# TCDS TC00062IB: Embraer S.A.

- Type: Type certificate data sheet
- Status: Current
- Holder: Embraer S.A.
- Revision: 17
- Revised: August 25, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25, Part 21
- Registered aircraft: 332, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/e5/b7/e5b7dfc3553e595e4a3aa044a717a3ae0ed7871800552ec3050e51a94c64f4f7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135852061820260825183111.0001
- Page: https://openairdocs.org/tcds/TC00062IB

## Models (2)

As the data sheet lists them.

- EMB-550
- EMB-545

## What the data sheet says

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

```text
Page No. 1 2 3 4 5 6 7 8 9  
Rev. No. 14 10 10 7 14 12 7 10 17  
 
DEPARTMENT OF TRANSPORATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
 
 
 
 
 
 
 
 
 
TYPE CERTIFICATE DATA SHEET NO. TC00062IB 
 
This data sheet which is part of  Type Certificate No. TC00062IB prescribes conditions and limitations under 
which the product for which the type certificate was issued meets the airworthiness requirements of Title 14 
of the Code of Federal Regulations. 
 
Type Certificate Holder Embraer S.A. 
Av. Brigadeiro Faria Lima, 2.170 
12227-901 -- São José dos Campos -- SP 
Brazil 
 
 
I.  Model EMB-550, (Transport Category), (See certification basis) Approved October 21, 2014 
 
II.  Model EMB-545, (Transport Category), (See certification basis) Approved August 26, 2015 
 
Engines: Two Honeywell AS907-3-1E 
 Engine Type certificate E00010LA 
Fuel: Fuels conforming to: 
ASTM D1655 grade JET A and JET A1 
MIL-DTL-83133 Turbine Fuels, Aviation, Kerosene Types, NATO F-34 
(JP-8), NATO F-35 and JP-8+100 
Brazilian Specification for Aviation Turbine Fuels CNP08 or superseding 
specification QAV-1 
No. 3 Jet Fuel (Peoples Republic of China Specification GB6537-94 or 
superseding specification) 
Defense Standard DEF STAN 91-91 AVTUR 
 EMB-550 approved additives are: 
Corrosion inhibitor per MIL-I-25017 or similar 
 
Anti-fungi additives: 
 1. Biobor JF 
 2. Kathan FP 1.5 (Rhom & Hass) 
 
Icing inhibitors (FSII) conforming to MIL-I-27686 (NATO S-748), ASTM-
D4171, MIL-I-85470A, GOST 8313-88 (Russia) or similar. 
 Note these are different than the approved additives in the Honeywell engine 
installation manual 24-IM-8030. 
 
TC00062IB 
Revision 17 
Embraer 
 
EMB-545 
EMB-550 
 
August 25, 2026

TC00062IB Page 2 of 9 Rev 17  
. 
Engine Limits: 
EMB-550 
Static thrust lb, ambient temperature, sea level 
Max Continuous Takeoff 
 
7,335 at ISA +22.5ºC 7,638 at ISA + 18ºC 
 
EMB-545 
Static thrust lb, ambient temperature, sea level 
Max Continuous Takeoff 
6,855 at ISA +22.5ºC 7,138 at ISA + 18ºC 
 
 For engine operating limits see the FAA approved Airplane Flight Manual. 
Airspeed Limits: VMO/MMO = 320 KIAS / 0.83M 
 For other airspeed limits, including the performance changes for the 
EMB-550 MOD, see the FAA approved Airplane Flight Manual. 
Center of Gravity Range: See the FAA Approved Airplane Flight Manual 
Empty Weight CG Range: None 
 
Datum: EMB-550: The Airplane Datum is a plane, perpendicular to the fuselage 
centerline, located 429.92 inches ahead of the wing jack points. 
 EMB-545: The Airplane Datum is a plane, perpendicular to the fuselage centerline, located 404.4 inches ahead of the wing jack points 
Leveling Means: EMB-550: Located in the main door region on the omega beam between 
frames 11 and 12 (see the Airplane Maintenance Manual Part II Chapter 8 
for further information) 
 EMB-545: Located in the main door region on the omega beam between 
frames 10 and 11 (see the Airplane Maintenance Manual Part II Chapter 8 
for further information) 
Maximum Weights:   
 
 EMB-550 EMB-545 
 Without 
SB 550-042-0004 
With 
SB 550-042-0004 
MOD 
(See Note 4) 
Without 
SB 550-042-0004 
With 
SB 550-042-0004 
MOD 
(See Note 4) 
Max Ramp Weight 38,096 lb 
(17,280 kg) 
38,536 lb 
(17,480 kg) 
42,990 lb 
(19,500 kg) 
35,406 lb 
(16,060 kg) 
35,891 lb 
(16,280 kg) 
37,699 lb 
(17,100 kg) 
Max Takeoff 
Weight 
37,920 lb 
(17,200 kg) 
38,360 lb 
(17,400 kg) 
42,857 lb 
(19,440 kg) 
35,274 lb 
(16,000 kg) 
35,758 lb 
(16,220 kg) 
37,567 lb 
(17,040 kg) 
Max Landing 
Weight 
34,128 lb 
(15,480 kg) 
34,524 lb 
(15,660 kg) 
37,478 lb 
(17,000 kg) 
32,518 lb 
(14,750 kg) 
32,518 lb 
(14,750 kg) 
34,172 lb 
(15,500 kg) 
Max Zero Fuel 
Weight 
 
 
 
 
26,500 lb 
(12,020 kg) 
 
 
26,500 lb 
(12,020 kg) 
 
28,660 lb 
(13,000 kg) 
 
25,904 lb 
(11,750 kg) 
 
25,904 lb 
(11,750 kg) 
25,959 lb 
(11,775 kg) 
26,510* lb 
(12,025 kg) 
* If SB 550-00-0016 is installed or with an equivalent modification factory incorporated

TC00062IB Page 3 of 9 Rev 17  
. 
 
 
Minimum Crew: Two pilots 
 
Number of Passengers: EMB-550: Limited to 12 for step-down distance with the Type III exit. 
EMB-545: Limited to 9 for step-down distance with the Type III exit. 
 
Maximum Compartment Weights: 
EMB-550 
Wardrobe 88 lb (153.15 inches aft of datum) 
Internal Stowage Compartment 330 lb (452.76 inches aft of datum) 
External Cargo Compartment 881 lb (543.30 inches aft of datum) 
 
EMB-545 
Wardrobe 88 lb (153.15 inches aft of datum) 
Internal Stowage Compartment 330 lb (409.45 inches aft of datum) 
External Cargo Compartment 881 lb (500 inches aft of datum) 
 
Fuel Capacity: 
 
 
Total Fuel Capacity Total Usable Fuel Total Unusable Fuel 
EMB-550 
except for EMB-550 
MOD (see Note 4) 
13,146 lbs 
6,573 lbs each in two wing 
tanks at +367.72 in. 
 
13,058 lbs 
6,529 lbs each 
 
88.6 lbs 
SEE NOTE 1 
 
 
EMB-550 MOD 
(see Note 4) 
16,265 lbs 
6,573 lbs each in two wing 
tanks at +356.50 in. 
1,432 lbs in a forward tank at 
+279.53 in. and 1,687 lbs in 
a ventral tank at +462.60 in. 
16,145 lbs 
6,529 lbs each wing 
tank 
1,432 lbs aft tank 
1,655 lbs ventral tank 
 
 
120.3 lbs 
SEE NOTE 1 
EMB-545 
post-SB 550-28-0002 
(or equivalent 
factoryincorporated 
modification) except for 
EMB-545 
MOD (see Note 4) 
 
12,940 lbs 
6,470 lbs each in two wing 
tanks at +339.5 in. 
 
 
11,925 lbs 
5,962.5 lbs each 
 
 
88.6 lbs 
SEE NOTE 1 
EMB-545 
pre-SB 550-28-0002 
except for EMB-545 
MOD (see Note 4) 
10,939.7 lbs 
5,469.8 lbs each in two wing 
tanks at +342.1 in. 
 
10,851.1 lbs 
5,425.6 lbs each 
 
88.6 lbs 
SEE NOTE 1 
 
EMB-545 MOD 
(see Note 4) 
13,146 lbs 
6,573 lbs each in two wing 
tanks at +367.72 in. 
 
13,058 lbs 
6,529 lbs each 
 
88.6 lbs 
SEE NOTE 1 
 
Oil Capacity (total): 
Tank mounted on each engine: 7.6 U.S. quarts (7.19 liters) total on each engine 
 
Maximum Operating Altitude: 
45,000 ft (13,716 m). See the Approved Airplane Flight Manual - AFM 3921

TC00062IB Page 4 of 9 Rev 17  
. 
Control Surface Movements: 
Elevator Up 25° ±1° 
Down 15° ±1° 
 
Rudder Right 30° ±1° 
Left 30° ±1° 
Aileron Up 25° ±0.8° 
Down 15° ±0.8° 
Outboard Wing Flap TO 6.56° ±1° 
TO/Land 19.72° ±1° 
Land 36.58° ±1.5° 
Inboard Wing Flap TO 6.77° ±1° 
TO/Land 20.11° ±1° 
Land 35.72° ±1.5° 
Spoiler 1 and 3 In Air 30° Inbd ±1.3° / Outbd ±1.9° 
On Ground 40.5° Inbd ±1.3° / Outbd ±1.9° 
Spoiler 2 In Air 30° ± 1.4° 
On Ground 43° ± 1.4 
Horizontal Stabilizer Up 12° ±0.5° 
Down 3° ±0.5° 
 
Manufacturer’s Serial Numbers: 
EMB-550 (except EMB-550 MOD, See Note 4): 
55000001 up to 55009999, except for 55000009, 55000020, and 55000070 
EMB-550 MOD:  55000070, 55020002, 55020103 and subsequent 
EMB-545:  55000009, 55000020, 55010003 up to 55019999 
 
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, EMB-545, EMB-550: 
1) 14 CFR part 25, effective February 1, 1965, including Amendments 25-1 through 25-129 in their 
entirety. 
 
2) Special Conditions: 
The following special conditions have been applied: 
 
SC No. Subject 
25-475-SC Hydrophobic Coatings in Lieu of Windshield Wipers 
25-476-SC Flight Envelope Protection: Performance Credit for Automatic Takeoff Thrust 
Control System (ATTCS) During Go-Around 
25-478-SC Electronic Flight Control System: Control Surface Awareness and Mode 
Annunciation 
25-479-SC Limit Pilot Forces for Sidestick Control 
25-480-SC Design Roll Maneuver for Electronic Flight Controls 
25-481-SC Interaction of Systems and Structures

TC00062IB Page 5 of 9 Rev 17  
. 
25-482-SC Flight Envelope Protection: High Speed Limiting 
SC No. Subject 
25-483-SC Electronic Flight Control System: lateral-Directional and Longitudinal Stability 
and Low Energy Awareness 
25-485-SC Electrical/Electronic Equipment Bay Fire Detection and Smoke Penetration 
25-486-SC  Flight Envelope Protection: Pitch and Roll Limiting Functions 
25-490-SC Landing Pitch over Condition 
25-491-SC Dive Speed Definition With Speed Protection System 
25-492-SC Flight Envelope Protection: General Limiting Requirements 
25-494-SC Sudden Engine Stoppage 
25-495-SC Side-Facing Seats; Installation of Airbag Systems in Shoulder Belts 
25-496-SC Airplane Electronic System Security Protection From Unauthorized External 
Access 
25-497-SC Isolation or Airplane Electronic System Security Protection from Unauthorized Internal 
Access 
25-498-SC Sidestick Controllers 
25-520-SC Flight Envelope Protection: Normal Load Factor (g) Limiting 
25-520A-SC Flight Envelope Protection: Normal Load Factor (g) Limiting (EMB-550 only) 
25-554-SC  Installation of Rechargeable Lithium Batteries 
25-557-SC  Operation Without Normal Electrical Power 
25-558-SC Stowage Compartment Fire Protection 
25-564-SC Flight Envelope Protection: High Incidence Protection System 
25-595-SC  Seats With Inflatable Lap Belts (EMB-545 only) 
25-603-SC Occupant Protection For Side-Facing Seats Forward of Aft-Facing Seats 
25-629-SC Synthetic Vision System and Enhanced Flight Vision System on Head-Up Display 
25-679-SC  Non-Rechargeable Lithium Batteries (Effective to design changes applied for 
after May 26, 2017. See the applicability section of this special condition for more 
information on which design changes must meet it.)  
 
3) Equivalent Safety Findings 
Equivalent Level of Safety (ELOS) findings have been made for the following regulations: 
 
TAD ELOS Memo No. Regulation Title 
TC0717IB-T-A-2 §§ 25.629, 25.671, 25.1309 Aeroelastic Stability 
Requirements 
TC0717IB-T-A-6 §§ 25.721, 25.963(d), 25.994 Crash Protection of Fuel Tanks 
and Systems 
TC0717IB-T-A-11 § 25.331(c)(2) Checked Maneuver Loads 
TC0717IB-T-A-13 §§ 25.341, 25.343, 25.345, 
25.371, 35.373, 25.391, 
25.1517 
Gust and Turbulence Design 
Loads; Rough Air Speed 
TC0717IB-T-C-1 § 25.807 Step-down distance outside the 
airplane for the Type III exit 
located on the right side of the 
airplane 
TC0717IB-T-C-5 §§ 25.811, 25.812 Emergency Exit Marking; 
Emergency Lighting 
TC0717IB-T-C-9 §25.811(e)(4) Emergency Exit Marking 
AT10411IB-T-C-19 § 25.562, 25-495-SC Belted Toilet Side-Facing Seat 
ATD 
Placement on Embraer Model 
EMB- 
545 and Model EMB-550 airplanes 
TC0717IB-T-F-25 § 25.255 Out of Trim Characteristics

TC00062IB Page 6 of 9 Rev 17  
. 
TC0717IB-T-P-3 § 25.1305, 25.1549(a)(b)(c) Powerplant Instruments; 
Powerplant and Auxiliary Power 
Unit 
TC0717IB-T-P-7 part 25 subparts E, F, and G Powerplant, Equipment, Operating 
Limitations and Information 
TC0717IB-T-P-9 § 25.1203(a) Fire Detector System 
TAD ELOS Memo No. Regulation Title 
TC0717IB-T-P-10 §§ 25.933(a)(1)(ii) Flight Critical Thrust Reverser 
TC0717IB-T-P-19 appendix I25.5(b)(4) Lack of On/Off Switch for ATTCS 
TC0717IB-T-P-24 § 25.934 Turbojet Engine Thrust Reverser 
System Tests 
TC0717IB-T-P-26 § 25.1141(f)(2) Powerplant Controls and 
Accessories 
TC0717IB-T-S-2 §§ 25.1301, 25.1309 Equipment, Systems, and 
Installations 
TC0717IB-T-S-3 § 25.671(c)(2) Flight Control System Failure 
Criteria 
TC0717IB-T-SE-2 § 25.1303(a) Flight and Navigation Instruments 
TC0717IB-T-SE-4 § 25.1317(b) High-Intensity Radiated Fields 
(HIRF) Protection 
TC0717IB-T-SE-5 § 25.1383(b) Landing Lights Single Switch 
TC0717IB-T-SE-13 §§ 25.1389(b), 25.1391, 
25.1393, 25.1395, 25.1401(f) 
Position and Anti-Collision 
Lighting 
Systems Luminous Intensity 
Deviations 
TC0717IB-T-SM-5 § 25.841(a)(b)(6) Pressurized Cabins 
TC0717IB-T-SM-6 § 25.831(g) Cabin Ventilation – Humidity 
Requirement 
TC0717IB-T-SM-13 §§ 25.841(b)(1), 25.843(b)(1) Pressurized Cabins and Tests for 
Pressurized Cabins 
 
4) Exemptions from 14 CFR Part 25 
Exemption No. 10338, August 24, 2011. Grant of Exemption for “private, not-for-hire” operations 
to § 25.813(e), for configurations with interior doors installed between passengers and emergency 
exits. 
 
Exemption No. 10338A, August 7, 2015. This exemption granted an amendment to exemption No 
10338 to add the Model EMB-545 airplane. 
 
Exemption No. 10338B, June 11, 2018. This exemption granted an amendment to exemption No 
10338 to install electrically actuated interior doors installed between passengers and emergency 
exits. 
 
Exemption No. 10431, January 11, 2012. Grant of Exemption to § 25.981(a)(3), Relief from the 
requirements for fuel-tank-ignition prevention as it relates to structural lightning protection. 
 
Exemption No. 10557, June 11, 201. Partial Grant of Exemption for “private, not for hire, not for 
common carriage” operations to § 25.791(a), Relief to allow the installation of a single no-smoking 
placard located near the passenger-entry door. 
 
Exemption No. 10557A, August 7, 2015. This exemption granted an amendment to exemption No 
10557 to add the Model EMB-545 airplane. 
 
Exemption No. 10757, April 25, 2013. Grant of Exemption to § 25.809(a), Relief to allow viewing 
the first point of contact with the ground after the exit has been opened and the evacuee is on the 
upper surface of the wing.

TC00062IB Page 7 of 9 Rev 17  
. 
Exemption No. 10757A, August 7, 2015. This exemption granted an amendment to exemption No 
10757 to add the Model EMB-545 airplane. 
 
Exemption 10974B, December 15, 2016. Grant of Exemption to §§ 25.562(a) and 25.785(b) and 
Special Condition 25-495-SC number 2(e), Relief from the lower-leg flail requirements for the 
forward-most seat position on all side-facing seats to all Embraer model EMB-545 and EMB-550 
delivered through December 31, 2017. 
 
5) Modifications Affecting the Certification Basis 
Modification Certification Basis for Affected Areas 
EMB-550 MOD: 
 
DCA 0550-000-00026-2016 
and 
DCA 0550-031-00067-2016 
 
 
 
 
 
EMB-550 MOD adopts EMB-550’s Certification Basis, plus, for 
the components and areas affected by the change, the following 
additional requirements: 
Amendments 25-1 through 25-142 in its entirety except: 
 25.21(g)  at Amd 25-135 
 25.143(c) and (h) at Amd 25-129 
 25.253(c) at Amd 25-135 
 25.571  at Amd 25-96 
 25.903  at Amd 25-100 
 25.1322  at Amd 25-38 
 25.1323  at Amd 25-109 
  25.1325  at Amd 25-108 
  25.1521  at Amd 25-72 
  25.1533  at Amd 25-92 
  H25.4  at Amd 25-123 
 and Special condition 25-520A-SC, Flight Envelope Protection: 
Normal Load Factor (g) Limiting  
  
 
6) Optional Requirements complied with: 
The following Optional Design Regulations have been complied with: 
 
Ice Protection: §§ 25.1403, 25.1419 
Safety Equipment: §§ 25.1411(a),(b),(c), 25.1415(e) 
 
7) Environmental Standards 
14 CFR part 36, effective December 1, 1969 including Amendments 36-1 through 36-28. 
14 CFR part 34, effective September 10, 1990, including Amendments 34-1 through 34-5A. 
 
8) RVSM Capability 
The aircraft is RVSM capable from S/N 55000001 and on. Each operator must obtain RVSM operating 
approval directly from the FAA. 
 
Additional Design Requirements and Conditions: 
The following design details or information must be maintained to ensure that an unsafe design 
condition is not present: 
 
Inflight Engine Restart: Compliance shown by test. Any modifications to the associated AFM procedures 
require evaluation to ensure an unsafe condition is not introduced. Changes in the engine design 
affecting engine restart require aircraft-level evaluation. 
 
Engine Damage from Wing Ice Caused by Cold Soaked Fuel: Compliance shown with an AFM 
procedure for a tactile check for wing ice. Any modification to the AFM procedure requires evaluation to 
ensure an unsafe condition is not introduced.

TC00062IB Page 8 of 9 Rev 17  
. 
Certification: Type Certificate TC00062IB granted October 21, 2014. 
Date of Application: May 14, 2009 amended to October 14, 2010 
Equipment: 
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification 
Basis) must be installed in the airplane for certification. 
 
Service Information: 
Service bulletins, repair instructions (letters, drawings, specifications, forms used for transmitting repair 
descriptions, etc.), structural repair manuals, vendor manuals, AFMs, and overhaul and maintenance 
manuals, which contain a statement that the document is approved by ANAC are accepted by the FAA 
and are considered FAA approved. (These approvals pertain to the design data only.) 
 
 
NOTE 1. A current weight and balance report, including a list of equipment included in the certificated 
 
 empty weight, and loading instructions when necessary must be provided for each aircraft at the 
time of original certification. 
 The certificated empty weight and corresponding center of gravity location must include: 
 
EMB-550, except EMB-550 MOD (See Note 4) 
Unusable fuel  88.6 lb at 356.50 inches aft of datum 
Full engine oil  48.5 lb at 559.37 inches aft of datum 
APU oil  4.4 lb at 673.50 inches aft of datum 
Hydraulic Fluid 109.6 lb at 496.34 inches aft of datum 
 
EMB-550 MOD (See Note 4) 
Unusable fuel 88.6 lb at 356.50 inches aft of datum (wing tanks) 
5.5 lb at 279.53 inches aft of datum (forward tank) 
26.2 lb at 462.60 inches aft of datum (ventral tank) 
Full engine oil 48.5 lb at 559.37 inches aft of datum 
APU oil  4.4 lb at 673.50 inches aft of datum 
Hydraulic Fluid 109.6 lb at 496.34 inches aft of datum 
 
EMB-545 
Unusable fuel 88.6 lb at 330.7 inches aft of datum 
Full engine oil 48.5 lb at 519.7 inches aft of datum 
APU oil 4.4 lb at 631.2 inches aft of datum 
Hydraulic Fluid 105.2 lb at 467.2 inches aft of datum 
 
EMB-545 MOD (See Note 4) 
Unusable fuel  88.6 lb at 330.7 inches aft of datum 
Full engine oil  48.5 lb at 519.7 inches aft of datum 
APU oil 4.4 lb at 631.2 inches aft of datum 
Hydraulic Fluid   105.2 lb at 467.2 inches aft of datum 
NOTE 2. Airplanes must be operated according to the FAA approved Airplane Flight Manual (AFM), 
Embraer document number: 
• AFM-3921-200 for the EMB-550 except the EMB-550 MOD, 
• AFM-3921-800 for the EMB-550 MOD, 
• AFM-3921-500 for the EMB-545 except the EMB-545 MOD, or 
• AFM-3921-850 for the EMB-545 MOD. 
Required placards and markings are listed in Chapter 11 of the Aircraft Illustrated Parts Catalog 
(AIPC) and Airplane Maintenance Manual (AMM).

TC00062IB Page 9 of 9 Rev 17  
. 
NOTE 3. The Airworthiness Limitations Section is found in Chapter 4 of the Aircraft Maintenance Manual 
(AMM-5613). The life limit for rotating parts on the AS907-3-1E engine is in the engine Light 
Maintenance Manual, Airworthiness Limitations Section. 
 
NOTE 4. The EMB-550 with the weight increase, fuel tank additions, and new winglets described in DCA 
0550-000-00026-2016, “EMB-550 Performance Enhancements,” and the avionics updates 
described in DCA 0550-031-00067-2016, “Pro Line Fusion Avionics Load 6.3,” is often referred 
to in Embraer marketing literature as the “Praetor 600.” This name is strictly for marketing 
purposes and is not part of the official model designation. This TCDS distinguishes it as 
EMB550 MOD. 
 
The EMB-550, except for EMB-550 MOD, is often referred to in Embraer marketing literature 
as the “Legacy 500.” This name is strictly for marketing purposes and is not part of the official 
model designation. 
 
“PRAETOR 600E” is strictly a marketing designation of “PRAETOR 600” with a factory-
incorporated “New Interior Configuration” modification (ref.: DCA 0550-025-00123-
2023/FAA), and is not part of the official model designation. 
 
The EMB-545 modified by SB 550-00-0011 to include the weight increase, fuel increase, and 
new winglets described in DCA 0550-000-00100-2018, “EMB-545 Weight Increase and 
Modified Winglet,” and modified by the avionics updates described in DCA 0550-031-00076-
2019, “Pro Line Fusion Avionics Load 6.3,” is often referred to in Embraer marketing literature 
as the “Praetor 500.” This name is strictly for marketing purposes and is not part of the official 
model designation. This TCDS distinguishes it as EMB-545 MOD. 
 
The EMB-545, except for EMB-545 MOD, is often referred to in Embraer marketing literature 
as the “Legacy 450.” This name is strictly for marketing purposes and is not part of the official 
model designation. 
 
“PRAETOR 500E” is strictly a marketing designation of “PRAETOR 500” with a factory-
incorporated “EMB-545 New Interior Configuration” modification (ref.: DCA 0550-025-00123-
2023/FAA and DCA 0550-025-00122-2023/ANAC), and is not part of the official model 
designation. 
 
NOTE 5. The EMB-550 FAA type design definition is contained in Embraer document number 
550TDSD002, "Type Design Standard Document.” 
 
The EMB-545 FAA type design definition is contained in Embraer document number 
550TDSD005, "Type Design Standard Document.” 
 
NOTE 6: Serial numbers 55000073, 55000074, 55000076, 55000080, 55010014, 55010029 and 55010039 
were produced by Embraer Executive Aircraft Inc. in Melbourne, Florida, under the Type 
Certificate. 
 
END
```

## ADs (12, 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 2026-08-52](https://openairdocs.org/ad/2026-08-52): Flight controls · Embraer EMB-545 and EMB-550. Effective May 26, 2026
- [AD 2025-13-02](https://openairdocs.org/ad/2025-13-02): Doors · Embraer EMB-545 and EMB-550. Effective Aug 5, 2025
- [AD 2024-23-07](https://openairdocs.org/ad/2024-23-07): Landing gear · Embraer EMB-545 and EMB-550. Effective Nov 20, 2024
- [AD 2024-16-16](https://openairdocs.org/ad/2024-16-16): Windows · Embraer EMB-550 and EMB-545. Effective Oct 30, 2024
- [AD 2024-15-13](https://openairdocs.org/ad/2024-15-13): Windows · Embraer EMB-545 and EMB-550. Effective Oct 23, 2024
- [AD 2024-05-13](https://openairdocs.org/ad/2024-05-13): Auto Flight · Embraer EMB-545 and EMB-550. Effective Apr 10, 2024
- [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 2022-19-14](https://openairdocs.org/ad/2022-19-14): Equipment/furnishings · Embraer EMB-545 and EMB-550. Effective Apr 14, 2023
- [AD 2022-21-08](https://openairdocs.org/ad/2022-21-08): Flight Controls · Embraer EMB-545. Effective Dec 22, 2022
- [AD 2020-25-07](https://openairdocs.org/ad/2020-25-07): Windows · Embraer EMB-545 and EMB-550. Effective Jan 21, 2021
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## Registered aircraft by registry model (OpenAirDocs)

- [Embraer S A EMB-545](https://openairdocs.org/model/embraer-s-a-emb-545): 171 aircraft (registry code 3260418)
- [Embraer EMB-550](https://openairdocs.org/model/embraer-emb-550): 156 aircraft (registry codes 3260425, 3260426)
- [Embraer Executive EMB-545](https://openairdocs.org/model/embraer-executive-emb-545): 3 aircraft (registry code 3260400)
- [Embraer Executive EMB-550](https://openairdocs.org/model/embraer-executive-emb-550): 2 aircraft (registry code 3260450)
- [Embraer S A EMB-545 LR](https://openairdocs.org/model/embraer-s-a-emb-545-lr): 0 aircraft (registry code 3260421)

## STCs approved under this data sheet (18)

- [STC ST04764NY](https://openairdocs.org/stc/ST04764NY): True Blue Power TS56 Emergency Battery Power Supply Replacement. Mid-Continent Instrument Co., Inc.
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST11982CH](https://openairdocs.org/stc/ST11982CH): Installation of SpaceX Starlink Aviation System i. Nextant Aerospace
- [STC ST12094CH](https://openairdocs.org/stc/ST12094CH): Installation of Gogo MB13 antenna provisions. Premier Air Center, LLC d/b/a West Star Aviation
- [STC ST04560AT](https://openairdocs.org/stc/ST04560AT): Replacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assemblies. Quiet Technology Aerospace
- [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 ST11934IB](https://openairdocs.org/stc/ST11934IB): Installation of Gogo AVANCE L5/LX5 System. Sky Service F.B.O Inc.
- [STC ST11863CH](https://openairdocs.org/stc/ST11863CH): Installation of Gogo Dual Directional Antennas. Premier Air Center LLC. d/b/a West Star Aviation
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST04665CH](https://openairdocs.org/stc/ST04665CH): Installation of a Galley 115VAC/60Hz inverter and USB Charging Ports in accordance with Premier Air 
Center Master Data List Document No. A23377L-755, Revision C, dated June 7, 2024, or later FAA 
approved revision.. PREMIER AIR CENTER LLC dba WEST STAR AVIATION
- [STC ST04650CH](https://openairdocs.org/stc/ST04650CH): Installation of a Gogo Avance L5 Broadband System. PREMIER AIR CENTER LLC, d/b/a WEST STAR AVIATION
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc.
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST00012IB](https://openairdocs.org/stc/ST00012IB): Installation of interior leather finishes in one or more locations. Embraer Engineering & Technology Center - USA Inc.
- [STC ST04464AT](https://openairdocs.org/stc/ST04464AT): Replacement of the inner aluminum barrel of the engine inlet cowl. Quiet Technology Aerospace
- [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 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

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