Customer Support: +353 (0)1 857 6730

Corporate Website About Us
  • There are no items in your cart
Please enter a keyword to search
Advanced search
Home
FAA
FAA AC 33-10 : 2014

FAA AC 33-10 : 2014

Current

Current

The latest, up-to-date edition.

STATISTICAL ANALYSIS CONSIDERATIONS FOR COMPARATIVE TEST AND ANALYSIS BASED COMPLIANCE FINDINGS FOR TURBINE ENGINE AND AUXILIARY POWER UNIT REPLACEMENT, REDESIGN AND REPAIRED PARTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Related Advisory and Reading Material
4. Background
5. Guidance
Appendix A - Advisory Circular Feedback
Information

Defines acceptable statistical methods, but not the only methods, to help develop substantiating data for comparative test and analysis compliance findings.

DocumentType
Standard
Pages
13
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 33-11 : 2014 OXIDATION, HOT CORROSION, THERMAL FATIGUE, AND EROSION CHARACTERISTICS TESTING TO SUPPORT 14 CFR, PART 33, SECTION 33.15, COMPLIANCE FOR TURBINE ENGINES

FAA AC 33.83-1 : 2009 COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS
FAA AC 33-8 : 2009 GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION

View more information
€37.32
Excluding VAT
EUR
CAD
CHF
CNY
DKK
EUR
GBP
HKD
IDR
INR
JPY
KRW
MXN
NOK
NZD
SEK
SGD
USD
ZAR
Hardcopy - English
PDF - English
01
02
03
04
05
06
07
08
09
10
11
12
13
14
15
16
17
18
19
20

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

Get in touch with us