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EC 135 T2+

EC 135 T2+

EC 135 T2+

21
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M. W.
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M. W.
Diese Lernkarten bieten eine detaillierte Übersicht über die Leistungsparameter und Betriebsgrenzen des EC 135 T2+. Sie konzentrieren sich auf Werte wie FLI, max TRQ, TOT, sowie auf die verschiedenen Leistungsmodi wie kontinuierliche und transienten Betrieb. Die Karteikarten decken auch die Betriebsgrenzen für verschiedene Massenbereiche und Höhen ab, einschließlich der maximalen Betriebs- und Hover-Höhen. Piloten und Wartungstechniker profitieren von diesen Informationen, um die optimale Leistung und Sicherheit des Helikopters zu gewährleisten.
Cartes-fiches
21
Utilisateurs
1
Langue
Allemand
Catégorie
Technique
Niveau
Autres
Créé / Mis à jour
11.11.2012 / 11.11.2012
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Cartes-fiches

Maximum approved gross mass is ... kg

2910

Maximum allowable floor loading is ... kg/m2

600

Maximum allowable load per tie-down ring is ... kg

100

Lateral center of gravity limits left and right of the fuselage centerline are ... mm

100

VNE for OEI operation under all conditions is ... kt or as shown in the VNE- tables (Fig. 2-2), whichever is less.

110

VNE for steady autorotation under all conditions is ... kt or as shown in the VNE- tables (Fig. 2-2), whichever is less.

90

Maximum operating altitude is ... ft

20000

Maximum operating altitude for hover in ground effect / takeoff and landing is ... ft DA

15000

For gross mass above 2720 kg and up to 2835 kg, maximum operating altitude is ... ft

12000

For gross mass above 2835 kg and up to 2910 kg, maximum operating altitude is ... ft

10000

Battery temperature limits:

For engine start-up at outside air temperatures below ... °C using the aircraft battery, the aircraft battery shall be preheated to at least ... °C.

-20 / -20

ROTOR RPM LIMITATIONS (POWER ON)

Minimum Transient (max. ... s) ... %

Minimum Continuous 1900 kg <= GM: ... %

Maximum Continuous ... %

20s / 85% / 97% / 104%

ROTOR RPM LIMITATIONS (POWER OFF)

Minimum Continuous 1900 kg <= GM: ... %

Maximum Continuous ... %

Maximum Transient (max. ... s) ... %

85% / 106% / 20s / 112%

Engine Starting Transient (max. ... sec) ... FLI / max TOT ... °C

5s / 11 FLI / 895 °C

Engine Starting unlimited ... FLI / max TOT ... °C

8,5 FLI / 810 °C

All Engines Operating

Takeoff Power TOP (... min) V <= Vy (... FLI / max TRQ ... % / max TOT ... °C)

5 min / 10 FLI / 2x78% / 897 °C

All Engines Operating

Max. Continuous Power (... FLI / max TRQ ... % / max TOT ... °C)

9,5 FLI / 2x69% / 879 °C

One Engine Inoperative

30 sec. Power (... FLI / max TRQ ... % / max TOT ... °C)

13,5 FLI / 1x128% / 1024 °C

One Engine Inoperative

2.0 min. Power (... FLI / max TRQ ... % / max TOT ... °C)

13 FLI / 1x125% / 994 °C

One Engine Inoperative

Max. Contin. Power (... FLI / max TRQ ... % / max TOT ... °C)

11 FLI / 1x89,5% / 942 °C

A transient AEO TOP power limit of 2 x ... % torque (... FLI) has been established for V <= ... and unintended use of max. ... seconds duration only. Exceeding of any one of those limits requires maintenance action (refer to the

maintenance manual)

82% / 10,4 FLI / Vy / 10 sec

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