Beechcraft 23 Musketeer Checklist
Beechcraft 23 Musketeer · Checklist
Overview
This document serves as a checklist for the Beechcraft 23 Musketeer, providing pilots with a structured guide to ensure all necessary pre-flight, in-flight, and post-flight procedures are followed. It is designed for both new and experienced pilots to enhance safety and operational efficiency. The checklist includes critical steps that must be completed before takeoff, during flight, and after landing, ensuring that the aircraft is in optimal condition for safe operation. The document emphasizes the importance of thorough checks and adherence to procedures to prevent accidents and ensure compliance with aviation regulations.
- Conduct a thorough preflight inspection including fuel and oil checks.
- Follow specific engine start procedures to ensure safety.
- Complete all before takeoff checks including instrument functionality.
- Monitor engine performance and fuel consumption during flight.
- Secure the aircraft and complete post-flight inspections and logs.
Document
Source
Originally published by jasonblair.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Pages
- 12
- File size
- 5.5 MB
- Publisher
- jasonblair.net
Most owners only have the POH. Here's the essential set for the Beechcraft 23 Musketeer.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 23 Musketeer to your watchlist and track it in one place.
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In this document
Preflight Inspection
The preflight inspection checklist includes a thorough examination of the aircraft's exterior and interior. Pilots should check fuel levels, oil levels, control surfaces, and the condition of tires. Specific attention should be given to the fuel quantity, ensuring that there is enough for the planned flight plus reserves.
Engine Start Procedures
The engine start procedures outline the steps for safely starting the aircraft's engine. This includes checking the throttle position, ensuring the mixture is set correctly, and verifying that the ignition switch is in the proper position before cranking the engine.
Before Takeoff
Before takeoff, pilots must complete a series of checks including verifying that all instruments are functioning, ensuring that the flaps are set correctly, and confirming that the runway is clear. The checklist also includes a final review of the weight and balance calculations.
In-Flight Checks
In-flight checks focus on monitoring engine performance, fuel consumption, and navigation instruments. Pilots should regularly check for any abnormal indications and be prepared to respond to any emergencies that may arise.
Post-Flight Procedures
Post-flight procedures include securing the aircraft, conducting a walk-around inspection, and completing the flight log. Pilots should ensure that all equipment is turned off and that the aircraft is properly tied down.
Safety notes
- Always verify fuel levels before flight.
- Ensure all safety equipment is onboard and functional before departure.
- Follow emergency procedures as outlined in the checklist.
Full document text
DATE RECORDING TODAYS FLIGHT TOTAL TIME IN SERVICE TACH 192002 TIME Rd. APRIL 23 NEW:2626.42 Old: 2628.68 Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) 2628.68 INSTALLED HORIZON INSTRUMENts Model P-1000 elecTRONIE. digital eNGING TACHOMETER S/N 0210105 fer INSTALLATION & INSTRUCTION MANUAL. FLIGHT MANUAl supplement has been Pilots INCLUDED IN THE OPERATIONS MANUAL. 337 HAS been APPROVED ON APRil 12, 2002 AS A One Time Field APPROVAL. No weiGHT & balANCE CHANGE. Equip List MODIFIED. - 4 INSTALLED New T.C.M. IGNITION SWITCH P/N 10-357200-1 S/N HO11. Key CODE PK 718. > huch IA 143629 3 Эрушев DATE TACH 2 TIME June 14 647 2002, June 14 2647.56 - 2649.82 ReplaceD Nose Wheel L.H. beARING seal. ©1991 ASA c/w 91.207 PARA (d) ELT INSPECTION & FUNCTIONAL ck. New ELT BATTERY INSTALLED DUE July 2004. CLEANED & PAINTED BATTERY box AS VOCESSARY, ReplACED L/L Bulb (outbd). 2003 July 16 2691 Alterations Number of cific entries.) lecTRONIC -STALLATION it has been I HAS been eField ST MODIFIED. = 10.357200-1L 93 FUNCTIONAL ck. 2004. PSSARY RECORDING TODAYS DATE 2002 19 TACH TIME FLIGHT JUNE 14 2647.56 - 2003 July 16 2691.25 TOTAL TIME IN SERVICE Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) 2649.82 ReplaceD ROTATING beacon Lamp. c/w AD 73.20.07RZ Visual INSPECTION OF FWD. WING ATTACH bolts. C/N AD 75-01-04 FUNCTIONAL CHeck of Fuel SelecTOR VALUE eks-ok. 2/arch Date 6/14/02 Total Time In Service IA 1436293 2649.82 inspection and ЛЯ 1436299 I certify that this airframe has been inspected in ANNUAL accordance with a. was determined to be in airworthy condition. Frank C. Lynch 2693.51 C/W 91.207 PARA (d) ELT INSPECTION & FUNCTIONAL el. Replaced guild 4/L bulb. Replaced ROTATING besem Lamp Replacal RH Nov & Tail NAV Lamps C/W AD 73-20-07 R2 Visual Inspection of 212 ©1991 ASA DATE 2003 RECORDING TODAYS TACH TIME FLIGHT July 16 2691.25 - TOTAL TIME IN SERVICE Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) 2693.51 Fun wING ATTACH bolts c/w AD 75-01-04 FUNCTIONAL CHock of Fuel selector value. -cks ok.. C/W AD 76-07-12 Functional check of BeNDIX Ight fu (WAD 87-02-08 INSP OF STAY. ATTACH brackets. Date July/16/2003 Total Time In Service 2693.51; I certify that this airframe has been inspected in accordance with a. ANNUA was determined to be in airworthy condition. 7 houch + + Frank C. Lynck + inspection and ЛЯ 1436299 1991 ASA DATE RECORDING TACH TIME Iterations Number of ific entries.) Fuel selector x 1ght sw. prackets. DATE RECORDING TACH TIME THE ALTIMETER AND STATIC SYSTEM TESTS REQUIRED BY F.A.R. PART 91.411 E/Feb05. HAS BEEN PERFORMED THIS DATE ALTIMETER TESTED IN COMPLIANCE WITH APPENDIX E PART 43 TO 15000 FEET. DATE/FEB05 STATIC SYSTEM CHECK PERFORMED BY RAY ALLEN'S ELECTRONICS, INC. BUTLER, GA. F.A.A. R/S #HS4R243M SIGNED R Allen DATE 1 Febo 5 (SERIAL #) (MAKE) NARCO TE: /Fobos DATE I CERTIFY THIS ATC TRANSPONDER (MODEL) AT-SOA HAS BEEN TESTED, INSPECTED AND FOUND TO COMPLY WITH APPENDIX F OF F.A.R. 43 AND PART 21.413 F.A.A. R/S #HS4R243M SIGNED Q DATE / Fell 05 TESTS PERFORMED BY RAY ALLEN'S ELECTRONICS, INC. BUTLER, GA. N9700L Sn: MB-506 TT: 2698.82 Lycoming 0-320-E2C SN: L-19046-27AC EngTT: 3996.06 SMOH 987.63 Tach 2696.56 Sensinich 74-DM6-S5-0-54 SN: K31844 Performed 100 Hr. inspection I.A.W. Beech maintenance and service manuals. Replaced ELT battery and tested I.A.W. FAR 91.207(d) batteries due for replacement FEB 2007 Replaced both gaskets and diaphragm in wet compass. Replaced door seal. Installed new vacuum relief valve filter. Lubed all flight controls, pulleys, bell-cranks, chains, hinges, gears, and wear surfaces. Removed, cleaned, inspected and repacked all wheel bearings. Serviced hydraulic reservoir and bled brakes. AD 76-06-12 complied with, Ign Switches, by operation. All remaining AD's complied with through this date, see separate list. I certify this airframe to be airworthy at this time. irs and Alterations tificate Number of her specific entries.) LUTHER E. HERNDON 01 Feb 2005 A&P 257926689 ©1991 ASA DATE RECORDING TODAYS TACH FLIGHT 2005 TIME 2 FEB 2005 2696.56 ©1991 ASA TOTAL TIME IN SERVICE Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) DATE/FEB 2005 TT 2698.82 N9700L PERFORMED ANNUAL INSPECTION. I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION Dayal 258643895 A&P/A 2698.82 Removed & Replaced 10 Amp Fuel Boost Pump Circuit Breaker Switch with new part. Luther Late Herndon A/P 257926689 DATE RECORDING TACH 05 TIME 3/29/05 2679.00 3/22/06 2753:0 and Alterations ficate Number of r specific entries.)**. Fuel Boost 2 with 257926689 DATE RECORDING 20 TACH TODAY FLIGHT TUTAL 05 TIME TIME IN SERVICE 3/29/05/2699.00 3/22/06/2755.0 Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) 2701.26 REMOVED: HORIZ IND. 5000B-5 S/N 12447E 41030481 INSTALLED: ALLEN RCA22-2 S/N 6452- OVER HAULED By Rady A/C "INST, 3/02/05 REPLACED, INST AIR FILTER . 9/1253901021 2757.26 PREFORMED 100HR. INSPECTION Z.A. W. BEECH MAINTENANCE & SERVICE MANUALS, ELT OUE: FEB OF INSTALLED NEW VACUUM FILTER, INSTALLED NEW BRACKETT AIR FILTER, INSTALLED NEW OIL TEMP BulB, Drainting, Oil, REPLACED OIL FILTER AND FILLED WITH
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8 gut: 20W50 Phillips, LUBED ALL Flight CONTROLS, PULLEYS BELL-CRANKS, HINGES, GEARS AND WEAR SURFACES, INSPECTED AND REPACKED ALL WHEEL BEARINGS, SERVICED AND BLED BRAKES, AD 76-06-12 IgN. SWITCH COMPLIED WITH, ALL REMAINING AD's Complice WITH THIS DATE: I CERTIFY THIS AIRFRAME To Be AIR WORTHY AT THI's Tying. Colok A&P 253901021 © 1991 ASA DATE 19 TIME RECORDING TODAYS TACH TOTAL FLIGHT TIME IN SERVICE ©1991 ASA Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) DATE RECOR TACH 19 TIME 2016 277 1. 2. 3. Complied with AD 87-02-08 (Stabilator Hinge Assemblies) effective 03-04-1987, by visual inspection. No discrepancies noted. Due Next annual or 100 hours. MODEL MB-19 AIRFRAME LOG ENTRY Hobbs AF S/N MB-506 AF REG# N9700L 257.8 Page 1 of 1 Tach Time 2798.8 2778.0 DATE 157 05/27/20172016 Complied with Annual Inspection using Beechcraft Musketeer checklist as a guide IAW the Beechcraft Musketeer maintenance manual and O-320 manual. Complied with AD 89-24-09 (Aileron Rodends) effective 12-04-1989, by visual inspection and lubricated. No discrepancies noted. Due Next annual or 100 hours. 4. 5. 6. 7. 8. 9. Complied with AD 75-01-04 (Fuel Selector Valve) effective 01-07-1975, by operational check. No discrepancies noted. Due Next annual or 100 hours. Complied with AD 73-20-07R2 (Wing Attach Bolts/Brackets) effective 09-03-1982, by visual inspection. No discrepancies noted. Visual Due Next annual or 100, NDT Due @3067.2 Complied with AD 76-07-12 R1 by operational check of the mag switch. Due Next annual or 100 hours. Installed a New ELT Battery, Inspected and Tested the AT-King ELT Per. FAR 91.207(d.), no discrepancies noted. ELT Battery Due date Dec. 2025. Removed the R/H Brake Master Cylinder disassembled, cleaned and inspected the housing and puck, installed a new O-ring, then reassembled the brake, and performed brake bleeding procedure. Deffered Gyro-HSI per FAR 91.213 I certify that with respect to the work performed this (Airframe,) was repaired and/or inspected in accordance with an (Annual) Inspection using the (Beechcraft, Musketeer) inspection guide as listed in the manufacturers maintenance manual as a guide, which meets the intent of 14 CFR Part 43 Appendix D and was determined to be airworthy and has been approved for return to service. No other representations concerning airworthiness are expressed or implied. " Name: Mark Fayerman Title: IA-A&P # 3599607 2779 2016 2799 N, 30, L3,10,100 Falcon Aviation f LOG ID# 1658 N9700L S/N M AFTT 2779.5 PERFORMED TRAN 91.413. NO DEF ABOVE WAS REPA APPROVED FOR R Doma INSPECTOR/30 ■ Alterations ce Number of ecific entries.) For N 30 60 E 120 150 RECORDING TODAYS Steer Steer 360 30 63 90 120 150 ctions, Tests, Repairs and Alterations 180 210 240 270 271 329 with Name, Rating and Certificate Number of DATE 07/07/2016 lity. (See back pages for other specific entries.) DATE TACH FLIGHT TOTAL TIME IN For S 210 240 W 300 330 19. TIME SERVICE M 2016 2016 27998 27795 27795 27998157 N, 30, 63, 98, 120, 130, 8, 210, 240, W, 297, 329 AIRPATH Installed Serviceable Attitude Attitude Gyro P 23-501-017 SIN 867892 Ref Lowe Aviation Services 8130-3 w/o 1118-2 ops check normal, work performed Ref Beech Muskete M.M. Section 2. Much Layern H+P 3599607 END- Performed Compass Swing and Filled Card for Correction. Installed correction Card in hircraft. - Mark Fayerman A+P3599607- Falcon Aviation Maintenance 95 E. Aviation Way Newnan, Ga 30263 9X3R785C LOG ID# 1658 08-July-2016 N9700L S/N MB-506 AFTT 2779.5 BEECHCRAFT 19 TACH 2779.5 Pg 1/1 PERFORMED TRANSPONDER CERTIFICATION PROCEDURES IAW 14CFR 43 APPENDIX F TO COMPLY WITH 14CFR 91.413. NO DEFECTS NOTED. THE AIRCRAFT, ENGINE, COMPONENT, PROPELLER OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED IN REFERENCEWITH CURRENT FEDERAL AVIATION AGENCY REGULATIONS AND IS HEREBY APPROVED FOR RETURN TO SERVICE. D Hudso INSPECTOR / JONATHAN D. HUDSON 9X3R785C CERTIFICATE # 7-8-2016 DATE ©1991 ASA AIRFRAME LOG ENTRY Page 1 of 1 DATE ons DATE 19 MODEL MB-19 AF S/N MB-506 AF REG# N9700L Hobbs 282.8 Tach Time 2798.09 DATE of 2019 RECORDING TACH 12/01/2017 os.) TIME 1. Complied with Annual Inspection using Beechcraft Musketeer checklist as a guide IAW Beechcraft Musketeer Maint. Man. 2. Complied with AD 89-24-09 (Aileron Rodends) effective 12-04-1989, by visual inspection and lubricated. No discrepancies noted. Due Next annual or 100 hours. 3/31 303 3. Complied with AD 87-02-08 (Stabilator Hinge Assemblies) effective 03-04-1987, by visual inspection. No discrepancies noted. Due Next annual or 100 hours. 4. Complied with AD 75-01-04 (Fuel Selector Valve) effective 01-07-1975, Removed Fuel Selector Valve and installed Overhauled Valve P/N 169-380086-1 S/N AA1570. No discrepancies noted. Repetitive inspection no longer required Per AD paragraph (b). 5. 6. ©1991 ASA 7. 8. 9. Complied with AD 73-20-07R2 (Wing Attach Bolts/Brackets) effective 09-03-1982, by visual inspection. No discrepancies noted. Visual Due Next annual or 100, NDT Due @3067.2 Complied with AD 76-07-12 R1 by operational check of the mag switch. Due Next annual or 100 hours. Complied with AD 2017-16-01 (Ameri-King Corporation Emergency Locator Transmitters) Effective date 10-24-2017, by paragraph (G) performed general visual inspections of the ELT for discrepancies; checks, tests, and verifications, as applicable, to ensure the ELT is functioning; in accordance with section 3.4, "Periodic Maintenance," of AmeriKing Corporation Document IM-450, "INSTALLATION & OPERATION MANUAL," Revision A, dated October 18, 1995. This also meets the requirements of FAR 91.207(d.), no discrepancies noted. ELT Battery Due date Dec. 2020. Complied with Mandatory Service Bulletin SB 27-3459 (Flight Control Gust Lock Inspection / Replacement), Rev. 2 dated November 2016. Inspected Gust Lock and found correct Ref section 3A(1) Replaced Left and Right Fuel Cap O-rings P/N MS29513-338. 10. Replaced intake Bracket Air Filter P/N BA7305 11. Replaced Vacuum Filter B-3. I certify that with respect to the work performed this (Airframe,) was repaired and/or inspected in accordance with an (Annual) Inspection using the (Beechcraft, Musketeer) inspection guide as listed in the manufacturers maintenance manual as a guide, which meets the intent of 14 CFR Part 43 Appendix D and was determined to be airworthy and has been approved for return to service. No other representations concerning airworthiness are expressed or implied. Much Sayernian Name: Mark Fayerman Title: IA-A&P # 3599607 02 MAY 201 1. Inspected Inspected 2. due May, 3. AD89-24-0 due at ann 4. AD87-02-0 at annual 5. AD73-20-0 due at ann AD76-07-1 6. 7. Replaced 8. Replaced I certify that this a airworthy condition Jeffery Peabody A&P 3416904 IA ons bf es.) RECORDING TODAYS TIME IN SERVICE DATE 2018 TOTAL 19 TACH TIME FLIGHT 3/21 303-8 - 2802. Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) NEW GILL 7035-28 battery installed. Direct w/3 change. replacement for old battery no SN G02991147 Eie Fenly. 02 MAY 2012 N9700L Beechcraft B-19 SN MB-506 Tach: 2806.3 AFTT: 2808.6 1. Inspected airframe Beechcraft Musketeer check list IAW B-19 Maintenance Manual. 2. Inspected and functionally tested ELT and found it meets the requirements of FAR 91.207(d). Next inspection is due May, 2020. ELT batteries are due replacement December 2020. 3. AD89-24-09(12/04/2989) Inspection of Aileron Rod-ends by visual inspection and lubrication. No defects noted. Next due at annual or ACTT 2908.6 4. AD87-02-08(03/04/1987) Inspection of Stabilator Hinge Assemblies by visual inspection. No defects noted. Next due at annual or ACTT 2908.6 5. AD73-20-07R2(09/03/1982) Inspection of Wing Attach Bolts/Brackets by visual inspection. No defects noted. Next due at annual or 2908.6 6. AD76-07-12R1 by operational check of mag switch. Next due at annual or 2908.6 7. Replaced bracket air filter BA7305 8. Replaced nose tire Installed Condor 15X6.0-6 I certify that this aircraft has been inspected in accordance with an annual inspection and was determined to be in an airworthy condition. Allen & Deag Jeffery Peabody A&P 3416904 IA ©1991 ASA 13b. Authorized Signature JAMES D. MURPHY 24/Jun/2019 User/Installer Resi | It is important to understand that the existence of this document alone does not automatically com Where the staller performs work in accordance with the national regulations of an airwo |Bank, 1, 11 in ponențial that the mer/installer ensures that his/her airworthiness authority accepts tatements in Block 13a and 14a do not constitute installation certification. In all cases, aircraft the nationale egulations by the user/installer before the aircraft may be flown. FAA Form 8130-3 (02-14) DATE 2019 RECORDING TACH TODAYS FLIGHT TIME TOTAL TIME IN SERVICE Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) N9700L 6/8/2019 S/N: MB-506 TTAF: 2858.91 Installed new carb heat scat tubing. Ground operational check good. Signed: 3. SAP 3813281 6/23/19 Tach time: 2859. 6 TTAF: 2861.8 Removed and replaced right hand Nav Light. litter Perational Check good. N9700L 9/28/2019 S/N: MB-506 Tach:2878.4 TTAF: 2880.66 CPL 4018706 Removed Starter p/n 1109511 installed new starter p/n 149NL s/n H-T062027 see Hartzell Engine Technologies W/O# M677250 for details. Adjusted weight and balance. Ground operational check good. Signed: - AP3813281IA ©1991 ASA DATE RECORDING N9700L 1/29/202 19. Removed vacuum details. Ground ope N9700L Installed ne ai R S D pairs and Alterations d Certificate Number of for other specific entries.) 813281 ht hand Nav good. росс chnologies W/O# M677250 for TA ᏭᏙᏞ 799981 ᏞᏙIᏞᏘ ᏚᏙ RECORDING TODAYS TOTAL DATE N9700L 19. Description of Inspections, Tests, Repairs and Alterations 1/29/2020 S/N: MB-506 Tach:2892.2 TTAF: 2894.46 Removed vacuum pump installed overhauled vacuum pump pn 215CC s/n 186562 see Rapco, Inc. W/O# 186562 for overhaul details. Ground operational check good. Signed: JS AP3813281IA N9700L 2/4/2020 S/N: MB-506 Tach:2892.2 TTAF: 2894.46 Installed new Pilot side LH brake master cylinder o-rings. Ground operational check good. Leak check good. Signed: - AP3813281IA ©1991 ASA