# TCDS A31SO: Embraer S.A.

- Type: Type certificate data sheet
- Status: Current
- Holder: Embraer S.A.
- Revision: 14
- Revised: January 21, 2022
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25, Part 36, Part 21, Part 25, Part 36, Part 21, Part 25, Part 36, Part 21, Part 25, Part 36, Part 21, Part 25, Part 36
- Registered aircraft: 41, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/c9/e8/c9e8b22cda1f27474baaae8bca13602915ed8084918a7a77952257453d9250e7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A7F09A0D981A552862587D4004F1371.0001
- Page: https://openairdocs.org/tcds/A31SO

## Models (5)

As the data sheet lists them.

- EMB-120ER
- EMB-120
- EMB-120RT
- EMB-120FC
- EMB-120QC

## What the data sheet says

Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 
Revision No. 14 11 11 11 11 11 11 11 11 11 14 13 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
A31SO 
Revision 14 
Embraer 
EMB-120 
EMB-120RT 
EMB-120ER 
EMB-120FC 
EMB-120QC 
 
January 21, 2022 
TYPE CERTIFICATE DATA SHEET NO. A31SO 
 
This data sheet which is part of Type Certificate No. A31SO pres cribes 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   Embraer S.A. 
    Av. Brig. Faria Lima, 2170 
    12227-901 São Jose dos Campos, SP 
    Brazil 
 
Type Certificate Holder Record  Yaborã Indústria Aeronaútica S.A. transferred the TC No A31SO to Embraer S.A. on 
January 1st, 2022. 
Embraer S.A. transferred TC No A31SO to Yaborã Indústria Aeronáutica S.A. on 
January 31, 2020. 
Empresa Brasileira de Aeronáutica S.A. (Embraer) changed company name to Embraer 
S.A. effective November 2010. 
 
1. - Model EMB-120 Brasilia  (Transport Category), Approved July 9, 1985 
 
Engines 2 Pratt & Whitney of Canada Ltd PW 115 
  
Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to P&W 
 specifications PWA522 or CPW204. See NOTE 4. 
  
Oil In accordance with P&W Specification 
 PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). 
 
Engine Limits  
 
Shaft HP 
 
Jet Thrust 
(lbf) 
 
Torque 
% 
Prop. 
NP 
% 
 
Int-Turbine T6 
Temp.°C (°F)  
Gas 
Gen.NH 
% 
Max. Take-off 
(5 min. max.) 
 
1760 
 
212 
 
110 
 
100 
 
785  (1445) 
 
100 
Max. Continuous 1600 212 100 100 785  (1445) 100 
Transient 
(20 sec. max.) 
    
110 
 
850  (1562) 
 
102 
Starting  
(5 sec. max.) 
     
950  (1742) 
 
Max. Reverse    80   
NOTE: The above engine limits are individual maximum operating limits and are not 
for setting engine power.  Refer to AFM Section 4 for power setting data. 
 
Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when 
Ground Operation cleared for takeoff or during landing roll. 
  
 Power Levers must remain at or below Flight Idle during all ground operations, except 
 for brief (approximately 5 seconds) excursions as needed to maneuver the airplane 
 
Max. Operating Altitude S/N 12000004, 12000006 through 12000011 
 Enroute - 25,000 ft. (Bleed on) 
 - 20,000 ft. (Bleed off)

Revision 14 A31SO 
January 21, 2022 Page 2 of 12 
 
 
  
 
 
 S/N 12000012 and up 
   Bleed On Bleed Off  
 Enroute - EEC on 32,000 ft. 25,000 ft  
 EEC off 25,000 ft 20,000 ft  
  
Temperature Operating S/N 12000004, 12000006 through 12000020 
Limits Maximum ISA +32° C 
 Minimum -54° C 
  
 S/N 12000021 and up 
 Maximum ISA +35° C 
 Minimum -54° C 
  
Maximum Weight  
(mass)   lb. kg  
 Start of take-off 25,353 11,500  
 Landing 24,802 11,250  
 Zero Fuel  23,148 10,500  
 
Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. 
  
Maximum Baggage 1213 lb (See NOTE 7). 
 
2. - Model EMB-120RT Brasilia  (Transport Category),  Approved October 23, 1986 
  
Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 
 2 Pratt & Whitney of Canada Ltd. PW 118A or 
 2 Pratt & Whitney of Canada Ltd. PW118B or 
 1 Pratt & Whitney of Canada Ltd. PW 118 and 
 1 Pratt & Whitney of Canada Ltd. PW 118A (see AFM for operating limits) 
  
Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A,  Jet A-1 & Jet B conforming to P&W. 
 specifications PWA522 or CPW204. See NOTE 4. 
  
Oil In accordance with P&W Specification PWA521 Type II (MIL-L-23699) 
 or CPW202 (MIL-L-23699A). 
 
Engine Limits  
Shaft 
 HP 
 
Jet Thrust 
(lbf) 
Prop 
Torque 
% 
 
NP 
% 
 
Int-Turbine, T6 
Temp.°C (°F) 
Gas 
Gen.NH 
% 
Gas 
Gen.NL 
% 
PW 118 Max. 
Take-off(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816  (1500) 
 
100 
 
100 
PW 118A Max 
Take-off(5 min. max.) 
1980 230 110 100 816  (1500) 102 102 
PW 118B Max 
Take-off(5 min. max.) 
1980 230 110 100 816  (1500) 102 102 
PW 118 Max 
Continuous 
1800 
 
230 100 100 800 (1472) 100 100 
PW 118A Max 
Continuous 
1800 
 
230 100 100 800 (1472) 102 102 
PW 118B Max 
Continuous 
1800 
 
230 100 100 800 (1472) 102 102 
Transient 
(20 Sec. max.) 
  120 110 850 (1562) 102 102 
Starting 
(5 sec. max.) 
    950 (1742)   
Max. Reverse    80

Revision 14 A31SO 
January 21, 2022 Page 3 of 12 
 
 NOTE: The above engine limits are individual maximum operating limits and are not 
for setting engine power.  Refer to AFM Section 4 for power setting data. 
 
 
Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when 
Ground Operation cleared for takeoff or during landing roll. 
 
 Power Levers must remain at or below Flight Idle during all ground operations, except 
 for brief (approximately 5 seconds) excursions as needed to maneuver the airplane. 
 
Max. Operating Altitude   Bleed On Bleed Off  
 EEC on  32,000 ft 25,000 ft.  
 EEC off  25,000 ft. 20,000 ft  
      
Temperature Operating  
Limits Maximum ISA +35° C 
 Minimum -54° C 
  
 S/N 12000021 and up 
 Maximum ISA + 35°C 
 Minimum -54°C 
  
Maximum Weight (mass)  
  lb. kg  
 Start of take-off 25,529 11,580  
 Landing  24,802 11,250  
 Zero Fuel  23,148 10,500  
      
Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. 
  
Maximum Baggage 1213 lb (See NOTE 7). 
  
3.  Model EMB-120ER Brasilia (Transport Category), Approved March 20, 1992 
  
Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 
 2 Pratt & Whitney of Canada Ltd. PW 118A or 
 2 Pratt & Whitney of Canada Ltd. PW118B or 
 1 Pratt & Whitney of Canada Ltd. PW 118 and 
 1 Pratt & Whitney of Canada Ltd. PW 118A 
 (see AFM for operating limits) 
 
Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to 
 P&W specifications PWA522 or CPW204.  See NOTE 4 
  
Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 
 (MIL-L-23699A). 
 
Engine Limits  
 
Shaft HP 
 
Jet Thrust 
(lbf) 
 
Torque 
% 
Prop 
NP 
% 
 
Int-Turbine, T6 
Temp. °C (°F) 
Gas 
Gen. NH   
% 
Gas 
Gen. NL 
% 
PW 118 Max Take-off 
(5 min. max) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
100 
 
100 
PW 118A Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118B Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 
PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 
PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 
Transient 
(0 sec. max.) 
   
120 
 
110 
 
850 (1562) 
 
102 
 
102

Revision 14 A31SO 
January 21, 2022 Page 4 of 12 
 
Starting 
(5 sec. max.) 
 
 
    
950 (1742) 
  
Max. Reverse    80    
 NOTE:  The above engine limits are individual maximum operating limits and are not for 
setting engine power.  Refer  to AFM Section 4 for power setting data. 
 
Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when 
Ground Operation cleared for takeoff or during landing roll 
  
 Power Levers must remain at or below Flight Idle during all ground operations, except 
 for brief (approximately 5 seconds) excursions as needed to maneuver the airplane 
 
Max. Operating Altitude   Bleed On Bleed Off  
 EEC on  32,000 ft 25,000 ft.  
 EEC off  25,000 ft. 20,000 ft  
      
Temperature Operating  
Limits Maximum ISA +35° C 
 Minimum -54° C 
  
Maximum Weight (mass)  
  lb. kg  
 Ramp 26,609 12,070  
 Takeoff  26,433 11,990  
 Landing  25,794 11,700  
 Zero Fuel  24,030 10,800  
 
      
Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. 
  
Maximum Baggage 1213 lb (See NOTE 7). 
  
 
4. Model EMB-120FC Brasilia (Transport Category, Full Cargo version), Approved July 17, 2000. 
  
Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 
 2 Pratt & Whitney of Canada Ltd. PW 118A or 
 2 Pratt & Whitney of Canada Ltd. PW118B or 
 1 Pratt & Whitney of Canada Ltd. PW 118 and 
 1 Pratt & Whitney of Canada Ltd. PW 118A 
 (see AFM for operating limits) 
  
Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to 
 P&W specifications PWA522 or CPW204.  See NOTE 4. 
  
Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 
 (MIL-L-23699A). 
 
Engine Limits  
 
Shaft HP 
 
Jet Thrust 
(lbf) 
 
Torque 
% 
Prop 
NP 
% 
 
Int-Turbine, T6 
Temp. °C (°F) 
Gas 
Gen. NH   
% 
Gas 
Gen. NL 
% 
PW 118 Max Take-off 
(5 min. max) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
100 
 
100 
PW 118A Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118B Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 
PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 
PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 
Transient 
(0 sec. max.) 
   
120 
 
110 
 
850 (1562) 
 
102 
 
102

Revision 14 A31SO 
January 21, 2022 Page 5 of 12 
 
Starting 
(5 sec. max.) 
 
 
    
950 (1742) 
  
Max. Reverse    80    
 NOTE:  The above engine limits are individual maximum operating limits and are not for 
setting engine power.  Refer  to AFM Section 4 for power setting data. 
 
Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when 
Ground Operation cleared for takeoff or during landing roll 
  
 Power Levers must remain at or below Flight Idle during all ground operations, except 
 for brief (approximately 5 seconds) excursions as needed to maneuver the airplane 
 
  
Max. Operating Altitude   Bleed On Bleed Off  
 EEC on  32,000 ft 25,000 ft  
 EEC off  25,000 ft 20,000 ft  
      
Temperature Operating  
Limits Maximum ISA +35° C 
 Minimum -54° C 
  
Maximum Weight (mass)  
  lb. kg  
 Ramp 26,609 12,070  
 Takeoff  26,433 11,990  
 Landing  25,794 11,700  
 Zero Fuel  24,030 10,800  
      
Number of Seats None. Approved for cargo only.  No passengers allowed. 
  
Maximum Occupants Not to exceed 3, including pilot, copilot and 1 check pilot; 
  
Maximum Load on   
Cargo Compartment 8150 lb. 
 
Maximum Loading  
    Distribution on Cargo Compartment 
 
 
CARGO COMPARTMENT 
 
STATION LIMITS  
X  (ft) 
 
MAX.  LOAD 
(lb) 
FLOOR  LOAD LIMIT 
(lb/sqft) 
E1 From x=18.57 to x=26.41 2490 61 
E2 From x=26.41 to x=35.20 2645 61 
E3 From x=35.20 to x=44.71 2550 61 
E4 From x=44.71 to x=49.05 1210 100 
E1+E2 From x=18.57 to x=35.20 4400 61 
 
E1+E2+E3+E4 
 
 
From x=18.57 to x=49.05 
 
8150 
According to corresponding 
cargo compartment 
 
  
5. Model EMB-120QC Brasilia (Transport Category, Quick Change Cargo version), Approved October 1, 2003. 
  
Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or

Revision 14 A31SO 
January 21, 2022 Page 6 of 12 
 
 2 Pratt & Whitney of Canada Ltd. PW 118A or 
 2 Pratt & Whitney of Canada Ltd. PW118B or 
 1 Pratt & Whitney of Canada Ltd. PW 118 and 
 1 Pratt & Whitney of Canada Ltd. PW 118A 
 (see AFM for operating limits) 
 
  
Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to 
 P&W specifications PWA522 or CPW204.  See NOTE 4. 
  
Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 
 (MIL-L-23699A). 
 
 
Engine Limits  
Shaft 
 HP 
 
Jet Thrust 
(lbf) 
 
Torque 
% 
Prop 
NP 
% 
 
Int-Turbine, T6 
Temp. °C (°F) 
Gas 
Gen. NH   
% 
Gas 
Gen. NL 
% 
PW 118 Max Take-off 
(5 min. max) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
100 
 
100 
PW 118A Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118B Max Take-off 
(5 min. max.) 
 
1980 
 
230 
 
110 
 
100 
 
816 (1500) 
 
102 
 
102 
PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 
PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 
PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 
Transient 
(0 sec. max.) 
   
120 
 
110 
 
850 (1562) 
 
102 
 
102 
Starting 
(5 sec. max.) 
 
 
    
950 (1742) 
  
Max. Reverse    80    
 NOTE:  The above engine limits are individual maximum operating limits and are not for 
setting engine power.  Refer  to AFM Section 4 for power setting data. 
 
Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when 
Ground Operation cleared for takeoff or during landing roll 
  
 Power Levers must remain at or below Flight Idle during all ground operations, except 
 for brief (approximately 5 seconds) excursions as needed to maneuver the airplane 
  
Max. Operating Altitude   Bleed On Bleed Off  
 EEC on  32,000 ft 25,000 ft.  
 EEC off  25,000 ft. 20,000 ft  
      
Temperature Operating  
Limits Maximum ISA +35° C 
 Minimum -54° C 
  
Maximum Weight (mass)  
  lb. kg  
 Ramp 26,609 12,070  
 Takeoff  26,433 11,990  
 Landing  25,794 11,700  
 Zero Fuel (see NOTE 11) 24,030 10,800  
 
Maximum Number  
of Occupants With an original forward lavatory configuration, maximum 34 including 1 pilot, 1 
copilot, 1 flight attendant, 1 check pilot and 30 passengers.  With an original aft lavatory 
configuration, maximum 31 including 1 pilot, 1copilot, 1 flight attendant, 1 check pilot 
and 27 passengers.  With a cargo configuration, maximum 03, 1 pilot, 1copilot and 1 
check pilot, no passengers or flight attendant are allowed.

Revision 14 A31SO 
January 21, 2022 Page 7 of 12 
 
Maximum Load on  
Cargo Compartment When operating with passenger version, 1213 lb (see NOTE 7).  
When operating with cargo (class E) version: 
7715 lb to comply with the requirement FAR 121 
7500 lb to comply with the requirement FAR 135 
 
 
Maximum Loading  
Distribution on Cargo (Class E) Compartment 
 
 
CARGO COMPARTMENT 
 
STATION LIMITS 
X  (ft) 
 
MAX.  LOAD 
(lb) 
FLOOR  LOAD LIMIT 
(lb/sqft) 
E1 From x=20.5 to x=28.4 2490 61 
E2 From x=28.4 to x=36.6 2645 61 
E3 From x=36.6 to x=44.5 2550 61 
E4 From x=44.5 to x=49.0 1210 100 
E1+E2 From x=20.5 to x=36.6 4400 61 
 
Data Pertinent to All Models  
  
Propeller and Propeller Limits 2- Hamilton Standard Model 14RF-9 
 Blade: RFC11E1-6A, RFC11M1-6A,  RFC11N1-6A or RFC11U1-6A 
 Diameter: 10.5 ft. nominal   
      
 Pitch settings at STA 42 ins   
 Feather 79.2°    
 Flight fine 17.3°    
 Ground fine -4.5°    
 Full reverse -15.0°    
      
 Propeller (Np)     
  - Takeoff 1300 rpm (100%) 
  - Max. Continuous 1300 rpm (100%)

Revision 14 A31SO 
January 21, 2022 Page 8 of 12 
 
 
 
 
 
 
 
Airspeed Limits (IAS) 
 Maximum Operating Limit Speed (Vmo)   
 
 
   Knots MPH 
 Vfe (Flaps extended) Flaps 15° 200 230 
  Flaps 25° 150 175 
  Flaps 45° 135 156 
 VA (Maneuvering)  200 230 
 VLO (Landing gear operation)  200 230 
 VLE (Landing gear extended)  200 230 
 
Minimum Crew 2 (Pilot and Copilot)   
     
Fuel Capacity 882 gallons (441 gallons each tank)   
 Unusable fuel 7.4 gallons (3.7 gallons each tank)   
    
Oil Capacity 13.0 gal. (6.5 gal. in each engine).   
    
Datum 366.4" forward of the 66% wing chord line (frame 28). 
The 66% wing chord line is 0.67" aft of the rear jack points. 
 
Leveling Means Plumb from the upper part of the floor frame 28 using a mark in the 
lower part of the frame as a reference. 
 
   
Maximum Baggage   
(Passenger Configuration) 1213 lb  
   
Maximum Cargo Deleted.  Previous note not applicable to US configuration

Revision 14 A31SO 
January 21, 2022 Page 9 of 12 
 
 
 
 
 
 
 
C.G. Limits EMB-120 and EMB-120RT 
 
26000
24000
22000
20000
18000
16000
14000
0 10 4020 30 50
% MAC
W
EIGHT
-lb
19.5%
21.0%
42.0%
43.5%
16.3%
13.4%
4.0% 6.0%
15873 lb
(7200 kg)MOW
18297 lb (8300 kg)
22707 lb
(10300 kg)
MTOW=25353 lb (11500 kg)
19.8%
MZFW=23148 lb (10500 kg)
22707 lb (10300 kg)
MRW=25529 lb (11580 kg)
44.0%14330 lb-(6500 kg)
MLW=24802 lb (11250 kg)
TAKEOFF AND LANDING LIMITS
IN-FLIGHT LIMITS (FLAPS AND GEAR UP)

Revision 14  A31SO
January 21, 2022  Page 10 of 12
C.G. Limits EMB-120ER, EMB-120FC and EMB-120QC
• TAKEOFF AND LANDING LIMITS
- - IN-FLIGHT LIMITS (FLAPS AND GEAR UP)
28000
23.3%  42.0%
12000 mad  = MTOW = 26433 lb (11990 kg) =  MRW = 26609 lb (12070 kg;
26000  MLW = 25794 lb (11700 kg)  43.5%:
: 25353 Ib (11500 kg)
21.9%
11000 -  MZFW = 24030 Ib =
24000-  : (10900 kg)  €19.5%
18.2%
22707 1b:  22707 Ib
(10300 kg)  1(10300 kg)
10000 -  22000
13.4%;
| 44.0%:
9000 -  20000
18297 Ib (8300 kg)
18000
8000 -
4.0% 1:  • 6.0%
16000  715873 16
7000 -  EMOV  =(7200 kg)
14330 Ib (6500 kg)
14000
6000 -
10  20  30  40  50
% MAC
Control Surface Movements  Deflections measured normal to hinge lines:
Main Rudder (hinge at 70% chord)  Right  20° + 1°  Left 17° + 1°
Secondary Rudder (hinge at 86% chord)  Right  15°+ 1°  Left  13°+ 1°
Up  20° + 1°  Down  15° + 1°
Up  25° + 1°  Down  15° + 1°
Flaps (Outboard and Inboard)
Max. deflection  45° + 1°
Flap (Middle) - Max. deflection  51° + 1°
Elevator Tabs  (Trim deflections)  Up  3.3° + 0.5° or  Down 22° + 1°
5.5° + 0.5°
Right Aileron Tab Trim Deflections
(Aileron Neutral)  Up  11° + 1°  Down  11° + 1°
Aileron Automatic Tab  25° Up 14.7° + 1°  15° down  8.5° + 1°

Revision 14 A31SO 
January 21, 2022 Page 11 of 12 
 
      
Serial Numbers Eligible A Brazilian Certificate of Airworthiness for Export endorsed as noted under "Import 
Requirements" must be submitted for each individual aircraft for which application for 
U.S. certification is made. 
  
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 Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-49, 
effective September 10, 1979; FAR 25, including Amendments through 25-54, effective 
October 14, 1980; FAR 25.832, Amendment 25-56; Special FAR (SFAR) 27, including 
Amendments through 27-5 effective January 11, 1984, and FAR 36, including 
Amendments through 36-12 effective August 1, 1981 for EMB-120 and EMB-120RT, 
through 36-18 effective August 18, 1992 for EMB-120ER, through 36-22 effective 
October 13, 1999 for EMB-120FC and through 36-24 effective August 07, 2002 for 
EMB-120QC ; Exemption from FAR 25.571 (e) (2) as specified in Exemption No. 
3722; Equivalent Safety Finding to FAR 25.783 (f) Cargo Door.  Airplanes 
incorporating Embraer Service Bulletin No. 120-25-0220 comply with FAR 
25.811(c)(2)(ii), Amendment 25-79, instead of FAR 25.811(e)(3), Amendment 25-54. 
  
 Date of application for EMB-120; June 8, 1981. 
  
 Date of application for EMB-120RT; August 20, 1986. 
  
 Date of application for EMB-120ER; August 16, 1991. 
  
 Date of application for EMB-120FC; December 2, 1999. 
  
 Date of application for EMB-120QC; October 6, 2000. 
 
 
Part 26 – Continued Airworthiness and Safety Improvements for Transport Category Airplanes: 
 Based on § 21.29(a) for new import TCs, or § 21.101(g) for changes to TCs, applicable 
provisions of Part 26 are included in the certification basis.  For any future Part 26 
amendments, the holder of this TC must demonstrate compliance with the applicable 
sections. 
 
Service Information Service bulletins, structural repair manuals, vendor manuals, aircraft flight manuals, and 
overhaul and maintenance manuals, which contain a statement that the document is 
ANAC approved, are accepted by the FAA and are considered FAA approved.  These 
approvals pertain to the type design only. 
  
Ditching Compliance has been shown with the ditching requirements of FAR 25.801. When the 
operating rules require emergency ditching equipment, compliance with 25.1415 must 
be demonstrated. 
  
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations 
(see Certification Basis) must be installed in the aircraft for certification.  The "Basic 
Equipment Checklist," "Chart A," lists all the required and optional equipment and is 
included in the POH and ANAC approved AFM

Revision 14 A31SO 
January 21, 2022 Page 12 of 12 
 
 
 
NOTE 1. Current weight and balance report including list of equipment included in certificated empty 
weight and loading instructions must be provided for each aircraft at the time of original 
certification. For loading procedures the Weight and Balance Manual WB120/701, must be 
followed. The certificated empty weight and corresponding center-of-gravity location must 
include system (undrainable) oil (not included in oil capacity) and unusable fuel (not included in 
usable fuel) as follows: 
  
 Fuel: 48 lbs.  at  348.8 in.   
 Oil: 16 lbs.  at  272.2 in.   
 
NOTE 2 The aircraft must be operated in accordance with the ANAC Approved Airplane Flight Manual. 
For cargo configuration required placards see also Embraer Service Bulletin nº 120-25-0245 
  
NOTE 3 The Airworthiness Limitations are listed on Section 6 of document MRB-HI-200 “Maintenance 
Review Board Report”, as follows 
 Part A - System & Powerplant 
Part B - Strucuture 
Part C - Life-Limited Components 
Part D - Critical Design Configuration Control Limitations (CDCCL) 
Part E - Fuel System Limitations 
  
NOTE 4 If fuel conforming to specifications PWA522 or CPW204 is not available it is permissible to use 
aviation gasoline MIL-G-5572 of all grades for a total time period not exceeding 150 hours 
during any overhaul period. 
JET B or JP-4 fuel should only be used when no other fuel is available. 
  
NOTE 5 Aircraft S/N 12000004 and 12000006 through 12000021, inclusive, have been converted to the 
model EMB-120RT by the accomplishment of the Embraer Service Bulletin nº 120-72-0001. 
  
NOTE 6 The engine Pratt & Whitney PW-118A may be installed in accordance with the Embraer Service 
Bulletin nº 120-072-0002. 
  
NOTE 7 The passenger baggage compartment maximum capacity may be increased to 1540 lb thru 
accomplishment of SB 120-25-0205. All pax aircraft S/Ns 12000281, 12000286 through 
12000288, and 12000290 and on are factory modified for 1540 lb. 
  
NOTE 8 All EMB-120RT S/Ns may be converted into the model EMB-120ER by the accomplishment of  
Embraer Service Bulletin nº 120-00-0008. 
  
NOTE 9 All EMB-120ER S/Ns may be converted into the model EMB-120FC by the accomplishment of 
Embraer Service Bulletin nº 120-25-0245 
  
NOTE 10 All EMB-120ER S/Ns may be converted into the model EMB-120QC by the accomplishment of 
Embraer Service Bulletins nº 120-25-0244 and 120-25-0243. 
  
NOTE 11. All EMB-120QC operating cargo must comply with Embraer Service Bulletins nº 120-25-0252 
and 120-25-0253. 
 
...END...
```

## ADs (70, first 50, in force first)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-02-09](https://openairdocs.org/ad/2025-02-09): Fuselage · Embraer EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Mar 18, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2017-10-04](https://openairdocs.org/ad/2017-10-04): Landing Gear · Embraer EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 29, 2017
- [AD 2011-08-09](https://openairdocs.org/ad/2011-08-09): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-19-04](https://openairdocs.org/ad/2010-19-04): Airborne Auxiliary Power · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Oct 27, 2010
- [AD 2008-04-18 R1](https://openairdocs.org/ad/2008-04-18-R1): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Nov 16, 2009
- [AD 2009-15-18](https://openairdocs.org/ad/2009-15-18): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Sep 2, 2009
- [AD 2008-15-01](https://openairdocs.org/ad/2008-15-01): Elevator trim system · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 21, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-26-21](https://openairdocs.org/ad/2007-26-21): EMB-120 wing section · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 20, 2008
- [AD 2006-12-14](https://openairdocs.org/ad/2006-12-14): Shut-off and crossbleed valves of the bleed air system · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 18, 2006
- [AD 2006-11-10](https://openairdocs.org/ad/2006-11-10): De-icing system ejector flow control valves · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 30, 2006
- [AD 2006-10-09](https://openairdocs.org/ad/2006-10-09): Wiring harnesses · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 20, 2006
- [AD 2006-07-18](https://openairdocs.org/ad/2006-07-18): Elevator control surface · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective May 12, 2006
- [AD 2006-02-02](https://openairdocs.org/ad/2006-02-02): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 24, 2006
- [AD 2005-25-01](https://openairdocs.org/ad/2005-25-01): Electrical harnesses · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jan 9, 2006
- [AD 2004-14-24](https://openairdocs.org/ad/2004-14-24): Rotary variable inductive transducers (RVITs) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 23, 2004
- [AD 2004-14-25](https://openairdocs.org/ad/2004-14-25): Lower rotating beacon to the airframe · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 23, 2004
- [AD 2004-13-12](https://openairdocs.org/ad/2004-13-12): Airplane Flight Manual - propeller synchronizer switch · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 6, 2004
- [AD 2004-13-13](https://openairdocs.org/ad/2004-13-13): Access door ramp of the fueling control panel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 3, 2004
- [AD 2004-12-18](https://openairdocs.org/ad/2004-12-18): Vertical Cargo Nets in Cargo-Configured Cabins · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 27, 2004
- [AD 2004-12-12](https://openairdocs.org/ad/2004-12-12): Main landing gear (MLG) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 21, 2004
- [AD 2004-06-07](https://openairdocs.org/ad/2004-06-07): Pitot/static 1, 2 and auxiliary sensors · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Apr 29, 2004
- [AD 2004-01-04](https://openairdocs.org/ad/2004-01-04): Hydraulic tube assemblies · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 13, 2004
- [AD 2003-15-05](https://openairdocs.org/ad/2003-15-05): Flight idle stop system circuit breaker · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Sep 4, 2003
- [AD 2003-12-12](https://openairdocs.org/ad/2003-12-12): Airplane Flight Manual - flight attendant's seat · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Jul 28, 2003
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 2001-20-17](https://openairdocs.org/ad/2001-20-17): Airplane Flight Manual-Ice Accretion · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Oct 22, 2001
- [AD 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001
- [AD 2001-06-18](https://openairdocs.org/ad/2001-06-18): AFM Revisions - Limitations Section - Ice Protection System · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Apr 16, 2001
- [AD 2000-23-30](https://openairdocs.org/ad/2000-23-30): Elevator Control Cable · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Jan 2, 2001
- [AD 2000-23-09](https://openairdocs.org/ad/2000-23-09): Hydraulics · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 20, 2000
- [AD 2000-22-12](https://openairdocs.org/ad/2000-22-12): Circuit Breakers · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 12, 2000
- [AD 2000-22-08](https://openairdocs.org/ad/2000-22-08): Mass-Balance Weights of the Aileron · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 11, 2000
- [AD 2000-19-07](https://openairdocs.org/ad/2000-19-07): Direct Current (DC) Relay Box · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Oct 31, 2000
- [AD 2000-19-10](https://openairdocs.org/ad/2000-19-10): Prevent Sudden Change In Pitch Attitude · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Oct 13, 2000
- [AD 99-19-28](https://openairdocs.org/ad/99-19-28): Brake Assemblies Of Main Landing Gear · Embraer - Empresa Brasileira de Aeronautica EMB-120ER and EMB-120RT. Effective Oct 20, 1999
- [AD 99-17-04](https://openairdocs.org/ad/99-17-04): Aileron Control Cables And Nylon Grommets · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Sep 22, 1999
- [AD 99-02-18 R1](https://openairdocs.org/ad/99-02-18-R1): Titanium Thermal Insulating Blankets · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 3, 1999
- [AD 98-15-22](https://openairdocs.org/ad/98-15-22): Wing De-Ice Boot · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Aug 27, 1998
- [AD 98-13-29](https://openairdocs.org/ad/98-13-29): AFM - Limitation Section - Power Levers · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jul 29, 1998
- [AD 98-03-19](https://openairdocs.org/ad/98-03-19): Prevent Generator Overload Conditions · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 18, 1998
- [AD 97-05-02](https://openairdocs.org/ad/97-05-02): Channel Fairings And Shims · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Apr 2, 1997
- [AD 97-02-21](https://openairdocs.org/ad/97-02-21): Inspect Wing Skin For Fuel Leakage · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 3, 1997
- [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 96-09-24](https://openairdocs.org/ad/96-09-24): AFM- Icing · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jun 11, 1996
- [AD 95-25-11](https://openairdocs.org/ad/95-25-11): AFM - Limitations Sections Propeller · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Dec 27, 1995

All 70: https://openairdocs.org/tcds/A31SO/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er): 38 aircraft (registry code 3260203)
- [Embraer EMB-120](https://openairdocs.org/model/embraer-emb-120): 3 aircraft (registry code 3260201)
- [Embraer EMB-120FC](https://openairdocs.org/model/embraer-emb-120fc): 0 aircraft (registry code 3260204)
- [Embraer EMB-120QC](https://openairdocs.org/model/embraer-emb-120qc): 0 aircraft (registry code 3260205)
- [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt): 0 aircraft (registry code 3260202)

## STCs approved under this data sheet (81, first 50)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc.
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc.
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC SA5845NM](https://openairdocs.org/stc/SA5845NM): Installationof cabin interior fluorescent lighting system.. Bruce Aerospace Inc.
- [STC ST104CH](https://openairdocs.org/stc/ST104CH): Installation of a TCAS I and optional Data Recorder Unit. Acron Aviation Inc.
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc.
- [STC ST01110DE](https://openairdocs.org/stc/ST01110DE): Installation of a Luma Technologies Multiple Alarm Panel (MAP). Peregrine
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST03022AT](https://openairdocs.org/stc/ST03022AT): Installation of a Sandel Model ST3400 Terrain Awareness and Warning System (TAWS).. Woven Electronics, LLC
- [STC ST03375AT](https://openairdocs.org/stc/ST03375AT): Installation of Garmin GPS 165 TSO Global Positioning System (GPS).. Woven Electronics
- [STC ST00598WI](https://openairdocs.org/stc/ST00598WI): Conversion of airplane from a passenger configuration to an all cargo configuration.. Worldwide Aviation LLC
- [STC SA8840SW](https://openairdocs.org/stc/SA8840SW): Replace core assembly of AiResearch Primary/Secondary Air-to-Air Heat Exchanger, part number 194546-3. Honeywell International Inc.
- [STC SA8466SW](https://openairdocs.org/stc/SA8466SW): Recore of AiResearch Engine Oil Coolers Part Numbers 160282-3 and 160282-4 with LORI Core Assembly Part Number L8602548-1. Honeywell International Inc.
- [STC ST00895DE](https://openairdocs.org/stc/ST00895DE): Installation of the Garmin G700 TXi Avionics Suite. Peregrine
- [STC ST00075WI-D](https://openairdocs.org/stc/ST00075WI-D): Installation of provisions for the Bendix/King CAS 66A TCAS I system.. Honeywell International Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00007IB](https://openairdocs.org/stc/ST00007IB): Installation of a Honeywell Mode S Transponder model MST 67 and TCAS II model CAS 81. Embraer Engineering & Technology Center - USA Inc.
- [STC ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST03089NY](https://openairdocs.org/stc/ST03089NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02499AK](https://openairdocs.org/stc/ST02499AK): Approval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installed. ADS-B Technologies, LLC
- [STC ST04136CH](https://openairdocs.org/stc/ST04136CH): Installation of a TFD-8601 EFIS (Electronic Flight Instrument System) Display. StandardAero Business Aviation Services, LLC
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01157SE](https://openairdocs.org/stc/ST01157SE): Installation of increased security cockpit door. Cascade Aviation Services Inc
- [STC ST02600LA](https://openairdocs.org/stc/ST02600LA): Replacement of original SAFT 4076-9 Nickel-Cadmium battery with a Concorde RG-380E/40B or RG-380E/44 or RG-380E/46 Valve Regulated Lead Acid Battery. Concorde Battery Corporation
- [STC ST02660NY-D](https://openairdocs.org/stc/ST02660NY-D): Installation of a Rockwell Collins TCAS-94. B/E Aerospace Inc
- [STC ST02661NY-D](https://openairdocs.org/stc/ST02661NY-D): Installation of a Honeywell CAS-67A TCAS 11. B/E Aerospace Inc
- [STC ST02014LA](https://openairdocs.org/stc/ST02014LA): Installation of Hawker 9750W0370-7 Steel Cased, 24 Volt, 43 Amp-hour, Sealed Lead Acid Battery.. Securaplane Technologies
- [STC ST01713WI](https://openairdocs.org/stc/ST01713WI): Modification of a Rockwell Collins, Inc. AHC-85( ) (AHRS) installation. Rockwell Collins Inc
- [STC ST02281AK](https://openairdocs.org/stc/ST02281AK): Installation of an increased security cockpit door. Jet Midwest Group
- [STC SA5472NM](https://openairdocs.org/stc/SA5472NM): Installation of a Teledyne Controls  Flight Data Acquisition Unit P/N 2231266-4. Teledyne Controls
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation.. Rockwell Collins Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.. Rockwell Collins Inc
- [STC SH1053NE](https://openairdocs.org/stc/SH1053NE): Remove existing starter-generator and install Aircraft Parts starter generator P/N 400SG135Q.. Skurka Aerospace Inc.
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST151CH](https://openairdocs.org/stc/ST151CH): Installation of strobe upper anticollision light, P/N 30-1033-53.. Honeywell International Inc.
- [STC SA8815SW](https://openairdocs.org/stc/SA8815SW): Installation of a single Mode S Transponder with provisions for a Bendix TCAS II.. Worldwide Aviation LLC
- [STC ST01142WI-D](https://openairdocs.org/stc/ST01142WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head.. Rockwell Collins Inc
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models.. SMR Technologies
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST02990AT](https://openairdocs.org/stc/ST02990AT): Installation of Control Column Push-To-Talk (PTT) Switch with Gold Contacts.. Chippewa Aerospace, Inc.
- [STC ST02517AT](https://openairdocs.org/stc/ST02517AT): Installation of Avidyne FlightMax 850 display.. Chippewa Aerospace, Inc.
- [STC ST02777AT](https://openairdocs.org/stc/ST02777AT): Installation of a FA2100CVR Cockpit Voice Recorder (CVR).. Chippewa Aerospace, Inc.
- [STC ST02778AT](https://openairdocs.org/stc/ST02778AT): Installation of a FA2100FDR Flight Data Recorder (FDR).. Chippewa Aerospace, Inc.

All 81: https://openairdocs.org/tcds/A31SO/stcs.md

---
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