Page 3
Rev 21
76-00-00
Engine Controls
DA20-C1 AMM
DA201-C1
14 Jan 13
B.
Mixture Control
The mixture control sets the fuel mixture between RICH and LEAN. It also stops the fuel supply to
the engine when set to CUTOFF. The mixture lever attaches to the control quadrant in the center
console. The mixture lever is the right hand lever in the control quadrant.
The mixture control lever has a lock-out lever attached. The lock-out lever prevents accidental
movement of the mixture control lever. The spring loaded lock-out lever engages in a toothed rack.
The toothed rack attaches to the tubular spacers at the right of the control quadrant.
A bowden cable connects between the mixture lever in the cockpit and the mixture control-lever at
the engine. The bowden-cable wire-end attaches to the mixture lever through a hole in a swivel
fitting. A screw locks it in position. A bracket holds the inboard end of the swivel fitting. Two rivets
attach the bracket to the mixture lever. The outer sheath of the bowden cable has a threaded end
fitting. Two nuts attach the end fitting to a tab on the side of the control quadrant.
The bowden cable goes from the center console up, behind the instrument panel and through the
firewall to the engine bay. A feed-thru fitting holds the cable in position at the firewall. A fire
resistant compound seals the bowden cable where it goes through the firewall. From the firewall
the bowden cable goes through a rubber grommet in the aft baffle on the left hand side.
On aircraft equipped with a standard fuel pump, the outer sheath of the mixture control bowden
cable has a threaded end that attaches to a bracket at the apron with two nuts, which can be used
to adjust the range of movement of the mixture control lever. The bowden-cable wire-end attaches
to the fuel-mixture control-lever of the fuel pump through a hole in the attachment bolt. You can
adjust the length of the wire at this point to set the correct fuel mixture control position.
On aircraft equipped with an altitude compensating fuel pump, the mixture cable has a notched
swivel termination at the engine end. The notch slides onto the mixture support bracket, which is
fastened to the apron. A keeper is bolted to the bracket to secure the bowden cable. There is a
rod-end attached to the end of the bowden cable that connects the mixture control cable to the fuel
mixture lever by a bolt.
C.
Alternate Air
The alternate air control opens a by-pass for the engine air filter if it becomes blocked with debris
or ice. The alternate air lever attaches to the control quadrant in the center console. The alternate
air lever is the left hand lever in the control quadrant.
A bowden cable connects between the alternate air lever in the cockpit and the lever at the air-box.
The bowden-cable wire-end attaches to the alternate air lever through a hole in a swivel fitting. A
screw locks it in position. A small bracket holds the inboard end of the swivel fitting. Two rivets
attach the bracket to the alternate air lever.
The outer sheath of the bowden cable has a threaded end fitting. The end fitting attaches to a tab
bent from the side of the quadrant.
The bowden cable goes from the center console, up behind the instrument panel and through the
firewall to the engine bay. A feed-thru fitting holds the cable in position at the firewall. A fire
resistant compound seals the bowden cable where it goes through the firewall.
Summary of Contents for DA20-C1
Page 25: ...Page 1 Rev 16 52 TITLE Doors DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 52 00 DOORS ...
Page 26: ...Doors DA20 C1 AMM 52 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 28: ...52 TOC DA20 C1 AMM Doors 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 30: ...Doors DA20 C1 AMM 52 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 34: ...Doors DA20 C1 AMM 52 10 00 30 Oct 09 Page 4 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 48: ...Doors DA20 C1 AMM 52 40 00 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 49: ...Page 1 Rev 16 53 TITLE Fuselage DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 53 00 FUSELAGE ...
Page 50: ...Fuselage DA20 C1 AMM 53 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 52: ...53 TOC DA20 C1 AMM Fuselage 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 54: ...Fuselage DA20 C1 AMM 53 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 67: ...Page 1 Rev 16 55 TITLE Stabilizers DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 55 00 STABILIZERS ...
Page 68: ...Stabilizers DA20 C1 AMM 55 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 72: ...Stabilizers DA20 C1 AMM 55 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 74: ...Stabilizers DA20 C1 AMM 55 10 00 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 80: ...Stabilizers DA20 C1 AMM 30 Oct 09 Page 2 DA201 C1 Rev 16 55 20 00 Figure 1 Elevator Structure ...
Page 93: ...Page 1 Rev 16 56 TITLE Windows DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 56 00 WINDOWS ...
Page 94: ...Windows DA20 C1 AMM 56 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 96: ...56 TOC DA20 C1 AMM Windows 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 98: ...Windows DA20 C1 AMM 56 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 103: ...Page 5 Rev 16 56 10 00 Windows DA20 C1 AMM DA201 C1 30 Oct 09 Figure 3 Crack Repairs ...
Page 109: ...Page 1 Rev 16 57 TITLE Wings DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 57 00 WINGS ...
Page 110: ...Wings DA20 C1 AMM 57 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 112: ...57 TOC DA20 C1 AMM Wings 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 114: ...Wings DA20 C1 AMM 57 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 119: ...Page 5 Rev 16 57 10 00 Wings DA20 C1 AMM DA201 C1 30 Oct 09 Figure 2 Wing Structure Ribs ...
Page 120: ...Wings DA20 C1 AMM 57 10 00 30 Oct 09 Page 6 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 132: ...Wings DA20 C1 AMM 30 Oct 09 Page 2 DA201 C1 Rev 16 57 50 00 Figure 1 Flap Structure ...
Page 138: ...Wings DA20 C1 AMM 30 Oct 09 Page 2 DA201 C1 Rev 16 57 60 00 Figure 1 Aileron Structure ...
Page 141: ...Page 1 Rev 16 61 TITLE Propeller DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 61 00 PROPELLER ...
Page 142: ...Propeller DA20 C1 AMM 61 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 144: ...61 TOC DA20 C1 AMM Propeller 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 146: ...Propeller DA20 C1 AMM 61 00 00 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 148: ...Propeller DA20 C1 AMM 61 10 00 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 157: ...Page 1 Rev 16 71 TITLE Power Plant DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 71 00 POWER PLANT ...
Page 158: ...Power Plant DA20 C1 AMM 71 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 162: ...Power Plant DA20 C1 AMM 14 Jan 13 Page 2 DA201 C1 Rev 21 71 00 00 Figure 1 Power Plant ...
Page 166: ...Power Plant DA20 C1 AMM 71 00 00 14 Jan 13 Page 6 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 192: ...Power Plant DA20 C1 AMM 30 Oct 09 Page 2 DA201 C1 Rev 16 71 10 00 Figure 1 Engine Cowlings ...
Page 202: ...Power Plant DA20 C1 AMM 71 20 00 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 214: ...Power Plant DA20 C1 AMM 71 70 00 30 Oct 09 Page 4 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 221: ...Page 1 Rev 16 72 TITLE Engine DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 72 00 ENGINE ...
Page 222: ...Engine DA20 C1 AMM 72 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 224: ...72 TOC DA20 C1 AMM Engine 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 226: ...Engine DA20 C1 AMM 14 Jan 13 Page 2 DA201 C1 Rev 21 72 00 00 Figure 1 Engine ...
Page 247: ...Page 1 Rev 16 74 TITLE Ignition DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 74 00 IGNITION ...
Page 248: ...Ignition DA20 C1 AMM 74 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 250: ...74 TOC DA20 C1 AMM Ignition 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 254: ...Ignition DA20 C1 AMM 74 00 00 14 Jan 13 Page 4 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 269: ...Page 1 Rev 16 75 TITLE Air DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 75 00 AIR ...
Page 270: ...Air DA20 C1 AMM 75 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 272: ...75 TOC DA20 C1 AMM Air 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 290: ...76 TOC DA20 C1 AMM Engine Controls 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 343: ...Page 1 Rev 16 78 TITLE Exhaust DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 78 00 EXHAUST ...
Page 344: ...Exhaust DA20 C1 AMM 78 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 346: ...78 TOC DA20 C1 AMM Exhaust 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 348: ...Exhaust DA20 C1 AMM 14 Jan 13 Page 2 DA201 C1 Rev 21 78 00 00 Figure 1 Exhaust ...
Page 355: ...Page 1 Rev 16 79 TITLE Oil DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 79 00 OIL ...
Page 356: ...Oil DA20 C1 AMM 79 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 358: ...79 TOC DA20 C1 AMM Oil 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 364: ...Oil DA20 C1 AMM 79 00 00 14 Jan 13 Page 6 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 379: ...Page 1 Rev 16 80 TITLE Starting DA20 C1 AMM DA201 C1 30 Oct 09 CHAPTER 80 00 STARTING ...
Page 380: ...Starting DA20 C1 AMM 80 TITLE 30 Oct 09 Page 2 DA201 C1 Rev 16 Intentionally Left Blank ...
Page 382: ...80 TOC DA20 C1 AMM Starting 14 Jan 13 Page 2 DA201 C1 Rev 21 Intentionally Left Blank ...
Page 392: ...Wiring Diagrams DA20 C1 AMM 92 TOC 14 Jan 13 Page 4 DA201 C1 Rev 21 Intentionally Left Blank ...