APPS/glidr-content.git - git.mnsoft.org

..	..	@@ -51,7 +51,7 @@
51	51
52	52	#### Source
53	53
54		-- Examen Blanc: [VV Q30 p.217](Questionnaire%20toutes%20branches%20VV.pdf#page=217) (score: 0.24)
	54	+- [VV Q30 p.217](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=217) (score: 0.24)
55	55	- PDF Answer: D
56	56
57	57	### Q3: After one wing stalls and the nose drops, what is the correct technique to prevent a spin? ^t80q3
..	..	@@ -151,7 +151,7 @@
151	151
152	152	#### Source
153	153
154		-- Examen Blanc: [VV Q52 p.64](Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.23)
	154	+- [VV Q52 p.64](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.23)
155	155	- PDF Answer: D
156	156
157	157	### Q7: What purpose does the vertical tail fin (rudder assembly) serve? ^t80q7
..	..	@@ -176,7 +176,7 @@
176	176
177	177	#### Source
178	178
179		-- Examen Blanc: [VV Q52 p.222](Questionnaire%20toutes%20branches%20VV.pdf#page=222) (score: 0.25)
	179	+- [VV Q52 p.222](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=222) (score: 0.25)
180	180	- PDF Answer: D
181	181
182	182	### Q8: In a coordinated level turn at 60 degrees of bank, the load factor is approximately ^t80q8
..	..	@@ -274,7 +274,7 @@
274	274
275	275	#### Source
276	276
277		-- Examen Blanc: [S1S Q16 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.27)
	277	+- [S1S Q16 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.27)
278	278	- PDF Answer: C
279	279
280	280	### Q12: In straight and level flight, what happens to the required angle of attack as speed increases? ^t80q12
..	..	@@ -304,7 +304,7 @@
304	304
305	305	#### Source
306	306
307		-- Examen Blanc: [VV Q21 p.184](Questionnaire%20toutes%20branches%20VV.pdf#page=184) (score: 0.23)
	307	+- [VV Q21 p.184](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=184) (score: 0.23)
308	308	- PDF Answer: B
309	309
310	310	### Q13: What is the function of wing fences or boundary layer fences? ^t80q13
..	..	@@ -397,7 +397,7 @@
397	397
398	398	#### Source
399	399
400		-- Examen Blanc: [VV Q36 p.187](Questionnaire%20toutes%20branches%20VV.pdf#page=187) (score: 0.29)
	400	+- [VV Q36 p.187](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=187) (score: 0.29)
401	401	- PDF Answer: D
402	402
403	403	### Q17: What does the term "load factor" describe? ^t80q17
..	..	@@ -426,7 +426,7 @@
426	426
427	427	#### Source
428	428
429		-- Examen Blanc: [VV Q13 p.77](Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.24)
	429	+- [VV Q13 p.77](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.24)
430	430	- PDF Answer: A
431	431
432	432	### Q18: How does increasing aircraft weight affect the best glide ratio? ^t80q18
..	..	@@ -470,7 +470,7 @@
470	470
471	471	#### Source
472	472
473		-- Examen Blanc: [VV Q20 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.21)
	473	+- [VV Q20 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.21)
474	474	- PDF Answer: C
475	475
476	476	### Q20: What is the effect of extending airbrakes (spoilers) on a glider? ^t80q20
..	..	@@ -495,7 +495,7 @@
495	495
496	496	#### Source
497	497
498		-- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.25)
	498	+- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.25)
499	499
500	500	### Q21: In which flight condition is induced drag greatest? ^t80q21
501	501
..	..	@@ -520,7 +520,7 @@
520	520
521	521	#### Source
522	522
523		-- Examen Blanc: [S1S Q13 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.22)
	523	+- [S1S Q13 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.22)
524	524	- PDF Answer: A
525	525
526	526	### Q22: What is the primary function of an elevator trim tab? ^t80q22
..	..	@@ -568,7 +568,7 @@
568	568
569	569	#### Source
570	570
571		-- Examen Blanc: [S1S Q18 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.31)
	571	+- [S1S Q18 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.31)
572	572	- PDF Answer: C
573	573
574	574	### Q24: What is the centre of pressure of an aerofoil? ^t80q24
..	..	@@ -595,7 +595,7 @@
595	595
596	596	#### Source
597	597
598		-- Examen Blanc: [VV Q15 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.24)
	598	+- [VV Q15 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.24)
599	599	- PDF Answer: D
600	600
601	601	### Q25: At what point during flight is parasite drag greatest? ^t80q25
..	..	@@ -621,7 +621,7 @@
621	621
622	622	#### Source
623	623
624		-- Examen Blanc: [VV Q50 p.64](Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.21)
	624	+- [VV Q50 p.64](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.21)
625	625	- PDF Answer: B
626	626
627	627	### Q26: What is the Bernoulli principle as applied to an aerofoil? ^t80q26
..	..	@@ -773,7 +773,7 @@
773	773
774	774	#### Source
775	775
776		-- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.25)
	776	+- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.25)
777	777	- PDF Answer: D
778	778
779	779	### Q32: What is the purpose of a laminar-flow aerofoil? ^t80q32
..	..	@@ -821,7 +821,7 @@
821	821
822	822	#### Source
823	823
824		-- Examen Blanc: [VV Q30 p.113](Questionnaire%20toutes%20branches%20VV.pdf#page=113) (score: 0.28)
	824	+- [VV Q30 p.113](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=113) (score: 0.28)
825	825	- PDF Answer: D
826	826
827	827	### Q34: What is the difference between static stability and dynamic stability? ^t80q34
..	..	@@ -889,7 +889,7 @@
889	889
890	890	#### Source
891	891
892		-- Examen Blanc: [VV Q95 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.22)
	892	+- [VV Q95 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.22)
893	893	- PDF Answer: B
894	894
895	895	### Q37: In which direction does the centre of pressure move as the angle of attack increases (pre-stall)? ^t80q37
..	..	@@ -915,7 +915,7 @@
915	915
916	916	#### Source
917	917
918		-- Examen Blanc: [VV Q16 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.40)
	918	+- [VV Q16 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.40)
919	919	- PDF Answer: C
920	920
921	921	### Q38: What determines the critical angle of attack at which a wing stalls? ^t80q38
..	..	@@ -968,7 +968,7 @@
968	968
969	969	#### Source
970	970
971		-- Examen Blanc: [VV Q171 p.143](Questionnaire%20toutes%20branches%20VV.pdf#page=143) (score: 0.22)
	971	+- [VV Q171 p.143](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=143) (score: 0.22)
972	972	- PDF Answer: C
973	973
974	974	### Q40: Which types of drag make up total drag? ^t80q40
..	..	@@ -1020,8 +1020,8 @@
1020	1020
1021	1021	#### Source
1022	1022
1023		-- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.24)
1024		-- [QuizVDS Q41](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A
	1023	+- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.24)
	1024	+- [QuizVDS Q41](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A
1025	1025
1026	1026	### Q42: To recover from a stall, it is essential to ^t80q42
1027	1027
..	..	@@ -1081,8 +1081,8 @@
1081	1081
1082	1082	#### Source
1083	1083
1084		-- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.20)
1085		-- [QuizVDS Q41](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A
	1084	+- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.20)
	1085	+- [QuizVDS Q41](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A
1086	1086	- PDF Answer: D
1087	1087
1088	1088	### Q44: The critical angle of attack ^t80q44
..	..	@@ -1114,8 +1114,8 @@
1114	1114
1115	1115	#### Source
1116	1116
1117		-- Examen Blanc: [VV Q48 p.221](Questionnaire%20toutes%20branches%20VV.pdf#page=221) (score: 0.26)
1118		-- [QuizVDS Q44](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q44): Answer C
	1117	+- [VV Q48 p.221](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=221) (score: 0.26)
	1118	+- [QuizVDS Q44](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q44): Answer C
1119	1119	- PDF Answer: D
1120	1120
1121	1121	### Q45: What leads to a lower stall speed Vs (IAS)? ^t80q45
..	..	@@ -1150,8 +1150,8 @@
1150	1150
1151	1151	#### Source
1152	1152
1153		-- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.21)
1154		-- [QuizVDS Q45](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q45): Answer B
	1153	+- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.21)
	1154	+- [QuizVDS Q45](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q45): Answer B
1155	1155	- PDF Answer: D
1156	1156
1157	1157	### Q46: Which statement about a spin is correct? ^t80q46
..	..	@@ -1200,8 +1200,8 @@
1200	1200
1201	1201	#### Source
1202	1202
1203		-- Examen Blanc: [S1S Q17 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.25)
1204		-- [QuizVDS Q47](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q47): Answer B
	1203	+- [S1S Q17 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.25)
	1204	+- [QuizVDS Q47](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q47): Answer B
1205	1205	- PDF Answer: C
1206	1206
1207	1207	### Q48: What types of boundary layers are found on an aerofoil? ^t80q48
..	..	@@ -1295,7 +1295,7 @@
1295	1295
1296	1296	#### Source
1297	1297
1298		-- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82)
	1298	+- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82)
1299	1299	- PDF Answer: D
1300	1300
1301	1301	### Q52: During a sideslip, the permitted flap position is ^t80q52
..	..	@@ -1318,7 +1318,7 @@
1318	1318
1319	1319	#### Source
1320	1320
1321		-- Examen Blanc: [S1S Q15 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65)
	1321	+- [S1S Q15 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65)
1322	1322	- PDF Answer: A
1323	1323
1324	1324	### Q53: An aircraft is said to have dynamic stability when ^t80q53
..	..	@@ -1341,7 +1341,7 @@
1341	1341
1342	1342	#### Source
1343	1343
1344		-- Examen Blanc: [S1S Q19 p.43](Exa%20Blanc%20Série_1_Specifiques.pdf#page=43) (score: 0.88)
	1344	+- [S1S Q19 p.43](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=43) (score: 0.88)
1345	1345	- PDF Answer: A
1346	1346
1347	1347	### Q54: In severe turbulence, airspeed must be reduced ^t80q54
..	..	@@ -1364,7 +1364,7 @@
1364	1364
1365	1365	#### Source
1366	1366
1367		-- Examen Blanc: [VV Q19 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.22)
	1367	+- [VV Q19 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.22)
1368	1368	- PDF Answer: D
1369	1369
1370	1370	### Q55: In the ICAO standard atmosphere, the temperature lapse rate in the troposphere is ^t80q55
..	..	@@ -1391,7 +1391,7 @@
1391	1391
1392	1392	#### Source
1393	1393
1394		-- Examen Blanc: [S1S Q1 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70)
	1394	+- [S1S Q1 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70)
1395	1395	- PDF Answer: D
1396	1396
1397	1397	### Q56: At approximately what altitude does atmospheric pressure fall to half its sea-level value? ^t80q56
..	..	@@ -1417,7 +1417,7 @@
1417	1417
1418	1418	#### Source
1419	1419
1420		-- Examen Blanc: [S1S Q3 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.54)
	1420	+- [S1S Q3 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.54)
1421	1421	- PDF Answer: C
1422	1422
1423	1423	### Q57: Density altitude always corresponds to ^t80q57
..	..	@@ -1444,7 +1444,7 @@
1444	1444
1445	1445	#### Source
1446	1446
1447		-- Examen Blanc: [S1S Q4 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.66)
	1447	+- [S1S Q4 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.66)
1448	1448	- PDF Answer: C
1449	1449
1450	1450	### Q58: The simplified continuity law applied to an airflow states: In a given period of time, a flowing air mass is conserved regardless of the cross-section it passes through. This means that ^t80q58
..	..	@@ -1472,7 +1472,7 @@
1472	1472
1473	1473	#### Source
1474	1474
1475		-- Examen Blanc: [S1S Q5 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70)
	1475	+- [S1S Q5 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70)
1476	1476	- PDF Answer: A
1477	1477
1478	1478	### Q59: The aerodynamic resultant (drag and lift) depends on air density. When air density decreases ^t80q59
..	..	@@ -1500,7 +1500,7 @@
1500	1500
1501	1501	#### Source
1502	1502
1503		-- Examen Blanc: [S1S Q6 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.52)
	1503	+- [S1S Q6 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.52)
1504	1504	- PDF Answer: A
1505	1505
1506	1506	### Q60: What is the name of the point about which, when the angle of attack changes, the pitching moment around the lateral axis does not vary? ^t80q60
..	..	@@ -1526,7 +1526,7 @@
1526	1526
1527	1527	#### Source
1528	1528
1529		-- Examen Blanc: [S1S Q11 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65)
	1529	+- [S1S Q11 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65)
1530	1530	- PDF Answer: D
1531	1531
1532	1532	### Q61: The angle between the aerofoil chord line and the aircraft's longitudinal axis is called ^t80q61
..	..	@@ -1553,7 +1553,7 @@
1553	1553
1554	1554	#### Source
1555	1555
1556		-- Examen Blanc: [S1S Q9 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.56)
	1556	+- [S1S Q9 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.56)
1557	1557	- PDF Answer: D
1558	1558
1559	1559	### Q62: What does the transition point correspond to? ^t80q62
..	..	@@ -1576,7 +1576,7 @@
1576	1576
1577	1577	#### Source
1578	1578
1579		-- Examen Blanc: [S1S Q17 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65)
	1579	+- [S1S Q17 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65)
1580	1580	- PDF Answer: C
1581	1581
1582	1582	### Q63: Geometric or aerodynamic wing twist results in ^t80q63
..	..	@@ -1599,7 +1599,7 @@
1599	1599
1600	1600	#### Source
1601	1601
1602		-- Examen Blanc: [S1S Q10 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.61)
	1602	+- [S1S Q10 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.61)
1603	1603	- PDF Answer: B
1604	1604
1605	1605	### Q64: The profile drag (form drag) of a body is primarily influenced by ^t80q64
..	..	@@ -1622,7 +1622,7 @@
1622	1622
1623	1623	#### Source
1624	1624
1625		-- Examen Blanc: [S1S Q14 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.71)
	1625	+- [S1S Q14 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.71)
1626	1626	- PDF Answer: C
1627	1627
1628	1628	### Q65: The aerodynamic drag of a flat disc in an airflow depends notably on ^t80q65
..	..	@@ -1652,7 +1652,7 @@
1652	1652
1653	1653	#### Source
1654	1654
1655		-- Examen Blanc: [S1S Q12 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.68)
	1655	+- [S1S Q12 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.68)
1656	1656	- PDF Answer: B
1657	1657
1658	1658	### Q66: On the speed polar, which tangent touches the curve at the point of minimum sink rate? ^t80q66
..	..	@@ -1686,7 +1686,7 @@
1686	1686
1687	1687	#### Source
1688	1688
1689		-- Examen Blanc: [S1S Q16 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.55)
	1689	+- [S1S Q16 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.55)
1690	1690	- PDF Answer: C
1691	1691
1692	1692	### Q67: Induced drag increases ^t80q67
..	..	@@ -1719,7 +1719,7 @@
1719	1719
1720	1720	#### Source
1721	1721
1722		-- Examen Blanc: [S1S Q13 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.33)
	1722	+- [S1S Q13 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.33)
1723	1723	- PDF Answer: A
1724	1724
1725	1725	### Q68: How does the minimum speed of an aircraft in a level turn at 45-degree bank compare to straight-and-level flight? ^t80q68
..	..	@@ -1746,7 +1746,7 @@
1746	1746
1747	1747	#### Source
1748	1748
1749		-- Examen Blanc: [S1S Q18 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.33)
	1749	+- [S1S Q18 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.33)
1750	1750	- PDF Answer: C
1751	1751
1752	1752	### Q69: Adverse yaw is caused by ^t80q69
..	..	@@ -1769,7 +1769,7 @@
1769	1769
1770	1770	#### Source
1771	1771
1772		-- Examen Blanc: [S1S Q8 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.59)
	1772	+- [S1S Q8 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.59)
1773	1773	- PDF Answer: D
1774	1774
1775	1775	### Q70: True Airspeed (TAS) is the speed shown by the ASI ^t80q70
..	..	@@ -1797,7 +1797,7 @@
1797	1797
1798	1798	#### Source
1799	1799
1800		-- Examen Blanc: [S1S Q7 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65)
	1800	+- [S1S Q7 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65)
1801	1801	- PDF Answer: D
1802	1802
1803	1803	### Q71: The speed range authorised for the use of slotted flaps is: ^t80q71
..	..	@@ -1823,7 +1823,7 @@
1823	1823
1824	1824	#### Source
1825	1825
1826		-- Examen Blanc: [S2 Q1 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.43)
	1826	+- [S2 Q1 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.43)
1827	1827
1828	1828	### Q72: Wing tip vortices are caused by pressure equalisation from: ^t80q72
1829	1829
..	..	@@ -1845,7 +1845,7 @@
1845	1845
1846	1846	#### Source
1847	1847
1848		-- Examen Blanc: [S2 Q2 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.33)
	1848	+- [S2 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.33)
1849	1849
1850	1850	### Q73: The angle of attack of an aerofoil is always the angle between: ^t80q73
1851	1851
..	..	@@ -1871,8 +1871,8 @@
1871	1871
1872	1872	#### Source
1873	1873
1874		-- Examen Blanc: [S2 Q3 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.65)
1875		-- [QuizVDS Q14](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B
	1874	+- [S2 Q3 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.65)
	1875	+- [QuizVDS Q14](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B
1876	1876
1877	1877	### Q74: In the standard atmosphere, the values of temperature and atmospheric pressure at sea level are: ^t80q74
1878	1878
..	..	@@ -1907,7 +1907,7 @@
1907	1907
1908	1908	#### Source
1909	1909
1910		-- Examen Blanc: [S2 Q4 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.91)
	1910	+- [S2 Q4 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.91)
1911	1911
1912	1912	### Q75: Regarding airflow, the simplified continuity equation states: At the same moment, the same mass of air passes through different cross-sections. Therefore: ^t80q75
1913	1913
..	..	@@ -1931,7 +1931,7 @@
1931	1931
1932	1932	#### Source
1933	1933
1934		-- Examen Blanc: [S3 Q20 p.41](Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.42)
	1934	+- [S3 Q20 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.42)
1935	1935
1936	1936	### Q76: In a correctly executed turn without altitude loss, why is slight back-pressure on the elevator necessary? ^t80q76
1937	1937
..	..	@@ -1953,7 +1953,7 @@
1953	1953
1954	1954	#### Source
1955	1955
1956		-- Examen Blanc: [S3 Q6 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.53)
	1956	+- [S3 Q6 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.53)
1957	1957
1958	1958	### Q77: When the frontal area of a disc in an airflow is tripled, drag increases by: ^t80q77
1959	1959
..	..	@@ -1990,7 +1990,7 @@
1990	1990
1991	1991	#### Source
1992	1992
1993		-- Examen Blanc: [S2 Q7 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.64)
	1993	+- [S2 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.64)
1994	1994
1995	1995	### Q78: Aerodynamic wing twist (washout) is a modification of: ^t80q78
1996	1996
..	..	@@ -2031,7 +2031,7 @@
2031	2031
2032	2032	#### Source
2033	2033
2034		-- Examen Blanc: [S2 Q8 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.75)
	2034	+- [S2 Q8 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.75)
2035	2035
2036	2036	### Q79: What is the average value of gravitational acceleration at the Earth's surface? ^t80q79
2037	2037
..	..	@@ -2056,7 +2056,7 @@
2056	2056
2057	2057	#### Source
2058	2058
2059		-- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82)
	2059	+- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82)
2060	2060	- PDF Answer: D
2061	2061
2062	2062	### Q80: The speed displayed on the airspeed indicator (ASI) is a measurement of: ^t80q80
..	..	@@ -2079,7 +2079,7 @@
2079	2079
2080	2080	#### Source
2081	2081
2082		-- Examen Blanc: [S2 Q10 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.72)
	2082	+- [S2 Q10 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.72)
2083	2083
2084	2084	### Q81: The horizontal and vertical stabilisers serve in particular to: ^t80q81
2085	2085
..	..	@@ -2103,7 +2103,7 @@
2103	2103
2104	2104	#### Source
2105	2105
2106		-- Examen Blanc: [S2 Q11 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.36)
	2106	+- [S2 Q11 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.36)
2107	2107
2108	2108	### Q82: When slotted flaps are extended, airflow separation: ^t80q82
2109	2109
..	..	@@ -2153,7 +2153,7 @@
2153	2153
2154	2154	#### Source
2155	2155
2156		-- Examen Blanc: [S2 Q13 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.89)
	2156	+- [S2 Q13 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.89)
2157	2157
2158	2158	### Q84: Pressures are expressed in: ^t80q84
2159	2159
..	..	@@ -2175,7 +2175,7 @@
2175	2175
2176	2176	#### Source
2177	2177
2178		-- Examen Blanc: [S2 Q14 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.71)
	2178	+- [S2 Q14 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.71)
2179	2179
2180	2180	### Q85: TAS (True Air Speed) is the speed of: ^t80q85
2181	2181
..	..	@@ -2200,7 +2200,7 @@
2200	2200
2201	2201	#### Source
2202	2202
2203		-- Examen Blanc: [S2 Q15 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.48)
	2203	+- [S2 Q15 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.48)
2204	2204
2205	2205	### Q86: Yaw stability of an aircraft is provided by: ^t80q86
2206	2206
..	..	@@ -2222,7 +2222,7 @@
2222	2222
2223	2223	#### Source
2224	2224
2225		-- Examen Blanc: [S2 Q16 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.30)
	2225	+- [S2 Q16 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.30)
2226	2226
2227	2227	### Q87: The trailing edge flap shown below is a: ^t80q87
2228	2228
..	..	@@ -2246,7 +2246,7 @@
2246	2246
2247	2247	#### Source
2248	2248
2249		-- Examen Blanc: [S2 Q16 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.39)
	2249	+- [S2 Q16 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.39)
2250	2250
2251	2251	### Q88: The risk of airflow separation on the wing occurs mainly: ^t80q88
2252	2252
..	..	@@ -2268,7 +2268,7 @@
2268	2268
2269	2269	#### Source
2270	2270
2271		-- Examen Blanc: [S2 Q18 p.40](Exa%20Blanc%20Série_2.pdf#page=40) (score: 0.53)
	2271	+- [S2 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=40) (score: 0.53)
2272	2272
2273	2273	### Q89: The drag of a body in an airflow depends notably on: ^t80q89
2274	2274
..	..	@@ -2295,7 +2295,7 @@
2295	2295
2296	2296	#### Source
2297	2297
2298		-- Examen Blanc: [VV Q5 p.212](Questionnaire%20toutes%20branches%20VV.pdf#page=212) (score: 0.40)
	2298	+- [VV Q5 p.212](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=212) (score: 0.40)
2299	2299	- PDF Answer: D
2300	2300
2301	2301	### Q90: In the drawing below, the aerofoil chord is represented by: ^t80q90
..	..	@@ -2337,7 +2337,7 @@
2337	2337
2338	2338	#### Source
2339	2339
2340		-- Examen Blanc: [S2 Q12 p.26](Exa%20Blanc%20Série_2.pdf#page=26) (score: 0.20)
	2340	+- [S2 Q12 p.26](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=26) (score: 0.20)
2341	2341
2342	2342	### Q91: The angle of attack of an aerofoil is always measured between: ^t80q91
2343	2343
..	..	@@ -2370,8 +2370,8 @@
2370	2370
2371	2371	#### Source
2372	2372
2373		-- Examen Blanc: [S3 Q1 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.71)
2374		-- [QuizVDS Q14](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B
	2373	+- [S3 Q1 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.71)
	2374	+- [QuizVDS Q14](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B
2375	2375
2376	2376	### Q92: Given equal frontal area and equal airflow speed, what determines the drag of a body? ^t80q92
2377	2377
..	..	@@ -2402,7 +2402,7 @@
2402	2402
2403	2403	#### Source
2404	2404
2405		-- Examen Blanc: [S3 Q2 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.50)
	2405	+- [S3 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.50)
2406	2406
2407	2407	### Q93: What is the origin of induced drag on a wing? ^t80q93
2408	2408
..	..	@@ -2428,7 +2428,7 @@
2428	2428
2429	2429	#### Source
2430	2430
2431		-- Examen Blanc: [S3 Q3 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.45)
	2431	+- [S3 Q3 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.45)
2432	2432
2433	2433	### Q94: What is the sea-level pressure in the ICAO standard atmosphere? ^t80q94
2434	2434
..	..	@@ -2458,7 +2458,7 @@
2458	2458
2459	2459	#### Source
2460	2460
2461		-- Examen Blanc: [S3 Q4 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.58)
	2461	+- [S3 Q4 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.58)
2462	2462
2463	2463	### Q95: In the aerofoil diagram below, which line represents the mean camber line? ^t80q95
2464	2464
..	..	@@ -2509,7 +2509,7 @@
2509	2509
2510	2510	#### Source
2511	2511
2512		-- Examen Blanc: [S3 Q6 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.45)
	2512	+- [S3 Q6 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.45)
2513	2513
2514	2514	### Q97: A wing stall occurs: ^t80q97
2515	2515
..	..	@@ -2539,7 +2539,7 @@
2539	2539
2540	2540	#### Source
2541	2541
2542		-- Examen Blanc: [S3 Q7 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.43)
	2542	+- [S3 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.43)
2543	2543
2544	2544	### Q98: At what condition does airflow separation from an aerofoil occur? ^t80q98
2545	2545
..	..	@@ -2568,7 +2568,7 @@
2568	2568
2569	2569	#### Source
2570	2570
2571		-- Examen Blanc: [S3 Q8 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.30)
	2571	+- [S3 Q8 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.30)
2572	2572
2573	2573	### Q99: What is the mean gravitational acceleration at the surface of the Earth? ^t80q99
2574	2574
..	..	@@ -2597,7 +2597,7 @@
2597	2597
2598	2598	#### Source
2599	2599
2600		-- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.73)
	2600	+- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.73)
2601	2601	- PDF Answer: D
2602	2602
2603	2603	### Q100: True Airspeed (TAS) is obtained from the airspeed indicator (ASI) reading by: ^t80q100
..	..	@@ -2630,7 +2630,7 @@
2630	2630
2631	2631	#### Source
2632	2632
2633		-- Examen Blanc: [S3 Q10 p.39](Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.39)
	2633	+- [S3 Q10 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.39)
2634	2634
2635	2635	### Q101: A shift of the centre of gravity is caused by: ^t80q101
2636	2636
..	..	@@ -2659,7 +2659,7 @@
2659	2659
2660	2660	#### Source
2661	2661
2662		-- Examen Blanc: [VV Q16 p.77](Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.50)
	2662	+- [VV Q16 p.77](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.50)
2663	2663	- PDF Answer: C
2664	2664
2665	2665	### Q102: The high-lift device shown in the diagram is a: ^t80q102
..	..	@@ -2687,7 +2687,7 @@
2687	2687
2688	2688	#### Source
2689	2689
2690		-- Examen Blanc: [S3 Q12 p.39](Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.30)
	2690	+- [S3 Q12 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.30)
2691	2691
2692	2692	### Q103: The resultant of all aerodynamic forces on a wing profile acts through the: ^t80q103
2693	2693
..	..	@@ -2713,7 +2713,7 @@
2713	2713
2714	2714	#### Source
2715	2715
2716		-- Examen Blanc: [VV Q15 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.37)
	2716	+- [VV Q15 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.37)
2717	2717	- PDF Answer: D
2718	2718
2719	2719	### Q104: At approximately what altitude is the air density half of its sea-level value? ^t80q104
..	..	@@ -2743,7 +2743,7 @@
2743	2743
2744	2744	#### Source
2745	2745
2746		-- Examen Blanc: [S3 Q14 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.75)
	2746	+- [S3 Q14 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.75)
2747	2747
2748	2748	### Q105: The airspeed indicator (ASI) reading is based on a measurement of: ^t80q105
2749	2749
..	..	@@ -2774,7 +2774,7 @@
2774	2774
2775	2775	#### Source
2776	2776
2777		-- Examen Blanc: [S2 Q10 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.63)
	2777	+- [S2 Q10 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.63)
2778	2778
2779	2779	### Q106: Roll stability is influenced by: ^t80q106
2780	2780
..	..	@@ -2800,7 +2800,7 @@
2800	2800
2801	2801	#### Source
2802	2802
2803		-- Examen Blanc: [S3 Q16 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.64)
	2803	+- [S3 Q16 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.64)
2804	2804
2805	2805	### Q107: The speed range for operating slotted flaps: ^t80q107
2806	2806
..	..	@@ -2830,7 +2830,7 @@
2830	2830
2831	2831	#### Source
2832	2832
2833		-- Examen Blanc: [S3 Q17 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.62)
	2833	+- [S3 Q17 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.62)
2834	2834
2835	2835	### Q108: When the wing's angle of incidence is larger at the root than at the tip, this is called: ^t80q108
2836	2836
..	..	@@ -2859,7 +2859,7 @@
2859	2859
2860	2860	#### Source
2861	2861
2862		-- Examen Blanc: [S3 Q18 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.29)
	2862	+- [S3 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.29)
2863	2863
2864	2864	### Q109: Barometric pressure in the Earth's atmosphere has the characteristic of: ^t80q109
2865	2865
..	..	@@ -2885,7 +2885,7 @@
2885	2885
2886	2886	#### Source
2887	2887
2888		-- Examen Blanc: [S3 Q18 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.31)
	2888	+- [S3 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.31)
2889	2889
2890	2890	### Q110: The simplified continuity equation says the same mass of air passes through different cross-sections at the same instant. Therefore: ^t80q110
2891	2891
..	..	@@ -2911,7 +2911,7 @@
2911	2911
2912	2912	#### Source
2913	2913
2914		-- Examen Blanc: [S3 Q20 p.41](Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.39)
	2914	+- [S3 Q20 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.39)
2915	2915
2916	2916	### Q111: On the aerofoil diagram, what does point number 4 represent? ^t80q111
2917	2917
..	..	@@ -3017,8 +3017,8 @@
3017	3017
3018	3018	#### Source
3019	3019
3020		-- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25)
3021		-- [QuizVDS Q53](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A
	3020	+- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25)
	3021	+- [QuizVDS Q53](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A
3022	3022	- PDF Answer: A
3023	3023
3024	3024	### Q115: Rotation about the vertical axis is termed ^t80q115
..	..	@@ -3045,8 +3045,8 @@
3045	3045
3046	3046	#### Source
3047	3047
3048		-- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.27)
3049		-- [QuizVDS Q56](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q56): Answer C
	3048	+- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.27)
	3049	+- [QuizVDS Q56](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q56): Answer C
3050	3050	- PDF Answer: A
3051	3051
3052	3052	### Q116: Rotation about the lateral axis is termed ^t80q116
..	..	@@ -3073,8 +3073,8 @@
3073	3073
3074	3074	#### Source
3075	3075
3076		-- Examen Blanc: [VV Q75 p.69](Questionnaire%20toutes%20branches%20VV.pdf#page=69) (score: 0.27)
3077		-- [QuizVDS Q57](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q57): Answer B
	3076	+- [VV Q75 p.69](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=69) (score: 0.27)
	3077	+- [QuizVDS Q57](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q57): Answer B
3078	3078	- PDF Answer: B
3079	3079
3080	3080	### Q117: The elevator causes the aircraft to rotate around the ^t80q117
..	..	@@ -3103,7 +3103,7 @@
3103	3103
3104	3104	#### Source
3105	3105
3106		-- Examen Blanc: [VV Q40 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.28)
	3106	+- [VV Q40 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.28)
3107	3107	- PDF Answer: C
3108	3108
3109	3109	### Q118: What must be considered regarding the centre of gravity position? ^t80q118
..	..	@@ -3293,8 +3293,8 @@
3293	3293
3294	3294	#### Source
3295	3295
3296		-- Examen Blanc: [VV Q26 p.185](Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.20)
3297		-- [QuizVDS Q77](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q77): Answer C
	3296	+- [VV Q26 p.185](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.20)
	3297	+- [QuizVDS Q77](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q77): Answer C
3298	3298	- PDF Answer: B
3299	3299
3300	3300	### Q125: The pressure equalisation between the upper and lower wing surfaces results in ^t80q125
..	..	@@ -3399,8 +3399,8 @@
3399	3399
3400	3400	#### Source
3401	3401
3402		-- Examen Blanc: [S2 Q7 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.23)
3403		-- [QuizVDS Q9](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B
	3402	+- [S2 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.23)
	3403	+- [QuizVDS Q9](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B
3404	3404
3405	3405	### Q129: In the diagram, what does number 3 represent? ^t80q129
3406	3406
..	..	@@ -3536,7 +3536,7 @@
3536	3536
3537	3537	#### Source
3538	3538
3539		-- Examen Blanc: [S1S Q6 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.29)
	3539	+- [S1S Q6 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.29)
3540	3540	- PDF Answer: A
3541	3541
3542	3542	### Q134: Which combination of measures can improve the glide ratio of a sailplane? ^t80q134
..	..	@@ -3618,8 +3618,8 @@
3618	3618
3619	3619	#### Source
3620	3620
3621		-- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22)
3622		-- [QuizVDS Q54](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q54): Answer B
	3621	+- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22)
	3622	+- [QuizVDS Q54](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q54): Answer B
3623	3623	- PDF Answer: A
3624	3624
3625	3625	### Q137: Which structural element provides directional stability? ^t80q137
..	..	@@ -3700,8 +3700,8 @@
3700	3700
3701	3701	#### Source
3702	3702
3703		-- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22)
3704		-- [QuizVDS Q60](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q60): Answer B
	3703	+- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22)
	3704	+- [QuizVDS Q60](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q60): Answer B
3705	3705	- PDF Answer: A
3706	3706
3707	3707	### Q140: What happens when the rudder is deflected to the left? ^t80q140
..	..	@@ -3891,7 +3891,7 @@
3891	3891
3892	3892	#### Source
3893	3893
3894		-- Examen Blanc: [VV Q40 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.26)
	3894	+- [VV Q40 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.26)
3895	3895	- PDF Answer: C
3896	3896
3897	3897	### Q147: Which of the following factors causes the load factor to increase during cruise flight? ^t80q147
..	..	@@ -3921,8 +3921,8 @@
3921	3921
3922	3922	#### Source
3923	3923
3924		-- Examen Blanc: [VV Q66 p.225](Questionnaire%20toutes%20branches%20VV.pdf#page=225) (score: 0.21)
3925		-- [QuizVDS Q74](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q74): Answer D
	3924	+- [VV Q66 p.225](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=225) (score: 0.21)
	3925	+- [QuizVDS Q74](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q74): Answer D
3926	3926	- PDF Answer: A
3927	3927
3928	3928	### Q148: While approaching the next updraft, the variometer shows 3 m/s descent. You expect a mean climb rate of 2 m/s in the thermal. How should you set the McCready ring? ^t80q148
..	..	@@ -4030,7 +4030,7 @@
4030	4030
4031	4031	#### Source
4032	4032
4033		-- Examen Blanc: [S1S Q9 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.21)
	4033	+- [S1S Q9 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.21)
4034	4034	- PDF Answer: D
4035	4035
4036	4036	### Q152: In the figure, the angle (alpha) is referred to as ^t80q152
..	..	@@ -4085,8 +4085,8 @@
4085	4085
4086	4086	#### Source
4087	4087
4088		-- Examen Blanc: [VV Q41 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.29)
4089		-- [QuizVDS Q68](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q68): Answer B
	4088	+- [VV Q41 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.29)
	4089	+- [QuizVDS Q68](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q68): Answer B
4090	4090	- PDF Answer: A
4091	4091
4092	4092	### Q154: What must be taken into account when flying a sailplane with water ballast? ^t80q154
..	..	@@ -4219,8 +4219,8 @@
4219	4219
4220	4220	#### Source
4221	4221
4222		-- Examen Blanc: [S3 Q2 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.23)
4223		-- [QuizVDS Q9](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B
	4222	+- [S3 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.23)
	4223	+- [QuizVDS Q9](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B
4224	4224
4225	4225	### Q159: "Longitudinal stability" refers to stability around which axis? ^t80q159
4226	4226
..	..	@@ -4246,8 +4246,8 @@
4246	4246
4247	4247	#### Source
4248	4248
4249		-- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25)
4250		-- [QuizVDS Q53](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A
	4249	+- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25)
	4250	+- [QuizVDS Q53](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A
4251	4251	- PDF Answer: A
4252	4252
4253	4253	### Q160: What does "wing loading" mean? ^t80q160
..	..	@@ -4325,8 +4325,8 @@
4325	4325
4326	4326	#### Source
4327	4327
4328		-- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.26)
4329		-- [QuizVDS Q90](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q90): Answer B
	4328	+- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.26)
	4329	+- [QuizVDS Q90](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q90): Answer B
4330	4330
4331	4331	### Q163: Does air density affect the minimum speed (IAS) of a glider? ^t80q163
4332	4332
..	..	@@ -4354,7 +4354,7 @@
4354	4354
4355	4355	#### Source
4356	4356
4357		-- Examen Blanc: [VV Q57 p.223](Questionnaire%20toutes%20branches%20VV.pdf#page=223) (score: 0.92)
	4357	+- [VV Q57 p.223](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=223) (score: 0.92)
4358	4358	- PDF Answer: C
4359	4359
4360	4360	### Q164: In which speed range can vibrations and flutter occur? ^t80q164
..	..	@@ -4383,7 +4383,7 @@
4383	4383
4384	4384	#### Source
4385	4385
4386		-- Examen Blanc: [VV Q27 p.185](Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.33)
	4386	+- [VV Q27 p.185](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.33)
4387	4387	- PDF Answer: C
4388	4388
4389	4389	### Q165: Vibrations can occur when ^t80q165
..	..	@@ -4406,7 +4406,7 @@
4406	4406
4407	4407	#### Source
4408	4408
4409		-- Examen Blanc: [VV Q79 p.227](Questionnaire%20toutes%20branches%20VV.pdf#page=227) (score: 0.58)
	4409	+- [VV Q79 p.227](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=227) (score: 0.58)
4410	4410	- PDF Answer: A
4411	4411
4412	4412	### Q166: Vibrations can also occur under which conditions? ^t80q166
..	..	@@ -4429,7 +4429,7 @@
4429	4429
4430	4430	#### Source
4431	4431
4432		-- Examen Blanc: [VV Q80 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.56)
	4432	+- [VV Q80 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.56)
4433	4433	- PDF Answer: C
4434	4434
4435	4435	### Q167: In which speed range can the maximum load factor be exceeded, leading to structural overload? ^t80q167
..	..	@@ -4457,7 +4457,7 @@
4457	4457
4458	4458	#### Source
4459	4459
4460		-- Examen Blanc: [VV Q81 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.59)
	4460	+- [VV Q81 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.59)
4461	4461	- PDF Answer: B
4462	4462
4463	4463	### Q168: Above which speed can abrupt or full control deflections damage the glider's structure? ^t80q168
..	..	@@ -4480,7 +4480,7 @@
4480	4480
4481	4481	#### Source
4482	4482
4483		-- Examen Blanc: [VV Q83 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.93)
	4483	+- [VV Q83 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.93)
4484	4484	- PDF Answer: A
4485	4485
4486	4486	### Q169: When the maximum load factor is exceeded, what is the primary risk? ^t80q169
..	..	@@ -4503,7 +4503,7 @@
4503	4503
4504	4504	#### Source
4505	4505
4506		-- Examen Blanc: [VV Q31 p.186](Questionnaire%20toutes%20branches%20VV.pdf#page=186) (score: 0.53)
	4506	+- [VV Q31 p.186](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=186) (score: 0.53)
4507	4507	- PDF Answer: C
4508	4508
4509	4509	### Q170: The mass balance (mass balancing) of an aileron has lost lead weights. What can be the consequence? ^t80q170
..	..	@@ -4526,7 +4526,7 @@
4526	4526
4527	4527	#### Source
4528	4528
4529		-- Examen Blanc: [VV Q85 p.229](Questionnaire%20toutes%20branches%20VV.pdf#page=229) (score: 0.48)
	4529	+- [VV Q85 p.229](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=229) (score: 0.48)
4530	4530	- PDF Answer: B
4531	4531
4532	4532	### Q171: What is the danger of flying at minimum speed in turbulent air? ^t80q171
..	..	@@ -4549,7 +4549,7 @@
4549	4549
4550	4550	#### Source
4551	4551
4552		-- Examen Blanc: [VV Q92 p.230](Questionnaire%20toutes%20branches%20VV.pdf#page=230) (score: 0.79)
	4552	+- [VV Q92 p.230](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=230) (score: 0.79)
4553	4553	- PDF Answer: C
4554	4554
4555	4555	### Q172: How does air density change when temperature increases? ^t80q172
..	..	@@ -4578,7 +4578,7 @@
4578	4578
4579	4579	#### Source
4580	4580
4581		-- Examen Blanc: [VV Q94 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.55)
	4581	+- [VV Q94 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.55)
4582	4582	- PDF Answer: A
4583	4583
4584	4584	### Q173: In what proportion does drag change with airspeed? ^t80q173
..	..	@@ -4606,7 +4606,7 @@
4606	4606
4607	4607	#### Source
4608	4608
4609		-- Examen Blanc: [VV Q96 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.33)
	4609	+- [VV Q96 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.33)
4610	4610	- PDF Answer: D
4611	4611
4612	4612	### Q174: What is understood by static pressure? ^t80q174
..	..	@@ -4629,7 +4629,7 @@
4629	4629
4630	4630	#### Source
4631	4631
4632		-- Examen Blanc: [VV Q97 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.64)
	4632	+- [VV Q97 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.64)
4633	4633	- PDF Answer: C
4634	4634
4635	4635	### Q175: How does the maximum permissible speed Vne of a glider in IAS behave as altitude increases? ^t80q175
..	..	@@ -4659,7 +4659,7 @@
4659	4659
4660	4660	#### Source
4661	4661
4662		-- Examen Blanc: [VV Q20 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.67)
	4662	+- [VV Q20 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.67)
4663	4663	- PDF Answer: C
4664	4664
4665	4665	### Q176: In what proportion does lift change when airspeed increases? ^t80q176
..	..	@@ -4682,7 +4682,7 @@
4682	4682
4683	4683	#### Source
4684	4684
4685		-- Examen Blanc: [VV Q104 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.23)
	4685	+- [VV Q104 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.23)
4686	4686	- PDF Answer: B
4687	4687
4688	4688	### Q177: Which statement is FALSE regarding the relationship between lift/drag and airspeed? ^t80q177
..	..	@@ -4705,7 +4705,7 @@
4705	4705
4706	4706	#### Source
4707	4707
4708		-- Examen Blanc: [VV Q105 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.63)
	4708	+- [VV Q105 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.63)
4709	4709	- PDF Answer: C
4710	4710
4711	4711	### Q178: What is understood by total pressure? ^t80q178
..	..	@@ -4734,5 +4734,5 @@
4734	4734
4735	4735	#### Source
4736	4736
4737		-- Examen Blanc: [VV Q106 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.83)
	4737	+- [VV Q106 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.83)
4738	4738	- PDF Answer: C