DEPARTMENT OF TRANSPORTATION L 33 Solo N120BB Type Certificate G71eu

User Manual: L-33 Solo N120BB Type Certificate G71eu

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DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
G71EU
Revision 2
LET
L33 SOLO
January 11, 2006
TYPE CERTIFICATE DATA SHEET No. G71EU
This data sheet which is a part of Type Certificate No. G71EU prescribes conditions and limitations under
which the product for which the type certificate was issued meets the airworthiness requirements of the
Federal Aviation Regulations.
Type Certificate Holder. Aircraft Industries a.s.
686 04 Kunovice 1177
Czech Republic
Type Certificate Holder Record: LETECKÉ ZÁVODY a.s. transferred TC G71EU to Aircraft Industries a.s. on September
26, 2005
LET Aeronautical Works transferred TC G71EU to LETECKÉ ZÁVODY a.s.
on October 15, 2002
I. Model L33 SOLO (Utility Category), approved November 2, 1993.
Airspeed Limits (C.A.S.). Max. speed to 15,000' MSL (Vne) 130 knots (150 m.p.h.)
15,000' to 20,000' MSL 127 knots (146 m.p.h.)
20,000' to 25,000' MSL 125 knots (144 m.p.h.)
25,000' to 30,000' MSL 123 knots (142 m.p.h.)
30,000' to 35,000' MSL 121 knots (139 m.p.h.)
Maneuvering speed (VA) 82 knots (94 m.p.h.)
Airplane Tow (VT) 82 knots (94 m.p.h.)
Auto-winch Tow (VW) 68 knots (78 m.p.h.)
C.G. Range. (+68.89 inches) to (+74.73 inches) at all weights aft of datum
(21 to 39% MAC)
Empty Weight C.G. Range. 84.63 ± 0.32 inches (69.5±1% MAC) aft of datum.
Datum. Leveling point No. 1 - red marked rivet on bulkhead No. 1
Leveling Means. Slope of rear top edge of fuselage 1000 to 53
(Points marked on side of fuselage)
Maximum Take-Off Weight. 750 lbs
Empty Weight. 463 lbs ± 3%
No. of Seats. 1 (at 39.2 inches)
Equipment and Baggage Weight. Baggage 44 lb (70.68 inches)
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Rev. No. 2 - -
G71EU Page 2 of 3
Control Surface Movements. Elevator Up 25º + 1º
Down 15º + 1º
Rudder Right 25º + 2º
Left 25º + 2º
Aileron Up 26º + 1.5º
Down 15º ± 1º
Weak Links for Towing. Auto-Winch launching 1460 lb
Airplane tow 1460 lb
Serial Numbers Eligible. Each individual aircraft manufactured under this type certificate must
be accompanied by a Certificate of Airworthiness for Export (or
certifying statement endorsed by the Exporting Civil Airworthiness
Authority (ECAA) as noted below under "Import Requirements")
when an application for a U.S. airworthiness is made.
L33 SOLO: 930101, 930102, 930105, 930106, 930201, and
subsequent
Import Requirements. A U.S. Standard Airworthiness Certificate may be issued on the basis
of a Certificate of Airworthiness for Export endorsed by a
representative of the original manufacturer's airworthiness authority
(Civil Aviation Inspectorate, Czech Republic) containing the following
statement: "The aircraft covered by this certificate has been examined,
tested, and found to conform to the type design approved under Type
Certificate No. G71EU and is in a condition for safe operation."
Serial Nos. 930101, 930102 must be modified in accordance with LET
Mandatory Bulletin No. L33/001, for conformity with the type design,
and verified by the modifier to be in a condition for safe operation.
Serial Nos. 930105, 930106 must be modified in accordance with LET
Mandatory Bulletin No. L33/002, for conformity with the type design,
and verified by the modifier to be in a condition for safe operation.
Certification Basis. JAR 22 Ch. 4 issued April 1, 1980 (Amend. 22/91/1, effective
December 9, 1991), amended as follows:
- JAR 22.177(b) including AC 21.17-2, para. 6.c.(6)(i)(A),(B),(C),and
(D),
- JAR 22.207(b) including AC 21.17-2, para. 6.c.(6)(ii),
- JAR 22.1545 including AC 21.17-2, para. 6.c.(6)(iii).
Validation Basis. Type Certificate G71EU was issued pursuant to FAR 21.29 in
validation of a Czech Republic (CAI) certification of compliance with
the aforementioned certification basis, and in accordance with the
standard airworthiness certificate provisions of FAR 21.183(c).
Equipment. The basic required equipment as prescribed in the applicable
airworthiness regulations (see Certification Basis) must be installed in
the aircraft for airworthiness certification. In addition, the following
items of equipment are required:
Page 3 of 3 G71EU
1. Model L33 SOLO - CAI approved (for the FAA) Sailplane
Flight Manual, Ref. LET Document No. DO-L33.1012.3 dated
October 25, 1993, or later approved revision.
2. Standard Equipment:
- Airspeed Indicator (knots)
- Altimeter (Feet)
- Lap and shoulder straps
- Magnetic direction indicator
- Variometer (vertical speed indicator) Feet/Minute or Knots
Additional equipment required for Cloud flying:
- Turn and bank indicator
NOTES.
NOTE 1. A current weight and balance report including list of equipment in
certificated empty weight, and loading instructions, must be provided
with each aircraft at the time of original airworthiness certification,
and at all times thereafter.
NOTE 2. Placards (Refer to Manufacturer's Specifications, Maintenance Manual
Doc. No. DO-L33.1031.3) for a complete listing): All required
placards as listed in the approved Airplane Flight Manual must be
installed in the appropriate locations.
(1) The following placard must be displayed in clear view of the pilot:
"THE MARKINGS AND PLACARDS INSTALLED IN THIS
SAILPLANE CONTAIN OPERATING LIMITATIONS WHICH
MUST BE COMPLIED WITH THEN OPERATING IN UTILITY
CATEGORY. OTHER LIMITATIONS ARE CONTAINED IN
SAILPLANE FLIGHT MANUAL."
(2) Refer to the Airplane Flight Manual, Section 2, Limitations for a
listing of other required placards.
NOTE 3. Instructions for Continued Airworthiness and Service Life Limits of
components are contained in the LET L33 SOLO Maintenance
Manual Doc. No. DO-L33.1031.3. Revisions to Airworthiness
Limitations must be FAA approved.
Manufacturer's service bulletins (and other manual material) which
contain a statement that the document is approved by the exporting
airworthiness authority (CAI) may be interpreted as FAA approved.
These approvals pertain to the type design only.
Service bulletins classified as Mandatory by the Czech Republic Civil
Aviation Authority are identified to that effect and are subject to an
Airworthiness Directive issued by the FAA.
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