Aircraft General Flashcards
The danger area surrounding the weather radar antenna is:
100 feet for large metallic objects and 9
feet for personnel. PTM Pg. 1-6
The pilot and co-pilot windshields are constructed of:
2 ply layer with the outer layer being glass and
the inner a polycarbonate material providing structural integrity. PTM Pg. 1-16
A ( ) is applied to the windshield to provide rain repellency.
Coating PTM Pg. 1-16
In the event the outer glass pane of the windshield shatters:
Structural integrity is maintained by the
polycarbonate inner pane. QRH Pg. A-13
In the event the outer glass pane of the windshield shatters:
The checklist to run is found in the amber
section of the QRH. QRH Pg. A-13
During taxi, if the wing clears a stationary object:
The tail will also clear that object.
PTM Pg. 1-21
There are ( ) vortilons attached to the underside of each wing.
4 PTM Pg. 1-19
There are ( ) triangles attached to the inboard leading edge section of each wing. PTM Pg. 1-18
8 PTM Pg. 1-18
( )static wicks dissipate more static electricity than the inboard, therefore it is acceptable to be missing the inboard static wicks per the MEL.
Outboard PTM Pg. 1-22
The ( ) antenna is located on the bottom of the aircraft and the ( ) antenna is located on the top of the aircraft.
VHF 1 , VHF 2 PTM Pg. 1-23
Maximum Structural Take Off Weight is limited to Pounds, for the Lear 45.
21,500 lbs. PTM Pg. 1-2
Maximum Landing weight is limited to ( ) or the Lear 45.
19,200 lbs. AFM Pg. 1-3.
MMO/VMO for a Lear 45 is Mach and KIAS.
.81 Mach & 330 KIAS AFM Pg. 1-7
Maximum Ramp weight is limited to ( ) lbs., for the Lear 45.
21,750 lbs. AFM Pg. 1-2
The emergency exit can be locked by:
Inserting an internal security pin into the locking mechanism.
PTM Pg. 1-15