Glasair Sportsman GS-2 Owner's Manual

page of 216

/ 216
Contents
Table of Contents
Bookmarks

Table of Contents

Quick Links

Model GS-2

TAILDRAGGER

OWNER'S MANUAL

Serial #__________

P/N 063-03002-01

EVISION

ATE

AGE

12/29/04

Table of Contents

Chapters

Table of Contents

Need help?

Do you have a question about the Sportsman GS-2 and is the answer not in the manual?

Questions and answers

Summary of Contents for Glasair Sportsman GS-2

Page 2 No part of this manual may be reproduced in any form without the prior written permission of the publisher. Copyright 2004 by GLASAIR AVIATION, LLC All Rights Reserved. Printed in USA EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 3: Table Of Contents
EMERGENCY PROCEDURES ...........Section 3 NORMAL OPERATING PROCEDURES ........Section 4 WEIGHT AND BALANCE............Section 5 SYSTEMS DESCRIPTIONS ............Section 6 HANDLING, SERVICE AND MAINTENANCE......Section 7 FLIGHT TEST ................Section 8 SAFETY INFORMATION ............Section 9 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 7: Table Of Contents
1-4 USE OF THE MANUAL ..............4 1-5 REVISIONS ...................5 1-6 WARNINGS, CAUTIONS AND NOTES........5 1-7 AIRPLANE 3-VIEW...............6 1-8 SPECIFICATIONS .................8 1-9 PERFORMANCE DATA ............. 10 1-10 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY....12 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 8: Introduction
Furthermore, this does not provide a discussion of all possible dangerous situations an owner or operator may encounter. Flying in itself is not inherently dangerous, but to an even greater EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 9: Faa Regulations
The performance data presented in this manual are estimates based on flight tests of Glasair Aviation’s own aircraft. Due to differences in the engine and propeller installed, quality of workmanship and many other variables, each airplane will vary somewhat in performance.
Page 10: Use Of The Manual
The manual is divided into nine major sections, which are listed in the Table of Contents. Each section also has its own individual Table of Contents. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 11: Revisions
CAUTION Procedures, practices, etc., which if not strictly observed may result in damage to or destruction of equipment. NOTE An operating procedure, condition, etc., which it is considered essential to emphasize. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 14: Specifications
Front Door Width ................37.0 in. Height ..................31.5 in. Sill to Ground ................33.0 in. Rear Door Width................26.0 in. Height ..................31.0 in. Baggage Space ................37.0 ft. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 15 Auxiliary Tanks ................19 gal. Seats......................4 Tire Size: Main Gear (standard)..............6.00 × 6 Main Gear (optional)...............8.00 × 6 Main Gear (optional)............26.00 × 10.5 Tail Wheel..............2.80/2.50 × 4 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 16: Performance Data
180 h.p..............140 kts./161 m.p.h. Cruise Speed (75% power @ 8,000 ft., TAS): 180 h.p..............135 kts./155 m.p.h. Cruise Speed (65% power @ 8,000 ft., TAS): 180 h.p..............130 kts./149 m.p.h. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 17 Fuel Consumption at 65% power: 180 h.p................8.0 gal./hr. Range at 65% power (no wind, VFR reserve): 180 h.p..............747 n.m./859 s.m. Service Ceiling (estimated): 180 h.p................20,000 ft. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 18: Symbols, Abbreviations And Terminology
— Indicated Airspeed is the speed of an airplane as shown on the airspeed indicator when corrected for instrument error. IAS values published in this manual assume zero instrument error. KIAS — Indicated Airspeed expressed in knots. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 19 — Best Rate-of-Climb Speed is the airspeed that delivers the greatest gain in altitude in the shortest possible time. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 21: Limitations
PEED 2-5 VACUUM PRESSURE ..............9 2-6 WEIGHT LIMITS................9 2-7 CENTER OF GRAVITY LIMITS ............9 2-8 FLIGHT LOAD FACTORS............10 2-9 AEROBATIC MANEUVER LIMITATIONS......... 10 2-10 INTENTIONAL SPINS ............... 10 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 22 2-14 PLACARDS................. 12 2-14.1 P FAR......12 LACARDS ARKINGS EQUIRED BY 2-14.2 F ..........13 ILLER LACARDS 2-14.3 B ....... 13 AGGAGE OMPARTMENT LACARDS 2-14.4 F ........... 13 ALVE ARKINGS EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 23: Airspeed Limitations
Definitions of these airspeeds are given in FAR Part 1, Paragraph 1.2. All airspeeds are calibrated airspeeds (CAS). During flight test, the airspeed indicator should be calibrated so as to distinguish indicated airspeeds (IAS) from CAS. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 24: Airspeed Indicator Markings
* Indicated gross weight stall speed with flaps for the white arc and indicated clean stall speed for the green arc are derived from tests of the Glasair Aviation Sportsman prototype. Slight variations may be experienced in customer-built aircraft. Actual stall speeds should be determined from flight test of each individual aircraft, and the airspeed indicator markings should be adjusted appropriately.
Page 25: Powerplant Limitations
1. Lycoming O-360-A1A, -A1F6 or -A4M engines. Other engines may be installed on the Sportsman, but the above listed engines are the only ones that have been tested by Glasair Aviation and the only ones for which Glasair Aviation supplies propellers, engine mounts, cowlings and other firewall-forward accessories and installations.
Page 26: 2-4.2 Oil Pressure
Start and Warm-up Maximum (red line) ........100 p.s.i. Green Arc ................60–90 p.s.i. 2-4.3 O EMPERATURE Lycoming O-360: Recommended ...............82°C/180°F Maximum (red line)..............118°C/245°F Green Arc ............60°–104°C/140°–220°F Yellow Arc ............38°–60°C/100°–140°F EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 27: 2-4.4 Fuel Pressure
Lycoming O-360 (at inlet to carburetor): Maximum ..................8.0 p.s.i. Recommended..................3.0 p.s.i. Minimum ...................0.5 p.s.i. 2-4.5 C YLINDER EMPERATURE Lycoming O-360: Maximum (red line) ............. 260°C/500°F Normal Operating (green arc)......66°–204°C/150°–400°F EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 28: 2-4.6 Engine Crankshaft Speed
Sensenich prop. The O-360-A4M is a solid-crank engine that cannot be used with a constant-speed propeller, but has no r.p.m. restrictions for the Sensenich fixed-pitch propeller. 2-5 VACUUM PRESSURE Operating Range ..............4.3–5.9 in. Hg EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 29: Weight Limits
The reference datum is 58.0 in. forward of the cowling attach flange joggle. Stations are measured in inches from the datum. See “S ECTION 5: W ” for further information. EIGHT AND ALANCE EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 30: Flight Load Factors
2-10 INTENTIONAL SPINS Due to many variables that affect spin recovery and our lack of control over these variables, Glasair Aviation prohibits intentional spins in the Sportsman. Some of the variables are: pilot technique, the manner in which the spin is entered, slight differences in wing and horizontal...
Page 31: Flight In Icing Conditions
Part 23 standards for lightning protection. For this reason, the Sportsman is prohibited from flight in conditions that would expose the airplane to the possibility of a lightning strike. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 32: Required Equipment
FAR 45.13. This information includes the name of the manufacturer (your name, not Glasair Aviation), the aircraft type (Sportsman GS-2), and the serial number (your kit number). The data plate must be located on the exterior of the aircraft, either just...
Page 33: 2-14.2 Fuel Filler Cap Placards
2. A placard such as, “Keep all articles securely stowed to avoid the possibility of interference with the control system.” 2-14.4 F ALVE ARKINGS Clearly mark the ON (pointing forward) and OFF (pointing to the right) positions of the fuel valve. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 35 3-3.3.2 In-Flight Engine Fire..........3-3.3.3 Electrical Fire on the Ground ........ 3-3.3.4 In-Flight Electrical Fire........... 3-3.4 S ............8 PINS AND PIRAL IVES 3-3.4.1 Spin Recovery ............3-3.4.2 Spiral Dive Recovery..........EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 36: Emergency Procedures
3-4.3.2 In-Flight Engine Fire ..........3-4.3.3 Electrical Fire on the Ground......3-4.3.4 In-Flight Electrical Fire ........3-4.4 S ............15 PINS AND PIRAL IVES 3-4.4.1 Spins..............3-3.4.2 Spiral Dives ............EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 37: Introduction
Each pilot must make the final decision as to the correct procedure under the circumstances and is responsible for the consequences of that decision. NOTE In any emergency, maintaining control of the aircraft is always the highest priority. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 38: Airspeeds For Emergency Operations
1. Airspeed: 65 kts./75 m.p.h. If flaps are on, do not retract them. 2. Mixture full lean. 3. Fuel valve OFF. 4. Ignition switch OFF. 5. Master switch OFF. 6. Wing flaps as required. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 39: 3-3.1.3 Engine Failure During Flight
11. Extend full flaps on short final and bleed airspeed to touch down as slowly as possible. 12. Unlatch doors before touchdown. 13. Touch down slightly tail low. 14. Apply brakes heavily while holding full aft stick. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 40: 3-3.3 Fire
7. Open or close cabin air vents and/or crack open the doors, as necessary, to minimize smoke and fumes in the cockpit. 8. Execute a forced landing as soon as possible. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 41: 3-3.3.3 Electrical Fire On The Ground
3. Master switch OFF. 4. Reduce speed. 5. Open air vents and/or cabin doors to provide fresh air. 6. Extinguish fire, if possible. 7. Land as soon as possible. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 42: 3-3.4 Spins And Spiral Dives
3. Neutralize the rudder. 4. Pull out of the dive. 3-3.4.2 Spiral Dive Recovery 1. Reduce power and simultaneously… 2. Level the wings. 3. Pull out of the dive. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 43: Explanations Of Emergency Procedures
65 kts./75 m.p.h. We recommend using full flaps, if you have time to extend them. If the flaps are extended when the engine fails, do not retract them. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 44: 3-4.1.3 Engine Failure During Flight
If you encounter engine roughness or power loss in flight, check all engine gauges to verify that the pressures and temperatures fall EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 45: 3-4.2 Forced Landing Without Engine Power
If you are too high on approach, however, extend flaps or slip the airplane. We recommend always using flaps for the final approach, if possible, to minimize the touchdown airspeed. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 46 Sacrifice other parts of the airframe (wings, landing gear) to absorb the impact energy. As soon as the airplane comes to rest, evacuate it as quickly as possible to escape a possible post-crash fire. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 48: 3-4.3.2 In-Flight Engine Fire
Extinguish the fire, if possible. Land as soon as possible and remedy the problem before further flight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 49: 3-4.4 Spins And Spiral Dives
G forces will begin to build. If allowed to continue, the aircraft will either strike the ground at high speed or will suffer in-flight structural failure from excessive G loads. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 50 A spiral dive is a common result (usually fatal) of flying into instrument conditions without proper training or proper instrumentation. For this reason, pilots who are not rated and current in IFR flight must avoid flight in conditions of reduced visibility. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 51 TAXIING ..................15 TAKEOFF ................... 16 4-6.1 G ................16 ENERAL 4-6.2 N ............. 17 ORMAL AKEOFF 4-6.3 S ............18 HORT IELD AKEOFF 4-6.4 H ........19 ENSITY LTITUDE AKEOFF EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 52 ..............32 PPROACH 4-13.3 L ................ 34 ANDING 4-13.4 S ............ 35 HORT IELD ANDING 4-13.5 S ................36 LIPS 4-13.6 C ..............37 ROSSWINDS 4-14 ENGINE SHUT-DOWN ............. 38 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 53: Introduction
Limitations and Flight Test sections before attempting any ground or flight operations. Pilots must also be familiar with the performance data in “S 1: G .” ECTION ENERAL NFORMATION EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 54: Preflight Checklist
Prior to any flight, inspect the exterior and interior of the aircraft for anything that looks suspicious or out of line. Use the following preflight walk-around checklist as a guide when inspecting the aircraft. Remedy any problems or defects before flight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 55 4. Check propeller for nicks and cracks. Check spinner for security and integrity. 5. Check cowling fasteners for security. 6. Check engine cooling inlets for obstructions (bird nests, etc.). EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 56 6. Aux fuel sump: drain fuel into clear cup and check for water and debris. Drain until water or debris is gone. 7. Check security and integrity of wingtip fairing and nav/strobe lights. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 57 6. Grasp stabilizer by the right tip and shake gently to check for secure attachment and structural integrity. 7. Check stabilizer and elevator right-side tip fairings for security and integrity. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 58 18. Check baggage door for security. 19. Fuel system low-point drain: drain fuel into clear cup and check for water and debris. Drain until water or debris is gone. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 59 (Use a length of 1/4" I.D. tubing to blow into vents.) 3. Aux fuel sump: drain fuel into clear cup and check for water 4. Check security and integrity of delta wings. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 60: Pre-Start And Engine-Start Checklist
30 seconds of operation. If proper oil pressure does not develop, shut the engine down and determine the cause before proceeding. Let the engine warm up at about 1,000– 1,200 r.p.m. before takeoff. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 61: 4-3.2 Normal Start
CAUTION Starting an engine without proper preheat in cold weather can cause damage from lack of lubrication due to congealed oil in the system. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 62: 4-3.3.1 Lycoming Engine
Then: 1. Open the throttle fully. 2. Set mixture full lean. 3. Engage starter. When engine fires, advance the mixture control and move the throttle to desired setting. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 63: Run-Up And Pre-Takeoff Checklist ("Cigars")
• At high density altitude, lean mixture appropriately for best power during takeoff. ATTITUDE: • Trim set at neutral position (for takeoff). • Flaps checked for full travel and extended as appropriate for takeoff. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 64: Taxiing
Since visibility over the nose is excellent, taxiing the Sportsman is easier than in many other tailwheel-equipped airplanes. Steering is by cables connected between the rudder yoke and the tailwheel. Above EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 65: Takeoff
Follow the throttle with right rudder, as necessary, to overcome the torque effects of the engine and propeller and to keep the airplane tracking straight down the runway. Hold the stick fully aft EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 66: 4-6.2 Normal Takeoff
As the airplane accelerates after lift-off, ease the flaps up, making sure that they are completely retracted before reaching Vfe (90 kts./103m.p.h.). Let the airplane accelerate to at least 85 kts. (97 m.p.h.) which is the best rate-of-climb airspeed. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 67: 4-6.3 Short -Field Takeoff
Encountering such conditions when at the edge of the performance envelope can lead to an accident. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 68: 4-6.4 High Density -Altitude Takeoff
Therefore, a higher-than- normal climb speed might be required on hot days. Additionally, at its best-rate-of-climb airspeed, the attitude of the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 69: Stalls
Sportsman pilot be proficient at identifying and recovering from both power-off and power- on stalls. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 70 W A R N I N G Intentional spins are prohibited in the Sportsman. Be familiar with standard spin recovery procedures in the event of an inadvertent spin entry while practicing stalls. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 71: 4-8.2 Power -Off Stalls
There is no need in the Sportsman as in some aircraft to push the stick forward to aggressively lower the nose; this procedure EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 72: 4-8.3 Power -O N Stalls
Enter a power-on stall by establishing and holding a climb angle until the airspeed bleeds off to the stall speed. With any but the lowest EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 73 Use of rudder only to arrest wing drop during a stall is a good, standard practice to cultivate regardless of the aircraft being flown. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 74: 4-8.4 Accelerated Stalls
In the event of a secondary stall in the Sportsman, recover just as you would from a power-on stall: relax back pressure and pick up the dropped wing with top rudder. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 75: Cruise
The following figures are to be used as guides for determining the desired cruise power settings and speeds. Performance numbers are the actual data from Glasair Aviation’s prototype Sportsman. The 180 h.p. numbers are for aircraft equipped with Lycoming O-360 engines, and Hartzell constant-speed propellers.
Page 76 If an EGT gauge is used, lean a Lycoming engine to 50 F rich of peak EGT (hottest cylinder) to obtain the optimum fuel consumption rate; or follow the recommendations in your engine operator’s manual. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 77: Fuel Management
Turning on the pumps with more than 10 gals. in the mains risks pumping fuel overboard through the vents. It takes the pumps approximately 20 minutes to drain the auxiliary tanks. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 78: Descent
Maximum structural cruising speed (Vno) of the Sportsman is 140 kts. or 161 m.p.h. IAS. Gradually push the mixture control rich during long descents. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 79: Approach And Landing
We recommend completing the pre-landing checklist before entering the pattern so that the pilot’s attention can be directed outside the airplane to clear for other traffic while in the pattern. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 83: 4-13.3 Landing
Sportsman, but pilots accustomed to skimming the runway end lights and touching down a third of the way down the runway must be prepared for a somewhat different experience. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 84: 4-13.4 Short -Field Landing
“short-field” performance capabilities of most aircraft and certainly exceeds the requirements of any established airport. However, the rugged construction, generous payload and exceptional slow-flight capabilities of the Sportsman invite its use under more EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 85: 4-13.5 Slips
With its large, effective rudder and ailerons, however, the Sportsman slips marvelously. Easily controlled slipping descents exceeding 1,000 ft./min. can be achieved at typical 65 kt. (75 m.p.h.) EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 86: 4-13.6 Crosswinds
Each pilot is urged to practice crosswind landing tasks of progressive difficulty and to honestly assess his/her own capability along with that of the aircraft. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 87: Engine Shut-Down
3. Turn radios off. 4. Turn all accessory switches off. 5. Set mixture to idle cut-off (full lean) and wait for the engine to stop. 6. Turn off ignition and master switches. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 89 5-3 FLIGHT CG CALCULATIONS ........... 10 5-3.1 F CG L ..........11 ORWARD IMIT HECK 5-3.2 R CG L ..........15 EARWARD IMIT HECK 5-3.3 L ............20 OADING ROBLEM EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 90: General Data
CG Limits — The extreme center of gravity locations within which the airplane must be operated at a given weight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 91: Weight And Balance
— The weight of chocks, blocks, stands, etc., used on the scales when weighing an airplane. Useful Load — Difference between maximum gross weight and empty weight. Waterline — A horizontal reference plane running longitudinally through the fuselage. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 92: 5-1.2 Weight And Balance Data
Cowling Mounting Flange Joggle ........Station 58.0 Firewall...................Station 60.5 Wing Leading Edge...............Station 89.4 Pilot and Passenger...............Station 101.0 Fuel ..................Station 108.0 Baggage, Forward Zone............Station 130.0 Rear Passengers ..............Station 144.0 Baggage, Aft Zone..............Station 165.0 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 93: Empty Weight Cg Calculation
See Figure 5-1. These distances represent the stations of the landing gear. Enter the results of your measurements here: (X)____________ (Y)____________ AILWHEEL EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 95: 5-2.2 Weigh The Aircraft
CALE READING ARE WEIGHT EIGHT _________ – _________ =_________ EFT MAIN GEAR _________ – _________ =_________ IGHT MAIN GEAR _________ – _________ =_________ AILWHEEL _________ – _________ =_________ OTAL AIRCRAFT EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 96: 5-2.3 Calculate The Station Of The Empty Weight Cg
(99 lb. X 289.0 in.) + (632 lb. + 632 lb.)(80.0in.) 1,363 lb. = 129,993 in.-lb. = Station 95.3 1,363 lb. Enter the results of your empty weight CG calculations here: CG S __________ MPTY EIGHT TATION EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 97: Flight Cg Calculations
The following examples are based on the empty weight and empty- weight CG of the Sportsman taildragger prototype; your numbers will vary! NOTE For all weight and balance calculations, note that gasoline weighs 6 pounds per gallon. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 98: 5-3.1 Forward Cg Limit Check
CG limit checks. However, the converse is not true; if you weigh more than 170 lb., you must use the 170 lb. standard weight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 99 In this example, both the total gross weight and the station of the CG are within limits. An airplane with a heavier engine or a lighter pilot, however, could possibly have a CG forward of the allowable range. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 100 Using the sample forward CG limit check as a guide, enter the data for your Sportsman in Table 5-2 and perform your own forward CG limit check. Enter your result here: — S __________ ORWARD LIMIT CHECK TATION EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 101 If your Sportsman is so equipped, be particularly aware of your weight and balance condition when you fly with little or no baggage and low fuel, especially if you are flying solo. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 102: 5-3.2 Rearward Cg Limit Check
Passenger 101.0 Fuel (30.6 gal.) 300.0 108.0 32,400.0 Forward baggage 130.0 Passenger 144.0 Aft baggage 300.0 165.0 49,500.0 2,133.0 — 229,003 OTAL Table 5-3: Sample Rearward CG Limit Check EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 103 Sportsman in Table 5-4 and perform your own rearward limit check. Enter the result here: — S _________ EARWARD LIMIT CHECK TATION Baggage compartment restrictions — Forward zone __________ Passenger zone __________ Aft zone __________ EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 104 (if less than 300 lb.) and how it must be distributed to bring the CG within limits. Then placard the baggage compartment with the results. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 105 CG and re-perform the forward and rearward limit checks. The loaded aircraft weight and the station of the CG must fall within the shaded area of the graph shown in Figure 5-2. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 107: 5-3.3 Loading Problem
Figure 5-1. The dividing line between the forward and aft baggage zones is located 25" forward of the baggage compartment bulkhead or just forward of the baggage door. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 108 /1000 /1000 Empty Sportsman 1,363 130.0 Pilot 17.2 Passenger 13.6 Fuel (6 lb./gal.) 32.4 Fwd baggage 13.0 Rear Passenger 19.4 Aft baggage 2,243 232.2 OTAL Table 5-5: Loading Problem EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 111 FUEL SYSTEM ................4 OIL SYSTEM ................5 LANDING GEAR ................5 BRAKES..................6 COCKPIT ..................6 CONTROL SYSTEM..............7 WING-FOLD SYSTEM .............. 12 6-10 HEATING AND VENTILATION SYSTEMS....... 13 6-11 ELECTRICAL SYSTEM.............. 13 6-12 INSTRUMENTATION..............14 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 113: Powerplant
YSTEMS ESCRIPTIONS 6-1 POWERPLANT Powerplants supported by Glasair Aviation for the Sportsman are the the Lycoming O-360 (180 h.p.). See “S 2: L ” for ECTION IMITATIONS further details. Glasair Aviation supplies engine mounts, exhaust systems, cowlings and other firewall-forward options for all of the supported engines.
Page 114: Fuel System
A carbureted engine can be primed with an optional hand-actuated essex pump located on the instrument panel. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 115: Oil System
6, 8.00 × 6 and 26 x 10.5 x 6 wheels and brakes are available as options. The main gear toe-out is 1/32" measured at the end of the axle, or about 1/3°. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 116: Brakes
A rear passenger door is provided on the left side of the aircraft just behind the pilot’s door. Larger baggage can also be loaded through the large cabin doors by folding the seat backs forward. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 117: Control System
The Sportsman elevator trim system uses a large trim tab in the elevator. Standard elevator trim is manually operated by a cockpit- mounted trim wheel; electric trim is optional. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 122: Wing-Fold System
See Section 7-4 for a description of procedures to fold the wings and remove the stabilizer. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 123: Heating And Ventilation Systems
Optional navigation/strobe light units can be mounted to the wingtip fairings. The standard lower engine cowling has a molded recess for a landing light lens, so an optional landing light can be easily installed. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 124: Instrumentation
The ELT must have a remote actuation switch on the panel. Instruments such as a directional gyro or artificial horizon, if used, are typically operated by vacuum pressure. We recommend using an EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 125 If an electrical system is used, an ammeter should also be used in conjunction. All additional instruments, avionics, etc. are subject to the builder’s preferences. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 127 7-6.8 P ....... 13 REPARATION FOR ETURN TO ERVICE 7-7 50 HOUR POWERPLANT INSPECTION ........14 7-7.1 G ........14 ENERAL NGINE OMPARTMENT 7-7.2 I ............... 14 GNITION YSTEM EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 128 ............39 IXED ITCH ROPELLER 7-9.7 I ............40 NDUCTION ILTER 7-9.8 A ..............40 IRFRAME 7-9.9 W ..........42 INDSHIELD AND INDOWS 7-9.10 E .............. 43 NGINE LEANING EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 129: General
For the second 25 hours, we recommend performing a major inspection after each 5 hours of flight or if anything appears out of the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 130: Ground Handling
1. Make sure that the magnetos are off, the throttle is closed and the mixture is in the idle cut-off position when pushing or pulling on the propeller blades. 2. Do not exert force on the control surfaces. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 131: Tie Down
5. Use a cabin cover to keep moisture and sunlight from entering the cockpit. 6. Make sure that all drain holes in the tail section are clear to prevent the collection of water in any part of the airframe. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 132: Folding The Wings And Removing The Stabilizer
3. Remove the top-deck hatches to provide space for the inboard ends of the flaps. 4. Install the support struts between the eye bolts at the forward spar roots and the bases of the wing struts (optional, but recommended). EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 133 9. Repeat Steps 6–8 for the other wing. If the airplane is to be trailered, instead of just stored at the airport, the support struts mentioned in Step 4 are essential to prevent structural EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 134 W A R N I N G Besides verifying the security of the spar pins and safety clips after extending the wings, make sure to remove the fuel tank vent line plugs before flight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 135: 7-4.2 Removing The Horizontal Stabilizer
Again, it’s best to have two people involved, especially to get the stabilizer in position with the spar pins properly seated in the forward attach bracket bushings. 7-5 JACKING THE AIRPLANE EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 136 1". To work on the tailwheel, simply support the tail of the airplane with a sturdy, padded sawhorse under the aft fuselage. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 137: Out-Of-Service Care
(Section 7-3). To prevent oxidation of the finish, we recommend the use of light-colored slip covers over the composite fuselage during extended periods of outdoor tie-down. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 138: 7-6.3 Engine Preparation For Storage
Make sure both cabin doors are securely closed. If the aircraft is stored outdoors, we recommend that covers be installed over the cabin area to keep out moisture and sunlight. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 139: 7-6.7 During Flyable Storage
Remove all covers, gust locks, etc., and give the airplane a thorough inspection. Particularly check control openings and the cowl inlets and outlets for bird nests. Preflight the airplane following procedures in Section 4-2. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 140: Hour Powerplant Inspection
Check the ignition harness for security of the mounting clamps and make sure all connections are tight and properly torqued at the spark plug and magneto terminals. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 141: Revision : Date : Page
For Lycoming engines, see Service Instruction 1319 B for further details. For Continental engines, refer to your engine Maintenance Manual . Also, see Section 7-9.1 of this manual. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 142: 7-7.5 Exhaust System
Excessive heat is indicative of internal damage to the cylinder; if found, its cause must be determined and corrected before the aircraft resumes operation. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 143: Annual Condition Inspection
3. Left magneto drop. 4. Right magneto drop. 5. Propeller control and governor action. 6. Suction gauge. 7. Static r.p.m. 8. Idle r.p.m. 9. Carburetor heat. 10. Magneto ground. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 144 D. Engine Controls: check the following controls for security, full range of travel, chafing, safety. Lubricate if necessary. 1. Throttle. 2. Mixture. 3. Propeller pitch control. 4. Carburetor heat. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 145 11. Check all breather and overboard lines for security and obstructions. 12. Inspect the fuel filter element and replace if necessary. Safety wire the fuel filter bowl. 13. Clean the carburetor or injector screens and check the fuel EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 146 22. Check the cowling for chafing, cracks or heat damage. 23. Check the engine for any loose hardware and tools that may have been left in the engine compartment during maintenance. G. Ground Run-up Check: 1. Oil pressure. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 147: 7-8.2 Cabin , Fuselage And Empennage
A. Inspect the control system cables, pulleys, pushrods and rod-end bearings for corrosion, safety, security and chafing. Lubricate all pivot points, bearing surfaces and pulleys as necessary. Check the following systems: 1. Aileron system. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 148 J. Replace the vacuum air filter. K. Check all instrument wiring and plumbing for security and chafing. Replace any nylon tie wraps or spiral wrap that is brittle or discolored. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 149 X. Check and lubricate the elevator, rudder and trim tab hinges. Verify that the hinges are properly safetied. Y. Check all aft-fuselage bulkheads for integrity. Check security of the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 150 Reattach the elevator pushrod and the trim system. CC. Check the elevator and the rudder for proper travel: 1. Elevator: 23° up and 20° down (±1°). 2. Rudder: 25° left and right (±1°). EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 151: 7-8.3 Landing Gear
If the brakes feel soft or spongy, bleed them as described in Section 7-9.4.2. I. Check the tailwheel spring attach bracket for security. J. Check the tailwheel steering linkage for security and integrity. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 152: 7-8.4 Wings
I. Inspect the aileron counterweights for integrity, security and chafing. (Be sure any wiring in the wing tips cannot jam the aileron EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 153 N. Check inside the wings for loose hardware and tools. O. Reinstall the wingtip fairings and check the operation of the navigation and anti-collision lights. P. Reinstall the inspection covers. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 154: 7-8.5 Paperwork
H. Log book: make a log book entry, noting any discrepancies and other pertinent information. Sign off the annual condition inspection as required by the operating limitations imposed with your Experimental Airworthiness Certificate. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 155: Servicing
50 hours. See Lycoming Service Instruction 1319 B. If the engine does not have an air filter, change the oil every 50 hours. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 156: 7-9.2 Battery
If the battery is filled when in a low state of charge, it will overflow when charged. CAUTION Excessive overcharging can cause heating and boiling. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 157: 7-9.3 Tires
There is no need to adjust the brakes since the brake pistons move to compensate for brake pad wear. Inspect the brake pads at every preflight, however, and replace them if worn excessively. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 158 40) on the caliper anchor pins. Petroleum-base lubricants are sticky and attract dust and dirt, which can impede the floating action of the calipers. Use a dry lubricant, such as silicon or graphite. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 159: 7-9.4.1 Brake Lining Replacement
As the brake lining wears, the piston protrudes farther from the caliper housing. To accommodate the thickness of the new linings EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 160 (the end that is formed during brake lining installation) fits into the counterbored side of the pressure plate or back plate. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 161 Proceed slowly and rotate the assembly while driving the rivet so that the tail is evenly formed. Check the rivet frequently as you go to make sure it isn’t splitting. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 162 (there is no movement when wiggled by hand) but before the rivets or the lining begin to crack from over-driving. The brake plates are now ready for remounting to the caliper housing. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 163 6: C HECK THE PERATION OF THE RAKES Check the brakes for firm pedal pressure and bleed the system if either brake feels spongy. See Section 7-9.4.2 for bleeding instructions. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 164: 7-9.4.2 Bleeding The Brakes
Repeat for both brake calipers until the brakes feel solid. Finally, drain the reservoir until it is about 7/8 full. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 165: 7-9.5 Constant -Speed Propeller
Remove the spinner and inspect the propeller blades for nicks and gouges. Repair nicks and gouges using the procedures described in the propeller owner’s manual. Always consider propeller balance when EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 166: 7-9.6 Fixed -Pitch Propeller
Clean bug and grass stains off the propeller when you wash the rest of the airframe. Never use a harsh, corrosive cleaner on the propeller blades. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 167: 7-9.7 Induction Air Filter
Unpainted aluminum surfaces can be polished, if desired, using any standard aircraft aluminum polish. Storing your Sportsman in a hangar rather EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 168 If no damage has occurred to the structure, the glass will be smooth and translucent. If damage has occurred, contact Glasair Aviation for repair consultation. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 169: 7-9.9 Windshield And Windows
(Mirrorglaze or similar). The wax will fill in minor scratches and help prevent further scratching. Apply a thin, even coat of wax and bring it to a high polish by rubbing lightly with a clean, dry, EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 170: 7-9.10 Engine Cleaning
Particular care should be given to electrical equipment before cleaning. Do not allow cleaning fluids to enter the magnetos, the starter, the alternator or the like. All other openings should be covered before cleaning. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 171 8-4 FINAL INSPECTION ..............11 8-5 FIRST FLIGHT................13 8-6 FURTHER FLIGHT TESTING............18 8-6.1 G ................18 ENERAL 8-6.2 E ............19 NVELOPE XPANSION 8-7 FINAL CERTIFICATION............... 21 EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 173: Introduction
Over half of all homebuilt accidents occur within the first 40 hours of operation. To help reduce the accident rate during the flight test period, Glasair Aviation is proud to have participated in the Amateur Built Aircraft development of FAA Advisory Circular 90-89, Flight Testing Handbook .
Page 174: Ground Tests
Check the oil pressure, the alternator output, left and right magneto drops and the r.p.m. drop with carburetor heat. Switch the magnetos off momentarily to check the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 175 A good engine break-in requires that the oil film that lubricates the piston rings and cylinder wall break down slightly and allow some wear to occur. This wear, or “seating,” of the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 176 Operate new or overhauled engines on straight mineral oil for a minimum of 50 hours or until oil consumption has stabilized. After this period, change to an approved additive oil if so desired. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 177: Taxi Testing
Hold the stick back when taxiing to enhance tailwheel steering. Also practice locking the brake on one side and adding power to pivot the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 178: 8-3.2 High -Speed Taxi
High-speed taxi testing should be done on a long airport runway (at least 4,000–5,000 ft.). Practice steering by tracking the runway centerline. Almost immediately upon application of full power, the tail EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 179 Erratic movement on the ground is usually caused by pilot- induced oscillations. Do not make large, jerky control inputs. The airplane responds better and you are less likely to get into trouble with smooth, steady, firm control pressures. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 180 Limited Duration Experimental Airworthiness Certificate. We recommend breaking the hour into short segments to avoid overheating the engine or the brakes. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 181: Final Inspection
ELT installation, pilot and passenger restraints, properly marked N- number and the appropriate permanently-installed placards. (See Owner’s Manual Section 2-14.1 of this for a description of the placards required for certification of an experimental amateur built aircraft.) EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 182 This will verify that the construction has been accomplished in accordance with acceptable workmanship methods, techniques and practices. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 183: First Flight
Recruit a small ground crew, consisting of a friend or two with a hand-held radio, to provide immediate assistance in the event of an emergency, but don’t make the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 185 (90 m.p.h.) climb. Keep monitoring the operating temperatures. Reduce power and level off if temperatures during climb-out become excessive. If temperatures continue to rise, return to the airfield and troubleshoot the problem. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 186 Add power, retract the flaps, and climb back to 5,000 ft. AGL. Now, try a few gentle stalls. Make sure the area is clear of other traffic. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 187 After the first flight, remove the upper and lower engine cowling and all inspection cover plates. Give the entire aircraft a general inspection. Check the engine compartment for leaks, wiring problems, hot spots EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 188: Further Flight Testing
Design and plan an organized flight test program to verify compliance with part 91.42(b). EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 189: 8-6.2 Envelope Expansion
Also, ballast the airplane to shift the location of the CG fore and aft to gradually explore the handling of the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 191: Final Certification
The aircraft builder can be certified as a repairman to enable him to perform the condition inspection. Specific information regarding repairman certification can be found in AC No. Certification of Repairmen (Experimental Aircraft Builders) 65-23, EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 193 9-4 INFORMATION ON SPECIFIC TOPICS........10 9-4.1 F ..............10 LIGHT LANNING 9-4.2 M ..........10 AINTENANCE NSPECTION 9-4.3 F ............11 LIGHT PERATIONS 9-4.4 M ..........19 EDICAL ACTS FOR ILOTS EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 195: Introduction
The following material in this Safety Section covers several subjects in limited detail. Here are some General Do’s and Don’ts: EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 196 Be sure all loose articles and baggage are secured. Check freedom of all controls during preflight inspection and before takeoff. Maintain the prescribed airspeeds in takeoff, climb, descent and landing. Avoid large airplane wake turbulence. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 197 Don’t fly into weather conditions that are beyond your ratings or current proficiency. Don’t attempt any takeoff or landing without using the checklist. Don’t fly when physically or mentally exhausted or below par. Don’t trust to luck. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 198: General Sources Of Information
Maintenance, preventive maintenance, alterations, inspection and maintenance records These are only some of the topics covered. The owner and the pilot are responsible for compliance with all requirements of FAR Part 91. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 199: 9-3.2 Airworthiness Directives
Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402. The subjects discussed in the AIM are: Controlled air space Services available to pilots Radio phraseology and technique Airport operations Clearances and separations EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 200 The FAA issues advisory circulars to inform the aviation public of non- regulatory material of interest. Advisory Circulars contain information with which the prudent pilot should be familiar. A complete list of EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 201 FAA General Aviation News is sold on subscription by the Superintendent of Documents at the above address. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 202: Information On Specific Topics
In addition to maintenance inspections and preflight information required by FAR Part 91, a complete preflight inspection is imperative. It is the responsibility of the owner and the operator to assure that the EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 203: 9-4.3 Flight Operations
LIGHT PERATIONS General The pilot must be thoroughly familiar with all information published by Glasair Aviation concerning the airplane and must operate the aircraft Owner’s Manual in compliance with all limitations imposed by the Turbulent Weather A complete and current weather briefing is a requirement for a safe trip.
Page 204 Maintain straight and level attitude in either up or down drafts. Use trim sparingly to avoid being grossly out of trim as the vertical air columns change velocity and direction. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 205 Part 23 Standards for lightning protection. For this reason, the Sportsman is prohibited from flight in conditions that would expose the airplane to the possibility of a lightning strike. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 206 “roll clouds,” but only if sufficient moisture is present. A mountain wave downdraft may exceed the climb capability of your airplane. Avoid mountain wave downdrafts. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 207 IFR, and must be avoided by inexperienced or non-IFR rated pilots. Vertigo—Disorientation Disorientation can occur in a variety of ways. During flight, inner ear balancing mechanisms are subjected to varied forces not normally EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 208 This can happen when the pilot’s physical condition will not permit him to concentrate on his instruments, when the pilot is not proficient in flying instrument conditions in the airplane he is flying or EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 209 (fouling). The second of these is the more serious consideration; the engine may not respond to the throttle when it is desired to discontinue the descent. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 210 Plan to fly slightly above and to the windward side of the other airplane’s flight path. Because of the wide variety of conditions that can be encountered, there is no set rule to follow to EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 211: 9-4.4 Medical Facts For Pilots
The pilot is just as essential to a successful flight as the control surfaces. To ignore the pilot in preflight planning would be as senseless as failing to inspect the integrity of the control surfaces EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 212 It is impossible to predict when or where hypoxia will occur during a given flight, or how it will manifest itself. Some of the common EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 213 Under conditions of emotional stress, fright or pain, breathing rate may increase, causing increased lung ventilation. Since there is no corresponding increase in the carbon dioxide output of the body cells, carbon dioxide is “washed out” of the blood. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 214 The body metabolizes ingested alcohol at a rate of about one-third of an ounce per hour. Even after the body completely destroys a moderate amount of alcohol, a pilot can still be severely EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 215 If sufficient time has not elapsed for your system to rid itself of this excess gas before takeoff, you may experience the bends at altitudes even under 10,000 ft. where most light planes fly. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...
Page 216 8,000 to 10,000 ft. Smoking several cigarettes can result in a carbon monoxide saturation sufficient to affect visual sensitivity equal to an increase of 8,000 ft. of altitude. EVISION 12/29/04 Copyright2004 Glasair Aviation, LLC Arlington, Washington All rights reserved...

Glasair Sportsman GS-2 Owner's Manual

Table of Contents

Table of Contents

Limitations

Table of Contents

Introduction

Airspeeds for Emergency Operations

Emergency Check Lists

Explanations of Emergency Procedures

Table of Contents

Table of Contents

General Data

Empty Weight Cg Calculation

Flight Cg Calculations

Table of Contents

Table of Contents

General

Ground Handling

Tie down

Folding the Wings and Removing the Stabilizer

Jacking the Airplane

Out-Of-Service Care

Hour Powerplant Inspection

Annual Condition Inspection

Servicing

Table of Contents

Table of Contents

Introduction

General

General Sources of Information

Information on Specific Topics

Quick Links

Chapters

Need help?

Questions and answers

Related Manuals for Glasair Sportsman GS-2

Summary of Contents for Glasair Sportsman GS-2