CHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS

Size: px
Start display at page:

Download "CHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS"

Transcription

1 CHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS General...2 Kinds of Operations...2 Structural and weight limitations...2 Maneuvering limitations...3 Flight load factor limitations...3 Power plant limitations...3 Engine starter limitations...3 Engine operating limitations...3 Oil limitations...4 Propeller limitations...4 Fuel limitations...4 Electrical System limitations...5 Airspeeds limitations...5 Airspeed indicator markings...5 Normal operations airspeeds...6 Emergency operations airspeeds...7 Training maneuvers limitations...7 Excerpts from Airworthiness directives / Service Bulletins... NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 1

2 General This section presents a partial summary of the operating limitations and aircraft information necessary for the safe operation of the PA28R200 Arrow. This section is provided for quick reference only, and is not intended to substitute the approved Aircraft Flight Manual and other official materials. All BSU Aircraft are operated in accordance with the FAA regulations and BSU Aviation policies and procedures. In some cases, BSU policies and procedures will be more restrictive. Pilots shall refer to the BSU AOM and be familiar with/adhere to all general BSU aircraft operating procedures. In all cases, pilots operating the BSU Piper PA28R200 Arrow shall be thoroughly familiar with the information contained in the approved Aircraft Flight Manual, FAA regulations and applicable BSU Aviation policies and procedures. Observance of these limitations is mandatory. This chapter provides only a partial summary of limitations in accordance with the Aircraft Flight Manual. Pilots must refer to the Aircraft Flight Manual and BSU Aviation Operations manual to become familiarize with all required information. NOTE For aircraft equipped with specific options, refer to the Pilot s Information Manual (PIM) and FAA Approved Airplane Flight Manual (AFM) for amended operating limitations, procedures, performance data and/or other necessary information. Kinds of Operations The airplane is approved for the following operations when equipped in accordance with 14 CFR Part 91: Day V.F.R. Night V.F.R. Day I.F.R. Night I.F.R. Non-icing The BSU PA28R200 Arrow is not equipped for flight into icing conditions. Structural and Weight Limitations Flight into known icing conditions is PROHIBITED. Maximum Ramp Weight...2,658 lbs Maximum Takeoff Weight...2,650 lbs Maximum Landing Weight)...2,650 lbs Rear Baggage Area Maximum Weight lbs NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 2

3 Maneuvering Limitations The PA28R200 Arrow is rated in the Normal category only. The only authorized maneuvers in the Arrow are those maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and steep turns (with not more than 60 0 of bank). W A R N I N G Avoid any situations and maneuvers that may place the aircraft outside of the approved Normal category limits. All intentional aerobatic maneuvers, including SPINS are PROHIBITED. Flight Load Factor Limitations - Normal Category Positive Load Limit Negative Load Limit +3.8 g Flaps Up No inverted maneuvers approved. Power Plant Limitations Manufacturer... Lycoming Model Numbers... IO-360-C1C Maximum Horsepower BHP Maximum Engine Rotation Speed (RPM) Minimum Fuel Flow psi (2.0 gal/hr) Minimum Fuel Pressure psi Maximum Fuel Flow psi (21.4 gal/hr) Maximum Fuel Pressure psi Fuel Minimum Grade (Green) / 100 LL (Blue) Engine Starter Limitations Maximum continuous cranking time (single start attempt) seconds Minimum cool-down time between attempts seconds Maximum number of start attempts...3 Engine Operating Limitations (all operations) Maximum Continuous Power RPM Maximum RPM for all operations RPM Maximum Oil Temperature F Oil Temperature Range (Normal) F Maximum Oil Pressure...90 psi Oil pressure range (normal) psi Minimum Oil Pressure...25 psi NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 3

4 Power Plant Instrument Markings INSTRUMENT Tachometer (RPM) Oil Pressure (PSI) Oil Temp. ( 0 F) Fuel Flow/Press. (GPH) Vacuum Press. (Hg) Red Line (Min) Green Arc Normal Red Line (Max) (Range at Idle) gph 21.4 gph 21.4 gph 14 psi psi 45 psi NOTE Proper engine (oil) temperature management is critical to air-cooled engine reliability and maximum service life. Flight crews will monitor oil temperature and adjust airspeed, climb gradient and power/mixture settings, as appropriate, in accordance with the AFM and above limitations for all operations. Oil Limitations Maximum Oil Capacity (per engine)... 8 qts Minimum Oil Quantity (per engine) / Flight of under 2 hours (BSU Policy)... 6 qts Minimum Oil Quantity (per engine) / Flight of 2 hours or more (BSU Policy)... 7 qts Do not operate the engine with less than six (6) quarts of oil. Propeller Specifications and Limitations Manufacturer... Hartzell / Model HC-C2YK-1/7666A-2 Type... Controllable Pitch Max. Diameter Min. Diameter Blade Angle Low Limit / Blade Angle High Limit / Avoid continuous static operations (over 5 minutes) between RPM below 15 of manifold pressure. NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 4

5 Fuel Limitations Approved Fuel... Aviation Grade 100LL (Blue) or 100 (Green) Total Capacity (all tanks) Gallons Total Usable Fuel (all tanks) Gallons Total Unusable Fuel (all tanks)... 2 Gallons Usable Fuel (each wing tank) gallons Unusable Fuel (each wing tank)... 1 Gallon W A R N I N G The fuel remaining in the tank(s) when the quantity indicator reads zero cannot be safely used in flight. Flight crews shall avoid maneuvers that could uncover or un-port the wing outlet in the fuel tanks. Un-porting can result in fuel flow interruption and power loss. Avoid extreme running takeoffs, slips/skids resulting in altitude loss in excess of 2000, or other radical or extreme maneuvers. Electrical System Limitations Electrical system voltage Volts Alternator Output Volts Amps Load... Maximum 60 Amps Battery Output / Capacity Volts / 25 Amp/hour Minimum voltage to attempt engine start Volts W A R N I N G Alternator must be functional to initiate a flight. Departing on battery power alone, without a functional alternator, is prohibited. Airspeed Limitations The Airspeed Indicator for this aircraft is marked on the OUTER RING as MPH (miles per hour) and as KIAS on the INNER RING. Flight crews must take care to adhere to published airspeed limitations regardless of the type of marking used. NOTE The primary airspeed reference for the purposes of this manual will be in MILES PER HOUR (MPH). NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 5

6 Instrument Marking White Arc Green Arc Yellow Arc Airspeed Indicator Markings Explanation Full Flap Operating Range: Lower limit is max. weight V SO in the landing configuration. Upper limit is maximum speed permissible with flaps fully extended. Normal Operating Range: Lower limit is max. weight V S1 with flaps retracted. The upper limit is V NO. Caution Range: Flight in this range is limited to smooth air only, and then with caution. MPH Red Line Never Exceed Speed: Maximum speed for all operations. 214 NOTE The maximum crosswind component for this aircraft is 17 KNOTS (20 MPH) The maximum crosswind component allowed for any BSU PA28R200 operations is 17 KNOTS (20 MPH), unless specifically authorized otherwise prior to flight. NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 6

7 NORMAL OPERATIONS AIRSPEEDS Symbol Reference Definition MPH V FE Max Flap Extend Speed Do not deploy wing flaps above this speed, and do not exceed this speed with wing flaps extended V LO V LE Max Landing Gear Operating Speed Max. Landing Gear Extended Speed Do not cycle the landing gear above these speeds. UP DOWN Do not exceed this speed with the landing gear extended V A Maneuvering Speed Do not make full or abrupt control movements above this speed lbs lbs. V NO Max Structural Cruising Speed Do not exceed this speed except in smooth air, and then only with extreme caution V NE Never Exceed Speed Maximum speed for all operations. V S1 Stall Speed, Specified Stall speed in a specified Configuration configuration, flaps up V SO Stall Speed, Landing Configuration Stall speed in the landing configuration, typically flaps down Vr Rotation speed Rotate at this speed on take-off Normal Short-field V X V Y Best Angle of Climb (max climb over distance) Best Rate of Climb (max vertical speed in climb) Maintain this speed until clear of obstacles, to gain maximum altitude in minimum forward distance Gear DOWN Gear UP Maintain this speed to gain greatest altitude in minimum time Gear DOWN Gear UP V climb Enroute or cruise climb speed Maintain this speed for the best combination of visibility, engine cooling and climb performance Traffic Pattern Typical speed to be maintained Maintain this airspeed in the at TPA, if appropriate downwind leg of a traffic pattern V ref(normal) Final approach speed / NORMAL landing Maintain this airspeed on final approach (with no gusts) V ref(short) Final approach speed / SHORT- FIELD landing Maintain this airspeed on final approach (with no gusts) 83 V ref(no flap) X/W component Final approach speed / NO FLAP landing Maximum crosswind component on takeoff and landing Maintain this airspeed on final approach (with no gusts) Do not intentionally exceed this crosswind component on takeoff and landing mph / 17 knots NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 7

8 EMERGENCY OPERATIONS AIRSPEEDS Symbol Reference Definition MPH V ref(no flap) V G Final approach speed / NO FLAP landing Best Glide Speed (engine inoperative) Maintain this airspeed on final approach during no-flap landings (with no gusts) Maintain this speed with the engine inoperative Training maneuvers limitations W A R N I N G No intentional touch-and-go operations are permitted in BSU retractable gear aircraft. Full stop / stop-and-go landings are authorized only. All intentional aerobatic maneuvers, including spins, are prohibited. Min. altitude for any portion of stalls and slow flight, including recovery, is 1500 AGL. Intentional banks in excess of 60 are prohibited. Airworthiness Directives The following section lists the current Airworthiness Directives and Service Bulletins for the Piper PA-28R-200 Arrow. Flight crews are responsible for reviewing the maintenance summary sheet to ensure that the aircraft is in compliance with the following ADs and SBs: AD R1 Main Gear Side-brace Stud This amendment revises (AD) , which currently requires repetitively inspecting the main gear side-brace studs for cracks on (Piper) Models PA-28R series airplanes, and replacing any main gear side-brace stud found cracked. The FAA has approved certain alternative methods of compliance (AMOC) for AD This AD retains all the actions of AD , and will incorporate certain AMOC s as a way of accomplishing the actions specified in AD The actions specified by this AD are intended to prevent a main landing gear collapse caused by main gear side-brace stud cracks, which could result in loss of control of the airplane during landing operations. Effective 12/8/98. AD Flap Handle Attachment Bolt The FAA issued this AD to require inspection and modification of the flap lever assembly. Reports of worn flap handle attach bolts and elongated holes in the flap lever to cable mounting attach point prompted issuance of the AD. The AD requirements are intended to prevent failure of the flap handle attach bolt and sudden retraction of the flaps, which, if not detected and NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 8

9 corrected, could result in loss of control of the airplane. Compliance time was established as follows: with a 2,000 hour TIS threshold or within the next 100 hours TIS for those airplanes with greater than 2,000 hours TIS. Effective 6/14/96. AD Oil Cooler Hose Inspection Numerous incidents/accidents caused by oil cooler hose rupture or failure on the affected airplanes prompted this action. This amendment superseded (AD) , which required replacing oil cooler hoses on Piper Model PA airplanes, and inspecting for a minimum clearance between the oil cooler hose assemblies and the front exhaust stacks and adjusting if proper clearance was not obtained. This AD maintains the clearance inspection and oil cooler hose replacements, requires this inspection and these replacements to be repetitive, and extends the applicability to include other PA28 series airplanes. It also provides the option of installing approved TSO-C53a, Type D oil cooler hose assemblies as terminating action for the repetitive inspection requirement. The actions specified by this AD are intended to prevent these oil cooler hoses from failing or rupturing, which could result in engine stoppage and subsequent loss of control of the airplane. This AD requires a repetitive 100-hour time-in-service (TIS) inspection and 8-year (or 1,000 hours TIS) repetitive oil cooler hose assembly replacement. Effective 2/05/96. AD Nose Landing Gear Modification This AD requires installing a certain nose landing gear modification kit (Piper part number (P/N) ). Several service difficulty reports of collapsed nose gear on the affected airplanes prompted the AD. The reports revealed failure of the bolt (AN4-20) connecting the lower nose gear drag link to the upper drag link. The actions specified by this AD are intended to prevent nose gear collapse because of AN4-20 bolt failure, which could lead to airplane damage. Effective 8/19/94. AD Ammeter Replacement This AD was issued to prevent smoke in the cockpit and possibly complete electrical failure resulting from shorting of ammeter terminal posts, and required the following: Within 50 hours time-in-service (TIS) after the effective date of the AD, replacement of the ammeter(s) with Ammeter Replacement Kit(s), Piper Part No , on the above listed airplanes in accordance with the instructions contained in Piper Service Bulletin No. 811A, dated May 12, Effective 8/21/86. AD Nose Landing Gear, Inspect, Rig, Modify This AD was issued to require modification of the nose landing gear that would prevent the inadvertent retraction of the nose landing gear. Within the next 100 hours time-in-service after the effective date of the AD, owners/operators are required to inspect, rig and modify the nose landing gear in accordance with Piper Service Bulletin No. 724A, dated April 20, 1982, Parts I and II as applicable, except dye penetrant must be used for detection of cracks. A record of compliance with this AD is required via an appropriate entry in the airplane maintenance records. Effective 6/16/82. NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 9

10 AD Oil Drain Valves This AD requires compliance within the next 50 hours time in service (TIS) or at the next oil change, whichever comes first, after the effective date of the AD (unless it has already accomplished). The AD was issued to prevent possible loss of oil due to installation of an incorrect engine oil quick drain valve. The AD requires installation of two warning placards, one on each side, on the lower engine mount beneath the intake and exhaust tubes. For those airplanes equipped with an engine oil quick drain valve, the following actions are required: Inspection of the oil quick drain valve and installation and correct safety wiring of Piper Part No V. If an incorrect valve is installed, replace with Piper PN V, and safety wire. Effective 10/2/81. AD Carbon Monoxide in Cabin This AD was issued to prevent possible leakage of carbon monoxide into the cabin. Compliance is required within the next 50 hours time in service (TIS) after the effective date of the AD unless already accomplished, and includes the following actions: Removal of upper and lower engine cowling, removal and discard of clips on muffler shroud end plates, inspection for movement between the muffler shroud end plates and the muffler pipes. Piper Service Bulletin No. 691, dated August 6, 1980, pertains to this subject. Effective 9/12/80. AD Control Rod Ends This AD applied to PA-28R-200 serial numbers 28R through 28R , and was issued to prevent power loss due to thermal contraction binding on a control rod end. Inspection of the rod bearing ends for the throttle, mixture, and propeller controls was required to be performed within 25 hours after issuance of the AD. If the rod bearing ends did not pass inspection, replacement with a serviceable part was required. Effective 11/14/77. AD Fuel Quantity Indicators This AD applied to PA-28R-200 serial numbers 28R through , and was intended to prevent fuel exhaustion resulting erroneous readings on the fuel gauges. The AD required the installation of a placard reading "WARNING FUEL GAUGES MAY INDICATE AS MUCH AS 2 1/2 GALLONS WHEN TANKS ARE EMPTY" within 10 hours TIS after issuance of the AD, and an inspection of the gauges for proper operation within the next 200 hours TIS or 12 calendar months, whichever came first. Effective 1/7/77. AD Nose Gear Trunnion This AD applied to PA-28R-200 serial numbers 28R to 28R inclusive, and all PA-28R-200 airplanes that had the Nose Gear Trunnion Assembly (Piper part number V) replaced with one supplied by the manufacturer between 8/1/75 and 8/1/76. The AD required a visual inspection of the nose gear trunnion to detect any obvious cracks on the trunnion ear that attaches to the nose landing gear arm spring. The AD allowed the inspection to be conducted by the pilot or by other persons authorized to perform preventive maintenance under FAR 43. Effective 8/6/1976. NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 10

11 AD Rear Seat Leg Inspection This AD was issued to prevent the seats from coming loose during an accident, and required an inspection within the next 100 hours time in service or at the next annual inspection, whichever came first. The inspection required inspection of the rear legs on the quick-disconnect seats in accordance with Piper Service Letter No. 763, and adjustment or replacement of any component that did not pass inspection. Effective November 21, AD Fuel Drain Valves This AD was issued to detect and correct an unsecured fuel drain valves installed at the gascolator. Compliance was required prior to next flight (or 50 hours time in service after the effective date of the AD) unless already accomplished, and was to be accomplished by a pilot check of the fuel gascolator drain valve, (Piper Part No ) to determine if it is tight in the fitting by attempting to turn the valve counter-clockwise by hand. Effective April 4, AD Rear Seatbelt Installation This AD was issued to require the installation of improved rear seat belt by relocating the rear seat safety belt outboard attachments in accordance with Piper Service Bulletin Number 393. Effective 4/24/74. Service Bulletin No. 866A Backup Landing Gear Extender Removal The Piper PA-28R Back Up Gear Extender System was designed as a safety device to help prevent both inadvertent landing with the gear retracted and premature retraction of the gear during takeoff. When correctly operated and maintained, the system automatically extends the landing gear when the airspeed falls below a certain value, and also prevents the landing gear from being retracted before a specified airspeed. Allegedly, properly functioning systems were contributing factors in certain aircraft accidents, propagated by other emergencies. Piper issued Service Bulletin No. 866A, requiring the removal of the BGE system to eliminate the possibility of accidents occurring due to the system. NF ISSUE 9/12 AIRCRAFT INFORMATION SUMMARY 11

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A13CE

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A13CE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A13CE Revision 28 CESSNA 177 177A 177B November 16, 2010 TYPE CERTIFICATE DATA SHEET NO. A13CE WARNING: Use of alcohol-based fuels can cause

More information

a. Lycoming IO-520J 250 HP c. Lycoming O-540-J3C5D 235 HP b. Continental O450T 330 HP d. Lycoming O-360A 180 HP

a. Lycoming IO-520J 250 HP c. Lycoming O-540-J3C5D 235 HP b. Continental O450T 330 HP d. Lycoming O-360A 180 HP Three points each question Page 1 of 6 References: Pilot's Operating Handbook for the 1979 Cessna R182 Model; Flying Magazine Article "Cessna 182 Safety Report;" RAFA SOP; and Refueling Instructions found

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11EA Revision 9 American General Aircraft Holding Co. AA-1 AA-1A AA-1B AA-1C June 7, 1995 TYPE CERTIFICATE DATA SHEET NO. A11EA This data sheet,

More information

PA-28R 201 Piper Arrow

PA-28R 201 Piper Arrow Beale Aero Club Aircraft Written Test PA-28R 201 Piper Arrow (Required passing score: 80%) 1. If an engine power loss occurs immediately after take off, the pilot s reaction should be to: a. maintain safe

More information

TYPE CERTIFICATE DATA SHEET 2A10

TYPE CERTIFICATE DATA SHEET 2A10 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2A10 Revision 23 LAVIA S.A. PA-25 PA-25-235 PA-25-260 TYPE CERTIFICATE DATA SHEET 2A10 November 30, 2000 This data sheet which is a part of

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A16EA Revision 15 True Flight Holdings LLC AA-5, AA-5A, AA-5B AG-5B September 18, 2009 TYPE CERTIFICATE DATA SHEET NO. A16EA This data sheet,

More information

TYPE CERTIFICATE DATA SHEET 2A8

TYPE CERTIFICATE DATA SHEET 2A8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET 2A8 2A8 Revision 20 LAVIA S.A. PA-25 PA-25-235 PA-25-260 November 30, 2000 This data sheet which is part of Type

More information

TYPE CERTIFICATE DATA SHEET 2A10

TYPE CERTIFICATE DATA SHEET 2A10 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2A10 Revision 28 LAVIA ARGENTINA S.A. PA-25 PA-25-235 PA-25-260 TYPE CERTIFICATE DATA SHEET 2A10 July 2, 2013 This data sheet which is a part

More information

Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures

Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures Flight Express, Inc. This take-home self-test partially satisfies the recurrent ground training

More information

PA28R ARROW CHECKLIST

PA28R ARROW CHECKLIST PA28R ARROW CHECKLIST 2300.11.0112 1 Normal Procedures Initial PREFLIGHT CHECK General Appearance... CHECKED Position & Taxi Path... CHECKED Tie Downs, Locks, Chocks & Covers... REMOVED Cockpit Controls...UNLOCKED

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 1A13 Revision 27 Revo, Inc. COLONIAL C-1 COLONIAL C-2 LAKE LA-4 LAKE LA-4A LAKE LA-4P LAKE LA-4-200 LAKE

More information

DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test. Cessna - 182

DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test. Cessna - 182 DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 182 For the following questions, you will need to refer to the Pilots Information Manual for the C-182R. The bonus questions

More information

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation.

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. AIRCRAFT FLASHCARDS Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. Knowing your aircraft well is essential to safe flying. These

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST FEB 2014 Elmendorf Aero Club Aircraft Test Cessna - 185 For the following questions, you will need to refer to the Pilots Information Manual for the C-185F and Graphic Engine

More information

SECTION 2 LIMITATIONS

SECTION 2 LIMITATIONS GENERAL This section includes operating limitations, instrument markings, and basic placards required for safe operation of the helicopter, its engine, and other standard systems. This helicopter is approved

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.073 for Beechcraft 390 (PREMIER I and IA) Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 USA For Models: Model 390 1

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A6 Revision 33 PIPER PA-22 PA-22-108 PA-22-135 PA-22S-135 PA-22-150 PA-22S-150 PA-22-160 PA-22S-160 February 12, 1999 AIRCRAFT SPECIFICATION

More information

FAA APPROVED FOR MAULE M-5-180C. (S/n s 8070C 8094C) Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.

FAA APPROVED FOR MAULE M-5-180C. (S/n s 8070C 8094C) Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED FOR Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED: Manager, Aircraft Certification Office Federal Aviation Administration Atlanta,

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 172 For the following questions, you will need to refer to the Pilots Information Manual for the C-172R (180hp). The bonus

More information

3. What is the total fuel capacity with normal tanks? Usable? 4. What is the total fuel capacity with long range tanks? Usable?

3. What is the total fuel capacity with normal tanks? Usable? 4. What is the total fuel capacity with long range tanks? Usable? Pilot Name: Last, first, mi. Date: (mo/dy/yr) Instructor: Pass/Fail: Instructors Initials: 1. What is the engine Manufacturer: Model: Type: 2. What is the horsepower rating? 3. What is the total fuel capacity

More information

FAA Approved Airplane Flight Manual Supplement

FAA Approved Airplane Flight Manual Supplement FAA Approved Airplane Flight Manual Supplement DOCUMENT NUMBER 172060 For Serial No. 17271035 and 17274009 Serial No: Reg. #: This supplement must be attached to the Pilots Operating Handbook and the FAA

More information

Jump to Table of Contents

Jump to Table of Contents Jump to Table of Contents PIPER AIRCRAFT CORPORATION PA-28R-201, CHEROKEE ARROW III SECTION 3 EMERGENCY PROCEDURES 3.3 EMERGENCY PROCEDURES CHECK LIST ENGINE FIRE DURING

More information

RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (9/25/2016) "A Safe Pilot Knows His Equipment"

RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (9/25/2016) A Safe Pilot Knows His Equipment RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (9/25/2016) "A Safe Pilot Knows His Equipment" NAME: Date: Aircraft: Cessna 182Q Registration Number: N631S Serial Number: The purpose of this questionnaire is to

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A19SO

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A19SO DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A19SO Revison 14 Piper Aircraft, Inc PA-44-180 PA-44-180T TYPE CERTIFICATE DATA SHEET NO. A19SO October 28, 2014 This data sheet, which is part

More information

FAA Approved Supplemental Airplane Flight Manual

FAA Approved Supplemental Airplane Flight Manual FAA Approved Supplemental Airplane Flight Manual DOCUMENT NUMBER 172056 For Serial No. 17265685 to 17271034 Serial No: Reg. #: The information contained in this flight manual is FAA Approved Material,

More information

PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, YERO BEACH, RA.

PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, YERO BEACH, RA. r'refared DEVELOPMENT CENTER, YERO BEACH, RA. AIRPLANE FLIGHT MANUAL MODEL PA - 28-180 FAA IDENTIFICATION NO. SERIAL NO. N8338W 28-2520 THIS DOCUMENT MUST BE KEPT IN AIRPLANE AT ALL TIMES. FAA : Original

More information

Liberty Aerospace, Inc. Section 1 SECTION 1 GENERAL TABLE OF CONTENTS

Liberty Aerospace, Inc. Section 1 SECTION 1 GENERAL TABLE OF CONTENTS Liberty Aerospace, Inc. Section 1 SECTION 1 TABLE OF CONTENTS Introduction... 1-3 Airplane Three Views... 1-4 Descriptive Data... 1-5 Engine... 1-5 Propeller... 1-5 Fuel... 1-5 Oil... 1-5 Maximum Certificated

More information

RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (6/3/2018) "A Safe Pilot Knows His Equipment"

RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (6/3/2018) A Safe Pilot Knows His Equipment RFC Dallas, Inc. AIRCRAFT QUESTIONNAIRE (6/3/2018) "A Safe Pilot Knows His Equipment" NAME: Date: Aircraft: Bonanza Registration Number: Serial Number: The purpose of this questionnaire is to aid the pilot

More information

OUTLINE. Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions

OUTLINE. Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions T-34B GROUND SCHOOL OUTLINE Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions COMMERCIAL REQUIREMENTS 61.129 Aeronautical experience. (a) For an airplane

More information

AIR TRACTOR, INC. OLNEY, TEXAS

AIR TRACTOR, INC. OLNEY, TEXAS TABLE OF CONTENTS LOG OF REVISIONS... 2 DESCRIPTION... 4 SECTION 1 LIMITATIONS... 5 SECTION 2 NORMAL PROCEDURES... 8 SECTION 3 EMERGENCY PROCEDURES... 8 SECTION 4 MANUFACTURER'S SECTION - PERFORMANCE...

More information

USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017

USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017 USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017 Instructions Complete the supplement following exam using the answer sheet provided. Do not assume information not specifically

More information

EGLIN AERO CLUB C-172 OPEN BOOK EXAMINATION Apr Total usable fuel capacity for the aircraft with long range tanks is:

EGLIN AERO CLUB C-172 OPEN BOOK EXAMINATION Apr Total usable fuel capacity for the aircraft with long range tanks is: (The following questions are taken from the C-172N POH) 1. Total usable fuel capacity for the aircraft with long range tanks is: a. 54 gallons b. 50 gallons c. 62 gallons d. 40 gallons 2. Total fuel capacity

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 182 For the following questions, you will need to refer to the Pilots Information Manual for the C-182R. The bonus questions

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna 172RG For the following questions, you will need to refer to the Pilots Information Manual for the C-172RG and the Auxiliary

More information

AIRCRAFT FAMILIARIZATION. Some questions may not apply to the aircraft you are flying.

AIRCRAFT FAMILIARIZATION. Some questions may not apply to the aircraft you are flying. 541-895-5935 Name Date AIRCRAFT FAMILIARIZATION Note: If this information is not provided in the aircraft s flight manual give it your best guess. Some questions may not apply to the aircraft you are flying.

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET S205-S208 Page 1 TYPE-CERTIFICATE DATA SHEET No. EASA.A.587 S205 S208 Type Certificate Holder: LEONARDO S.p.A. Divisione Velivoli Piazza Monte Grappa, 4 00195 Rome Italy Airworthiness Category: Small Aeroplanes

More information

Performance That Counts! 2099 Georgia Highway 133 South Moultrie, GA (229) Fax: (229) or (229)

Performance That Counts! 2099 Georgia Highway 133 South Moultrie, GA (229) Fax: (229) or (229) Performance That Counts! 2099 Georgia Highway 133 South Moultrie, GA 31788 (229) 985-2045 Fax: (229) 985-2048 or (229) 890-2402 www.mauleairinc.com LOG OF REVISIONS REV. TO PAGES DESCRIPTION APPROVAL AND

More information

GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #:

GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #: GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E Name: GACE #: Score: Checked by: CFI #: Date: (The majority of these questions are for N5312S. All N5928E questions will be marked 28E) 1. What

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A18SW Revision 2 Fairchild Aircraft, Inc. SA227-CC SA227-DC (C-26B) November 14, 1996 TYPE CERTIFICATE DATA SHEET A18SW Type Certificate Holder:

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 5A5

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 5A5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A5 Revision 30 Cessna (USAF 0-1A) 305A (USAF 0-1E) 305C (USAF 0-1G) 305D 305F April 4, 1994 AIRCRAFT SPECIFICATION NO. 5A5 Type Certificate

More information

Hawker Beechcraft Corporation on March 26, 2007

Hawker Beechcraft Corporation on March 26, 2007 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00010WI Revision 8 Hawker Beechcraft 390 March 26, 2007 TYPE CERTIFICATE DATA SHEET NO. A00010WI This data sheet, which is part of Type Certificate

More information

Cessna 172RG WARNING. Maximum Demonstrated Crosswind. Takeoff or landing..15 KTS

Cessna 172RG WARNING. Maximum Demonstrated Crosswind. Takeoff or landing..15 KTS Cessna 172RG INTRODUCTION: This aircraft checklist contains information from the original manufacturer s Pilot Information Manual. Normal procedures associated with optional systems can be found in Section

More information

FAA APPROVED FOR MAULE MX-7-180A. Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.

FAA APPROVED FOR MAULE MX-7-180A. Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED FOR Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED: Manager, Aircraft Certification Office Federal Aviation Administration Atlanta,

More information

Van s Aircraft RV-7A. Pilot s Operating Handbook N585RV

Van s Aircraft RV-7A. Pilot s Operating Handbook N585RV Van s Aircraft RV-7A Pilot s Operating Handbook N585RV PERFORMANCE SPECIFICATIONS SPAN:..25 0 LENGTH...20 4 HEIGHT:.. 7 10 SPEED: Maximum at Sea Level...180 knots Cruise, 75% Power at 8,000 Ft...170 knots

More information

CARENADO COPYRIGHTS. Normal & Emergency Checklist

CARENADO COPYRIGHTS. Normal & Emergency Checklist NORMAL PROCEDURES CHECKLIST PREFLIGHT CHECK Control wheel -- RELEASE BELTS Avionics -- OFF Master Switch -- ON Fuel quantity gauges -- CHECK Master switch -- OFF Ignition -- OFF Exterior -- CHECK FOR DAMAGE

More information

Piper Archer II (PA )

Piper Archer II (PA ) 1. Oil... 6-8 qts, Cap Secure CABIN 1. POH & Documents.. Check Available 2. Magneto Switch...... OFF 3. Pitot/Static Drains... Push to Drain 4. Avionics/Electrical Switches... OFF 5. Master Switch. ON

More information

TYPE CERTIFICATE DATA SHEET NO. A8SO

TYPE CERTIFICATE DATA SHEET NO. A8SO DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A8SO Revision 21 (Pitts) S-1S S-1T S-2 S-2A S-2S S-2B S-2C February 15, 2005 TYPE CERTIFICATE DATA SHEET NO. A8SO This data sheet, which is

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines)

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines) DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-804 Revision 14 LAND-AIR (TEMCO) (LUSCOMBE) 11A 11E April 6, 2005 AIRCRAFT SPECIFICATION NO. A-804 Type Certificate Holder Luscombe Aircraft

More information

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures..

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures.. INDEX Preflight Inspection Pages 2-4 Start Up.. Page 5 Take Off. Page 6 Approach to Landing. Pages 7-8 Emergency Procedures.. Page 9 Engine Failure Pages 10-13 Propeller Governor Failure Page 14 Fire.

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.A.607 for BS 115 Type Certificate Holder BLACKSHAPE S.P.A. Strada Statale 16 KM 841+900 70043 Monopoli (BA) ITALY For models: BS 115 TE.CERT.00048-001 European Aviation

More information

CESSNA P 337 H Pressurized Skymaster

CESSNA P 337 H Pressurized Skymaster CESSNA P 337 H Pressurized Skymaster N777SN Quick reference training guide This training manual cannot be used as a substitute for the official pilots operating handbook. Page 1 - 1. Take off (normal)

More information

Aircraft Checklist Commander 114

Aircraft Checklist Commander 114 Aircraft Checklist Commander 114 This is an abbreviated checklist. Most explanatory items, notes cautions and warnings have been omitted for brevity. Procedures in red/bold text in this checklist should

More information

Vso 61. Vs1 63. Vr 70. Vx 76. Vxse 78. Vy 89. Vyse. 89 (blue line) Vmc. 61 (radial redline) Vsse 76. Va 134) Vno 163

Vso 61. Vs1 63. Vr 70. Vx 76. Vxse 78. Vy 89. Vyse. 89 (blue line) Vmc. 61 (radial redline) Vsse 76. Va 134) Vno 163 PA34-200T Piper Seneca II Normal procedures V-speeds Knots Vso 6 Vs 63 Vr 70 Vx 76 Vxse 78 Vy 89 Vyse Vmc 89 (blue line) 6 (radial redline) Vsse 76 Va 2-36(@4507lbs 34) Vno 63 Vfe 38 (0*)/2(25*)/07(40*)

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A49NM Jetcruzer 450 June 14, 1994 TYPE CERTIFICATE DATA SHEET NO. A49NM This data sheet which is a part of Type Certificate A49NM, prescribes

More information

N1523J CHECKLIST PA Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE Tel. (402)

N1523J CHECKLIST PA Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE Tel. (402) CHECKLIST N1523J 1967 Cherokee 140 PA-28-140 F Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE 68110 Tel. (402) 342-4314 www.nebflight.com Piper Cherokee 140 N1523J 1967 GENERAL INFORMATION

More information

European Aviation Safety Agency

European Aviation Safety Agency TCDS A.075 GROB G 120 Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET G 120 Type Certificate Holder: GROB Aircraft AG Manufacturer: GROB Aircraft AG For Models: G 120A G 120A-I

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A9. 4 Baltimore Avenue Georgetown, DE 19947

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A9. 4 Baltimore Avenue Georgetown, DE 19947 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A9 1A9 Revision 18 Taylorcraft 2000, LLC 19 F19 F21 F21A F21B F22 F22A F22B F22C August 8, 2000 Type Certificate

More information

Registration Number. Serial Number

Registration Number. Serial Number Registration Number Serial Number This supplement must be attached to the DMCR Approved Airplane Flight Manual listed on page 2 of this supplement or later approved revision and must be carried in the

More information

I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK

I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK SCHODACK AVIATION Page 1 of 10 I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK 1. Flight Planning 1. Aircraft requirements & preparation: Required aircraft documents: Airworthiness Certificate Registration

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A21CE

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A21CE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A2CE A2CE Revision American Champion (Bellanca) (Champion) August 25, 997 This data sheet, which is part of

More information

Registration Number. Serial Number

Registration Number. Serial Number Registration Number Serial Number This supplement must be attached to the DMCR Approved Airplane Flight Manual dated October 1, 1954 or later approved revision and must be carried in the airplane when

More information

FAA APPROVED FOR MAULE MX Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.

FAA APPROVED FOR MAULE MX Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED FOR Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED: Manager, Aircraft Certification Office Federal Aviation Administration Atlanta,

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes Mooney M20 Series 28 August 2014 Notes 1. This AD schedule is applicable to Mooney Aircraft Corp. M20C, M20E, M20F, M20G M20J, M20M, and M20R aircraft manufactured

More information

I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK

I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK SCHODACK AVIATION Page 1 of 10 I. DISPATCH PLANNING & AIRCRAFT EXTERIOR CHECK 1. Flight Planning 1. Aircraft requirements & preparation: 1. Required aircraft documents: 1. Airworthiness Certificate 2.

More information

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE The Critical Engine The critical engine is the engine whose failure would most adversely affect the airplane s performance or handling

More information

SECTION 2 LIMITATIONS

SECTION 2 LIMITATIONS SECTION 2 TABLE OF CONTENTS PARAGRAPH PAGE 2.1 INTRODUCTION 2-1 2.2 KINDS OF OPERATIONS LIMITS 2-1 2.3 AIRSPEED 2-3 2.4 AIRSPEED INDICATOR MARKINGS 2-3 2.5 POWER PLANT 2-4 2.6 POWER PLANT INSTRUMENT MARKINGS

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1/8 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Cirrus Design SF50 Type Certificate Holder: Cirrus Design Corporation 4515 Taylor Circle Duluth, Minnesota 55811 United States

More information

PA32-RT LANCE II CHECKLIST

PA32-RT LANCE II CHECKLIST PA32-RT LANCE II CHECKLIST 6815.10.1112 1 Normal Procedures PREFLIGHT CHECK Control Wheel... RELEASE BELTS Parking brake... Set Master Switch... ON Fuel Quantity Gauges... check Master Switch... OFF Ignition...

More information

Aircraft Checklist Cessna 182T

Aircraft Checklist Cessna 182T Aircraft Checklist Cessna 182T This is an abbreviated checklist. Most explanatory items, notes cautions and warnings have been omitted for brevity. Procedures in red/bold in this checklist should be committed

More information

PREFLIGHT CHECK COCKPIT RIGHT WING. NORMAL PROCEDURRES CHECKLIST PA-28RT 201 Arrow IV

PREFLIGHT CHECK COCKPIT RIGHT WING. NORMAL PROCEDURRES CHECKLIST PA-28RT 201 Arrow IV NORMAL PROCEDURRES CHECKLIST PA-28RT 201 Arrow IV PREFLIGHT CHECK COCKPIT Control Wheel -- Release Restraints Avionics -- OFF Parking Brake -- SET All Switches -- OFF Mixture -- IDLE CUT-OFF Master Switch

More information

I - Model CITATION (Transport Category), approved 09 October 1998.

I - Model CITATION (Transport Category), approved 09 October 1998. TYPE CERTIFICATE DATA SHEET Nº EA-9810 Type Certificate Holder: CESSNA AIRCRAFT CO. P. O. Box 7704 Wichita, Kansas, 67277 USA EA-9810-02 Sheet 01 CESSNA CITATION 750 X 10 October 2011 This data sheet,

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A4 Revision 24 Piper Aircraft, Inc PA-20 PA-20S PA-20 "115" PA-20S "115" PA-20 "135" PA-20S "135" AIRCRAFT SPECIFICATION NO. 1A4 August 7,

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes Piper PA-28 Series (Cherokee, Cruiser, Warrior, Archer, Pathfinder, Dakota and Arrow) 28 February 2013 Notes 1. This AD schedule is applicable to Piper PA-28

More information

Wings of Carolina Flying Club PA Aircraft Type Checkout and Currency Quiz

Wings of Carolina Flying Club PA Aircraft Type Checkout and Currency Quiz Wings of Carolina Flying Club PA-28-161 Aircraft Type Checkout and Currency Quiz Pilot Instructor Score Date Instructor: Please note the final score (subtract 2.5 points from 100 for each wrong answer)

More information

CESSNA 182 CHECKLIST. LEFT WING Trailing Edge 1. Aileron CHECK freedom of movement and security

CESSNA 182 CHECKLIST. LEFT WING Trailing Edge 1. Aileron CHECK freedom of movement and security CESSNA 182 CHECKLIST PRE-FLIGHT INSPECTION CABIN 1. Pilot s Operating Handbook AVAILABLE IN THE AIRPLANE (A.R.R.O.W.E) 2. Landing Gear Lever DOWN 3. Control Wheel Lock REMOVE 4. Ignition Switch OFF 5.

More information

European Aviation Safety Agency

European Aviation Safety Agency TCDS A.185 Tecnam P2006T Page 1 of 8 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2006T Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli

More information

CIVIL AVIATION AUTHORITY SAFETY AND AIRSPACE REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-82 ISSUE: 2

CIVIL AVIATION AUTHORITY SAFETY AND AIRSPACE REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-82 ISSUE: 2 TYPE: EV-97 Eurostar SL Microlight (1) MANUFACTURER: Light Sport Aviation Ltd, Wycombe Air Park, Hangar 1, Booker, Marlow, Buckinghamshire, SL7 3DP (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.503 for (King Air) Type Certificate Holder Textron Aviation Inc. Once Cessna BoulevardWichita, KS 67215 USA For models: C90A C90GT C90GTi TE.CERT.00048-001 European

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST JAN 2014 Elmendorf Aero Club Aircraft Test SENECA II For the following questions, you will need to refer to the Pilots Information Manual for the PA-34-200T. USE ANSWER SHEET

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes Piper PA-28 Series (Cherokee, Cruiser, Warrior, Archer, Pathfinder, Dakota and Arrow) 25 January 2018 Notes: 1. This AD schedule is applicable to Piper PA-28

More information

AIRPLANE FLIGHT MANUAL

AIRPLANE FLIGHT MANUAL Thrush Aircraft Inc Model S2R-R1340 MANUAL ORGANIZATION SECTION I -----------------------------------------------------LIMITATIONS SECTION II -------------------------------------- NORMAL PROCEDURES SECTION

More information

CHAPTER 3 LIFE-LIMITED COMPONENTS

CHAPTER 3 LIFE-LIMITED COMPONENTS CHAPTER 3 LIFE-LIMITED COMPONENTS Section Title 3.100 Life-Limited Components..................................... 3.1 3.110 Time-in-Service Records................................... 3.1 3.120 Fatigue

More information

T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS

T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS ABORT START PROCEDURE or STARTER switch AUTO/RESET EMERGENCY ENGINE SHUTDOWN

More information

Normal T/O Procedure. * * * Engine Failure on T/O * * *

Normal T/O Procedure. * * * Engine Failure on T/O * * * Normal T/O Procedure After adding full power: Engine Instruments green Airspeed alive 1,000 AGL Accelerate to enroute climb 113 KIAS Set climb power Vr 78, but it will come off the ground before Stay in

More information

Cessna 172 Skyhawk. Aircraft Checklist Models: R & S

Cessna 172 Skyhawk. Aircraft Checklist Models: R & S Cessna 172 Skyhawk Aircraft Checklist Models: R & S This is an abbreviated checklist. Most explanatory items, notes cautions and warnings have been omitted for brevity. Procedures in red/bold text in this

More information

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST COCKPIT

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST COCKPIT PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST COCKPIT Check airworthiness certificate, registration, weight & balance documentation Battery - CONNECTED Plug in headsets or secure as required Fuel ON Magnetos

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1 of 17 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.011 Extra Flugzeugproduktions- und Vertriebs GmbH Schwarze Heide 21 D-46569, Hünxe Germany For models: -500 Issue 24

More information

T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS

T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS ABORT START PROCEDURE EMERGENCY ENGINE SHUTDOWN ON THE GROUND EMERGENCY GROUND

More information

JODEL D.112 INFORMATION MANUAL C-FVOF

JODEL D.112 INFORMATION MANUAL C-FVOF JODEL D.112 INFORMATION MANUAL C-FVOF Table of Contents I General Description...4 Dimensions:...4 Powertrain:...4 Landing gear:...4 Control travel:...4 II Limitations...5 Speed limits:...5 Airpeed indicator

More information

CESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S revised 10/05/06)

CESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S revised 10/05/06) INTRODUCTION, POH CESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S10315 - revised 10/05/06) 1. Rate of climb at sea level: 2. Service ceiling: 3. Takeoff performance,

More information

Pilatus Aircraft Ltd. P.O. Box 992 CH Stans SWITZERLAND

Pilatus Aircraft Ltd. P.O. Box 992 CH Stans SWITZERLAND F -3 1 of 7 This Data Sheet which is a part of Type Certificate No. F -3 prescribes conditions and limitations under which the product, for which the Type Certification was issued, meets the airworthiness

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A50NM Dassault Aviation Falcon 2000 December 19, 1995 TYPE CERTIFICATE DATA SHEET No. A50NM This data sheet which is part of Type Certificate

More information

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST PRE-FLIGHT CHECKLIST COCKPIT Check airworthiness certificate, registration, weight & balance documentation Battery - CONNECTED Plug in headsets or secure as required Fuel ON Primer CLOSED & LOCKED Carb

More information

Preflight Inspection Cabin EMPENNAGE RIGHT WING Trailing Edge RIGHT WING NOSE

Preflight Inspection Cabin EMPENNAGE RIGHT WING Trailing Edge RIGHT WING NOSE Preflight Inspection Cabin 1. Control Wheel Lock REMOVED 2. Ignition Switch OFF 3. Avionics Power Switch OFF 4. Master Switch ON 5. Fuel Quantity Indicators CHECK QUANTITY 6. Master Switch OFF 7. Fuel

More information

N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIONS. Best Rate of Climb (gear up, flaps up)

N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIONS. Best Rate of Climb (gear up, flaps up) N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIS Best Rate of Climb (gear down, flaps up) Best Rate of Climb (gear up, flaps up) Turbulent Air

More information

FAA APPROVED FOR MAULE M Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.

FAA APPROVED FOR MAULE M Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED FOR Airplane Serial No. Registration No. THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES. FAA APPROVED: Acting Manager, Atlanta Aircraft Certification Office, FAA, Central Region DATE:

More information

LOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual

LOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Revision A12 - May, 2015 Title Page LOEP LOR Section 1 All Reformatted to

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET Issue: 03 Date: 25/07/2018 TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.636 for Model 3000 Type Certificate Holder Textron Aviation Defense LLC 9709 East Central 67206 Wichita, Kansas United States of America

More information

Fokker 50 - Limitations GENERAL LIMITATIONS MASS LIMITATIONS. Page 1. Minimum crew. Maximum number of passenger seats.

Fokker 50 - Limitations GENERAL LIMITATIONS MASS LIMITATIONS. Page 1. Minimum crew. Maximum number of passenger seats. GENERAL LIMITATIONS Minimum crew Cockpit: Two pilots Maximum number of passenger seats Sixty-two (62) Maximum operating altitudes Maximum operating pressure altitude: Maximum take-off and landing pressure

More information

Hamilton. Hamilton. Jet A/A1 (See Approved Flight Manual for additional fuels) Engine Limits: Gas Gen RPM % Ng (2006)

Hamilton. Hamilton. Jet A/A1 (See Approved Flight Manual for additional fuels) Engine Limits: Gas Gen RPM % Ng (2006) TCDS No A-14 Revision 16 Pacific Aerospace Ltd 750XL 14 June 2018 TYPE CERTIFICATE DATA SHEET No A-14 This data sheet which is part of Type Certificate No A-14 prescribes the conditions and limitations

More information