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AND, BECAUSE THERE ARE NON-SERVICEABLE PARTS ON AIRPLANES THAT IS WHERE THE M/M/S AIRCRAFT REGISTRATION HAPPENS? THEN, YOU JUST REPLACE THE PLANE?

IN A FAULTED CIRCUT OF THE GYROSCOPE DUE TO INSTRUMENT GUAGE FAILURE FROM PRESSURE IE. THE PETOT OR THE SLIGHT MISALIGNMENT OF AIR PRESSURE DUMP VALVES OR SMALL HOLE OR OTHER PROBLEM ETC IN WHICH THE LEGACY INPUT OR FLIGHT COMPUTER STOPS AND THE SCREEN DISAPPEARS IN PHASE OUT THEN YOU TYPE OR PULL THE UPSET AIRPLANE KNOB AND THEN FOLLOW THE EMERGENCY CHANNEL AND LAND? THIS IS FOUND IN THE REVISED UPSET AIRPLANE MANUAL? OF COURSE THIS IS WHY YOU USE THE AIRCRAFT REGISTRATION M/M/S LIST TO ROTATE OUT HIGH MILEAGE AIRPLANES TO PREVENT THIS? THIS IS A TRAINING CALL JET TRAINING ON A FLIGHT SIMULATOR?

TO AVOID ISSUES WITH AIRPLANE MAINTENANCE PLEASE DO THE AIRCRAFT REGISTRATION M/M/S LIST AND THIS WILL ROTATE THE FLEET TO PREVENT FLIGHT PROBLEMS?

BE AWARE OF A TRAINED LANDING GEAR SOUND, HAVE SPARE BULBS READY FOR THE INSTRUMENT? BE AWARE OF THE PRACTICLE TEST STANDARDS?

WAIT TILL AFTER LANDING TO CHECK THE AFTER LANDING GEAR CHECK LIST? THIS WILL KEEP YOU FROM NOT LOWER THE GEAR?

Vle-THE MAXIMUM AIRSPEED WITH THE GEAR DOWN? NORMALLY, THE GEAR WILL ONLY BE DOWN IN RSVM SPEED?

THE AMT WILL CHECK THE GEAR?

IN SOME SITUATIONS IN QUICKLY RETRACTING THE LANDING GEAR EARLY? ALSO, SOME SITUATIONS THE GEAR MAY NEED TO BE LET DOWN?

THE INSTRUMENT GEAR GUAGE CAN BE CHECKED BY PRESSING THE CHECK BUTTON?

AS ELECTROHYDRAULIC LANDING GEAR USES A HYDRAULIC PUMP TO LOWER AND RAISE THE GEAR? THERE IS A INSTRUMENT GUAGE AND ALSO THERE IS A TURN HANDLE ALSO IF THE HYDRAULIC FAILS?

AS ELECTROHYDRAULIC SYSTEM USES A HYDRAULIC FUEL PUMP?

IF ANY EXHAUST GAS STALL THEN SHUT DOWN THE ENGINE OR MOST LIKELY THE ENGINE WILL ALREADY BE? THEN, LAND? AND, OF COURSE YOU WOULD TYPE EXTENGUISH IN THE LEGACY FLIGHT SYSTEM INPUT OR PULL THE KNOB?

A COMPRESSOR PISTON ENGINE OPERATES ON ENGINE INTAKE SENSORS FOR INLET TEMPERATE, MIXTURE WHICH GOVERNS FUEL TO AIR RATIO, AND CAL FLAPS TO LET OUT THE EXHAST?

AT HIGH ALTITUDES AN AUXILLARY PRESSURE MAY BE NEEDED TO STOP VAPORIZING OF FUEL?

AS RPM INCREASES THE MANIFOLD PRESSURE INCREASES?

AND, ROTARY PROPELLOR ENGINES HAS AN AIR INTAKE AND A WASTEGATE? THE WASTE GATE HAS A CONTROL SENSOR TO COMPRESS THE MANIFOLD PRESSURE?

A JET ENGINE HAS AN INTAKE, THEN WASTE GATE? IN BETWEEN THERE ARE ROTARY GEARS?

A TURBOCHARGER IS A EXHAUST AIR COMPRESSOR CONNECTED TO THE AIR INTAKE?

ALSO, THE RPM READS THE MAXIMUM OPERATING THROTTLE POWER?

THE RPM SHOULD COME UP TO 40 RPM OF THE MAXIMUM RPM? THE MANIFOLD PRESSURE SHOULD BE INCREASED WITH THROTTLE? THE MANIFOLD PRESSURE SHOULD BE RESEARCHED IN THE AIRPLANE MANUAL?

A FIXED PROPELLOR MUST ACCELERATE DOWN A RUNWAY TO WARM UP THE ENGINE? THERE IS NO SUCH THING AS A FIXED PROPELLOR PLANE?

THE RPM GUAGE DOES INDICATE THE NORMAL RANGE NEEDED TO WARM THE ENGINE?

IF AN ADJUSTABLE ROTARY BLADE PROPELLOR CAN OVERSPEED IF NOT EXERSIZED FIRST? THERE NEEDS TO BE A WARM UP ON THE RUNWAY?

IN THE ROTARY PROPELLOR PLANE THERE IS A ROTARY BLADE ANGLE STOP POSITION THEN THE RPM INCREASES? IN TAKEOFF THERE IS LESS OF A PITCH IN THE ROTARY BLADE TO CIRCULATE THE OIL?

THE ROTARY PROELLOR AIRPLANE THE GOVERNOR WORKS BY OIL PRESSURE WITH MORE PRESSURE TOWARDS MORE PITCH OR OPEN?

IN A ROTARY PROPELLOR THERE IS LESS THROTTLE TO KEEP THE PLANE ALOFT?

THERE IS USALLY AN ANGLE OF ATTACK GOVERNOR IN ROTARY PROPELLOR PLANE WHICH APPLIES A BLADE ANGLE? AS THE LOWER THROTTLE THE BLADES ARE SET TO MAXIMUM RPM BY MORE BLADE ANGLE AT LANDING?

BECAUSE THERE IS AN ANGLE OF ATTACK PERCENTAGE BEFORE A STALL IN FLAPS THE SETTINGS NOWADAYS IS 22 PERCENT THRUST PER 20 PERCENT OF THROTTLE?

TRIM IS USED IN SOME LANDINGS TO PUSH DOWN TO LOWER THE AIRPLANE ON THE RUNWAY?

THEN THERE IS LANDING WHICH SHORTER AIRFEILDS WHERE THE FLAPS WILL BE MORE TO PROVIDE LIFT WITH LESS ENGINE THRUST TO REACH THE RUNWAY?

THE PIOLT MUST RELATE THE AIRPLANE MANUAL FOR FLAP EXTENSION IN ROTATIONS?

PARASITE DRAG IS LIFT COEFFICIENT=DRAG-(X\15) WHERE X IS THE SURFACES?

THERE WILL BE AEROFOILS WITH TWO CAMBERS WHICH MAY INCLUDE TRAILING EDGE FLAPS TO PROVIDE ON ANGLE OF CAMBER? WITH AYSMETRICAL CAMBER THE AEROFOILS PROVIDE LIFT? THE FLAPS CAN ALSO BE USED TO LIFT THE AIRPLANE IN A ROTATION TAKEOFF?

A COMPLEX AIRPLANE HAS OVER 200 HORESPOWER ENGINE, RETRACTABLE LANDING GEAR, ENGINES CONTROL MAY BE PRESENT? THERE WILL BE FLIGHT INSTRUCTOR NEEDED?

I was searching for this video and finally I got your video Thank you very much 🙂 Just want to know that I'm studying on 777 engine which is GE-90 Type so is it okay if I get interviewed regarding the removal procedure is this video able to help me out?

34:09 to myself for later

super helpful, thank you

Awesome!! Thanks

I like the new style & voice.

Thank u

I got it (full book): www.faa.gov/regulations_policies/handbooks_manuals/aviation/amtg_handbook.pdf

I would like to have the pdf of that chapter 12. Where can I get it?

This got me hot and bothered

This really helps me, i cant stare at a book/screen for 3 hours so this is fantastic

Tu🎉

*chapter 😉

Unbelievably bad narration. These synthetic narrators are NOT ready for prime time! For Pete's sake man the material is free. You can't add just a TINY bit of your own value and read it ?

While very appreciative that this is on UA-cam, the AI voice is very tough to listen to and skips entire sections. At least a half a page at a time in places. Definitely makes it tough to study with

Thank you

Hallelujah there is a audio version of this book 🙏