Engine EASA MOdule 15
Engine EASA MOdule 15
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abbas8m
Abbas Aviation is a page created by an 83 year old retired aircraft maintenance engineer specializing in aeronautical engineering. With over 50 years of experience, the goal is to keep the acquired information living for upcoming generations of engineers.
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The CFM56-3 N2 rotor section consists of
B737_ATA_70_QUIZ_04
The CFM56-3 N2 rotor section consists of
#B737_NG_QUIZ #B1#b2 #Airdraft #Engineer #capton #[olpt ATA_70 # POWER_ PLANT #CFM # section #N2
The CFM56-3 N1 low pressure turbine consists of
B737_ATA_70_QUIZ_03
The CFM56-3 N1 low pressure turbine consists of
#B737_NG_QUIZ #B1#b2 #Airdraft #Engineer #capton #[olpt ATA_70 # POWER_ PLANT #CFM # section #N1
The CFM56-3 N1 rotor section consists of
+70_QUIZ_02
The CFM56-3 N1 rotor section consists of
#B737_NG_QUIZ #B1#b2 #Airdraft #Engineer #capton #[olpt ATA_70 # POWER_ PLANT #CFM # section
The CFM International CFM56-3-B1 is
B737_ATA_70_QUIZ_01
The CFM International CFM56-3-B1 is
#B737_NG_QUIZ #B1#b2 #Airdraft #Engineer #capton #[olpt ATA_70 # POWER_ PLANT #CFM
The DUAL BLEED light is illuminated. Engine thrust
#B737_NG_QUIZ #N1 #b2 #Airdraft #Engineer #capton #[olpt ATA_36 #[meumatics #Fan # A.P.U # isolation
What initial action is required in the event of a WING BODY OVERHEAT light illuminating.
#B737_NG_QUIZ #N1 #b2 #Airdraft #Engineer #capton #[olpt ATA_36 #[meumatics #Fan # A.P.U # isolation
The isolation valve is
#B737_NG_QUIZ #N1 #b2 #Airdraft #Engineer #capton #[olpt ATA_36 #[meumatics #Fan # A.P.U # isolation
The A.P.U. bleed valve is
#B737_NG_QUIZ #N1 #b2 #Airdraft #Engineer #capton #[olpt ATA_36 #[meumatics #Fan # A.P.U
The source air ducted through the pre-cooler is
#B737_NG_QUIZ #N1 #b2 #Airdraft #Engineer #capton #[olpt ATA_36 #[meumatics #Fan