Honeywell International Inc. - Additional Comments

Document ID: FAA-2008-0556-0005
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: June 30 2008, at 04:26 PM Eastern Daylight Time
Date Posted: July 1 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: May 19 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: July 3 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 8064c2fb
View Document:  View as format xml

View Comment

Further comments in addition to those submitted on 6/26/08 from Honeywell International Inc. recommend wording changes as follows; 1. (j) For any INU identified in Table 2 of this AD on which Mod L was found to be installed during the inspection required by paragraph (g) of this AD, or for aircraft on which paragraph (h) of this AD was accomplished: Within 30 months after December 1, 2006, do an inspection of the modification plate on the Honeywell Primus II NV-850 NRM; part number 7510134-811, -831, -901, or -931; which is part of the Honeywell Primus II RNZ-850( )/-851( ) INU; to determine if Mod L, N, P, R, or T is installed. The modification plate located on the bottom of the Honeywell Primus II RNZ-850( )/-851( ) INU is labeled NV-850, and contains the part number and serial number for the Honeywell Primus II NV-850 NRM. If Mod L, N, P, R, or T is installed, the corresponding letter on the modification plate will be blacked out. Honeywell Alert Service Bulletin 7510100-34-A0035, dated July 11, 2003, is an acceptable source of service information for this inspection. If Mod L, N, P, or R is installed, within 30 months after December 1, 2006, do all applicable related investigative, corrective, and other specified actions, in accordance with the Accomplishment Instructions of Honeywell Alert Service Bulletin 7510100-34- A0035, dated July 11, 2003; and Honeywell Service Bulletin 7510100-34-0037, dated July 8, 2004; to ensure that the NRM is at the Mod T configuration. Once the actions in this paragraph are completed, the AFM revision required by paragraph (h) of this AD may be removed from the AFM. (k) If the inspection specified in paragraph (j) of this AD is done within the compliance time specified in paragraph (f) of this AD, paragraph (g) of this AD does not need to be done. 2. (l) For any INU that is not identified in Table 2 of this AD: Within 30 months after the effective date of this AD, perform a one-time general visual inspection of the modification plate for the Honeywell Primus II NV-850 Navigation Receiver Module (NRM); part number 7510134-611, -631, -701, -731, -811, -831, -901, or - 931; which is part of the Honeywell Primus II RNZ-850( )/-851( ) INU; to determine whether Mod L, N, P, R, or T is installed. The modification plate located on the bottom of the Honeywell Primus II RNZ-850( )/-851( ) INU is labeled NV-850, and contains the part number and serial number for the Honeywell Primus II NV-850 NRM. If Mod L, N, P, R, or T is installed, the corresponding letter on the modification plate will be blacked out. Honeywell Alert Service Bulletin 7510100-34- A0035, dated July 11, 2003, is an acceptable source of service information for this inspection. (1) If the NRM is part number 7510134-611, -631, -701, -731 and has Mod T installed: No further action is required by this paragraph. (2) If Mod L, N, P, or R is installed: Within 30 months after the effective date of this AD, do all applicable related investigative, corrective, and other specified actions, in accordance with the Accomplishment Instructions of Honeywell Alert Service Bulletin 7510100-34-A0035, dated July 11, 2003; and Honeywell Service Bulletin 7510100-34-0037, dated July 8, 2004; to ensure that the NRM is at the Mod T configuration. 3. Service Bulletin 7510134-34-A0017, Rev. Original, dated July 11, 2003 should be added to Table 1.

Related Comments

   
Total: 3
Expressjet Airlines
Public Submission    Posted: 06/27/2008     ID: FAA-2008-0556-0004

Jul 03,2008 11:59 PM ET
Honeywell International Inc. - Additional Comments
Public Submission    Posted: 07/01/2008     ID: FAA-2008-0556-0005

Jul 03,2008 11:59 PM ET
Honeywell International Inc.
Public Submission    Posted: 06/26/2008     ID: FAA-2008-0556-0003

Jul 03,2008 11:59 PM ET