SECTION 8
PA-28-181, ARCHER III HANDLING, SERV & MAINT
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: JANUARY 5, 2004 8-1
SECTION 8
AIRPLANE HANDLING, SERVICING, AND MAINTENANCE
8.1 GENERAL
This section provides guidelines relating to the handling, servicing, and
maintenance of the ARCHER III. For complete maintenance instructions,
refer to the PA-28-181 Maintenance Manual.
WARNING
Inspection, maintenance and parts requirements for all
non-PIPER approved STC installations are not included in this
handbook. When a non-PIPER approved STC installation is
incorporated on the airplane, those portions of the airplane
affected by the installation must be inspected in accordance with
the inspection program published by the owner of the STC.
Since non-PIPER approved STC installations may change
systems interface, operating characteristics and component
loads or stresses on adjacent structures, PIPER provided
inspection criteria may not be valid for airplanes with
non-PIPER approved STC installations.
WARNING
Modifications must be approved in writing by PIPER prior to
installation. Any and all other installations, whatsoever, of any
kind will void this warranty in it’s entirety.
SECTION 8
PA-28-181, ARCHER III HANDLING, SERV & MAINT
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: JANUARY 5, 2004 8-1
SECTION 8
AIRPLANE HANDLING, SERVICING, AND MAINTENANCE
8.1 GENERAL
This section provides guidelines relating to the handling, servicing, and
maintenance of the ARCHER III. For complete maintenance instructions,
refer to the PA-28-181 Maintenance Manual.
WARNING
Inspection, maintenance and parts requirements for all
non-PIPER approved STC installations are not included in this
handbook. When a non-PIPER approved STC installation is
incorporated on the airplane, those portions of the airplane
affected by the installation must be inspected in accordance with
the inspection program published by the owner of the STC.
Since non-PIPER approved STC installations may change
systems interface, operating characteristics and component
loads or stresses on adjacent structures, PIPER provided
inspection criteria may not be valid for airplanes with
non-PIPER approved STC installations.
WARNING
Modifications must be approved in writing by PIPER prior to
installation. Any and all other installations, whatsoever, of any
kind will void this warranty in it’s entirety.
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