Czech Aircraft CRUISER AIRCRAFT PS-28 Cruiser 2021 User manual

CR-MM-1-0-00
Date of issue: 2021-01-15 Revision No.: 25
i
This document is prepared in accordance with the AP DOA Approval No. AP.507
PS-28 Cruiser
PS-28N Cruiser
MAINTENANCE MANUAL
Copy No.:
This document contains EASA approved Chapter 2A – Airworthiness Limitation Section.

CR-MM-1-0-00
Revision No.: 25 Date of issue: 2021-01-15
ii
INTENTIONALLY LEFT BLANK

CR-MM-1-0-00
Date of issue: 2021-01-15 Revision No.: 25
iii
This document is prepared in accordance with the AP DOA Approval No. AP.507
PS-28 Cruiser
PS-28N Cruiser
MAINTENANCE MANUAL
PS-28 Cruiser and PS-28N Cruiser aircrafts
are designed and manufactured by
Czech Aircraft Group s.r.o.
Na Záhonech 212, 686 04 Kunovice
Czech Republic
Website: www.cruiseraircraft.cz
E-mail: [e-mail]
This document contains EASA approved Chapter 2A – Airworthiness Limitation Section.

CR-MM-1-0-00
Revision No.: 25 Date of issue: 2021-01-15
iv
INTENTIONALLY LEFT BLANK

CR-MM-1-0-00
PS-28 Cruiser
PS-28N Cruiser
RECORD OF REVISION
Date of issue: 2017-12-05 Revision No.: 20
0 - 1
Rev.
No. Revision name Changed pages Issue date
Date and
signature
1
Formal correction, supplementation
of engine Rotax 912 S,
supplementation of chapter
General Safety Information;
supplementation of parts with life
limitation, revision of inspections
tasks and lubrication chart;
supplementation of aileron rod
sealing;
change of control surface
deflections;
supplementation of BRS and ELT;
check after shimmy occurrence;
change of fuel quantity sensor
type, supplementation of fuel filter
cleaning;
supplementation of engine Rotax
912 S, supplementation of fuses,
change of battery type;
chapter rename, supplementation
of typical instrument panels and
COMM / NAV equipment
description and maintenance
practices
i to iv, 0-1, 0-6 to 0-9,
1-1, 1-3 to 1-6, 1-8,
1-9
2-1 to 2-16
4-6, 4-7,
6-27,
7-1 to 7-12,
8-1, 8-12 to 8-15, 8-
17 to 8-23,
9-1, 9-5, 9-8, 9-12
10-1 to 10-40
11-2, 11-6, 11-7, 11-
11, 11-12
12-1 to 12-30,
2011-07-08 2011-07-08
Konečný
2
Specification of engines marking,
supplementation of chapters,
Equipment List, Sources to
Purchase Parts, List of Disposable
Replacement Parts, Weight and
Balance Information, Tire Inflation
Pressure, Approved Oils and
Capacities, Recommended
Fastener Torque Values and
supplementation Definitions.
supplementation of Sensenich
3B0R5R68C propeller,
specification of 50H inspections,
correction of some maintenance
works, modification of lubrication
chart
supplementation of sunshield and
sliding window, formal correction
baggage weight reduction, wing
removal procedure specification
modification of checking
procedures
i to iv, 0-1, 0-6, 0-7, 1-
1, 1-3, 1-8, 1-10 to 1-
12
2-1 to 2-18
3-4, 3-5, 3-8
4-5, 4-6
6-25 to 6-32
2011-11-08 2011-11-08
Konečný

PS-28 Cruiser
PS-28N Cruiser
CR-MM-1-0-00
RECORD OF REVISION
Revision No.: 20 Date of issue: 2017-12-05
0 - 2
Rev.
No. Revision name Changed pages Issue date
Date and
signature
2
Supplementation of Loctite
threadlocker, supplementation of
procedure of lubrication
correction of fuel scheme
supplementation of Sensenich
3B0R5R68C propeller and
appropriate maintenance practices
supplementation of switches /
circuit breakers, battery life
supplementation of PS-28 Cruiser
instrument panels
8-1, 8-18, 8-23
9-1 to 9-3
10-1 to 10-42
11-4 to 11-6
12-1 to 12-32
2011-11-08 2011-11-08
Konečný
3
Formal correction,
supplementation of definition,
specification of battery life
limitation, supplementation of EFIS
D-100 battery, supplementation of
propeller Special Scheduled
Inspection, supplementation of
brake pad check, supplementation
of EFIS D-100 battery capacity
test,
supplementation of cross reference
specification of safety harnesses,
supplementation of the third friction
washer on nose gear leg
supplementation of fuel scheme,
modification of the fuel system
tightness check
correction of Rotax manuals
section, torque moment and
exhaust installation, correction of
engine test report, supplementation
of Klassic 170/3/R propeller
inspections
supplementation of SkyView
system switches / circuit breakers,
supplementation of SkyView
system description and
maintenance practices,
supplementation of EFIS D100,
EMS D120 firmware upgrade
i to iv, 0-2, 0-6 to 0-9
1-10
2-1 to 2-3, 2-5 to 2-7,
2-13, 2-14
7-2, 7-4, 7-5
8-18
9-2 to 9-5, 9-7, 9-13
10-2, 10-3 to 10-5,
10-9, 10-10, 10-12 to
10-14, 10-28, 10-29,
10-37 to 10-46, 10-48
11-4 to 11-7, 11-14
12-1 to 12-46
2012-05-28
EASA Minor
Change
Approval
10041497
21. 9. 2012
4
Supplementation of GTN 650 / 750
description and maintenance
practices, supplementation of GPS
antenna maintenance practices,
supplementation of reference to
avionics manufacturer
documentation, supplementation of
Dynon avionics pitot / static test,
i to iv, 0-2, 0-3, 0-6 to
0-9
12-1 to 12-54
2012-12-10
EASA Minor
Change
Approval
10043463
30. 1. 2013

CR-MM-1-0-00
PS-28 Cruiser
PS-28N Cruiser
RECORD OF REVISION
Date of issue: 2015-05-24 Revision No.: 13
0 - 3
Rev.
No. Revision name Changed pages Issue date Date and
signature
4
supplementation of GTN post
installation checkout log 17-1, 17-2, 17-6 to 17-10 2012-12-10
EASA Minor
Change
Approval
10043463
30. 1. 2013
5
Supplementation of stall warning
system description and
maintenance practices
i to iv, 0-3 to 0-6, 0-8,
0-9, 12-1, 12-2, 12-9,
12-20, 12-21, 12-53 2013-02-04
EASA Major
Change
Approval
10043557
6. 2. 2013
6
Supplementation of efficient
heating system and carbon
monoxide detector installation.
i to iv, 0-3, 0-6, 0-9, 0-
10, 13-1 to 13-10 2013-03-11
EASA Minor
Change
Approval
10045960
31. 7. 2013
7 Check of nose landing gear leg
for cracks i to iv, 0-3, 0-6, 0-7,
2-7, 2-11, 8-1, 8-17 to
8-26
2013-10-09 2013-10-09
Konečný
8
Supplementation of Sensenich
3B0R5R68C propeller
installation on PS-28 airplanes
i to iv, 0-3, 0-6, 0-8,
10-2, 10-3, 10-8,
10-11, 10-24, 10-43 2014-01-30
EASA Major
Change
Approval
10047966
31. 1. 2014
9
Correction of cross reference,
supplementation of improved
nose landing gear and
modification of relevant
maintenance practices
i to iv, 0-3, 0-6, 0-7,
2-5, 2-7, 2-11, 2-12,
8-4, 8-5, 8-19 2014-02-17
EASA Minor
Change
Approval
10048185
18. 2. 2014
10
Supplementation of balance
ballast description and
installation.
i to iv, 0-3, 0-6, 3-1,
3-5, 3-10, 3-11 2014-08-22
EASA Minor
Change
Approval
10050318
27. 8. 2014
11
Revision of SkyView system,
supplementation of SkyView
system adjustment, extension of
nose landing gear leg check for
cracks, supplementation of ELT
Kannad 406, supplementation of
XPDR control unit TC20.
i to iv, 0-3, 0-6 to 0-9,
2-2, 7-1, 7-3, 7-4, 7-10
to 12, 8-1, 8-18, 8-19,
8-20, 12-2, 12-8 to 10,
12-12, 12-17, 12-18,
12-38 to 44, 12-46 to
49, 12-54 to 62
2014-10-29
EASA Major
Change
Approval
10051301
21. 11. 2014
12
Increasing of the airframe
service life, improvement of 100
h / annual inspection in fuselage
and wing area
i to iv, 0-3, 0-6, 2-2,
2-8, 2-9 2014-11-24
EASA Major
Change
Approval
10051602
11. 12. 2014
13 Supplementation of Scheduled Inspection after 25 H concerning
NLG No SG0270N.
i to iv, 0-3, 0-6, 2-1,
2-3, 2-4, 2-7, 2-8,
2-20 2015-05-24
EASA Major
Change
Approval
10053460
29.5.2015

PS-28 Cruiser
PS-28N Cruiser
CR-MM-1-0-00
RECORD OF REVISION
Revision No.: 22 Date of issue: 2018-09-27
0 - 4
Rev.
No. Revision name Changed pages Issue date Date and
signature
14 Change of the circuit breaker value
for Attitude Indicator and
Directional Gyro
i, ii, iii, iv, 0-4, 0-6, 0-8,
11-6 2015-09-07
EASA Minor
Change
Approval
10054830
22.09.2015
15
Coolant Temperature (CT) as an
alternative to the Cylinder Head
Temperature (CHT) added for
cases that the engine is equipped
with new cylinder heads design
acc.to the SB-912-066 and SB-
912-066UL Rotax bulletin
i to iv, 0-4, 0-6, 0-8,
0-9, 0-10, 1-10, 10-3,
10-4, 10-5, 10-6,
10-38, 10-46, 12-3, 12-
4, 12-5, 12-6, 12-7, 12-
8, 12-12, 12-18, 12-42,
17-5
2015-09-23
EASA Major
Change
Approval
10055978
11.12.2015
16
New / updated propeller limits
(inspections, works) for:
Woodcomp Klassic 170/3/R
Sensenich 3B0R5R68C
i to iv
0-4, 0-6, 0-8,
2-2, 2-3, 2-7, 2-8, 2-14
10-1, 10-2, 10-39,
10-40, 10-41, 10-42,
10-43
2016-02-19
EASA Major
Change
Approval
10057611
30.3.2016
17
Landing Light Replacement added
– type TrailTech 4213-SX replaced
by type Kuntzleman 11-06854
- valid from S/N 0571
i to iv
0-4, 0-6, 0-8
11-5, 11-6 2016-08-17
EASA Minor
Change
Approval
10059451
16.9.2016
18 Dual Circuit Thermostat Hektik
F1107 in the PS-28 Cruiser Engine
Liquid Cooling System
i to iv
0-4, 0-8
10-1, 10-2, 10-6, 10-7,
10-47
2016-10-24
EASA Major
Change
Approval
10060546
21.12.2016
19 Installation of ELT Kannad 406 AF Compact in Airplanes with Analog
Equipment
i to iv
0-4, 0-6, 0-7
7-1, 7-3, 7-10, 7-12 2017-06-06
EASA Minor
Change
Approval
10062712
24.7.2017
20
Supplementation of TrailTech
D112-SX landing light
Supplementation of oil filter
information
Administrative corrections
i to iv
0-4, 0-6, 0-7, 0-8,
1-3, 1-8, 2-1, 2-3, 2-8,
10-1, 10-2, 10-11, 10-17,
10-33, 10-34, 10-37,
10-40, 10-41, 10-42,
11-1, 11-4, 11-5, 11-6,
11-12, 11-13, 11-14
2017-12-05
EASA Minor
Change
Approval
10065161
6.4.2018
21 Administrative correction: Chapter 18 – Valid Supplements
page added
i to iv
0-4, 0-10,
1-1, 18-1, 18-2, 18-3,
18-4
2018-04-13
EASA Major
Change
Approval
10066844
11.9.2018
22
Installation of the SG0160L/P
reinforced main gear leg and info
on torque moments, locknuts,
spacer added.
Number of washers on stabilizer
and on wing updated.
i to iv
0-4 to 0-9,
1-1, 2-1, 2-4, 2-9, 2-16,
3-1, 3-10, 4-1, 4-5 to 4-
10, 5-1, 5-6 to 5-11, 6-
1, 6-7, 6-8, 6-10 to 6-
15,
2018-09-27
EASA Major
Change
Approval
10070985
17.9.2019

CR-MM-1-0-00
PS-28 Cruiser
PS-28N Cruiser
RECORD OF REVISION
Date of issue: 2021-01-15 Revision No.: 25
0 - 5
Rev.
No. Revision name Changed pages Issue date Date and
signature
22
Redundant washer from landing
gear wheel deleted.
Caution for engine test updated.
New page 0-5 added.
Repairman (LS-M) or Mechanic
(A&P) was replaced by new
definition.
6-17, 6-18, 6-21, 7-1, 7-5, 7-
7, 7-9, 7-10, 8-1, 8-3, 8-7 to
8-9, 8-12 to 8-14, 8-22, 9-1,
9-8 to 9-10, 10-1, 10-2,
10-12, 10-13, 10-15, 10-16,
10-18, 10-19, 10-22, 10-23,
10-28, 10-29, 10-32, 11-1,
11-12, 11-13, 12-1, 12-2,
12-19 to 12-23, 12-25, 12-
26, 12-28 to 12-43, 12-45 to
12-50
2018-09-27
EASA Major
Change
Approval
10070985
17.9.2019
23 Inspection and lubrication of
Gerdes or ACS ignition switches
i to iv
0-5, 0-6,0-8, 0-9,
2-8,
12-2, 12-62 to 12-66
2020-01-15
EASA Minor
Change
Approval
10072846
18.03.2020
24
Airworthiness Limitation Section
(ALS) integration
i to iv
0-5, 0-6, 0-7, 0-8, 0-10
1-1, 1-4, 1-7, 1-8, 1-10, 1-
11, 1-12, 1-13, 1-14
2-1, 2-2, 2-3, 2-4, 2-5, 2-6,
2-7, 2-8, 2-9, 2-10, 2-11, 2-
12, 2-13, 2-14, 2-15, 2-16,
2-17, 2-18, 2-19, 2-20
3-1, 3-5, 3-6, 3-12
6-2
7-3, 7-7, 7-9
9-3, 9-5
10-1, 10-2, 10-10, 10-17,
10-18, 10-19, 10-35, 10-36,
10-37, 10-38
17-2, 17-3, 17-5
2020-11-19
EASA Major
Change
Approval
10075099
07.12.2020
25 PS-28N implementation
i to iv
0-5, 0-6, 0-7, 0-8, 0-9
1-5, 1-6
2-1, 2-2, 2-13
6-5
7-1, 7-4, 7-13, 7-14, 7-16
9-1, 9-6
10-1, 10-2, 10-6, 10-7, 10-9,
10-34, 10-35
11-1, 11-5, 11-7, 11-8, 11-9,
11-10, 11-15, 11-16, 11-17,
11-18, 11-19
12-1, 12-2, 12-6, 12-9,
12-12, 12-20, 12-21, 2-22,
12-24, 12-25, 12-56, 12-57,
12-59, 12-61, 12-62
2021-01-15
EASA Major
Change
Approval
EASA.A.546
26.04.2021

PS-28 Cruiser
CR-MM-1-0-00
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Revision No.: 25 Date of issue: 2021-01-15
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Title Page
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2021-01-15
2-12
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2021-01-15
2-13
2021-01-15
2-14
2020-11-19
2-15
2020-11-19
RoR
0-1
2017-12-05
2-16
2020-11-19
0-2
2017-12-05
2-17
2020-11-19
0-3
2015-05-24
2-18
2020-11-19
0-4
2018-09-27
2-19
2020-11-19
0-5
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2020-11-19
LoEP
0-6
2021-01-15
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3-1
2020-11-19
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3-2
2011-03-08
0-8
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2-3
2011-03-08
0-9
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3-4
2012-12-10
0-10
2020-11-19
3-5
2020-11-19
3-6
2020-11-19
3-7
2011-03-08
1
1-1
2020-11-19
3-8
2011-11-08
1-2
2011-03-08
3-9
2011-03-08
1-3
2017-12-05
3-10
2018-09-27
1-4
2020-11-19
3-11
2014-08-22
1-5
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3-12
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1-6
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1-7
2020-11-19
1-8
2020-11-19
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4-1
2018-09-27
1-9
2011-07-08
4-2
2011-03-08
1-10
2020-11-19
4-3
2011-03-08
1-11
2020-11-19
4-4
2011-03-08
1-12
2020-11-19
4-5
2018-09-27
1-13
2020-11-19
4-6
2018-09-27
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2020-11-19
4-7
2018-09-27
4-8
2018-09-27
4-9
2018-09-27
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2-1
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4-10
2018-09-27
2-2*
2021-01-15
4-11
2011-03-08
2-3
2020-11-19
4-12
2011-03-08
2-4
2020-11-19
2-5
2020-11-19
2-6
2020-11-19
2-7
2020-11-19
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2020-11-19
2-9
2020-11-19
*EASA approved page

CR-MM-1-0-00
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5-1
2018-09-27
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7-1
2021-01-15
5-2
2011-03-08
7-2
2012-05-28
5-3
2011-03-08
7-3
2020-11-19
5-4
2011-03-08
7-4
2021-01-15
5-5
2011-03-08
7-5
2018-09-27
5-6
2018-09-27
7-6
2012-05-28
5-7
2018-09-27
7-7
2018-09-27
5-8 2018-09-27 7-8 2011-07-08
5-9
2018-09-27
7-9
2014-10-29
5-10
2018-09-27
7-10
2018-09-27
5-11 2018-09-27 7-11 2018-09-27
5-12
2011-03-08
7-12
2014-10-29
7-13
2021-01-15
7-14
2021-01-15
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6-1
2018-09-27
7-15
2017-06-06
6-2
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7-16
2021-01-15
6-3
2011-03-08
6-4 2011-03-08 8 8-1 2018-09-27
6-5
2021-01-15
8-2
2011-03-08
6-6
2018-09-27
8-3
2018-09-27
6-7 2018-09-27 8-4 2014-02-17
6-8
2011-03-08
8-5
2014-02-17
6-9
2018-09-27
8-6
2011-03-08
6-10
2018-09-27
8-7
2018-09-27
6-11
2018-09-27
8-8
2018-09-27
6-12
2018-09-27
8-9
2018-09-27
6-13
2018-09-27
8-10
2011-03-08
6-14 2018-09-27 8-11 2011-03-08
6-15
2011-03-08
8-12
2018-09-27
6-16
2018-09-27
8-13
2018-09-27
6-17 2018-09-27 8-14 2018-09-27
6-18
2011-03-08
8-15
2011-03-08
6-19
2011-03-08
8-16
2011-03-08
6-20
2011-11-08
8-17
2017-12-05
6-21
2011-11-08
8-18
2017-12-05
6-22
2011-11-08
8-19
2014-10-29
6-23
2011-11-08
8-20
2014-10-29
6-24 2011-11-08 8-21 2013-10-09
6-25
2011-11-08
8-22
2018-09-27
6-26
2011-11-08
8-23
2013-10-09
8-24 2013-10-09
8-25
2013-10-09
8-26
2013-10-09

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2012-05-28
9-2
2012-05-28
10-28
2011-11-08
9-3 2020-11-19 10-29 2011-11-08
9-4
2012-05-28
10-30
2011-11-08
9-5
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10-31
2011-03-08
9-6
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10-32
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9-7
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10-33
2011-11-08
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10-39
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2011-03-08
10-40
2017-12-05
9-15
2011-07-08
10-41
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2011-11-08
10-42
2017-12-05
10-43
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10-45
2017-12-05
10-2
2021-01-15
10-46
2017-12-05
10-3 2015-09-23
10-4
2015-09-23
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11-1
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10-5
2015-09-23
11-2
2011-07-08
10-6
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2011-03-08
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10-8
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10-10
2014-01-30
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2011-03-08
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CHAPTER 1 – GENERAL
Date of issue: 2020-11-19 Revision No.: 24
1 - 1
CHAPTER 1 GENERAL ............................................................................1-3
CHAPTER 2 TIME LIMITS / MAINTENANCE CHECKS............................2-1
CHAPTER 2A AIRWORTHINESS LIMITATION SECTION .....................2-2
CHAPTER 2B INSPECTION AND MAINTENANCE................................2-3
CHAPTER 3 FUSELAGE ..........................................................................3-1
CHAPTER 4 WING....................................................................................4-1
CHAPTER 5 TAIL UNIT ............................................................................5-1
CHAPTER 6 CONTROL SYSTEM.............................................................6-1
CHAPTER 7 EQUIPMENT.........................................................................7-1
CHAPTER 8 LANDING GEAR ..................................................................8-1
CHAPTER 9 FUEL SYSTEM.....................................................................9-1
CHAPTER 10 POWERPLANT ..................................................................10-1
CHAPTER 11 ELECTRICAL SYSTEM......................................................11-1
CHAPTER 12 INSTRUMENTS AND AVIONICS .......................................12-1
CHAPTER 13 VENTING / HEATING.........................................................13-1
CHAPTER 14 AIRPLANE HANDLING......................................................14-1
CHAPTER 15 AIRPLANE REPAIRS.........................................................15-1
CHAPTER 16 WIRING DIAGRAMS..........................................................16-1
CHAPTER 17 APPENDICES.....................................................................17-1
CHAPTER 18 VALID SUPPLEMENTS PAGE...........................................18-1

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1. GENERAL
Content
1.1 Introduction............................................................................................................ 1-4
1.2 Airplane Classification ........................................................................................... 1-4
1.2.1 Power Unit ................................................................................................ 1-4
1.2.2 Main Technical Data................................................................................. 1-5
1.3 Airplane Manufacturer and Type Certificate Holder .............................................. 1-7
1.4 Chapter Order........................................................................................................ 1-7
1.4.1 Page Numbering....................................................................................... 1-7
1.5 Warnings, Cautions and Notes.............................................................................. 1-7
1.6 Equipment List....................................................................................................... 1-8
1.7 Sources to Purchase Parts.................................................................................... 1-8
1.8 List of Disposable Replacement Parts................................................................... 1-8
1.9 Weight and Balance Information ........................................................................... 1-8
1.10 Tire Inflation Pressure............................................................................................ 1-8
1.11 Approved Oils and Capacities ............................................................................... 1-8
1.12 Recommended Fastener Torque Values............................................................... 1-8
1.13 General Safety Information.................................................................................... 1-9
1.14 Definitions and Abbreviations.............................................................................. 1-10

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1.1 Introduction
In accordance with requirements of the ASTM LSA regulations, the Czech Aircraft Group s.r.o.,
as manufacturer of PS-28 Cruiser airplane, provides information on maintaining airworthiness
of the PS-28 Cruiser airplane. Information is also contained in the following manuals issued by
airplane manufacturer or by manufacturers of equipment used on the airplane:
•Pilot Operating Handbook
•Maintenance Manual
•Illustrated Parts Catalog
•Operator's Manual for ROTAX Engine Type 912 Series
•Maintenance Manual for ROTAX Engine Type 912 Series
•Technical description and operation instructions for the propeller
This Maintenance Manual contains information on airplane maintenance including description
of airplane structure and function.
1.2 Airplane Classification
PS-28 Cruiser airplane is two-seat, single engine, low-wing, all-metal airplane with fixed three-
wheel landing gear.
The airplane is designed for basic and advanced training and for leisure time flying.
1.2.1 Power Unit
Power unit consists of:
•Four-stroke, four-cylinder engine with opposite pistons Rotax 912 S2 / 912 ULS2 with max.
continuous power of 69 kW (92.5 hp) at 5,500 RPM.
•Three-blade, ground adjustable propeller or
•Two-blade, ground adjustable propeller or
•Two-blade, in flight adjustable propeller.

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1.2.2 Main Technical Data
Wing
•Span………………………………………………….....8.600 m (28.21 ft)
•Area...........................................................................12.3 m2 (132.30 sq.ft)
•MAC ..........................................................................1,500 mm (59.10 in)
•Wing loading .............................................................49 kg/m2 (10.00 lb/sq.ft)
•Aileron area...............................................................0.40 m2 (4.31 sq.ft)
•Flap area...................................................................0.65 m2 (7.00 sq.ft)
Fuselage
•Length ………..…………………………………….…..6.680 m (21.91 ft)
•Width.........................................................................1.280 m (50.40 in)
•Height…………………………………………………...2.340 m (7.67 ft)
•Cockpit width.............................................................1.170 m (46.00 in)
Horizontal tail unit
•Span..........................................................................2.930 m (9.61 ft)
•HTU area...................................................................2.2 m2 (23.70 sq.ft)
•Elevator area.............................................................0.8 m2 (8.60 sq.ft)
Vertical tail unit
•Height........................................................................1.07 m (3.51 ft)
•VTU area...................................................................1 m2 (10.70 sq.ft)
•Rudder area..............................................................0.4 m2(4.30 sq.ft)
Landing gear
•Wheel track...............................................................1.520 m (4.98 ft)
•Wheel base...............................................................2.030 m (6.66 ft)
•Nose landing gear wheel diameter ...........................343 mm (13.50 in)
•Main landing gear wheel diameter............................343 mm (13.50 in)

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Fig. 1-1: Three-view drawing