190-00734-15 Rev. 3
AFMS, Garmin GTX 33X and 3X5 XPDR with ADS-B
Page 12 of 17
FAA APPROVED
Section 2.
LIMITATIONS
2.1
Minimum Equipment
The GTX 33X and GTX 3X5 must have the following system interfaces fully
functional in order to be compliant with the requirements for 14 CFR 91.227 ADS-
B Out operations:
Interfaced Equipment
Number Installed
Number
Required
Uncorrected Pressure Altitude
Source
1
1
GPS SBAS Position Source
1 or more
1
Remote Control Display (for
remotely mounted transponders)
1 or more
1
Table 2
–
Required Equipment
2.2
ADS-B Out
The GTX 33X and GTX 3X5 only comply with 14 CFR 91.227 for ADS-B Out
when all required functions are operational. When the system is not operational,
ADS-B Out transmit failure messages will be present on the remote control display
interface, or the GTX 330 or GTX 3X5 panel display. If a Gables 7534 controller is
being used the ADS-B equipment failure condition will be annunciated on the
Gables dis
a T a
de Fai hi e he ADS
-B Out Position failure will be
a
cia ed b he e
e i
a ed ADS
-B POSN FAIL
A
cia .
2.3
TIS Traffic Display with User Navigation Angle
Display of TIS traffic from a GTX 33/330 or GTX 335 is not permitted with an
i e faci g di
a c fig ed f a a iga i a g e f
e .
Summary of Contents for 177 Cardinal
Page 2: ...PERFORMANCE SPECIFICATIONS N35031 1 426 lbs 1 073 lbs N35031 ...
Page 5: ...CONGRATULATIONS ...
Page 6: ......
Page 10: ...OPERATING CHECKLIST See APPENDIX 86 19 11 Preflight Fuel System Check ...
Page 11: ......
Page 12: ......
Page 19: ......
Page 21: ......
Page 23: ...ELECTRICAL SYSTEM MASTER SWITCH AMMETER OVER VOLTAGE SENSOR AND WARNING LIGHT ...
Page 24: ...ELECTRICAL SYSTEM ...
Page 25: ...LIGHTING EQUIPMENT CIRCUIT BREAKERS AND FUSES EXTERIOR LIGHTING ...
Page 26: ...INTERIOR LIGHTING ...
Page 27: ...CABIN HEATING VENTILATING AND DEFROSTING SYSTEM ...
Page 28: ...SHOULDER HARNESSES ...
Page 31: ...TAXIING DIAGRAM ...
Page 32: ...TAKE OFF MAGNETO CHECK ALTERNATOR CHECK POWER CHECK ...
Page 33: ...WING FLAP SETTINGS PERFORMANCE CHARTS CROSSWIND TAKE OFFS ...
Page 35: ...CRUISE PERFORMANCE ...
Page 36: ...LEANING WITH A CESSNA ECONOMY MIXTURE INDICATOR EGT ...
Page 37: ...SPINS STALLS LANDING SHORT FIELD LANDINGS ...
Page 43: ...FORCED LANDINGS PRECAUTIONARY LANDING WITH ENGINE POWER EMERGENCY LANDING WITHOUT POWER ...
Page 44: ...FIRES DITCHING ENGINE FIRE DURING START ON GROUND ...
Page 45: ...ENGINE FIRE IN FLIGHT ELECTRICAL FIRE IN FLIGHT ...
Page 46: ...EXECUTING A 180 TURN IN CLOUDS EMERGENCY LET DOWNS THROUGH CLOUDS DISORIENTATION IN CLOUDS ...
Page 48: ...ROUGH ENGINE OR LOSS OF POWER CARBURETOR ICING SPARK PLUG FOULING ...
Page 49: ...ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS MAGNETO MALFUNCTION LOW OIL PRESSURE ...
Page 50: ...INSUFFICIENT RATE OF CHARGE EXCESSIVE RATE OF CHARGE ...
Page 56: ......
Page 57: ...OPERATIONS AUTHORIZED MANEUVERS NORMAL CATEGORY OPERATING LIMITATIONS ...
Page 58: ...MANEUVERS UTILITY CATEGORY ...
Page 63: ...LOADING ARRANGEMENTS STANDARD SEATING 2ND ROW SEAT REMOVED ...
Page 65: ... LOADING GRAPH ...
Page 66: ... CENTER OF GRAVITY MOMENT ENVELOPE ...
Page 67: ...GROUND HANDLING MOORING YOUR AIRPLANE CARE OF THE AIRPLANE ...
Page 69: ...ALUMINUM SURFACES PROPELLER CARE ...
Page 70: ...INTERIOR CARE ...
Page 71: ...MAA PLATE FINISH AND TRIM PLATE AIRCRAFT FILE ...
Page 73: ...CESSNA PROGRESSIVE CARE CESSNA CUSTOMER CARE PROGRAM ...
Page 74: ...SERVICING REQUIREMENTS ...
Page 75: ...OWNER FOLLOW UP SYSTEM PUBLICATIONS ...
Page 76: ...OPERATIONAL DATA ...
Page 77: ......
Page 78: ...2500 2200 1900 2500 2200 1900 ...
Page 79: ... 2500 2400 2300 2200 2100 2 500 FEET ...
Page 80: ... 2500 2400 2300 2200 2100 5 000 FEET ...
Page 81: ... 2500 2400 2300 2200 2100 7 500 FEET ...
Page 82: ... 2500 2400 2300 2200 2100 2600 2700 10 000 FEET ...
Page 83: ... 2500 2400 2300 2200 2100 2600 2700 12 500 FEET ...
Page 84: ...2500 Horton 540 Horton 50 ...
Page 88: ...N35031 17702167 ...
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Page 93: ......
Page 94: ...N35031 17702167 Cessna 177B ...
Page 111: ......