No Revision Aircraft
Date
VA502 7
SB7L-235 SB7L-360 SB7L-360A SB7L-360A2 5 May 2016
TYPE CERTIFICATE DATA SHEET
This data sheet, which is part of Type Certificate No. VA502, Issue 4, lists the conditions and operational limitations under which the aircraft for which the Type Certificate was issued meets the airworthiness requirements of the Civil Aviation Safety Authority.
Certificate Holder Seabird Aviation Australia Pty Ltd Hervey Bay Airport
PO Box 618 Pialba Qld 4655 Australia
Model SB7L-235
Engine
Engine Limits
Fuel
Oil
Propeller
Utility Categoiy - approved 12 March 1993.
Textron Lycommg 0-235-N2C.
Maximum take-off"
Maximum continuous-
2700 rpm.
2500rpm@25"MAP.
(Cruise noise limit).
100LL or 100/130 minimum grade aviation gasoline.
As specified in the latest revision ofTextron Lycoming Service Instruction No. 1014.
MT-Propeller model MTV-7-F/LD 165-03.
Diameter 1650 mm (no cut off allowed).
Pitch Settings at the 560 mm station.
High pitch-24° ±1°.
Low pitch-12° ±0.2°.
Fine Pitch Limit Contacts Set fine pitch to give 2590 rpm ± 10 rpm at full throttle static with the propeller on the fine pitch stop.
Propeller Restricted Range 2300 rpm to 2500 rpm.
Air Speed Limits
Centre of Gravity
Datum
Levelling Means
Maximum Weight
Oil Capacity
Control Surface Deflections
Never exceed (VNE) Manoeuvring (VA)
Max structural cruise (V^o) Max flaps extended (Vpp.)
Forward Limit: 2251 mm aft of datum at all weights.
(KIAS) 147117 no95
(KCAS) 144115 10893
Aft Limit: 2384 aft of datum at all weights.
2043 mm forward of the wing leading edge at butt line 2122 mm.
Plumb bob from drilled bolt in cockpit overhead bow to centre mark on the forward undercan'iage bay cross member.
Take Off 754 kg.
Landing 754 kg.
Minmium Crew
Number of Seats
Total load front seats
Maximum Baggage
Fuel Capacity
One pilot.
Two.
Pilot seat arm
Passenger seat arm
Minimum:
Maximum:
Maximum seat
seat forward:
seat aft:
arm seat forward:
seat aft:
load — full fuel:
45 kg at 2312 mm aft of datum.
Total 148: litres (2 x 74 litre
1286 mm aft of datum 1446 mm aft of datum 1286 mm aft of datum 1646 mm aft of datum
65 kg.
180kg.
77.1kg.
tanks at 2312 mean fuel ar Usable 136 litres.
Refer to the flight manual for fuel distribution weight and balance
data.
5.6 litres.
Aileron Up Down Elevator Up
Down
112 mm ± 5 mm at the trailing edge.
74 mm ± 5mm at the trailing edge.
160 mm ± 5mm at the trailing edge.
83 mm ± at the trailing edge.
Elevator fixed tabs Trailing edge of tabs 40 to 50 mm below plane of elevator upper surface.
Operating Altitude
Crosswind Component
Manoeuvres permitted
Types of Operations
Required Placards Certification Basis
TCDS No. VA502 Revision 7
Rudder Left and Right - 170 mm ± 5 mm at the trailing edge.
Wing flaps Retracted 0°±1°
First Notch 20° ±1°
Full 40° ±1°
Maximum 10,000 feet AMSL.
Maximum for take-off and landing - 10 knots.
Non aerobatic manoeuvres as for normal flight including stalls (except whip stalls), chandelles, lazy eights and steep turns (angle of bank less than 60°).
MANOEUVRE
Stalls Chandelles Lazy eights Steep turns
ENTRY SPEED
Slow deceleration.
105 KIAS.
105 KIAS.
75-80KIAS.
Aerobatic manoeuvres, including intentional spins, are prohibited.
VFR by day.
Flight into known or forecast icing conditions is prohibited.
Refer to the approved flight manual.
Civil Aviation Order 101.22, Issue 4, dated 1 May 1981 up to and including Amendment 72 and FAR 23 up to and including
Amendment 34.
Serial Numbers Eligible No aircraft of this model have been produced. Future production will require approval from CASA.
Model SB7L-360 (Seeker) Restricted Category - approved 12 March 1 999.
Engine Textron Lycoming 0-3 60-B2C.
Engine Limits Maximum take-off 2500 rpm (No time limit).
Fuel
Oil
80/87 minimum grade aviation gasoline.
Unleaded automotive gasoline.
As specified in the latest revision ofTextron Lycoming Service Instruction No. 1014.
Propeller
Air Speed Limits
Centre of Gravity
Datum
Levelling Means
Maximum Weight
Minimum Crew
Number of Seats
Maximum Baggage Fuel Capacity
(KIAS) 133105 10595
(KCAS)
129 105105 93
Seabird Aviation, wooden, 2 blade fixed pitch, pusher.
Model: BB 177.
Diameter: 1770 mm.
Pitch; 1350 nun at 750 mm radius.
Static rpm at full throttle:
Maximum: 2300 rpm.
Minimum: 2200 rpm.
Never exceed (VNE) Manoeuvring (VA)
Max structural cruise (VNC>) Max flaps extended (VFE)
Forward Limit: 2251 mm affc of datum at all weights.
Aft Limit: 2384 aft of datum at 800 kg or less.
2362 aft of datum at 897 kg.
Variation is linear between 800 kg and 897 kg.
2043 mm forward of the wing leading edge at butt line 2122 mm.
Plumb bob from drilled bolt in cockpit overhead bow to centre mark on the forward undercardage bay cross member.
Take Off 897 kg.
Landing 897 kg.
One pilot.
Two.
Pilot seat arms seat forward:
seat aft;
Passenger seat arm seat forward:
seat aft:
45 kg at 2090 mm aft of datum.
1286 mm aft of datum.
1446 mm aft of datum.
1286 mm aft of datum.
1646 mm aft of datum.
Oil Capacity
Total 184 litres (2 x 92 litre tanlcs at 2312 mean fuel arm).
Usable 172 litres.
Refer to the flight manual for fuel distribution weight and balance
data.
7.5 litres.
Control Surface Deflections
Operating Altitude Crosswind Component
Types of Operation
Manoeuvres Permitted
Aileron Up Down Elevator Up
Down Elevator fixed tabs
Rudder
TCDSNO.VA502 Revision 7
112 mm ± 5 mm at the trailing edge.
74 mm ± 5mm at the trailing edge.
160 mm ± 5mm at the trailing edge.
83 mm ± at the trailing edge.
Trailing edge of tabs 40 to 50 mm below plane of elevator upper surface.
Left and Right 170 mm ± 5 mm at the trailing edge.
Wing flaps Retracted 0°±1°
First Notch 20° ±1°
Full 40° ±1°
Maximum 15,000 feet AMSL.
Maximum for take-offand landing - 12 knots.
VFR (day and night).
Flight into known icing conditions is prohibited.
Non aerobatic manoeuvres as for normal flight including stalls (except whip stalls), chandelles, lazy eights and steep turns (angle of bank < 60°).
MANOEUVRE
Stalls Chandelles Lazy eights Steep turns
ENTRY SPEED
Slow deceleration
105 KIAS 105 KIAS
75 - 80 KIAS.
Aerobatic manoeuvres, including intentional spins, are prohibited.
Purpose of Operation
Required Placards
Operations are restricted to the following special purposes:
(a) forest and wildlife conservation;
(b) Aerial surveying and scientific research, eg. photography, mapping, oil and mineral exploration;
(c) Patrolling, eg. pipelines, power lines and canals;
(d) Forest fire surveillance; and
(e) Operations authorised in Regulation 262AL of the Civil Aviation Regulations 1988.
Refer to the approved flight manual.
Certification Basis
Serial Numbers Eligible Production Basis
Noise Certification
Civil Aviation Safety Regulations (1998) 21.17 and 21.25.
This aircraft meets the certification basis for the model SB7L-360A except that sections of the aircraft S/No 92005 do not conform to the type design for the SB7L-360A (see Note 3).
92005 only (See Note 6).
CAA Certificate of Approval 3252 dated 3 February 1994.
Compliance with ICAO Annex 16 Chapter 10 and FAR 36 Appendix G has been shown.
Model SB7L-360A (Seeker) Normal Category - approved 24 January 1 994.
Engine Textron Lycoming 0-360-B2C.
Maximum take-off power Serial Numbers: 94006, 070010,070011,070012 and 070014 2500 rpm (No time limit).
Serial Numbers: 070009, and SA01 100 and subsequent 2700 rpm (No time limit).
Fuel
Oil
Propeller
80/87 minimum grade aviation gasoline.
Unleaded automotive gasoline.
As specified in the latest revision ofTextron Lycoming Service Instruction No. 1014.
Seabird Aviation, wooden 2 blade fixed pitch, pusher.
Model: BB177.
Diameter: 1770 mm.
Pitch: 1350 mm at 750 mm radius.
or
Hoffinan GmbH, wooden 2 blade fixed pitch pusher.
Model: H044HM-177 138LD.
Diameter: 1770mm.
Pitch: 1380mm.
Static rpm at full throttle (both propellers):
Maximum: 2300 rpm.
Minimum: 2200 rpm.
Air Speed Limits
Centre of Gravity
Datum
Levelling Means
Maximum Weight
Minimum Crew
Number of Seats
Maximum Cargo
Fuel Capacity
Never exceed (VNE) Manoeuvring (VA)
Max structural cmise (V^o) Max flaps extended (VFE)
Forward Limit: 2251 mm aft of datum at all weights.
(KIAS) 134107 10795
TCDSNO.VA502 Revision 7
(KCAS) 133 105105 93
Aft Limit: 2384 aft ofdatimi at 800 kg or less.
2362 aft of datum at 925 kg.
Variation is linear between 800 kg and 925 k^
2043 mm forward of the wing leading edge at butt line 2122 mm.
Plumb bob from drilled bolt in cockpit overhead bow to centre mark on the forward undercamage bay cross member.
Take Off 925 kg.
Landing 925 kg.
One pilot.
Two.
Pilot seat arms seat forward:
seat aft:
Passenger seat arms seat forward:
seat aft:
45 kg at 2090 mm aft of datum.
1286 mm aft of datum.
1446 mm aft of datum.
1286 mm aft of datum.
1646 mm aft of datum.
Oil Capacity
Serial Number: 94006
Total 160 litres (2 x 80 litre tanks at 2312 mean fuel arm).
Usable 148 litres.
Serial Numbers: 070010, 070011, 070012,070014
Total 184 litres (2 x 92 litre tanks at 2312 mean fuel arm).
Usable 172 litres.
Aircraft Serial Numbers: 070009, and SA01100 and subsequent.
Total 184 litres (2 x 92 lib-e tanks at 2312 mean fuel arm).
Usable 182 litres.
Refer to flight manual for fuel distribution weight and balance data.
7.5 litres.
Control Surface Deflections
Aileron
Elevator
Up
Down
Up
Down
Operating Altitude
Crosswind Component
Types of Operation
Manoeuvres permitted
Required Placards Certification Basis
Elevator fixed tabs
112 mm ± 5 mm at the trailing edge.
74 mm ± 5mm at the trailing edge.
160 mm ± 5mm at the trailing edge.
83 mm ± at the trailing edge.
Trailing edge of tabs 40 to 50 mm below plane of elevator upper surface.
Rudder Left and Right 170 mm ± 5 mm at the trailing edge.
Wing flaps Retracted 0° ± 1°
First Notch 20° ±1°
Full 40° ±1°
Maximum 15,000 feet AMSL.
Maximum demonstrated for talce-off and landing 12 knots.
VFR, day and night, or IFR (see serial number eligibility).
Flight into known icing conditions is prohibited.
Non aerobatic manoeuvres as for normal flight including stalls (except whip stalls), chandelles, lazy eights and steep turns (angle of bank < 60°).
MANOEUVRE
Stalls Chandelles Lazy eights Steep turns
ENTRY SPEED
Slow deceleration
105 KIAS 105KIAS
75-80KIAS.
Refer to the approved flight manual.
Serial Numbers: 94006, 070011, 070012, 070014
Civil Aviation Order 101.22, Issue 4, up to and includmg
Amendment 72 and FAR 23 up to and including Amendment 34.
Serial Number: 070010
Civil Aviation Order 101.22, Issue 4, up to and including
Amendment 72 and FAR 23 up to and including Amendment 34 except that FAR 23.1307, 23.1326 and 23.1353 are at Amendment 49, and 23.1557 is atAmdt 50.
TCDSNo.VA502 Revision 7
Serial Numbers: 070009, and SA01 100 and subsequent
FAR 23 up to and including Amendment 34, except that FARs - 23.331, 23.445 and 23.1163 are at Amdt 42,
- 23.993, 23.1103, 23.1147, 23.1193, 23.1322, 23J385, 23J387, 23.1389, 23.1391, 23.1393 and 23.1395 are at Amdt 43, - 23.251,23.773, 23.1525, 23.1549 and 23.1557 are at Amdt 45, - 23.335, 23371 and 23.572 are at Amdt 48,
- 23.867, 23.1307, 23.1321, 23.1323, 23.1351, 23.1353, 23.1383 and 23.1401 are at Amdt 49,
- 23.71, 23.145, 23.161, 23.201, 23.203, 23J521, 23.1543, 23.1583, 23.1585, 23.1587 and 23.1589 are atAmdt 50, - 23.955, 23.1041, 23.1043, 23.1047, 23.1091, 23.1093, 23.1107,
23.1141, 23.1143, 23.1181, 23.1183, 23.1203 and 23.1337 are atAmdt51,
-23.1305 is at Amdt 52, -23.1308 is at Amdt 57,
- 23.777, 23,853, 23.1301, 23.1303, 23.1309, 23.1310, 23.1311, 23.1331, 23.1431 and 23.1559 are at Amdt 62.
23.1326 is at CASA Special Condition Al 326, and
ELOS Seabird -1233/01 was detennmed for FAR 23.1337(l)(b). CASA document Dl 6/112954 refers.
Type Design Data Serial numbers 94006,070011,070012,070014:
1. Master Drawing List SB7L-360A, SBR02/10, Issue 1, dated 8 September 2005, including later approved changes.
2. SB7L-360A Pilot's Operating Handbook and CASA approved Flight Manual Document SBR 02/96, Issue 3, dated 30 April 2008 including later approved changes.
3. Maintenance Manual SB7L-360A, SBR05/04 Issue 1, dated 13 December 2004 Including later approved changes.
Serial number 070010 (JFR approval):
1. Master Drawing List, SBR07/14 Issue 0, dated 13 July 2012.
2. SB7L-360A Pilot's Operating Handbook and CASA approved Flight Manual Document SBR 03/13, Issue 1, dated 11 April 2013 including later approved changes,
3. Maintenance Manual SB7L-360A, SBR04/13 Issue 1, dated 3 April 2013 including later approved changes.
Serial numbers 070009, and SAG 1 100 and subsequent:
1. Master Drawing List, SBR07/14 Issue 3, dated 1 April 2016, including later approved changes.
2. SB7L-360A Pilot's Operating Handbook and CASA approved Flight Manual Document SBR 28/15, dated 5 May 2016 including later approved changes.
3. Maintenance Manual SB7L-360A, SBR29/15 Issue 1, dated 1 April 2016 including later approved changes.
Serial Numbers Eligible 94006 (see Note 6), 070009, 070010,070011,070012,070014.
SAG 1100 and subsequent.
Production Basis
Noise Certification
CASA Production Certificate No. 417197, dated 25 November 2003.
Compliance with ICAO Annex 16 Chapter 10 and FAR 36 Appendix G has been shown.
Model SB7L-360A2 fSeeker) Normal Category - approved 24 September 2013.
Engine Textron Lycommg IO-390-A1A6. (S/N 070015)
Textron Lycoming IO-390-A1B6. (S/N SA02100 and subsequent) Maximum take-off power 2700 ipm (No time limit).
Fuel
Oil
Propeller
AvgaslOOLL(Blue) Avgas 100 (Green)
As specified in the latest revision ofTextron Lycoming Service Instruction No. 1014.
Seabird Aviation, wooden, 2 blade fixed pitch, pusher.
Model: Bishton BB177-70-55.
Diameter: 1770 mm.
Pitch: 1400 mm at 750 mm radius.
Static rpm at full throttle:
Maximum: 2450 rpm.
Minimum: 2350rpm.
Air Speed Limits
Centre of Gravity
Datum
Levelling Means
Never exceed (VNE) Manoeuvring (VA)
Max structural cruise (VNO) Max flaps extended (Vpa)
Forward Limit: 2274 mm aft of datum at all weights.
(KIAS) 134107 107 95
(KCAS) 133105 105 93
Aft Limit: 2409 mm aft of datum at all weights.
2043 mm forward of the wing leading edge at butt line 2122 mm.
MAC is 1200mm.
Plumb bob from drilled bolt in cockpit overhead bow to centre mark on the forward undercarriage bay cross member.
TCDS No. VA502 Revision 7
Maximum Weight
Minimum Crew
Number of Seats
Maximum Cargo
Fuel Capacity
Take Off 974 kg.
Landing 925 kg.
One pilot.
Two.
Pilot seat arms seat forward:
seat aft:
Passenger seat arms seat forward:
seat aft:
45 kg at 2090 mm aft of datum.
1286 mm aft of datum.
1446 mm aft of datum.
1286 mm aft of datum.
1646 mm aft of datum.
Oil Capacity
Control Surface Deflections
7.6 litres.
Aileron
Elevator
Up
Down
Up
Down Serial Number: 070015
Total 184 litres (2 x 92 litre tanks at 2312 mean fuel arm).
Usable 172 litres.
Serial Numbers: SA02100 and subsequent.
Total 184 litres (2 x 92 litre tanks at 2312 mean fuel arm).
Usable 182 litres.
Refer to flight manual for fuel distribution weight and balance data.
112 mm ± 5 mm at the trailing edge.
74 mm ± 5mm at the trailing edge.
160 mm ± 5mm at the trailing edge.
83 mm ± at the trailing edge.
Trailing edge of tabs 40 to 50 mm below plane of elevator upper surface.
Elevator fixed tabs
Rudder Left and Right 170 mm ± 5 mm at the trailing edge.
Wing flaps Retracted 0° ± 1 ° First Notch 20° ±1°
Full 40° ±1°
Operating Altitude Maximum 15,000 feet AMSL.
Crosswind Component Maximum demonstrated for take-off and landing- 12 knots.
Types of Operation VFR, day and night, or IFR.
Flight into known icmg conditions is prohibited.
Manoeuvres permitted Non aerobatic manoeuvres as for normal flight including stalls (except whip stalls), chandelles, lazy eights and steep turns (angle of bank less than 60°).
MANOEUVRE ENTRY SPEED
Stalls Slow deceleration Chandelles 105 KIAS
Lazy eights 105KIAS
Steep turns 75 - 80 KTAS.
Required Placards Refer to the approved flight manual.
Certification Basis Aircraft Serial Number: 070015
Civil Aviation Safety Regulations, Part 21, as m force on 2 February 2011, and
FAR 23 up to and mcluding Amendment 34, except that FARs 23.71, 23.145, 23.161, 23.201 and 23.203 are atAmdt 50;
23.251 is at Amdt 45; 23.331 is at Amdt 42;
23.335 and 23.371 are atAmdt 48;
23.445 is at Amdt 42; 23.572 is at Amdt 48;
23.1041,23.1043,23.1047,23.1091,23.1093,23.1103,23.1107, 23.1141 and 23.1143 are at Amdt 51;
23.1147 is at Amdt 43; 23.1163 is at Amdt 42;
23.1181 and 23.1183 are at Amdt 51; 23.1193 is at Amdt 43;
23.1203 is atAmdt 51; 23.1305 is at Amdt 52;
23.1307 is at Amdt 49; 23.1308 is at Amdt 57;
23.1309, 23.1311, 23.1326 and 23.1329 are atAmdt49;
23.1331 is at Amdt 43; 23.1337 is at Amdt 51;
23.1351,23.1353 and 23.1383 are at Amdt 49; 23.1385, 23.1387, 23.1389, 23.1391, 23.1393 and 23.1395 are atAmdt 43;
23.1401 and 23.1431 areatAmdt49;23J521 isatAmdt50;
23.1525, 23.1549, 23.1557 are at Amdt 45; and
23.1559, 23.1583, 23.1585, 23.1587 and 23.1589 are atAmdt 50.
Aircraft Serial Number: SA02100 and subsequent
FAR 23 up to and including Amendment 34, except that FARs - 23.331, 23.445 and 23.1163 are atAmdt 42,
- 23.993, 23.1103, 23.1147, 23.1193, 23.1322, 23.1385, 23.1387, 23J389, 23.1391, 23.1393 and 23.1395 are atAmdt 43, -23.251, 23.773, 23.1525, 23.1549and23.1557 areatAmdt45, - 23.335, 23.371 and 23.572 are at Amdt 48,
- 23.867, 23.1307, 23.1321, 23.1323, 23.1351, 23.1353, 23.1383 and 23.1401 are at Amdt 49,
TCDSNO.VA502 Revision 7
- 23.71, 23.145, 23.161, 23.201, 23.203, 23.1521, 23.1543, 23.1583, 23.1585, 23.1587 and 23.1589 are atAmdt 50, - 23.955, 23.1041, 23.1043, 23.1047, 23.1091, 23.1093, 23.1107,
23.1141, 23.1143, 23.1181, 23.1183, 23.1203 and 23.1337 are atAmdt51,
-23.1305 is at Amdt 52, -23.1308 is at Amdt 57,
- 23.777, 23.853, 23.1301, 23.1303, 23.1309, 23.1310, 23.1311, 23.1331, 23.1431 and 23.1559 are at Amdt 62.
23J326 is at CASA Special Condition A1326, and
ELOS Seabird -1233/01 was determined for FAR 23.1337(l)(b). CASA document D 16/112954 refers.
Type Design Data Serial Number 070015
1. Master Drawing List SB7L-360A2, SBR07/14 , Issue 1 , dated 22 July 2013, including later approved changes.
2. SB7L-360A2 Pilot's Operating Handbook and CASA Approved Flight Manual Document SBR 05/13, Issue 3, amended 27 August 2015, including later approved changes.
3. Maintenance Manual SB7L-360A2, SBR06/13 Issue 1, dated 24 September 2013, including later approved changes.
Serial Number SA02100 and subsequent.
1. Master Drawing List SB7L-360A2, SBR07/14, Issue 3, dated 1 April 2016, including later approved changes.
2. SB7L-360A2 Pilot's Operating Handbook and CASA Approved Flight Manual Document SBR 30/15, dated 5 May 2016, including later approved changes.
3. SB7L-360A2 Maintenance Manual, SBR 31/15 Issue 1, dated 1 April 2016, including later approved changes.
Serial Numbers Eligible 070015, and SA02100 and subsequent.
Production Basis CASA Production Certificate No. 417197, dated 25 November 2003, as revised to include the A2 model.
Noise Certification Compliance with ICAO Annex 16 Chapter 10 and FAR 36 Appendix G has been shown.
NOTES
Note 1. Service life limits for life limited parts are contained in the applicable
manufacturer's Maintenance Manuals, Chapter 4, Airworthiness Limitations.
Note 2. Sections of the airframe on aircraft Serial No 92005 in the areas of the wing carry through structure, the lift strut carry through structure, the boom to rear fuselage cluster joint, the fuselage joints one bay forward of the boom attachment, and the boom exterior skin in the vicinity of the rear of the forward top hat sections do not conform to the standard for the SB7L-360A.
Therefore the fatigue analysis of the SB7L-360A in these areas is not applicable. Information in respect to additional fatigue inspections on aircraft Serial No 92005 is listed in the manufacturer's Maintenance Manual, Chapter 4, Airworthiness Limitations.
Note 3. Model SB7L-235, although certificated in the Utility category, is restricted to Normal category manoeuvres only.
Note 4. MTOW of aircraft Serial Numbers 92005 and 94006 is limited to 897 kg.
Note 5. Aircraft serial numbers 070007 and 070008 were not manufactured under an Australia production approval, and are not covered by this TCDS.
Note 6. Acceptance of serial numbers 92005 and 94006 was made under CASA Certificate of Type Approval (CTA) Number 169-1 Issue 2, dated 24 January 1994. These aircraft meet the requirements of this data sheet. This type certificate supersedes that Certificate of Type Approval.
RE VISION NOTES
Revision 2. - adds the Hoffman H044HM-177 138LD propeller as an alternative propeller for the SB7L-360A model.
Revision 3. - adds IFR approval for model SB7L-360A.
Revision 4. - adds new model SB7L-360A2.
Revision 5. - corrects the document number for the -360A2 model flight manual.
- identifies type design data by a new MDL number, in a new format. MDL SBR07/14 Issue 1 consolidates SBR19/1 1 Revision 4 and SBR 20/13
Revision 1 into one document, and is a later revision of both of those MDLs.
- adds noise compliance statement for model SB7L-360A2.
Revision 6. - amends SB7L-360Amax engine RPM.
- updates usable fuel in S/N 070009, SA01100, SA02100 and subsequent.
- adds certification basis and type design data for SB7L-360A and SB7L-360A2 upgraded cockpit.
- amends SB7L-360A and SB7L-360A2 eligible serial numbers.
- updates SB7L-360A2 engine model number
Revision 7. - amends listed total fuel capacity of SB7L-360A and SB7L-360A2 models.
END -
