") (the "Inspection Facility") which shall consist of a: (i) a modified Gulfstream Condition Survey as listed on Exhibit E hereto; (ii) borescope of the Auxiliary Power Unit and Engines; (iii) the review of the Aircraft and Engine log books and maintenance records (collectively the "Aircraft Documents") (which shall be

air • Low pressure (LP) bleed air from the engines • High pressure (HP) bleed air from the engines • Bleed air from the single compressor stage of the Auxiliary Power Unit (APU) • External air from a comparable bleed air source (external pneumatic rig) The pneumatics system consists of two identical and independent sy

each AN960CI0L washers; 5 each MS21059.13 nuiplates that were attached to the panel with 10 each MS20427M3-3 rivets. Performed operational check of the Auxiliary Power Unit, including electrical and pneumatic loading, using applicable procedures contained in the Gulfstream Aerospace G-IV FAA Approved Aircraft Flight Ma