TB20 N113AC

Aircraft approved for European IFR including BRNAV and GPS/RNAV approaches
4 seater, 500kg max load including 234kg fuel
163kt TAS at 75% power at 6500ft
Max range 1300nm
3-blade TKS de-iced propeller
KLN94 BRNAV and Approach certified GPS
KMD550 multifunction display (GPS moving map + stormscope + TCAS)
WX500 stormscope displaying on 2 x SN3500 & KMD550
Avidyne TAS605 TCAS displaying on 2 x SN3500 & KMD550
2 x SN3500 EHSI
2nd altimeter
2nd electric horizon (P2 position)
EDM700 6 cylinder CHT & EGT monitor (3", on LHS) with data logging
KN63 DME
KR87 ADF
GTX330 Mode S Transponder
1x KX155A COM/VOR/ILS
1x KX165A COM/VOR/ILS (8.33)
PMA7000 intercom with markers & music input
Shadin fuel computer, calibrated, linked to KLN94 GPS
KFC225 autopilot with flight director, ALT and VS preselects, tracks VOR/GPS/LOC/ILS
121.5/406MHz fitted ELT

Oxygen with O2D2 automatic demand regulators for 4 persons
Emergency equipment comprises 4 life jackets, 4/6-person raft, 121.5/406MHz EPIRB,
Garmin handheld GPS, VHF transceiver/VOR/ILS receiver

Cruise Performance Data:

Power
MP
RPM
Fuel lit/hr
IAS
kt
Endurance
hr
Range
nm
MPG
ukm/ukg
75%
24"
2400
52
147
6.1
901
14.8
65%
22"
2300
46
140
6.9
971
16.0
55%
20"
2200
40
130
7.9
1030
16.9
45%
21"
1800
32
120
9.9
1136
18.7

The above are from the handbook. The normal cruise configuration is 23" 2400RPM and lean of peak at approx 10.5 USG/HR, giving an endurance of 8:30 hours and 138KT IAS, with a zero-fuel range of over 1300nm possible at 2200rpm at 8000-10000ft. TAS at 16,000 feet is approximately 145-150kt.

The one below is a Socata stock picture. The rest are the real aircraft.

Original panel pic:

2014 panel pic:


Site last updated on: 22nd August 2013

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