FONDATION AÉROVISION QUÉBEC INC.
5430 chemin de Chambly, Saint Hubert, J3Y 3P1
450-678-1720
courriel...
More
FONDATION AÉROVISION QUÉBEC INC. 5430 chemin de Chambly, Saint Hubert, J3Y 3P1 450-678-1720 courriel :info@aerovision. org site web : www. aerovision. org
Less
From Antoine Daoust
Soirée d intronisation au Panthéon de l’Air et de l’Espace du Québec 2010
Présenté par la Fondation Aérovision Québec
From Antoine Daoust
La Caisse Desjardins
de Saint-Hubert
est fière partenaire de la Fondation Aérovision
Que son importante mission, celle de préserver et de faire
connaître l histoire de la navigation aérienne, puisse susciter
dans le coeur de toute personne qui s y intéresse,.
.
.
.
.
.
une vive passion pour l aéronautique et l aviation.
Siège...
More
La Caisse Desjardins de Saint-Hubert est fière partenaire de la Fondation Aérovision Que son importante mission, celle de préserver et de faire connaître l histoire de la navigation aérienne, puisse susciter dans le coeur de toute personne qui s y intéresse,. . . . . . une vive passion pour l aéronautique et l aviation. Siège social 2400, boul. Gaétan-Boucher Centre de services Bernard-Racicot 5040, boul. Gaétan-Boucher Centre de services Hector-Martin 5045, boul. Cousineau Caisse de Saint-Hubert COOPÉRER POUR CRÉER L AVENIRAndré Benoit Directeur général Un seul numéro de téléphone : 450 443-0047 www. desjardins. com/caissesainthubert
Less
From Antoine Daoust
.
---------------------------------------------------------------------------------------------------1
V:SCOU~T MAINTENANCE Mi~t;:Ut\L
pm1En PLA.
.
.
1 \T COl:TROLS
CHAPTE?
PAGE
DATE
to de:eTdine the a~olliltthe
replace~ent bracket should be
scre~ed into the support
:;I"acl-:e"t e
d.
Scre~ the shaft out of the
suppor-t bz-acke t and...
More
. ---------------------------------------------------------------------------------------------------1 V:SCOU~T MAINTENANCE Mi~t;:Ut\L pm1En PLA. . . 1 \T COl:TROLS CHAPTE? PAGE DATE to de:eTdine the a~olliltthe replace~ent bracket should be scre~ed into the support :;I"acl-:e"t e d. Scre~ the shaft out of the suppor-t bz-acke t and r encve -chc a888:::1bly. InstallC _tion 4. The Ln board friction dampers may be installed as follows: a. Using the assembly wh i. ch was r-emoved as a gui de , screvr the . jam nut of the new as semo. Ly on the shaft to the same relative position. b. Screw the shaft into the suuDO!" -: ~racke-: to tr:e deI ~~ p~~set D~r . ~ tte j2D r. ut. c. Tighter!. the j9. . :l nut , d. Refit the centrol rods and c~eck o?eratic~ paying ?artic~13r attention to the clearance aro~nd e. \ ~en t1:e adj usttaen t is sa"cis~2CkO~~ d-~ 1 + ne Sh~~k ("~l ~~ k~Q_ •• l, ":" . ; . . •. . _ ~ _ 1,,0. •• L. . ••. . L. oJ vr. . . . . . . . _~::> . "J. . . ••. •. ••
Less
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 102
Views: 3
Downloads: 0
CHAPTER 32
-~------ --- -~-- ~~--- - ,",- CHAPTER
INDEX ,
DATE
32
1
Jun 6/67
SECTION 1
SSCTION 2
?PROPELLER SYSTEN DESCRIPTION
.
10 General Description
.
11 Principles of Operation
ILLUSTRATIOHS
Fig.
1 Sectional Vim.
; of Propeller
Fig.
2 Controller Unit
Fig.
3 Constant Sreeding in Flight
FiB .
4 Underspeed
Fig.
5 Oversneed
Fig....
More
CHAPTER 32 -~------ --- -~-- ~~--- - ,",- CHAPTER INDEX , DATE 32 1 Jun 6/67 SECTION 1 SSCTION 2 ?PROPELLER SYSTEN DESCRIPTION . 10 General Description . 11 Principles of Operation ILLUSTRATIOHS Fig. 1 Sectional Vim. ; of Propeller Fig. 2 Controller Unit Fig. 3 Constant Sreeding in Flight FiB . 4 Underspeed Fig. 5 Oversneed Fig. 6 Feathering FiG_ 7 Unfeathering FiG. 8 AutoP. laticFeatherinG FiC. 9 Breakdown of Flight Fine Pitch Lock F. :r- 10 Propeller Controls in Coc:-:::it. . J. . . u• . . " PROPSLL3R SYSTEM ELEC~R!CAL CI~CCI7S . 10 Introduction . 11 General . 12 Location of Equipment . 13 Description ,~ . 14 Full Cycle of Pitch;. Contro . , O i"i " •15 . :. . nergencycer-a t~oh ". , . ~. •16 Feathering -~, . 17 Auto-?eathering . 18 Unfeathering . 19 Circuit Descri?tion, FeRtherinG _~~. 20 Circuit Description, Unfcathering . 21 Circuit Description, Auto-Feathering . 22 GFP Circuit Description . 23 Ground Fine Pitch \iarning Lights ILLUSTRATION Fig. 1 Propeller Feather
Less
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 98
Views: 2
Downloads: 0
CRAP rllJ-l )6
SPINNER
SECTION 1
ISSUED I JUNE 20, 1957
VISCOUNT MAINTENA NeE MANUAL
CHAPTER 36
INDEX 1
DESCRIPTION
SPI NNER I1Ef~RlfnON
.
10 Introduction
.
11 Shell Group
.
12 Backplate Assembly
.
13 Electrical De-Icing
ILL USTRAT1 ONS
Fig.
1 Propeller Spinner
.
Trans-Canada Air Lines
-r:
W
W
W
.
AEROVISION.
ORG
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 81
Views: 1
Downloads: 0
FUSELAGE STRUCTURE
radio frequency signals thereby protecting the crew from radiation.
The radome is hinged at the top to
perr.
liteasy access to the antenna
area.
In the open position, the radome is supported by two jury struts,
which are attached to the bulkhead
at Station 24.
In the closed position, the radome is secured by four...
More
FUSELAGE STRUCTURE radio frequency signals thereby protecting the crew from radiation. The radome is hinged at the top to perr. liteasy access to the antenna area. In the open position, the radome is supported by two jury struts, which are attached to the bulkhead at Station 24. In the closed position, the radome is secured by four flush fitting toggle fasteners. The exterior surface of the radome is painted to match the exterior a. ir-cr-af tfinish. 3. The cockpit hood assembly consists of an internally braced dome attacr. ed to the hood ring, which extends around the aperture in the fuselage. The dome is covered by an u~pressurized fairing, thus obtaining a smooth junction at the upper fuselage. Five window frames are fitted into the frames between. the fuselage hood ring and cockpit dcme , These five window frarnes are fitted trith three f orwar-d facing windshields. The two frames, one on each side of the cockpit, are each fit. t. edwith a fixed window and a sliding wind
Less
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 95
Views: 1
Downloads: 0
VISCOUNT f·LAINTENA:;CEVLANUAL
G HAPTER 45
CHAPTER 45
nlDEX 1
D!·~tlE Dec 14/66
FUSELAGE STRUCTURE
MAlNTENANCE
FUSELAGE STRUCTUIm l"LUNTENJlNCE
.
10 General
.
11 Lubrication
.
12 Pres sure Seal:iJ1g
.
13 Damage Limitations
.
14 Contamination By Alkali Batteries
.
15 Protective Paint Schemes
.
16 Temporary Skin Repairs
.
17 Sealing of...
More
VISCOUNT f·LAINTENA:;CEVLANUAL G HAPTER 45 CHAPTER 45 nlDEX 1 D!·~tlE Dec 14/66 FUSELAGE STRUCTURE MAlNTENANCE FUSELAGE STRUCTUIm l"LUNTENJlNCE . 10 General . 11 Lubrication . 12 Pres sure Seal:iJ1g . 13 Damage Limitations . 14 Contamination By Alkali Batteries . 15 Protective Paint Schemes . 16 Temporary Skin Repairs . 17 Sealing of Rivets . 18 Use of Duralac . 19 Radome Removal . 20 Dummy Radome Installation . 21 Radome Installation . 22 Radome Damage LL~its . 23 Nose Gear Bracing Structure ILLUSTRATIONS Fig. 1 Knife-Cut Rupture Fit. 2 Hole Damage Fig. 3 Nose U/G Br-ac mg Structure Fig. 4 Detail of Nose ulC Bracing StrucD~re HlliDOHS . 10 General . 11 Cabin 1rJindowsMaintenance . 12 Cabin v. TindowInstallation . 13 Emergency Window Operational Check . 14 Cabin ~hndow Removal . 15 Loose Window Spacer Rubber Covers . 16 Direct Vision Panels . 17 Direct Vision w indovls- Installation . 18 Nesa Windshield - Service Limitations . 19 Nesa Windshield - Removal ~20 Nesa Windshield - Ins
Less
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 119
Views: 3
Downloads: 0
CHAPTER h8
VISCOiJNTMAINTENANCEMANUAL
NACELLES STRUCTURE
S~;CTION 1
S~~CTION 2
SECTION J
SECTION 4
DESCRIPTION
NACELLES STRUCTUHE DESCRIPTION
.
10 General
UNASSIGNED
INNER NACELLES
.
10 Nacelle Structure
•11 Fairings
.
12 Collector Drains
ILLUSTRATIONS
CHAPTER 48
INDEX 1
DATE May 2/60
Fig.
1 Inner Nacelle Station Diagram
Fig.
2...
More
CHAPTER h8 VISCOiJNTMAINTENANCEMANUAL NACELLES STRUCTURE S~;CTION 1 S~~CTION 2 SECTION J SECTION 4 DESCRIPTION NACELLES STRUCTUHE DESCRIPTION . 10 General UNASSIGNED INNER NACELLES . 10 Nacelle Structure •11 Fairings . 12 Collector Drains ILLUSTRATIONS CHAPTER 48 INDEX 1 DATE May 2/60 Fig. 1 Inner Nacelle Station Diagram Fig. 2 Inner Nacelle Access and Inspection Panels Fig. 3 Inner Nacelle Structure OUTm NACELLES . 10 Nacelle Structure . 11 Fairings . 12 Collector Drains ·ILLUSTRATIONS Fig. 1 Outer Nacelle Station Diagram Fig. 2 Outer Nacelle Access and Inspection Panels Fig. 3 Outer Nacelle Trans-Canada Air Lines W W W . AEROVISION. ORG
Less
From Antoine Daoust
Adobe PDF document
Pub. on July 22nd 2011
Pages: 38
Views: 2
Downloads: 0
Canada
Facebook
Digg
del.icio.us
Furl
rededit
StumbleUpon