Table of Contents
CHAPTER1GENERAL
1-1Background
1-2Limitations
1-3Definitions
CHAPTER2SECTION33.28GENERAL
2-1RuleText
2-2IntentofRule
CHAPTER3SECTION33.28(a)
3-1RuleText
3-2IntentofRule
a.General
b.AirplaneInstallationandCertification
3-3Guidance
a.ControlSystemDescription
b.InstallationRequirements
c.OperationalRequirements
d.CertificationDataInterfaceDocument
CHAPTER4SECTION33.28(b)
4-1RuleText
4-2IntentofRule
4-3Guidance
a.General
b.FailureofAircraft-SuppliedPower
c.FailureofAircraft-SuppliedData
CHAPTER5SECTION33.28(c)
5-1RuleText
5-2IntentofRule
a.Single-FaultTolerance
b.UnsafeCondition
5-3Compliance
5-4Guidance
a.EECSAGeneral
b.EECSAAssumptions
c.EECSAQuantitativeAnalysis
d.TLOImplementationRequirements
e.EECSAQualitativeAnalysis
CHAPTER6SECTION33.28(d)
6-1RuleText
6-2IntentofRule
6-3Guidance
6-4ElectricalEnvironmentalLimitations
a.DeclaredLevels
b.TestProcedures
c.Pass/FailCriteria
d.ComponentandSoftwareDesignChanges
e.MaintenanceRequirements
6-5PhysicalEnvironmentalLimitations
CHAPTER7SECTION33.28(e)
7-1RuleText
7-2IntentofRule
7-3Guidance
a.ComplianceElements
b.SoftwareLevelRequirement
c.SoftwarePartitioning
d.SoftwareIntegrity
CHAPTER8INTEGRATIONOFENGINE,PROPELLERANDAIRCRAFTSYSTEMS
8-1EECSystemIntegrationPlan
a.DistributionofComplianceTasks
b.InterfaceDefinitionOtherData
c.DesignChangeControl
8-2AircraftFunctionsIntegratedintotheEngine
ControlSystem
a.IntegrationActivities
b.CertificationConsiderations
8-3IntegrationofEngineControlFunctionsinto
AircraftSystems
a.IntegrationActivities
b.CertificationConsiderations
APPENDIX1CERTIFICATIONCOMPLIANCEDOCUMENTS Abstract
Gives guidance and acceptable methods, but not the only methods, that may be used by designers of reciprocating engine electronic control systems to demonstrate compliance with Section 33.28 of Title 14 of the Code of Federal Regulations (14 CFR 33.28), Electrical and electronic engine control systems.
