Cessna 404 Titan

Number of Active Aircraft: 52 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 10
Empty Weight: 4980 lbs
Max Weight 8400 lbs
Useful Load: 3420 lbs
Engine Name CONT GTSIO-520-M
Engine Number 2
Horsepower 375 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 26000 ft
Max Fuel 348 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 217 kts
GPH (75% BHP): 45
MPG (75% BHP) 4.8
Range (75% BHP): 1560 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 270 $
MPG per 1000 lbs of Payload 16.49
F-T (Speed^2/FuelBurn) 10.5 HP
F-T Payload 35.9 kts
MPH To HP: 5.8 kts
T/O Roll - T/O over 50 FT OBST 1788 ft / 2367 ft

SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00103WI Installation of a heated windshield panel Amended 1/20/2011
SA00161BO (2 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00243BO (3 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (1OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00279SE Installation of redesigned engine exhaust stacks. Amended 2/8/2005
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00556DE Installation of a left-hand exhaust stack assembly. Issued 9/23/2004
SA00571SE Replacement of certain BF Goodrich pneumatic deicer boots. Reissued 6/13/2001
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00709LA Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Reissued 5/14/2002
SA00729SE Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. Amended 11/30/2005
SA00804SE Installation of an engine failure indicator system also referred to as a low Thrust Detector system.  Amended 7/16/2000
SA00823CH Installation of various de-icer wire harnesses. Reissued 10/10/2002
SA00833WI Installation of a seat headrest. Issued 11/5/1999
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00944CH Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) Amended 6/20/2000
SA00977CH Replacement of certain BFGoodrich pneumatic deicer boots. Amended 12/30/2003
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01118WI Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 Amended 11/30/2013
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01420WI Installation of Garmin GNS 430A / 530A COMM/NAV/GPS Systems. Data required: (1) Scandinavian Avionics Design GmbH Drawing List 2027438-DL-02 Issue 2 or later EASA approved revisions. (2) Scandinavian Avionics Design GmbH Approved Aircraft Flight Manual Supplement Doc. 2027438-AM-02A Issue 1 and Doc. 2027438-AM-02B Issue 2 both approved by EASA under approval No. EASA.A.S.01389 dated 07-09-2005 or later EASA approved revision. );INSERT INTO stc_table VALUES (  Issued 4/6/2007
SA01436SE (1 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (2 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01828SE Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System Reissued 5/12/2011
SA01860NY (3 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 2)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02045AK-D Fabrication and installation of Aero Twin Inc Single Place Folding Seat P/N ATFS1-01W Issued 2/29/1996
SA02095AK Installation of hourmeter airspeed switch. Issued 12/10/1997
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02217AK (3 OF 5 Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02254AK Installation of Single Screen Amended 11/7/2011
SA02395AK Installation of DFS2T Single Place Seats Issued 4/25/2012
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02546NY Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1 Issued 7/9/2008
SA02738CH (PAGE 5) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09472SC Conversion of existing Cessna air conditioning system from R12 to R134a refrigerant. Amended 2/14/2000
SA1005NE Installation of Teledyne Avionics Power Analyzer and Recorder (PAR) Part No. SL17052 Reissued 8/14/2007
SA1006NE Installation of Teledyne Avionic angle of attack indicating system P/N112-9500. Reissued 8/14/2007
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA103RM Installation of exhaust turbo connector P/N 30477-3 Amended 11/28/1990
SA1199GL Limit maximum passenger seating capacity to nine or less. Issued 8/21/1987
SA1200GL Limit maximum passenger seating capacity to nine or less. Issued 8/21/1987
SA1274GL Install Egan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 805. Reissued 5/1/1997
SA1297CE Installation of King KFC 200 2-axis(3 optional) flight control system. Reissued 2/28/2000
SA1304CE Installation of Enk Aviation fire protection system. Amended 12/5/1979
SA143RM Installation of air conditioner system. Reissued 5/17/2013
SA1482CE Installation of Tull microwave landing system. Issued 4/9/1979
SA1528CE-D Installation of King KAS 297 altitude selector option in airplanes equipped with KFC-200 Flight Control System with Flight Director installed under STC SA1297CE. Reissued 2/28/2000
SA1600CE Installation of stretcher per Avcon Ind. D/N 4001 7/17/80 or later for standard stretcher 3/3/82 for back adjustable stretcher. Reissued 8/21/1990
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1645GL Replace existing Southwind combustion heater P/N 8259HL-2 with C&D Airmotive combustion heater P/N 1071. Issued 9/23/1991
SA1863SW Installation of single and dual aerial survey cameras and navigation sights Reissued 12/16/2013
SA195GL Installation of radome. Amended 10/31/1996
SA195RM New slip joint exhaust manifold. Issued 12/20/1979
SA20GL Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) Reissued 4/30/2007
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2650NM Cockpit Sun Visor Installation. Amended 6/4/2004
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2872SW Installation of wing nacelle locker tanks. Reissued 7/5/1990
SA2993SW Installation of nose fuselage fuel tank. Reissued 7/5/1990
SA3384WE Removal of cargo doors and instal- lation of P/N A770000 airstream deflector. Issued 6/8/1977
SA3388WE Installation of recognition lights on horizontal stabilizer. Reissued 2/28/1980
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4017WE Installation of Hoskins model CFS-2000 -2001 or FT-200 fuel flow indicating system. Reissued 1/30/1998
SA4024NM Replace the standard Cessna oil drain plug with a Bogert Aviation quick drain. Amended 4/12/1989
SA4105WE Installation of tail stinger and/or nose stinger. Issued 2/21/1980
SA4163WE Installation of doppler radar antenna. Issued 5/21/1980
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA430GL Installation of Collins LRN-70 Omega/VLF navigation system with computer program 11113322334.1. Issued 8/14/1980
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA472CH Removal of Nav-O-Matic 400B autopilot restriction. (404 S/N 404-0613) Issued 12/19/1995
SA4745NM Installation of Lifeport Patient Loading and Support System. Amended 11/23/1993
SA5137NM Installation of sun visor. Amended 2/22/2005
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA5929SW Installation of P&W Canada PT6A-34 engines increase interior seating and increase takeoff and landing gross weights. Amended 10/9/1991
SA71GL Installation of air filters Reissued 6/20/2000
SA721NW Installation of camera bays. Reissued 7/22/1988
SA722NW Installationo f a Geometrics G803-905 tail stinger Reissued 7/22/1988
SA723NW Installation of Model AS-1350 Advanced Absorber Doppler Antenna and Radome Reissued 7/22/1988
SA781GL Replace existing main wheel and brakes by installing Parker Hannifin conversion kit 199-78. Issued 5/31/1984
SA859NW Installation of Advanced Absorber Doppler Antenna and Radome Reissued 7/22/1988
SA860NW Installation of a Geometrics tail stinger Reissued 7/22/1988
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA986NW Installation of a Geometrics G803-905 tail stinger Reissued 7/22/1988
SA987NW Installation of an air sampling port Reissued 7/22/1988
SA988NW Installation of Model AS-1350 Advanced Absorber Doppler Antenna and Radome Reissued 7/22/1988
SA989NW Installation of a cabin heater exhaust system Reissued 7/22/1988
SP00400SE  Installation of various propeller electrical de-icer models  Amended 7/25/2006
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)