# TCDS A57NM: Embraer S.A.

- Type: Type certificate data sheet
- Status: Current
- Holder: Embraer S.A.
- Revision: 26
- Revised: October 1, 2025
- Product: Aircraft, Large Airplane
- Certification basis: Part 25, Part 21
- Registered aircraft: 50, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/a2/4b/a24b5c9b82da579c9d4ed09828734ddf48a4994b695842c36d61ddb7a6c1e4da
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194156626420251001141527.0001
- Page: https://openairdocs.org/tcds/A57NM

## Models (9)

As the data sheet lists them.

- ERJ 190-400
- ERJ 190-200 STD
- ERJ 190-100 STD
- ERJ 190-100 LR
- ERJ 190-100 ECJ
- ERJ 190-300
- ERJ 190-200 LR
- ERJ 190-200 IGW
- ERJ 190-100 IGW

## 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 
 
 
FAA TYPE CERTIFICATE DATA SHEET NO. A57NM 
 
This data sheet which is part of Type Certificate No. A57NM prescribes conditions and limitations under which the product for 
which the Type Certificate was issued meets the airworthiness requirements of the US 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 Aeronáutica S.A. transferred TC No A57NM to Embraer S.A. on 
January 1, 2022. 
Embraer S.A. transferred TC No A57NM 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. 
 
I.  Model ERJ 190-100 STD (Transport Category Airplane) approved on September 2, 2005 
 
Engines Two General Electric Aircraft Engines (GE) models: CF34-10E7, CF34-10E6, CF34-10E6A1, 
CF34-10E5, CF34-10E5A1. (Engine Type Certificate E00070EN) (See Note 8). 
Auxiliary Power Unit One – Hamilton Sundstrand APS 2300 Auxiliary Power Unit. 
Fuel Specifications: 
Brazilian Specification ANP nº 1/2003 - QAV1 
ASTM D-1655 JET A or JET A1 
MIL-T-83133 JP-8 
Russian GOST 10227-86 (RT, TS-1 Premium and TS-1 Regular) 
Ukranian GSTU 320.001.499.43.011 (TS-1) 
Ukranian GSTU 320.001.499.43.007 (RT) 
 
Oil Types of approved oils for use in engines or APU are: 
Synthetic Oil conforming to MIL-PRF-23699 or MIL-PRF-7808 
 
Engine Limits Refer to AFM No. AFM-1912.  
APU Limits Maximum RPM 108%  
 Maximum EGT 717ºC (continuous) 
1032ºC (start) 
 
Other limitations as stated in Hamilton Sundstrand Document No. ESR 1235. 
 
 
 
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 
Rev. No. 23 15 9 24 11 15 12 15 12 15 24 24 24 26 24 24 26 23 26 24 
A57NM 
Revision 26 
Embraer 
ERJ 190-100 STD 
ERJ 190-100 LR 
ERJ 190-100 IGW 
ERJ 190-100 ECJ 
ERJ 190-200 STD 
ERJ 190-200 LR 
ERJ 190-200 IGW 
ERJ 190-300 
ERJ 190-400 
 
October 1, 2025

A57NM 2 of 20 
 
Airspeed Limits (I.A.S.) VMO 300 KIAS from sea level to 8,000 ft. 
increasing linearly to 320 KIAS at 10,000 ft. 
VMO 320 KIAS from 10,000 ft to 28,887 ft. 
MMO 0.82 Mach from 28,887 ft to 41,000 ft. 
VA (Maneuvering) 250 KIAS from sea level increasing linearly to 
286 KIAS at 25,590 ft., and increasing linearly to 
295 KIAS at 32,684 ft. 
VA (Maneuvering) 0.82 Mach from 32,684 ft to 41,000 ft. 
 
VFE (Flaps Extended)  Detent 1 230 KIAS 
(IAS up to 25,590 ft) Detent 2 215 KIAS 
Detent 3 200 KIAS 
Detent 4 180 KIAS 
Detent 5 180 KIAS 
Detent FULL 165 KIAS 
 
Maximum Landing Gear Operating Speed (VLO): 
Retraction 235 KIAS 
Extension265 KIAS 
Maximum Landing Gear Extended Speed (VLE): 265 KIAS 
Tire Speed 225 MPH 
Datum A perpendicular plane to the fuselage centerline, located at 14,857 mm ahead of the wing jack 
points, as illustrated below. 
 
 
 
Mean Aerodynamic Chord The MAC length is 3,682 mm. 
Leveling Means Plumb line between the points P1 and P2 located inside of the landing gear compartment on the 
 left side, as illustrated below.

3 of 20 A57NM 
 
 
 
 
 
Center of Gravity Limits Refer to AFM No. AFM-1912. 
Maximum Weights Max Ramp Weight: 
Max Takeoff Weight: 
Max Landing Weight: 
Max Zero Fuel Weight: 
105,711 lb. (47,950 kg) 
105,359 lb. (47,790 kg) 
94,798 lb. (43,000 kg) 
89,948 lb. (40,800 kg) 
Maximum Baggage Forward Cargo Compartment 
Aft Cargo Compartment 
4,078 lb. (1,850 kg) 
3,638 lb. (1,650 kg) 
 
Fuel Capacity 4,267 gallons (16,152.6 liters) in two tanks of 2,133 gallons (8,076.3 liters) each. 
Unusable fuel of 29.96 gallons (113.4 liters) (56.7 liters at 0.811 kg/liter in each tank). 
 
Minimum Crew 2 - Pilot and Copilot. 
 
Maximum Passenger Seating Capacity 110 maximum through S/N 190-00348. 
112 maximum S/N 190-00349 and on. 
 
Oil Capacity Oil capacity per Engine: 
Total: 13.8 liters (14.6 US quarts) 
Useable: 9.4 liters (9.9 US quarts) 
 
Maximum Altitudes 41,000 ft. (operating) 
10,000 ft. (takeoff and landing)* 
14,000 ft. (takeoff and landing)** 
* Standard Altitude 
** If post-mod SB 190-35-0005 
 
Control Surface Movements Ailerons 25° TE up, 15° TE down 
Elevator 25° TE up, 18° TE down 
Stabilizer 11° TE up, 4° TE down 
Rudder 31.5° right, 31.5° left 
Ground Spoiler 60° 
Outboard Spoiler  40°

A57NM 4 of 20 
 
Flap and Slat 
Detent Inboard Flap Outboard Flap Slat 1/Slat 2,3&4 
 Main/Aft Main/Aft  
0 0°/0° 0° 0°/0° 
1 7.07°/15.36° 7.04° 12°/15° 
2 10.11°/16.62° 10.06° 12°/15° 
3 20.20°/19.18° 19.99° 12°/15° 
4 20.20°/19.18° 19.99° 20°/25° 
5 20.20°/19.18° 19.99° 20°/25° 
Full 37.07°/22.01° 36.49° 20°/25° 
Deflections are in the planes normal to the hinge lines, except for the flaps, which are in 
stream wise planes normal to the wing reference plane. Deflections of a surface 
supported by another moveable surface are relative to the parent surface. Stabilizer 
deflections are relative to the airplane horizontal reference. Elevator and rudder 
maximum deflections are scheduled by the flight control system as a function of airspeed; 
the data presented herein correspond to zero airspeed. See AMM for control surface 
deflection tolerances. 
 
Serial Numbers 19000002, 19000004, 19000006 and subsequent. 
 
 
II.  Model ERJ 190-100 LR (Transport Category Airplane) approved on September 2, 2005 
 
Same as model ERJ 190-100 STD, except for the following items: 
 
Maximum Weights Max Ramp Weight: 111,245 lb. (50,460 kg) 
 Max Takeoff Weight: 110,892 lb. (50,300 kg)* 
  110,230 lb. (50,000 kg)** 
 Max Landing Weight: 94,798 lb. (43,000 kg) 
 Max Zero Fuel Weight: 89,948 lb. (40,800 kg) 
 
* Standard Weight or if post-mod SB 190-00-0003 is applied 
** If post-mod SB 190-00-0002 is applied 
Center of Gravity Limits Refer to AFM No. AFM-1912. 
III.  Model ERJ 190-100 IGW (Transport Category Airplane) - This model has two unique configurations, Passenger and Freighter 
III(a) Passenger configuration, approved on September 2, 2005 
 
Same as model ERJ 190-100 LR, except for the following items: 
Maximum Weights Max Ramp Weight: 114,552 lb. (51,960 kg) 
 Max Takeoff Weight: 114,199 lb. (51,800 kg)* 
 Max Takeoff Weight: 101,412 lb. (46,000 kg)** 
 Max Takeoff Weight: 110,231 lb. (50,000 kg)*** 
 Max Landing Weight: 97,003 lb. (44,000 kg) 
 Max Zero Fuel Weight: 90,169 lb. (40,900 kg) 
* Standard Weight or if post-mod SB 190-00-0009 or 190-00-0021 
** If post-mod SB 190-00-0008 
*** If post-mod SB 190-00-0020 
Center of Gravity Limits Refer to AFM No. AFM-1912. 
III(b) Freighter configuration (post-MOD SB 190-25-0270), approved on August 26, 2024 
 
Same as model ERJ 190-100 IGW passenger configuration, except for the following items: 
Maximum Weights Max Ramp Weight: 114,552 lb. (51,960 kg) 
 Max Takeoff Weight: 114,199 lb. (51,800 kg) 
 Max Landing Weight: 97,003 lb. (44,000 kg) 
 Max Zero Fuel Weight: 90,169 lb. (40,900 kg) 
   
Maximum Baggage Forward Cargo Compartment 
Aft Cargo Compartment 
3,483 lb. (1,580 kg) 
3,638 lb. (1,650 kg) 
   
Maximum Passenger Seating Capacity:  01 Supernumerary 
Center of Gravity Limits:               Refer to AFM No. AFM-1912.

5 of 20 A57NM 
 
IV.  Model ERJ 190-100 ECJ (Transport Category Airplane) approved on November 7, 2007 
 
Same as model ERJ 190-100 IGW, except for the following items: 
 
Engines Two General Electric Aircraft Engines (GE) models: CF34-10E7-B (Engine Type Certificate 
E00070EN) 
(See Note 8) or CF34-10E6 (See Note 14). 
Airspeed Limits (I.A.S.) VA (Maneuvering) 265 KIAS from sea level increasing linearly to 269 KIAS at 15,000 
ft., increasing linearly to 286 KIAS at 25,590 ft. and increasing 
linearly to 295 KIAS at 32,684 ft. 
Maximum Passenger Seating Capacity 19 maximum. Limited by requirement §25.807(g) Emergency Exits. 
Maximum Baggage Forward Cargo Compartment 705 lb. (320 kg) 
Aft Cargo Compartment 2,293 lb. (1,040 kg) 
 
Serial number 19000109 and subsequent. 
 
Maximum Weights Max Ramp Weight: 120,591 lb. (54,700 kg), 114,552 lb. (51,960 kg) (See Note 14) 
Max Takeoff Weight: 120,150 lb. (54,500 kg), 114,199 lb. (51,800 kg) (See Note 14) 
100,000 lb. (45,360 kg)* 
95,000 lb. (43,092 kg)** 
90,000 lb. (40,824 kg)*** 
Max Landing Weight: 100,970 lb. (45,800 kg), 97,003 lb. (44,000 kg) (See Note 14) 
Max Zero Fuel Weight: 80,467 lb. (36,500 kg), 90,169 lb. (40,900 kg) (See Note 14) 
76,212 lb. (34,570 kg)**** 
77,712 lb. (35,250 kg)***** 
* If post-mod SB 190LIN-00-0018 
** If post-mod SB 190LIN-00-0017 
*** If post-mod SB 190LIN-00-0016 
**** If post-mod SB 190LIN-00-0012 
***** If post-mod SB 190LIN-00-0007R01 
 
Fuel Capacity Maximum usable fuel: 7,194 gallons (27,232.0 liters) in two wing tanks totaling 4,268 gallons 
(16,155 liters) and in auxiliary fuel tanks totaling 2,926 gallons (11,077.0 liters). 
Maximum usable fuel: 4,267 gallons (16,152.6 liters) in two tanks of 2,133 gallons (8,076.3 liters) 
each (See Note 14) 
Unusable fuel: 43.5 gallons (165.2 liters) (72.1 liters at 0.803 kg/liter in each wing tank and 21 
liters in auxiliary tanks). 
Unusable fuel: 29.96 gallons (113.4 liters) (56.7 liters at 0.811 kg/liter in each wing tank) (See 
Note 14). 
Center of Gravity Limits  Refer to AFM No. AFM-1912. 
Maximum Altitudes 41,000 ft. (operating) 
10,000 ft. (takeoff and landing)* 
14,000 ft. (takeoff and landing)** 
* Standard Altitude 
** If post-mod SB 190LIN-35-0004 
 
 
V.  Model ERJ 190-200 STD (Transport Category Airplane) approved on June 20, 2007 
 
Same as model ERJ 190-100 LR, except for the following items: 
 
Engines Two General Electric Aircraft Engines (GE) models: CF34-10E6, CF34-10E6A1, CF34-10E5, 
CF34-10E5A1, CF34-10E7. (Engine Type Certificate E00070EN) (See Note 8). 
 
Airspeed Limits (I.A.S.) VA (Maneuvering) 253 KIAS from sea level increasing linearly to 
288 KIAS at 25,590 ft., and increasing linearly to 
295 KIAS at 32,680 ft. 
VA (Maneuvering) 0.82 Mach from 32,680 ft. to 41,000 ft.

A57NM 6 of 20 
 
Datum A perpendicular plane to the fuselage centerline, located at 15,670 mm ahead of the wing jack points, 
as illustrated below. 
 
 
Mean Aerodynamic Chord The MAC length is 3,682 mm. 
Leveling Means Plumb line between the points P1 and P2 located inside of the landing gear compartment on the 
 left side, as illustrated below. 
 
 
 
Maximum Weights Max Ramp Weight: 
Max Takeoff Weight: 
Max Landing Weight: 
Max Zero Fuel Weight: 
107,914 lb. (48,950 kg) 
107,562 lb. (48,790 kg) 
99,206 lb. (45,000 kg) 
93,695 lb. (42,500 kg) 
Center of Gravity Limits Refer to AFM No. AFM-1912.  
Maximum Baggage Forward Cargo Compartment 
Aft Cargo Compartment 
4,189 lb. (1,900 kg) 
3,968 lb. (1,800 kg) 
 
Maximum Passenger Seating Capacity 124 maximum (Note 13). 
 
Serial Numbers 19000005, 19000029 and subsequent.

7 of 20 A57NM 
 
VI.  Model ERJ 190-200 LR (Transport Category Airplane) approved on June 20, 2007 
 
Same as model ERJ 190-200 STD, except for the following items: 
Maximum Weights Max Ramp Weight: 112,324 lb. (50,950 kg) 
 Max Takeoff Weight: 111,971 lb. (50,790 kg)* 
 Max Landing Weight: 99,206 lb. (45,000 kg) 
 Max Zero Fuel Weight: 93,695 lb. (42,500 kg) 
 
Center of Gravity Limits Refer to AFM No. AFM-1912. 
 
VII.  Model ERJ 190-200 IGW (Transport Category Airplane) approved on June 20, 2007 
 
Same as model ERJ 190-200 LR, except for the following items: 
Maximum Weights Max Ramp Weight: 115,631 lb. (52,450 kg) 
 Max Takeoff Weight: 115,278 lb. (52,290 kg) 
 Max Landing Weight: 100,970 lb. (45,800 kg) 
 Max Zero Fuel Weight: 93,915 lb. (42,600 kg) 
 
VIII.  Model ERJ 190-300 (Transport Category Airplane) approved on February 28, 2018 
 
Engines Two Pratt & Whitney Engine PW1900G series, models: PW1919G and PW1922G (Engine Type 
Certificate E00090EN). 
Auxiliary Power Unit  Pratt & Whitney model APS2600[E]. 
Fuel Specifications: 
Brazilian Specification RANP37-2009 and RANP38-2011 from ANP, QAV-1 Jet Fuel 
ASTM Specification D1655, Grades JET A and JET A-1 neat (no additives); 
Specification DEF STAN 91-91 JET A-1; 
Specification MIL-DTL-83133 JP-8 (NATO codes F-34 / F-35) and JP-8+100 (NATO code 
F-37); 
Specification MIL-DTL-5624 JP-5; 
Russian Specification GOST 10227-86 grades TS-1 and RT; 
Ukrainian Specification GSTU 320.00149943.011 grade TS-1 and .007 grade RT; 
Chinese Specification GB 6537-2006, No.3. 
 
Oil Types of approved oils for use in engines or APU are: 
Synthetic Oil conforming to MIL-PRF-23699 or MIL-PRF-7808 
 
Engine Limits Refer to AFM No. AFM-5692. 
 
APU Limits Maximum RPM 108% 
 
Other limitations as stated in Hamilton Sundstrand Document No. ESR 1235. 
 
Airspeed Limits (I.A.S.) VMO (Maximum operating limit speed): 
300 KIAS from sea level to 8,000 ft. 
increasing linearly to 320 KIAS at 10,000 ft. 
320 KIAS from 10,000 ft. to 28,887 ft. 
0.82 Mach from 28,887 ft. to 41,000 ft. 
VA (Maneuvering) 265 KIAS from sea level to 15,000 ft. 
increasing linearly to 320 KIAS at 28,887 ft. 
0.82 Mach from 28,887 ft to 41,000 ft. 
 
VFE (Flaps Extended) Detent 1 230 KIAS 
(IAS up to 25,590 ft) Detent 2 215 KIAS 
 Detent 3 200 KIAS 
 Detent 4 180 KIAS 
 Detent 5 180 KIAS 
 Detent FULL 165 KIAS 
 
Maximum Landing Gear Operating Speed (VLO): 
Retraction 220 KIAS 
Extension 250 KIAS 
Maximum Landing Gear Extended Speed (VLE): 265 KIAS 
Tire Speed 225 MPH

A57NM 8 of 20 
 
Datum A perpendicular plane to the fuselage centerline, located at 13,571 mm ahead of the wing jack 
points, as illustrated below. 
 
 
 
Mean Aerodynamic Chord The MAC length is 3,665 mm. 
Leveling Means Plumb line between the points P1 and P2 located inside of the landing gear compartment on the 
 left side, as illustrated below. 
 
LEVELING OF FUSELAGE 
COORDINATE POINTS 
POINT 
P1 
P2 
X 
15,881.02 
15,881.02 
Y 
-211.00 
-211.00 
Z 
-851.49 
-1,736.42 
 
Center of Gravity Limits Refer to AFM No. AFM-5692. 
Maximum Weights Max Ramp Weight: 
Max Takeoff Weight: 
Max Landing Weight: 
124,781 lb. (56,600 kg) 
124,340 lb. (56,400 kg) 
108,136 lb. (49,050 kg) 
 Max Zero Fuel Weight: 102,876 lb. (46,700 kg) 
Maximum Baggage Forward Cargo Compartment 
Aft Cargo Compartment 
3,505 lb. (1,590 kg) 
4,210 lb. (1,910 kg) 
Fuel Capacity 4,504 gallons (17,060 liters)  
720 gallons (2,730 liters) in each LH or RH wing tank and 3064 gallons (11,600 liters) in 
center tank. 
Unusable fuel of 19.65 gallons (74.4 liters) (37.2 liters at 0.803 kg/liter in each wing 
tank).

9 of 20 A57NM 
 
Minimum Crew 2 - Pilot and Copilot. 
Maximum Passenger Seating Capacity 114 
Oil Capacity Oil capacity per Engine: 
Total: 24.4 liters (25.8 US quarts) 
Useable: 6.1 liters (6.4 US quarts) 
 
Maximum Altitudes 41,000 ft. (operating) 
14,000 ft. (takeoff and landing) 
 
Control Surface Movements Ailerons 25° TE up, 15° TE down 
Elevator 25° TE up, 18° TE down 
Stabilizer 11.6° TE up, 4.4° TE down 
Rudder 30.0° right, 30.0° left 
Ground Spoiler 60° 
Outboard Spoiler 40° 
Flap and Slat 
 
0 0.0° 0.0° 0.0° 0.0° 
1 11.2° 10.6° 7.3° 8.0° 
2 11.2° 10.6° 18.2° 20° 
3 21.5° 22.0° 18.2° 20° 
4 25.9° 26.9° 22.8° 25° 
5 25.9° 26.9° 22.8° 25° 
Full 33.0° 35.1° 22.8° 25° 
 
Deflections shown in degrees (°) are in the planes normal to hinge lines, excepting for the flaps, 
which are in stream wise planes normal to wing reference plane. 
Deflections of a surface supported at another movable surface are relative to the parent surface. 
Stabilizer defections are relative to the airplane horizontal reference. 
For tolerances, see AMM. 
 
Serial Numbers 19020009, and subsequent 
 
IX.  Model ERJ 190-400 (Transport Category Airplane) approved on April 15, 2019 
 
Same as model ERJ 190-300, except for the following items: 
 
Engines Two Pratt & Whitney Engine PW1900G series, models: PW1921G, PW1923G and 
PW1923G-A (Engine Type Certificate E00090EN). 
 
Datum A perpendicular plane to the fuselage centerline, located at 16,497 mm ahead of the wing 
jack points, as illustrated below. 
 
 
 
 
Flap setting Inboard Outboard  Slat position 
position flap flap 1 2, 3 & 4

A57NM 10 of 20 
 
Leveling Means Plumb line between the points P1 and P2 located inside of the landing gear compartment 
on the left side, as illustrated below. 
 
 
LEVELING OF FUSELAGE 
COORDINATE POINTS 
POINT 
P1 
P2 
X 
18,807.02 
18,807.02 
Y 
-211.00 
-211.00 
Z 
-851.49 
-1,736.42 
 
Maximum Weights Max Ramp Weight: 
Max Takeoff Weight: 
Max Landing Weight: 
Max Zero Fuel Weight: 
136,025 lb. (61,700 kg) 
135,584 lb. (61,500 kg) 
119,049 lb. (54,000 kg) 
114,309 lb. (51,850 kg) 
Maximum Baggage Forward Cargo Compartment 
Aft Cargo Compartment 
5,236 lb. (2,375 kg) 
5,634 lb. (2,555 kg) 
Maximum Passenger Seating Capacity 146  
 
Control Surface Movements Stabilizer 12.0° TE up, 3.5° TE down 
Serial Numbers 19020018, and subsequent

11 of 20 A57NM 
 
DATA PERTINENT TO MODELS ERJ 190-100 AND ERJ 190-200 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 14 CFR part 25, effective February 1, 1965, including the following amendments: 
- Amendments 25-1 through 25-101 in entirety; 
- Amendment 25-102, §§ 25.981(a) and (b), H25.4 only; 
- Amendments 25-103 through 25-105 in entirety; 
- Amendment 25-107, § 25.731(d) and (e); § 25.735(a) through (g), and (i) 
through (k) only; 
- Amendments 25-108 through 25-110 in entirety; 
- Amendments 25-112 through 25-114 in entirety; 
- Amendment 25-117 in entirety; and 
- Amendment 25-120 in entirety. 
Note: The ERJ 190-100 ECJ (Commercially Known as Lineage 1000) auxiliary 
fuel tanks comply with the requirement 25.981(c) of Amendment 25-102. 
 
Special Conditions: 
No. 25-296-SC, consisting of the following subjects: 
- Interaction of Systems and Structure; 
- Limit Engine Torque Loads for Sudden Engine Stoppage; 
- Control Surface Position Awareness; 
- Performance Credit for ATTCS During Go-Around; 
- High Intensity Radiated Fields (HIRF); and 
- Operations without Normal Electrical Power. 
No. 25-559-SC, Enhanced Flight-Vision System. 
No. 25-685-SC, Non-Rechargeable Lithium Batteries (Effective to design changes 
applied for after May 31, 2017. See the applicability section of this special condition for 
more information on which design changes must meet it.) 
 
For the ERJ 190-100 ECJ: 
No. 25-372-SC, Multiple Electrical/Electronic equipment bays; and 
No. 25-273-SC, Flight Accessible Class C Cargo Compartment. 
 
For the ERJ 190-100 STD, 190-100 LR, and 190-100 IGW: 
No. 25-408-SC, Seats with Non-Traditional, Large, Non-Metallic Panels. 
 
NOTE: The FAA Special Conditions referenced above may be accessed at the 
FAA’s Dynamic Regulatory System website. 
 
Equivalent Level of Safety Findings: 
- § 25.331(c)(2), Pitch Maneuver Conditions (documented in TAD ELOS 
Memo TC0099IB-T-A-10); 
- § 25.1301, 25.1309, Equipment, Systems, and Installations (documented in 
TAD ELOS Memo TC0099IB-T-S-13); 
- § 25.933(a)(1)(ii), Flight Critical Thrust Reverser (documented in TAD 
ELOS Memo TC0099IB-T-P-3 for ERJ 190-100 models and TAD ELOS 
Memo AT0286IB-T-P-22 for ERJ 190-200 models); 
- 14 CFR part 25 subparts E, F, & G requirements applicable to APU 
installations, APU Certification Rules (documented in TAD ELOS Memo 
TC0099IB-T-P-4); 
- 14 CFR part 25 Appendix I25.4(a), ATTCS - Reduction in initial power 
setting to less than 90% of takeoff thrust (documented in TAD ELOS Memo 
TC0099IB-T-F-28); 
- 14 CFR part 25 Appendix I25.5(b)(4), ATTCS - Deactivation control 
(documented in TAD ELOS Memo TC0099IB-T-P-10); 
- § 25.1305(c)(3), Digital Only Display of Turbine Engine High/Intermediate 
Pressure Rotor Speed (documented in TAD ELOS Memo TC0099IB-T-P-18);

A57NM 12 of 20 
 
- § 25.1389(b), 25.1391, 25.1393, 25.1395, Position Light Intensities 
(documented in TAD ELOS Memo TC0099IB-T-S-34); 
- § 25.831(g), Humidity Requirement (documented in TAD ELOS Memo 
TC0099IB-T-S-36); 
- § 25.811(d)(1) and (3), Emergency Exit Locator Sign (documented in TAD 
ELOS Memo TC0099IB-T-C-9) (See Note 11); 
- § 25.811(d)(1), (2), (3) and 25.812(b)(1), Emergency Exit Sign for the ERJ 
190-100 ECJ (documented in TAD ELOS Memo TD0490IB-T-C11); 
- § 25.841(b)(6), Cabin Altitude Warning System – High Altitude Takeoff and 
Landing Operations (documented in TAD ELOS Memo TD0629IB-T-S-58); 
- § 25.1443(c), Determination of Minimum Oxygen Flow for the Lavatory 
Oxygen System (documented in TAD ELOS Memo AT10108IB-T-SM-1); 
- § 25.1441(c), Crew Determination of Quantity of Oxygen in Lavatory 
Oxygen System Distributed Bottles (documented in TAD ELOS Memo 
AT10108IB-T-SM-2); 
- § 26.43, Sec. 26.45, Sec. 26.47, Three Stage Approval Process for New 
Repairs to Alteration Structure (documented in TAD ELOS Memo 
TD0756IB-T-A-1); and 
- § 26.43, Sec. 26.45, Sec. 26.47, DT data for Existing Unpublished Repairs to 
Alteration Structure (documented in TAD ELOS Memo TD0756IB-T-A-1). 
- § 25.1389(b), 25.1395 LED Position Light Intensities (documented in TAD 
ELOS Memo AT10315IB-T-S-61 
- § 25.1389(b)(1) and (b)(2), 25.1391, 25.1393 Minimum Intensity of Position 
Lights System with Protective Tape (documented in ELOS Memorandum 
AT11188IB-T-25.1389-1) 
 
NOTE: The FAA Equivalent Level of Safety Memos referenced above may be 
accessed at the FAA’s Dynamic Regulatory System website. 
 
Exemptions: 
- Exemption No. 8613, 14 CFR part 25, Section 25.901(c), Uncontrollable High 
Thrust; and 
- Exemption No. 8612, 14 CFR part 25, Section 25.841(a)(2)(i) and (ii), 
Pressurized Cabin. 
 
For the ERJ 190-100 ECJ: 
- Exemption No. 9459, 14 CFR part 25, Section 25.785(b), General 
occupant protection for occupants of multiple-place side-facing seats that 
are occupied during takeoff and landing; 
- Exemption No. 9457, 14 CFR part 25, Section 25.785(j), Firm handhold 
along each aisle; and 
- Exemption No. 9458A, 14 CFR part 25, Section 25.813(e), Prohibits 
installation of interior doors in between passenger compartments. 
 
NOTE: The FAA Exemptions referenced above may be accessed at the FAA’s 
Dynamic Regulatory System website. 
 
Optional Requirements complied with: 
- Section 25.801 Ditching; 
- Sections 25.1411, 25.1415 Safety equipment required for ditching 
certification (ERJ190-100 models 
only); 
- Section 25.1403 Wing icing detection lights; 
- Section 25.1419 Ice protection; and 
- Section 25.1421 Megaphones 
 
Part 26 of the Federal Aviation Regulations: 
Based on § 21.29(a) for new 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.

13 of 20 A57NM 
 
Environmental Standards complied with: 
- All Models: 14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 
through 36-24, Stage 3. See the appropriate FAA Approved Airplane Flight Manual for 
aircraft configurations certified as Stage 3 through amendment 36-28 and for 
applicability of Stage 4 Noise Recertification through amendment 36-31. 
- ERJ 190-100 ECJ: 14 CFR Part 36 effective December 1, 1969, including Amendments 
36-1 through 36-28, Stage 3. 
- 14 CFR Part 34 effective September 10, 1990, including all amendments effective on 
the TC date. 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations 
(see the Certification Basis) must be installed in the aircraft. The lists of all equipment as 
well as optional approved equipment are contained in the Embraer documents: 
- Type Design Standard Document for ERJ 190-100 No. 190-100TDSD; 
- Type Design Standard Document for ERJ 190-200 No. 190-200TDSD_FAA; 
and 
- Type Design Standard Document for ERJ 190-100 No. 190-100TDSD_ECJ, 
Airplane Flight Manual ANAC approved Airplane Flight Manual AFM-1912. 
Service Information Service bulletins, repair instructions (letters, drawings, specifications, forms used for 
transmitting repair descriptions, etc.), structural repair manuals, airplane flight manuals, 
vendor manuals, and overhaul and maintenance manuals that are published in the English 
language and indicate applicability to the U.S. approved type designs included in this 
Type Certificate and that include a statement “ANAC Approved” are accepted by the 
FAA and are considered “FAA Approved” (See Note 9). These approvals pertain to the 
type design only. 
 
Additionally, changes to type design that are approved by ANAC designated engineering 
representatives via ANAC form F-200-06 are also considered FAA approved (See Note 
9). 
 
DATA PERTINENT TO MODEL ERJ 190-100 IGW post-MOD SB 190-25-0270 
 
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 Airworthiness Standards for Components and Areas Not Affected by the Change: 
 
The original certification basis for the Model ERJ 190-100 IGW as shown in this TCDS 
 
Airworthiness Standards for Components and Areas Affected by the Change:  
 
14 CFR Part 25 – Based on the RBAC 21.101, the certification basis for ERJ 190-
100 Freighter Configuration is as follows: 
14 CFR Part 25 up to Amendment 146, with exceptions requested and permitted by 
14 CFR Part §21.101 for the requirements 14 CFR Part §25.611, §25.571, Appendix 
H25.4, §25.795(c)(2), §25.855, §25.869, §25.1301, §25.1302, §25.1309, 
§25.1316(*), §25.1317(*), §25.1322, §25.1353, §25.1357, §25.1435(c)(3) and 
Subpart H (§25.1701 to §25.1733) for which the baseline certification basis is 
maintained, plus additional applicable Special Conditions, Equivalent Levels of 
Safety Findings, Exemptions and Deviations. 
(*) Applicable to Air Management System and Smoke Detection System only. 
 
Equivalent Levels of Safety: 
- 14 CFR 25.812(g)(2) Emergency Lighting 
(documented in P&S ELOS Memorandum AT11666IB-T-25.812-1) 
- 14 CFR 25.855(i) Cargo or Baggage Compartments 
(documented in P&S ELOS Memorandum AT11666IB-T-25.855-1) 
Exemptions: 
- Exemption No. 22556, 14 CFR part 25, Section §25.810(a)(1), §25.813(b) 
and §25.857(e).

A57NM 14 of 20 
 
DATA PERTINENT TO MODEL ERJ 190-300 
 
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. 
 
In order for the FAA to make the finding that the first ERJ 190-300 aircraft to be 
registered in the US is in a condition for safe operation, the FAA certificating inspector 
or other authorized person must contact the Manager, Certification Program 
Management Branch, AIR-510, FAA Integrated Certificate Management Division; 2200 
South 216th Street; Des Moines, Washington 98198; telephone 1-516-228-7300, prior 
to issuance of the US airworthiness certificate to obtain the FAA Required 
Airworthiness Action List (RAAL) for the ERJ 190-300. 
 
The RAAL contains a list of type design modifications and inspections that have been 
determined by the Agência Nacional de Aviação Civil (ANAC), which is the state of 
design authority for the Embraer ERJ 190-300, to be required to correct unsafe 
conditions discovered on the original type design of the ERJ 190-300.  ANAC has 
issued Airworthiness Directives that require the accomplishment of these modifications 
and inspections to correct the identified unsafe conditions and has advised the FAA of 
this mandatory continuing airworthiness information (MCAI).  Based on this MCAI, the 
FAA has determined that the airworthiness actions identified in the ANAC ADs listed 
in Model ERJ 190-300 RAAL are required in the interest of safety and are necessary for 
this airplane to be in a condition for safe operation.  
 
Prior to the issuance of a Standard Certificate of Airworthiness (C of A) on any 
Embraer ERJ 190-300 model aircraft, all airworthiness actions shown in the Model ERJ 
190-300 RAAL must be accomplished in accordance with the compliance times listed 
in the MCAI, except as noted in the RAAL.  The MCAI listed in the RAAL are 
airworthiness limitations in addition to those listed in note 3 of this TCDS and must be 
included in the operator’s airplane maintenance or inspection program.  All inspections, 
or modifications required by the ANAC MCAI, that have surpassed the initial 
compliance time, must be accomplished prior to issuance of the C of A. 
 
The ERJ 190-300 RAAL will be finalized before the first ERJ 190-300 aircraft is 
registered in the US. 
 
Any deviation from the requirements of the MCAIs listed in the RAAL must be 
approved by the Manager of the Certification Program Management Branch, AIR-510, 
FAA Integrated Certificate Management Division.  A Notice of Policy Statement 
announcing the FAA’s policy with respect to foreign MCAI, when no aircraft of the 
affected design are currently registered in the U.S. was published in the Federal 
Register on May 1, 1998, docket 98-11648.  Additional guidance is contained in FAA 
advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, 
Propellers, and Related Products Imported into the United States. 
 
Certification Basis Airworthiness Standards for Components and Areas Not Affected by the Change: 
 
The original certification basis for the Model ERJ 190-100 IGW as shown in this TCDS 
Airworthiness Standards for Components and Areas Affected by the Change: 
14 CFR Part 25 – Airworthiness Standards: Transport Category Airplanes, effective 
February 1, 1965, including Amendments 25-1 through 25-139 and Amendment 25-141. 
Special Conditions: 
- No. 25-693-SC, Interaction of Systems and Structures 
- No. 25-643-SC, Dive Speed Definition with Speed Protection System 
- No. 25-624-SC, Landing Pitchover Condition 
- No. 25-697-SC, Design Roll Maneuver Requirement for Electronic Flight Controls 
- No. 25-408-SC, Large Surface Area Seat Panels 
- No. 25-655-SC, Flight Envelope Protection: General Limiting Requirements 
- No. 25-646-SC, Flight Envelope Protection: Pitch and Roll and High Speed Limiting 
Functions 
- No. 25-694-SC, Flight Envelope Protection: Normal Load Factor (g) Limiting 
- No. 25-699-SC, Flight Envelope Protection: High Incidence Protection and Situation

15 of 20 A57NM 
 
Awareness 
- No. 25-296-SC, Performance Credit for ATTCS during Go-Around 
- No. 25-668-SC, Operation Without Normal Electrical Power 
- No. 25-685-SC, Installed Non-Rechargeable Lithium Batteries Special Conditions 
- No. 25-689-SC, Aircraft Electronic System security Protection from Unauthorized 
External Access 
- No. 25-690-SC, Isolation of Aircraft Electronic System Security Protection from 
Unauthorized Internal Access 
- No. 25-640-SC, Electrical/Electronic Equipment Bay Fire Detection and Smoke 
Penetration 
- No. 25-639-SC, Electronic Flight Control System: Control Surface Position Awareness, 
Multiple Modes of Operation, Flight Control in all attitudes 
 
Equivalent Level of Safety Findings: 
- § 25.629, Failure Criteria considered under the Aeroelastic Stability 
Requirements of § 25.629 (documented in ELOS Memo AT10219IB-T-A-12); 
- § 25.811, Exit Handle Marking (documented in ELOS Memo AT10219IB-T- 
C-2); 
- § 25.811(d)(1) and (d)(3), Emergency Exit Locator Sign (documented in 
ELOS Memo AT10219IB-T-C-3); 
- § 25.811, Graphical/Symbolic Exit Signs (documented in ELOS Memo 
AT10219IB-T-C-8); 
- § 25.795(a)(1), Protection of flight crew compartment – Reduced Energy 
(documented in ELOS Memo AT10219IB-T-C-10); 
- §§ 25.809(b) 25.810(a)(1)(ii), Emergency Assist Means Time (documented in 
ELOS Memo AT10219IB-T-C-12); 
- § 25.813(c)(2)(i), Minor Obstruction to the Type III Exit Provided 
(documented in ELOS Memo AT10219IB-T-C-13); 
- §§ 25.904; 25.149; part 25, appendix I, paragraph I25.4(a), Performance 
Credit for Use of Automatic Power Reserve (APR) during Reduced Thrust 
Takeoffs (documented in ELOS Memo AT10219IB-T-F-13); 
- § 25.255, Electronic Flight Control System: Mistrim Maneuvering 
(documented in ELOS Memo AT10219IB-T-F-3); 
- § 25.1549(a)(b)(c), Digital only Display of turbine engine high/ pressure 
sensor, oil pressure, oil temperature and fuel flow (documented in ELOS Memo 
AT10219IB-T-P-10); 
- 14 CFR part 25 Appendix I25.5(b)(4), Lack of On/Off Switch for Automatic 
Thrust Takeoff Control System (ATTCS) (documented in ELOS Memo 
AT10219IB-T-P-12); 
- 14 CFR part 25 subparts E, F, & G requirements applicable to APU 
installations, Adoption of APU Harmonized Requirements (documented in 
ELOS Memo AT10219IB-T-P-14); 
- § 25.1141(f)(2), Engine shutoff valve indication (documented in ELOS 
Memo AT10219IB-T-P-16); 
- §§ 25.1181(a)(6) 25.1182(a), Fire Safety Requirements for the Engine Fan 
Case Compartment (documented in ELOS Memo AT10219IB-T-P-17); 
- § 25.1193(e)(3), Resistance to Fire of Nacelle Cowlings (documented in 
ELOS Memo AT10219IB-T-P-4); 
- § 25.933(a)(1)(ii), Flight Critical Thrust Reverser (documented in ELOS 
Memo AT10219IB-T-P-9); 
- §§ 25.1301, 25.1309, Equipment, Systems and Installations Requirements: 
Use of ARAC Recommendations (documented in ELOS Memo AT10219IB-T- 
S-1); 
- § 25.671(c)(2) and (c)(3), Flight Control System Failure Criteria (documented 
in ELOS Memo AT10219IB-T-S-19); 
- § 25.1443(c), Determination of Minimum Oxygen Flow to Cabin Occupant 
Masks (documented in ELOS Memo AT10219IB-T-S-24); 
- § 25.1443(c), Determination of Minimum Oxygen Flow to Lavatory Occupant 
Masks (documented in ELOS Memo AT10219IB-T-S-25); 
- § 25.841(a) and (b)(6), Cabin Pressurization - High Altitude Takeoff and 
Landing Operations up to 14,000ft (documented in ELOS Memo AT10219IB- 
T-S-28); 
- § 25.1441(c), Crew Determination of Quantity of Oxygen in Lavatory 
Oxygen System Distributed Bottles (documented in ELOS Memo AT10219IB- 
T-S-32); 
- § 25.831(g), Cabin Ventilation - humidity requirement (documented in ELOS 
Memo AT10219IB-T-S-34); 
- § 25.1438, Pneumatic Systems – Harmonized 25.1438 (documented in ELOS 
Memo AT10219IB-T-S-36); 
- § 25.841(b)(1), Combined Aircraft Pressurization Outflow and Positive

A57NM 16 of 20 
 
Pressure Differential Relief Valves (documented in ELOS Memo AT10219IB- 
T-S-37); 
- §§ 25.1389(b)(3), 25.1395, Position Lighting Systems Maximum Overlapping 
Intensity Deviations (documented in ELOS Memo AT10219IB-T-S-43); 
- §§ 25.251(b), Vibration and Buffeting Requirements for External Modifications 
(documented in ELOS Memo AT10939IB-T-EV-04); 
 
NOTE: The FAA Equivalent Level of Safety Memos referenced above may be 
accessed at the FAA’s Dynamic Regulatory System website. 
 
Exemptions: 
- Exemption No. 17561, 14 CFR part 25, Section 25.841(a)(2)(i) and (ii), Relief 
of the requirement that during a decompression the airplane cabin altitude 
cannot exceed 40,000 feet for any duration; 
- Exemption No. 17529, 14 CFR part 25, Section 25.809(a), Relief of the 
outside viewing requirements for the overwing exits 
- Exemption No. 17535, 14 CFR part 25, Section 25.901(c), Uncontrollable 
High Thrust; and 
- Exemption No. 17708, 14 CFR part 25, Section 25.981(a)(3), Alternative Fuel 
Tank Structural Lightning Protection 
 
Optional Requirements complied with: 
- Section 25.1403 Wing Icing Detection Lights; 
- Section 25.801 Ditching; 
- Sections 25.1411 and 24.1415 Safety Equipment Required for 
Ditching Certification; 
- Section 25.1419 Ice protection; and 
- Section 25.1421 Megaphones 
 
Part 26 of the Federal Aviation Regulations: 
Continued Airworthiness and Safety Improvements for Transport Category Airplanes, 
effective December 10, 2007, including Amendments 26-1 through 26-6. 
 
Environmental Standards complied with: 
- 14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through 36- 
29, Stage 4. See the appropriate FAA Approved Airplane Flight Manual for applicability 
of Stage 5 Noise Recertification through amendment 36-31. 
- 14 CFR Part 34 effective September 10, 1990, including all amendments effective on 
the amended TC date. 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations 
(see the Certification Basis) must be installed in the aircraft. The lists of all equipment as 
well as optional approved equipment are contained in the Embraer document: 
- Type Design Standard Document for ERJ 190-300- Nº196TDD300 Rev./ 
Airplane Flight Manual ANAC approved Airplane Flight Manual AFM-5692 
Service Information Service bulletins, repair instructions (letters, drawings, specifications, forms used for 
transmitting repair descriptions, etc.), structural repair manuals, airplane flight manuals, 
vendor manuals, and overhaul and maintenance manuals that are published in the English 
language and indicate applicability to the U.S. approved type designs included in this 
Type Certificate and that include a statement “ANAC Approved” are accepted by the 
FAA and are considered “FAA Approved” (See Note 9). These approvals pertain to the 
type design only. 
 
Additionally, changes to type design that are approved by ANAC designated engineering 
representatives via ANAC form F-200-06 are also considered FAA approved (See Note 
9). 
 
DATA PERTINENT TO MODEL ERJ 190-400 
 
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.

17 of 20 A57NM 
 
In order for the FAA to make the finding that the first ERJ 190-400 aircraft to be 
registered in the US is in a condition for safe operation, the FAA certificating inspector 
or other authorized person must contact the Manager, Certification Program 
Management Branch, AIR-510, FAA Integrated Certificate Management Division; 2200 
South 216th Street; Des Moines, Washington 98198; telephone 1-516-228-7300, prior 
to issuance of the US airworthiness certificate to obtain the FAA Required 
Airworthiness Action List (RAAL) for the ERJ 190-400. 
 
The RAAL contains a list of type design modifications and inspections that have been 
determined by the Agência Nacional de Aviação Civil (ANAC), which is the state of 
design authority for the Embraer ERJ 190-400, to be required to correct unsafe 
conditions discovered on the original type design of the ERJ 190-400.  ANAC has 
issued Airworthiness Directives that require the accomplishment of these modifications 
and inspections to correct the identified unsafe conditions and has advised the FAA of 
this mandatory continuing airworthiness information (MCAI).  Based on this MCAI, the 
FAA has determined that the airworthiness actions identified in the ANAC ADs listed 
in Model ERJ 190-400 RAAL are required in the interest of safety and are necessary for 
this airplane to be in a condition for safe operation.  
 
Prior to the issuance of a Standard Certificate of Airworthiness (C of A) on any 
Embraer ERJ 190-400 model aircraft, all airworthiness actions shown in the Model ERJ 
190-400 RAAL must be accomplished in accordance with the compliance times listed 
in the MCAI, except as noted in the RAAL.  The MCAI listed in the RAAL are 
airworthiness limitations in addition to those listed in note 3 of this TCDS and must be 
included in the operator’s airplane maintenance or inspection program.  All inspections, 
or modifications required by the ANAC MCAI, that have surpassed the initial 
compliance time, must be accomplished prior to issuance of the C of A. 
 
The ERJ 190-400 RAAL will be finalized before the first ERJ 190-400 aircraft is 
registered in the US. 
 
Any deviation from the requirements of the MCAIs listed in the RAAL must be 
approved by the Manager of the Certification Program Management Branch, AIR-510, 
FAA Integrated Certificate Management Division.  A Notice of Policy Statement 
announcing the FAA’s policy with respect to foreign MCAI, when no aircraft of the 
affected design are currently registered in the U.S. was published in the Federal 
Register on May 1, 1998, docket 98-11648.  Additional guidance is contained in FAA 
advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, 
Propellers, and Related Products Imported into the United States. 
 
Certification Basis Airworthiness Standards for Components and Areas Not Affected by the Change: 
 
The original certification basis for the Model ERJ 190-300 as shown in this TCDS 
Airworthiness Standards for Components and Areas Affected by the Change: 
14 CFR Part 25 – Airworthiness Standards: Transport Category Airplanes, effective 
February 1, 1965, including Amendments 25-1 through 25-139 and Amendment 25-141. 
 
Equivalent Level of Safety Findings: 
- §§ 25.1389(b)(1), (b)(2), (b)(3); 25.1391; 25.1393; 25.1395, Position Lighting Systems 
Maximum Overlapping Intensity Deviations (documented in Transport Standards Branch 
ELOS Memorandum AT10316IB-T-SE-14) 
- §§ 25.251(b), Vibration and Buffeting Requirements for External Modifications (documented 
in ELOS Memo AT10939IB-T-EV-04); 
 
NOTE: The FAA Equivalent Level of Safety Memo referenced above may be 
accessed at the FAA’s Dynamic Regulatory System website. 
 
Optional Requirements complied with: 
- Section 25.1403 Wing Icing Detection Lights; 
- Section 25.801 Ditching; 
- Sections 25.1411 and 25.1415 Safety Equipment Required for 
Ditching Certification; 
- Section 25.1419 Ice protection; and 
- Section 25.1421 Megaphones 
 
Part 26 of the Federal Aviation Regulations: 
Continued Airworthiness and Safety Improvements for Transport Category Airplanes,

A57NM 18 of 20 
 
effective December 10, 2007, including Amendments 26-1 through 26-6. 
 
Environmental Standards complied with: 
- 14 CFR Part 36 effective December 1, 1969, including Amendments 36-1 through 36- 
30, Stage 4. See the appropriate FAA Approved Airplane Flight Manual for applicability 
of Stage 5 Noise Recertification through amendment 36-31. 
- “No Emissions Change” in accordance with §21.93(c) 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations 
(see the Certification Basis) must be installed in the aircraft. The lists of all equipment as 
well as optional approved equipment are contained in the Embraer document: 
- Type Design Standard Document for ERJ 190-400 – Report Nº 196TDD400 
Rev. B 
 
Airplane Flight Manual ANAC approved Airplane Flight Manual AFM-5692 
 
Service Information Service bulletins, repair instructions (letters, drawings, specifications, forms used for 
transmitting repair descriptions, etc.), structural repair manuals, airplane flight manuals, 
vendor manuals, and overhaul and maintenance manuals that are published in the 
English language and indicate applicability to the U.S. approved type designs included 
in this Type Certificate and that include a statement “ANAC Approved” are accepted by 
the FAA and are considered “FAA Approved” (See Note 9). These approvals pertain to 
the type design only. 
 
Additionally, changes to type design that are approved by ANAC designated engineering 
representatives via ANAC form F-200-06 are also considered FAA approved (See Note 
9). 
 
NOTES: 
 
NOTE 1: Weight and balance. Current weight and balance report including a form of weight and list of 
equipment included in certificated empty weight and loading instructions must be provided for each 
aircraft at the time of original certification. 
 
The certificated basic empty weight and corresponding center of gravity location must include the 
total engine oil, hydraulic fluid and unusable fuel. 
NOTE 2: All placards required by either FAA Approved Airplane Flight Manual, the applicable operating 
rules, or the Certification Basis must be installed in the airplane. 
 
NOTE 3: For the ERJ 190-100 and -200 models, excluding the ERJ 190-100 ECJ, the mandatory systems 
certification maintenance requirements, raised from the safety analysis, are listed in the “Appendix 
A Part 1 – Certification Maintenance Requirements (CMR)” of the document MRB Report P/N 
1928. The mandatory structure certification maintenance requirements, raised from the damage 
tolerance analysis, are listed in the “Appendix A Part 2 - Airworthiness Limitation Inspections 
(ALI) - Structures” of the document MRB Report P/N 1928. The list of the tasks raised from the 
compliance with the RBHA/FAR 25-981 Amdt. 102 (a) and (b) is provided in the “Appendix A Part 
3 – Fuel System Limitation Items (FSL)” of the document MRB Report P/N 1928. 
 
For the ERJ 190-100 ECJ model, the Appendix A (Part 1, 2, 3 and 4) of the Maintenance Planning 
Guide (MPG-2928) document must be considered as reference for mandatory maintenance 
requirements mentioned above. 
 
For the ERJ 190-300 model, the Airworthiness Limitations Section is found in Appendix A (Part 1, 
2, 3, 4 and 5) of the document MRB Report P/N 5881, revision 0 or subsequent ANAC approved 
revision. For the ERJ 190-400 model, the Airworthiness Limitations Section is found in Appendix 
A (Part 1, 2, 3, 4 and 5) of the document MRB Report P/N 5881, revision 1 or subsequent ANAC 
approved revision. 
 
The list of the life-limited components is provided in the “Appendix A Part 4 – Life - Limited Items 
(LLI) of the document MRB Report 1928 for the 190-100 and 190-200 models (excluding 190-100 
ECJ), MPG 2928 for the 190-100 ECJ model, and MRB Report 5881 for the 190-300 and 190-400 
model. 
 
The Structures Repair Manual P/N 1929 is applicable to all ERJ 190-100 and ERJ 190-200, except 
for the ERJ 190-100 ECJ model, and it is approved and controlled by ANAC. The Structures 
Repair Manual P/N 2773 is applicable to model ERJ 190-100 ECJ. The Structures Repair Manual 
P/N 6736 is applicable to the ERJ 190-300 and ERJ 190-400 models and it is approved and 
controlled by ANAC. An approval statement is stamped in each Service Bulletin (See Note 9).

19 of 20 A57NM 
 
For the ERJ 190-300 and ERJ 190-400, the airworthiness corrective actions required by the 
ANAC ADs are listed in the ERJ 190-300/ERJ 190-400 RAAL. 
 
NOTE 4: The systems containing User Modifiable Data are: 
- User Partition of the Owner Requirements Table (ORT) of the SATCOM (Satellite 
Communication System); 
- Airline Modifiable Information (AMI) of the Communication Management Function (CMF); 
- System Setting Data - Airline Operational Data (APM) System Setting Data (Airline 
Operational Data); and 
- User Application of the Aircraft Condition Monitoring Function (ACMF). 
User Modifiable Data is not approved as part of the type design. 
NOTE 5: Any new interior configuration affecting the cockpit door access area, including adjacent 
structures such as galleys and wardrobes, must be submitted for FAA Aircraft Certification Office 
(ACO) approval, specifically for compliance with 14 CFR 25.809(b). FAA ACO’s should 
coordinate any such changes with the TC issuing office (ANM-116). 
 
NOTE 6: The Model ERJ 190-100 xx and ERJ 190-200 xx are often referred to in Embraer marketing 
literature as the “Embraer 190 xx” and “Embraer 195 xx,” respectively, with the appropriate model 
(LR, STD, etc.) substituted for the “xx”. These names are strictly marketing designations and are 
not part of the official model designations. The exceptions to this rule are the Models ERJ 190-100 
IGW and ERJ 190-200 IGW, which have been given the marketing designation “Embraer 190 AR” 
and “Embraer 195 AR,” respectively. 
The ERJ 190-100 ECJ model is frequently mentioned in Embraer publicity literature as 
“Lineage1000.” 
The ERJ 190-300 model is often mentioned in Embraer publicity literature as the “Embraer 190E2.” 
The ERJ 190-400 model is often mentioned in Embraer publicity literature as the “Embraer 195E2.” 
 
NOTE 7: As stated in Exemption No. 8613 (ERJ 190), the FAA has concluded that the occurrence of any 
uncontrollable high thrust failure condition or any of the associated causal failures listed below, are 
reportable under §§ 121.703 (c), 125.409 (c), and 135.415(c): 
 
- FADEC – Full Authority Digital Engine Control; 
- TCQ – Thrust Control Quadrant; and 
- FMU – Fuel Metering Unit. 
 
NOTE 8: The CF34-10E engines configuration, according to the designation presented in the Engine Parts 
List, must follow the suffix Gxx. For the ERJ 190-100 models, the following designation list is 
approved for operation (mixing of different engine configurations on the same airplane is permitted 
for the listed trios only): 
− CF34-10E6G03, CF34-10E6G05 and CF34-10E6G07 
− CF34-10E6A1G03, CF34-10E6A1G05 and CF34-10E6A1G07 
− CF34-10E5G03, CF34-10E5G05 and CF34-10E5G07 
− CF34-10E5A1G03, CF34-10E5A1G05 and CF34-10E5A1G07 
− CF34-10E7-BG03, CF34-10E7-BG05 e CF34-10E7-BG07. 
 
For the ERJ 190-200 models, the following designation list is approved for operation (mixing of 
different engine configurations on the same airplane is permitted for the listed pairs only): 
− CF34-10E6G03 and CF34-10E6G05 
− CF34-10E6A1G03 and CF34-10E6A1G05 
− CF34-10E5G03 and CF34-10E5G05 
− CF34-10E5A1G03 and CF34-10E5A1G05 
− CF34-10E7G03 and CF34-10E7G05. 
 
Engine configuration part numbers ECP 2041M42P02, -P06, -P08, and -P09 are not permitted on 
any ERJ 190 CF34-10E engines configuration. 
 
NOTE 9: The “Agência Nacional de Aviação Civil” - ANAC (National Agency of Civil Aviation) took over 
responsibility for Brazilian civil aircraft certification on March 21, 2006. Approvals made prior to 
that date will reference the CTA as the responsible Brazilian aviation authority. 
 
NOTE 10: For the ERJ 190-100 ECJ model, the compliance requirements of cabin safety will be demonstrated 
on interior installation and certification of aircraft. 
 
NOTE 11: Emergency Exit Locator Sign ELOS is not applicable for ERJ 190-100 ECJ. 
 
NOTE 12: The type design reliability and performance of the Model 190-100 STD, -100 LR and -100 IGW 
airplanes have been approved in accordance with 14 CFR 25.1535 and found suitable for extended

A57NM 20 of 20 
 
operations (ETOPS) up to 120 minutes when operated and maintained in accordance with the ERJ 
190 Configuration, Maintenance and Procedures (CMP) document, CMP-2925. For the Model 
ERJ 190-100 ECJ the ERJ 190 CMP document, CMP-2927. This finding does not constitute 
approval to conduct ETOPS operations. 
 
 The type design reliability and performance of the Model 190-300 and -400 airplanes have been 
approved in accordance with 14 CFR 25.1535 and found suitable for extended operations 
(ETOPS) up to 120 minutes when operated and maintained in accordance with the ERJ 190 CMP 
document, CMP-8507. This finding does not constitute approval to conduct ETOPS operations. 
 
NOTE 13: For the ERJ 190-200 models, the maximum passenger limit is a total of 124 passengers with a 
maximum of 72 passengers seats located aft of the centerline of the overwing exits. 
 
NOTE 14: Data applicable only to airplanes S/N 19000109 to 19000225 without SB190LIN-28-0011 
incorporated. 
 
NOTE 15: For ERJ 190-100 and ERJ 190-200 models, initial airworthiness requirements for operation in 
Reduced Vertical Separation Minimum (RVSM) airspace have been met. Refer to AFM No. 
AFM- 1912. 
 For the ERJ 190-300 and ERJ 190-400 models, RVSM operation is limited to 50 aircraft 
from S/N 19020009. 
 Each operator must obtain RVSM operating approval directly from the FAA. 
  
NOTE 16: The ERJ 190-100 IGW is converted to freighter configuration by application of Embraer 
Service Bulletin (SB) nº SB190-25-0270 (aircraft conversion to full cargo configuration). 
 
NOTE 17: The ERJ190-100 IGW post-MOD SB190-25-0270 does not constitute a new model, and it 
can be referred to in marketing literature as “EMBRAER 190F”, “E190F”, “E-Freighter”. 
 
NOTE 18: To carry cargo on ERJ190-100 IGW post-MOD SB190-25-0270, an FAA approved Cargo 
Loading System must be installed, which is not part of this TC. 
 
 ...END...
```

## ADs (86, 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 2026-10-01](https://openairdocs.org/ad/2026-10-01): Pneumatic · Embraer ERJ 190-100 ECJ. Effective Jun 26, 2026
- [AD 2026-02-11](https://openairdocs.org/ad/2026-02-11): Navigation · Embraer ERJ 190-300 and ERJ 190-400. Effective Feb 17, 2026
- [AD 2025-14-05](https://openairdocs.org/ad/2025-14-05): Nacelles/Pylons · Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE and 12 more. Effective Aug 25, 2025
- [AD 2025-06-09](https://openairdocs.org/ad/2025-06-09): Landing gear · Embraer ERJ 190-300 and ERJ 190-400. Effective Apr 14, 2025
- [AD 2024-25-01](https://openairdocs.org/ad/2024-25-01): Flight Controls · Embraer ERJ 190-400. Effective Jan 29, 2025
- [AD 2024-25-04](https://openairdocs.org/ad/2024-25-04): Flight Controls · Embraer ERJ 190-300. Effective Jan 29, 2025
- [AD 2024-20-06](https://openairdocs.org/ad/2024-20-06): Fuel · Embraer ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD and 3 more. Effective Nov 29, 2024
- [AD 2024-17-03](https://openairdocs.org/ad/2024-17-03): Time Limits/Maintenance Checks · Embraer ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 ECJ and 4 more. Effective Nov 4, 2024
- [AD 2023-26-01](https://openairdocs.org/ad/2023-26-01): Navigation · Embraer ERJ 190-300 and ERJ 190-400. Effective Jan 18, 2024
- [AD 2023-21-11](https://openairdocs.org/ad/2023-21-11): Wings · Embraer ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW and 3 more. Effective Dec 26, 2023
- [AD 2023-15-02](https://openairdocs.org/ad/2023-15-02): Landing gear · Embraer ERJ 190-300 and ERJ 190-400. Effective Aug 18, 2023
- [AD 2023-15-04](https://openairdocs.org/ad/2023-15-04): Navigation · Embraer ERJ 190-300 and ERJ 190-400. Effective Aug 18, 2023
- [AD 2023-10-01](https://openairdocs.org/ad/2023-10-01): Flight Controls · Embraer ERJ 190-300 and ERJ 190-400. Effective Jun 20, 2023
- [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 2023-03-16](https://openairdocs.org/ad/2023-03-16): Landing gear · Embraer ERJ 190-300. Effective Mar 20, 2023
- [AD 2022-27-06](https://openairdocs.org/ad/2022-27-06): Instruments · Embraer ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 ECJ and 4 more. Effective Feb 16, 2023
- [AD 2022-25-10](https://openairdocs.org/ad/2022-25-10): Nacelles/pylons · Embraer ERJ 190-300 and ERJ 190-400. Effective Jan 6, 2023
- [AD 2022-24-16](https://openairdocs.org/ad/2022-24-16): Doors · Embraer ERJ 190-300 and ERJ 190-400. Effective Dec 29, 2022
- [AD 2022-12-11](https://openairdocs.org/ad/2022-12-11): Time Limits/Maintenance Checks, Landing Gear · Embraer ERJ 190-100 ECJ. Effective Aug 31, 2022
- [AD 2022-16-01](https://openairdocs.org/ad/2022-16-01): Windows · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Aug 15, 2022
- [AD 2022-09-05](https://openairdocs.org/ad/2022-09-05): Hydraulic power · Embraer ERJ 190-300 and ERJ 190-400. Effective May 27, 2022
- [AD 2021-25-02](https://openairdocs.org/ad/2021-25-02): Nacelles/pylons · Yaborã Indústria Aeronáutica ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 ECJ and 4 more. Effective Jan 20, 2022
- [AD 2021-18-03](https://openairdocs.org/ad/2021-18-03): Turbine/turboprop engine · Yaborã Indústria Aeronáutica ERJ 190-400. Effective Oct 1, 2021
- [AD 2021-12-14](https://openairdocs.org/ad/2021-12-14): Electrical power · Yaborã Indústria Aeronáutica ERJ 190-300 and ERJ 190-400. Effective Jul 26, 2021
- [AD 2020-25-08](https://openairdocs.org/ad/2020-25-08): Flight controls · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Jan 21, 2021
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2020-07-21](https://openairdocs.org/ad/2020-07-21): Landing gear · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective May 26, 2020
- [AD 2020-04-16](https://openairdocs.org/ad/2020-04-16): Wings · Yaborã Indústria Aeronáutica ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD and 3 more. Effective May 7, 2020
- [AD 2020-05-21](https://openairdocs.org/ad/2020-05-21): Indicating/recording systems · Yaborã Indústria Aeronáutica ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR and 4 more. Effective Apr 24, 2020
- [AD 2019-19-03](https://openairdocs.org/ad/2019-19-03): Fuselage · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Oct 31, 2019
- [AD 2019-03-21](https://openairdocs.org/ad/2019-03-21): Landing Gear · Embraer ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD and 3 more. Effective Apr 2, 2019
- [AD 2017-21-09](https://openairdocs.org/ad/2017-21-09): Fuselage · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 10 more. Effective Nov 27, 2017
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2016-12-14](https://openairdocs.org/ad/2016-12-14): Pneumatic · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 10 more. Effective Jul 27, 2016
- [AD 2013-25-04](https://openairdocs.org/ad/2013-25-04): Equipment/Furnishings · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Feb 10, 2014
- [AD 2013-16-22](https://openairdocs.org/ad/2013-16-22): Fuselage · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Sep 27, 2013
- [AD 2013-11-17](https://openairdocs.org/ad/2013-11-17): Pneumatic · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Aug 6, 2013
- [AD 2013-11-07](https://openairdocs.org/ad/2013-11-07): Landing gear · Embraer ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR and 4 more. Effective Jul 9, 2013
- [AD 2013-05-12](https://openairdocs.org/ad/2013-05-12): Fire Protection · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective May 3, 2013
- [AD 2013-03-13](https://openairdocs.org/ad/2013-03-13): Doors · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Mar 19, 2013
- [AD 2012-16-09](https://openairdocs.org/ad/2012-16-09): Air Conditioning · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Sep 21, 2012
- [AD 2012-15-03](https://openairdocs.org/ad/2012-15-03): Landing Gear · Embraer ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR and 4 more. Effective Sep 4, 2012
- [AD 2011-18-04](https://openairdocs.org/ad/2011-18-04): Equipment/furnishings · Embraer - Empresa Brasileira de Aeronautica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Oct 14, 2011
- [AD 2011-18-14](https://openairdocs.org/ad/2011-18-14): Nacelles/Pylons · Embraer - Empresa Brasileira de Aeronautica ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR and 4 more. Effective Oct 14, 2011
- [AD 2011-10-03](https://openairdocs.org/ad/2011-10-03): Fuselage · Embraer - Empresa Brasileira de Aeronautica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 10 more. Effective Jun 15, 2011
- [AD 2011-08-08](https://openairdocs.org/ad/2011-08-08): Electrical power · Embraer - Empresa Brasileira de Aeronautica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective May 18, 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 2010-18-04](https://openairdocs.org/ad/2010-18-04): Fuselage · Embraer - Empresa Brasileira de Aeronautica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 10 more. Effective Sep 29, 2010
- [AD 2010-10-07](https://openairdocs.org/ad/2010-10-07): Wings · Embraer - Empresa Brasileira de Aeronautica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 11 more. Effective Jun 17, 2010

All 86: https://openairdocs.org/tcds/A57NM/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw): 26 aircraft (registry code 3260408)
- [Embraer Empresa Brasileira De ERJ 190-100 IGW](https://openairdocs.org/model/embraer-empresa-brasileira-de-erj-190-100-igw): 8 aircraft (registry code 3260424)
- [Embraer S A ERJ 190-100 LR](https://openairdocs.org/model/embraer-s-a-erj-190-100-lr): 5 aircraft (registry code 3260409)
- [Embraer ERJ 190-100 ECJ](https://openairdocs.org/model/embraer-erj-190-100-ecj): 4 aircraft (registry code 3260413)
- [Embraer ERJ 190-200 LR](https://openairdocs.org/model/embraer-erj-190-200-lr): 3 aircraft (registry code 3260520)
- [Embraer S A ERJ 190-200 IGW](https://openairdocs.org/model/embraer-s-a-erj-190-200-igw): 2 aircraft (registry code 3260920)
- [Embraer Empresa Brasileira De ERJ 190-100 ECJ](https://openairdocs.org/model/embraer-empresa-brasileira-de-erj-190-100-ecj): 1 aircraft (registry code 3260411)
- [Empresa Brasileira De Aero S A ERJ 190-200 LR](https://openairdocs.org/model/empresa-brasileira-de-aero-s-a-erj-190-200-lr): 1 aircraft (registry code 3260960)
- [Embraer Empresa Brasileira De ERJ 190-200 IGW](https://openairdocs.org/model/embraer-empresa-brasileira-de-erj-190-200-igw): 0 aircraft (registry code 3260950)
- [Embraer S A ERG 190-100](https://openairdocs.org/model/embraer-s-a-erg-190-100): 0 aircraft (registry code 3260901)
- [Embraer S A ERJ 190-100 ECJ](https://openairdocs.org/model/embraer-s-a-erj-190-100-ecj): 0 aircraft (registry code 3260919)
- [Embraer S A ERJ 190-100 IGW](https://openairdocs.org/model/embraer-s-a-erj-190-100-igw): 0 aircraft (registry code 3260915)
- [Embraer-Empresa Brasileira De ERJ 190 AR](https://openairdocs.org/model/embraer-empresa-brasileira-de-erj-190-ar): 0 aircraft (registry code 3260419)
- [Yabora Industria Aeronautica S ERJ 190-100 IGW](https://openairdocs.org/model/yabora-industria-aeronautica-s-erj-190-100-igw): 0 aircraft (registry code 3260998)

## STCs approved under this data sheet (77, first 50)

- [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 ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc.
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc.
- [STC ST12354IB](https://openairdocs.org/stc/ST12354IB): Installation of Starlink Aviation In-Flight Connectivity System. PMV Engineering
- [STC ST03133CH](https://openairdocs.org/stc/ST03133CH): Installation of Printed Advertising onto cabin interior surfaces. Atin OOH LLC
- [STC ST04525CH](https://openairdocs.org/stc/ST04525CH): Installation of a Video Server and Wireless Access Points in accordance with Row 44 Master Data Index Listing, Document No. RWR100-0001-00, Revision IR, dated April 16, 2021 or later FAA approved revision.. Anuvu IFC Corporation
- [STC ST12238IB](https://openairdocs.org/stc/ST12238IB): Installation of cabin system upgrades, comprising Photoluminescent Floor Path Marking (PLFPM). Cobalt Aerospace Limited
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST01989LA-D](https://openairdocs.org/stc/ST01989LA-D): Adjustable Cargo Net Installations.. Safran Cabin Inc.
- [STC ST02003LA](https://openairdocs.org/stc/ST02003LA): C&D Zodiac, Inc. Interior Installations and Modifications. Safran Cabin Inc.
- [STC ST02391LA](https://openairdocs.org/stc/ST02391LA): Interior Installations and Modifications. Safran Cabin Inc.
- [STC ST02565LA](https://openairdocs.org/stc/ST02565LA): Interior installations and modifications. Safran Cabin Inc.
- [STC ST02568LA](https://openairdocs.org/stc/ST02568LA): Interior Installations and Modifications. Safran Cabin Inc.
- [STC ST02571LA](https://openairdocs.org/stc/ST02571LA): Interior Installation and Modifications. Safran Cabin Inc.
- [STC ST12056IB](https://openairdocs.org/stc/ST12056IB): The Manufacture and Installation of External Printed Aircraft Graphics Film. Libellule Monde Inc.
- [STC ST02534SE](https://openairdocs.org/stc/ST02534SE): Installation and maintenance of a Crane Aerospace & Electronics Tire Pressure Sensor Assembly. ELDEC Corporation
- [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 ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc.
- [STC ST11852IB](https://openairdocs.org/stc/ST11852IB): Installation of mounting device and power supply connection for PIVOT EFB. SABENA TECHNICS BGC
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST04799NY](https://openairdocs.org/stc/ST04799NY): Installation of a Panasonic Avionics In-Flight Entertainment System. Delta Engineering Corporation
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04104NY](https://openairdocs.org/stc/ST04104NY): Installation of provisions for an Intelsat 2Ku radome/antenna. Delta Engineering Corporation
- [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 ST04253NY](https://openairdocs.org/stc/ST04253NY): 124 PAX PASSENGER SEAT RE-PITCH AND CABINET INSTALLATION. ALOFT AeroArchitects
- [STC ST03407NY](https://openairdocs.org/stc/ST03407NY): Installation of a gogo Cabin Connectivity System. Delta Engineering Corporation
- [STC ST04535AT](https://openairdocs.org/stc/ST04535AT): Installation of the CES-170 Emergency Light Power Unit (ELPU). Chippewa Aerospace Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC
d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc.
- [STC ST04116CH](https://openairdocs.org/stc/ST04116CH): Installation of 802.11 ac protocol Cabin Wireless Access Points (acWAP) retrofit for existing Cabin Wireless Access Points. Intelsat Inflight LLC
- [STC ST03177AT](https://openairdocs.org/stc/ST03177AT): Installation of a LIVE TV LTV 2000 In-Flight Entertainment System. Thales Avionics Inc
- [STC ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [STC ST04395NY](https://openairdocs.org/stc/ST04395NY): Change to introduce a modification to Zodiac Standard 'Elite' Double seats. 365 Aerospace Ltd Aerospace Logistics Centre
- [STC ST01000DE](https://openairdocs.org/stc/ST01000DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery. MarathonNorco Aerospace Inc
- [STC ST02700LA](https://openairdocs.org/stc/ST02700LA): Installation of Toilet Assembly. Monogram Systems
- [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 ST09898AC](https://openairdocs.org/stc/ST09898AC): Installation of alternative/replacement trolleys and container; trolley part numbers. Driessen Aircraft Interior Systems USA Inc
- [STC ST04271NY](https://openairdocs.org/stc/ST04271NY): Installation of the Automated Flight Information Reporting System (AFIRS) 228. FLYHT Aerospace Solutions Ltd
- [STC ST04435AT](https://openairdocs.org/stc/ST04435AT): Installation of Astronics Passenger In-Seat Power in the Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 Series Aircraft. Chippewa Aerospace Inc
- [STC ST04361AT](https://openairdocs.org/stc/ST04361AT): Installation of a ADS-B Out. Chippewa Aerospace Inc
- [STC ST03904AT](https://openairdocs.org/stc/ST03904AT): Installation of an AirCell Airborne Wireless Wi-Fi System. Chippewa Aerospace Inc
- [STC ST02580SE](https://openairdocs.org/stc/ST02580SE): Installation of two Securaplane Model 9750W0360-12 24 VDC/28 Ah sealed lead acid batteries. Securaplane Technologies

All 77: https://openairdocs.org/tcds/A57NM/stcs.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.