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FAA orders · airworthiness directive · current

98-25-02: Top-mounted Antenna

FAA order 98-25-02 is an airworthiness directive in force since December 22, 1998. The FAA's subject line: Top-mounted Antenna. It names Airbus Helicopters AS-365, Beechcraft 300 King Air 300, Beechcraft 65, Beechcraft A100, Beechcraft A200, Beechcraft B100, Beechcraft B200 King Air B200, Beechcraft B300 King Air 350, Bell 206 JetRanger and LongRanger, Bell 407, Bell 525, Cessna 172 Skyhawk, Cessna 182 Skylane, Cessna 206 Stationair, Cessna 208 Caravan, Cessna 210 Centurion, Cessna 310, Cessna 320, Cessna 335, Cessna 336, Cessna 337 Skymaster, Cessna 340, Cessna 401, Cessna 402, Cessna 404, Cessna 411, Cessna 414 Chancellor, Cessna 421 Golden Eagle, Cessna 425 Conquest I, Cessna 441 Conquest II, Cessna 500 Citation I, Cessna 501 Citation I/SP, Cessna 525 CitationJet (CJ series), Cessna 550 Citation II, Cessna 551, Cessna 560 Citation V, Ultra, Encore and Excel, Daher (Socata) TBM-700 TBM 700 through TBM 960, Dassault FALCON 10, Dehavilland DHC-6, Hawker Siddeley HS.125 SERIES 700A, Israel Aircraft Industries 1124, Mitsubishi MU-2, Mooney M-20, Mooney M22, Piper PA-23 Apache and Aztec, Piper PA-31 Navajo and Chieftain, Piper PA-32 Cherokee Six, Lance and Saratoga, Piper PA-34 Seneca, Piper PA-42, Piper PA-46 Malibu, Mirage, Matrix and M-Class: about 65,033 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: instruments and avionics.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
Bell Helicopter Textron Canada Limited; Cessna Aircraft Company; Dassault Aviation; Airbus Helicopters; Mooney Aircraft Corporation; Mooney Aviation Company Inc; SOCATA; Viking Air Limited; Textron Aviation Inc.; Israel Aircraft Industries Ltd.; Mitsubishi Heavy Industries Ltd.; Piper Aircraft Inc.
Models
407, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172RG, 172S, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, 206, 206H, 208, 208B, 210, 210-5 (205), 210-5A (205A), 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, 310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, 310I, 310J, 310J-1, 310K, 310L, 310N, 310P, 310Q, 310R, 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 321, 335, 336, 337, 337A, 337B, 337C,...
On this site
Airbus Helicopters AS-365 20 registered
Beechcraft 300 King Air 300 132 registered
Beechcraft 65 201 registered
Beechcraft A100 15 registered
Beechcraft A200 34 registered
Beechcraft B100 59 registered
Beechcraft B200 King Air B200 718 registered
Beechcraft B300 King Air 350 784 registered
Bell 206 JetRanger and LongRanger 1,455 registered
Bell 407 985 registered
Bell 525 7 registered
Cessna 172 Skyhawk 20,669 registered
Cessna 182 Skylane 11,828 registered
Cessna 206 Stationair 213 registered
Cessna 208 Caravan 1,022 registered
Cessna 210 Centurion 1,526 registered
Cessna 310 1,410 registered
Cessna 320 137 registered
Cessna 335 27 registered
Cessna 336 35 registered
Cessna 337 Skymaster 372 registered
Cessna 340 707 registered
Cessna 401 51 registered
Cessna 402 174 registered
Cessna 404 26 registered
Cessna 411 10 registered
Cessna 414 Chancellor 605 registered
Cessna 421 Golden Eagle 770 registered
Cessna 425 Conquest I 161 registered
Cessna 441 Conquest II 172 registered
Cessna 500 Citation I 63 registered
Cessna 501 Citation I/SP 189 registered
Cessna 525 CitationJet (CJ series) 1,968 registered
Cessna 550 Citation II 500 registered
Cessna 551 34 registered
Cessna 560 Citation V, Ultra, Encore and Excel 1,341 registered
Daher (Socata) TBM-700 TBM 700 through TBM 960 1,006 registered
Dassault FALCON 10 57 registered
Dehavilland DHC-6 115 registered
Hawker Siddeley HS.125 SERIES 700A 7 registered
Israel Aircraft Industries 1124 73 registered
Mitsubishi MU-2 177 registered
Mooney M-20 6,247 registered
Mooney M22 14 registered
Piper PA-23 Apache and Aztec 1,316 registered
Piper PA-31 Navajo and Chieftain 935 registered
Piper PA-32 Cherokee Six, Lance and Saratoga 3,917 registered
Piper PA-34 Seneca 998 registered
Piper PA-42 59 registered
Piper PA-46 Malibu, Mirage, Matrix and M-Class 1,692 registered

Dates and paperwork

In force since
December 22, 1998
Published
December 3, 1998 (signed November 24, 1998)
Docket
98-CE-107-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment adopts a new airworthiness directive (AD) that applies to all BF Goodrich Avionics Systems, Inc. (BF Goodrich) SKYWATCH SKY497 installations with a top-mounted antenna that are installed on aircraft. This AD requires incorporating information into the airplane flight manual (AFM) that specifies verifying the correct antenna configuration each time an aircraft equipped with a SKY497 installation with a top-mounted antenna is powered-up. The AD also requires removing from service any of these SKY497 installations with an incorrect antenna configuration. This AD results from numerous reports of internal component failure of the above-referenced installations, which changed the antenna configuration (from TOP to BOTTOM mount). The actions specified by this AD are intended to prevent the display of target indicators on the wrong side of the aircraft caused by an internal component failure in the SKY497 installations with a top-mounted antenna, which could resultin the pilot making an incorrect initial maneuver based on the displayed information while trying to visually acquire the aircraft.

The order itself the regulatory text, as published

Show the full text (6,188 characters)
98-25-02 BFGOODRICH AVIONICS SYSTEMS, INC.: Amendment 39-10924, Docket No. 98-CE-107-AD. \n\n\tApplicability: SKYWATCH SKY497 installations with a top-mounted antenna that are installed on, but not limited to, the following aircraft, all serial numbers, certificated in any category: \n\n\nManufacturer\nAircraft Models and/or Series\nRaytheon\nBeech 90, 100, 200, and 300 Series\nCessna\n172, 182, 206, 208, 210, 300, 400, and 500 Series\nPiper\nPA-23, PA-31-360, PA-31T, PA-32, PA-34, PA-42, and PA-46\nHawker\nHS-700 and HS-800\nMitsubishi\nMU-2 Series\nDassault\nF10\nMooney\nM20 Series\nBombardier\nDHC-6 Series\nWestwind\n1124\nBell\n407\nEurocopter\nAS365\nSocata\nTBM700 \n\n\tNOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. \n\n\tCompliance: Required as indicated in the body of this AD, unless already accomplished. \n\n\tTo prevent the display of target indicators on the wrong side of the aircraft caused by an internal component failure in the SKY497 installations with a top-mounted antenna, which could result in the pilot making an incorrect initial maneuver based on the displayed information while trying to visually acquire the aircraft, accomplish the following: \n\n\t(a)\tWithin the next 25 hours time-in-service (TIS) after the effective date of this AD, place the information in the Appendix to this AD into the Limitations Section of the airplane flight manual (AFM). \n\n\t\t(1)\tThis information specifies verifying the correct antenna configuration each time an aircraft equipped with a SKY497 installation with a top-mounted antenna is powered-up. \n\n\t\t(2)\tThis information is a duplication of the information presented in BF Goodrich Alert Service Bulletin #78A, dated October 21, 1998. \n\n\t(b)\tIf an incorrect antenna configuration is found during any of the power-up procedures specified in the AFM information required by this AD, prior to further flight, remove the SKY497 installation from service. \n\n\t(c)\tInserting the information into the Limitations Section of the AFM as required by paragraph (a) of this AD may be performed by the owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7), and must be entered into the aircraft records showing compliance with this AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). \n\n\t(d)\tSpecial flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. \n\n\t(e)\tAn alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Chicago Aircraft Certification Office (ACO), 2300 East Devon Avenue, Des Plaines, Illinois 60018. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Chicago ACO. \n\n\tNOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Chicago ACO. \n\n\t(f)\tThe service information referenced in this AD may be obtained from BF Goodrich Avionics Systems, Inc. 5353 52nd Street,Southeast, P.O. Box 873, Grand Rapids, Michigan 49588-0873. This document or other information related to this AD may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri. \n\n\t(g)\tThis amendment becomes effective on December 22, 1998. \n\nAPPENDIX TO AD 98-25-02; \nAMENDMENT 39-10924; DOCKET NO. 98-CE-107-AD. \n\nPOWER-UP PROCEDURES FOR SKYWATCH SKY497 \nINSTALLATIONS WITH A TOP-MOUNTED ANTENNA \n___________________________________________________________________________________________________\n\nThe following power-up procedure must be accomplished each time the system is powered-up: \n\n1.\tIf a WX-1000 is installed with the SKYWATCH, ensure that the STORMSCOPE/CWS switch is in the CWS position. \n\n2.\tAt the SKYWATCH display, access the service menu by holding the left two buttons depressed and switch the system on. Hold the buttons until the Service Menu is displayed. The Service Menu is shown in figure 1.3.\tHighlight SYSTEM DATA (press NEXT button two times) and then press SELECT. The SYSTEM DATA screen, as shown in figure 2 will be displayed. \n\n4.\tHighlight CONFIGURATION by pressing the NEXT button and then press SELECT. The configuration display consists of 4 pages. Advance to Page 3 of 4 (see figure 3) by pressing the NEXT button two times. \n\n5.\tVerify that the antenna position is configured for TOP mount (i.e., as shown in figure 3). \n\n\nAPPENDIX TO AD 98-25-02; \nAMENDMENT 39-10924; DOCKET NO. 98-CE-107-AD. \n\nPOWER-UP PROCEDURES FOR SKYWATCH SKY497 \nINSTALLATIONS WITH A TOP-MOUNTED ANTENNA \n(Continued) \n___________________________________________________________________________________________________\n\n\n\n\n\n6.\tIf the antenna configuration is correct, press EXIT until the start-up screen (see figure 4) is displayed. \n\n\n\n\n\n7.\tIf a WX-1000 is installed, position the STORMSCOPE/CWS switch to the STORMSCOPE position and exit the STORMSCOPE servicemenu by pressing the EXIT button. \n\n8.\tIf the antenna configuration is not correct (i.e., configured for Bottom mount), turn SKYWATCH off and return the unit for service.

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/98-25-02.json · aircraft systems.