Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA
CESSNA 172R SKYHAWK · Checklist
Overview
This document is a checklist for the 1998 Cessna Skyhawk 172R, detailing essential aircraft data, operational speeds, and performance specifications. It includes information on weight limits, fuel capacity, and electrical systems, as well as V-speeds for various flight maneuvers.
- Empty weight: 1666.20 lbs
- Max takeoff weight: 2550.0 lbs
- Useful load: 790.80 lbs
- Fuel capacity: 56 gallons
- Usable fuel: 53 gallons
- Normal category load factor: +3.8 G to -1.52 G
- Maximum crosswind component: 15 knots
- Engine power: 180 HP
Document
Source
Originally published by rochesterair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- Year ·
- 1998
- File size ·
- 838 KB
- Publisher ·
- rochesterair.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Useful load (lb) ·
- 790.80
- Empty weight (lb) ·
- 1666.20
- Usable fuel gals ·
- 53
- Fuel capacity gals ·
- 56
- Max t o weight (lb) ·
- 2550.0
Performance
- Max crosswind component knots ·
- 15
V-speeds
- VA_KIAS ·
- 105
- VG_KIAS ·
- 68
- VR_KIAS ·
- 55
- VX_KIAS ·
- 62
- VY_KIAS ·
- 74
- VNE_KIAS ·
- 163
- VNO_KIAS ·
- 129
- VS1_KIAS ·
- 48
- VSO_KIAS ·
- 40
- VFE_10_DEG_KIAS ·
- 110
- VFE_20_30_DEG_KIAS ·
- 85
What is the Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA?
The Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA is a checklist for the CESSNA 172R SKYHAWK, dated 1998.
Where does the Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA come from?
This copy of the Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA was originally published by rochesterair.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA published?
The Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA — the CESSNA 172R SKYHAWK checklist on file — is dated 1998.
Most owners only have the POH. Here's the essential set for the CESSNA 172R SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA 172R SKYHAWKmanuals & documents
- Supplemental Airplane Flight ManualOther Documents
- Airworthiness Directives; Cessna Aircraft Company Models 172R and 172S AirplanesAirworthiness Directives
- WEIGHT & BALANCE – CESSNA 172 R – N87GVWeight And Balance
- Performance Data for Cessna Model 172R and Challenger 605Performance
- Cessna 172R - G5 ChecklistChecklist
In this document
Aircraft Data
Details the empty weight, maximum takeoff weight, useful load, and fuel capacities.
Electrical System
Describes the alternator and battery specifications.
V-Speeds
Lists various V-speeds including VNE, VNO, VFE, and others for different flight conditions.
Commercial Maneuvers Speeds
Outlines RPM and KIAS for different flight phases and maneuvers.
Go-Around Procedure
Describes the steps for executing a go-around, including flap settings and climb pitch.
Maximum Flaps for Forward Slip
States that the maximum flaps for a forward slip is 20 degrees.
Safety notes
- Minimum oil level: 6 quarts
- Maximum oil level: 8 quarts
- Full power required for go-around
- Flaps should be incrementally raised during climb
- Maintain positive rate of climb before retracting flaps
Full document text
Summary Aircraft Data 1998 Cessna Skyhawk 172R N314RA Empty Weight (lbs) Max T/O Weight (lbs) Useful Load (lbs) Fuel Capacity (gals) Useable Fuel (gals) 1666.20 2550.0 790.80 56 53 Electrical System Engine Oil Alternator 28 V 60 amp 180 HP Min level = 6 qts Battery 24 V 60 amp hr IO-360-L2A Max level = 8 qts Normal Category Load Factor: +3.8 G to -1.52 G V – Speeds KIAS: Standard Traffic Pattern VNE = 163 VNO = 129 VFE = 110 for 10 deg flaps 85 for 20 – 30 deg VA (max T/O weight) = 105 VY = 74 VX = 62 VG = 68 VR = 55 VSO = 40 VS1 = 48 Maximum Crosswind Component = 15 knots @ 90 deg to runway. GO-AROUND: Full Power, Flaps to 20 deg, pitch for normal climb, positive rate of climb established, flaps up incrementally until reaching traffic pattern altitude. Maximum Flaps for Forward Slip = 20 deg Commercial Maneuvers Speeds RPM KIAS Flaps Trim Downwind 1900 85 NONE As Req. Abeam Touchdown Pt. 1700 80 10 deg. As Req. Base 1500 70 – 75 20 deg. As Req. Final 1300 – 1200 60 – 65 30 deg. As Req. Maneuver Entry Speed KIAS Chandelle 105 Lazy Eight 105 Steep Turn (45 – 50 deg bank) 95