{"id":89,"date":"2016-08-07T15:15:06","date_gmt":"2016-08-07T22:15:06","guid":{"rendered":"http:\/\/ec2-54-164-154-147.compute-1.amazonaws.com\/?page_id=89"},"modified":"2016-08-08T18:39:36","modified_gmt":"2016-08-09T01:39:36","slug":"specs","status":"publish","type":"page","link":"https:\/\/www.n915l.com\/?page_id=89","title":{"rendered":"Data Sheet"},"content":{"rendered":"

*Do Not Use This Information For Flight Planning<\/span><\/b><\/p>\n

Powerplant<\/h5>\n\n\n\n
Engine Make
\nEngine Model
\nPower<\/p>\n

Propeller Make
\nPropeller Model<\/td>\n

Lycoming
\nO-320-E2D
\n150hp@2700rpm<\/p>\n

McCauley
\n1C160\/DTM7553<\/td>\n

Oil Quantity
\nOil Type (>16\u00b0C)
\n(-18\u00b0C-21\u00b0C)<\/p>\n

RPM Limit<\/td>\n

6qt.-8qt.
\nSAE50
\nSAE10W30<\/p>\n

2700rmp<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n

Engine Type: Four cylinders, direct drive, horizontally opposed, air cooled, carburetor-equipped.
\nPropeller Type: two blades, fixed pitch.<\/p><\/blockquote>\n

Fuel System<\/h5>\n\n\n\n
Total Capacity
\nTotal Usable<\/td>\n		42gal.
\n28gal.<\/td>\n		Each Tank
\nApproved Grades<\/td>\n		21gal.
\n100LL,\u00a0<\/span>100<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n

System Description: The airplane is equipped with a standard fuel system consisting of two vented fuel tanks, a fuel tank selector valve, fuel strainer, manual primer, and carburetor. Fuel flows by gravity from one or both tanks to the fuel selector, through a fuel strainer to the carburetor. From the carburetor, the fuel\/air mixture flows to the cylinders. The fuel selector should be in the BOTH position for takeoff, climb, descent, landing, and maneuvers that involve prolonged slips or skids. Operation from either the LEFT or RIGHT position is reserved for level cruising flight only<\/p><\/blockquote>\n

Weight Limites<\/h5>\n

Open Weight and Balance Calculator<\/a><\/p>\n\n\n\n
\nRamp Weight
\nTakeoff Weight
\nLanding Weight
\nBaggage Weight
\nArea 1
\nArea 2<\/td>\n		Normal<\/span>
\n2307 lbs.
\n2300 lbs.
\n2300 lbs.
\n120 lbs.
\n120 lbs.
\n50 lbs.<\/td>\n		Utility<\/span>
\n2007 lbs.
\n2000 lbs.
\n2000 lbs.
\nnone
\nnone
\nnone<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n
Electrical System<\/h5>\n\n\n\n
Alternator<\/td>\n14 vlot, 60 amp<\/td>\nBattery<\/td>\n12 volt, 25 amp hour<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n

System Description: Power is supplied to most general electrical items through the primary bus. All avionics are powered by the avionics bus. The two busses are tied together through the avionics power switch, which also functions as a circuit breaker for the avionics bus. The avionics power switch should be turned off prior to starting the engine to prevent harmful transient voltages from damaging the avionics equipment. The ammeter shows a charge or discharge on the battery and should remain at or near the zero indication after a brief charging period.<\/p><\/blockquote>\n

Tire Inflation<\/h5>\n\n\n\n
Main Tires<\/td>\n29 psi.<\/td>\nNose Tire<\/td>\n31 psi.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n
Airspeed Limitations<\/h5>\n\n\n\n
Never Exceed Speed
\nMax.\u00a0Structural Cruising Speed
\nManeuvering Speed
\n2300 lbs.
\n1600 lbs.
\nMax.\u00a0Flaps extended Speed<\/td>\n		VNE<\/sub>
\nVNO<\/sub>
\nVA<\/sub><\/p>\n

VFE<\/sub><\/td>\n

160 KIAS
\n128 KIAS<\/p>\n

97 KIAS
\n80 KIAS
\n85 KIAS<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n\n\n\n
BEST GLIDE SPEED
\nStalling Speed, Flaps Up
\nStalling Speed, Landing Configuration
\nBest Angle-of-Climb Speed, Sea Level
\nBest Rate-of-Climb Speed, Sea Level
\nRotate Speed
\nEnroute Climb
\nNormal Approach, Flaps Up
\nNormal Approach, Flaps 40\u00b0
\nSoft Field Approach, Flaps\u00a040\u00b0
\nMax. Demonstrated Crosswind Component<\/td>\n		VG<\/sub>
\nVS<\/sub>
\nVS0<\/sub>
\nVX<\/sub>
\nVY<\/sub>
\nVR<\/sub><\/td>\n		65 KIAS
\n47 KIAS
\n41 KIAS
\n64 KIAS
\n78 KIAS
\n55 KIAS
\n80-90 KIAS
\n60-70 KIAS
\n55-65 KIAS
\n60 KIAS
\n15\u00a0KNOTS<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n
Links<\/h5>\n

1976 Cessna 172M PILOT’S OPERATING HANDBOOK<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"

*Do Not Use This Information For Flight Planning Powerplant Engine Make Engine Model Power Propeller Make Propeller Model Lycoming O-320-E2D 150hp@2700rpm McCauley 1C160\/DTM7553 Oil Quantity Oil Type (>16\u00b0C) (-18\u00b0C-21\u00b0C) RPM Read More …<\/a><\/span><\/p>\n","protected":false},"author":3,"featured_media":283,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":[],"_links":{"self":[{"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/pages\/89"}],"collection":[{"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/users\/3"}],"replies":[{"embeddable":true,"href":"https:\/\/www.n915l.com\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=89"}],"version-history":[{"count":140,"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/pages\/89\/revisions"}],"predecessor-version":[{"id":287,"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/pages\/89\/revisions\/287"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/www.n915l.com\/index.php?rest_route=\/wp\/v2\/media\/283"}],"wp:attachment":[{"href":"https:\/\/www.n915l.com\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=89"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}