# TCDS A11EA: True Flight Holdings LLC

- Type: Type certificate data sheet
- Status: Current
- Holder: True Flight Holdings LLC
- Revision: 13
- Revised: December 12, 2013
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Registered aircraft: 720, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/36/71/3671aa9bb1e25fbc7efd5e5f08a93e1647fc830fd3ef94479c11f855d4f5078c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A6E45C3465F16FE386257C3F00671C44.0001
- Page: https://openairdocs.org/tcds/A11EA

## Models (4)

As the data sheet lists them.

- AA-1C
- AA-1A
- AA-1
- AA-1B

## 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 
Rev. No. 13 5 6 5 6 10 8 10 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A11EA 
Revision 13 
 
True Flight Holdings LLC 
(American General) 
AA-1 
AA-1A 
AA-1B 
AA-1C 
 
December 12, 2013 
 
TYPE CERTIFICATE DATA SHEET NO. A11EA 
 
This data sheet, which is a part of Type Certificate No. A11EA, prescribes conditions and limitations under which the product 
for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.  
 
Type Certificate Holder True Flight Holdings LLC 
 2300 Madison Highway 
 Valdosta, GA  31601 
 
Type Certificate Holder Record: American Aviation Corporation transferred TC A11EA to  
 Grumman American Aviation Corporation on February 27, 1973 
 
 Grumman American Aviation Corporation transferred TC A11EA to  
 Gulfstream American Corporation on September 1, 1978 
 
 Gulfstream American Corporation transferred TC A11EA to 
 Gulfstream Aerospace Corporation on November 15, 1982 
 
 Gulfstream Aerospace Corporation transferred TC A11EA to 
 American General Aircraft Corporation on October 29, 1992 
 
 American General Aircraft Corporation transferred TC A11EA to 
 American General Aircraft Holding Company, Inc. on August 23, 1993 
 
 American General Aircraft Holding Corporation, Inc. transferred TC A11EA to 
 Tiger Aircraft LLC on March 22, 2000 
 
 Tiger Aircraft LLC transferred TC A11EA to  
 True Flight Holdings LLC on August 31, 2007 
 
I. - Model AA-1, Yankee, 2 PCLM, Utility Category, Approved August 29, 1967, Normal Category Approved July 16, 1968.  
 
 Engine Lycoming O-235-C2C (Carburetor Setting 10-4953 or 10-3103-1) 
 
 Fuel 80/87 minimum grade aviation gasoline 
 
 Engine limits For all operations 2600 r.p.m. (108 h.p.) 
 
 Propeller and propeller limits 1. McCauley Model 1A105/SCM-7157 fixed pitch propeller.  Static r.p.m. at 
maximum permissible throttle setting; not over 2300; not under 2150.  Diameters:  
not over 71 inches, not under 69.5 inches.

A11EA Page 2 
  2. McCauley Model 1A105/SCM-7153 and 1A105/SCM-7154 fixed pitch propellers.  
Static r.p.m. at maximum permissible throttle setting; not over 2400; not under 
2250.  Diameter:  not over 71 inches, not under 69.5 inches. 
 
  3. McCauley Model 1A106/NCM-7157 fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2400; not under 2300.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
  4. McCauley Model 1A106/NCM-7153 hub and fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2475; not under 2375.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
 Airspeed limits (CAS) Vne  Never exceed   195 m.p.h. (169 knots) 
  Vno  Maximum structural cruising 144 m.p.h. (125 knots) 
  Va   Maneuvering (Utility Category) 132 m.p.h. (115 knots) 
  Va   Maneuvering (Normal Category) 125 m.p.h. (109 knots) 
  Vfe  Flaps extended 100 m.p.h. (  87 knots) 
    Canopy half open 130 m.p.h. (113 knots) 
 
 Center of gravity (C.G) range (+78.5) to (+81.0) at 1500 lb. 
  (+77.5) to (+81.0) at 1430 lb. 
  (+75.0) to (+81.0) at 1245 lb. 
  Straight line variation between points given. 
 
  
Gross
Weight
lb.
1500
1430
1245
Fuselage Station inches
75.0 77.5 78.5 81.0
Normal
Utility
 
 
 Empty weight C.G. range None 
 
 Maximum weight 1430 lb. (Utility Category) 
  1500 lb. (Normal Category) 
 
 Number of seats 2 at (+92.5) (For optional child's seat refer to Equipment List.) 
 
 Maximum baggage 100 lb. at (+120) 
 
 Fuel capacity 24 gal. (2 wing tanks) at (+84.5) (See Note 1 for unusable fuel) 
 
 Oil capacity 6 qt. at (+39) (2 qt. minimum) 
 
 Control surface movements Elevator 25° ± 2° up 15° ± 2° down 
  Rudder  25° ± 2° left 25° ± 2°  right 
  Ailerons 25° ± 2° up 20° ± 2°  down 
  Flaps    30° ± 2°  down 
  Elevator tab trim 21.5° ± 2° up 11° ± 2°  down 
 
 Serial numbers eligible AA1-0001 and up (Normal and Utility Category)

Page 3 A11EA 
 
II - Model AA-1A, Trainer, 2 PCLM, Utility Category, Approved January 14, 1971, Normal Category Approved January 14, 1971.  
 
 Engine Lycoming O-235-C2C (Carburetor Setting 10-4953 or 10-3103-1) 
 
 Fuel 80/87 minimum grade aviation gasoline 
 
 Engine limits For all operations 2600 r.p.m. (108 h.p.) 
 
 Propeller and propeller limits 1. McCauley Model 1A105/SCM-7157 fixed pitch propeller.  Static r.p.m. at 
maximum permissible throttle setting; not over 2300; not under 215C.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
  2. McCauley Model 1A105/SCM-7153 and 1A105/SCM-7154 fixed pitch propellers.  
Static r.p.m. at maximum permissible throttle setting; not over 2400; not under 
2250.  Diameter:  not over 71 inches, not under 69.5 inches. 
 
  3. McCauley Model 1A106/NCM-7157 fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2400; not under 2300.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
  4. McCauley Model 1A106/NCM-7153 hub and fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2475; not under 2375.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
 Airspeed limits (CAS) Vne Never exceed 195 m.p.h. (169 knots) 
  Vno  Maximum structural cruising 144 m.p.h. (125 knots) 
  Va   Maneuvering (Utility Category) 127 m.p.h. (110 knots) 
  Va   Maneuvering (Normal Category) 120 m.p.h. (104 knots) 
  Vfe  Flaps extended 115 m.p.h. (100 knots) 
    Canopy half open 130 m.p.h. (113 knots) 
 
 Center of gravity (C.G) range (+78.5) to (+80.0) at 1500 lb. 
  (+77.5) to (+80.0) at 1430 lb. 
  (+75.0) to (+80.0) at 1245 lb. 
  Straight line variation between points given. 
 
  
Gross
Weight
lb.
1500
1430
1245
Fuselage Station inches
75.0 77.5 78.5 80.0
Normal
Utility
 
 Empty weight C.G. range None 
 
 Maximum weight 1430 lb. (Utility Category) 
  1500 lb. (Normal Category) 
 
 Number of seats 2 at (+92.5) (For optional child's seat refer to Equipment List.) 
 
 Maximum baggage 100 lb. at (+120) 
 
 Fuel capacity 24 gal. (2 wing tanks) at (+84.5) (See Note 1 for unusable fuel)

A11EA Page 4 
 Oil capacity 6 qt. at (+39) (2 qt. minimum) 
 
 Control surface movements Elevator 25° ± 2° up 15° ± 2°  down 
  Rudder  25° ± 2° left 25° ± 2°  right 
  Ailerons 25° ± 2° up 20° ± 2°  down 
  Flaps    30° ± 2°  down 
  Elevator tab trim 14.5° ± 2° up 18° ± 2°  down 
 
 Serial numbers eligible AA1A-0001 and up (Normal and Utility Category) 
 
III - Model AA-1B, Trainer/TR-2, 2 PCLM, Utility Category, Approved June 30, 1972 
 
 Engine Lycoming O-235-C2C (Carburetor Setting 10-4953 or 10-3103-1) 
 
 Fuel 80/87 minimum grade aviation gasoline 
 
 Engine limits For all operations 2600 r.p.m. (108 h.p.) 
 
 Propeller and propeller limits 1. McCauley Model 1A105 with 1A105/SCM hub and 7157 blades.  Static r.p.m. at 
maximum permissible throttle setting; not over 2300; not under 2150.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
  2. McCauley Model 1A105/SCM-7153 and 1A105/SCM-7154 fixed pitch propellers.  
Static r.p.m. at maximum permissible throttle setting; not over 2400; not under 
2250.  Diameter:  not over 71 inches, not under 69.5 inches. 
 
  3. McCauley Model 1A106/NCM-7153 fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2400; not under 2300.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
  4. McCauley Model 1A106/NCM-7157 fixed pitch propellers.  Static r.p.m. at 
maximum permissible throttle setting; not over 2475; not under 2375.  Diameter:  
not over 71 inches, not under 69.5 inches. 
 
 Airspeed limits (CAS) Vne  Never exceed 195 m.p.h. (169 knots) 
  Vno  Maximum structural cruising 144 m.p.h. (125 knots) 
  Va   Maneuvering  135 m.p.h. (117 knots) 
  Vfe  Flaps extended 115 m.p.h. (100 knots) 
    Canopy half open 130 m.p.h. (113 knots) 
 
 Center of gravity (C.G) range (+78.25) to (+80.0) at 1560 lb. 
  (+75.0) to (+80.0) at 1300 lb. 
  
Gross
Weight
lb.
1560
1300
Fuselage Station inches
75.0 78.25 80.0
 
 
 Empty weight C.G. range None 
 
 Maximum weight 1560 lb.

Page 5 A11EA 
 Number of seats 2 at (+92.5) (For optional child's seat refer to Equipment List.) 
 
 Maximum baggage 100 lb. at (+120) 
 
 Fuel capacity 24 gal. (2 wing tanks) at (+84.5) (See Note 1 for unusable fuel) 
 
 Oil capacity 6 qt. at (+39) (2 qt. minimum) 
 
 Control surface movements Elevator 25° ± 2° up 15° ± 2°  down 
  Rudder  25° ± 2° left 25° ± 2°  right 
  Ailerons 25° ± 2° up 20° ± 2°  down 
  Flaps    30° ± 2°  down 
  Elevator tab trim 14.5° ± 2° up 18° ± 2°  down 
 
 Serial numbers eligible AA1B-0001 and up (Utility Category) 
 
 
IV - Model AA-1C, T-Cat/Lynx, 2 PCLM, Utility Category, Approved December 21, 1976.  (Same as AA-1B except for engine, 
 propeller, engine mount/baffles, and AA-5 elevator). 
 
 Engine Lycoming O-235-L2C (Carburetor Setting 10-4953 or 10-3103-1) 
 
 Fuel 100/130 minimum grade aviation gasoline 
 
 Engine limits For all operations 2700 r.p.m. (115 h.p.) 
 
 Propeller and propeller limits 1. Sensenich Model 72CK-0-56 fixed pitch propeller.  Static r.p.m. at maximum 
permissible throttle setting; not over 2275; not under 2125.  No additional tolerance 
permitted.  Diameter:  not over 72 inches, not under 70.5 inches. 
 
  2. Sensenich Model 72CK-0-52 fixed pitch propellers.  Static r.p.m. at maximum 
permissible throttle setting; not over 2475; not under 2325.  No additional tolerance 
permitted.  Diameter:  not over 72 inches, not under 70.5 inches. 
 
 Airspeed limits (CAS) Vne  Never exceed 195 m.p.h. (169 knots) 
  Vno  Maximum structural cruising 144 m.p.h. (125 knots) 
  Va   Maneuvering  135 m.p.h. (117 knots) 
  Vfe   Flaps extended 115 m.p.h. (100 knots) 
    Canopy half open 130 m.p.h. (113 knots) 
 
 Center of gravity (C.G) range (+78.00) to (+81.0) at 1600 lb. 
  (+75.5) to (+81.0) at 1385 lb. 
  
Gross
Weight
lb.
1600
1385
Fuselage Station inches
75.50 78.00 81.00
Utility
 
 Empty weight C.G. range None 
 
 Maximum weight 1600 lb.

A11EA Page 6 
 Number of seats 2 at (+92.5) (For optional child's seat refer to Equipment List.) 
 
 Maximum baggage 100 lb. at (+120) 
 
 Fuel capacity 24 gal. (2 wing tanks) at (+84.5) (See Note 1 for unusable fuel) 
 
 Oil capacity 6 qt. at (+39) (2 qt. minimum) 
 
 Control surface movements Elevator 12° ± 1° up 28° ± 2°  down 
  Rudder  25° ± 2° left 25° ± 2°  right 
  Ailerons 25° ± 2° up 20° ± 2°  down 
  Flaps    30° ± 2°  down 
  Elevator tab trim 15° ± 4° up 15° ± 2°  down 
 
 Serial numbers eligible AA1B-0601 and AA1C-0001 and up (Utility Category) 
 
 
DATA PERTINENT TO ALL MODELS: 
 Datum 50.0 inches forward of front face of firewall (wing chord 48 inches for Model AA-1 and 
49.32 inches for Models AA-1A, AA-1B, and AA-1C).  
 Leveling means  Top of  fuselage canopy slide rail. 
 
 Certification basis FAR 23 effective February 1, 1965, and amendments 23-1 and 23-2; and FAR 36 
amended through 36-4 for the Model AA-1C. 
 
  Type Certificate No. A11EA issued August 29, 1967.  Data of Application for Type 
Certificate October 22, 1965. 
 
 Production basis None.  Prior to original certification of each aircraft manufactured subsequent to May 12, 
2000, an FAA representative must perform a detailed inspection for workmanship, 
materials and conformity with the approved technical data and a check of the flight 
characteristics. 
 
 Equipment The basic required equipment prescribed in the applicable airworthiness regulations (see 
Certification Basis) must be installed in the airplane for certification.  In addition, 
equipment for the particular operation must be installed. 
 
NOTE 1. Current weight and balance report including a list of equipment included in the certificated empty weight, a nd 
loading instructions when necessary must be provided for each aircraft at the time of original certification.  
 
  The certificated empty weight and corresponding center of gravity location must include 12 lb. (2 gal.) at (+84.5) of 
unusable fuel. 
 
NOTE 2. The following placards must be installed in full view of the pilot: 
 
  (a) Models AA-1 and AA-1A: 
 
   "THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE IN 
COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, 
MARKINGS, AND MANUALS." 
 
  NORMAL CATEGORY   AA-1 AA-1A 
  Maximum Design Weight   1500 lb. 1500 lb. 
  Design Maneuvering Speed, Va  125 mph CAS 120 mph CAS 
  Flight Load Factors:    
    Flaps Up   +3.8, -1.52 +3.8, -1.52 
    Flaps Down   +2.0 +3.5 
 
   NO ACROBATIC MANEUVERS INCLUDING SPINS APPROVED (AA-1 and AA-1A)

Page 7 A11EA 
 
 
  UTILITY CATEGORY   AA-1 AA-1A 
  Maximum Design Weight   1430 lb. 1430 lb. 
  Design Maneuvering Speed, Va  130 mph CAS 127 mph CAS 
  Flight Load Factors: 
   Flaps Up   +4.4, -1.76 +4.4, -1.76 
   Flaps Down   +2.0 +3.5 
 
  ACROBATIC MANEUVERS ARE LIMITED TO THE FOLLOWING: 
 
  MANEUVER    ENTRY SPEED (MPH, CAS) 
        AA-1 AA-1A 
  Chandelles    132 127 
  Lazy Eights    132 127 
  Steep Turns    132 127 
  Stalls (Except Whip Stalls)   Slow Deceleration Slow Deceleration 
 
  Models AA-1B and AA-1C: 
 
   "THIS AIRPLANE MUST BE OPERATED AS A UTILITY CATEGORY AIRPLANE IN COMPLIANCE 
WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS, AND 
MANUALS." 
 
        AA-1B AA-1C 
 
  Maximum Design Weight   1560 Lb. 1600 Lb. 
  Design Maneuvering Speed, Va  135 Mph Cas 117 Knots Cas 
  Flight Load Factors: 
   Flaps Up   +4.4, -1.76  +4.4, -1.76 
   Flaps Down   +3.5  +3.5 
 
  ACROBATIC MANEUVERS ARE LIMITED TO THE FOLLOWING: 
 
  MANEUVER  ENTRY SPEED (MPH, CAS)  ENTRY SPEED (KNOTS, CAS) 
        AA-1B  AA-1C 
  Chandelles    135  117 
  Lazy Eights    135  117 
  Steep Turns    135  117 
  Stalls (Except Whip Stalls)   Slow Deceleration  Slow Deceleration 
 
  Maximum Altitude Loss In Stalls  300 Feet (AA-1) 
        250 Feet (AA-1A) 
        300 Feet (AA-1B) 
        200 Feet (AA-1C) 
 
  Demonstrated Crosswind Velocity  15 Mph (AA-1) 
        13 mph (AA-1A) 
        18 mph (AA-1B) 
        16 knots (AA-1C) 
 
  KNOWN ICING CONDITIONS TO BE AVOIDED.  (Models AA-1, AA-1A, and AA-1B) 
 
  THIS AIRPLANE NOT APPROVED FOR FLIGHT IN ICING CONDITIONS.   (Model AA-1C)

A11EA Page 8 
 
 All Models: 
 
   THIS AIRPLANE IS CERTIFICATED FOR THE FOLLOWING OPERATIONS AS OF DATE OF 
ORIGINAL AIRWORTHINESS CERTIFICATE:  IFR, VFR, DAY, NIGHT.  (When properly equipped per 
FAR 91) 
 
   REFER TO WEIGHT AND BALANCE DATA FOR LOADING INSTRUCTIONS. 
 
   READ FUEL GAGES IN LEVEL FLIGHT ONLY. 
 
   FOR NORMAL OPERATION, MAINTAIN FUEL BALANCE. 
 
   DEMONSTRATED FUEL UNBALANCE   7 GAL. 
 
  (b) On left side of cabin: 
 
   "130 MPH MAX WITH CANOPY OPEN TO HERE.  NO FLIGHT WITH CANOPY OPEN BEYOND THIS 
POINT."  Placard Part No. 5803007-22 or equivalent.  (Models AA-1, AA-1A, AA-1B) 
 
   "113 KNOTS MAX WITH CANOPY OPEN TO HERE.  NO FLIGHT WITH CANOPY OPEN BEYOND 
THIS POINT."  Placard Part No. 5803007-51 or equivalent.  (Model AA-1C). 
 
  (c) In baggage compartment (All Models): 
 
   "BAGGAGE CAPACITY 100 LBS.  MAX."  Placard Part No. 803007-40 or equivalent. 
 
  (d) On instrument panel in full view of pilot (All Models): 
 
   "SPINS PROHIBITED."  Placard Part No. 803007-56 or equivalent. 
 
  (e) On instrument panel near the airspeed indicator stall speed vs. bank angle placard.  
 
   Placard Part No. 803007-53 (Model AA-1), 803007-54 (Model AA-1A), 803007-55 (Model AA-1B), 
   803007-67 (Model AA-1C). 
 
NOTE 3. Deleted  
 
....END....
```

## ADs (18, 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 2021-14-12](https://openairdocs.org/ad/2021-14-12): Horizontal Stabilizer, Plate/Skin, Elevator, Plates/Skin Structure · True Flight Holdings AA-1, AA-1A, AA-1B and 2 more. Effective Jul 27, 2021
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [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
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 85-21-02](https://openairdocs.org/ad/85-21-02): Seat Belt Attachment Bracket · True Flight Holdings AA-1, AA-1A, AA-1B and 1 more. Effective Oct 28, 1985
- [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981
- [AD 79-16-02](https://openairdocs.org/ad/79-16-02): Safety Belt Assemblies · Indiana Mills & Manufacturing Safety Belts, AA-1B, AA-1C and 3 more. Effective Aug 2, 1979
- [AD 78-13-04](https://openairdocs.org/ad/78-13-04): Fuel Measurement Gauge · True Flight Holdings AA-1, AA-1A and AA-1B. Effective Jun 30, 1978
- [AD 76-17-03](https://openairdocs.org/ad/76-17-03): Delaminations in Bonded Skin · True Flight Holdings AA-1, AA-1A, AA-1B and 3 more. Effective Aug 30, 1976
- [AD 75-09-07](https://openairdocs.org/ad/75-09-07): Mixture Control Wires · True Flight Holdings AA-1, AA-1A and AA-1B. Effective Apr 25, 1975
- [AD 72-06-02](https://openairdocs.org/ad/72-06-02): Rudder Aileron and Elevator Control Cables · True Flight Holdings AA-1, AA-1A, AA-1B and 1 more. Effective Aug 29, 1974
- [AD 72-07-10](https://openairdocs.org/ad/72-07-10): Wear on Elevator Bungee Housing · True Flight Holdings AA-1, AA-1A and AA-1B. Effective Jul 10, 1974
- [AD 73-13-07](https://openairdocs.org/ad/73-13-07): Placard Installation · True Flight Holdings AA-1, AA-1A and AA-1B. Effective Jun 25, 1973
- [AD 71-04-03](https://openairdocs.org/ad/71-04-03): Nose Gear Strut · True Flight Holdings AA-1. Effective Feb 25, 1971
- [AD 70-25-05](https://openairdocs.org/ad/70-25-05): Bungee Mounting Plate · True Flight Holdings AA-1. Effective Dec 8, 1970
- [AD 70-05-05](https://openairdocs.org/ad/70-05-05): Muffler Inspection · True Flight Holdings AA-1. Effective Mar 13, 1970
- [AD 75-07-04](https://openairdocs.org/ad/75-07-04): Rudder Control Bar Assemblies · True Flight Holdings AA-1, AA-1A, AA-1B and 2 more

## Registered aircraft by registry model (OpenAirDocs)

- [Grumman American Avn. AA-1B](https://openairdocs.org/model/grumman-american-avn-aa-1b): 231 aircraft (registry code 3960103)
- [American AA-1A](https://openairdocs.org/model/american-aa-1a): 207 aircraft (registry code 0630710)
- [American AA-1](https://openairdocs.org/model/american-aa-1): 153 aircraft (registry code 0630610)
- [Grumman American Avn. AA-1C](https://openairdocs.org/model/grumman-american-avn-aa-1c): 102 aircraft (registry code 3960100)
- [American AA-1B](https://openairdocs.org/model/american-aa-1b): 26 aircraft (registry code 0630820)
- [Grumman American Avn. AA-1A](https://openairdocs.org/model/grumman-american-avn-aa-1a): 1 aircraft (registry code 3960102)
- [Grumman American Avn. AA-1](https://openairdocs.org/model/grumman-american-avn-aa-1): 0 aircraft (registry code 3960101)

## STCs approved under this data sheet (195, 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position  Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [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 SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [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 SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [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 SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA1010CE](https://openairdocs.org/stc/SA1010CE): Installation of wing leading edge cuffs.. Curry Aviation LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA1016NW](https://openairdocs.org/stc/SA1016NW): Installation of a Lycoming O-360-A4M engine, Sensenich 76EM8-0-62 propeller, and AA-5 elevator system. Fletchair Inc.
- [STC SA1208NW](https://openairdocs.org/stc/SA1208NW): Installation of a Lycoming engine with Sensenich propeller. Fletchair Inc.
- [STC SA1209NW](https://openairdocs.org/stc/SA1209NW): Relocation of battery from forward face of firewall to aft baggage compartment bulkhead.. Fletchair Inc.
- [STC SA2169NM](https://openairdocs.org/stc/SA2169NM): Installation of a Sensenich 72 CK series propeller, Gulfstream American spinner (P/N 506006-50), engine oil cooler on a Lycoming O-235-C2C engine.. Fletchair Inc.
- [STC SA809NW](https://openairdocs.org/stc/SA809NW): Installation of fixed (flush) cowl flap, nose gear strut fairing and retainer.. Fletchair Inc.
- [STC SA810NW](https://openairdocs.org/stc/SA810NW): Installation of main landing gear fairings from the AA-5 series aircraft incorporating sheet metal covers over rubber in place of stock rubber parts.. Fletchair 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 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 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 SA1009NW](https://openairdocs.org/stc/SA1009NW): Installation of a dorsal fin (P/N 5302040-1) and associated assemblies. Air Mods NW
- [STC SA1012NW](https://openairdocs.org/stc/SA1012NW): Installation of auxiliary fuel tank models 2 TAFTA and 4 TAFTA and incresed gross weight. Air Mods NW
- [STC SA2129NM](https://openairdocs.org/stc/SA2129NM): Installation of a Lycoming O-320-E2G engine, AA-5A engine mount, cowling, air induction, and a McCauley 1C172/ SBTM/7359 propeller.. Air Mods NW
- [STC SA4387NM](https://openairdocs.org/stc/SA4387NM): Installation of Lycoming 0-320-A, C, or E series engine and a Sensenich 74DM6-0-58/64 or 74DM7-0-58/64 propeller.. Air Mods NW
- [STC SA4708NM](https://openairdocs.org/stc/SA4708NM): Installation of bolts to strengthen the nose gear torque tube assembly.. Air Mods NW
- [STC SA4722NM](https://openairdocs.org/stc/SA4722NM): Installation of a hat shelf in the aft baggage compartment.. Air Mods NW
- [STC SA991NW](https://openairdocs.org/stc/SA991NW): Installation of model AA-5A engine mount, cowling and carburetor air box. Air Mods NW

All 195: https://openairdocs.org/tcds/A11EA/stcs.md

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