In the military, I flew and completed formal training/qualified in:
T-34C
T-2C
TA-4J
F-14A
E-2C
F-14B
F/A-18C/D
Additionally, I flew in the following with a qualified pilot:
TH-57
HH-60
S-3B
EA-6B
F-5E
F-16N
I’ve flown the following civilian airplanes but only as second pilot, no training:
C-152
C-172
C-182 turbo
Citation I
Stearman PT-17
Piper Archer
Cirrus SR-20
Nanchang CJ-6
Formal training/type rating on the following civilian airplanes:
Piper PA-44 Seminole (just to get my ATP)
Airbus A-320
Boeing 747-400
Boeing 757/767
From that background, let me say that yep, six weeks, to several months of is necessary to get a pilot trained to operate that airplane with sufficient safety margins (or combat effectiveness) to allow them to be considered qualified.
Look airplanes aren’t like a car. They just aren't. They’re far, far more complex. The systems vary. Procedures vary. Handling qualities vary. Even the act of just flying straight and level requires that you have the correct speed for the current configuration, but...airspeeds vary across types and within types depending on temperature, altitude, weight and configuration.
Emergency procedures vary, and must be memorized, you don't have time to look some things up. They must be memorized and done instantly.
The operators manual for the 757/767 is over 2,600 pages long and it must be read, understood, and followed. You can't just "get it close". You must get it precisely right, every time.
*****
So, let's examine a minor system problem in a 767-300, and compare that with a warning light on your dash of a car. This is just one of a great many potential failures and in training, you will experience this, in a simulator, and have to fly the airplane to a safe landing.
You are expected to know what each of the systems are (and I don't have time to explain each one, but if you're a pilot, you'll understand) and to which switch the steps are referring. Here is a 767-300 overhead panel, for reference, as you follow along...so that you can see each of the switches.
View attachment 173868
So, you get an EICAS warning for center hydraulic system pressure.
1. C AIR HYD DEMAND PUMP selector - ON
2. Chose one
SYS PRESS light extinguishes - continue normal operation.
SYS PRESS light remains illuminated - go to step 3.
3. C AIR HYD DEMAND PUMP selector - OFF
4. C1 and C2 ELEC HYD PRIMARY PUMP switches - off
5. Speed brake lever - Down. Do not arm speedbrakes for landing.
6. Manually extend speedbrakes for landing.
7. Use flaps 20 and Vref 20 for landing
8. Do not autoland.
The following items are inoperative:
- Center autopilot
- HMG#
- Right autopilot stabilizer trim
- Some spoiler panels on each wing. Roll rate may be reduced in flight. Speed brake effectiveness will be reduced in flight and during landing.
- Center system hydraulic power to stabilizer trim inoperative. Left system powers trim at one half rate.
- Normal flap operation inoperative. Alternate flap operation is needed. Allow 3 minutes for flap extension during approach.
- Normal landing gear extension inoperative. Alternate gear extension is needed.
- Automatic Speed brake system inoperative. Manual deployment is needed.
9. Check the non-normal Configuration landing distance tables in the performance chapter*
Now you have to figure out where to take the airplane. This is based on runway length, airport and enroute weather, approach facilities (including any that may be NOTAMed inoperative on that day), airport traffic, fuel state, landing weight and airport ramp/taxiway size and weight bearing capacity, emergency facilities, including fire/rescue capabilities (many airports can't handle a widebody), aircraft performance with this malfunction, terrain and missed approach calculations, geo-political factors (internationally, this matters) and pilot familiarity.
So, you get an oil pressure light on your dash, you pull over and shut down the car. Simple. Easy by comparison. Looking for a safe place to pull over, and you don't even have to worry about what speed keeps you in the air, compared with every consideration I just listed?
Child's play by comparison.
*****
That is what you learn in training. Every airplane is different. You must understand the machine completely just to operate it safely.
In the military, you learned to operate it safely and then you learned to employ the weapon system - a whole different level of complexity.
So, back to the question - is that much training needed? Yeah. Every time. You can't just jump in and go. Only Hollywood believes that. In the real world, it's fantasy. You cannot expect to fly an airplane without learning it first.
# Hydraulic motor generator. A back-up power source used for long range operations.
*This is a multi-step process, based on performance at sea level, zero wind, using full reverse, Vref +5 at touchdown, maximum manual braking, touchdown at 1,000 feet down runway, standard temperature, and less than 1 degree runway slope. It requires adjustments for gross weight, height above sea level, each knot of tailwind, each knot flown above Vref +5, inoperative reversers, and then the addition of a 15% safety margin. This step determines the minimum runway required to land this airplane with this problem on this day and it must be performed before a determination of where to land can be made.
Edit: a bit of exposition. The center system is normally pressurized by two electric hydraulic pumps, each one powered by a separate electric bus, so that in event of electric failure, you still have center system hydraulics. The first step of the procedure is to try and restore pressure using the back up, or demand, pump. If the cause of the system pressure loss was the failure (electric or mechanical) of the system pumps, then this step might resolve the system pressure. But if the failure was due to fluid loss, then, in step 2, you move on and shut off all the pumps to prevent further damage. Running a high pressure pump with no fluid can cause an overheat - leading to other problems. The pump itself is already toast, we just don't want it catching on fire from an overheat.
You're expected to know how to emergency extend both the flaps and the gear. There are checklists to back you up on the performance of those tasks.
The use of flaps 20 for landing, as opposed to the normal positions of flaps 25 or 30, allows the airplane to meet climb gradient criteria in the event of a missed approach. A normal go around starts with the application of power, then retraction of flaps to 20, then raising the gear. But in our airplane with a problem, all of this has changed. Some of it can't be done. A go around requires the airplane to meet certain climb gradient criteria, and we have to modify how we configure the airplane for landing to ensure that we can meet those criteria (or we potentially impact terrain - not good - on a missed approach).
The flap emergency extension system would not retract the flaps at the normal rate, meaning there would be more drag if normal flaps were to be used for landing. Moreover, the emergency gear extension process leaves the gear down permanently, so, as a result, the airplane has more drag should a missed approach be executed. Selection of flaps 20 for landing, vs. a normal setting, changes the drag characteristics, handling qualities, approach speed, landing distance, and visual cues on landing, but we accept all of those parameter changes to get better climb performance should a go around be required.
Did everyone find the pertinent cockpit controls and indicators for this emergency from the diagram? You don't have time to be fumbling around...