FAR Project G31 (done)

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Aviation Institute of Maintenance, Duluth *

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BLK04

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Mechanical Engineering

Date

Dec 6, 2023

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pdf

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6

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FAR Project G31 09/21/2022 Page 1 of 6 AVIATION INSTITUTE OF MAINTENANCE FEDERAL AVIATION REGULATIONS PROJECT G31 Name: Jharamid Linarez Date: __________________ Score: ___________ ITEM: Demonstrate ability to read, comprehend, and apply information contained in FAA and manufacturers’ aircraft maintenance specifications, data sheets, manuals, publications, and related Federal Aviation Regulations, Airworthiness Directives, and Advisory Material. STUDENT PERFORMANCE GOALS: OBJECTIVE: Locate and use information from aircraft specifications, type certificate data sheets, aircraft listings and airwortiness directives (AD’s) . PROCEDURE: 1. Locate information from FAA Type Certificate Data Sheets (TCDS). 2. Apply information obtained from applicable airframe, engine, and propeller TCDS. 3. Complete the following sheet by filling-in the required data elements and/or responding to the questions provided. 4. Complete a list containg five (5) of the latest Airworthiness Directives (AD's) that apply to your assigned aircraft. Scoring: Procedures 1-3: Each question is worth 3 points = total of 75 points. Procedure 4 is worth 15 points with neatness and legibility worth 10 points = 25 points. THIS PROJECT COMPLIES WITH THE FOLLOWING REQUIRED ACS ELEMENTS: AM.I.I.R1 Completeness or accuracy of documentation. AM.I.I.R4 Adherence to warnings, cautions, or notes in maintenance and operational manuals. AM.I.I.S4 Complete an aircraft maintenance record entry for the compliance of a reoccurring AD for a specific airframe, aircraft engine, appliance, or propeller. AM.I.I.S8 Determine applicability of an AD. AM.I.I.S14 Determine maximum allowable weight of a specific aircraft.
FAR Project G31 09/21/2022 Page 2 of 6 Assigned Aircraft: Make: cessna Model: 150L N number: 19439 Serial number: 15074419 Circle the applicable engine Circle the applicable engine Left / Front Engine Right / Rear Engine If using a single engine aircraft: use the left-side engine information column. Mfg: continental Mfg: ______________________ Model: 0-200 Model: ____________________ S/N: 15072629-15073658 S/N: ______________________
FAR Project G31 09/21/2022 Page 3 of 6 Questions: AIRCRAFT TCDS/SPECS 1. What is the TCDS number for your aircraft? 3A19 2. What is the TCDS revision number and date? 50 , 07/21/2017 Verify this data with your instructor before proceeding! 3. Which propeller/hub assemblies are approved for installation on this aircraft? List at least two. (1) McCauley 1A101/GCM (2) McCauley 1A101/GCM 4. What engines are approved for installation on this aircraft? Continental O-200-A 5. What is the minimum fuel grade required? 22.5gal 6. What is the never exceed speed (VNE)? 162 mph, or 141 kts 7. What is the maximum weight of the aircraft? 1600lbs 8. What is the center of gravity range of your aircraft? Show all data. (+32.9) to (+37.5) at 1600lbs (31.5) to (+37.5) at 1280lbs or less 9. What is the useful load of your aircraft? To determine this, find the aircraft’s empty weight and subtract that weight from the maximum take-off weight. Empty weight data can be found in the aircraft ’s weight and balance record. 10. What is the total fuel capacity of your aircraft (as it appears on the TCDS, not the actual aircraft in the hanger)? 33.29 11. What is the oil capacity for each engine of your aircraft? 464 12. What is the aileron travel (in degrees or inches) on your aircraft? UP: 20 + 2, -0 DOWN: 14 +2, -0 degrees 13. What are the eligible serial numbers for your model aircraft? 15074419
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FAR Project G31 09/21/2022 Page 4 of 6 ENGINE TCDS / SPECS 1. What is the TCDS/Spec sheet number for your engine? 3A19 2. What is the maximum horsepower of your engine? 100 At what RPM does the engine develop maximum horsepower? 2750 3. What is the compression ratio of your engine? 7:1 4. What is the dry weight of your engine? 190 5. What is the timing (in degrees before top center, BTC) of your engine? 24 top 24 bottom 6. What is the reference used to determine approved spark plug types for your engine(s)? NOTE 6 SIL03-2 7. What is the reference used to determine the type-oil approved for your engine(s)? SAE 20 , SAE 40 Using that reference for engine oil, list the approved types. 8. What type of carburetor or fuel injection is approved for this engine? Marvel-Schebler MA-3SPA 9. What type magnetos are approved for this engine? slick electro 4301 PROPELLER TCDS/SPECS 1. Regardless of the make or model hub assembly, what is the maximum diameter for propeller blades that may be installed on your engine? 72- 66” 2. Regardless of the make or model hub assembly, what is the minimum diameter for propeller blades that may be installed on your engine? 72- 66” 3. List the required placards (if applicable) for your engine and propeller combination. Avoid continuous operation between 2650 and 2750 r.p.m Scoring: Procedures 1-3: Each question is worth 3 points = total of 75 points. Procedure 4 is worth 15 points with neatness and legibility worth 10 points = 25 points
FAR Project G31 09/21/2022 Page 5 of 6 Airworthiness Directive Worksheet Name: _____________________________ Page_____ of _____ Aircraft/Engine Make: Model Serial # AD # Subject Applicable yes/no-if not why One time AD Method of compliance Date & hrs complied Next compliance due 80-11-04 Cracked Nutplates yes Compliance with this AD is no longer required if the NAS 10684A nutplates are replaced with AN365- 428, MS20365-428, MS2l042L4 or MS21044N4 nuts. 80-11-04 1045.5 86-24-07 Engine Controls Installation yes Modify the engine controls installation by installing a drilled steel bolt, AN3l0 type castellated nut and a steel cotter pin in accordance with Cessna Single-Engine Customer Care Service Information Letter SE79-6.
FAR Project G31 09/21/2022 Page 6 of 6
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