AIRWORTHINESS DIRECTIVE

CAA-AD-T-072/1999

Date of issue: July 19, 1999

APPLIANCE - NAVIGATION SYSTEMS USING A GPS (ATA 34) - MODIFICATION/INSPECTION

Applicability: This Airworthiness directive applies to all IFR certified aircraft fitted with a navigation system including a GPS sensor listed in Appendix 1.

Effective date: Upon receipt.

Compliance : Required as indicated in DGAC AD 1999-258(AB).

Remarks: Where applicable, the requirements of this AD must be integrated into the Aircraft´s Logbook(s). Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel: 420 2 33320922, fax: 420 2 20562270.

Ing. Pavel MATOUŠEK
Director of Airworthiness Division CAA CZ

DGAC AD ref.: 1999-258(AB)

GPS

Navigation svstems using a GPS (ATA 34)

1. EQUIPMENT AFFECTED

This Airworthiness directive applies to all IFR certified aircraft fitted with a navigation system including a GPS sensor listed in Appendix 1.

This Airworthiness Directive applies to GPS multisensor or standalone systems certified (see Flight Manual) as:

- supplemental IFR navigation systems in accordance with AC 20-138 or AC 20-130A.

- BRNAV systems certified in accordance with AMJ 20X2 or JAA TGL 2.

- primary remote area/ oceanic navigation systems certified in accordance with FAA order N8110-60.

2. REASON

During night from August 21 to 22, 1999, the GPS system week number will transition from 1023 to 1024, and the GPS EPOCH will change. Several GPS systems will erroneously consider week 1024 as week 0 and will consequently use the corresponding EPOCH 0, dated January 6,1980.

This week number roll over ( WNRO) may affect the navigation function, either by inducing a loss of position computation, or an erroneous position.

A test allows to check proper functioning of the equipment after WNRO. The use of the equipments not listed as WNRO immune is prohibited by this AD after August 18, 1999, until the test is performed satisfactorily. August 18, 1999 date has been retain because GPS receiver may anticipate almanach change until 70 hours before GPS End of Week.

3. REQUIRED ACTIONS AND COMPLIANCE

3.1. The use of GPS systems is prohibited on and after August 18, 1999, until the test described in paragraph 3 is successfully passed.

3.2. Before August 1 st ,1999, install a placard near the navigation system control panel, stating

"GPS INOPERANT A PARTIR DU 18 AOUT 1999".

The reactivation of the GPS and the removal of the placard may not be performed until the test described in paragraph 3 is satisfactorily passed.

3.3. Test of proper functioning after WNRO

Switch on the navigation system and check the following :

* check that the GPS date is correct.

*check that the GPS time is correct ( if this cannot be displayed, check that the GPS position is correct, i.e check that the difference between the GPS position and the aircraft position does not exceed 0,5 NM).

*check that the GPS uses the satellites indicated by the new almanach, by comparing the satellites used by the GPS with those indicated by a GPS prediction software for the test date and time.

If not possible, check that the GPS position is correct (see above).

* check that there is no alarm or messages.

EFFECTIVE DATE : JUNE 26, 1999

APPENDIX 1

NON COMPLIANT RECEIVER OR LACK OF RESPONSE FROM GPS MANUFACTURER

MANUFACTURER

TYPE

P/N

HONEYWELL

 

HG 2021 AB

UNIVERSAL

UNS 1 Msp

1114-5X-0XX

ROCKWELL-COLLINS

GPS 900

822-0935-003

ROCKWELL-COLLINS

GPS 4000

822-0931-001

NORTHSTAR

M 3 GPS

1200-0101

TRIMBLE

TNL 2100T

80822-00-XXXX

TRIMBLE

TNL 2101 PLUS

81439-13-XXXX

TRIMBLE

TNL 2101 IO PLUS

81440-13-XXXX

TRIMBLE

TNL 2100TI0

80822-10-XXXX