Jabiru Aircraft
SECTION 5
CASA APPROVED
Model J160-C
PERFORMANCE
JP-FM-06 Revision:
0
21 Dec 2005
Page 5-5
range. The performance information is not valid when the outside air temperature and/or
pressure height exceeds the maximum values for which this information is scheduled.
Outside Air Temperature (degC)
-20
-10
0
10
20
30
38
540
0
369
391
415
439
464
490
511
2000
413
438
465
493
523
553
579
4000
464
494
525
559
593
630
661
6000
524
560
598
638
680
726
764
8000
598
641
687
737
790
847
897
Weight
(kg)
Pressure
Altitude
(ft)
Take Off Distance
For every 1 knot of head-wind component, the take-off distance can be reduced by 11-metres.
For every 1 knot of tail-wind component the take-off distance required MUST be increased by 16
–metres.
5.2.4
Landing Distances
The landing distance table presented below provides information to achieve the minimum landing
distance for a variety of operating conditions. The data is applicable when using a power off
glide approach with the flaps extended to the “Landing Flap” or fully extended position, and is
based on landing distances from a height of 15 metre (50 feet) to stop.
The landing distance is provided for a hard bitumen surface. Wet and/or slippery surfaces will
increase the landing distance over that scheduled and the pilot should therefore ensure that
adequate strip length is available to cover these conditions.
The technique used in establishing the Power Off Approach Landing Chart distance is such that
the aircraft approaches with idle power down to the 15 metre (50 foot) height point at 63 KIAS.
After touch down maximum wheel braking is used to bring the aircraft to a stop.
When the outside air temperature and/or pressure height is below the lowest range scheduled on
the charts, the aircraft performance shall be assumed to be no better than that appropriate to this
lowest range. The performance information is not valid when the outside air temperature and/or
pressure height exceeds the maximum values for which this information is scheduled.
Outside Air Temperature (degC)
-20
-10
0
10
20
30
38
540
0
432
440
448
456
464
472
478
2000
447
456
464
473
481
490
497
4000
464
473
482
491
500
510
517
6000
482
492
502
511
521
531
539
8000
501
512
523
533
544
555
563
Weight
(kg)
Pressure
Altitude
(ft)
Landing Distance (metres)
For every 1 knot of head-wind component, the landing distance can be reduced by 11-metres.
For every 1 knot of tail-wind component the landing distance required MUST be increased by 17
–metres
Summary of Contents for J160-C
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