The ERJ is not certified for ditching.

TCDS No.: EASA.IM.A.032 EMB-145 Page 20/25
Issue: 06 Date: 03 August 2012
SECTION 4: NOTES (ALL MODELS) - continued
EMB-145LR, EMB-145LU, EMB-135BJ with SB/Mod per DCA 145-000-
00020/2008:
H30 x 9.50-16 (Main); 19.5 x 6.75-8 (Nose)
1.6 Ditching
All EMB-145 () and EMB-135 () models are not approved for ditching
2. EMB-135BJ
2.1 EMB-135BJ below S/N 145625
Engines: Two Rolls-Royce Corp. USA AE3007A1P turbofan engines
Maximum certified weights
MODEL EMB-135BJ
below SN 145625
Taxi and ramp 22270 kg
Take-off 22200 kg*
Landing 18500 kg
Zero fuel 16000 kg
*For airplanes Pos-mod. SB 145LEG-25-0078 the MTOW will be 22 000 kg (to increase again the
MTOW up to 22 200 kg, the SB 145LEG-25-0079 must be incorporated)
Fuel Capacity:
Maximum usable fuel of 10152 liters (two forward fuselage tanks of 1056 liters at
+8440 mm, two wing tanks of 3198 liters at 13147 mm and two aft fuselage tanks
of 822 liters at +20293 mm). Unusable fuel of 106 liters (forward tanks 27 liters,
wing tanks 44 liters and aft tanks 35 liters).
2.2 EMB-135BJ modified with new Engines AE3007A2, MTOW increase and more fuel
tank according to the DCA 0145-000-00020-2008/EASA (EMB-135BJ
PERFORMANCE ENHANCEMENTS). The EMB-135BJ with this modification
embodied is commercially known as Legacy 650.
Engines: Two Rolls-Royce Corp. USA AE3007A2 turbofan engines
Maximum certified weights
Taxi and ramp 24 370 kg
Take-off 24 300 kg
Landing 20 000 kg
Zero fuel 16 400 kg
*For airplanes Pos-mod. SB 145LEG-25-0078 the MTOW will be 22 000 kg (to increase again the
MTOW up to 24 300 kg, the SB 145LEG-25-0079 must be incorporated)