Number of Active Aircraft: 110 Active- Map


Introduced in 1947 and produced through 1949 with a total of 235 built, it was an extension of the PA12. It increased seat capacity up to four but its range was limited with a full load.

Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1020 lbs
Max Weight 1850 lbs
Useful Load: 830 lbs
Engine Name Lycoming O-235-C1
Engine Number 1
Horsepower 115 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12500 ft
Max Fuel 38 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 95 kts
GPH (75% BHP): 6.6
MPG (75% BHP) 14.4
Range (75% BHP): 471 nm
Fuel Cost Per Seat Mile 0.1 $
Fuel Cost Per Hour 39.6 $
MPG per 1000 lbs of Payload 11.95
F-T (Speed^2/FuelBurn) 13.7 HP
F-T Payload 11.4 kts
MPH To HP: 8.3 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 965 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00132SE Fabrication of F. Atlee Dodge aft fuselage weld-on fittings for the mounting of Edo Model 89-2000 floats. Reissued 7/5/2005
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00349SE Installation of numerous items re photographs in FAA project file. Issued 5/30/1996
SA00467SE Fabrication and installation of vortex generators mounted on the wings and a tail strake mounted on either side of the empennage. Reissued 5/27/1999
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00780SE (PAGE 1) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00805CH Installation of Air-Energy Service Inc. (AESI) P/N AESI-12-1900 (-1) wing fuel tanks. Reissued 2/9/2009
SA00932SE Installation of the Stewart wing tip assembly in accordance with Stewart Wing Tip Assembly Master Drawing List SWT 3001 dated April 8 2001 or later FAA approved revision. Amended 1/25/2002
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01063CH Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. Reissued 2/16/2006
SA01074CH Installation of Air-Energy Service Inc. Leading Edge Part Number AESI #1511. Reissued 10/8/2004
SA01104CH Installation of Swing Type Engine Mount. Reissued 10/23/2004
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01251SE The manufacture of a Sunvisor System. Amended 2/28/2012
SA01333CH Installation of a 24-gallon wing fuel tanks. Reissued 2/9/2009
SA01704LA Installation of the Grove Disk Brake System Issued 12/21/2004
SA01734SE (PG 3) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01944CH (2 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004 0:00
SA02007AK Installation of main landing gear long step no. 3195. Amended 5/23/2006
SA02033AT (PAGE 3) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02049AK Fabrication and installation of Airglas Engineering Co. Inc. Model LTC18 cargo pod/bell Reissued 10/28/2011
SA02089AK Installation of Airglas LW2500 fixed wheel penetration skis. Issued 9/22/1997
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02115AK Fabrication and installation of 30.5 gallon wing fuel tank sight gages. Amended 1/20/2004
SA02123AK Installation of Baumann Model BF-2100 floats. Reissued 10/23/2001
SA02128LA Installation of aileron and flap hinge repair bushings Amended 6/10/2009
SA02153AK Installation of Burl s Aircraft Rebuild Magnum I tail wheel penetration tail ski per Burl s Aircraft Rebuild LLC Master Data List No. MDL-3234-1 latest FAA approved revision. Issued 12/22/1999
SA02170AK Installation of McCauley propellers Models 1A175-GM8241 through 1A175-GM8244. Issued 1/3/2001
SA02188AK Fabrication and installation of p/n 3284 three-inch extended PA-18 type main landing gear together with p/n 3164-4 extended shock strut assemblies. Applies to those models previously modified by SA148AL SA543AL or SA669AL or for Piper PA-12S models planes must have been converted to landplane configuration. Issued 1/11/2002
SA02190AK Fabrication and installation of p/n 3344A main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to those aircraft previously modified by STCs such as SA02188AK. Issued 1/11/2002
SA02203AK (PAGE 2)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02214AK Installation of Alpha Omega Suspension System in place of original bungees or bungees and hydasorbs. Amended 11/15/2005
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02295AK Installation of a high capacity fule gascolator assembly. Issued 8/21/2007
SA02299AK Installation of a replacement fuel selector valve. Issued 9/13/2007
SA02309AK Installation of a stabilizer trim system Issued 4/17/2008
SA02316AK Installation of 8.50-6 and 8.50-10 tires Issued 9/5/2008
SA02321AK Installation of EDO 89-2000 floats modified Issued 8/29/2008
SA02421AK Installation and rigging of F.Atlee Dodge Model F.A. DODGE X-1 wheel replacement skis Issued 12/23/2013
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-51 Installation of a Lycoming O-290-D2 engine in combination with Edo 89-2000 floats and water rudder and seaplane fin. Reissued 2/10/2006
SA1-510 Installation of Sur-Vent fuel tank filler cap manufactured. Reissued 5/11/1994
SA1-573 Lycoming O-320 150 hp engine with PA-18A-150 cylinder baffles Sensenich M74DM propeller and Harrison AP13SJ03-01 oil cooler. Reissued 2/10/2006
SA1-644 Installation of Edo 89-2000 floats water rudder and seaplane fin. Reissued 2/10/2006
SA11RM Installation of modified axles wheels and brakes Amended 7/13/1999
SA126SO Installation of wing fabric attachment clips. Reissued 6/3/1991
SA1344GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA1350WE Replace existing fabric on wings fuselage empennage and/or control surfaces with fiberglass cloth. Reissued 3/6/1969
SA1351WE (PG 2) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983 0:00
SA144AL Remote compass bracket. Issued 1/1/1960
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA147AL Electric fuel quantity gauge system. Issued 1/1/1961
SA148AL PA-18 main landing gear and installation of EDO 2000 floats. Amended 3/3/1969
SA149AL Installation of auxiliary baggage compartment. Issued 1/1/1960
SA1536NM Installation of stamped aluminum wing ribs. Issued 2/25/1983
SA1584NM Installation of replacement long-life lift strut. Reissued 1/29/1999
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1629WE Installation of left-hand door and associated fuel line routing and stabilizer trim cable changes. (PA-14 S/N 14-66 N4262H) Reissued 5/1/1996
SA189AL Install left side cabin door. Issued 1/1/1960
SA1903NM Installation of Schneider wheel skis 6-inch to 10-inch aluminum wheel adapters and 29x11.0-10 8 ply minimum tires on main landing gear. Issued 12/14/1982
SA190AL Increased gross weight to1935 pounds. Issued 1/1/1960
SA192AL Flap handle installation and adjustable fore and aft pilot and co-pilot s seat. Issued 1/1/1960
SA196SW Hartzell HC-82XL-6F/7636D-4 propeller Woodward 210080P governor and Piper 14-733-00 propeller control Issued 1/1/1960
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA2040AK Installation of vented fuel cap assembly (P/N 3267). Issued 9/7/1995
SA2083CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON + MON)/2. Intermixing with aviation gasoline also approved. Amended 6/23/1992
SA2127WE Installation of Madras Air Service Model 104 wing tips. Amended 2/4/1982
SA213SO Electric fuel quantity indicator. indicator. Issued 1/1/1960
SA214AL Install L1650A and L-2000A wheel replacement skis. Issued 1/1/1960
SA215AL Install L-2500A wheel replacement skis. Issued 1/1/1960
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA22RM Manufacture of exact replacement parts front and rear lift strut assembly. Reissued 7/11/1981
SA2313SW Install 22-1/2 gallon fuel tank. Reissued 1/26/2012
SA2345NM Installation of SWS-11000 Tundra tires wheels and hubs. Issued 8/29/1986
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2508SO Replacement of Cleveland brake discs No. 164-67 or 164-167 with Appalachian Accessories stainless steel brake discs Part No. 73-67. Reissued 9/29/1995
SA253AL Installation of McCauley 1A175/GM propeller. Amended 8/4/1971
SA2610CE Operation of airplane on leaded or unleaded automotive gasoline 91 minimum antiknock index(RON+MON)/2 per ASTM Specification D-439. Intermixing with aviation gasoline also approved. Issued 4/17/1990
SA262AL Install 6x6x44 fish pole tube. Issued 1/1/1960
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA289AL Install rudder centering device. Issued 1/1/1960
SA293AL Installation of Stoddard improved brake system. Reissued 7/9/1981
SA2NE Installation of Cleveland wheels and brakes 7.00-6 or 6.00-6 C38500-HA 40-6 in accordance with S.V. Scherbon modifications 3/6/73 on several models of Piper aircraft. Issued 4/5/1973
SA3-106 Edo 89-2000 floats water rudder and auxiliary tail fin. Issued 1/1/1960
SA308EA (2 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978 0:00
SA3213WE Installation of George M. Adams DGA-2000 or Bodell BMI-2000 wheels and Bodell BMI-252 brakes. Reissued 6/25/2003
SA356AL Installation of AD 2500x10.5 wheel replacement skis and rigging. Issued 1/1/1960
SA3603NM Installation of landing gear fueling step. Issued 9/18/1986
SA3625NM Application of polyurethane finishing system. Issued 7/15/1987
SA3634NM Fabrication of North River Avia. Model 8400 brake booster assembly and modifcation of Scott Aviation Model B-711 brake master cylinders. Reissued 1/26/2006
SA368AL Installation of McCauley1A175/GM8242 GM8244 or GM8246 propellers. Amended 8/18/1972
SA378SW Lycoming O-320 engine -6-inch wheels and Piper PA-18 horizontal tail surfaces. Issued 1/1/1960
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA398AL Conversion of 4-inch wheels and brakes to 6-inch wheels and brakes. Issued 8/19/1970
SA3AL Installation of Fred A. Shaw tundra-bird Model 2500 skis. Reissued 9/11/2009
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-410 Lycoming 150 hp engine O-320-A2A. Issued 1/1/1960
SA4-411 Modification of fuel system to PA-18 to facilitate takeoff either tank. Issued 1/1/1960
SA4-412 Large PA-18 tail surfaces. Issued 1/1/1960
SA4-561 Application of glass cloth to fuselage and to horizontal and vertical stabilizer. Issued 1/1/1960
SA4-78 Installation of a Lycoming O-320 engine and Sensenich M74DM59 propeller. Installation of Piper PA-18A-150 engine cooling baffles modified to fit cowling. Installation of oil cooler (Harrison AP13SJ03-01) in accordance with Piper Drawing 14368. Installation of pressure type gas tank caps. Reissued 11/19/2012
SA4-81 Lycoming O-290-D2 engine and Sensenich M76AM-2/74-52 propeller. Issued 1/1/1960
SA4-840 Fabric replaced with glass cloth on wings fuselage empennage and/or control surfaces. Issued 1/1/1960
SA4-913 Ceconite 101 covering of wings fuselage and vertical fin. Issued 1/1/1960
SA4-977 Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons. Amended 10/6/2005
SA4005NM (PG 3) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA41AL Six inch wheels and brakes. Issued 3/7/1963
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA460SW Install wing tips in accordance with Cub Crafters Inc. Master Drawing List. MDL102400 Revision C dated May 30 2001 or later FAA approved revision. Reissued 1/26/2012
SA4617NM Fabrication and installation of P/N 3166-2 main landing gear cabane vee assembly. Issued 8/7/1989
SA4620NM Fabrication and installation of P/N 3164-2 main landing gear shock strut assemblies. Issued 8/7/1989
SA4635NM Modification of wing lift struts. Issued 2/1/1991
SA469AL Installation of electric fuel gauges. Reissued 7/9/1981
SA477AL Installation of fiberglass wing tips. Reissued 9/11/2009
SA496AL Installation of leading edge cuff. (PA-14 Seaplanes) Amended 3/4/1977
SA5-13 Installation of 8.50x6 tires and tubes with Hayes 6-inch wheels. Reissued 9/11/2009
SA5-33 Removed unbalanced tail surfaces and installed balanced tail surfaces. Install elevators Piper 12789-00 and 12789-01 and stabilizers Piper 12790-00 and12790-01. Reissued 6/12/1997
SA5-39 Large horizontal stabilizers and elevators. Issued 1/1/1960
SA5-60 Installation of Russ Simpson sea fins. Issued 1/1/1960
SA5-65 25x11x4 tires on Goodrich 4-inch wheels 841696 using rim adapter A-1. Reissued 3/31/2004
SA5-66 Structural approval only of Fred A. Shaw engine mount and forward fuselage modification for installation of 150 hp engine. Reissued 9/11/2009
SA5-9 25x11x4 tires and tubes with Airglass Engineering Company adapters LWA 950. Issued 1/1/1960
SA502AL Installation of cargo door in right side of aircraft. Amended 10/31/1973
SA505AL Installation of landing gear safety cables. Issued 10/1/1973
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA528AL Installation of welded steel rear float fittings. Reissued 2/20/1976
SA534AL Installation of auxiliary fuel tank. Reissued 1/26/2012
SA538AL Installation of modified landing gear (PA-18 type) with main landing gear legs lengthened6 inches. Reissued 9/11/2009
SA541AL Installation of Avco Lycoming O-360-A2A engine and McCauley 1A200/DFA8245 propeller. For PA-14 normal category only. Amended 9/25/2002
SA546AL Installation of Day & Night 4-1 fiberglass propeller spinner. Reissued 9/11/2009
SA548AL Installation of Piper PA-18 type landing gear. Reissued 9/11/2009
SA562AL Installation of Day & Night 2-4 aluminum engine cowling. Reissued 9/11/2009
SA567AL Installation of O-320-A2B Lycoming engine. Reissued 9/11/2009
SA573SW Installation of Plane Booster wing tip kit 101-250. Reissued 1/28/1996
SA5781NM Installation of Model 3140-51630.5 gallon wing fuel tanks. Amended 1/9/2004
SA57NW Installation of Lycoming O-320 series engine McCauley 1A170/1C172 and Sensenich M74DM propellers and associated alternator systems Amended 3/6/1974
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
SA593AL  Installation of Day & Night Inc. square horizontal stabilizers elevators and rudder on Piper Model PA-14 airplanes Reissued 9/11/2009
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA594AL Installation of Day & Night Inc. extended flaps and modified ailerons and flap control system on a Piper Model PA-14 airplane Reissued 9/11/2009
SA595AL  Installation of Day & Night Inc. swept vertical tail and reduced-sized square horizontal surfaces on a Piper Model PA-14 airplane Reissued 9/11/2009
SA598AL Installation of Day & Night modified flap control system. Reissued 9/11/2009
SA600AL Extend flaps and modified aileron and flap control sys. Reissued 9/11/2009
SA615EA (PAGE 2) 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
SA630AL Install fiberglass wing tip assembly. Issued 4/28/1978
SA645AL Install Avco Lycoming O-320-D2A or O-320-B2B engine and McCauley1A175/GM8246 prop. Issued 7/31/1978
SA647AL Install Motorola 32.5 amp alternator. Issued 8/4/1978
SA657AL Install Avco Lycoming O-320-A2B or O-320-E2D engine and McCauley1A175/GM 8246 propeller. Issued 11/27/1978
SA686AL Installation of PA-18 main landing gear. Issued 7/8/1980
SA688AL Installation of left side cabin door. Issued 7/16/1980
SA690AL Increase gross weight to 1 935 lbs. Issued 7/8/1980
SA702AL Installation of skis. Issued 11/24/1980
SA717AL Installation of Schneider Model SWS-4000 main wheel skis and Schneider Model SWS-1000 tail wheel skis. Issued 4/6/1982
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA800EA (PAGE 2) 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
SA8075SW (PAGE 3) Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) Reissued 11/10/2003 0:00
SA83AL Installation of Lycoming O-320 Series engines and Sensenich M74DM propeller and Stoddard engine mount 501. (PA-14 Seaplane) Reissued 7/9/1981
SA950GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA95AL Maule SFS-1-4-P8 tail wheel Hayes D-15-26 brake assembly using Kennedy Air Service adapter 64-1 Hayes wheel assembly D3-105MD and800x6 850x6 or 900x6 4-ply tires and tubes. Issued 1/1/1960
SA98CH Installation of replacement wing ribs. Amended 1/13/1997
SA99AL Installation of six-inch wheels and brakes. Reissued 7/9/1981
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
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
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
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
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)


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