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TCDS TC00062IB

Historical · Aircraft · Large Airplane · Rev 5 (12/28/2016) · FAA TCDS database

Embraer S.A. drs.faa.gov ↗

The TCDS PDF on drs.faa.gov is authoritative for design-as-certified weight limits, performance, equipment and operating limitations.

Models covered (2)

Special conditions + ELOS findings

  • SC 25-554-SC Special Conditions: Embraer S.A., Model EMB-550 Airplane; Installation of Rechargeable Lithium Batteries
  • SC 25-623-SC Special Conditions: Embraer S.A. Model EMB-545 and EMB-550 Airplanes; Installation of an Airbag System To Limit the Axial Rotation of the Upper Leg on Single- and Multiple-Place Side-Facing Seats
  • SC 25-603-SC Special Conditions: Embraer Model EMB-545 and EMB-550 Airplanes; Occupant Protection For Side-Facing Seats Forward of Aft-Facing Seats
  • SC 25-595-SC Special Conditions: Embraer Model EMB-545 Airplanes; Seats With Inflatable Lap Belts
  • ELOS AT1041ITB-T-C-l9 Belted Toilet Side-Facing Seat ATD Placement on Embraer Model EMB-545 and Model EMB-550
  • ELOS TC0717IB-T-C-9 INFORMATION: The Type II Emergency exit marking located on the left side of the airplane, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-A-6 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Crash Protection of Fuel Tanks and Systems on a Model EMB-550 airplane, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-P-26 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Engine Fuel Shutoff Valve Indication on a Model EMB-550 airplane, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-C-5 INFORMATION: Equivalent Safety Finding for Graphical Exit Signs on Embraer Model EMB-550 Series Aircraft, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-A-2 INFORMATION: Equivalent Safety Finding for Failure Criteria Considered Under the Aeroelastic Stability Requirements of 25.629 on Embraer Model EMB-550 Program, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-A-13 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Embraer s project on the EMB-550, FAA Project # TC0717IB-T
  • ELOS TC0717IB-T-C-1 INFORMATION: Step-down distance outside the airplane for the Type III exit located on the right side of the airplane, FAA Project # TC0717IB-T

Certification basis — 14 CFR

Specific sections

  • Sec. 25.255
  • Sec. 25.331
  • Sec. 25.341
  • Sec. 25.343
  • Sec. 25.345
  • Sec. 25.371
  • Sec. 25.391
  • Sec. 25.562
  • Sec. 25.629
  • Sec. 25.671
  • Sec. 25.721
  • Sec. 25.791
  • Sec. 25.807
  • Sec. 25.809
  • Sec. 25.811
  • Sec. 25.812
  • Sec. 25.813
  • Sec. 25.831
  • Sec. 25.841
  • Sec. 25.933
  • Sec. 25.934
  • Sec. 25.963
  • Sec. 25.981
  • Sec. 25.994
  • Sec. 25.1141
  • Sec. 25.1203
  • Sec. 25.1301
  • Sec. 25.1303
  • Sec. 25.1305
  • Sec. 25.1309
  • Sec. 25.1317
  • Sec. 25.1383
  • Sec. 25.1389
  • Sec. 25.1391
  • Sec. 25.1393
  • Sec. 25.1395
  • Sec. 25.1403
  • Sec. 25.1411
  • Sec. 25.1419
  • Sec. 25.1517
  • Sec. 25.1549
  • Sec. 25.5
  • Sec. 25.785
  • Sec. 25.843
  • Sec. 25.1401
  • Sec. 25.1415

Fleet view · 45 registered tails · FAA registry, median and p10–p90

Seats
14
n=45
Year of mfr
2024
2012–2025

Engines on the type, by tail count

  • HONEYWELL AS907-3-1E 42
NTSB events
22
across all model variants
Applicable ADs
32
FAA airworthiness directives
Per-tail rate
0.49 events / tail · 0.71 ADs / tail