximum for all operations; Full throttle at sea level 
I0-540-D4A5: 260 HP at 2700 r.p.m. 
I0-540-L1C5:  300 HP at 2700 r.p.m. 
 
Propeller and Hartzell 3-blade variable pitch  HC-C3YR-1RF/F8468A-2R 
Propeller Limits Diameter:  Maximum 84 inches, Minimum 83 inches 
 
Pitch setting at Station 30.0: low 10.3° 
high 31.0° 
Constant Speed Governor, Hartzell V-5-4 
Gross Weight Forward Limit Aft Limit 
2850 lb. +17.0 in. +24.5 in. 
2250 or less +15.3 in. +24.5 in. 
 Straight line variation between points given  
Empty Weight 
C.G. Range 
None  
Datum Main landing gear beam center line  
M.A.C. 62.3 in.  
Leveling means Aircraft cabin floor level - laterally and longitudinally  
Maximum weight Landplane and Skiplane   2850 lb. 
Seaplane 2850 lb.  (See Note 3 for eligibility at 3,000 lbs.) 
 
Minimum crew 1 Pilot  
Number of Seats 5, including pilot (2 at +17.8 in., 3 at +61.75 in.)  
Maximum baggage 150 lb. at +92.5 in.  
Fuel capacity 56.0 Imperial gallons (67.3 U.S. gallons) total (+22.2 in.) 
28  Imperial gallons (33.6 U.S. gallons) each wing tank. 
55.0 Imperial gallons (66.1 U.S. gallons) usable. 
 
Oil capacity 10.5 Imperial quarts (12.6 U.S. quarts) max. (-38.8 in.)  
Control surface Wing Flaps 0° up 32° down  
Movements Aileron 18° up 12° 
Elevator (0° Stab.) 29.5° up 21.5° 
Stabilizer 3° up 5° 
Rudder 30° left 30° 
down 
down 
down 
right

A7EA Page 3 of 17 
 
 
 
Airspeed Limits With 260 HP I0-540-D4A5 engine  
(CAS) Vne (never exceed) 162 m.p.h.  (141 knots)  
 Vno (max. structural cruising) 145 m.p.h.  (126 knots)  
 VA (maneuvering) 135 m.p.h.  (117 knots)  
 Vfe (flaps extended) 118 m.p.h.  (103 knots) 
 
With 300 HP I0-540-L1C5 engine 
Vne  (never exceed) 162 m.p.h.  (141 knots) 
Vno          (max. structural cruising) 145 m.p.h.  (126 knots) 
VA (maneuvering) 135 m.p.h.  (117 knots) 
Vfe (flaps extended) 118 m.p.h.  (103 knots) 
 
C.G. range Landplane and Skiplane 
(Landing Gear Fixed)  Gross Weight Forward Limit  Aft Limit 
3200 lbs. +17.0 in. +24.5 in. 
1900 +17.0 in. +24.5 in. 
 
Seaplane 
Gross Weight Forward Limit Aft Limit 
3500 lbs. +17.0 in. +23.5 in. 
1900 +17.0 in. +23.5 in. 
 
Straight line variation between points given. 
Additional limitations for specific ski and float installations may be contained in Notes 4 and 5. 
 
Empty Weight None 
C.G. Range 
 
Datum Land Plane: Main Wheel Axle 
Sea Plane: Lower Forward Corner of Front Door 
 
M.A.C. 62.3 in. 
Leveling Means Aircraft  cabin floor level – laterally and longitudinally. 
Maximum Weight Landplane and skiplane    3,200 lbs. 
Seaplane 3500 lbs. (see Note 5 for specific weight limitation with 
each float installation.) 
 
Minimum crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. at 94 in.  
Fuel Capacity At +21.8 in 
Usable 
Liters 
372 
Imp. Gals. 
81.9 
U.S. Gals. 
98.3 
 Unusable 6 1.4 1.7 
 Total 378 83.3 100.0 
 
Oil Capacity 11.4 liters / 10 imperial quarts / 12 U.S. quarts maximum (at -40 in.) 
 
Control Surface 
Movements 
Wing Flaps 
Aileron 
0° 
18° 
up 
up 
8,15,22,32 
12° 
down 
down 
 Elevator (0° Stab.) 
Stabilizer 
Rudder 
29.5° 
6° 
30° 
up 
up 
left 
21.5° 
4° 
30° 
down 
down 
right 
Serial Numbers 
Eligible 
28 through 99

A7EA Page 4 of 17 
 
 
 
 
III- Model FBA-2C2, (Bush Hawk XP) (Normal Category), Approved January 11, 2005 by the FAA and May 14, 2004 by 
the Canadian Department of Transport (DOT) 
 
Engine Lycoming I0-540-L1C5 (300 HP) 
 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
Engine limits Maximum for all operations 2700 r.p.m. 
Propeller and 1. Hartzell 3-blade variable pitch  HC-C3YR-1RF/F8468A-2R 
Propeller Limits Diameter:  Maximum 84 inches, Minimum 83 inches 
Pitch setting at Station 30.0: low 10.3° 
high 31.0° 
Constant Speed Governor, Hartzell V-5-4 
 
2. Hartzell 3-blade variable pitch HC-C3YR-1RF/F8068 
Diameter:  Maximum 82 inches, Minimum 81 inches 
Pitch setting at Station 30.0: low 12.3° 
high 31.0° 
Constant Speed Governor, Hartzell V-5-4 
 
Airspeed Limits Vne          (never exceed) 182 m.p.h.  (158 knots) 
Vno          (max. structural cruising) 161 m.p.h.  (140 knots) 
VA (maneuvering) 131 m.p.h.  (114 knots) 
Vfe (flaps extended) 132 m.p.h.  (115 knots) 
 
C.G. range Landplane 
(Landing Gear Fixed)   Gross Weight Forward Limit Aft Limit 
3500 lbs. +20.5 in. +24.5 in. 
2750 lbs +17.0 in. +24.5 in. 
1950 lbs +17.0 in. +24.5 in. 
 
Seaplane 
Gross Weight Forward Limit Aft Limit 
3800 lbs. +20.5 in +23.5 in. 
2750 lbs +17.0 in. +23.5 in. 
2250 lbs +17.0 in. +23.5 in. 
 
Straight line variation between points given. Gross weight and c.g. may vary depending on 
the installation of Optional Equipment. 
 
Empty Weight None 
C.G. Range 
 
Datum Landplane: Main wheel axle. 
Seaplane: Lower forward corner of the front door. 
 
M.A.C. 62.3 in. 
Leveling Means Aircraft  cabin floor level – laterally and longitudinally. 
Maximum Weight Landplane3,500 lbs. 
Seaplane 3,800 lbs. (see Note 5 for specific weight limitation with 
each float installation.) 
 
Minimum crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. at 94 in.

A7EA Page 5 of 17 
 
 
 
 
Fuel Capacity At +21.8 in. Liters Imp. Gals. U.S. Gals.  
 Usable 372 81.9 98.3 
 Unusable 6 1.4 1.7 
 Total 378 83.3 100.0 
 
Oil Capacity 11.4 liters / 10 imperial quarts / 12 U.S. quarts maximum (at -40 in.) 
 
Control Surface 
Movements 
Wing Flaps 
Aileron 
0° 
18° 
up 
up 
30° 
12° 
down 
down 
 Elevator (0° Stab.) 29.5° up 21.5° down 
 Stabilizer 3° up  *** 5° down  ***  
 Rudder 24° left 24° right 
*** UP and DOWN refer to the leading edge of the stabilizer 
Serial Numbers 100 and subsequent. 
Eligible 
 
 
 
IV. MODEL FBA-2C3 (Expedition E350) (Normal Category), Approved December 23, 2008 by the FAA and July 25, 2008 by 
the Canadian Department of Transport (DOT). 
 
This model is the 315 HP tricycle landing gear equipped version of the FBA-2C2. 
Engine Lycoming IO-580-B1A (315 HP) 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
Engine Limits Maximum 2700 r.p.m. for all operations 
Propeller and Hartzell  3-blade variable pitch HC-C3YR-1RF/F8068 
Propeller Limits Diameter:  Maximum 82 ins., Minimum 81 ins. 
Pitch setting at Station 30.0: Low 12.3° 
High 31.0° 
Constant Speed Governor, Hartzell V-5-4 
 
Airspeed Limits Knots 
(CAS) V NE (Never Exceed) 188 
VA (Maneuvering) 117 
VNO (Max. Structural Cruise) 153 
VFE Flaps Extended) 115 
 
C.G. Range Landplane 
Gross Weight Fwd. Limit Aft Limit 
3800 lbs. (1724 kg) +20.5 in. +24.5 in. 
2600 lbs. (1179 kg) +15.0 in. +24.5 in. 
2200 lbs. (997 kg) +15.0 in. +24.5 in. 
Straight line variation between points 
 
Seaplane 
See the Optional Equipment section for specific float installations. 
 
Empty Weight None 
C.G. Range 
 
Datum Landplane: ½” aft of the lower hinge pin on front door. 
Seaplane: Same as above. 
 
Levelling Means Aircraft cabin floor level - laterally and longitudinally.

A7EA Page 6 of 17 
 
 
 
 
Maximum Weight Landplane 3,800 lbs. (1724 kg) 
Seaplane 3,800 lbs. (1724 kg) *** 
*** Gross weight and C of G limits may vary depending on the option installed. 
 
Minimum Crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. (113 kg) at 94 in. 
 
Fuel Capacity At +21.8 in. Litres U.S. Gals. 
Usable 372 98.3 
Unusable 6 1.7 
Total 378 100.0 
Oil Capacity 10.4 litres / 11 U.S. quarts maximum (at -40 in.) 
 
Control Surface Wing Flaps 0° Up 30° Down 
Aileron 18° Up 12° Down 
Elevator (0    Stab.) 33° Up 22° Down 
Stabilizer 3° Up*** 5° Down*** 
Rudder 24° Left 28° Right 
*** Up and Down refer to the leading edge of the stabilizer 
 
Serial Numbers Serial number 300 and subsequent. 
Eligible 
 
 
V. MODEL FBA-2C4 (Normal Category), Approved July 2, 2012, by the FAA and June 5, 2012 by the Canadian Department 
of Transport (DOT). 
 
This model is a tail wheel landing gear version of the FBA-2C3. 
 
Engine Lycoming IO-580-B1A (315 HP) 
 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
 
Engine Limits Maximum 2700 r.p.m. for all operations 
 
Propeller and Hartzell  3-blade variable pitch HC-C3YR-1RF/F8068 
Propeller Limits Diameter:  Maximum 82 ins., Minimum 81 ins. 
Pitch setting at Station 30.0: Low 12.3° 
High 31.0° 
Constant Speed Governor, Hartzell V-5-4 
 
Airspeed Limits Knots 
(CAS) V NE (Never Exceed) 188 
VA (Maneuvering) 117 
VNO (Max. Structural Cruise) 153 
VFE Flaps Extended) 115 
 
C.G. Range Landplane 
Gross Weight Fwd. Limit Aft Limit 
3800 lbs. (1724 kg) +20.5 in. +24.5 in. 
2600 lbs. (1179 kg) +15.0 in. +24.5 in. 
2200 lbs. (997 kg) +15.0 in. +24.5 in. 
Straight line variation between points 
 
Seaplane 
See the Optional Equipment section for specific float installations.

A7EA Page 7 of 17 
 
 
 
 
Empty Weight None 
C.G. Range 
 
Datum Landplane: ½” aft of the lower hinge pin on front door. 
Seaplane: Same as above. 
 
Levelling Means Aircraft cabin floor level – laterally and longitudinally. 
 
Maximum Weight Landplane 3,800 lbs. (1724 kg) 
Seaplane 3,800 lbs. (1724 kg) *** 
*** Gross weight and C of G limits may vary depending on the option installed. 
 
Minimum Crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. (113 kg) at 94 in. 
 
Fuel Capacity At +21.8 in. Litres U.S. Gals. 
Usable 372 98.3 
Unusable 6 1.7 
Total 378 100.0 
Oil Capacity 10.4 litres / 11 U.S. quarts maximum (at -40 in.) 
 
Control Surface Wing Flaps 0° Up 30° Down 
Aileron 18° Up 12° Down 
Elevator (0    Stab.) 33° Up 22° Down 
Stabilizer 3° Up*** 5° Down*** 
Rudder 24° Left 28° Right 
*** Up and Down refer to the leading edge of the stabilizer 
 
Serial Numbers Serial number 4000 and subsequent. 
Eligible 
 
VI MODEL FBA-2C3T (Normal Category), Approved July 2, 2012, by the FAA and June 5, 2012 by the Canadian Department 
of Transport (DOT). 
 
This model is the 300 HP turbocharged engine equipped version of the FBA-2C3. 
 
Engine Lycoming TIO-540-AH1A (300 HP) 
 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
 
Engine Limits Maximum 2500 r.p.m. for all operations 
 
Propeller and Hartzell  3-blade variable pitch HC-C3YR-1RF/F8068+2 
Propeller Limits Diameter:  Maximum 84 ins., Minimum 83 ins. 
Pitch setting at Station 30.0: Low 12.3° 
High 41.5° 
 
Airspeed Limits Knots 
(CAS) V NE (Never Exceed) 188 from S/L to 14,000 ft MSL 
Linearly reducing from 188 @ 14,000 ft 
to 150 @ 25,000 ft. 
VA (Maneuvering) 117 
VNO (Max. Structural Cruise) 153 from S/L to 14,000 ft MSL 
Linearly reducing from 153 @ 14,000 ft 
to 122 @ 25,000 ft.

A7EA Page 8 of 17 
 
VFE (Flaps Extended) 115 
 
C.G. Range Landplane 
Gross Weight Fwd. Limit Aft Limit 
3800 lbs. (1724 kg) +20.5 in. +24.5 in. 
2600 lbs. (1179 kg) +15.0 in. +24.5 in. 
2200 lbs. (997 kg) +15.0 in. +24.5 in. 
Straight line variation between points 
 
Seaplane 
See the Optional Equipment section for specific float installations. 
 
Empty Weight None 
C.G. Range 
 
Datum Landplane: ½” aft of the lower hinge pin on front door. 
Seaplane: Same as above. 
 
Levelling Means Aircraft cabin floor level – laterally and longitudinally. 
 
Maximum Weight Landplane3,800 lbs. (1724 kg) 
Seaplane 3,800 lbs. (1724 kg) *** 
*** Gross weight and C of G limits may vary depending on the option installed. 
 
Minimum Crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. (113 kg) at 94 in. 
 
Fuel Capacity At +21.8 in. Litres U.S. Gals. 
Usable 372 98.3 
Unusable 6 1.7 
Total 378 100.0 
Oil Capacity 10.4 litres / 11 U.S. quarts maximum (at -40 in.) 
 
Control Surface Wing Flaps 0° Up 30° Down 
Aileron 18° Up 12° Down 
Elevator (0    Stab.) 33° Up 22° Down 
Stabilizer 3° Up*** 5° Down*** 
Rudder 24° Left 28° Right 
*** Up and Down refer to the leading edge of the stabilizer 
 
Serial Numbers Serial number 0001 and subsequent. 
Eligible 
 
VII MODEL FBA-2C4T (Normal Category), Approved July 2, 2012, by the FAA and June 5, 2012 by the Canadian Department 
of Transport (DOT). 
 
This model is the 300 HP turbocharged engine equipped version of the FBA-2C4. 
 
Engine Lycoming TIO-540-AH1A (300 HP) 
 
Fuel 100LL or 100 (Formerly 100/130) Grade aviation fuel 
 
Engine Limits Maximum 2500 r.p.m. for all operations 
 
Propeller and Hartzell  3-blade variable pitch HC-C3YR-1RF/F8068+2 
Propeller Limits Diameter:  Maximum 84 ins., Minimum 83 ins.

A7EA Page 9 of 17 
 
 
 
Pitch setting at Station 30.0: Low 12.3° 
High 41.5° 
 
Airspeed Limits Knots 
(CAS) V NE (Never Exceed) 188 from S/L to 14,000 ft MSL 
Linearly reducing from 188 @ 14,000 ft 
to 150 @ 25,000 ft. 
VA (Maneuvering) 117 
VNO (Max. Structural Cruise) 153 from S/L to 14,000 ft MSL 
Linearly reducing from 153 @ 14,000 ft 
to 122 @ 25,000 ft. 
VFE (Flaps Extended) 115 
 
C.G. Range Landplane 
Gross Weight Fwd. Limit Aft Limit 
3800 lbs. (1724 kg) +20.5 in. +24.5 in. 
2600 lbs. (1179 kg) +15.0 in. +24.5 in. 
2200 lbs. (997 kg) +15.0 in. +24.5 in. 
Straight line variation between points 
 
Seaplane 
See the Optional Equipment section for specific float installations. 
 
Empty Weight None 
C.G. Range 
 
Datum Landplane: ½” aft of the lower hinge pin on front door. 
Seaplane: Same as above. 
 
Levelling Means Aircraft cabin floor level – laterally and longitudinally. 
 
Maximum Weight Landplane3,800 lbs. (1724 kg) 
Seaplane 3,800 lbs. (1724 kg) *** 
*** Gross weight and C of G limits may vary depending on the option installed. 
 
Minimum Crew 1 Pilot 
 
Number of Seats 5, including pilot. (2 at +17.8 in., and 3 at +62 in.) 
 
Maximum Baggage 250 lbs. (113 kg) at 94 in. 
 
Fuel Capacity At +21.8 in. Litres U.S. Gals. 
Usable 372 98.3 
Unusable 6 1.7 
Total 378 100.0 
Oil Capacity 10.4 litres / 11 U.S. quarts maximum (at -40 in.) 
 
Control Surface Wing Flaps 0° Up 30° Down 
Aileron 18° Up 12° Down 
Elevator (0    Stab.) 33° Up 22° Down 
Stabilizer 3° Up*** 5° Down*** 
Rudder 24° Left 28° Right 
*** Up and Down refer to the leading edge of the stabilizer 
 
Serial Numbers Serial number 0001 and subsequent. 
Eligible

A7EA Page 10 of 17 
 
 
 
Data Pertinent To All Models (Except As Indicated) 
 
Import Requirements Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new 
and used aircraft based on the scope of the agreement, to identify any required statements by the exporting 
authority on the export certificate of airworthiness (or equivalent document), and for procedures for 
coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, 
Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for 
imported aircraft. 
 
Certification Basis FBA-2C 
CAR 3 dated May 15, 1956 and Amendments 3-1 to 3-7 inclusive. Type Certificate No. A7EA issued June 
23, 1965.  Date of Application for Type Certificate February 11, 1963. 
 
FBA-2C1 
Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 23-6 
except as follows: 
FAR 23.51; 23.65; 23.75; 23.77; 23.611; 23.619; 23.623; 23.683; 23.689; 23.775; 23.871; 23.954; 
23.1147; 23.1323; and 23.1563 amended by amendment 23-7. 
FAR 23.1524 amended by amendment 23-10. 
FAR 23.771 and 23.1365 amended by amendment 23-14. 
FAR 23.607; 23.675; 23.685; 23.733; and 23.1309 amended by amendment 23-17. 
FAR 23.959 amended by amendment 23-18. 
FAR 23.1301 amended by amendment 23-20. 
FAR 23.1353; 23.1541; and 23.1559 amended by amendment 23-21. 
FAR 23.603; 23.605; 23.863; and 23.1545 amended by amendment 23-23. 
FAR 23.1529 amended by amendment 23-26. 
FAR 23.995; 23.1143; 23.777; 23.779; and 23.781 amended by amendment 23-29. 
FAR 23.1; 23.853; and 23.1165; amended by amendment 23-34. 
FAR 23.787 amended by amendment 23-36. 
FAR 23.1311 and 23.1321 amended by amendment 23-41. 
FAR 23.301; 23.331; 23.351; 23.421; 23.423; 23.425; 23.427; 23.441; 23.443; 23.677; 23.701; 23.735 and 
23.831 amended by amendment 23-42. 
FAR 23.901; 23.903; 23.905; 23.925; 23.951; 23.953; 23.955; 23.957; 23.963; 23.965; 23.967; 23.971; 
23.973; 23.975; 23.977; 23.991; 23.993; 23.997; 23.999; 23.1093; 23.1145; 23.1303; 23.1322; 23.1337; 
23.1351; 23.1357; 23.1361; and 23.1385 amended by amendment 23-43. 
FAR 23.562(a) and 23.562(e) amended by amendment 23-44. 
FAR 23.33; 23.305; 23.321; 23.397; 23.561; 23.572; 23.613; 23.621; 23.655; 23.731; and 23.1549 
amended by amendment 23-45. 
FAR 23.783; 23.805; 23.807 and 23.811 amended by amendment 23-46. 
 
FAR 36 dated December 1,1969, as amended by Amendment 36-1 through 36-22. 
 
 
FBA-2C2 
The Certification Basis for the model FBA-2C1, except as follows: 
FAR 23.49; 23.141; and 23.867 amended by amendment 23-7. 
FAR 23.1397; 23.1401 amended by amendment 23-11. 
FAR 23.345; 23.723 amended by amendment 23-23. 
FAR 23.2 amended by amendment 23-36. 
FAR 23.1305; 23.1307; 23.1365; 23.1387; 23.1389; 23.1391; 23.1393; 23.1395, and 23.1431 
amended by amendment 23-43. 
FAR 23.25; 23.207; and 23.473 amended by amendment 23-45. 
 
FAR 36 dated December 1,1969, as amended by Amendment 36-1 through 36-22. 
 
 
FBA-2C3 
Part 23 of the U. S. Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 
23-6 except as follows: 
As amended by Amendment 23-7 
23.141, 23.395, 23.505, 23.619, 23.623, 23.625, 23.683, 23.689, 23.726, 23.727, 23.871, 23.954, 23.1147 
23.1505

A7EA Page 11 of 17 
 
 
 
As amended by Amendment 23-10 
23.1524 
As amended by Amendment 23-11 
23.1397, 23.1401 
As amended by Amendment 23-14 
23.507, 23.509, 23.771, 23.1017, 23.1182 
As amended by Amendment 23-17 
23.675, 23.685, 23.1125 
As amended by Amendment 23-20 
23.1301, 23.1327, 23.1547 
As amended by Amendment 23-21 
23.29, 23.1501, 23.1541 
As amended by Amendment 23-23 
23.603, 23.605 
As amended by Amendment 23-26 
23.1529 
As amended by Amendment 23-29 
23.995, 23.1143 
As amended by Amendment 23-33 
23.781 
As amended by Amendment 23-34 
23.1, 23.333, 23.863, 23.1165, 23.1523 
As amended by Amendment 23-36 
23.2 
As amended by Amendment 23-42 
23.331, 23.351, 23.421, 23.423, 23.425, 23.427, 23.445, 23.831 
As amended by Amendment 23-43 
23.905, 23.943 23.951, 23.957,  23.961, 23.967, 23.971, 23.977, 23.991, 23.993, 23.997, 23.999, 23.1011, 
23.1103, 23.1123,  23.1145, 23.1193, 23.1303, 23.1307, 23.1322, 23.1331, 23.1357, 23.1385, 23.1387, 
23.1389, 23.1391, 23.1393, 23.1395, 23.1431 
As amended by Amendment 23-44 
23.562(a), 23.562(e) 
As amended by Amendment 23-45 
23.23, 23.305, 23.321, 23.361, 23.397, 23.485, 23.523, 23.525, 23.527, 23.529, 23.531, 23.613, 23.621, 
23.655, 23.731, 23.733, 23.737, 23.751, 23.753, 23.773, 23.851, 23.1507, 23.1525, 23.1527, 23.1549, 
23.1557 
As amended by Amendment 23-46 
23.805, 23.811 
As amended by Amendment 23-48 
23.301, 23.335, 23.337, 23.341, 23.343, 23.345, 23.347, 23.349, 23.371, 23.391, 23.393, 23.399, 23.441, 
23.443, 23.455, 23.473, 23.499, 23.521, 23.561, 23.572, 23.573, 23.607, 23.611, 23.657, 23.673, 23.725, 
23.865 
As amended by Amendment 23-49 
23.677, 23.701, 23.723, 23.729, 23.735, 23.745,  23.775, 23.783, 23.785, 23.787, 23.807, 23.853, 23.855, 
23.867, 23.1309, 23.1311, 23.1321, 23.1323, 23.1351, 23.1353, 23.1359, 23.1361, 23.1365, 23.1383 
As amended by Amendment 23-50 
23.3, 23.25, 23.33, 23.45, 23.49, 23.51, 23.53, 23.63, 23.65, 23.69, 23.71, 23.73, 23.75, 23.77, 23.201, 
23.203, 23.207, 23.237, 23.1325, 23.1511, 23.1521, 23.1543, 23.1545, 23.1553, 23.1555, 23.1559, 
23.1563, 23.1567, 23.1581, 23.1583, 23.1585, 23.1587, 23.1589 
As amended by Amendment 23-51 
23.777, 23.779, 23.907, 23.925, 23.955, 23.959, 23.963, 23.965, 23.973, 23.975, 23.1041, 23.1043, 
23.1047, 23.1091, 23.1093, 23.1105, 23.1107, 23.1121, 23.1181, 23.1183, 23.1191, 23.1337 
As amended by Amendment 23-52 
23.1305 
As amended by Amendment 23-53 
23.901 
As amended by Amendment 23-54 
23.903 
 
Airworthiness Manual Chapter 516, Change 516-06, Volume I, Aircraft Noise, effective 23 November 
1999.

A7EA Page 12 of 17 
 
 
 
 
For aircraft equipped with a Garmin G500, G500TXi or G600 avionics system (which includes a 
Garmin 430W, 530W, 6XX or 7XX Navigator), the additional certification basis, for installation 
specific items only, is amended to include the following regulations at the amendment level stated: 
23.1303 as amended by Amendment 23-49 
23.1307 as amended by Amendment 23-49 
23.1308 as amended by Amendment 23-57 
23.1431 as amended by Amendment 23-49 
 
For aircraft equipped with an S-Tec autopilot system, the additional certification basis, for installation 
specific items only, is amended to include the following regulations at the amendment level stated: 
23.1329 as amended by Amendment 23-49 
23.1335 as amended by Amendment 23-20 
 
FBA-2C4 
The Certification Basis for the model FBA-2C3 with the addition of the following requirement: 
23.497 Supplementary conditions for tail wheels (Amdt. 23-48) 
 
FBA-2C3T 
The Certification Basis for the model FBA-2C3 with the addition of the following requirements: 
23-909 Turbocharger systems (Amdt 23-43) 
23.939 Powerplant operating characteristics (Amdt 23-42) 
23.1441 Oxygen equipment and supply (Amdt 23-43) 
23.1443 Minimum mass flow of supplemental oxygen (Amdt. 23-62) 
23.1445 Oxygen distribution system (Amdt. 23-62) 
23.1447 Equipment standards for oxygen dispensing units (Amdt. 23-62) 
23.1449 Means for determining use of oxygen (Amdt. 23-9) 
23.1451 Fire protection for oxygen equipment (Amdt. 23-49) 
23.1453 Protection of oxygen equipment from rupture (Amdt. 23-49) 
 
FBA-2C4T 
The Certification Basis for the model FBA-2C3 with the addition of the following requirements: 
23.497 Supplementary conditions for tail wheels (Amdt. 23-48) 
23-909 Turbocharger systems (Amdt 23-43) 
23.939 Powerplant operating characteristics (Amdt 23-42) 
23.1441 Oxygen equipment and supply (Amdt 23-43) 
23.1443 Minimum mass flow of supplemental oxygen (Amdt. 23-62) 
23.1445 Oxygen distribution system (Amdt. 23-62) 
23.1447 Equipment standards for oxygen dispensing units (Amdt. 23-62) 
23.1449 Means for determining use of oxygen (Amdt. 23-9 
23.1451 Fire protection for oxygen equipment (Amdt. 23-49) 
23.1453 Protection of oxygen equipment from rupture (Amdt. 23-49) 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification 
Basis) must be installed in the aircraft for certification. 
 
FBA-2C 
In addition, the following items of equipment are required: 
Landplane, Skiplane and Seaplane: 
(a) D.O.T. Approved Flight Manual dated February 25, 1964. 
(b) Stall Warning Indicator per Found Brothers Drawing No. W-535. 
 
FBA-2C1 
In addition, the following items of equipment are required: 
With 260 HP engine: 
Transport Canada Approved Flight Manual FAC2-M100 dated May 20, 2000, or later approved revision. 
With 300 HP engine:

A7EA Page 13 of 17 
 
 
 
Transport Canada Approved Flight Manual FAC2-M300 dated May 20, 2000, or later approved revision 
 
FBA-2C2 
In addition, the following items of equipment are required: 
Transport Canada Approved Flight Manual FAC2-M400, dated December 9, 2003, or later approved 
revision.. 
 
FBA-2C3 
In addition, the following items of equipment are required: 
Transport Canada Approved Flight Manual P/N FM2C3 dated July 25, 2008, or later approved revision. 
 
FBA-2C4 
In addition, the following items of equipment are required: 
Transport Canada Approved Flight Manual P/N FM2C4 dated December 31, 2011, or later approved 
revision. 
 
FBA-2C3T 
In addition, the following items of equipment are required: 
Transport Canada Approved Flight Manual P/N FM2C3T dated February 20, 2012, or later approved 
revision. 
 
FBA-2C4T 
In addition, the following items of equipment are required: 
Transport Canada Approved Flight Manual P/N FM2C4T dated February 20, 2012, or later approved 
revision. 
 
Service Information The Airworthiness Limitations Section of the Maintenance Program (P/N FAC2-M200) and AFMs which 
contain a statement that the document is approved by the Transport Canada, are accepted by the FAA and 
are considered FAA approved. (These approvals pertain to the design data only).” 
 
NOTE 1. (a) Current weight and balance report including list of equipment included in the certificated empty 
weight, and loading instructions when necessary, must be in each aircraft at the time of original 
certification and at all times thereafter. 
 
(b) The certificated empty weight and corresponding center of gravity locations must include 
unusable fuel. 
FBA-2C 7.5 lbs. (+22.2 in.) and unusable oil of 2.8 lb. (-38.8 in.). 
FBA-2C1 Bush Hawk   10.2 lbs. (+21.8 in) 
FBA-2C2 Bush Hawk XP 10.2 lbs. (+21.8 in) 
FBA-2C3 Expedition E350 10.2 lbs. (+21.8 in) 
FBA-2C4 10.2 lbs. (+21.8 in) 
FBA-2C3T 10.2 lbs. (+21.8 in) 
FBA-2C4T 10.2 lbs. (+21.8 in) 
 
NOTE 2. The following placards must be displayed in clear view of the pilot: 
 
FBA-2C 
 
(a) "THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN 
COMPLIANCE WITH THE OPERATING LIMITATIONS IN THE FORM OF PLACARDS, 
MARKINGS AND MANUALS". 
 
(b) "NO ACROBATIC MANEUVERS INCLUDING SPINS APPROVED". 
 
FBA-2C1, FBA-2C2, FBA-2C3, FBA-2C4, FBA-2C3T, and FBA-2C4T 
 
(a) “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.”

A7EA Page 14 of 17 
 
 
 
 
(b) Normal Category: “No acrobatic maneuvers including spins approved.” 
(c) “Flight into known icing conditions is prohibited. This airplane is certified for the following 
flight operations: 
 
DAY-NIGHT-VFR-IFR 
(WITH REQUIRED EQUIPMENT)” 
 
NOTE 3. FBA-2C1, FBA-2C2, FBA-2C3, FBA-2C4, FBA-2C3T, and FBA-2C4T 
Transport Canada approved Airworthiness Limitations are included in Section 4 of the Maintenance 
Program P/N FAC2-M200. 
 
NOTE 4. Ski Installations: 
 
FBA-2C 
 
(a) Federal Model CF3000; installed in accordance with Found Brothers Drawing No. 2C36-1 
Issue 2C. 
 
FBA-2C1 
(a) Wipaire/Fluidyne/Federal C3200 skis. Maximum gross weight allowable 3200 lbs. Installation 
and operation in accordance with the latest Transport Canada approved revisions of Master 
Drawing List, Document No. MDL-1101 and Flight Manual Supplement, P/N M300-S04 or other 
Transport Canada approved data. 
(b) Wipaire/Fluidyne/Federal C3600 skis. Maximum gross weight allowable 3200 lbs. Installation 
and operation in accordance with the latest Transport Canada approved revisions of Master 
Drawign List, Document No. MDL-1102 and Flight Manual Supplement, P/N M300-S04 or other 
Transport Canada approved data. 
 
FBA-2C2 
 
(a) Wipaire/Fluidyne/Federal C3200 skis. Maximum gross weight allowable 3200 lbs. Installation 
and operation in accordance with the latest Transport Canada approved revisions of Master 
Drawing List, Document No. MDL-1101 and Flight Manual Supplement, P/N M400-S05 or other 
Transport Canada approved data. 
(b) Wipaire/Fluidyne/Federal C3600 skis. Maximum gross weight allowable 3500 lbs. Installation 
and operation in accordance with the latest Transport Canada approved revisions of Master 
Drawing List, Document No. MDL-1102 and Flight Manual Supplement, P/N M400-S06 or other 
Transport Canada approved data. 
 
FBA-2C3, FBA-2C4, FBA-2C3T, and FBA-2C4T 
 
Ski Installation  (Reserved) 
 
NOTE 5. Float Installations: 
 
FBA-2C 
 
(a) EDO Model 249A-2870; installed in accordance with Found Brothers Drawing No. 2C37-1 
Issue2A. 
 
FBA-2C1 
 
(a) EDO Model 628-2960 floats , or Model 249A-2870 (modified per EDO drawing X-43521) 
floats, with 260 HP engine. Float installation in accordance with Found Aircraft Canada Inc. 
drawing No. D210 Issue 1. Maximum gross weight allowable 3200 lbs. 
(b) Aerocet Model 3500 floats with 260 HP engine. 
Float installation in accordance with Found Aircraft Canada Inc. drawing No. D211 Issue 1. 
Maximum gross weight allowable 3350 lbs. 
(c) Aerocet Model 3500L floats with 260 HP engine.

A7EA Page 15 of 17 
 
 
 
Float installation in accordance with Found Aircraft Canada Inc. drawing No. D211 Issue 1. 
Maximum gross weight allowable 3350 lbs. 
(d) Aerocet Model 3500 floats with 300 HP engine. 
Float installation in accordance with Found Aircraft Canada Inc. drawing No. D212 Issue 1. 
Maximum gross weight allowable 3500 lbs. 
(e) Aerocet Model 3500L floats with 300 HP engine. 
Float installation in accordance with Found Aircraft Canada Inc. drawing No. D212 Issue 1. 
Maximum gross weight allowable 3500 lbs. 
 
FBA-2C2 
 
a) Aerocet Model 3500 floats. Float installation and operation in accordance with Master Drawing 
List, Document No. MDL-1119 and Flight Manual Supplement M400-S02, both Transport 
Canada Approved December 19, 2003, or later approved revisions. Maximum gross weight 
allowable 3600 lbs. 
b) Aerocet Model 3500L floats. Float installation and operation in accordance with Master 
Drawing List, Document No. MDL-1119 and Flight Manual Supplement M400-S01, both 
Transport Canada Approved December 19, 2003, or later approved revisions. Maximum gross 
weight allowable 3800 lbs. 
c) Aerocet Model 3400 amphibious floats. Float installation and operation in accordance with 
Master Drawing List, Document No. MDL-1150 and Flight Manual Supplement M400-S10, both 
Transport Canada Approved December 19, 2003, or later approved revisions. Maximum gross 
weight allowable 3775 lbs. 
 
d) Wipaire 3450 amphibious floats. Float installation and operation in accordance with Master 
Drawing List, Document No. MDL-1118 and Flight Manual Supplement M400-S09, both 
Transport Canada Approved April 15, 2004, or later approved revisions. Maximum gross weight 
allowable 3700 lbs. 
e) Wipaire 3450 seaplane floats.  Float installation and operation in accordance with Master 
Drawing List, Document No. MDL-1182 and Flight Manual Supplement M400-S08, both 
Transport Canada Approved April 15, 2004, or later approved revisions. Maximum gross weight 
allowable 3700 lbs. 
 
FBA-2C3 and FBA-2C4  
 
(a) Aerocet Model 3500L and 3500 floats 
Maximum  gross weight allowable 3800 lbs. (1724 kg) 
Installation and operation in accordance with the latest DOT approved revisions of Master 
Drawing List, Document No. MDL-1273 and Flight Manual Supplement, P/N S02 or other DOT 
approved data. 
(b) Aerocet Model 3400 amphibious floats 
Maximum  gross weight allowable 3775 lbs. (1712 kg) 
Installation and operation in accordance with the latest DOT approved revisions of Master 
Drawing List, Document No. MDL-1272 and Flight Manual Supplement, P/N S01 or other DOT 
approved data. 
 
FBA-2C3T and FBA-2C4T 
 
Float Installation  (Reserved) 
 
NOTE 6. Oversize Tire Installations: 
 
FBA-2C1 
 
(a) GAR-AERO oversize wheels and tires, plus oversize tail wheel, with 260 HP or 300 HP engine. 
Wheel and tire installation in accordance with the following Found Aircraft Canada Inc. 
drawings: 
No. D205 Issue 1 with 260 HP engine. 
No. D206 Issue 1 with 300 HP engine.

A7EA Page 16 of 17 
 
 
 
FBA-2C2 
 
(a) GAR-Aero Wheel Adapters and 8.5-10 Tires.  Installation and operation in accordance with 
Master Drawing List, Document No. MDL-1117 and Flight Manual Supplement M400-S03, both 
Transport Canada Approved  April 15, 2004, or later approved revisions.  Maximum gross 
weight allowable 3500 lbs. 
 
FBA-2C4 
 
(a) Alaskan Bushwheel Tires, 26” (P/N 26126) and 29” (P/N 29136) 
Maximum  gross weight allowable 3800 lbs. (1724 kg) 
Installation and operation in accordance with the latest DOT approved revisions of Master 
Drawing List, Document No. MDL-2C4 and Flight Manual P/N FM2C4 or other DOT approved 
data. 
 
(b) Alaskan Bushwheel 10” Wheels (P/N ABI-1010) with 8.50-10 or 29x11-10 Tires 
Maximum  gross weight allowable 3800 lbs. (1724 kg) 
Installation and operation in accordance with the latest DOT approved revisions of Master 
Drawing List, Document No. MDL-2C4 and Flight Manual P/N FM2C4 or other DOT approved 
data. 
 
NOTE 7.  
FBA-2C 
 
Position and Instrument Lights per Found Brothers Modification No. 118. 
 
NOTE 8.  
Model FBA-2C1 aircraft modified per found Aircraft modification FAC2 1043 are structurally and 
functionally equivalent to the FBA-2C2 and may be equipped and operated with the optional equipments of 
the FBA-2C2 model. In addition, these aircraft must be operated in accordance with Found Aircraft Flight 
Manual FAC2-M400. 
 
NOTE 9. 
FBA-2C 
 
Serial Nos. 3,5 and up, eligible for 3,000lb. Gross weight modification on seaplane per Found Brothers 
Modification No. 117, and the following are applicable: 
 
Airspeed limits Vne (never exceed) 153 m.p.h.  
(CAS) Vno (max. structural cruising) 122 m.p.h.  
 VA (maneuvering) 133 m.p.h.  
 Vfe (flaps extended) 111 m.p.h. 
 
C.G. Range Fwd. Limit 15.3 in. aft of datum at all weights 
Aft limit 23.6 in aft of datum all weights 
 
Maximum Weight 3,000 lbs. 
 
Control surface 
movements 
 
Wing Flaps 
 
0° 
 
up 
 
32° 
 
down 
 Aileron 18° up 12° down  
 Elevator (0° Stab.) 29.5° up 21.5° down  
 Stabilizer 4.5° up 3.5° down  
 Rudder 30° left 30° right 
 
Equipment  In addition to the pertinent basic equipment specified in the applicable airworthiness 
regulations (CAR 3),  the following items of equipment must be installed: 
 
(a) Hartzell Constant Speed HC-927K-1D/8847-0 70 lb. (-63.0 in.) 
Diameter:  maximum 88 in. minimum 88 in.

A7EA Page 17 of 17 
 
 
 
Pitch setting at Station 30.0 in.:  low 12°, high 26.4° 
 
Woodward Constant Speed Governor B210340 
 
(b) D.O.T. approved Flight Manual dated April 28, 1965 
(c) Stall warning indicator per Found Brothers Drawing No. W-535. 
 
…..END…..
```

## ADs (4, in force first)

- [AD 2022-22-05](https://openairdocs.org/ad/2022-22-05): Aileron Control System · NZSkydive FBA-2C1, FBA-2C2, FBA-2C3 and 1 more. Effective Nov 9, 2022
- [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 2019-02-02](https://openairdocs.org/ad/2019-02-02): Flight controls · Pacific Aerospace FBA-2C1, FBA-2C2, FBA-2C3 and 1 more. Effective Feb 27, 2019
- [AD 68-01-04](https://openairdocs.org/ad/68-01-04): Forward Wing-to-Fuselage Attachment · Found Aircraft Canada FBA-2C. Effective Jan 9, 1968

## Registered aircraft by registry model (OpenAirDocs)

- [Found Acft Canada FBA-2C1](https://openairdocs.org/model/found-acft-canada-fba-2c1): 15 aircraft (registry code 3640103)
- [Found Aircraft Canada FBA-2C3](https://openairdocs.org/model/found-aircraft-canada-fba-2c3): 11 aircraft (registry code 3640105)
- [Found Acft Canada FBA-2C2](https://openairdocs.org/model/found-acft-canada-fba-2c2): 4 aircraft (registry code 3640104)
- [Pacific Aerospace FBA-2C3](https://openairdocs.org/model/pacific-aerospace-fba-2c3): 2 aircraft (registry code 3640110)
- [Found Aircraft Canada FBA-2C4](https://openairdocs.org/model/found-aircraft-canada-fba-2c4): 1 aircraft (registry code 3640106)
- [Nzskydive FBA-2C3](https://openairdocs.org/model/nzskydive-fba-2c3): 1 aircraft (registry code 3500712)
- [Found FBA-2C](https://openairdocs.org/model/found-fba-2c): 0 aircraft (registry code 3640102)

## STCs approved under this data sheet (92, 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 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 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 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 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 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 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 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 SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc.
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [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 SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. 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 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): 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 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 SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks  Starting Vibrator Booster Systems. Continental Motors, 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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [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 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 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

All 92: https://openairdocs.org/tcds/A7EA/stcs.md

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