曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

PA-28S-160 PA-28-236
PA-28S-180 PA-28RT-201
PA-28R-180 PA-28RT-201T
PA-28R-200 PA-28-201T
May 12, 1987
TYPE CERTIFICATE DATA SHEET NO. 2A13
This data sheet, which is a part of Type Certificate 2A13, prescribes conditions and limitations under which
the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air
Regulations.
Type Certificate Holder Piper Aircraft Corporation
2926 Piper Drive
Vero Beach, Florida 32960
I. Model PA-28-160, Cherokee, 4 PCLM (Normal Category), Approved October 31, 1960.
Engine Lycoming 0-320-B2B or 0-320-D2a with Carburetor setting 10-3678-32
Fuel 91/96 minimum grade aviation gasoline.
Engine Limits For all operations, 2700 r.p.m. (160 h.p.)
Propeller and Sensenich M74DM or 74DM6 on S/N 1 through 1760 1760A;
Propeller Limits Sensenich M74DMS or 74D6S5 on S/N 1761 and up. Static r.p.m. at
maximum permission throttle setting: Not over 2425, not under 2325.
No additional tolerance permitted.
Diameter: Not over 74", not under 72.5".
See Note 10.
Propeller Spinner Piper P/N 14422-00 on S/N 1 through 1760A;
Piper P/N 63760-04 or 65805 on S/N 1761 and up.
See Note 11.
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19
Rev. No. 41 36 36 35 35 36 36 35 36 36 35 35 36 35 36 35 36 36 36
Page No. 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38
Rev. No. 36 35 36 36 35 37 38 37 39 37 37 38 39 38 41 38 39 38 41
Page No. 39 40 41 42 43 44 45 46
Rev. No. 38 41 38 38 38 38 38 39
Figure 2-19. Excerpts from a Type Certificate Data Sheet.
2–9
Figure 2-19. Excerpts from a Type Certificate Data Sheet (continued).
2A13 –2– March 3, 1981
Revision 37
Airspeed Limits Never exceed 171 m.p.h. (148 knots) CAS
Maximum Structural 140 m.p.h. (121 knots) CAS
cruising 140 m.p.h. (121 knots) CAS
Maneuvering 129 m.p.h. (112 knots) CAS
Flaps extended 115 m.p.h. (100 knots) CAS
Center of Gravity (+84.0) to (+95.9) at 1650 lb. or less
Range (+85.9) to (+95.9) at 1975 lb.
(+88.2) to (+95.9) at 2200 lb.
Straight line variation between points given
Empty Wt. C.G. Range None
Maximum Weight 2200 lb.
No. of Seats 4 (2 at +85.5,2 at +118.1)
Maximum Baggage 125 lbs. (+142.8) (S/N 28-1 through 28-1760A)
See NOTE 8.
200 lbs. (+142.8) (S/N 28-1761 and up)
Fuel Capacity 50 gal. (2 wing tanks) (+95)
See NOTE 1 for data on system fuel.
Oil Capacity 8 qts. (+32.5), 6 qts. useable
See NOTE 1 for data on system oil.
Control Surface Wing flaps (±2°) Up 0° Down 40°
Movements Ailerons (±2°) Up 30° Down 15°
Rudder (±2°) Left 27° Right 27°
Stabilator (±2°) Up 18° Down 2°
Stabilator tab (±1°) Up 3° Down 12°
Nose Wheel Travel (+1°) Left 30° Right 30°
(Effective on S/N 1 through 3377)
Left 22° Right 22°
(Effective on S/N 3378 and up)
Manufacturer’s 28-03, 28-1 and up.
Serial Nos.
II. Model PA-28-150, Cherokee, 4 PCLM (Normal Category), Approved June 2, 1961
Engine Lycoming 0-320-A2B or 0-320-E2A with carburetor setting 10-3678-32
Fuel 80/87 minimum grade aviation gasoline
Engine Limits For all operations, 2700 r.p.m. (150 h.p.)
Propeller and Sensenich M74DM or 74DM6 on S/N 1 through 1760A;
Propeller Limits Sensenich M74DMS or 74DM6S5 on S/N 1761 and up
Static r.p.m. at maximum permissible throttle setting not over 2375,
not under 2275.
No additional tolerance permitted.
Diameter: Not over 74", not under 72.5."
See NOTE 10.
2–10
Figure 2-19. Excerpts from a Type Certificate Data Sheet (continued).
Data Pertinent to All Models:
Datum 78.4" forward of wing leading edge (straight wing only). 78.4" forward of
inboard intersection of straight and tapered sections (semi-tapered wings).
Leveling Means Two screws left side fuselage below window.
Certification Basis Type Certificate No. 2A13 issued October 31, 1960. Date of Application for
Type Certificate, February 14, 1965.
Delegation Option Authorization granted per FAR 21, Subpart J. July 17, 1968.
PA-28-140 and PA-28-151: CAR 3, effective May 15, 1956, including
Amendments 3-1, 3-2, 3-4, and paragraphs 3.304 and 3.705 of Amendment 3-7.
PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28S-160, PA-28S-180, PA-
28R-180, PA-28R-200; CAR 3, effective May 15, 1956, including
Amendments 3-1, 3-2 and paragraphs 3.304 and 3.705.
PA-28-161: CAR 3 effective May 15, 1956, through Amendment 3-2;
paragraph 3.387(d) of Amendment 3-4; paragraphs 3.304 and 3.705 of
Amendment 3-7; FAR 23.959 of Amendment 23-7; FAR 36 effective
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：飛機載重平衡手冊(12)