All About CAR-66 Module AME Licence Examination 2017 :: Full Detail

Point -1 

Candidates desirous of appearing for examination are required to submit their application for roll number ONLINE under https://www.viman.gov.in 

Point - 2

Examination Portal for the AME Modular Examination 1 st Session of 2017, will remain open from 1 st Feb 2017 to 15th Feb 2017, for all categories of examination Papers.

Point - 3

Application form can be seen on website only after completion of registration process on Viman Portal.

Point - 4

The Centers for online examinations are divided in the following zones:


ER- Zone Centers :        Kolkata, Guahati, Bhubaneshwar, Patna 

WR -  Zone Centers :     Mumbai, Bhopal, Ahemadabad

NR - Zone Centers :       Lucknow, New Delhi

SR- Zone Centers :         Chennai, Hyderabad, Kochi

BLR Zone Centers :        Bangaluru

General Instruction( For Applying Module Examination)

Before applying for examination all candidates are advised to read the respective chapter of the latest available User Manual, Notices and Instructions carefully. Candidates must select the correct applicable QPREF(s) with respect to the desired examination paper from the list of papers & applicability given in the Annexure of User Manual.

In a particular session initially, a candidate will be allowed to appear in any ONE category ( A1/A2/A3/A4/B1.1/B1.2/B1.3/B1.4 /B2 ) only and Maximum FOUR QPREF (s) of that particular category.

As per applicable rule, FEES to be paid online @ Rs.2500/- per Examination Paper (QPREF).

Once examination application form submitted successfully, no change/ alteration request will be entertained by CEO and fees will not be adjusted/ refunded under any circumstances.

Candidates are NOT REQUIRED to forward any hard copy of the registration form and supporting document to CEO.

Applicable Modules for BAMEEC/BAMEL Hoders(Paper 3)

ANNEXURE-III
MATRIX FOR BAMEL/BAMEEC HOLDERS TO AQUIRE CATEGORY-A LISENCE
S.N	BAMEL/BAMEECPRE-CAR 66	LICENSECategory	Module OR Sub Module (chapters) to be PASSED	QPREF to be passed
1	HEAVY AIRCRAFT &	A1	11.5,11.6,11.14,11.19, 11.20, &	1101
	JET AEROPLANE ENGINE		11.21 OF 11A
			5 (ALL)	0500
2	LIGHT AIRCRAFT &	A1	11A (ALL)	1100
	JET AEROPLANE ENGINE-		5 (ALL)	0500
3	HEAVY AEROPLANE AIRCRAFT	A1	1517 (ALL)(ALL)	15001700
			11.5,11.6,11.14,11.19, 11.20, &	1101
			11.21 OF 11A
			5 (ALL)	0500
4	AEROPLANE JET ENGINE	A1	11A5 (ALL)(ALL)	11000500
5	LIGHT AIRCRAFT &	A2	11.5,11.6 & 11.14 OF 11B	1111
	PISTON AEROPLANE ENGINE		5 (ALL)	0500
6	LIGHT AIRCRAFT	A2	11.5,11.6 & 11.14 OF 11B	1111
	AEROPLANE		1617 (ALL),(ALL)	16001700
			5 (ALL)	0500
7	PISTON ENGINE	A2	11B (ALL)	1110
	AEROPLANE		5 (ALL)	0500
8	ROTARY AIRCRAFT	A3	12.7, 12.8,12.15,12.17,	1201
	& JET ENGINE		12.155 (ALL)& 12.18 OF 12	0500
9	ROTARY AIRCRAFT	A3	1512.7,(ALL)12.8 12.17,12.18	15001201
			12.15 & 12.19 OF 12
			5 (ALL)	0500
10	JET AIRCRAFT ENGINE ROTARY	A3	125 (ALL)(ALL)	12000500
11	ROTARY& PISTON AIRCRAFT ENGINE	A4	12.7,12.1512.8& 12.1912.17,12.18OF 12	1201
			5 (ALL)	0500
12	ROTARY AIRCRAFT	A4	16 (ALL)	1600
			12.7,12.1512.8& 12.1912.17,12.18OF 12	1201
			5 (ALL)	0500
13	PISTON ENGINE	A4	12 (ALL)	1200
	ROTARY AIRCRAFT		5 (ALL)	0500

Annexure -1 
Details of CAR66 Modular Examination Papers

Details of CAR-66 Modular Examination Papers					ANNEXURE-I
www.dgcaquestionpapers.in
Sl.	Module	AllotedQPREF	Question Paper Reference Number (QPREF) Description	Applicable	MultipleNo of	Allowed Time
No	No	by CEO		Category	QuestionsChoice	(Minutes)
1	3	0300	Electrical Fundamentals	A	20	25
2	3	0310	Electrical Fundamentals	B1 & B2	52	65
3	4	0400	Electronic Fundamentals	B1	20	25
4	4	0410	Electronic Fundamentals	B2	40	50
5	5	0500	Digital Techniques Electronic Instruments Systems	A	16	20
6	5	0510	Digital Techniques Electronic Instruments Systems	B1.1 & B1.3	40	50
7	5	0520	Digital Techniques Electronic Instruments Systems	B1.2 & B1.4	20	25
8	5	0530	Digital Techniques Electronic Instruments Systems	B2	72	90
9	6	0600	Materials And Hardware	A	52	65
10	6	0610	Materials And Hardware	B1	72	90
11	6	0620	Materials And Hardware	B2	60	75
12	7	0700	Maintenance Practices	A	72	90
13	7	0710	Maintenance Practices	B1	80	100
14	7	0720	Maintenance Practices	B2	60	75
15	8	0800	Basic Aerodynamics	A	20	25
16	8	0810	Basic Aerodynamics	B1 & B2	20	25
17	9	0900	Human Factors	A	20	25
18	9	0910	Human Factors	B1 & B2	20	25
19	10	1000	Aviation Legislation	A	32	40
20	10	1010	Aviation Legislation	B1 & B2	40	50
21	11A	1100	TurbineSystemsAeroplane Aerodynamics,Structures And	A1	108	135
22	11A	1101	TurbineSystemsAeroplane(For OLD BAMELAerodynamics,Structurescandidates required to PASSAnd)	A1	32	40
23	11B	1110	PistonSystemsAeroplane Aerodynamics,Structures And	A2	72	90
24	11B	1111	PistonSystemsAeroplane(For OLD BAMELAerodynamics,Structurescandidates required to PASSAnd)	A2	20	25
25	11A	1120	TurbineSystems Aeroplane Aerodynamics,Structures And	B1.1	140	175
26	11A	1121	TurbineSystems Aeroplane(For REMOVALAerodynamics,StructuresOF Limitation 3 & 6 )      And	B1.1	40	50
27	11B	1130	PistonSystemsAeroplane Aerodynamics,Structures And	B1.2	100	125
28	11B	1131	PistonSystemsAeroplane(For REMOVALAerodynamics,StructuresOF Limitation 3 & 6 )     And	B1.2	20	25
29	12	1200	Helicopters Aerodynamics,Structures And Systems	A3 & A4	100	125
30	12	1201	Helicopters(For OLD BAMELAerodynamics,Structurescandidates required to PASS) And Systems	A3 & A4	32	40
31	12	1210	Helicopters Aerodynamics,Structures And Systems	B1.3 & B1.4	128	160
32	12	1211	Helicopters(For REMOVALAerodynamics,StructuresOF Limitation 3 & 6 )        And Systems	B1.3 & B1.4	40	50
33	13	1300	Aircraft Aerodynamics, Structures and Systems	B2	180	225
34	13	1301	Aircraft(For REMOVALAerodynamics,OF Limitation Structures3 )        and Systems	B2	52	65
35	13	1302	Aircraft(For REMOVALAerodynamics,OF Limitation 4Structures)        and Systems	B2	52	65
36	13	1303	Aircraft(For REMOVALAerodynamics,OF Limitation Structures5 )        and Systems	B2	52	65
37	14	1400	Propulsion-	B2	24	30
38	15	1500	Gas Turbine Engine	A1 & A3	60	75
39	15	1510	Gas Turbine Engine	B1.1 & B1.3	92	115
40	16	1600	Piston Engine	A2 & A4	52	65
41	16	1610	Piston Engine	B1.2 & B1.4	72	90
42	17	1700	Propeller	A1 & A2	20	25
43	17	1710	Propeller	B1.1 & B1.2	32	40

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