BRISTELL S-LSA, Руководство по техническому обслуживанию и инспекции

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10.CHAPTER
– POWER UNIT
Document: SLSA-MIP-5-4-0-US Date of Issue: 05/2016 Revision: -
10-26
Tab. 10
–1: Engine test report
ENGINE TEST REPORT
Aircraft BRISTELL S-LSA Registration S/N
Engine ROTAX Type 912 iS Sport S/N
Activity Set down values Measured values
Starting up the engine
Check if Warning Lamps illuminate and
extinguish after around 3 seconds
1. Min. oil pressure up to 10 sec. 0.8 bar (12 psi)
2. Max. oil pressure* 7 bar (102 psi)
3. Min. fuel pressure 2.8 bar (40.5 psi)
4. Max. fuel pressure 3 bar (43.5 psi)
5.
Increase RPM as soon as oil
pressure reaches
2 bar (29 psi)
6.
Warming up the engine at
2000
– 2500 RPM
smooth running
7. Voltage 12.4
– 15.1 V
Engine test
8. Min. oil temperature
50°C (122°F)
9. Oil pressure 2
–5 bar
(29
–73 psi)
10. Max. coolant temperature ***
120 °C (248 °F)
11.
LANE and Ignition check at 4000
rpm. RPM drop (LANE A or B off)
max 180 rpm.
max. 180
(115 RPM **)
11. Acceleration 2
– 3 sec.
12.
Max. RPM on the ground (max.10
sec)
5200 ± 100 RPM
13. Idle Approx. 1400 RPM
Defects:
*
During cold start for a short term only
**
The speed drop may not exceed 180 rpm engine speed, which corresponds 75 rpm propeller speed..
Conclusion
Complying
– Noncomplying
Complying if the measured values are not out of the range of the prescribed values.
Elaborated by: Signature: Date:
Checked by: Signature: Date: