KA350 Flashcards
Privileges of pilot type ratings
The holder of a pilot license and a pilot type rating is authorised to exercise the privileges of the license in an aircraft of the type covered by the rating. (CASR 61.770)
Limitations on exercise of privileges of pilot type ratings. Flight test in sim, single and multi-crew operation, IFR operation.
Flight test in flight simulator: authorised to exercise privileges of rating as PIC only if holder has at least 25 hours of flight time as pilot of an aircraft covered by the rating.
Single-pilot and multi-crew operation: holder of single-pilot type rating authorised to exercise privileges in multi-crew operation only if they hold a multi-crew type rating or completed an approved course of training in multi-crew cooperation.
The holder of a multi-crew type rating is authorised to exercise the privileges of the rating only in a multi-crew operation.
IFR operation: holder of pilot type rating authorised to pilot an aircraft under the IFR only if the flight test for the rating is conducted under the IFR or the holder has completed an IPC in an aircraft covered by the rating.
Part 135 Single Pilot Required Equipment
AATTCCVV PADAW
Airspeed indicator + Mach (2 for multi-crew)
Altimeter x2
Turn and slip indicator (2 for multi-crew)
Temperature (OAT)
Compass
Clock
Vertical speed indicator (2 for multi-crew)
Vacuum gauge
Pitot heat
Attitude indicator x3 (over 5700kg)
Direction indicator (2 for multi-crew)
Assigned altitude indicator (for CTA)
Altitude alerting system (Px turbine CTA >15000’)
Weather radar + Windshield wipers or similar
2 GNSS (TSO C145, C146, C196) or 1 GNSS (at least TSO C129) + VOR or ADF
Autopilot with heading and altitude hold, can be U/S VMC by day
ELT + FDR+CVR + ACAS
<5700kg carrying pax must be fitted with TAWS
>5700kg carrying pax must be fitted with GPWS
ASI, Altimeter, VSI must have alternate static or dual flush static ports.
AI, DI must have alternate power supply. 2nd AI must last 30 minutes after electrical failure.
Required aircraft lighting
Instrument lights with standby power and intensity control
Pilot and passenger compartment lights
Landing lights x2 (or two filaments)
Nav and anti-collision lights
Torch for each crew member
Takeoff Minima
Standard is 300ft ceiling + 2km visibility.
King Air 350 is a qualifying multi-engine aeroplane: single pilot with operative autofeather.
In the event of an engine failure is capable of maintaining terrain clearance until reaching the LSALT/MSA.
Ceiling 0ft + Visibility 800m. 550m Vis but only if:
- the runway has illuminated edge lighting has spacing less than 60m
- the runway has centreline lighting or centreline markings
- lighting supported by a secondary power supply with switchover of 1 second or less
- if the aerodrome is a non-controlled aerodrome or a controlled aerodrome where ATC is not in operation — the take-off is conducted by day and the aerodrome is one at which the carriage of radio is mandatory.
Landing Minima
For an RNP APCH-LNAV/VNAV, an RNP APCH-LPV, or a precision approach
procedure — the minimum altitude must not be below whichever of the following is the highest:
(a) the DA or DH specified on the instrument approach chart for the IAP being conducted
(b) relevant minima specified in the AFM
(c) relevant minima specified in the operator’s exposition or operations manual
For an RNP APCH-LNAV/VNAV, an RNP APCH-LPV, or a precision approach procedure — the minimum visibility must not be below whichever of the following is the highest:
(a) the RVR or visibility specified on the instrument approach chart for the IAP being conducted
(b) relevant minima specified in the AFM
(c) relevant minima specified in the operator’s exposition or operations manual
(d) 800 m, but only if:
(i) the TDZ RVR report is not available; or
(ii) the approach lighting system normally available beyond 420 m from the
runway threshold is inoperative;
(e) 1 200 m, but only if:
(i) the approach cannot be flown to at least the landing minima using a flight director, a HUD or an autopilot; or
(ii) the aircraft is not equipped with an operative failure warning system for the primary attitude and heading reference systems; or
(iii) high intensity runway edge lighting is not in operation; or
(iv) the approach lighting system normally available beyond 210 m from the
runway threshold is inoperative;
(f) 1 500 m — but only if the approach lighting system normally available for the runway is inoperative;
1.5 times either the RVR or the visibility specified on the instrument approach chart for the IAP being conducted — but only if:
(i) a lighting failure has occurred on a runway at a controlled aerodrome; and
(ii) doubled spacing of runway edge lights results.
Note At a controlled aerodrome, in the event of failure of 1 electrical circuit on a runway equipped with interleaved circuitry lighting, pilots will be notified of a doubled spacing of runway edge lights, that is, from 60 m spacing to 120 m spacing.
Departure Terrain Clearance
When instructed by ATC or flying a SID, established by 5nm.
Not departing via SID, terrain clearance is pilot responsibility. Must be assured to LSALT/MSA, including one-engine inoperative.
Can refer to APG for departure plan.
Obstacle Clearance and Gross Gradient Requirements
Standard Instrument Departure (SID): Climb at minimum of 3.3% (including OEI) or as chart specifies.
Missed Approach Point (MAP): Climb at minimum of 2.5% (including OEI). Provides 100ft of terrain clearance.
Minimum Safe Altitude (MSA): Provides 1000ft terrain clearance.
Net gradients are gross gradients reduced by 0.8%.
Assuming critical engine failure at V1
1st Segment (>0%) +ve: From 35ft AGL until the aircraft completes the gear retraction cycle.
2nd Segment (>2% to 400ft) >1.2%: from completion of the gear retraction cycle until reaching 400ft AGL (or higher until clearing all relevant obstacles).
3rd Segment (>1.2%) >0.4%: Level segment where aircraft is accelerated, flaps retracted and appropriate climb power set.
4th Segment (>1.2%) >0.4%: Extends from level segment to 1500ft AGL (or higher if terrain demands).
2nd Segment is generally most limiting for takeoff performance.
En-Route Requirement to have a positive slope at 1000ft above all terrain and obstructions within 5nm of the intended track to be flown OR clear all terrain and obstructions by at least 2000ft vertically, within 5nm of the intended track to be flown.
Must have a positive slope at 1500ft above the aerodrome where the landing is assumed to be made after the engine failure.
Pressure Altitude Calculation
PA = Airport Elevation + [30 x (1013-QNH)]
Takeoff and Landing Distance Requirements
Takeoff data from Beechcraft unfactored.
Landing data from Beechcraft (can only account for 70% of actual required) factored by 1.43 and an additional 1.15 (equivalent to 60% of actual required) on the resultant distance if the runway is wet.
Privileges of Instrument Rating
Allows you to pilot an aircraft under the IFR or at night under the VFR.
Index
IFR Takeoff+Landing Minima: MOS Part 91 Chapter 15
Fuel Requirements: MOS Part 135 Chapter 7
TODR+LDR and Climb Gradients: CAO 20.7.1B
Holds, Approaches, Weather, Minima, SID, STAR: AIP ENR 1.5
Pilot Type Ratings: CASR Part 61 61.770
Required Equipment: CASR Part 135 Chapter 11
Performance T/O, Climb, Landing: CASR Part 121 Chapter 9
