Jabiru J230-D 2020, Руководство по эксплуатации для пилотов

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Jabiru Aircraft Pilot Operating Handbook
Model J230-D
JP-FM-09 Revision: 6 28/2/2020 Page 20
Note #1 Time with CHT at between 180°C (356
o
F) and 200°C (392
o
F) is not to exceed 5
Minutes
Note #2 If temperature limits are reached, shut the engine down or cool it by pointing the
aircraft into wind.
Other limits are as follows:
•
Minimum oil pressure at idle: 80 kPa (11 psi)
•
Maximum oil pressure at start: 525 kPa (76 psi)
2.7 CROSSWIND
The maximum allowable crosswind velocity is dependent on many factors including:
- Aircraft limitations
- Pilot capability.
- Ground conditions
– i.e. turbulence from structures or trees
- Wind state
– i.e. steady wind or gusting / thermal conditions.
With average pilot technique, steady, direct crosswinds of up to 14 knots can be handled with
safety.
2.8 OTHER CLIMATIC RESTRICTIONS
Maximum Ambient Operating Temperature 38°C (100°F)
Flight into known icing conditions Prohibited
2.9 KINDS OF OPERATION
The standard J230-D, as detailed within this POH, is approved for Day VFR Operations only.
An optional package is available to allow the aircraft to conduct Night VFR Operations. Physically
this package consists of additional lights and equipment. Aircraft approved for Night VFR
Operations must also have such operations approved on their Certificate of Airworthiness
and
must carry the Jabiru J230-D Night VFR Operations Supplement (Document Number JP-MS-06).
Note
Carrying out Night VFR Operations without a valid, endorsed Pilot Licence, Certificate of
Airworthiness, Night VFR Supplement & properly equipped aircraft is illegal. Pilots must
ensure the aircraft is appropriate for the intended operations.
2.9.1 JABIRU USA ONLY
The J230-D is equipped for Night VFR as standard and must carry the Jabiru J230-D Night VFR
Operations Supplement (Document Number JP-MS-06).
Note
Carrying out Night VFR Operations without a valid, endorsed Pilot Licence, Night VFR
Operations Supplement & properly equipped aircraft is illegal. Pilots must ensure the
aircraft is appropriate for the intended operations.
2.10 POWER GENERATION SYSTEM LIMITATIONS