N727RT: Project Notebook

Progress:


05> Oct | Nov | Dec | 06> Jan | Feb | Mar | Apr | May | Jun | Jul | Aug | Sep | Oct | Nov | Dec | 07> Jan | Feb | Mar | Apr | May | Jun | Jul | Aug | Sep



How is the plane coming???

This page attempts to offer an answer via the 5 views (sections) below.
If you're new, you may want to start with section # 5) which explains my status tracking process or jump directly to #2) for photos.
 

1) Recent 2) Monthly 3) Reporting 4) Detail 5) Explanation
 Photos from last week (or so) Monthly progress summary & photo journal Progress reporting & analysis Detailed spreadsheet
(by sub-component)
A description of the status tracking process

 

1) Recent Activity

Each week (or so)  I'll post a few key photos from the prior week (below).

Week of Photos (click for larger photo) Comments
12/17 Test fitting lower engine cowl for turbo-charger clearance.  Fuselage is hanging on the engine hoist - cowl is resting on the step stool.

Approx 1" turbo clearanace (looking in the cowl/exhaust vent).  Note, hose fitting on turbo-oil reservoir will be relocated to "red dot".
12/10 Exploded view of aileron control linkage

Mock-up board to test aileron control movement.
12/3/06 Machined (polished) gear legs to fit.
Original legs fit too loose. Had weldments honed.  Had legs hard chromed to increase diameter.  Polished legs to fit. Note: progress marks on legs which depict each "round" of grinding/polishing until legs finally fit all the way into the weldments. Special thanks to my father - the precision machinist.
11/26/06   Exploded view of parking brake value.

Spar box cover and rear seat mock-up.
11/19/06 Installed Brake Pedals

Installed Seats using new/modified seat tracks.  The tracks are longer (allowing the seats to be moved aft approx 2"), and have a better adjustment mechanism.
11/12/06

 

  Assembled Brake Pedals and cylinders

Atteneded Advanced Aircraft Design Class by Martin Hollman - the Designer of the ES

11/5/06 Fixing and installing the front Strut Bearing Blocks.

Installing the Strut.  Note: "temporary" front tires :-)

Mounting the engine - With help from Frank - a local pilot friend (vroom, vroom)

     

Click Here to see an archive of past weekly photo updates.

<< Return to the Top >>

 

2) Monthly Activity Summary (& Photo Journal):

Each link below jumps to a page with photos and a short description of the month's activity.

  Monthly Activity Summary (Click below to jump to the page)
  Oct 05 - THE BEGINNING, PREP, & BUILDER ASSIST
  Nov 05 - THE TRIP HOME
  Dec 05 - UNPACKING & SETTING UP SHOP
  Jan 06 - WING AND GEAR FAIRINGS
  Feb 05 - WING FAIRING FIX
  Mar 06 - LANDING GEAR
  Apr 06 - SNF 2006: Purchase Engine & Prop
  May 06 - BODYWORKING THE BOTTOM
  Jun 06 - THE ENGINE
  Jul 06 - BOTTOM IN PRIMER & OSH 2006
  Aug 06 - FAIRING & GEAR ACCESS
  Sep 06 - FLAP CONTROLS
  Oct 06 - WEB SITE & PLANNING
  Nov 06 - FRONT STRUT & ENGINE
  Dec 06 -
  Jan 07 -
  Feb 07 -
  Mar 07 -
  Apr 07 -
  May 07 -
  Jun 07 -
  Jul 07 -
 

<< Return to the Top >>

 

 

3) Progress Reporting and Analysis:

Additional progress analysis:

<< add link to trend chart1 >>

<< Return to the Top >>

 

4) Detailed Progress Tracking Spreadsheet:

The link below will call up a PDF file of my recent progress tracking spreadsheet (or click the image to the right).

Progress Tracking Spreadsheet (PDF)

This spreadsheet is laid-out to track progress as described in the progress tracking process explanation further below.

NOTE: you must have the adobe acrobat reader program installed on your computer to read PDF files.  If you do not have it, you can download it for free from here  http://www.adobe.com

<< Return to the Top >>

 

5) Progress Tracking Approach & Process:

How is the plane coming???

While this seems like a simple question, there really isn't a simple answer - besides "fine" or "slow" (grin).  There are thousands of parts, many of which require some degree of trimming, fabrication, or special attention.  Additionally, many items highly interrelated.  When completed, the entire aircraft can be thought of as one fully integrated piece of equipment.  Thus, many things are done in parallel and most components are fabricated/fitted, then temporarily removed to facilitate working on other items, and then each is often re-installed/assembled and checked again later (multiple times).

Generic Activity Groups

To simplify the planning and progress tracking process, I've summarized all tasks into the following eight (8) generic activity groups:

Generic Activities Task Descriptions

Design

Since this is a kit, the "basic structure" and many parts are already designed.  However, several of the systems are left to the builder to design/build.  Design tasks include:

  • Gathering requirements (structural & operational);

  • Outlining options, conducting a failure analysis (FMEA);

  • Analyzing alternatives;

  • Selecting the desired design and validating the decision(s);

  • Defining tolerances & acceptance criteria; and

  • Updating the documentation.

To see the items requiring design effort, refer to the detailed progress PDF spreadsheet above.
 

Procurement

Many of the necessary parts/pieces are included in the kit.  Generally, the kit includes most items except for:

  • Engine, propeller/spinner, engine accessories (exhaust, intake, controls, hoses, probes and sensors, etc);

  • Avionics (flight instruments, radios, navigation equipment, backup/standby systems, etc);

  • Electronics (wire, switches, circuit breakers, lighting, etc);

  • Limited heater and/or fresh air system components;

  • Upholstery, cloth, insulation, trim, and "soft" interior/finish items;

  • Paint, data plate, tow bar handle, exterior finish/trim items.

 Form the the items not included in the kit the procurement tasks include:

  • Identifying the needed materials, items, and specs;

  • Locating suppliers,

  • Gathering comparative product and cost data;

  • Selecting a source;

  • Ordering;

  • Tracking shipping and confirming receipt,

  • Verifying conformance; and

  • Updating documentation.

Fabrication

Some parts are supplied in their 100% final form and thus require little or no fabrication (such as pre-machined parts, custom weldments, electrical components, etc).  However, many various other parts are made from raw materials (fiberglass, aluminum, tubing, etc), or are made from a rough molded part/shell which require trimming, forming, and/or pre-assembly, or are made from many small discrete parts that require pre-assembly.  Generally the kit is designed be built with common hand tools and require little or no:

  • Weldling;

  • Complex machining and or metal forming;

  • Plating and/or surface prep beyond sanding and painting;

  • Heat treating, tempering, etc.

Fabrication tasks typically include some combination:

  • Creating templates/fixtures (as needed);

  • Fabricating the part (cutting, molding/forming, drilling holes, bonding/riveting, etc);

  • Preassembly;

  • Validating conformance to the designed size, spec, weight and function;

  • Rework (when required); and/or

  • Finishing of internal parts (paint, lubrication, safety wire, etc);

  • Creating and/or updating documentation.

Fit/Trim & Install

Overall, some parts are supplied such that they simply bolt together with little fanfare (e.g. "some assembly required). Typically however, most parts  require some combination of the tasks listed below to be fit and installed in/on the airplane (both the prefabricated /final-form parts and the hand fabricated ones).  Note: this is one of the most time consuming activities in building an airplane (along with the body work and finishing).

  • Assessing the desired placement, orientation, fit, and clearance to other related, nearby, and/or critical items;

  • Modifying and/or fabricating brackets/attachment points;

  • Selecting the most appropriate attachment method, fastener, and orientation (i.e. bolts are generally inserted top down when feasible);

  • Reviewing any safety considerations regarding the final placement, fit, and installation;

  • Reviewing any future inspection and/or maintenance serviceability considerations regarding the final placement, fit, and installation;

  • Trimming and/or re-forming the part to it's final fit & location;

  • Installation and/or assembly (bolding, bolting, riveting, etc)

  • Verifying position, alignment, fit, function, and clearance;

  • Disassemble and reassemble as necessary;

  • Updating documentation.

Final Assembly

After the parts have been designed, procured, fabricated, and fit, the last activity is to put them all together (for the final time).  Depending the nature of each part (permanently attached, semi-permeate, and/or removable) the final assembly tasks may include:

  • Surface preparation;

  • Bonding;

  • Post-cure cleanup;

  • Assembly (rivet, crimp, and/or and torque to spec, etc);

  • Inspect;

  • Safety wire/seal;

  • Final verification;

  • Document and update final assembly checklist.

 

 

Body Work

One of the advantages of a composite (fiberglass & carbon fiber) airplane is the ability to create very smooth and aerodynamically efficient shapes.  However, the "cost" of this advantage is "paid" in the requirement for bodywork.  Body working composite structures entails the following tasks to get the desired final shape and smoothness:

  • Grinding and Filing;

  • Filling (micro and flox);

  • Coating (micro and primer);

  • Sanding;

  • Repeat process as necessary (grin)

Finishing

Following the tasks above, the final activity is to button it all up and make it look good. For this project, I define the finishing activity to include a wide variety of tasks which include:

  • Final primer and paint (external surfaces);

  • Upholstery, carpet, and cloth (interior)

  • Labeling and placards (as required)

  • Verifying functionality (mechanisms)

  • Paperwork and documentation (regulations)

One finishing related consideration is whether to conduct flight testing before or after final paint and upholstery.  There are advantages and disadvantages of each approach.  Since I am planning on testing prior to final paint and upholstery, those tasks will be completed following testing.
 

Testing

Testing includes all activities conducted to verify intended function and performance; including initial testing of individual materials and parts, bench testing of systems, ground testing, and flight testing.  As such testing actually occurs throughout the project.  For each phase of testing, the tasks include:

  • Preparing testing needs, objectives, plans & criteria;

  • Setting up the test;

  • Conducting the test;

  • Gathering/recording the results;

  • Evaluating and analyzing the results;

  • Identifying discrepancies and issues (if any);

  • Investigating issues;

  • Proposing remedies;

  • Taking corrective action;

  • Retesting as required;

  • Updating the documentation.


Progress Tracking Approach:

To create a structured progress tracking model, I applied each of the generic activities (from above) to my project information structure (ref: Intro-project structure page) at the sub-component level.  I use the sub-component level because the "component" level is too broad (and thus to subjective) for measuring progress; and the "item" level is too detailed (administratively inefficient).  However, the "component" level is useful for a rolled-up / summarized view and the "item" level is useful for ensuring accuracy and completeness of the sub-component progress assessments.

To assess progress, each sub-component is "scored" for each of the relevant activities (0= not started, 3= 50%, 6=Done, and NA=not applicable) and converted to a %.  Any % scoring could be used, I just found this one to be the simplest approach that would work.

A overall "Activity View" of progress can be created by "rolling-up" the sub-component progress assessments for each generic activity (i.e. Fabrication is 57% complete).

To get a progress view of a particular subcomponent (across activities), I apply the following standard weights to each activity and add-up the scores.  The activity weights are somewhat arbitrary, but directionally correct and ultimately add up to 100% (so if you benefit early, you pay later).  I use three sets of weighting factors depending on what "view" of progress I'm are interested in.

Generic Activities "Build" View FAA View Total View

Research / Design

20%   15%

Procurement

10%   5%

Fabrication

30% 25% 20%

Fit / Trim / Install

35% 30% 25%

Final Assembly

5% 5% 5%

Body Work

  30% 25%

Finishing

  10% 5%

Total

100 100 100

To create a summarized view of progress at the component and/or category level (or for the entire project), the sub-component assessments are "rolled-up" (i.e. Airframe is 77% complete).

To view my actual progress tracking sheet (at the sub-component level):

Goto 4) Detailed Progress Tracking Spreadsheet (above)

<< Return to the Top >>

 

 

Copyright © 2006. All rights reserved. This site is the online project notebook of Rick Titsworth and for the purpose of sharing information and opinions related to building N272RT.  No responsibility for the accuracy or usefulness of the information is expressed or implied.  Any person using these images, ideas, and tips does so at their own discretion and risk and without recourse against anyone related to this site or the n727rt project.  This site is not affiliated with Lancair International.