問題一覧
1
PW1100 for High Pressure Compressor control is using
two HPC VSV actuators (master and slave)
2
Flat Rating thrust of PW1100 engine is:
higher than PW1500/PW1900
3
Fan Blades of PW1100
has blade platforms
4
PW1100 engine weight is:
182 kg higher than PW1500G
5
Exciter Box of PW1100 engine is organized by:
115 VAC
6
Fan Exit Guide Vanes shims on PW1100 engine can be installed
on Fan Case side only
7
PW1100 engine can be installed on aircraft
Airbus A320neo
8
Magnetic Chip Collectors on PW1100 engine are installed:
5 pcs on Lubrication and Scavenge Oil Pump + 1 pcs on bearing No 4 scavenge tube
9
Bearing No 4 of PW1100 is cooled and pressurized by
Lop Pressure Compressor stage 2.5
10
Low Pressure Compressor Stator Vane Actuator on PW1100 engine is installed:
on LH side
11
Oil Debris Monitor sensor of PW1100 engine is installed:
scavenge line of oll to oil tank
12
N2 speed sensor on PW1100 is installed:
as a magnetic sensor on Angle Gearbox
13
Journal Oil Shuttle Valve of PW1100 engine is installed
on LH side of Compressor Intermediate Case firewall
14
On which side of Fan Case is installed EEC and PHMU on PW1100 engine?
RH side
15
Which modules of PW1100 engine are integrated, comparing to PW1500G engine
High Pressure Turbine and Turbine Intermediate Case
16
PW1100 engine has
20 fan bldes
17
Who is Type Certificate Holder for PW1100 engine?
International Aero Engines
18
There is… EGT probes on PW1100 engine
4
19
Which engine has Fan Cowlings latch sensors?
PW1100 only
20
Who is allowed to issue Airworthiness
FAA and EASA
21
PW1100 engine has Type Certificate issued by:
FAA, EASA, and Transport Canada
22
Boroscope plugs on PW1100 are located:
on RH side only
23
PW1100 engine has
4 brush seals
24
PW1100 High Pressure Compressor is composed from?
8 stages of Integrally Bladed Rotors