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Aircraft connectivity

STC SA2496NM

FAA DRS lists SA2496NM as Current · Surrendered, held by GTE Airfone Incorporated, for McDonnell Douglas DC-9-81 (MD-81), McDonnell Douglas DC-9-82 (MD-82), and McDonnell Douglas DC-9-83 (MD-83). Recorded change: Installation of air to ground public telephone communication system. Snapshot dated June 30, 2026.

FAA-listed holder
GTE Airfone Incorporated
Aircraft configurations
3
FAA revision date
FAA status
Current · Surrendered

Recorded modification

What the FAA record covers

Installation of air to ground public telephone communication system.

SA2496NM identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: McDonnell Douglas DC-9-81 (MD-81), McDonnell Douglas DC-9-82 (MD-82), and McDonnell Douglas DC-9-83 (MD-83). Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas DC-9-81 (MD-81)A6WEMcDonnell Douglas DC-9-82 (MD-82)A6WEMcDonnell Douglas DC-9-83 (MD-83)A6WE

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact McDonnell Douglas DC-9-81 (MD-81) and McDonnell Douglas DC-9-82 (MD-82), and 1 more aircraft configuration model, serial range, and configuration?
  2. 02Which antenna, radome, LRUs, and service assumptions are included?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

Related aircraft connectivity STCs

SA970NEAircraft connectivity

Installation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations: United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) ___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47. CONFIGURATION 1: Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows: Option 1: Radome In accordance with drawings 150017, 190011, 190018 and 190019. Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing 190019. This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system compatibility. Option 2: Dual Alternator System In accordance with drawings 4-7781 and 4-7782. Option 3: Bow Compartment Covers In accordance with drawing 4-3501. Option 4: Upper Fin Revision In accordance with drawing 4-2652, Revision C. Option 5: Disassembly Provisions In accordance with drawing 300015. Option 6: Dual Rudder/Aileron Electric Trim System In accordance with drawing 4-3519 and STC SA1142SO. CONFIGURATION 2: Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003.

FAA holder: Revo Inc

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