AD: Honeywell | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-07.14.25

Airborne-NextGen-07.15.25

AirborneUnlimited-07.16.25

Airborne-FlightTraining-07.10.25

AirborneUnlimited-07.11.25

Fri, Apr 02, 2010

AD: Honeywell

AD NUMBER: 2010-07-02

MANUFACTURER: Various Aircraft Equipped With Honeywell Primus II RNZ-850( )/-851( ) Integrated Navigation Units
SUBJECT: Airworthiness Directive 2010-07-02

SUMMARY: The FAA is superseding an existing airworthiness directive (AD) that applies to certain Honeywell Primus II RNZ-850( )/-851( ) integrated navigation units (INUs). As one alternative for compliance, the existing AD provides for a one-time inspection to determine whether a certain modification has been installed on the Honeywell Primus II NV-850 navigation receiver module (NRM), which is part of the INU. In lieu of accomplishing this inspection, and for aircraft found to have an affected NRM, that AD provides for revising the aircraft flight manual to include new limitations for instrument landing system approaches. That AD also requires an inspection to determine whether certain other modifications have been done on the NRM; and doing related investigative, corrective, and other specified actions, as applicable; as well as further modifications to address additional anomalies. This AD extends the compliance time for a certain inspection and associated actions. This AD also revises the applicability to include additional affected INUs. This AD results from reports indicating that erroneous localizer and glideslope indications have occurred on certain aircraft equipped with the subject INUs. We are issuing this AD to ensure that the flightcrew has accurate localizer and glideslope deviation indications. An erroneous localizer or glideslope deviation indication could lead to the aircraft making an approach off the localizer, which could result in impact with an obstacle or terrain.

FMI: http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/C443BE28C161C178862576F500579491?OpenDocument

Advertisement

More News

ANN FAQ: How Do I Become A News Spy?

We're Everywhere... Thanks To You! Even with the vast resources and incredibly far-reaching scope of the Aero-News Network, every now and then a story that should be reported on sl>[...]

Classic Aero-TV: The PB4Y-2 Privateer - A Priceless Aero-Treasure

From 2015 (YouTube Version): Oshkosh Reveals Many Treasures... Including Old Warbirds Full Of History While at EAA AirVenture 2015, ANN News Editor, Tom Patton, ventured out to vis>[...]

Aero-News: Quote of the Day (07.14.25)

"The aircraft achieved the maximum recorded airspeed of 180 Knots IAS at about 08:08:42 UTC and immediately thereafter, the Engine 1 and Engine 2 fuel cutoff switches transitioned >[...]

ANN's Daily Aero-Term (07.14.25): Temporary Flight Restriction (TFR)

Temporary Flight Restriction (TFR) A TFR is a regulatory action issued by the FAA via the U.S. NOTAM System, under the authority of United States Code, Title 49. TFRs are issued wi>[...]

ANN's Daily Aero-Linx (07.14.25)

Aero Linx: Aviation Without Borders Aviation Without Borders, a leading humanitarian aviation charity, uses its aviation expertise, contacts and partnerships to enable support for >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC