Jeppesen Oral- Chapter 13 (Powerplant and Propeller Airworthiness Inspections) Flashcards
MMM and FAR part 43 appendix D
Engine data plate
Power output (static and idle r.p.m.), magneto check, fuel and oil pressure check, cylinder and oil temperature check
MM, TCDS
Engine manual, TCDS, MMM
Determine integrity and wear of the hot section components
Refer to the MMM for the required procedures
Inspection of the hot section
STC (supplemental type certificate) or FAA field approval
When an AD references the service bulletin
100-hour inspections are required only on aircraft that carry persons for hire or a re used to give flight instruction for hire.
In Appendix D of FAR Part 43
In the Type Certificate Data Sheets for the engine
An A&P mechanic who holds an Inspection Authorization
A differential compression check and a direct compression check
The combustion section is checked for cracks and distortion. The turbine wheel, the turbine case, and the exhaust section are checked for cracks, indications of overheating, and any indication of warpage, erosion, or burning.
Cracks that are caused by the high concentration of heat in the hot section.
yes
mmm
The inside of the cylinder
