FAR Project G31 (done)
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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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A wiseup.wsu.acza/mod/quiz/attempt.php7attempt=610918cmid 148960&page=3
ops
O YouTube
M Gmail
Maps
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1 MONLO GOA
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uestion 4
Quz navigation
Gate AB in Figure below is 1.0 m long and 0.9 wide. Calculate force F on the gate and position X of its centre of
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QUESTION 2
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10
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O LeBron or MJ? X
April 8, 2020 –
B Lecture 13 – Flc x
P CIVENG 2004 ( X
CIVENG 2004
f (2) Facebook
b o LeBron or M. X
O Final_Exam_Pra x
E Untitled docum x
i dib10bmlvqabco.cloudfront.net/attach/k4x223h5u3g1u2/jp1nfmmkpsy79m/k8swrgggfeqt/Final_Exam_Practice_Problem.pdf
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0.5 m
3 m-
11.60 For a trapezoidal shaped channel (n = 0.014 and slope
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20-ft bottom width and side slopes of 1
Consider the flow under the sluice gate of Fig. P10.84. If
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У2
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O Type here to search
E O 4») ENG
21…
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Course Home
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to
Review | Constants
pour unistur very unu sıyın
mm nyurve.
Fv = 390 N
Sur
Previous Answers
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