Piper Malibu PA-46-310P Pilot Operating Handbook page 209

FAA APPROVED
MAKE
Boeing
26. Cessna
27. Cessna
28. Cessna
29.
Cessna
30. Cessna
Cessna
Cessna
Cessna
31 . Cessna
Cessna
32. Cessna
Cessna
33. Cessna
34. Cessna
35. Cessna
36. Cessna
37.
Cessna
36. Cessna
39. Cessna
40. Cessna
41. Cessna
42. Cessna
43. Cessna
44. Cessna
45. Cessna
46. Cessna
47.
Cessna
46. Cessna
MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM
SHEET 4
AIRCRAFT MODEL
Part Nu mber
T.C.D.S. (See P. 9 for Series)
875. E75. A75. A75L300.
1875A, E75N1 A75J1. A75N1, 875N1. 075N1 A-743 (7),(C)
140 3A43
(4), (A)
120 • 140. with 0-200 Conversion per STC-SA54 7EA A-768 (4), (A)
140A. with 0-200 Conversion per STC-SA547EA A-5A2 (4), (Al
•
150,A,B.C.O.E,F.G,H.J.K
3A19 (4),(A,
A150K. 150L. A150L. 150M.
A150M, 152, A 152
170. 170A. 1708
A-799 (6). {B)
172.172A,B.C.O.E,F ,G.H, 3A12 (6). (B)
1721,K.L,M.N,P,Q ,R,S.T 3A12 (4).(A)
172RG, P1720 3A17 (4).(A)
R172E,F,G,H,J.K, 175,175A,B,C 3A17 (6l. {Bl
177,177A, 1778 A13CE {4), {A)
177RG A20CE (4).{A)
180.180A,B.C.O,E.F,G.H,J,K 5A6 (6), (B)
182, 182A,B,C.O,E.F.G.H,J.K. 162L,M,N,P,O.R. S, T R162, 3A13 (6), (B)
T1 62. TR162 , 162RS, T162T,
162 Series STC SA00152WI 3A13 (6l, (Bl
182E,F,G,H,J,K, L, M. N, P. Q(Peterson,STC SA3825SW} 3A13 (6), (B)
165. 165A,B,C,O.E,A 165E,A 165F
3A24 (6),(B'
)
186, 166A, 186B,A166.A186A, A9CE cs·i. <B.
A1668,T166C
195.195A. 1958 A-790 (7), (C)
190 A-790 (9), (El
206,H P206.P206A.B.C.0.E. H
A4CE (6°), (8°)
TP206A.B,C,O,E,
U206,U2D6A,B,C.O.E,F,G,
TU206A,B,C,O,E,F,G
T206H
U206,U206A,B.C,0 .E.F.G. (Conv. Per STC 2123 NM) A4CE
(6°), (B·)
207 .207 A.T207 ,T207 A
A16CE (6°), (8°)
210,21 OA,B.C,O,E,F 3A21 (6°), (8°)
210-5,210-5A,T210F.210G.
T210G.210H,T210H,210J,T210J,
T210K,210K,210L,T210L,210M,
T210M,210N,P210N.T210N.210R P210R.T210R
310,310A,B,C,O,E,F,G,H, E310H,3101,J,K,L.N.P,O,R 3A10 (GT°), (BT")
310J-1 ,E310J,T310P,O,R
T3100,310R,T310R
321
3A1 1 (6TI, (BTI
320.A.B,C,O,E,F,320-1,335, 340(.340A 3A25 (6T 0 ) ,(B"
)
336
A2CE (GD. (B1 ,
T303 A34CE rsT·i. <BT·i
337, 337A,B.C,O.E,F,G,H AGCE (GT·). (BT·)
T337B,C,O,E,F.G,H,
M337B.P337H,T337H-SP
401, 401A,B, 402,402A,8 ,C, P.7CE (GT°), (BT")
FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT- 100/200 series.
RPM and MAP applicable to the PIN EGT-701, 4 and 6 cylinder engines only. Revision 13
FAA APPROVED MASTER ELIGIBILITY LIST J .P.INSTRUMENTS REPORT: SA 2586NM
MAKE AIRCRAFT MODEL
ELIGIBLE PART NUMBERS for EGT-701
Note (1) suffix
·r
designates twins. two instruments required.
Note (2) suffix • • • denotes turbocharged engines.
Part number Series
4
4
6
6
4 Cylinder with
4 Cylinder
6 Cylinder with
6 Cylinder
RPM
&
MAP RPM
&
MAP
EGT-701·( ) EGT-701-() EGT-701·() EGT-701-()
4C RIM 4C SCRIM
SC
4CORIM 4CO
6CORIM SCO
4CA RIM 4CA
6CARIM SCA
4CT RIM
4CT 6CT RIM 6CT
4CI RIM 4CI
6CIRIM 6CI
4CF RIM 4CF 6CF RIM SCF
4COARIM 4COA SCOARIM 6COA
4COTRIM 4COT 6COT RIM 6COT
•co,
RIM 4COI SCOI RIM 6COI
4COF RIM 4COF 6COF RIM 6COF
4COATRIM 4COAT 6COAT RIM 6COAT
4COAJ RIM 4COAI 6COAI RIM 6COAI
4COAF RIM 4COAF S COAF RIM SC OAF
4COATI RIM 4COATI 6COATIRIM 6COATI
4COATFR/M 4COATF 6COATF RIM 6COATF
4COTI RIM 4COTt 6COTI RIM SCOT!
4COTF..RIM 4COTF SCOTF RIM 8COTF
4COIT RIM 4COIT
SCOITRIM 6COIT
4COTIF RIM
4COTIF
SCOTIF RIM SCOT IF
4COAIF RIM 4COAIF 6COAIF RIM SCOAIF
4CA TIFRIM 4CATIF 6CATIF RIM
6CATIF
t
4CATRIM ... 4CAT SCATRIM SCAT
4CAI RIM 4CAI 6CAI RIM
SCAI
4CAF RI_ M 4CAF 6CAF RIM 6CAF
4CATI RIM 4CATI 6CATiRJM 6CATI
•4CATF RIM 4CATF SCATE RIM SCATF
4CAIF RIM 4CAIF SCAIF RIM SCAIF
4CTIF RIM 4CTIF 6CTIF RIM 6CTIF
4CTI RIM 4CTI 6CTI RIM SCTI
4CTFRIM 4CTF
6CTF RIM 8CTF.
4CIF RIM 4CIF 6CIF RIM
6CIF
4COATIF " RIM 4COATIF.. 6COATIF.RIM 6CQATIF
ELIGIBLE PART NUMBERS for EGT-100·( ) and EGT-200( )
Note (1) suffix T designates EGT-200 () series for twins
Note (2) suffix ··· denotes for lurbocharged engines.
Part number Series
A
4 cylinder
6 7
EGT-100-( ) EGT-100-(
EGT-100-(
4
6
4C 6C 7C SC
4CO 6CO 7CO
4CA 6CA
7CA
4CT 6CT 7CT
4CI 6CI 7CI
4COA 6COA
,!COT . 6COT
6COI
6COA I -
6COAJ
4COATI 6COATI
6COIT
SCAT·
6CAI
6CATI
4CTI 6CTI
7
7 Cylinder
EGT-70 1-()
7C
7CO
7CA
7CT
7CI
7CF
7COA
7COT
7COI
7COF
7COAT
7COAI
7COAF
7COATI
7COATF
7COTI
7COTF
7COIT
7COTIF
7COAIF
7CATIF
7CAT
7CAI
7CAF
7CI\Tt
7CATF
7CA!F
7CTIF
7CTI
7CTF
7CIF
7COATIF
9
9C
E
linder
SHEET 9
Part N umber
T.C.D.S. (See P. 9 for Series )
8 9 TIT
8 Cylinder 9 Cylinder
EGT-701-() EGT-701-()
SC
sco
SCA
SCT
SCI
SCF
SCOA
SCOT
SCOI
SCOF
SCOAT
SCOAI
SCOAF
SCOATI
SCOATF
SCOTt
SCOTF
SCOIT
SCOT IF
SCOAIF
SCATIF
SCAT
SCAI
SCAF
SCAT!
SCATF
BCAIF
S CTIF
SCTI
6CTF
SCIF
SCOATIF
TIT
9C
9CO
9CA
9CT
9CI
9CF
9COA
9COT
9COI
9COF
9COAT
9COAI
9COAF
9COATI
9COATF
9COTI
9COTF
9COIT
.9COTIF
9COAIF
9CATIF
SCAT
9CAI
9CAF
9CATI
9CATF
9CAIF
9CTIF
9CTI
9CTF
9CIF
9COATIF
Example:
see page 5
Cessna J I O (6P)
6 • any PN in that col umn
except • items in TIT column
T • Requi res two instruments
• • Includes TIT
(turbocharged ale only)
FAA approved AFM Supplement is required with the EGT-701. The EGT-701 i s applicable to all EGT-100/200 series.
RPM and MAP applicable to the PIN EGT-701, 4 and 6 cylinder engines only. Revis ion 13