Worksheetswood and fibric exam
Total questions: 78
Worksheet time: 39mins
The main longitudinal members of a wooden wing are called:
Ribs
Spars
Booms
Sitka spruce spars are commonly:
Only solid
Solid or laminated
Only laminated
Why are laminated spars used?
Weight increase
Easier to source defect-free pieces
Better paint adhesion
Compression members between spars are made of:
Steel or alloy tubes
Fabric ribs
Plastic spacers
Drag wires run from:
Front spar inboard to rear spar outboard
Rear spar inboard to front spar outboard
Tip rib to root rib
Anti-drag wires run from:
Rear spar inboard to front spar outboard
Wing tip to fuselage
Rib to rib
Box spars increase:
Paint coverage
Bending and torsion strength
Weight imbalance
Plywood webs in box spars:
Block airflow
Act as shear panels
Reduce glue use
Ribs form the:
Wing aerodynamic shape
Landing gear support
Instrument panel
Most critical wooden member in flight:
Stringer
Spar
Tape strip
Before detailed inspection, aircraft should be placed in:
Wet hangar
Dry, ventilated hangar
Open sun
Musty smell indicates:
Fresh glue
Fungal/damp condition
UV damage
Moisture accumulates at:
Top surfaces
Lowest enclosed areas
Near wing tips
Glue line inspection requires:
Leaving paint
Scraping to bare wood
Burning the surface
Feeler gauges used must be:
Thick
Thinnest possible
Bent pieces
Glue line must be inspected only when wood is:
Wet
Dry and unclamped
Frozen
Elongated bolt holes are repaired by:
Larger bolts only
Installing steel bushes
Adding dope
Compression failure is detected by:
Torch along grain
Hammer tapping
Smelling glue
Drain holes blocked =
No problem
Moisture retention and decay
Better pressure
Acceptable timber moisture content:
10% ±1
15% ±2
22% ±2
Oven dry testing temperature:
80–90°C
100–105°C
140°C
Discard timber end before moisture testing:
2 in
6 in
12 in
Limit of grain inclination (Grade A spruce):
1 in 10
1 in 15
1 in 5
Dote disease appears at:
Mid-span
Tree base
Tip only
Ring shake is caused by:
UV
Frost after rain
High glue heat
Pin-knot clusters should be:
Accepted
Rejected
Filled with resin
Rift-sawing is to improve:
Grain stability
Bolt clearance
Fabric tension
Crumbling wood spots indicate:
Dry rot
Excess paint
Excess glue
Synthetic adhesive system is:
One-part
Two-part (resin & hardener)
Powder only
Powder resin is mixed with:
Water
Fuel
Oil
Maturation time refers to:
Cure after gluing
Wait before applying after mixing
Storage life
Adhesive storage must be below:
10°C
21°C
40°C
Bad resin appears:
Gel-like or sticky
Transparent
Dry powder
Glue surfaces must be:
Painted
Lightly sanded and dry-fit
Wetted
Butt joint test acceptable failure:
25% fibers
50% fibers
75% fibers
Wet test immersion period:
2–3 hrs
24 hrs
1 week
Pre-coating is needed when:
Both woods are dense
Soft meets dense
Dense meets dense
Glue applied to:
One surface
Both surfaces
None
Warp runs:
Crosswise
Lengthwise
Diagonal only
Natural fabrics degrade due to:
Fuel
UV & mildew
Static only
Polyester and glass-fibre are:
Natural
Artificial
Not used
Fabric storage:
20°C dry, dark
Cold and wet
Sunlight
Fabric covering area must be:
Painted
Clean and taped
Left rough
Bias covering angle:
0°
45°
90°
Balloon seam stitch count:
2 per cm
4 per cm
8 per cm
Lap seam usage:
Always
Only if specified
Never
Overhand stitch count:
3 per cm
1 per cm
6 per cm
Stringing cord:
Linen single strand
Wire
Plastic
Standard rib pitch:
75 mm
37 mm
150 mm
Prop-blast pitch:
75 mm
37 mm
100 mm
Serrated tape width:
25 mm
37 mm
10 mm
Bee wax is used on thread to:
Stiffen
Ease sewing
Color
Fabric on metal surfaces needs:
Direct bond
Etch primer then dope
Grease coat
Drain eyelets placed:
Anywhere
As per spec drawings
Top only
Marine fabric eyelets must be:
Standard
Shrouded type
Removed
Martin clips require:
Rivets
Screw + washer + tape underneath
Glue only
Two dope types:
PU and epoxy
Nitrate & butyrate
PVC
First dope on natural fabric:
Butyrate
Nitrate
Aluminium
Fungicide needed for:
Polyester
Natural fabric
Glass-fibre
Aluminium dope purpose:
Gloss
UV protection
Weight reduction
Retarder thinners:
Speed drying
Slow drying to prevent blush
Increase solids
Spray room conditions:
21–26°C / 45–50% RH
10°C / 90% RH
40°C / 10% RH
Portable tester works at:
45°
90°
Any angle
Portable tester lowest reading is:
Ignored
Considered
Averaged
Patch after tester puncture:
10 mm
50–75 mm
No patch needed
Polyester tensioning done by:
Dope
Heat
Water
First coat for polyester:
Butyrate
Nitrate thinned 2–3:1
Aluminium
Fungicide for polyester first coat:
Required
Not needed
Optional
Glass-fibre priming uses:
Nitrate
Butyrate only
Epoxy
Glass-fibre weave fill needs:
1 coat
Up to 5 coats
No coats
Straight tear on fabric repaired by:
Glue
Baseball stitch + tape + patch
Rivets
Lock knot frequency in repair stitching:
Every 150 mm
Every 600 mm
No knots needed
Woods frame repairs allowed up to:
50 mm²
50 mm square
Only 10 mm
Darning allowed only if tear is:
100 mm
≤50 mm wide
200 mm
Before stitching repairs, dope around tear must be:
Left as is
Removed with thinners
Painted over
What is the main material used for aircraft wooden spars?
Oak
Mahogany
Sitka spruce
Why are laminated spars often used instead of solid spars?
They are equally strong and cheaper
They are stronger and cheaper
They are lighter but equally strong
Aluminium dope protects fabric from:
Heat
UV radiation
Corrosion
