DGCA CAR Paper-1 June,2013 Question Paper.
by:-
Mukul Sareen
1. organisation getting approval in form 133B require fee in;a. form 133A
b. FORM 62
C. fORM 133
2. AIC & NOTMAS ISSUE UNDER
A. 133A*
B. 133B
C. 133C
3. APPROVAL FOR ALTERNATIVE DESIGN ORG. APPROVAL IN FORM
A. CA 80
B. CA 81*
C. CA 82A
4. ITSO A IN SUB-PART
A. O*
B. P
C. L
5. RULE RELATED TO 3A UNDER WHICH PERMISSSION REQUIRE- CENTRAL GOVT. & AUTHORISED PERSON BY;
6. DROPING IN ANY RELIGIOUS PLACE FROM A/C OVER CROWD REQUIRES
A. RULE26*
B. PERMISSION GIVEN BY MEGISTRATE OF DELHI
C. ,, ,, ,, COMISNOR OF DELHI.
7. ANY MALFUNCTION ACROSS IN FLIGHT REQUIRES A/C ACCORDING DURING CONDITION
A. CCL
B. ECL*
C. MALFUNCTION CHECK LIST
D. NORMAL CHECK LIST
8. RULE-7
Ans. DOCUMENTS TO BE CARRIED ON BOARD.
9. RULE-55
Ans. SUSPENSSION OR CANCELATION OF C OF A.
10. RULE 133C
Ans. FEE REQUIRED FOR APPROVAL OF ORG.
11. IF ACCOUNTABLE MANAGER IS ABSENT FOR --- DAYS APPROVAL CAN SUSPEND
ANS. 60 DAYS
(30DAYS FOR CI)
12. A/C SYSTEM RELIABILITY IS MEASURED BY
A. NO. OF PILOT DEFECT REPORT/1000FLT.HRS*
B. TOTAL DEFECT REPORT PER 100HRS
C. TOTAL DEFECT REPORT AT 1000HRS.
13. IN CASE OF COMMERTIAL AIRCRAFT TRANSPORT , PRE-FLT INSPECTION IS RESPONSIBILITY OF;
A. OWNER
B. OPERATOR*
C. OWNER/OPERATOR
D. RAO.
14. RESPONSIBILITY OF COMERTIAL TRANS. A/C FOR PRE-FLT INSPECTION
ANS. OPERATOR (tHis que has been repeated twice in this atempt)
15. WHO WILL ACCESS TO DGCA FOR CHECKING FOR CONTINUED AIRWORTHYNESS OF A/C
A. OWNER
B. OPERATOR
C. OWNER/OPERATOR*
D. RAO
16. IN REGISTRATION MENTION
A. TYPE OF A/C;
B. NO OF PASSANGERS
C. NO OF CREW
D. ALL
17. WHICH ONE IS CORRECT.
A. AIRSHIP NON POWER DRIVEN , HEAVIER THAN AIR
B. GLIDER POWER DRIVEN , HEAVIER THAN AIR
C. AMPHIBIAN POWER DRIVEN. HEAVIER THAN AIR
D. ALL
18. LIMITATIONS IN APPROVAL SCHEDULE CA FORM 3
A. TYPE A/C*
B. ENGINE
C. AIRFRAME
D. ALL
19. MOE GIVEN IN WHICH
Ans. 145A:70
20. MATERIAL SPECIFY IN ACCEPTANCE IN 145
A. 145A'70
B. 145A;60
C. 145A;42
D. 145A;40
21. 145APPROVEDL ORG. REQUIRE APPROVAL IN WHICH CAT-A
A. LINE STATION LOCATED AT BASE STATION
B. BASE MAINTAINCE RESTRICTED IN LINESTATION
C. BOTH
22. 145 REQUIRE OR MEY BE APPROVED IN CAT A RATING MEY BE APPROVED
A. BASE MAINTANC.
B. LINE MATAINC.
C. BOTH BASE AND LINE
D. ALL
23. CHANGE IN 145 ORG. NOT REQUIRED TO REPORT TO DGCA
A. ORG. NAME
B. ADDITIONAL LOCATION
C. CERTIFY STAFF
D. ANY PERSON ....
24. AN UNINTENTIONAL LANDING AFFECT ON ACCOUNT OF FAILURE MALFUNCTION OF AN A/C COMPONENT SYSTEM IS CALLED
A. FORCE LANDING
B. NECESSARY LANDING
C. NORMAL "
D EMERGENCY*
25. CAR-M A/C MAINTAINC. PROGRAM APPROVAL WHICH IS CORRECT.
A. AMP IS APPROVED BY DGCA
B. AMP IS APPROVED BY CAMP ITSELF & THIS PROCEDURE GIVEN IN COME AT APPROPRIATE CONDITION
C. AS IN "A" AMP SUBMITTED TO RAO BEFORE 15DAYS THEIR AFFECTIVITY
D. ALL
26. TECHNICAL LOG BOOK RETAINED FOR A PERIOD OF
Ans. 36MONTHS
27. ENGINE OR PROPELLER LOG BOOK KEPT FOR
Ans. 12months
27. which cat liscence required fro overhauling of equipment
a. cat-x ICAO-1
B. CAT-X ICAO2
C. CAT-X ICAO3
28. DGCA ISSUE AERONAUTICAL INFO. CIR. (AIC) UNDER
ans.133A
29. unit of speed
A. 1KN/MIN
B. 1KN/HR*
C. 10MILES/MIN
D. 1 AERONAUTICAL/MIN
30. QUANTITY OF UNUSABLE FUEL IN GIVEN IN;
TYPE CERTIFICATE/ FLIGHT MANNUAL
C OF A
C OF R
ALL
31 ACCORDING TO CAR145 INDEPENDENT AUDIT IS CARRIED OUT.
1. CHECK AT EVERY 12MONTHS
2. OR UNDIVIDED OVER THE 12MONTHS PERIOD IN ACCORDANCE WITH SCHEDULED PLAN
3. IT MAY BE CARRIED OUT BY AN AUTHORISED PERSON (CHECK). NOT RESPONSIBLE FOR AIRWORTH.
4. ALL
32. RULE FOR FUELING
Ans. 25A
33. GYROHORIZON, INDICATOR, DIRECTIONAL GYRO MAXIMUM OVERHAULING PERIOD IS
ANS. 2YEARS/1000HRS( JO BHI PHELAY PURA HU JAIY)
34. A/C NOT IN AIRWORTHYNESS CONDITION BUT IT MEY BE SAFE TO FLY OVER SPECIFIED RAO CALLED
ANS. PERMIT TO FLY
35. AN OPERATOR SHALL IMPLIMENT AS SAFETY MANAGEMENT SYSTEM INCLUDED
1. TYPE CERTIFICATE PROVIDER IDENTIFIED HAZZARD
2. AS IN 1, AND ISSUE ITS REMEDIAL ACTION
3. PROVIDE TO CONTINOUS MONITORING AN REGULAR ASSESMENT OF SAFETY LEVEL ACHIEVED
4. AS IN 3, AND AIM TO MAKE CONTINOUS IMPROVEMENT TO THE OVERHAUL LEVEL SAFETY
36. SHELL MODEL. S, H,E,L,L STANDS FOR
37. A PERSON NOT AWARE TO REMOVE SCREW AT DARK NIGHT MEY BE FALL THE SCREW FROM THE PERSON MATCH
A. LIVE WAVE- SOFTWARE
2. LIVEWARE- __ METAL MISMATCH
3. HARDWARE- ENVIRONMENTAL MISMATCH.
4. ALL
38. MTCS
1. ACTIVE FAILURE NOT RECOGNIZED
2. LATENT FAILURE NOT RECOGNIZED
3. ACTIVE FAILURE IS MORE DANGEROUS THEN LATENT FAILURE
4. LATENT FAILURE OS MORE DANGEROUS THEN LATENT
39. MEL MEY INCLUDE
1. LANDING GEARS
2. WINGS
3. APU*
40. FERRY FLIGHT PERMIT MEY BE ISSUED
1. FLY AT MAIN BASE WITH PASSANGERS
2. FLY AT PLACE WHERE MAINTAINC. CAN BE DONE
3. FLY AT MAIN BASE WITHOUT PASSANGERS TO MAINTAINCE TO BE DONE ON A/C*
41. ___ WEIGHT OF AIRCRAFT DONE WHERE 2000KG LESS(INCOMPLETE QUE)
1. 1YEAR
2. 5YEARS-IN CASE MORE THAN 2000KG
3. WHEN ANY REPAIR / MODIFICATION
4. ALL
42. DUPLICATE ISSUE OF C OF A FEE
1. 10% OF C OF A
20%
30%
15%
43. SERIES F MAY SEEK APPROVAL IN
1 A-MANUFACTURING
2 E-FUELING & SPECIAL PRODUCTS
3 G-TRAINING INST.
4 BOTH 2,3
44. RELIABILITY OF A ENGINE FITTED IN A/C SHALL BE MEASURED IN TERMS OF
1 NO. OF IFSD
NATURE OF IFSD
3. BOTH*
45, REPLACING A COMPONENT AT SPECIFIED TIME IN AMM REQURES A COMPONENT FOR BENCH CHECKED, INSTU CHECK & TEST
1 HARDTIME
2 ON CONDITION*
3 CONDITION MONITORING
4 ALL
46. ENGINE DAMAGE MEANT REMOVAL OF ANY ENGINE ANT ITS REPLACEMENT BY
1 OVERHAUL ENGINE
2 AN ENGINE REMOVAL FROM ANY OPTHER POSSITON TO SAME A/C OR ANY OTHER A/C
3. REINSTALLATION OF THE SAME ENGINE ON THE SAME A/C ITS ORIGINAL OPSSITION WOULD NOT CONTRIBUTE AM ENGINE CHANGE FOR THIS PERPOSE
4 ALL
47. STORAGE SELF LIFE OF RUBBER PAERTS FOR HYDRAULIC & __ COMPONENT ARE
ANS 6YEARS & FOLLOW MANUFACTURE INSTRUCTIONS
48. REQUIRED FOR INSTRUMENTAL & EQUQMENT FOR VFR
1. ALT. ASI
2. VFR
3. FUEL INDICATOR, CHT INDICATOR & __
4 ALL*
49. ENGINE OIL COMPEPTION CHT & AIRFRAME SCTRUCTURE , ENTRY IS DONE IN
1 ENGINE LOG BOOK*
2 AIRFRAME
3 ENGINE AIRFRAME LOG BOOK
4 ALL
50 MTCS
ANS UNSUABLE FUEL IS NOT A PART OF EMPTY WT.
51. CAR 145 MAINTANC. AN A/C
1. SINGLE ENGINE A/C COMMERCIAL OPR.
2. MTOW LESS 5700KG COMMERCIAL OPERATOR
3. MI 720 HELICOPTOER
4 ALL*
52. REQUIREMENT FOR APPROVAL OF CAR145
1. REQUIREMENT IN ACCORDANCE 30B
2. STANED SIGN BY ACCOUNTABLE MANAGER OF APPROVAL ORG. IN CA FORM & GIVEN TO DGCA
3. BOTH
4. ALL ABOVE
53. IN CASE OF AGEING A/C MANUFACTURE PROVIDE A DOCUMENT FOR OPERATION OF SAFETY OF A/C
ANS= SSID, CPCP, ( + RAP)
54. A/C IS GROUNDED FROM MAIN BASE AND NO APPROPRIATE MAINTAINC. FACILITY FRO MAINCS. THEM
1. A RELATION MAKE A OPERATOR FRO MAINTAINC.
2. OPERATOR MEY ISSUE A ONE OFF AUTHORISATION TO PERSON
3. ORGANISATION MEY ISSUE ONE OFF AUTHO. TO A PERSON
4. AS IN 3, CHEAK APPROPRIATE KNOWLADGE AND MAINTNC. EXP. OF THE PERSON
55, EMBODIMENT & REPAIR GIVEN IN CAR21 WHICH SUBPART
ANS = F
56 PREVENTIVE MAINTC. IS WHICH MAMINTNC.
1. HARDTIME
2. ON CONDITION
3. CONDITION MONI.
4 BOTH 1,2,
57, WHEN PERFOMING A/C REVIEW ENTRY IN WHICH LOG BOOK
1. A/C LOG BOOK*
2/ TECHNICAL
3. ENGINE
4. ALL
58. A/C FUEL VEHICLES ARE APPROVED BY
ANS, CHIEF INSPECTOR OF EXPLOSIV
59. DIRECT READING OF MAG. COMPASS SHALL BE CALLIBRATED WHEN
A. AFTER INSTALATION STRONG MAG. FIELD IN COCKPIT
2. COMPASS IN DOUBT
3. AFTER APECIFIED PERIOD
4 ALL**
60. MTCS
1. NATIONALITY MARK SHOW EXACT COUNTRY OF A/C
2. REGISTRATION MARK SHOW COUNTRY OF A/C
3. REG. MARKING IDENTIFED NATIONALITY MAKING
4. ALL
61. MTCS
1. MINOR DEFECT REDUCE THE SAFETY OF A/C
2, MAJOR DEFECT REDUCE THE SAFETY OF A/C*
3 MAJOR AND MINOR BOTH REDUCE
62. MTCS RESPECT TO DAMAGE AND TOLRENCE
1. DAMAGE TOLRENCE CAM SUSTAIN DAMAGE
2 AS IN 1, IT CAN SUSTAIN DAMAGE WITHOUT STRUCTURE FAILURE
3, IN CAN SUSTAIN DAMAGE BUT STRUCTURE WILL DAMAGE
4 ALL
63 CAR-M PROVIDE CORROSPONDS TO TECHNICAL STANDARDS & GUIDELINES FOR CONTINUED AIRWDTH OF A/C
1 A/C REGISTRED IN INDIA & OPERATED IN FOREIGN
2. " " " " " " " INDIA
3, AC REG. IN INDIA
4. ALL...
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