Term
APU Limits
Max Altitude for Start
Max Tailwind for Start
Max Rotor speed
EGT: Start
Continuous
Starter Limits
Between three Consecutive Attempts
Between 2 series of 3 consecutive attempts |
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Definition
APU Limits
30 000ft
30kt
108% (Shuts off at 104%)
884°C
680°C
Starter Limits
1 min off
30 mins Off |
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Term
Power Plant
N1
N2
ITT: Start
Takeoff
Continuous
Oil Pressure: >88% N2
=<88% N2
Oil Temp Vibration LP: HP: |
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Definition
Power Plant
100%
102.5%
800°C
948°C(5mins Max)
901°C
34PSI -> 95 - 110psi (can be exceeded if oil temp>21°C engine must idle to get >95psi)
50psi ->95 - 110psi 21 - 126°C
1.8IPS 1.1IPS |
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Term
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Definition
| After start, the engines must run at idle or taxi thrust for at least 4 minutes for cold engines or 2 minutes for warm engines. Before takeoff, to increase N2 above 83% the engine oil temperature must be at 40°C minimum. In lieu of this limit, it is acceptable to either: - - run the engine for at least 8 minutes in idle or taxi thrust and check if the temperature is at least 21°C |
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Term
Operation in Icing Conditions |
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Definition
Max Temp for Anti-Icing Operations - 10°C
Minimum Temp for Manual A/I Operation - -40°C
Single Engine/Bleed Max Alt Operation in Icing - 15
Holding Config - Landing Gear - UP
- Flaps - UP
- Minimum Airspeed - 200kts
?Landing Gear extension prohibited ? |
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Term
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Definition
| Maximum load on main generator 400 A Maximum Load on APU Generator: Up to 30000 ft 400 A Above 30000 ft 300 A Maximum battery temperature 70°C |
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Term
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Definition
| Maximum differential pressure 7.8 psi Maximum differential overpressure 8.1 psi Maximum differential negative pressure -0.3 psi |
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Term
Weight
E135 LR (EASA = -10kgs MRW + MTOW)
MZFW
MRW
MTOW
MLW
E140 (E135 KL) ANAC
MZFW
MRW
MTOW
MLW |
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Definition
E135 LR
MZFW - 16 000kg
MRW - 20 090KG
MTOW - 19 990kg(-100kgs from MRW)
MLW - 18 500kg
E135 KL (E140) ANAC
MZFW - 17 100kg
MRW - 21 200kg
MTOW - 21 100kg (-100kgs from MRW)
MLW - 18 700kg |
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Term
Flap extension
Vfe
9°
18°
22°
45° |
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Definition
9° - 250kts (240kts)
18° - 200kts (190kts)
22° - 200kts (190kts)
45° - 145kts (140kts) |
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Term
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Definition
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Term
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Definition
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Term
Fuel
Total
Per wing
All Pumps working
No pumps working
Temps |
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Definition
Fuel
5188
2954
18kg Unusable
165kg Unusable
-40°C -> 52°C |
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Term
Power Plant Starter Limits
ON GROUND
Starting or Dry motoring - up to 5Mins ON, 5mins OFF
OR
1st to 4th cycles - 1min ON, 1min OFF
Following cycles
1Min ON, 5Mins OFF
IN FLIGHT
Max continuous Operation Time
5mins (No Cool Down period needed) |
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Definition
| Power Plant Starter Limits |
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Term
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Definition
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Term
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Definition
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Term
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Definition
Max Tailwind - 10kts
Cross-Wind Limits
Dry RWY - 30kts
Wet - RWY - 30kts
Compacted Snow - 25kts
Standing water, Slush, Dry snow - 20kts
Ice(No Melting)10kts |
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Term
Turbulent Air Penetration |
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Definition
Below 10 000ft - 200kias
Above 10 000ft - 250kias/0.63 - Whichever is lower |
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Term
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Definition
Minimum engagement Height - 1 000ft AGL
Minimum Use Height - 160 ft
Malfunction Altitude Loss:
Cruise - 80ft
Maneuver - 40ft
ILS - 15ft
(Coupled Go-Around Height Loss may be 75ft) |
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Term
CAT II Operation (Primus 1000) |
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Definition
2 AHRS OR 2 IRS
1 Yaw Damper system 1 Autopilot
2 Flight Director Systems 2 (PFD)
Windshield Wipers 2VHF/NAV Systems
1VHF/COMM System Both Engine
CAT II Checklist Logic 1 Electrical Trim System
1 Radio Altimeter 1 GPWS or EGPWS
1 Aural Warning Unit 2 Air Data Systems
1 Standby Attitude Indicator
1 Standby Airspeed Indicator
1 Standby Altimeter |
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Term
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Definition
Autopilot System - 100ft
Minimum use Height - 80ft (RA)
Minimum RVR - 300m
Wind components
Max Headwind - 23
Max Crosswind - 25
Flaps - 22° |
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