MODEL 510 MAINTENANCE MANUAL

Size: px
Start display at page:

Download "MODEL 510 MAINTENANCE MANUAL"

Transcription

1 1. Scope TOWING AND TAXIING - GENERAL A. This chapter gives the procedures used to tow and taxi the airplane. Obey the local tow and taxi procedures. Examples are the use of the correct ramp and the correct ramp speed. 2. Tools and Equipment NOTE: Equivalents can be used for the items that follow. Table 1. Tools and Equipment NAME NUMBER MANUFACTURER USE Towbar Towbarless Tow Vehicle I-Towbot AP8600EZ AP8600 AP8700B AP8750B AP8750B-AL AP8800SDA Tronair S Eber Rd. Holland, OH Lektro, Inc SE Flightline Drive Warrenton, OR TULSA TOWBOTS, 8511 Airport Way, Jones/Riverside Airport Tulsa, Oklahoma Web: To tow the nose gear. To tow the airplane without a towbar. (NOTE 1) To tow the airplane without a towbar. NOTE 1: The maximum weight for the towbarless tow vehicle must not be more than 8400 pounds ( kg). 3. Def nition A. Towing. (1) The airplane can be towed forward or aft on hard surfaces with a yoke-type towbar attached to the nose wheel. The airplane can also be towed by the nose wheel held on the platform of an electric towbarless tow vehicle. (2) The airplane can be towed with a f at tire, but it is not recommended. The airplane can be moved from an active runway or taxiway with a f at tire. Tow the airplane forward a minimum distance to clear the runway or taxiway and do not use sudden turns. The tire will be unserviceable, and the wheel must be examined. Refer to the Supplier's Overhaul Manual given in the Introduction, Supplier Publication List. B. Taxiing. (1) The airplane can be taxied on a hard surface, gravel, or sod taxiway and runway. The airplane has a nose wheel steering system. During taxi, the rudder pedal movement operates the nose steering system. CAUTION: Do not use too much engine thrust during a taxi with a f at tire. Monitor the inter-turbine temperature (ITT) indicator for engine over temperature. (2) It is not recommended to taxi the airplane with a f at tire. Under emergency conditions, the airplane can be taxied a short distance to clear the active runway or taxiway. Cessna Aircraft Company Aug 1/2010

2 1. General TOWING - MAINTENANCE PRACTICES A. The airplane can be towed with a yoke-type towbar attached to the nose wheel. The airplane also can be towed by the nose wheel held on the platform of an electric towbarless tow vehicle. (Refer to Figure 201). CAUTION: Do not turn the nose gear more than it's turn limit. If you do, the nose gear turn angle will break the stop bolts on the top of the trunnion. (1) When the airplane is towed, the vehicle operator must make sure that they do not turn the nose gear more than it's limits. (2) Steering is done with the towbar or the towbarless vehicle when the airplane is towed. B. An approved person must be in the airplane during the tow operation to be prepared for dangerous conditions. (1) Put personnel to walk with the wing and/or the tail to make sure that there is suff cient clearance between the airplane and adjacent equipment and structures. 2. Tools and Equipment A. For a list of tools and equipment, refer to Towing and Taxiing - General. 3. Nose Landing Gear Towing A. Tow the Airplane (Refer to Figure 202). CAUTION: Make sure that there is suff cient weight forward of the center of gravity. Add weight or remove weight as necessary to adjust the center of gravity for interior conf gurations or an airplane without fuel. CAUTION: Do not turn the nose landing gear more than an angle of 75 degrees to the right or to the left side of center. A nose gear that goes beyond the tow stop (75 degree limit) will break the stop bolts on the top of the trunnion and cause damage to the nosewheel steering system. CAUTION: Do not move the airplane in 15 minutes or less after the standby attitude indicator gyro has stopped. This can cause damage to the gyro. CAUTION: Make sure that the recommended towbar is used. Make sure that the towbar is in good condition, inspect the towbar at intervals for cracks and condition. CAUTION: Do not use the nose landing gear to release the airplane if it becomes caught in soft dirt. Contact Citation Customer Service. CAUTION: Make sure that you disengage the rudder control lock before you tow the airplane. If you do not disengage it, damage to the airplane can occur. (1) Position the towbar at the nosewheel and insert the towbar into the nosewheel axle. (2) Engage the towbar locking handle. (3) Connect the towbar to the tow vehicle.

3 Towbar Attachment Figure 201 (Sheet 1)

4 Towbar Turn Limits Figure 202 (Sheet 1)

5 (4) Put an approved person in the pilot's seat. NOTE: The airplane can be towed with the elevator and aileron control locks installed in the control column. (5) Disengage the rudder control lock. (6) Disengage the parking brake. (7) Make sure that the wheel chocks, static ground cables, and mooring ropes are removed. (8) Put personnel at the wing and/or the tail to walk and to look for suff cient clearance between the airplane and adjacent equipment or structures. (9) Tow the airplane and make smooth starts and stops during the procedure. (10) When the tow operation is complete, make sure that you do as follows: (a) Put the nosewheel to the center position. (b) Engage the parking brake. (c) If necessary, install the elevator and aileron control locks. (d) Put the chocks in position at the wheels. (e) Connect the static ground cables. (f) Engage the rudder control lock. (g) Remove the towbar from the airplane. B. Use the Electric Vehicle to Tow (Without a Towbar). CAUTION: Make sure that there is suff cient weight forward of the center of gravity. Add weight or remove weight as necessary to adjust the center of gravity for interior conf gurations or an airplane without fuel. CAUTION: Do not turn the nose landing gear more than an angle of 75 degrees to the right or to the left side of center. A nose gear that goes beyond the tow stop (75 degree limit) will break the stop bolts on the top of the trunnion and cause damage to the nosewheel steering system. CAUTION: Do not move the airplane in 15 minutes or less after the standby attitude indicator gyro has stopped. This can cause damage to the gyro. CAUTION: Make sure the recommended electric towbarless vehicle is used. CAUTION: Make sure that the electric towbarless vehicle is not more than pounds ( kg). CAUTION: Make sure that you disengage the rudder control lock before you tow the airplane. If you do not disengage it, damage to the airplane can occur. (1) Wind a winch-strap around the nose landing gear strut immediately above the fork and the electric towbarless vehicle. (2) Put an approved person in the pilot's seat. NOTE: The airplane can be towed with the elevator and aileron control locks installed in the control column. (3) Disengage the rudder control lock. (4) Disengage the parking brake. (5) Make sure that the wheel chocks, static ground cables, and mooring ropes are removed.

6 (6) Put personnel at the wing and/or the tail to walk and to look for suff cient clearance between the airplane and adjacent equipment or structures. CAUTION: Make sure that the tail stand is removed before you lift the nose. If it is not removed, the tail stand can hit the ground and cause damage to the airplane. (7) Lift the nose landing gear into the electric towbarless tow vehicle. (8) Tow the airplane and make smooth starts and stops during the procedure. (9) When the tow operation is complete, make sure that you do as follows: (a) Put the nose wheel to the center position. (b) Engage the parking brake. (c) If necessary, engage the control locks. (d) Put the chocks in position at the wheels. (e) Connect the static ground cables. (f) Engage the rudder control lock. (g) Remove the towbar from the airplane.

7 1. General TAXIING - MAINTENANCE PRACTICES A. The airplane is controlled with engine thrust, rudder pedal steering, and brakes during the taxi procedure. The taxi procedure can be done with one or both engines. B. Taxi Safety Precautions. (1) Personnel that taxi an airplane must be familiar with the airplane and the taxi turn limits. Refer to Figure 201. (2) Make sure that the hydraulic system and the brakes are in a serviceable condition. (3) Use only the necessary engine thrust to start movement and to keep the approximate taxi speed. (4) Do not use the brakes continuously to keep the correct speed. Adjust the engines as necessary. (5) Make sure that the taxi route is clear and free of all blockage, such as maintenance stands and vehicles. (6) Use an observer(s) to make sure that there is wing tip clearance. (7) On surfaces with ice, when the nosewheel is turned but has no result, do not let the nosewheel be turned left or right. Damage to the nose gear can result if a dry area is hit with the wheel in a turned position. 2. Taxi the Airplane A. The maximum steering angle when the rudder pedals are used is 20 degrees left and right of center. When the rudder pedals and left/right braking are used together, the maximum angle is limited to 75 degrees left and right of center. Steering during the taxi operation is done by the rudder pedals and left/right braking. Two-engine operation is recommended during taxi, due to the high thrust necessary to move the airplane from the parking area. B. Prepare the Airplane. (1) Clean the area around the airplane. (2) Examine the main wheels and remove the static ground cables and the tail stand. (3) Make sure that the fuel level in the wings is balanced as much as possible. (4) Close all of the access and the baggage doors. (5) Disconnect the ground cable. C. Taxi the Airplane (Refer to Figure 202). (1) Put two personnel in the f ight compartment, one in the pilot's seat to taxi the airplane, and one in the copilot's seat to help and to be an observer. (2) Engage the parking brake. WARNING: Make sure that personnel and equipment are clear of the engine inlet and the exhaust areas. (3) Start the engines. Refer to the Model 510 FAA Approved Airplane Flight Manual. (4) Remove the wheel chocks. (5) Release the parking brake. (6) Make sure that the ground power unit is disconnected. (7) Make sure that the taxi personnel know where the airplane will be moved to and what they need to do. (8) Make sure that personnel are clear of the engine inlet and the exhaust areas. (9) Use only suff cient thrust to the engines to start to move the airplane. Move the airplane forward before it is turned. (10) Do not apply the brakes while the airplane is taxied, decrease the engine thrust to decrease the taxi speed. (11) Use the brakes to control the taxi speed, but only use the brakes for a very small quantity of time. (12) Control the airplane using the rudder pedals. NOTE: Nose gear steering is operated with the rudder pedals. (13) Put personnel at each wing tip to make sure that the wings do not hit any object.

8 Brake and Taxi Turn limits Figure 201 (Sheet 1)

9 Engine Danger Area Figure 202 (Sheet 1)

10 (14) Taxi the airplane to the necessary area. (15) Apply the parking brake. CAUTION: Do not set the parking brake while the brakes are hot. Irregular friction surface mix transfer can cause brake chatter, noise, and vibration. (16) Stop the engines. Refer to the Approved Airplane Flight Manual. (17) Put a chock in position at the main wheels. (a) If the airplane is to be parked or moored, refer to Chapter 10, Parking - Maintenance Practices or Mooring - Maintenance Practices.

LEAR Description

LEAR Description LEAR 45 TOWING DESCRIPTION AND OPERATION 1. Description A. Towing and taxiing procedures are basically the same as those used for other aircraft equipped with tricycle landing gear. B. The aircraft can

More information

SD3-60 AIRCRAFT MAINTENANCE MANUAL. These procedures will be required by personnel engaged in manoeuvring the aircraft on the ground.

SD3-60 AIRCRAFT MAINTENANCE MANUAL. These procedures will be required by personnel engaged in manoeuvring the aircraft on the ground. AMM 9-00-00 1.0.0.0TOWING AND TAXIING 1. General This chapter deals with aspects of: - Towing. Refer to 9-10-00, pb201. - Taxiing. Refer to 9-20-00, pb201. These procedures will be required by personnel

More information

TOWING - MAINTENANCE PRACTICES

TOWING - MAINTENANCE PRACTICES TOWING - MAINTENANCE PRACTICES TASK 584 801 1. Towing of the Aircraft A. Personnel In open areas, a minimum of two persons are necessary to do this task. In small or confined areas, a minimum of five persons

More information

CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES

CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES 09 - Effective Pages AIRCRAFT MAINTENANCE MANUAL - PART I CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES Ch-Se-Su Effectivity Page Date Ch-Se-Su Effectivity Page Date ALL 1 09 - Contents ALL 1 ALL

More information

TOWING - MAINTENANCE PRACTICES. Lockpins. Installation of the Air Driven Generator (ADG) Lockpin

TOWING - MAINTENANCE PRACTICES. Lockpins. Installation of the Air Driven Generator (ADG) Lockpin TOWING - MAINTENANCE PRACTICES TASK 584 801 1. Towing of the Aircraft A. Reference Information REFERENCE TASK 10 10 01 400 801 TASK 10 10 01 400 802 TASK 10 10 01 400 803 TASK 10 10 01 587 801 TASK 10

More information

CHECKLIST 1969 CESSNA 172-K. NOTE: Verify all information with airplane's POH

CHECKLIST 1969 CESSNA 172-K. NOTE: Verify all information with airplane's POH CHECKLIST 1969 CESSNA 172-K NOTE: Verify all information with airplane's POH PRE-FLIGHT INSPECTION 1 CABIN 1 A.R.R.O.W. CHECK Airworthiness Cert. In Clear View Registration In Clear View Radio License

More information

AVANTI P180. Ground Handling

AVANTI P180. Ground Handling AVANTI P180 Ground Handling Towing The airplane should be moved on the ground with the aid of the nosewheel towing bar provided with the airplane. The tow bar is designed to attach to the nose wheel axle.

More information

CHAPTER 10 PARKING AND MOORING

CHAPTER 10 PARKING AND MOORING CHAPTER 10 PARKING AND MOORING P/N 135A-970-100 Chapter 10 REVISION ~ Page 1 of 12 Copyright 2009 All rights reserved. The information contained herein is proprietary to Liberty Aerospace, Incorporated.

More information

CHAPTER 1 AIRCRAFT GENERAL

CHAPTER 1 AIRCRAFT GENERAL CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure 1-1). This material does not supersede, nor is

More information

BEECHJET 400A TOWING AND TAXIING

BEECHJET 400A TOWING AND TAXIING TOWING AND TAXIING DESCRIPTION AND OPERATION Towing involves ground movement of the airplane without engine operation and is the preferred method of airplane positioning since it provides more safety and

More information

BD 700 AIRCRAFT MAINTENANCE MANUAL PART II GRAVITY REFUELING - SERVICING

BD 700 AIRCRAFT MAINTENANCE MANUAL PART II GRAVITY REFUELING - SERVICING GRAVITY REFUELING - SERVICING TASK 620 801 1. Use of Fuel Biocide Additive When Gravity Refueling A. Tools and Equipment REFERENCE Pneumatic Injector Shop Air, 90 ±10 psi (620.53 ±68.95 kpa) Test Panel,

More information

TOWING MAINTENANCE PRACTICES. A. Towing Aircraft (Figure 201 and Figure 202) Cord, headset extension GSE Ref. No

TOWING MAINTENANCE PRACTICES. A. Towing Aircraft (Figure 201 and Figure 202) Cord, headset extension GSE Ref. No TOWING MAINTENANCE PRACTICES 1. General All possible precautions must be taken to ensure the safety of personnel and the security of aircraft and equipment when moving aircraft. A. Towing Aircraft (Figure

More information

NORMAL CHECKLIST ATTENTION!

NORMAL CHECKLIST ATTENTION! Avion Training CHECKLIST Normal Checklist CESSNA 172R / TC-STS Cessna 172 R TC-STS NORMAL CHECKLIST ATTENTION! DO NOT STOW THIS CHECKLIST IN DIRECT SUNLIGHT Avion Training - Doc.nr. 212 Revision 1 / 02022018

More information

RAYTHEON PREMIER I. TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane.

RAYTHEON PREMIER I. TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane. RAYTHEON PREMIER I TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane. Towing involves ground movement of the airplane without engine

More information

4.1 General Information. 4.2 Turning Radii. 4.3 Clearance Radii. 4.4 Visibility From Cockpit in Static Position. 4.5 Runway and Taxiway Turn Paths

4.1 General Information. 4.2 Turning Radii. 4.3 Clearance Radii. 4.4 Visibility From Cockpit in Static Position. 4.5 Runway and Taxiway Turn Paths 4.0 GROUND MANEUVERING 4.1 General Information 4.2 Turning Radii 4.3 Clearance Radii 4.4 Visibility From Cockpit in Static Position 4.5 Runway and Taxiway Turn Paths 4.6 Runway Holding Bay DECEMBER 2002

More information

Cessna Aircraft Short & Soft Field Takeoff & Landing Techniques

Cessna Aircraft Short & Soft Field Takeoff & Landing Techniques Cessna Aircraft Short & Soft Field Takeoff & Landing Techniques Objectives / Content For short- and soft-field takeoff and landing operations in CAP Cessna aircraft, review: Standards (from ACS) Procedures

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

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

The tie to tube front windshield was rounded to avoid a distorted by this point.

The tie to tube front windshield was rounded to avoid a distorted by this point. CHANGES IN AIRFRAME IBIS MAGIC GS-700 (2.008) Drilling of plastic polycarbonate drill with 9/64 so that it is an amplitude when riveting. The tie to tube front windshield was rounded to avoid a distorted

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

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

TEMPORARY REVISION NUMBER

TEMPORARY REVISION NUMBER TEMPORARY REVISION NUMBER 7 DATED 1 DECEMBER 2011 MANUAL TITLE MANUAL NUMBER - PAPER COPY TEMPORARY REVISION NUMBER FR172 Reims Rocket 1968 Thru 1976 Service Manual D849-5-13 D849-5TR7 MANUAL DATE 15 August

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

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

Cessna 172P PPL Checklist Page 1

Cessna 172P PPL Checklist Page 1 Cessna 172P PPL Checklist 06-08-2017 Page 1 Cessna 172P PPL Checklist 06-08-2017 Page 2 Checklist Items Informational Items Critical Memory Items PREFLIGHT COCKPIT CHECK (DO-LIST) Pitot Cover -- REMOVE

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

EMERGENCY GEAR DOWN HANDLE CHECK VALVE GEAR DROP TO EXTEND POSITION DOOR SELECTOR DOOR SELECTOR VALVE UPLOCK RELEASE CYLINDER DOOR CYLINDER

EMERGENCY GEAR DOWN HANDLE CHECK VALVE GEAR DROP TO EXTEND POSITION DOOR SELECTOR DOOR SELECTOR VALVE UPLOCK RELEASE CYLINDER DOOR CYLINDER WARN HORN CUT BEECHJET Landing Gear System LEGEND VENT LINE PRESSURE LINE RETURN LINE NITROGEN ELECTRICAL CIRCUIT CABLE LINE PACKAGE DUMP LANDING SELECTOR CHECK SELECTOR EMERGENCY DOWN HANDLE DROP TO EXTEND

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A33EU Revision 2 DASSAULT-BREGUET Falcon 10 September 3, 1987 TYPE CERTIFICATE DATA SHEET NO. A33EU This data sheet which is a part of Type

More information

TEMPORARY REVISION NUMBER

TEMPORARY REVISION NUMBER TEMPORARY REVISION NUMBER 8 DATED 1 DECEMBER 2011 MANUAL TITLE MANUAL NUMBER - PAPER COPY TEMPORARY REVISION NUMBER 1978 Thru 1986 Model R182 & TR182 Service Manual D2069-3-13 D2069-3TR8 MANUAL DATE 15

More information

Hawker 800XP Ground Handling Checklist. Procedures

Hawker 800XP Ground Handling Checklist. Procedures Hawker 800XP Ground Handling Checklist Procedures A. Introduction This part of the Ground Handling Checklist gives the approved procedures, from the Aircraft Maintenance Manual, to accomplish the Pre-Flight

More information

CESSNA SECTION 4. Unless otherwise noted, the following speeds are based on a maximum weight of 2550 pounds and may be used for any lesser weight.

CESSNA SECTION 4. Unless otherwise noted, the following speeds are based on a maximum weight of 2550 pounds and may be used for any lesser weight. CESSNA SECTION 4 INTRODUCTION Section 4 provides procedures and amplified instructions for normal operations using standard equipment. Normal procedures associated with optional systems can be found in

More information

TEMPORARY REVISION NUMBER

TEMPORARY REVISION NUMBER TEMPORARY REVISION NUMBER 7 DATED 1 DECEMBER 2011 MANUAL TITLE MANUAL NUMBER - PAPER COPY TEMPORARY REVISION NUMBER Model 188 & T188 Series 1966 Thru 1984 Service Manual D2054-1-13 D2054-1TR7 MANUAL DATE

More information

CESSNA CITATION MODEL 500/501 INCREASED RAMP AND TAKEOFF WEIGHT INSTALLATION 1 SEPTEMBER 1994

CESSNA CITATION MODEL 500/501 INCREASED RAMP AND TAKEOFF WEIGHT INSTALLATION 1 SEPTEMBER 1994 MAINTENANCE MANUAL SUPPLEMENT NFC Document No. CESSNA MODEL 500/501 INCREASED RAMP AND TAKEOFF WEIGHT INSTALLATION 1 SEPTEMBER 1994 This supplement must be attached to the Cessna Citation Model 500/501

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

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

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

CHAPTER 3. A journey of a thousand miles begins with a single step. Confucius

CHAPTER 3. A journey of a thousand miles begins with a single step. Confucius CHAPTER 3 INTRODUCTION... 3-1 TAIL WHEELS... 3-2 TAILDRAGGER ADVANTAGES... 3-3 TAILDRAGGER DISADVANTAGES... 3-3 CONTROLS... 3-4 TAXI AERODYNAMICS... 3-5 GROUND OPERATIONS... 3-7 INTRODUCTION Hangar flying,

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

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

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

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

CHAPTER 10. WEIGHT AND BALANCE

CHAPTER 10. WEIGHT AND BALANCE 9/27/01 AC 43.13-1B CHG 1 CHAPTER 10. WEIGHT AND BALANCE SECTION 1 TERMINOLOGY 10-1. GENERAL. The removal or addition of equipment results in changes to the center of gravity (c.g.). The empty weight of

More information

PIPER AIRCRAFT PA NOTE- Perform all inspections or operations at each oj the inspection. 1. Inspectspinnerandbackplate

PIPER AIRCRAFT PA NOTE- Perform all inspections or operations at each oj the inspection. 1. Inspectspinnerandbackplate PPER ARCRAFT PA-38-111 (.MANTENANCE MANUAL SCHEDULED MANTENANCE. PERODC NSPECTONS. -NOTE- Perform all inspections or operations at each oj the inspection intervals as indicated by a circle (). nspection

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

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

Accident Prevention Program

Accident Prevention Program Accident Prevention Program Maintenance Aspects of Owning Your Own Airplane Introduction As an owner-pilot, FAR Part 43 allows you to perform certain types of inspections and maintenance on your airplane.

More information

Expanded Flight Checklist Cessna 152

Expanded Flight Checklist Cessna 152 OUTSIDE CHECK INSIDE CABIN 1 Magnetos... OFF 2 Mixture... IDLE CUT OFF 3 Master switch... ON 4 Fuel quantity... CHECKED 5 Master switch... OFF OUTSIDE CABIN 1 Left wing... CHECKED Surface condition Flap

More information

Servicing. Table of Contents

Servicing. Table of Contents Servicing Table of Contents Servicing Record...................... 6-3 Anti-Ice (TKS) Fluid Citation SII............. 6-5 Fuel.............................. 6-6 Capacities........................... 6-6

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes Cessna 120 26 November 2015 Notes 1. This AD schedule is applicable to Cessna 120 aircraft manufactured under Federal Aviation Administration (FAA) Type Certificate

More information

SERVICE BULLETIN REVISION

SERVICE BULLETIN REVISION Revision 7 REVISION TRANSMITTAL SHEET This sheet transmits Revision 7 to Service Bulletin. A. Replaces the AN960PD10L Washers with NAS1149D0316K Washers. B. Removes the optional Aviation Brake System antiskid

More information

PARKING - MAINTENANCE PRACTICES

PARKING - MAINTENANCE PRACTICES PARKING - MAINTENANCE PRACTICES TASK 000 801 1. Removal of the Nose Landing Gear (NLG) Lockpin A. Reference Information TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward

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

Airglas, Inc. Instructions for Continued Airworthiness Including Installation, Maintenance and Service Instructions MANUAL NO.

Airglas, Inc. Instructions for Continued Airworthiness Including Installation, Maintenance and Service Instructions MANUAL NO. Airglas, Inc. Instructions for Continued Airworthiness Including Installation, Maintenance and Service Instructions MANUAL NO. PA-32-105 PA-32LA 8.00x6 NOSE WHEEL INSTALLATION KIT For Piper PA-28 and PA-32

More information

Seabee Annual Inspection Procedures

Seabee Annual Inspection Procedures Procedures Due to the wide variety of Seabee s flying out there, these procedures should be modified to fit YOUR Seabee. Make sure that all AD s are complied with as well as any required Service Bulletins

More information

SECTION 3 EMERGENCY PROCEDURES CONTENTS

SECTION 3 EMERGENCY PROCEDURES CONTENTS CONTENTS Page Definitions.................................. 3-1 Power Failure - General......................... 3-1 Power Failure Above 500 feet AGL................ 3-2 Power Failure Between 8 and 500

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

CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev Abril 2012)

CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev Abril 2012) DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev. 2-10 Abril 2012) A.- LIMITATIONS: 1.- Limitations ( KIAS) V (Turbulence

More information

Owners Manual. Table of Contents 4.1. INTRODUCTION SPEEDS FOR NORMAL OPERATION CHECKLIST & PROCEDURES 4

Owners Manual. Table of Contents 4.1. INTRODUCTION SPEEDS FOR NORMAL OPERATION CHECKLIST & PROCEDURES 4 NORMAL OPERATIONS Table of Contents 4.1. INTRODUCTION 2 4.2. SPEEDS FOR NORMAL OPERATION 2 4.3. CHECKLIST & PROCEDURES 4 4.3.1. PREFLIGHT INSPECTION 4 4.3.2. BEFORE STARTING ENGINE 8 4.3.3. STARTING ENGINE

More information

PA34-220T Piper Seneca III

PA34-220T Piper Seneca III PREFLIGHT PA34-220T Piper Seneca III Weight and Balance Documents -Airworthiness Certificate -Registration -Airplane Flight Manual -Weight & Balance Hobbs/Time Landing Gear Avionics and Fan(s) Cowl Fuel

More information

SR22T Airplane Flight Manual (AFM) Temporary Change

SR22T Airplane Flight Manual (AFM) Temporary Change Cirrus Design TPOH Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications:

More information

Turbinator-2 Build Manual

Turbinator-2 Build Manual Turbinator-2 Build Manual Thank you for your purchase of the Turbinator-2 sport jet by Boomerang RC Jets. This RC Jet IS NOT A TOY and should only be flown and operated by experienced RC Turbine Pilots.

More information

Fokker 50 - Landing Gear & Flaps

Fokker 50 - Landing Gear & Flaps FLIGHT CONTROLS The flight controls can be operated manually and automatically. From the flight deck, all control surfaces are mechanically operated via rod-and-cable systems, except the electrically operated

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 01 Chapter 11 Aircraft Weight Distribution Tables No Component group Elements Weight X cg Y cg Z cg 1 Wing 1.1. Wing main structure 1..

More information

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL UNSCHEDULED MAINTENANCE CHECKS 1. DESCRIPTION The following describes those maintenance checks and inspections on the aircraft which are dictated by special or unusual conditions which are not related

More information

ICAA Advisory Pamphlet ICAA-AP-004

ICAA Advisory Pamphlet ICAA-AP-004 Iraq Civil Aviation Authority ICAA Advisory Pamphlet ICAA-AP-004 Subject: AIRCRAFT GROUND HANDLING AND SERVICING ICAA Document ICAA-AP-004 Date: 13/04/2008 AIR OPERATOR CERTIFICATION ICAA-AP-004 Revision

More information

SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST

SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST TABLE OF CONTENTS Page Introduction... 6-3 Airplane Weighing Procedures... 6-4 Airplane Weighing Form... 6-5 Sample Weight and Balance Record... 6-8 Loading

More information

Chapter 14 SERVICING TABLE OF CONTENTS ILLUSTRATIONS

Chapter 14 SERVICING TABLE OF CONTENTS ILLUSTRATIONS Chapter 14 SERVICING TABLE OF CONTENTS INTRODUCTION -------------------------------------------------------------------------- 3 General ----------------------------------------------------------------------------------

More information

Unscheduled Maintenance Checks

Unscheduled Maintenance Checks CIRRUS AIRPLANE MAINTENANCE MANUAL CHAPTER 5-50: UNSCHEDULED MAINTENANCE CHECKS GENERAL Unscheduled Maintenance Checks 5-50: UNSCHEDULED MAINTENANCE CHECKS 1. General The following describes those maintenance

More information

2.11 Other Equipment and Installations

2.11 Other Equipment and Installations 2.10 Tow Releases The tow release fitted at the C. G. is model TOST "Europa G 88" (Data Sheet No: 60.230/2). Models TOST "Europa G 72 or G 73" may be used as a replacement tow release. The forward tow

More information

PARKING - MAINTENANCE PRACTICES

PARKING - MAINTENANCE PRACTICES PARKING - MAINTENANCE PRACTICES TASK 000 801 1. Removal of the Nose Landing Gear (NLG) Lockpin A. Reference Information TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward

More information

CESSNA 172N SKYHAWK PRE-FLIGHT INSPECTION SUPPLEMENT

CESSNA 172N SKYHAWK PRE-FLIGHT INSPECTION SUPPLEMENT CESSNA 172N SKYHAWK PRE-FLIGHT INSPECTION SUPPLEMENT This visual inspection guide was created to supplement the Cessna 172N Pre-flight Inspection Checklist with additional information and photographs pertaining

More information

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL JACKING 1. DESCRIPTION Three jack points, located at each wing tiedown and tail tiedown, are provided to perform maintenance operations. Tie-down rings must be removed and replaced with jack points prior

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

AEROPRO Checklist B Service/Maintenance

AEROPRO Checklist B Service/Maintenance AEROPRO Checklist B Service/Maintenance 2 Periodic maintenance AIRFRAME Maintenance Interval Time Limitation - after first 25 2 hours when reached - after first 50 3 hours when reached - after 100 5 hours

More information

V - Speeds. RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias. 80 kias

V - Speeds. RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias. 80 kias RV-10 Check List V - Speeds RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias 87 kias V s1 Stall (Flap Up) 60 kias V s0 Stall (Flap 40 deg) 55 kias Best Glide 80 kias V

More information

FIRST FLYING TECHNIQUES COCKPIT PREPARATION STARTUP TAXI

FIRST FLYING TECHNIQUES COCKPIT PREPARATION STARTUP TAXI 1. Introduction FIRST FLYING TECHNIQUES COCKPIT PREPARATION STARTUP TAXI We aim to teach and demonstrate how to operate a general aviation aircraft and show some basic techniques and manoeuvres that every

More information

Chapter 3: Aircraft Construction

Chapter 3: Aircraft Construction Chapter 3: Aircraft Construction p. 1-3 1. Aircraft Design, Certification, and Airworthiness 1.1. Replace the letters A, B, C, and D by the appropriate name of aircraft component A: B: C: D: E: 1.2. What

More information

Technical report A-054/1999 APPENDICES

Technical report A-054/1999 APPENDICES Technical report A-054/1999 APPENDICES 95 Technical report A-054/1999 APPENDIX A Photographs, figures and graphs 97 Figure 1 Figure 2 MAIN WRECKAGE Aircraft Figure 3.1 Aerial View Figure 3.2 Main Wreckage

More information

M20J-201 Checklist BEFORE STARTING ENGINE

M20J-201 Checklist BEFORE STARTING ENGINE M20J-201 Checklist BEFORE STARTING ENGINE Preflight... COMPLETE Baggage door... LATCHED/LOCKED Door... LATCHED/LOCKED Seatbelts... FASTENED Passenger brief....... [seatbelts/exits/smoking/talking/traffic]

More information

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies. TITLE FUEL - WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT EFFECTIVITY MODEL UNIT NUMBERS 500/501-0001 thru -0689 REASON To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or

More information

4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES

4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES Normal Operating DA 40 AFM 4A.1 INTRODUCTION Chapter 4A contains checklists and describes extended procedures for the normal operation of the airplane. 4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES Flight

More information

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE Learning Objectives Airframes Instructor Training Manual Chapter 6 UNDERCARRIAGE 1. The purpose of this chapter is to discuss in more detail the last of the Four Major Components the Undercarriage (or

More information

CHECKLIST N8876B Cessna 172. Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE Tel. (402)

CHECKLIST N8876B Cessna 172. Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE Tel. (402) CHECKLIST N8876B 1958 Cessna 172 F Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE 68110 Tel. (402) 342-4314 www.nebflight.com Cessna 172 N8876B 1958 GENERAL INFORMATION Model... Cessna

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

Cessna Citation Model Stats

Cessna Citation Model Stats Cessna Citation Model Stats Cessna Citation Sovereign - Dimensions Length 63 ft 6 in (19.35 m) Height 20 ft 4 in (6.20 m) Wingspan 72 ft 4 in (22.04 m) Wing Wing Area Wing Sweep Wheelbase Tread 516 sq

More information

FALCON SERVICE ADVISORY

FALCON SERVICE ADVISORY Cold Weather Operations Jan 10, 11 Origin: Field Status: Closed Classification: Maint & Ops REASON At the approach of winter, we would like to offer some additional guidance for operating your aircraft

More information

Cessna Citation XLS - Anti-Ice & De-Ice Systems

Cessna Citation XLS - Anti-Ice & De-Ice Systems GENERAL The airplane utilizes a combination of engine bleed air, electrical heating elements and pneumatic boots to accomplish anti-ice/deice functions. The anti-ice system consists of bleed air heated

More information

@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING

@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING @AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must

More information

OPERATOR CONTACT F U E L O I L TIRE S P E E D. Vg (best glide/flps0) 85Mph 74KIAS COM FAIL

OPERATOR CONTACT F U E L O I L TIRE S P E E D. Vg (best glide/flps0) 85Mph 74KIAS COM FAIL OE-DLP CESSNA FR 172 G ROCKET 3fly.at: +43 2252 77340 MTOW: 1.157 kg / 2.250 lb A/C-Size: W: 10,93 m H: 2,9 m L: 8 m F P L ( E X A M P L E ) Tower LOAV +43 1 900729201 Maintenance LOAV +43 2252 790894

More information

SD3-60 AIRCRAFT MAINTENANCE MANUAL PROTECTION DESCRIPTION & OPERATION

SD3-60 AIRCRAFT MAINTENANCE MANUAL PROTECTION DESCRIPTION & OPERATION SD3-60 AIRCRAFT MAINTENANCE MANUAL z AMM 31.0.0.0COLD WEATHER PROTECTION DESCRIPTION & OPERATION 1. General This section details precautions necessary to protect the aircraft on the ground during cold

More information

Models AA-5, AA-5A & AA-5B Annual or 100-hour Inspection

Models AA-5, AA-5A & AA-5B Annual or 100-hour Inspection Models AA-5, AA-5A & AA-5B Registration Number Serial Number Hours Registered Owner(s) Street Address City State/ Postal Code Provence Inspector Signature License No. Date Airport/City State/ Provence

More information

Van s Aircraft RV-4. Pilot s Operating Handbook

Van s Aircraft RV-4. Pilot s Operating Handbook Van s Aircraft RV-4 Pilot s Operating Handbook PERFORMANCE SPECIFICATIONS SPAN:.. 23 0 LENGTH:. 19 9 HEIGHT:. 6 8 SPEED: Maximum at Sea Level.. Cruise, 75% Power at 8,000 Ft.. 173 Knots 165 Knots RANGE

More information

SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST

SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST TABLE OF CONTENTS Page Introduction... 6-3 Airplane Weighing Procedures... 6-4 Airplane Weighing Form... 6-5 Weight and Balance... 6-7 Sample Weight and Balance

More information

NORMAL PROCEDURRES CHECKLIST PA T SENECA II PREFLIGHT CHECK INSIDE CABIN OUTSIDE CABIN

NORMAL PROCEDURRES CHECKLIST PA T SENECA II PREFLIGHT CHECK INSIDE CABIN OUTSIDE CABIN NORMAL PROCEDURRES CHECKLIST PA-34-200T SENECA II PREFLIGHT CHECK INSIDE CABIN Avionics Master Switch -- OFF Landing Gear Control. -- DOWN Mixture Controls -- IDLE/CUTOFF Ignition Switches -- OFF Master

More information

Jabiru Aircraft Pty. Ltd. Final Inspection Checklist. Engine Compartment

Jabiru Aircraft Pty. Ltd. Final Inspection Checklist. Engine Compartment Jabiru Aircraft Pty. Ltd. Final Inspection Checklist Registration No: Aircraft Checklist Pre Ground Test Model: Serial No: Engine Compartment Propeller: Prop Size: 60 x 53 Other:.. Propeller Serial No:

More information

INTRODUCTION. This Catalog:

INTRODUCTION. This Catalog: Editor s Note: This Parts Catalog has been reproduced from the original Republic Parts Catalog. Obviously, most of the information is obsolete; the pictures are accurate and up-to-date. If nothing else,

More information

The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.

The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin. Single Engine Service Bulletin August 25, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280001 thru 17280724 172S 172S8001 thru 172S8201 REASON

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

CESSNA 172I CESSNA 172I PREFLIGHT INSPECTION

CESSNA 172I CESSNA 172I PREFLIGHT INSPECTION PREFLIGHT INSPECTION Visually check airplane for general condition during walk-around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.

More information