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Engine inspection
FAA AMP
Question | Answer |
---|---|
determine which portion of the AD is applicable for model 0-690 series engine serial No. 5863.40 with 283 hours' time in service | (B), (1) |
each powerplant installed on an airplane with a standard airworthiness certificate must have been | type certificated |
which of the following conditions is usually not acceptable to any extent in turbine blades? | cracks |
which of the following contains a minimum checklist for 100-Hour inspections of engines? | 14 CFR part 43 App. D |
when inspecting a aircraft reciprocating engine what document is used to determine if the proper magnetos are installed? | aircraft engine specifications or type certificate data sheets |
on a reciprocating engine aircraft using a shrouded exhaust muffler system as a source for cabin heat, the exhaust system should be | visually inspected for any indication of cracks or an operational carbon monoxide detection test should be done |
a cessna 180 aircraft has a McCauley propeller No. 2A34C50/90A. the propeller is severly damaged in a ground accident.... which of the following should be used to find an approved alternate replacement? | aircraft specifications/type certificate data sheets |
what publication contains the mandatory replacement time for parts of a turbine engine? | engine manufacturer's service instructions |
which of the following contains approved data for performing a major repair to an aircraft engine? | Manufacturer's maintenance instructions when FAA approved |
indentations on bearing races caused by high static loads are known as | brinelling |
which of the following can inspect and approve an engine major repair for return to service? | Certificated mechanic with an Inspection Authroization (IA) |
1) ADs are federal regulations and must be complied with unless specific exemption is granted. 2) ADs of an emergency nature may require immediate compliance. regarding the above: | Both are true |
which of the following component inspection is to be accomplished on a 100-hour inspection? | Check cylinder compression. |
which of the following is used to monitor the mechanical integrity of the turbines, as well as to check engine operating conditions of a turbine engine? | Exhaust gas temperature (EGT) |
you are performing a 100-Hour inspection on a R985-22 aircraft engine. what does the '985' indicate? | the total piston displacement of the engine |
what section in the instructions for continued airworthiness is FAA approved? | airworthiness limitations section |
select the Airworthiness Directive applicability statement which applies to an IVO-355 engine, serial number T8164, with 2,100 hours total tine and 300 hours since rebuilding? | applies to all IVO-355 engines, serial number T8000-T8300, having less than 2,400 hours total time. |
the breaking loose of small pieces of metal from coated surfaces, usually cause by defective plating or excessive loads, is called | flaking |
each powerplant installed on an airplane with a standard Airworthiness Certificate must have been | type certificated |
which of the following contains a table that lists the engines to whcih a given propeller is adaptable? | propeller type certificate data sheets |
straightening nitrided crankshafts is | Not recommended |
(1) serviceability limits for turbine blades are much more stringent than are those for turbine nozzle vanes. (2) a limited number of small nicks and dents can usually be permited in any area of a turbine blade. regarding the above | only (1) is true |
a ground incident that results in a propeller sudden stoppage would require a cranckshaft runout inspection. what publication would be used to obtain crankshaft runout tolerance | current manufacturer's maintenance instructions |
when must an airworthiness directive (AD) be complied with after it becomes effective? | as specified in the AD |
the airworthiness standards for the issue of type certificate for small airplanes with nine or less passenger seats in the normal, utillity, and acrobatic categories may be found in the | 14 CFR Part 23 |
What maintenance record(s) is/are required following a major repair of an aircraft engine? | entries on the engine maintenance record and FAA form 337 |
How is the flow range of the fuel discharge nozzles installed in a fuel injected reciprocating engine indicated? | by a letter stamped on the hex of the muzzle body |
where would one find type design information for an R1830-92 engine certificated under the Civil Air Regulations (CAR) and installed on a DC-3? | the aircraft engine specifications |
what publication is used for guidance to determine whether a powerplant repair is major or minor? | 14 CFR part 43 |
a severe condition of chafing or fretting in which a transfer of metal from one part to another occurs is called? | galling |