.
Ø 1/2 FLAPS - IAS < 300
kt
Ø Full FLAPS - IAS < 225
kt
Ø Load factor (full flaps)
- 2,5 g
JPT (Jet Pipe Temperature)
Ø On the ground : RPM -
8,400 JPT < 755 deg C
Ø In Flight: RPM = 8,400
JPT < 700 deg C
Ø RPM - 8,900 JPT < 735
deg C
Ø Peak JPT permissible on
throttle movements is 780 deg C for a period of 30 seconds maximum and 840 deg
C peak In flight, JPT generally exceeds 740 deg C at 8,400 RPM and 710 deg C at
8,900 RPM.
Ø High speed with AB or low
speed at high altitude the JPT reading at maximum engine RPM could fall and
must not go below 550 deg C
Ø Maximum takeoff weight -
15,200 Kg
Ø Normal landing weight -
9,000 Kg
Ø Exceptional landing
weight - 11,000 Kg
Ø Maximum rate of decent at
touchdown:
Ø 9,000 Kg - 450 ft/min
Ø 11,000 Kg - 350 ft/min
Gear and Flaps up
Ø 500 - 1000 ft IAS <
450 kt
Ø 1000 - 20,000 ft IAS <
650 kt
Ø 20,000 - 36-000 ft IAS
< 700 kt
Ø 36,000 - 50,000 ft MACH
< 2.0
Maximum of 15 seconds
Ø Half rolls only allowed
up to:
Ø M - 1.5
Ø TAT - 135 deg C
Ø Crosswind - 25 kt
Ø Maximum dive allowed may
not exceed -30 deg pitch
Ø Maximum continuous
operation - 9,000 RPM
Ø Instantaneous peak limit
- 9,250 RPM
Ø IAS 700 kt between 0 and
20,000 ft
Ø IAS 750 kt above 20,000
ft
Ø MACH limit = 2.10
Ø 55,000 ft