Army Preliminary Evaluation I. RV-1D/Quick Look II Aircraft

The United States Army Aviation Engineering Flight Activity conducted a limited handling qualities evaluation of the RV-1D/Quick Look II aircraft, manufactured by Grumman Aerospace Corporation. The aircraft was tested at the Grumman facility in Stuart, Florida, on 16 and 17 July 1974. Testing includ...

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Hauptverfasser:	Bender, Gary L, O'Connor, James C
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMIC STABILITY Aircraft modifications AIRSPEED Airworthiness FLIGHT ENVELOPE FLIGHT MANEUVERS FLIGHT TESTING OBSERVATION AIRCRAFT OV-1 D aircraft Patrol and Reconnaissance Aircraft Quick look 2 aircraft RV-1D aircraft STALLING TURBOPROP ENGINES V-1 aircraft
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creator	Bender, Gary L O'Connor, James C
description	The United States Army Aviation Engineering Flight Activity conducted a limited handling qualities evaluation of the RV-1D/Quick Look II aircraft, manufactured by Grumman Aerospace Corporation. The aircraft was tested at the Grumman facility in Stuart, Florida, on 16 and 17 July 1974. Testing included stability and control and miscellaneous engineering tests necessary to verify the flight envelope. No deficiencies were found during these tests. Two shortcomings were identified: inadequate stall warning in the power-approach and landing configurations, and the degraded single-engine performance and maneuvering capability caused by the inabilitey to jettison the Quick Look II antenna pods.
format	Report
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RV-1D/Quick Look II Aircraft</title><source>DTIC Technical Reports</source><creator>Bender, Gary L ; O'Connor, James C</creator><creatorcontrib>Bender, Gary L ; O'Connor, James C ; ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA</creatorcontrib><description>The United States Army Aviation Engineering Flight Activity conducted a limited handling qualities evaluation of the RV-1D/Quick Look II aircraft, manufactured by Grumman Aerospace Corporation. The aircraft was tested at the Grumman facility in Stuart, Florida, on 16 and 17 July 1974. Testing included stability and control and miscellaneous engineering tests necessary to verify the flight envelope. No deficiencies were found during these tests. Two shortcomings were identified: inadequate stall warning in the power-approach and landing configurations, and the degraded single-engine performance and maneuvering capability caused by the inabilitey to jettison the Quick Look II antenna pods.</description><language>eng</language><subject>AERODYNAMIC STABILITY ; Aircraft modifications ; AIRSPEED ; Airworthiness ; FLIGHT ENVELOPE ; FLIGHT MANEUVERS ; FLIGHT TESTING ; OBSERVATION AIRCRAFT ; OV-1 D aircraft ; Patrol and Reconnaissance Aircraft ; Quick look 2 aircraft ; RV-1D aircraft ; STALLING ; TURBOPROP ENGINES ; V-1 aircraft</subject><creationdate>1974</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27546,27547</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA005220$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Bender, Gary L</creatorcontrib><creatorcontrib>O'Connor, James C</creatorcontrib><creatorcontrib>ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA</creatorcontrib><title>Army Preliminary Evaluation I. RV-1D/Quick Look II Aircraft</title><description>The United States Army Aviation Engineering Flight Activity conducted a limited handling qualities evaluation of the RV-1D/Quick Look II aircraft, manufactured by Grumman Aerospace Corporation. The aircraft was tested at the Grumman facility in Stuart, Florida, on 16 and 17 July 1974. Testing included stability and control and miscellaneous engineering tests necessary to verify the flight envelope. No deficiencies were found during these tests. Two shortcomings were identified: inadequate stall warning in the power-approach and landing configurations, and the degraded single-engine performance and maneuvering capability caused by the inabilitey to jettison the Quick Look II antenna pods.</description><subject>AERODYNAMIC STABILITY</subject><subject>Aircraft modifications</subject><subject>AIRSPEED</subject><subject>Airworthiness</subject><subject>FLIGHT ENVELOPE</subject><subject>FLIGHT MANEUVERS</subject><subject>FLIGHT TESTING</subject><subject>OBSERVATION AIRCRAFT</subject><subject>OV-1 D aircraft</subject><subject>Patrol and Reconnaissance Aircraft</subject><subject>Quick look 2 aircraft</subject><subject>RV-1D aircraft</subject><subject>STALLING</subject><subject>TURBOPROP ENGINES</subject><subject>V-1 aircraft</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1974</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZLB2LMqtVAgoSs3JzM3MSyyqVHAtS8wpTSzJzM9T8NRTCArTNXTRDyzNTM5W8MnPz1bw9FRwzCxKLkpMK-FhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji6OBgamRkYGxgSkARklKo0</recordid><startdate>197408</startdate><enddate>197408</enddate><creator>Bender, Gary L</creator><creator>O'Connor, James C</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197408</creationdate><title>Army Preliminary Evaluation I. 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source	DTIC Technical Reports
subjects	AERODYNAMIC STABILITY Aircraft modifications AIRSPEED Airworthiness FLIGHT ENVELOPE FLIGHT MANEUVERS FLIGHT TESTING OBSERVATION AIRCRAFT OV-1 D aircraft Patrol and Reconnaissance Aircraft Quick look 2 aircraft RV-1D aircraft STALLING TURBOPROP ENGINES V-1 aircraft
title	Army Preliminary Evaluation I. RV-1D/Quick Look II Aircraft
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