1 LAMBADA SMALL CERTIFICATION



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Transcription:

1 LAMBADA SMALL CERTIFICATION GS Testflug DHV03 Apco Lambada S Deutscher Hängegleiterverband e.v. im DAeC DHV/OeAeC-Technikreferat LBA-anerkannte Prüfstelle für Hängegleiter und Gleitsegel Beauftragter der österreichischen Luftfahrtbehörde Test No 015380-GSTF03-654-Claude Test date 08.10.2005 Type Apco Lambada S Test type GS Testflug DHV03 Order Auftrag GS Musterprüfung Apco Lambada S, GS Ö MAK Apco Lambada S (Apco Aviation Ltd.) Customer Apco Aviation Ltd. Test standard Lufttüchtigkeitsforderungen für HG und GS Expert Thurnheer Result positive Billing to: 100% Technical peculiarities Datum / Unterschrift (Thurnheer) DHV test flight main data Harness type Advance Hi-Comp Take off weight [kg] 70 Weight limit for certification [kg] 70 Number of pilots 1 Trim speed [km/h] 36 Accelerated speed [km/h] 43 Classification 2 Supplementary remarks PG test flight specific Harness category GH Accelerator used? Yes Trimms - DHV PG Test flight 2003 data

Take off Take off class. 1-2 Inflation evenly, immediately Rising behaviour immediately comes over pilot Take off speed Take off handling Straight flight Straight flight class. 2 Speed range Roll damping Pitch damping Yaw stability Turn handling Turn handling class. 2 Spin tendency Control travel Agility Control pressure increase Control without brakes control through rear risers possible Symmetric stall Deep-stall limit 2 Deep-stall limit 60 cm - 75 cm Full stall limit 65 cm - 80 cm Full stall with full steering way yes, soft stall Falling back Increase in steering power Front collapse Front collapse class. 2 Effort Pre-acceleration Front collapse (accelerated) Front collapse accelerated class. 2 Effort Pre-acceleration Asymmetric collapse Asymmetric collapse class. 2

Change of course Max. roll/pitch angle < 90 degrees with deceleration greater than 45 degrees spontaneous spontaneous Asymmetric collapse (accelerated) Asymmetric collapse acc. class. 2 Change of course < 90 degrees with deceleration Max. roll/pitch angle greater than 45 degrees spontaneous spontaneous Countersteering an asymmetric collapse Countersteering an asymmetric collapse class. 2 countersteering Control travel Control pressure increase Turn in opposite direction, no tendency to stall Full stall, symm. exit Fullstall, symm. exit class 2 Behaviour stable - shoot forward no collapse no turn

Spin out of straight flight Spin out of straight flight class. 2 turn continues through shoot forward to one side no collapse no turn Spin out of turn Spin out of turn class. 1-2 shoot forward to one side no collapse no turn Spiral dive Spiral dive class. 2 Spin tendency turn continues through 180-360 degrees Sink rate after 720 [m/s] 10 B-line stall B-line stall class. 2 delayed acceleration < 4 sec Big ears Big ears 1-2 Recovery spontaneous, quickly Big ears accelerated Big ears acc. class. 1-2

Recovery spontaneous, quickly Landing Landing class. 2 Point of flare Landing speed Landing behaviour 08.11.2005 15:52:11 qi=250012 GS Testflug DHV03 Apco Lambada S Deutscher Hängegleiterverband e.v. im DAeC DHV/OeAeC-Technikreferat LBA-anerkannte Prüfstelle für Hängegleiter und Gleitsegel Beauftragter der österreichischen Luftfahrtbehörde Test No 015319-GSTF03-633-Harry Test date 09.10.2005 Type Apco Lambada S Test type GS Testflug DHV03 Order Auftrag GS Musterprüfung Apco Lambada S, GS Ö MAK Apco Lambada S (Apco Aviation Ltd.) Customer Apco Aviation Ltd. Test standard Lufttüchtigkeitsforderungen für HG und GS Expert Buntz Result positive Billing to: 100% Technical peculiarities Datum / Unterschrift (Buntz) DHV test flight main data Harness type PEAK Take off weight [kg] 90 Weight limit for certification [kg] 90 Number of pilots 1 Trim speed [km/h] 36 Accelerated speed [km/h] 44 Classification 2

Supplementary remarks Tendenz zu impulsiven Gegenklappern PG test flight specific Harness category GH Accelerator used? Yes Trimms - DHV PG Test flight 2003 data Take off Take off class. 1-2 Inflation evenly, immediately Rising behaviour immediately comes over pilot Take off speed Take off handling Straight flight Straight flight class. 2 Speed range Roll damping Pitch damping Yaw stability Turn handling Turn handling class. 2 Spin tendency Control travel Agility Control pressure increase Control without brakes control through rear risers possible Symmetric stall Deep-stall limit 2 Deep-stall limit 60 cm - 75 cm Full stall limit 65 cm - 80 cm Full stall with full steering way yes, soft stall Falling back Increase in steering power Front collapse Front collapse class. 2 Effort Pre-acceleration Front collapse (accelerated)

Front collapse accelerated class. 2 Effort Pre-acceleration Asymmetric collapse Asymmetric collapse class. 2 Change of course 180-360 degrees Max. roll/pitch angle greater than 45 degrees Asymmetric collapse (accelerated) Asymmetric collapse acc. class. 2 < 90 degrees Change of course 180-360 degrees Max. roll/pitch angle greater than 45 degrees Countersteering an asymmetric collapse Countersteering an asymmetric collapse class. 2 countersteering Control travel Control pressure increase Turn in opposite direction, no tendency to stall Full stall, symm. exit Fullstall, symm. exit class 2 Behaviour nervous

strong shoot forward front collapse Spin out of straight flight Spin out of straight flight class. 2 turn continues through < 90 degrees strong shoot forward to one side asymmetric collapse Spin out of turn Spin out of turn class. 2 strong shoot forward to one side asymmetric collapse Spiral dive Spiral dive class. 2 Spin tendency turn continues through 180-360 degrees Sink rate after 720 [m/s] 9 B-line stall B-line stall class. 2

delayed acceleration < 4 sec Big ears Big ears 2 Recovery not spontaneously Big ears accelerated Big ears acc. class. 2 Recovery not spontaneously Landing Landing class. 2 Point of flare Landing speed Landing behaviour 08.11.2005 15:51:17 qi=250012