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Aviation Skill Test Guide

The document outlines the Civil Aviation Requirements for skill tests and procedures for pilots operating commercial aeroplanes with an All-Up Weight (AUW) exceeding 5700 kgs. It details various emergency procedures, flight maneuvers, and instrument flight procedures that must be demonstrated during skill tests. Additionally, it specifies requirements for take-offs, landings, and handling abnormal situations, including engine failures and low visibility operations.

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Praveen Kumar
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0% found this document useful (0 votes)
57 views2 pages

Aviation Skill Test Guide

The document outlines the Civil Aviation Requirements for skill tests and procedures for pilots operating commercial aeroplanes with an All-Up Weight (AUW) exceeding 5700 kgs. It details various emergency procedures, flight maneuvers, and instrument flight procedures that must be demonstrated during skill tests. Additionally, it specifies requirements for take-offs, landings, and handling abnormal situations, including engine failures and low visibility operations.

Uploaded by

Praveen Kumar
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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SECTION 8

CIVIL AVIATION REQUIREMENTS


SERIES 'F'PART VIII 22ND DECEMBER 2016
CA 40/CA41
DGCA India
Page 2 of 2
License/Type Rating Skill Test/IR PPC
O Form for Commercial Aeroplanes with Rev 4 29 Oct 18
AUW exceeding 5700 kgs
35 M# ACAS/TCAS
be selected from 36 1to 36 8
Abnormal and emergency procedures (minimum of 3 M items shall
Inclusive) Fires including
36 1 M Fire dnlls eg Eng1ne, APU, Cabin, Cargo compartment, Flight deck, Electrical
Evacuat1on
362 M # Smoke control and removal.
363 M # Eng1ne failures, shut-down and restart, fuel jettison
364 M
Recognition and Management of Threat and Error( For lssuance of ATPL/IR)
365 M # Windshear at Take Off and Landing.
366 M Cabin pressure fa1lure/Emergency descent.
367 M Incapacitation of flight crew member
368 Other emergency procedures as outlined in the appropriate Aeroplane Flight Manual
37 Steep turns with 45° bank. 180° to 360° left and nght
warning device)
38# Early recognition and counter measures on approaching stall (up to activation of stall
38 1# Recovery from full stall or after activation of stall warning device in climb, cruise and approach
configuration.
39 Instrument flight procedures:
Adherence to departure and arrival routes and ATC instructions.
39 1MIR
392 IR Holding procedures.
393 M IR ILS-approaches down to a decision height (DH) not less than 60 m (200 ft):
3931 MIR manually, without flight director S
3932MIR manually, with flight director. (any one of 3.9.3.2 or 39.33)
3933M IR automatically, with Autopilot (see above)
3934MIR manually, with one engine simulated inoperative
NDB or VOR/LOCor RNAV approach down to the MDH/A
394 MIR
centerline from final approach
395 MIR Circling approach (if applicable) to a runway at least 90° off
MISSED APPROACH PROCEDURES
4
reaching decision height
4 1 IR Go-around with all engines operating after an ILS approach on
engine simulated inoperative after an ILS approach on reaching DH (see also
42IR Go -- around with one
3934)
43 MIR Rejected landing at (50 ft) above runway threshold and go-around.
5 LANDING(s)
flight on reaching DH
51 IR Normal landings also after an ILS approach with transition to visual
horizontal stabiliser in an any out-of-trim position S
Land1ng with sinulated jammed
52 #
53 Cross wind landings (aeroplane, if practicable)
partly extended flaps and slats
Traffic pattern and landing without extended or with
Landing with critical engine simulated inoperative S
55 M IV
3 and 4 engine aeroplanes)
56 M# Land1ng with tWO engines sirmulated inoperative (for
LOW VISIBILITY OPERATIONS INCLUDING CAT II/II(f applicable)
speed before eaching V1
61 M IR # RTO at minirnum authorized RVR at areasonable
etc)
(checking for SOP. task sharing, standard calls
62 MIR ILS approach using flight guidance system ground/arcraft equpment failure etc)
DH/AH (due reduced RVR,
63 MIR Go around- manual/automatic from
6 4 MIR Landing(s) manual/automatic from DH/AH with visual refereIce established
Take off in minimum T/O RVR <15Om
65 M #
/JRIPPC) PASETFAL (separate sheet fo raarks in case of fail)
OVERALL ASSESSMENT: SKILL TEST t 10 kts excepl in Approach phase when it would be +0/0kts) TRORAYAI
(Limitations: - Height + 100' > 15 Sec, Direction 10 Speed
DE/Examiner
Pilot under Check
Mandatory remarks in case of failure/s
FlightSafety
Textron Aviation
CIVIL AVIATION REQUIREMENTS SECTION 8
SERIES F' PART VII 22ND DECEMBER 2016
Appendix 6
DGCA India CA 40/CA41
Page 1 of 2
License/Type Rating Skill Tes/IR PPC Form
for Commercial Aeroplanes with AUW Rev 3 01 Jan 17
exceeding 5700 kgs
QPERATOR TEST ON SIMULAIOR LEVEL D/D) TEST DATE TESTIFLIGHT TPE OF TEST
ho
&AEROPLANEI TIME DURATION SKILL TEST
SIMULATOR)
MAnACAsn
AEROPLANE DAYONIGH) AEROPLANE/SIMULATOR
TYPE.
D YON/TAKE OFF OFFNANDING
REGISTRATION D
CSGOxLS
PILOT UNDER CHECK
LU-AO313 LICENSE NUMBER ,DE/EXAMINER AUTHOPISATIONICENSE
SANsA kumaRArle 3ne NUMBER

CREW STATUS SEAT OCCUPIED


CocHni fd.344
Noto. For ass95snent enter "S" (Sat1sfactor), "U (Unsatisfatrn OP NA (Nt
TRAINEELICENSED applicable). Iterns marked "H" to be completed only on Simulator
PICCO-PILOT skill test/PPC "IR"is mandatory for instrurnent rat1ng Any eng1nete1erSES
LHSkHS itoms narkod # Conducted on aeroplane are to be urnulated only thrah tosn drls

EXERCISE
S/UINA
1 FLIGHT PREPARATION
11 Performance calculation
12 Aeroplane external visual inspection, location of each item and purpose of inspection
13 Cockpit inspection NA
14 M Use of checklists prior to starting engines, starting procedures, radio and navigation
15 Taxying in compliance with ATC orinstructions of Examiner
16 M Pre-flight checks
2 TAKE-OFF(s)
21 Normal take offs with different flap settings
22 IR Instrument take off. transition to instrument flight during rotation or immediately after airborne
23 Cross wind take-off (aeroplane, if practicable)
S
24 Take-off at maximum take-off AUW (actual or simulated maximum take-off AUW)
25IR Simulated engine failure after V2
251 MIR # Simulated engine failure between V1 and V2
252 M# Rejected take-off at a reasonable speed before reaching V1
3 FLIGHT MANOEUVRES AND PROCEDURES
31 Turns with and without spoilers (as applicable)
32 # Tuck under and Mach buffets and other specific flight characteristics of the Aeroplane (e g Dutch Rol)
33 Normal operation of systems and control
34 Norrnal and abnormal operations of following systems (minimum of 3 Mitems shall be selected from
34 to 35 inclusive
340 M Engine (if necessary propeller)
34 1 M Pressurisation and air- Conditioning
34 2 M Pitot/stat1c systermn
343M Fuel systern
34 4 M Eletncal systerm
345 M Hydrauic systerm
34 6 M Flight control and Trim- systerm
34 7 M Antt and de icang systerm, Glare shield heatng
34 8 M Autopilot/F lighit director
349 M Stallwarning devices or stall avodance devices, and stability augma
34 10 M Ground Proxirnity Warning System, Weather radar, Radio altimeteA Sponder
34 11 M Radios, Navigation equiprment, Instruments, FlightManagemen8m
34 12 M
34 13 M
Landing gear and brake- system
Slat and flap systerm
FlightSatety
Textron Aviation
34 14 M Auxiliary Power Unit.

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