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3A13 Rev 70 | Flight Control Surfaces | Flap (Aeronautics)
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AIRCRAFT MAINTENACE PROGRAMM
2007 Amphibian White Paper
TYPE CERTIFICATE DATA SHEET NO. 3A13
This data sheet which is part of Type Certificate No. 3A13 prescribes conditions and limitations under which the product for
which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
WARNING: Use of alcohol-based fuels can cause serious performance degradation and fuel system component damage,
and is therefore prohibited on Cessna airplanes.
I - Model 182, Skylane, 4 PCLM (Normal Category), Approved March 2, 1956
80 minimum grade aviation gasoline
*Engine Limits
For all operations, 2600 r.p.m. (230 hp.)
1. Hartzell constant speed
(a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades
Diameter: not over 82 in., not under 80 in.
Pitch settings at 30 in. sta.:
low 12, high 24
(b) Cessna spinner 0752006
(c) Woodward governor 210065, 210105, 210155 or 210340
2. McCauley constant speed
(a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-8 blades
Pitch settings at 36 in. sta.:
low 10.5, high 22
(b) Cessna spinner 0752004
(c) Woodward governor 210065, 210105, 210155, 210345 or 210452,
or McCauley C290D2/T1 or C290D3/T1
Rev. 69
I - Model 182 (contd)
Propeller Limits (contd)
3. Hartzell constant speed
(a) Hub BHC-C2YF-1 with 8468-2 blades
low 13, high 24
(b) Cessna spinner 0752619
(c) Woodward governor 210105AF, 210340 or 210451
4. McCauley constant speed
(a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades
low 10.5, high 21.5
(c) Woodward governor 210065, 210105, 210155, 210345 or 210452
5. Aircraft reworked per Cessna Service Kit SK182-121:
McCauley constant speed (Threadless)
(a) Hub 2A34C203/90DCA-8 blades
Diameter: not over 82 in., not under 80.5 in.
low 12.5, high 25.0
(c) Woodward governor 210065, 210105, 210155, 210345, or 210452,
or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1
Maximum structural cruising
(+39.5) to (+45.8) at 2550 lb.
(+35.0) to (+45.8) at 2050 lb. or less
Empty Wt. C.G. Range
122 m.p.h.
(106 knots)
(139 knots)
(160 knots)
( 87 knots)
4 (2 at +36, 2 at +70)
120 lb. (+95)
60 gal. (55 gal. usable); two 30 gal. tanks in wings at +48.
See NOTE 1 for data on unusable fuel
12 qt. (-15) (6 qt. usable)
See NOTE 1 for data on undrainable oil
Up 20 2
Adj. stabilizer
Up 1 50' 15
Up 25 1
(With stabilizer full down)
Right 24 1
Serial Nos. Eligible
Model 182: 613 and 33000 through 33842 (1956 Model)
8 20' 15'
22 50' 1
II - Model 182A, Skylane, 4 PCLM (Normal Category), Approved December 7, 1956
(c) Woodward governor 210065, 210105, 210155 or 210452,
(c) Woodward governor 210065, 210105, 210155, 210345, 210452,
(+40.0) to (+45.8) at 2650 lb.
(+33.5) to (+45.8) at 2100 lb. or less
II - Model 182A (contd)
65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48
Up 1 50' 15'
Model 182A: 33843 through 34753 (1957 Model)
Model 182A: 34755 through 34999 and 51001 through 51556 (1958 Model)
III - Model 182B, Skylane, 4 PCLM (Normal Category), Approved August 22, 1958
80 minimum octane aviation gasoline
(c) Woodward governor 210065, 210105, 210155, or 210340
(c) Woodward governor 210105AF, 210340, or 210451
III - Model 182B, Skylane
Up 20 +2
Up 1 50' +15'
Up 25 +1
8 20' +15'
22 50' +1
Model 182B: 34754, 51557 through 52358 except 51623 (1959 Model)
IV - Model 182C, Skylane, 4 PCLM (Normal Category), Approved July 8, 1959
Model 182D, Skylane, 4 PCLM (Normal Category), Approved June 14, 1960
Pitch settings at 30 in. sta.: low 12.5, high 25.0
IV - Model 182C, Model 182D (contd)
Up 0 45' +15'
(measured parallel to 0.0.W.L.)
Model 182C:
Model 182D:
Down 14 +2
8 45' +15'
Down 22 50' +1
631, 52359 through 53007 (1960 Model)
51623, 18253008 through 18253598 (1961 Model)
V - Model 182E, Skylane, 4 PCLM (Normal Category), Approved June 27, 1961
Model 182F, Skylane, 4 PCLM (Normal Category), Approved August 1, 1962
Model 182G, Skylane, 4 PCLM (Normal Category), Approved July 19, 1963
(Not eligible on O-470-R engine installation)
V - Model 182E, Model 182F, Model 182G (contd)
(+38.4) to (+47.4) at 2800 lb.
(+33.0) to (+47.4) at 2250 lb. or less
4 (2 at +36, 2 at +71)
120 lb. (+97)
65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48
Up 25 +2
Elevator (relative to stabilizer) Up 26 +1
Right 24 +1
Model 182E: 18253599 through 18254423 (1962 Model)
Model 182F: 18254424 through 18255058 (1963 Model)
Model 182G: 18255059 through 18255844 (1964 Model)
(111 knots)
(168 knots)
( 96 knots)
40 +1, -2
Down 15 +1
Down 15 +2
Down 17 +1
Left 24 +1
VI - Model 182H, Skylane, 4 PCLM (Normal Category), Approved September 17, 1964
Model 182J, Skylane, 4 PCLM (Normal Category), Approved October 20, 1965
Model 182K, Skylane, 4 PCLM (Normal Category), Approved August 3, 1966
Model 182L, Skylane, 4 PCLM (Normal Category), Approved July 28, 1967
1. McCauley constant speed
(a) Hub 2A34C66/90AT-8 blades
(b) Cessna spinner 0752637
2. Aircraft reworked per Cessna Service Kit SK182-121:
Elevator(relative to stabilizer)
Up 26 +1
VI - Model 182H, Model 182J, Model 182K, Model 182L (contd)
Model 182H:
Model 182J:
Model 182K:
Model 182L:
634, 18255846 through 18256684 (1965 Model)
18256685 through 18257625 (1966 Model)
18255845, 18257626 through 18257698, 18257700 through 18258505
18258506 through 18259305 (1968 Model)
VII - Model 182M, Skylane, 4 PCLM (Normal Category), Approved September 19, 1968
(a) Hub 2A34C201/90DA-8 blades
low 13, high 24.5
3. McCauley constant speed
low 12.5, high 25
VII - Model 182M
Model 182M: 18257699, 18259306 through 18260055 (1969 Model)
VIII - Model 182N, Skylane, 4 PCLM (Normal Category), Approved September 17, 1969
Continental O-470-S (See NOTE 4)
(c) Woodward governor 210065, 210105, 210155, 210345, or A210452,
or Garwin 34-828-01-2A, or McCauley C290D2/T1 or C290D3/T1
(+39.9) to (+47.4) at 2950 lb.
2950 lb. takeoff only, 2800 lb. landing
131 m.p.h.
198 m.p.h.
(114 knots)
(172 knots)
VIII - Model 182N
4 Front standard (2 at +36 to +49)
Optional (2 at +32 to +44)
Rear (2 at +74)
120 lb. (+97) (S/N 18260056 through 18260445)
120 lb. (+97) and 80 lb. (+117) (S/N 18260446 and up)
Elevator(rel. to stabilizer)
Rudder (parallel to 0.00 W.L.) Right
(Perpendicular to hinge line) Right
Model 182N: 18260056 through 18260445 (1970 Model) 18260446 through 18260825
27 13' +1
IX - Model 182P, Skylane, 4 PCLM (Normal Category), Approved October 8, 1971
Continental O-470-R, Aircraft S/N 18260826 through 18263475
Continental O-470-S, Aircraft S/N 18260826 and up (See NOTE 4)
IX - Model 182P (contd)
(S/N 675, 18260826 through 18264295)
(See NOTE 5 on use of IAS)
(S/N 18264296 through 18265175)
(+39.5) to (+48.5) at 2950 lb.
(+33.0) to (+48.5) at 2250 lb. or less
4 (2 front at +32.0 to +50.0)
(2 rear at +74)
Serial Numbers 18260826 through 18263475
200 lb. (120 lb. at + 82.0 to +108.0)
(80 lb. at +108.0 to +124.0)
Serial Numbers 675 and 18263476 through 18265175
(80 lb. at +108.0 to +136.0)
(S/N 675, 18260826 through 18262250)
Standard Range Tanks:
84 gal. (79 gal. usable); two 42.0 gal. tanks in wings at +48
(S/N 18262251 through 18265175)
61 gal. (56 gal. usable); two 29 gal. tanks in wings at +48
80 gal. (75 gal. usable); two 37 gal. tanks in wings at +48
(109 knots)
Elevator (rel. to stabilizer)
Rudder(parallel to 0.00 W.L.)
(perpendicular to hinge line)
Model 182P:
18260826 through 18261425 (1972 Model)
18261426 through 18262465 (1973 Model)
18262466 through 18263475 (1974 Model)
675, 18263476 through 18264295 except 18263479 (1975 Model)
18264296 through 18265175 (1976 Model)
X - Model 182Q, Skylane, 4 PCLM (Normal Category), Approved July 28, 1976
100/130 minimum aviation grade gasoline (S/N 18265176 through 18265965)
100LL/100 aviation grade gasoline (S/N 18265966 through 18267715)
For all operations, 2400 r.p.m. (230 hp.)
(a) Hub C2A34C204/90DCB-8 blades
low 15, high 29.4
(c) McCauley governor C290D3/T14
200 lb. (120 lb. at +82.0 to +108.0)
61 gal. (56 gal. usable); two 30.5 gal. tanks in wings at +48
(S/N 18263479, 18265176 through 18266590)
80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48
92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wings at +46.5
(S/N 18266591 through 18267715)
12 qt. (-15.0) (6 qt. usable)
Rudder (parallel to 0.00 W.L.)
X - Model 182Q
Model 182Q:
18265176 through 18265965
18263479, 18265966 through 18266590
18266591 through 18267300
18267301 through 18267715, except 18267302
XI - Model R182, Skylane RG, 4 PCLM (Normal Category), Approved July 7, 1977
Model TR182, Turbo Skylane RG, 4 PCLM (Normal Category), Approved September 12, 1978
Model R182
Lycoming O-540-J3C5D, rated at 235 hp.
100LL/100 aviation grade gasoline
Full throttle for all operations, 2400 r.p.m.
McCauley constant speed (S/N R18200002 through R18201313)
(a) Hub B2D34C214/90DHB-8 blades
low 15.8, high 29.4
(b) Cessna prop & spinner installation 2250003
Cessna spinner installation 1750050
(c) McCauley governor C290D3/T16
(d) McCauley governor DC290D1/T4
McCauley constant speed (S/N R18201314 and on)
(a) Hub B2D34C218/90DHB-8 blades
(b) Cessna prop & spinner installation 2250124
Cessna spinner installation 2250123
(c) McCauley governor C290D3/T22
(d) McCauley governor DC290D1/T8
McCauley constant speed (S/N R18201629 through R18202041 and aircraft
reworked per SK182-71)
(a) Hub B3D32C407/82NDA-3 blades
Diameter: not over 79 in., not under 78 in.
low 16.0, high 31.7
(b) Cessna prop & spinner installation 2252076
Cessna spinner installation 2252074
Lycoming O-540-L3C5D, rated at 235 hp.
(Turbocharged in accordance with Cessna Drawing No. 2250065)
For all operations, 2400 r.p.m., 31 in. hg. mp.
McCauley constant speed (S/N R18200001, R18200584 through R18201313)
(a) Hub B2D34C217/90DHB-8 blades
low 15.8, high 31.9
(c) McCauley governor C290D3/T21
(d) McCauley governor DC290D1/T7
XI - Model R182, Model TR182 (contd)
Model TR182 (contd)
Models R182, TR182
(a) Hub B2D34C219/90DHB-8 blades
McCauley constant speed (S/N R18201315, R18201629 and on and
aircraft reworked per SK182-71 or SK182-72)
1978 Model R182 Maneuvering
1979 Model R182 Maneuvering
Model TR182 Maneuvering
1980 and up Model R182 Maneuvering
159 knots
(a) S/N R18200001 through R18201628 except R18200975 & R18201315
(+40.9) to (+47.0) at 3100 lb.
(+35.5) to (+47.0) at 2700 lb.
(+33.0) to (+47.0) at 2250 lb. or less
Moment change due to retracting gear (+3052 in.-lb.)
(b) S/N R18200975, R18201315, R18201629 through R18202041
(+40.9) to (+46.0) at 3100 lb.
(+35.5) to (+46.0) at 2700 lb.
(+33.0) to (+46.0) at 2250 lb. or less
(2 rear at +74.0)
200 lb. (120 lb. at +82.0 to +110.0)
( 80 lb. at +110.0 to +134.0)
(a) S/N R18200002 through R18200583
(b) S/N R18200001, R18200584 through R18202041
92 gal. (88 gal. usable); two 46.0 gal. integral tanks
in wings at +46.5
9 qt. (-14.8)
See NOTE 1 for data on oil
Down 40 +1, -2
Elevator (rel. to
Up 28 +1
Right 27 13' +1
Left 27 13' +1
(b) S/N R18200975, R18201629 through R18201798
Up 24 +2
Down 21 +1
Right 24 +0, -1
Left 24 +0, -1
Right 27 13' +0, -1 Left 27 13' +0, -1
(c) S/N R18201315, R18201799 through R18202041
Up 20 +1
Right 27 13' +0, -1 Left
Model R182:
R18200002 through R18200583
Model R182/TR182: R18200001, R18200584 through R18201313
Model R182/TR182: R18201314 through R18201628
except R18201315
Model R182/TR182: R18201629 through R18201798
Model R182/TR182: R18201799 through R18201928
Model R182/TR182: R18201929 through R18201973
Model R182/TR182: R18201974 through R18201999
Model R182/TR182: R18201315, R18202000 through R18202031
Model R182/TR182: R18202032 through R18202041
38 +0, -1
24 +0, -1
27 13' +0, -1
XII - Model 182R, 4 PCLM (Normal Category), Approved August 29, 1980
Model T182, 4 PCLM (Normal Category), Approved August 15, 1980
(a) Hub C2A34C204/90DCB-8
Lycoming 0-540-L3C5D, rated at 235 hp.
(a) Hub B2D34C219/90DHB-8
(b) Cessna spinner 2250124
(a) Hub B3D32C407/82NDA-3
(b) Cessna spinner 2252076
Model 182R Maneuvering
Model T182 Maneuvering
3100 lb. takeoff/flight
2950 lb. landing
XII - Model 182R, Model T182 (contd)
Model T182 (contd)
200 lb. (120 lb. at +92.0 to +108.0)
92 gal. (88 gal. usable); two 46 gal. integral tanks in wings at +46.5
12 qt. (-15.0)
(6 qt. usable)
(through S/N 18268055)
12 qt. (-14.1)
(S/N 18268056 and on)
(a) S/N 18267716 through 18268055
Rudder (parallel to
0.00 W.L.)
hinge line)
9 qt (-14.8)
(b) S/N 18268056 through 18268586
182R/T182:
182R:
18267302,
18268294
18268369
18267716 through 18268055
through 18268293
through 18268368
through 18268434
through 18268541
through 18268586
24 +1, -0
Data Pertinent to Model Items I through XII
Front face of firewall
Upper door sill. Top surface centerline of tailcone (S/N 18253599 through 18265965)
Jig located nutplates and screws on left of tailcone (S/N 18263479, 18265966 through
18268586) (S/N R18200001 through 18202041)
Data Pertinent to Model Items I through XII (contd)
Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through
3-12 and Paragraph 3.112 as amended October 1, 1959, for the Model 182E and on. In
addition, effective S/N 18266591 through 18268586, FAR 23.1559 effective March 1,
1978. FAR 36 dated December 1, 1969, plus Amendments 36-1 through 36-6 for Model
182Q and on. In addition, effective S/N 18268435 through 18268586, FAR 23.1545(a)
Amendment 23-23 dated December 1, 1978.
3-12 and Paragraph 3.112 as amended October 1, 1959; and Sections 23.901, 23.909,
23.1041, 23.1043, 23.1143, and 23.1305 of the Federal Aviation Regulations dated
February 1, 1965, as amended February 14, 1975; FAR 23.1559 effective March 1, 1978;
FAR 36 dated December 1, 1969, plus Amendments 36-1 through 36-10. In addition,
effective S/N 18268435 through 18268541, FAR 23.1545(a) Amendment 23-23 dated
3-12 and Paragraph 3.112 as amended October 1, 1959; and Sections 23.729, 23.777(e),
23.781, 23.1555(e)(1) and (2), and 23.1563 of the Federal Aviation Regulations dated
February 1, 1965, as amended February 14, 1975. In addition, effective
S/N R18200001, R18200584 and up, FAR 23.1559 effective March 1, 1978. FAR 36
dated December 1, 1969, plus Amendments 36-1 through 36-6. In addition, effective
S/N R18202000 through R18202041, FAR 23.1545(a) Amendment 23-23 dated
3-12 and Paragraph 3.112 as amended October 1, 1969; and Sections 23.729, 23.777(e),
23.781, 23.901, 23.909, 23.1041, 23.1043, 23.1143, 23.1305, 23.1555(e)(1) and (2), and
23.1563 of the Federal Aviation Regulations dated February 1, 1965, as amended
February 14, 1975; FAR 23.1559 effective March 1, 1978; FAR 36 dated December 1,
1969, plus Amendments 36-1 through 36-9. In addition, effective S/N R18202000
through R18202041, FAR 23.1545(a) Amendment 23-23 dated December 1, 1978.
Application for Type Certificate dated July 11, 1955.
Type Certificate No. 3A13 issued March 2, 1956, obtained by the
manufacturer under delegation option procedures.
S/N 18263479, 18264296 through 18267715
CAR 3.757 (See NOTE 5 on use of IAS)
CAR 3.778(a)
S/N 18267716 through 18268586
(S/N 18267716 through 18268434)
CAR 3.430
S/N R18200001 through R18202041
(S/N R18200001 through R18201999)
Production Certificate No. 4. Delegation Option Manufacturer No. CE-1 authorized to
issue airworthiness certificates under delegation option provisions of Part 21 of the
The basic required equipment as prescribed in the applicable airworthiness
requirements (see Certification Basis) must be installed in the aircraft for certification.
This equipment must include a current Airplane Flight Manual effective S/N 18266591
through 18268586 and R18200584 through R18202041. In addition, the following item
of equipment is required:
1. Stall warning indicator, Cessna Dwg. S1672-5.
The equipment portion of Aircraft Specification 3A13, Revision 15, or Cessna
Publication TS3000-13 should be used for equipment references on all aircraft prior to
the Model 182G. Refer to the applicable Equipment List for the Model 182G and
Current weight and balance report including list of equipment included in certificated empty weight, and
loading instructions when necessary must be provided for each aircraft at the time of original certification.
613 and 33000 through 34999
631 and 51001 through 53007
18253008 through 18264295 except 18263479
The certificated empty weight and corresponding center of gravity location must include unusable fuel of
30 lb. (+46) on Models 182, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N and 182P through
18264295 and 60 lb. (+46) on Models 182A, 182B, 182C and 182D and undrainable oil of 0 lb.
Serial Numbers 18263479, 18264296 through 18266590
30 lb. (+46) and full oil of 22.5 lb. at (-15.0).
Serial Numbers 18266591 through 18268055
24 lb. at (+48) and full oil of 22.5 lb. at (-15.0) for the 182Q, 182R Model, and include oil of 16.9 lb. at
(-14.8) for the T182 Model.
Serial Numbers 18268056 through 18268586
24 lb. at (+48) and full oil of 24.4 lb. at (-14.1) for the 182R, and include oil of 16.9 lb. at (-14.8) for the
Serial Numbers R18200002 through R18200583
30 lb. (+46) and include oil of 16.9 lb. (-15.7).
Serial Numbers R18200001, R18200584 through R18202041
24 lb. (+48) and include oil of 16.9 lb. (-14.8).
The following placards must be displayed in locations as indicated:
Applicable to Model 182 only:
(1) In full view of the pilot:
(a) "This airplane must be operated as a normal category airplane in compliance with operating
limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers
including spins approved.
Flight Maneuvering Load Factors
+3.8 -1.52
Maximum design weight 2550 lb.
Reference weight and balance data for loading instructions."
(b) "Both tanks on for takeoff and landing."
(c) "Flaps - Pull to extend
1st Notch 10
2nd Notch 20
3rd Notch 30
4th Notch 40
(2) In baggage compartment
"Maximum baggage 120 lb. For additional loading instructions see weight and balance data."
Applicable to Models 182A, 182B, 182C and 182D
Maximum design weight 2650 lb.
4th Notch 40"
Applicable to Models 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M
Flaps Down +3.5
Maximum design weight 2800 lb.
(2) On the fuel selector valve plate:
"Both off. Left tank level flight only 31 gal. Both on for landing and takeoff all flight attitudes
60 gal. Right tank level flight only 31 gal."
(3) On the control lock:
"Control lock - Remove before starting engine."
(4) On the baggage door:
"120 lb. maximum baggage and/or auxiliary seat passengers. For additional loading instructions,
see weight and balance data."
NOTE 2. (contd)
Applicable to Models 182N:
(a) Serial Numbers 18260056 through 18260445
"This airplane must be operated as a normal category airplane in compliance with the
operating limitations as stated in the form of placards, markings and manuals.
2950 lb. takeoff
Alt. loss in stall recovery-160 ft.
2800 lb. landing
131 m.p.h.-CAS
Flaps up +3.8, -1.52, Flaps down +3.5
Reference weight and balance data for loading instructions"
(b) Serial Numbers 182670446 through 18260825
131 m.p.h. CAS (114 knots)
Takeoff 2950 lb.
Landing 2800 lb.
+3.8, -1.52
No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery 160 ft.
Known icing conditions to be avoided. This airplane is certified for the following flight
operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR"
"Both off. Left tank level flight only 31 gal. Both on for landing and takeoff all flight attitudes,
(a) "120 lb. maximum baggage and/or auxiliary seat passengers. For additional loading
instructions, see weight and balance data."
Applicable to Models 182N, S/N 18260056 through 18260445.
(b) "120 lb. maximum baggage and/or auxiliary passenger forward of baggage door latch, and
80 pounds maximum baggage aft of baggage door latch. Maximum 200 lb. combined. For
additional loading instructions see weight and balance data." Applicable to Models 182N,
S/N 18260446 and up.
(5) On flap control indicator:
(a) "0 to 20 - T.O."
(b) "10 - 20 - Full.
(Indices at these positions with blue color code and 160 m.p.h. callout, and white color code with
110 m.p.h. callout; mechanical detent at 10 and 20)"
Applicable to Models 182P:
126 m.p.h. CAS (109 knots)
operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR."
(b) "This airplane must be operated as a normal category airplane in compliance with the
Maneuvering speed (IAS)
Flight into known icing conditions prohibited. This airplane is certified for the following
flight operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR"
(2) On the fuel selector valve plate: (S/N 675, 18260826 through 18262250)
Standard range tanks: "Off. Left tank level flight only 31 gal. Both on for landing and takeoff
all flight attitudes, 60 gal. Right tank level flight only 31 gal."
"Off. Left tank level flight only 39 gal. Both on for landing and takeoff
all flight attitudes, 79 gal. Right tank level flight only 39 gal."
On the fuel selector valve plate: (S/N 182622251 through 18265175)
Standard range tanks: "Off. Left tank level flight only 29 gal. Both on for landing and takeoff
all flight attitudes, 56 gal. Right tank level flight only 29 gal."
"Off. Left tank level flight only 37 gal. Both on for landing and takeoff
all flight attitudes, 75 gal. Right tank level flight only 37 gal."
(3) On the control lock: "Control lock - remove before starting engine."
(4) On the baggage door: (S/N 18260826 through 18263475)
"120 lb. maximum baggage and/or auxiliary passenger forward of baggage door latch, and 80 lb.
maximum baggage aft of baggage door latch. Maximum 200 lb. combined. For additional
loading instructions, see weight and balance data."
On the baggage door: (S/N 675, 18263476 through 18265175)
"Forward of baggage door latch, 120 lb. maximum baggage and/or auxiliary passenger.
Aft of baggage door latch, 80 lb. maximum baggage including 25 lb. maximum in baggage wall
hat shelf. Maximum 200 lb. combined. For additional loading instructions see weight and
balance data."
Applicable to Models 182P: (contd)
(5) On flap control indicator: (S/N 675, 18260826 through 18264295)
"(a) 0 to 10 (Blue color code and 160 m.p.h. callout;
also, mechanical detent at 10)
(b) 10 to 20Full (Indices at these positions with white color code and
110 m.p.h. callout; also, mechanical detent at 10 and 20)"
On flap control indicator (S/N 18264296 through 18265175)
"(a) 0 to 10 (Blue color code and 140 KTS callout;
95 KTS callout; also, mechanical detent at 10 and 20)"
(6) Forward of the filler cap on the wing surface: (S/N 675, 18260826 through 18262250)
"Service this airplane with 80/87 minimum aviation grade gasoline.
Capacity 32.5 gal."
Capacity 42.0 gal."
Forward of the filler cap on the wing surface: (S/N 18262251 through 18265175)
Capacity 30.5 gal."
Capacity 40.0 gal."
(7) On aft panel of baggage compartment:
"Oxygen refill." (All models with oxygen)
(8) Adjacent to overvoltage light:
(9) Above the left fuel gauge:
"Do not turn off alternator in flight except in emergency."
(Model 182P, S/N 18260826 through 18261425)
Applicable to Models 182Q:
(a) S/N 18263479, 18265176 through 18266590
flight operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR."
S/N 18266591 through 18267715
"The markings and placards installed in this airplane contain operating limitations which
must be complied with when operating this airplane in the Normal Category. Other operating
limitations which must be complied with when operating this airplane in this category are
contained in the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.
No acrobatic maneuvers, including spins, approved. Flight into known icing conditions
prohibited. This airplane is certified for the following flight operations as of date of original
airworthiness certificate: DAY-NIGHT-VFR-IFR." (as applicable)
Applicable to Models 182Q: (contd)
(1) (b) Near airspeed indicator:
"Maneuver Speed
111 KIAS"
S/N 18263479, 18265176 through 18266590
Standard range tanks: "Off.
Left - 29 gal. Level flight only.
Both - 56 gal. All flight attitudes.
Both on for takeoff and landing.
Right - 29 gal. Level flight only."
Long range tanks: "Off.
Left - 37 gal. Level flight only.
Both - 75 gal. All flight attitudes.
Right - 37 gal. Level flight only."
"Take Off - Both - Landing,
All Flight - 88.0 Gal. - Attitudes
Left - 44.0 Gal. Level Flight Only
Right - 44.0 Gal. Level Flight Only
"Forward of baggage door latch, 120 pounds maximum baggage and/or
auxiliary passenger. Aft of baggage door latch, 80 pounds maximum
baggage including 25 pounds maximum in baggage wall hat shelf.
Maximum 200 pounds combined. For additional loading instructions,
"0 to 10 (Blue color code and 140 KTS callout;
also, mechanical detent at 10)"
"0 to 20 Full (Indices at these positions with white color code and 95 KTS
callout; also, mechanical detent at 10 and 20)"
(6) Forward of the filler cap on the wing surface:
S/N 18265176 through 18265965
Standard range tanks: "Service this airplane with 100/130 minimum aviation
grade gasoline. Capacity 30.5 gal."
"Service this airplane with 100/130 minimum aviation
grade gasoline. Capacity 40.0 gal."
S/N 18263479, 18265966 through 18266590
Standard range tanks: "Service this airplane with 100LL/100 aviation
"Service this airplane with 100LL/100 aviation grade
gasoline. Capacity 40.0 gal."
"Fuel 100LL/100 minimum grade aviation gasoline.
Capacity 46 U.S. gal. Capacity 34.5 U.S. gal.
to bottom of filler collar."
G. Applicable to Models R182 and TR182, S/N R18200001 through R18201928:
No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery 240 ft.
must be complied with when operating this airplane in the Normal Category. Other
operating limitations which must be complied with when operating this airplane in this
category are contained in the Pilot's Operating Handbook and FAA Approved Airplane Flight
(c) Near Airspeed Indicator:
"MAX SPEED - KIAS
Gear Oper
G. Applicable to Models R182 and TR182, S/N R18200001 through R18201928: (contd)
(2) (b) S/N R18200001, R18200584 through R18201798
(c) S/N R18201799 through R18202041
"Both - 88.0 Gal. - Take Off - Landing - All Flight
Attitudes; Left - 44.0 Gal. - Level Flight Only
Right - 44.0 Gal. - Level Flight Only
Off - Off."
(a) S/N R18200001 through R18201798
(b) S/N R18201799 through R18202041
"Caution! Control Lock - Remove before starting engine."
"120 Pounds Maximum
Baggage And/Or Auxiliary Passenger
Forward of Baggage Door Latch And
Baggage Aft of Baggage Door Latch
Maximum 200 Pounds Combined
For Additional Loading Instructions See Weight and Balance Data"
(5) On the flap control indicator:
"0 to 10 - (Blue color code and 140 KTS callout;
"0 to 20 - Full (Indices at these positions with white color code and 95 KTS
Standard range tanks: "Service this airplane with 100LL/100 aviation grade gasoline.
"Service this airplane with 100LL/100 aviation grade gasoline.
Fuel 100LL/100 minimum grade aviation gasoline.
Capacity 46 U.S. gal. Capacity 34.5 U.S. gal. to
bottom of filler collar."
(7) Adjacent to overvoltage light:
(8) Near gear hand pump:
"Manual Gear Extension
1. Select Gear Down
2. Pull Handle Fwd.
3. Pump Vertically
Do Not Pump With Gear
Up Selected"
(9) Forward of each fuel filler cap:
"Fuel Cap Forward - Arrow Alignment, Cap Must Not Rotate During Closing."
H. Applicable to Models 182R and T182, S/N 18267302, 18267716 through 18268293:
(a) "The markings and placards installed in this airplane contain operating limitations which
airworthiness certificate: DAY-NIGHT-VFR-IFR." (as applicable).
(b) Near airspeed indicator:
"Take Off - Both - Landing, All Flight - 88.0 Gal. - Attitudes
"Both - 88.0 Gal. - Takeoff - Landing - All Flight Attitudes
Left - 44.0 Gal. - Level Flight Only
(4) On baggage door:
Forward of Baggage Door Latch and 80 Pounds Maximum
H. Applicable to Models 182R and T182, S/N 18267302, 18267716 through 18268293: (contd)
calout; also mechanical detent at 10 and 20)"
"Fuel 100LL/100 minimum grade aviation gasoline. Capacity 46 U.S. gal.
Capacity 34.5 U.S. gal. to bottom of filler collar."
(7) Forward of each fuel filler cap:
"Fuel cap fwd - arrow alignment, cap must not rotate during closing."
Applicable to Models R182 and TR182, S/N R18201929 through R18202041:
All placards required in the Pilot's Operating Handbook and FAA Approved Airplane
Flight Manual must be installed in the appropriate locations.
Applicable to Models 182R and T182, S/N 18268294 through 18268586:
The cylinder head thermistors must be installed as follows:
Engine and Cylinder Head Number
O-470-R O-470-S
O-470-U O-540-J
182N (1970 and 1971 Model)
182P (1972 and 1973 Model)
182P (1974 Model)
182P (1975 and 1976 Model)
182Q (1977 through 1980 Model)
182R (1981 Model through 18268160)
182R (18268161 through 18268586)
T182 (1981 Model through 1985 Model)
R182 (1978 and 1979 Model)
R182 (1980 Model through 1986 Model)
TR182 (1979 Model)
TR182 (1980 Model through 1986 Model) N/A
O-540-L
The installation of the 0-470-S engine in Model 182N and Model 182P (1970 through 1974) will require a
change of the oil temperature gauge. Reference Cessna Service Letter SE75-2 for information and
instructions for this change.
The marking of the airspeed indicator with IAS provides an equivalent level of safety to CAR 3.757 when
the approved airspeed calibration data presented in Section V of the Pilot's Operating Handbooks listed
below is available to the pilot:
182P, Cessna P/N D1062-13
182Q, Cessna P/N D1087-13
182Q, Cessna P/N D1114-13
182Q, Cessna P/N D1141-13PH
182Q, Cessna P/N D1176-13PH
182R, Cessna P/N D1196-13PH
182R, Cessna P/N D1215-13PH
182R, Cessna P/N D1233-13PH
182R, Cessna P/N D1254-13PH
(S/N 18265176 through 18265965)
(S/N 18263479, 18265966 through 18266590)
(S/N 18266591 through 18267300)
(S/N 18267301 through 18267715)
(S/N 18267716 through 18268055)
(S/N 18268056 through 18268293)
(S/N 18268294 through 18268368)
(S/N 18268369 through 18268434)
NOTE 5. (contd)
T182, Cessna P/N D1197-13PH
T182, Cessna P/N D1216-13PH
T182, Cessna P/N D1234-13PH
T182, Cessna P/N D1234R1-13PH
T182, Cessna P/N D1255-13PH
R182, Cessna P/N D1115-13
R182, Cessna P/N D1142-13PH
R182, Cessna P/N D1177-13PH
R182, Cessna P/N D1198-13PH
R182, Cessna P/N D1217-13PH
R182, Cessna P/N D1235-13PH
R182, Cessna P/N D1256-13PH
R182, Cessna P/N D1277-13PH
R182, Cessna P/N D1299-13PH
TR182, Cessna P/N D1143-13PH
TR182, Cessna P/N D1143-2-13PH
TR182, Cessna P/N D1178-13PH
TR182, Cessna P/N D1199-13PH
TR182, Cessna P/N D1218-13PH
TR182, Cessna P/N D1236-13PH
TR182, Cessna P/N D1257-13PH
TR182, Cessna P/N D1278-13PH
TR182, Cessna P/N D1300-13PH
(S/N 18267302, 18267716 through 18268055)
(Special) (S/N 18268365)
(S/N R18200002 through R18200583)
(S/N R18200584 through R18201313)
(S/N R18201314 through R18201628)
(S/N R18201629 through R18201798)
(S/N R18201799 through R18201928)
(S/N R18201929 through R18201973)
(S/N R18201974 through R18201999)
(S/N R18202000 through R18202031)
(S/N R18202032 through R18202041)
(S/N R18200001, R18200584 through R18201313
except R18200975)
(Special) (S/N R18200975)
(S/N R18201314 through R18201628 except R18201315)
(S/N R18201315, R18202000 through R18202031)
(182 series through S/N 18265965 except 18263479)
(182 series S/N 18263479, 18265966 through 18268586)
(R182 and TR182 series S/N R18200001 through R18202041)
Special Ferry Flight Authorization. Flight Standards District Offices are authorized to issue Special
overweight ferry flight authorizations. These airplanes are structurally satisfactory for ferry flight if
maintained within the following limits: (1) Takeoff weight must not exceed 130% of the maximum weight
for Normal Category; and (2) The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed
(VC) must be reduced by 30%; and (3) Forward and aft center of gravity limits may not be exceeded; and (4)
Structural load factors of +2.5 g. to -1.0 g. may not be exceeded. Requirements for any additional engine oil
should be established in accordance with Advisory Circular AC23.1011-1. Increased stall speeds and
reduced climb performance should be expected for the increased weights. Flight characteristics and
performance at the increased weights have not been evaluated. Procedures for issuing a Flight Permit for
operations of overweight aircraft may be found in Advisory Circular AC21-4B
In addition to the above specified placards, the prescribed operating limitations indicated by an asterisk (*) under
Sections I through XII must also be displayed by permanent markings.
XIII - Model 182S, Skylane, 4 PCLM (Normal Category), Approved 03 October 1996.
Model 182T, Skylane, 4 PCLM (Normal Category), Approved 23 February 2001.
Lycoming IO-540-AB1A5. Rated 230 Horsepower
For all operations, 2400 RPM
XIII - Model 182S, Model 182T (contd)
(1) McCauley Constant Speed (182S)
(a) Propeller: B2D34C235/90DKB-8 (2 blades)
Pitch settings at 30 in. sta.: Low 17.0, High 31.8
(b) McCauley Spinner: D-7267-2
(c) McCauley Governor: DC290D1/T8
(2) McCauley Constant Speed (182S, 182T)
(a) Propeller: B3D36C431/80VSA-1 (3 blades)
Diameter: not over 79 in., not under 77.5 in.
Pitch settings at 30 in. sta.: Low 14.9, High 31.7
(b) McCauley Spinner: D-7261-2
Static RPM at full throttle: Not over 2400; Not Under 2300
Airspeed Limits (182S):
Max Structural Cruising
Airspeed Limits (182T):
C.G. Range (182S):
C.G. Range (182T):
(1) Aft Limits:
(2) Forward Limits:
(1) Aft Limits
(2) Forward Limits
110 Knots IAS
140 Knots IAS
175 Knots IAS
100 Knots IAS
(108 Knots CAS)
(138 Knots CAS)
(170 Knots CAS)
( 99 Knots CAS)
(136 Knots CAS)
(171 Knots CAS)
46.0 inches aft of datum at 3100 lbs. or less.
Linear variation from 40.9 inches aft of datum at 3100
pounds to 33.0 inches aft of datum at 2250 lbs.; 33.0
inches aft of datum at 2250 lbs. or less.
46.0 inches aft of datum at 3,100 pounds or less.
Linear variation from 40.9 inches aft of datum at 3,100
pounds, to 35.5 inches aft of datum at 2,700 pounds, to
33.0 inches aft of datum at 2,250 pounds; 33.0 inches aft
of datum at 2,250 pounds or less.
Lower portion of front face of firewall
58.8 inches; Leading edge of MAC 25.98 inches aft of datum
Left side of Tailcone at 139.65 inches and 171.65 inches aft of datum
Maximum Weights (see Note 5)
3,110 pounds
4 (2 at 32.0 to 50.0 inches aft of datum; 2 at 74.0 inches aft of datum)
120 pounds at 82.0 to 109.0 inches aft of datum
80 pounds at 109.0 to 134.0 inches aft of datum
(Max. combined weight capacity for baggage areas is 200 pounds)
182S: 92 gallons total: 88 gallons usable
182T: 92 gallons total; 87 gallons usable
(Two 46 gallon tanks in wings at 46.5 inches aft of datum)
See NOTE 1 for data on usable fuel.
9.0 quarts at 14.8 inches forward of datum
5.0 quarts usable
(Relative to stabilizer)
Rudder: Right:
Left: 24 +0,-1
(Parallel to 0.00 W.L.)
2713 +0, -1 Left: 2713 +0,-1
182S: 18280001 through 18280944
182T: 18280945 and On
Data Pertinent to Model 182S and 182T
Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 23-6, except as
FAR 23.423; 23.611; 23.619; 23.623; 23.689; 23.775; 23.871; 23.1323; and 23.1563 as amended by Amendment 23-7.
FAR 23.807 and 23.1524 as amended by Amendment 23-10. FAR 23.507; 23.771; 23.853(a),(b) and (c); and 23.1365 as
amended by Amendment 23-14. FAR 23.951 as amended by Amendment 23-15. FAR 23.607; 23.675; 23.685; 23.733;
23.787; 23.1309 and 23.1322 as amended by Amendment 23-17. FAR 23.1301 as amended by Amendment 23-20. FAR
23.1353; and 23.1559 as amended by Amendment 23-21. FAR 23.603; 23.605; 23.613; 23.1329 and 23.1545 as amended
by Amendment 23-23. FAR 23.441 and 23.1549 as amended by Amendment 23-28. FAR 23.779 and 23.781 as amended
by Amendment 23-33. FAR 23.1; 23.51 and 23.561 as amended by Amendment 23-34. FAR 23.301; 23.331; 23.351;
23.427; 23.677; 23.701; 23.735; and 23.831 as amended by Amendment 23-42. FAR 23.961; 23.1093; 23.1143(g);
23.1147(b); 23.1303; 23.1357; 23.1361 and 23.1385 as amended by Amendment 23-43. FAR 23.562(a), 23.562(b)2,
23.562(c)1, 23.562(c)2, 23.562(c)3, and 23.562(c)4 as amended by Amendment 23-44. FAR 23.33; 23.53; 23.305; 23.321;
23.485; 23.621; 23.655 and 23.731 as amended by Amendment 23-45.
FAR 36 dated December 1, 1969, as amended by Amendments 36-1 through 36-21.
Equivalent Safety Items, 182S:
FAR 23.1093.
FAR 23.1143(g)
FAR 23.1147(b)
Date of Application for Amended Type Certificate was January 22, 1996.
Type Certificate No. 3A13 was amended October 3, 1996.
Equivalent Safety Items, 182T:
(1) Induction System Icing Protection
(3) Mixture Control
(4) Anti-collision Lights
(5) Aviation White Color Reqmt
FAR 23.1093; Refer to FAA letter dated 12/19/00
FAR 23.1143(g); Refer to FAA letter dated 12/19/00
FAR 23.1147(b); Refer to FAA letter dated 12/19/00
FAR 23.1401(d); Refer to FAA letter dated 2/20/01
14CFR 23.1397(c); Refer to ACE-07-11, FAA letter dated 11/29/07
Data Pertinent to Model 182S and 182T (contd)
Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only:
14 CFR 23.303; 23.307; 23.601; 23.1163(a)(1)(2); 23.1367 and 23.1381 as amended by Amendment 23-N/C. 14 CFR
23.1589 as amended by Amendment 23-13. 14 CFR 23.771(a) as amended by Amendment 23-14. 14 CFR 23.607 and
(Electrical System) 23.1309(a)(1)(2), (c) as amended by Amendment 23-17. 14 CFR 23.1301; 23.1327 and 23.1547(e) as
amended by Amendment 23-20. 14 CFR 23.1501 and 23.1541(a)(1), (a)(2), (b)(1), (b)(2) as amended by Amendment 2321. 14 CFR 23.603 and 23.605 as amended by Amendment 23-23. 14 CFR 23.1529 as amended by Amendment 23-26. 14
CFR 23.561(e); 23.1523; 23.1581(a)(2); 23.1583(a)(1), (a)(2), (b)(h) and 23.1585(a)(b)(d) as amended by Amendment 2334. 14 CFR 23.301 as amended by Amendment 23-42. 14 CFR 23.1322; 23.1331 and 23.1357(a)(b)(c)(d) as amended by
Amendment 23-43. 14 CFR 23.305; 23.773(a)(1), (a)(2); 23.1525 and 23.1549 as amended by Amendment 23-45. 14 CFR
23.1303(a)(b)(c)(f); 23.1309(a)(1)(i), (a)(1)(ii), (a)(2), (b)(1), (b)(2)(i), (b)(2)(ii), (b)(3), (b)(4)(i), (b)(4)(ii), (b)(4)(iii),
(b)(4)(iv), (c)(1), (c)(2)(iii), (c)(3), (d), (e), (f)(1); 23.1311; 23.1321(a)(c)(d)(e); 23.1323(a), (b)(1), (b)(2), (c);
23.1329(g)(h); 23.1351(a)(1), (a)(2)(i), (b)(1)(iii), (b)(2)(3), (c)(4), (d)(1); 23.1353(a)(b)(c)(d)(e); 23.1359(c); 23.1361;
23.1365(a)(b)(d)(e)(f) and 23.1431(a)(b)(d)(e) as amended by Amendment 23-49. 14 CFR 23.1325(a), (b)(1), (b)(2)(i),
(b)(3), (c)(d)(e); 23.1543(b)(c); 23.1545(a), (b)(1), (b)(2), (b)(3), (b)(4); 23.1553; 23.1555(a)(b); 23.1563(a) and 23.1567(a)
as amended by Amendment 23-50. 14 CFR 23.777(a)(b); 23.955(a)(2); 23.1337(a)(1), (a)(2), (b)(1), (c) as amended by
Amendment 23-51. 14 CFR 23.1305(a)(1), (a)(2), (a)(3), (b)(2), (b)(3)(i), (b)(4)(i), (b)(5), (b)(6)(i) as amended by
Amendment 23-52. 14 CFR 23.901(a)(b) as amended by Amendment 23-53.
Additions for the Garmin GFC-700 Automatic Flight Control System (AFCS) Only:
14 CFR 23.1335 as amended by Amendment 23-20, 14 CFR 23.1329 (a)(c)(d)(e)(f) as amended by Amendment 23-49.
No. 23-146-SC, Special Conditions: Cessna Aircraft Company; Cessna Model 182T/T182T Airplane; Installation of
Electronic Flight Instrument System and the Protection of the System From High Intensity Radiated Fields (HIRF).
Production Basis (Model 182S)
Production Certificate No. PC-4 issued June 30, 1997. Applies to airplane serial numbers 18280013, 18280016, 18280017,
18280019 and on. Airplane serial numbers not listed were produced under Type Certificate only. Cessna is authorized to issue
airworthiness certificates under the delegation provisions of Delegation Option Authorization No. CE-1 in accordance with Part
21 of the Federal Aviation Regulations.
Production Basis (Model 182T)
Production Certificate No. 4 issued March 8, 2001. Applies to airplane serial numbers 18280945 and on. Cessna is authorized
to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization
No. DOA-100129-CE in accordance with Part 21 of the Federal Aviation Regulations.
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed
in the airplane for certification.
Serial Nos. 18280001 Through 18280944; (Model 182S)
The certificated basic empty weight and corresponding center of gravity location must include unusable fuel
of 24 lbs. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum.
Serial Nos. 18280945 and On; (Model 182T)
of 30 lbs. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum.
FAA Approved Airplane Flight Manual (AFM): Part Number 182SPHUS00 (or later FAA approved
revisions) are applicable to the Model 182S. The Airplane must be operated according to the appropriate
AFM. Required placards are included in the AFM.
FAA Approved Airplane Flight Manual (AFM): Part number 182TPHUS00 (or later FAA approved revision)
is applicable to the Model 182T. The Airplane must be operated according to the appropriate AFM.
Required placards are included in the AFM.
FAA Approved Airplane Flight Manual (AFM): Part Number 182TPHAUS-00 (or later FAA approved
revisions) are applicable to the Model 182T equipped with Garmin G1000 Integrated Cockpit System. The
airplane must be operated according to the appropriate AFM. Required placards are included in the AFM.
FAA Approved Airplane Flight Manual (AFM): Part Number 182TPHBUS-00 (or later FAA approved
revisions) are applicable to the Model 182T equipped with Garmin G1000 Integrated Cockpit System and
Garmin GFC-700 AFCS. The airplane must be operated according to the appropriate AFM. Required
placards are included in the AFM.
The CHT probe must be installed on Head #1 (182S) or #3 (182T).
overweight ferry flight authorizations. This airplane is structurally satisfactory for ferry flight if maintained
within the following limits: (1) Takeoff weight must not exceed 130% of the maximum weight for Normal
Category; and (2) The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must
be reduced by 30%; and (3) Forward and aft center of gravity limits may not be exceeded; and (4) Structural
load factors of +2.5 g. to -1.0 g. may not be exceeded. Requirements for any additional engine oil should be
established in accordance with Advisory Circular AC23.1011-1. Increased stall speeds and reduced climb
performance should be expected for the increased weights. Flight characteristics and performance at the
increased weights have not been evaluated. Procedures for issuing a Flight Permit for operations of
overweight aircraft may be found in Advisory Circular AC21-4B
Model 182S airplane serial numbers 18280617 through 18280670 may differ structurally and are, therefore,
not eligible for any weight increases above the approved maximum takeoff weight limit of 3,100 pounds.
Any exceptions must first be coordinated with the Wichita Aircraft Certification Office. Exceptions to this
limitation have been inspected and found to comply with type data for the Model 182S, and include the
following serial number aircraft: 18280620.
XIV - Model T182T, Skylane, 4 PCLM (Normal Category), Approved 23 February 2001.
Lycoming TIO-540-AK1A. Rated 235 Horsepower
For all operations, 2,400 RPM
(a) McCauley Model B3D36C442/80VSB-1
Diameter: not over 79 inches; not under 77.5 inches
Pitch settings at 30 in. sta.: Low 15.1, High 35.4
Note: A low pitch setting of 15.3 is also acceptable for this model number prop.
(110 Knots CAS)
(137 Knots CAS)
(100 Knots CAS)
XIV - Model T182T (contd)
92 gallons total; 87 gallons usable
Oil Capacity (Qts.)
2713 +0, -1
T18208001 and On
Data Pertinent to Model T182T
FAR 36 dated December 1, 1969, as amended by Amendments 36-1 through 36-22.
Equivalent Level of Safety Items:
Aviation White Color Reqmt
FAR 23.1401(d); Refer to FAA letter dated 02/20/01
Production Basis (Model T182T)
Production Certificate No. 4 issued March 8, 2001. Applies to airplane serial numbers T18208001 and on. Cessna is authorized
to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. DOA-100129-CE in
accordance with Part 21 of the Federal Aviation Regulations.
Serial Nos. T18208001 and On (Model T182T)
30 lbs. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum.
Pilots Operating Handbook and FAA Approved Airplane Flight Manual (AFM): part number
T182TPHUS00 (or later approved revision) is applicable to Model T182T. The airplane must be operated
according to the appropriate POH/AFM. Required placards are included in the AFM.
FAA Approved Airplane Flight Manual (AFM): Part Number T182TPHAUS-00 (or later FAA approved
FAA Approved Airplane Flight Manual (AFM): Part Number T182TPHBUS-00 (or later FAA approved
revisions) are applicable to the Model T182T equipped with Garmin G1000 Integrated Cockpit System and
The CHT probe must be installed on Head #4.
overweight aircraft may be found in Advisory Circular AC21-4B.
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EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte19
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte20
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte15
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte17
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte16
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte10
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte14
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte13
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte9
EC-155B1 Complimentary Flight Manual - Section 7 Description and Systems Parte12
Designing Effective Static Tests for Spacecraft Structures - Sarafin (Ler)_Part9
Designing Effective Static Tests for Spacecraft Structures - Sarafin (Ler)_Part5
Structural Assy Central Fus 12
Structural Assy Central Fus 13
Structural Assy Central Fus 14
Structural Assy Central Fus 15
Structural Assy Central Fus 10
Structural Assy Central Fus 8
Structural Assy Central Fus 7
Structural Assy Central Fus 16
Structural Assy Central Fus 9
Popular in Constant Speed Propeller
139-0000-R14-WA
EASA Module 17 qtn