Specifications Subject to Verification/Inspection.
CESSNA 414A · Specifications
Overview
This document provides specifications for the 1981 Cessna 414A RAM VII, detailing its airframe, engines, avionics, and additional features. It serves as a reference for potential buyers or aviation enthusiasts interested in the aircraft's capabilities and maintenance history. The document outlines critical information such as total time on airframe and engines, maintenance schedules, and equipment installed, making it a valuable resource for understanding the aircraft's performance and operational limits.
- Total airframe time: 4921 hours
- Engine SMOH: 1111 hours each
- Max takeoff weight: 7087 lbs
- Useful load: 2062 lbs
- Fuel capacity: 206 gallons
- Max range: 1328 nautical miles
- Annual maintenance due: April 2019
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at macairgroup.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Year ·
- 1981
- Pages ·
- 4
- File size ·
- 2.4 MB
- Copy found at ·
- macairgroup.com
What is the Specifications Subject to Verification/Inspection.?
The Specifications Subject to Verification/Inspection. is a specifications for the CESSNA 414A, dated 1981.
How many pages is the Specifications Subject to Verification/Inspection.?
The copy of the Specifications Subject to Verification/Inspection. on file runs 4 pages.
What year was the Specifications Subject to Verification/Inspection. published?
The Specifications Subject to Verification/Inspection. — the CESSNA 414A specifications on file — is dated 1981.
Common. More common than 94% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 414A.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Airframe & Engines
The Cessna 414A has a total time of 4921 hours on the airframe. Both engines are RAM Continental TSIO-520-NB, each producing 335 HP, with a time since major overhaul (SMOH) of 1111 hours. The engines have a recommended time between overhaul (TBO) of 1600 hours.
Weights, Capacities & Capabilities
The maximum takeoff weight of the Cessna 414A is 7087 lbs, with a useful load of 2062 lbs. The fuel capacity is 206 gallons, allowing for a maximum range of 1328 nautical miles.
Avionics
The aircraft is equipped with advanced avionics including dual Garmin GNS-530 W and GNS-430 W GPS/Com systems, a Shadin 2001 fuel totalizer, and a JPI EDM760 twin engine monitor. Additional features include an S-TEC 55X autopilot with yaw damper and a Bendix RDR 160C color radar.
Maintenance History
The aircraft's annual maintenance is due in April 2019. It has complete logs and no known major damage history, indicating a well-maintained aircraft.
Additional Features
Notable features include a 77 cubic foot oxygen system, heated glass windshield, factory air conditioning, known ice capabilities, RAM winglets, and vortex generators.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
100 Aviation Boulevard South Portland, Maine 04106 Portland International Jetport (PWM) 207.780.1811 wwwmacjets.com Specifications Subject to Verification/Inspection. 1981 Cessna 414A RAM VII with RAM Winglets Serial#: 414A0634 Registration#: N675R Last Updated: 5/29/2018 Current Aircraft Location: Florida KFMY Airframe: 4921 TT Hours Engine: #1 1111 SMOH / RAM Continental TSIO-520-NB 335HP / TBO 1600 Engine: #2 1111 SMOH / RAM Continental TSIO-520-NB 335 HP / TBO 1600 Propellers: Left 1085 SMOH / Right 903 SMOH McCauley 3AF32C515 Maintenance: Annual Due April 2019 Garmin GNS-530 W GPS / Com Pilot HSI and Flight Director / Horizon Garmin GNS 430 W GPS / Com Shadin 2001 Fuel Totalizer Garmin GTX-328 Transponders “Dual” JPI EDM760 Twin Engine Monitor Garmin GDL-69A XM Weather KRA10 Radar Altimeter S-TEC 55X W / Yaw Damper Auto Pilot Shadin AMS-2000 Altitude Management Sys. Bendix RDR 160C Color Radar BFG 497 Skywatch Traffic ARC 800 Transponder RAM Syncrophaser PMA 8000BT Audio Panel Flight Director WX 10A Storm Scope 406 MHz ELT ADDITIONAL FEATURES 77 Cubic Foot Oxygen System Heated Glass Windshield Factory Air Conditioning Known Ice RAM Winglets 421 Style Seats GAMI Injectors RAM Hubcaps Tanis Engine Heaters Vortex Generators Complete Logs No Known Major Damage History AIRFRAME & ENGINES AVIONICS 100 Aviation Boulevard South Portland, Maine 04106 Portland International Jetport (PWM) 207.780.1811 wwwmacjets.com Specifications Subject to Verification/Inspection. PAINT & INTERIOR Exterior Matterhorn White with Gray Accent Stripes - New 2007 Interior Gray Leather Seats - New 2009 WEIGHTS, CAPACIIES & CAPABILITES Gross Weight (lbs.): 7087 lbs. Max T. O. weight Useful Load (lbs): 2062 Fuel Capacity (gal): 206 Gallons Max Range (nm): 1328 nm CONTACT MAC Aircraft Sales, LLC Joe Mottershead Sales Manager jmottershead@macaircraftsales.com Tel: +1 207-780-1811 Cell 207-671-9748 100 Aviation Boulevard South Portland, Maine 04106 Portland International Jetport (PWM) 207.780.1811 wwwmacjets.com Specifications Subject to Verification/Inspection. 100 Aviation Boulevard South Portland, Maine 04106 Portland International Jetport (PWM) 207.780.1811 wwwmacjets.com Specifications Subject to Verification/Inspection.