Bellanca 17-31A

Number of Active Aircraft: 101 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 2247 lbs
Max Weight 3325 lbs
Useful Load: 1078 lbs
Engine Name
Engine Number 1
Horsepower 300 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 18200 ft
Max Fuel 68 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 168 kts
GPH (75% BHP): 20.2
MPG (75% BHP) 8.3
Range (75% BHP): 465 nm
Fuel Cost Per Seat Mile 0.18 $
Fuel Cost Per Hour 121.2 $
MPG per 1000 lbs of Payload 8.97
F-T (Speed^2/FuelBurn) 14 HP
F-T Payload 15.1 kts
MPH To HP: 5.6 kts
T/O Roll - T/O over 50 FT OBST 980 ft / 1420 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
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00243BO (1 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
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
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00695SE Replacement of certain Rotomaster and Rayjay scavenge pumps Amended 2/14/2003
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00954SE (2 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (2 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005 1:00
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
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
SA01375AT Installation of adapter ring P/N J1001-1 and fuel cap assembly (usher type) P/N UO-3. Reissued 3/1/2001
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (1 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
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 1)  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 (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01988SE (PAGE 2) 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
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
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
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
SA02217AK (1 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
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
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
SA03286CH Install an electronic engine ignition system Issued 1/13/2014
SA09146AC-D Installation of S-TEC System 55two axis automatic flight guidance system Model ST-615 with optional autotrim system. Amended 10/3/2001
SA09366AC-D Installation of S-TEC system 20/30 single and two axcis automatic flight guidance systems Model ST-818-20/30. Issued 5/22/1998
SA09368AC-D Installation of S-TEC system 30 alt altitude hold system Model ST-819. Issued 6/1/1998
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09555SC Installation of Cablecraft cables: P/N 565-550-A-G-37.5 for throttle P/N 565-550-B-G-32 for mixture and P/N 565-550-C-G-69.5 for propeller. Issued 6/7/1999
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1118SW Installation of EDO-AIRE system Model 276.Mitchell manual electric trim Reissued 7/9/1984
SA1195SW Mitchell automatic flight system AS309 consisting of Century I automatic aileron stabilizer with omni tracker. Reissued 7/9/1984
SA1235SW Mitchell automatic flight system AK215 consisting of Century II autopilot with optional automatic aileron stabilizer and radio coupler. Reissued 7/9/1984
SA1236SW Mitchell automatic flight system AK233 consisting of Century III autopilot with optional command/automatic pitch trim radio coupler and aileron stabilizer. Reissued 7/9/1984
SA1257CE Installation of King KFC 200 2 axis flight control system with a KI 255 (or -256) flight command indicator or a KG 258 attitude horizon gyro with a KC 292 mode controller or stand alone electric trim. Reissued 2/28/2000
SA1344CE Chrome-plated brake disc installation. Issued 8/18/1977
SA1400GL Installation of Pamco emergency backup pneumatic system. Issued 8/4/1989
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1494SW Installation of Mitchell flight director remote annunciator Model AK375. Amended 7/10/1984
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1811SW Mitchell automatic flight system AK466 and AK466FD consisting of Century IV autopilot and Century IV flight director with electronic command/automatic pitch trim. Reissued 8/1/1984
SA1812SW Mitchell automatic flight system AK465 consisting of Century III autopilot with optional electronic command/automatic pitch trim optional radio coupler and optional glide slope coupler. Reissued 8/1/1984
SA2176SO Replacement of Cleveland brake discs P/N 164-15A or164-115A with Appalachian Accessories stainless steel brake discs P/N 75-15A. Issued 9/25/1987
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
SA2510NM Installation of inflatable door seal. Issued 8/27/1984
SA2586NM (PAGE 1) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
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
SA2831SO Installation of modified lower engine.cowling and addition nose gear doors. Amended 8/25/1994
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA3000SO Installation of Appalachian stainless steel brake discs No. 75-15A. Reissued 9/29/1995
SA3047SO Replacement of air intake pipes with aluminum pipe assembly. Issued 10/28/1991
SA3059SW-D Mitchell AK466 and AK466FD consisting of Century IV autopilot and Century IV flight director autopilot with optional annunciator. Reissued 8/16/1984
SA3060SW-D Mitchell flight system Model AK465consisting of Century III autopilot with optional electronic command/ automatic pitch trim optional radio coupler and optional glide slope coupler. Reissued 8/16/1984
SA3061SW-D Mitchell automatic flight system Model AK495 consisting of Century I autopilot with optional omni tracker. Reissued 8/16/1984
SA3071SW-D Mitchell automatic flight system AK546 consisting of Century IIB autopilot with optional radio coupler. Reissued 6/20/1984
SA3083SW-D Mitchell command electric trim AK545. Reissued 6/19/1984
SA3267WE Modification of aileron control system by addition of aileron centering spring and installation of Pathfinder autopilot systems and/or pitch trim systems. Reissued 9/30/1998
SA3461SW-D Installation of Century automatic flight system Model AK966consisting of a2010/2030/2031/2050/2051 autopilot. Amended 2/14/1997
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3571SW Installation of electrically driven standby vacuum pump. Reissued 4/6/2007
SA3688WE Installation of an air/oil separator. Reissued 9/28/2001
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4304WE Installation of Hoskins CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5158SW-D Installation of S-TEC System 60Two Axis Automatic Flight Guidance System Model ST-151 with Optional Automatic Electric Trim System. Reissued 10/12/1990
SA5159SW-D S-TEC System 60 pitch stabilization system ST-152 with optional automatic electric trim. Issued 5/2/1983
SA5174SW-D S-TEC System 60 single axis automatic flight guidance system ST-150. Issued 6/29/1983
SA5352SW-D Installation of S-TEC manual electric trim system Model ST-273. Issued 11/6/1984
SA574SO Installation of Bendix FCS-810automatic flight control system including manual electric pitch trim and optional flight director indicator DH-841. Issued 2/1/1974
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA615EA (PAGE 1) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA800EA (PAGE 1) Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. Amended 7/6/2010
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA846SW Wing root fairings. Reissued 1/24/1979
SA847SW Main landing wheel doors. Reissued 11/27/1978
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
SA903SO Reposition of fuel pump. Issued 7/30/1976
ST01700NY (1 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. Issued 7/8/2003
ST02547AT (1 OF 2) Installation of a voice alert system. Amended 5/13/2003
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)