# N972EA: 1999 Raytheon 1900D, registration cancelled 2017-07-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 14, 2017 - Exported to: Kenya - Status when cancelled: Valid registration - Airframe: [Raytheon 1900D](https://openairdocs.org/model/raytheon-1900d) (registry code 7150005) - Engine: [Pratt & Whitney Canada PT6-65AR](https://openairdocs.org/engine/pratt-whitney-canada-pt6-65ar) (registry code 52107) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Serial number: UE-389 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: December 11, 1999 - Certificate issued: January 4, 2011 - Last registry action: September 26, 2016 - Mode S code: AD8B78 - Owner when cancelled: [Icecap LLC Trustee](https://openairdocs.org/faa-owner/ICECAP%20LLC%20TRUSTEE) - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: Corporation - Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N972EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=972EA - Page: https://openairdocs.org/deregistered/N972EA-2017-07-14 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Raytheon 1900D: https://openairdocs.org/model/raytheon-1900d.md ## Service difficulty reports (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 7C7A201507090055](https://openairdocs.org/sdr/7C7A201507090055), Jun 20, 2015: SKIN. DENTED. DENT ON LT WING OUTER LE AT WS 304.625. REPAIRED IAW SRM 57-94-02 & ECO 190 57 15 02. - [SDR 7C7A2015041500003](https://openairdocs.org/sdr/7C7A2015041500003), Apr 15, 2015: SKIN. CRACKED. SKIN CRACK FROM EXTRUDING RIVET FA 163.95 JUST BELOW STR 9AR. REPAIRED USING BEECHCRAFT SRM. DATED 4/15/2015 - [SDR 7C7A2015041502](https://openairdocs.org/sdr/7C7A2015041502), Apr 15, 2015: STRUCTURE. CRACKED. CRACKED FOUND AT STRUCTURAL INSPECTION. DAMAGED AREA REPAIRED BY FR CO 104023R1. PARTS REPLACED AND DOUBLERS INSTALLED - [SDR 7C7A201504150001](https://openairdocs.org/sdr/7C7A201504150001), Apr 15, 2015: STRUCTURE. CHAFED. CHAFE DAMAGE AT LT FRAME FS 288-363.25 AND RT FRAME FS318.25 378.25 438.25 451.0. CHAFES ARE BLENDED AND POLISHED. NDT INSPECTED TO ENSURE NO CRACKS HAVE FORMED - [SDR 7C7A201503210020](https://openairdocs.org/sdr/7C7A201503210020), Mar 18, 2015: SWITCH. FALSE INDICATION. LEFT FIRE PULL TEE HANDLE (LEFT RED LIGHT) PULSED ON CLUMB OUT OF VDZ. DIMMED ON THEN OFF 3 TIMES. - [SDR ERAA20140022](https://openairdocs.org/sdr/ERAA20140022), Apr 18, 2014: INDICATOR. INOPERATIVE. LEFT PROP GAUGE INOPERATIVE ON TAKEOFF ROLL. R & R PROP INDICATOR, OPERATIONS CHECKED GOOD IAW MM 31-10-00. - [SDR ERAA201307080049](https://openairdocs.org/sdr/ERAA201307080049), Jul 5, 2013: SPAR WEB. CHAFED. RIGHT WING REAR SPAR HAS DEEP CHAFE SPOT CAUSED BY SPLIT FLAP SWITCH WIRE WS120.98 AND WS121.73. REPAIRED (BLENDED)CHAFING RT WING AFT SPAR WEB, WS 120 IAW FIEL - [SDR ERAA20130038](https://openairdocs.org/sdr/ERAA20130038), May 23, 2013: SEALANT. DEFECTIVE. "CABIN ALT.HIGH" LIGHT ON AT 20,000FT CONTINUED LOSS OF DIFF PRESSURE. AIR LEAK FOUND ALONG LOWER EDGE OF AIRSTAIR DOOR. SEALED ALONG EDGE OF FUSELAGE SKIN AT B - [SDR ERAA201303210031](https://openairdocs.org/sdr/ERAA201303210031), Mar 20, 2013: GAUGE. INOPERATIVE. RIGHT ITT BECAME INOPERATIVE IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE ITT GAUGE, RAN ENGINE, OPS CHECK GOOD. OK FOR SERVICE. - [SDR ERAA20120128](https://openairdocs.org/sdr/ERAA20120128), Dec 30, 2012: ACTUATOR. DEFECTIVE. LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED LT MLG ACTUATOR AND RIGGED IAW B1900D MAINTENANCE MANUAL 32-30-10 AND 32-30-09. BLED IAW 32-30-0 - [SDR ERAA201100010](https://openairdocs.org/sdr/ERAA201100010), Nov 25, 2011: CONTROLLER. INOPERATIVE. TCAS CONTROLLER AND TRANSPONDER CONTROLLER DISPLAY WENT BLANK ON SHORT FINAL INTO ANC. REPLACED CONTROLLER AND SYSTEM OPERATES OK. - [SDR ERAA201100003](https://openairdocs.org/sdr/ERAA201100003), Apr 4, 2011: ACTUATOR. CRACKED. AFTER LANDING FLIGHT CREW NOTED HYDRAULIC FLUID LEAKING FROM LEFT MAIN LANDING GEAR. MAINTENANCE FOUND LMLG ACTUATOR END CAP CRACKED AND LEAKING. REPLACED ACTUA - [SDR ERAAA201000002](https://openairdocs.org/sdr/ERAAA201000002), Jun 27, 2010: HANDLE. SEPARATED. CARGO DOOR HANDLE FELL OFF. REMOVED DOOR HANDLE, REPLACED SNAP RING AND REINSTALLED DOOR HANDLE IAW HB1900D MM 52-30-00. - [SDR ERAA200900008](https://openairdocs.org/sdr/ERAA200900008), Sep 5, 2009: TRANSDUCER. SHORTED. FAI - UPON CLIMBOUT FROM FAI FOUND OIL PRESSURE WENT TO "0" ON RIGHT ENGINE. SHUT DOWN RIGHT ENGINE AND RETURNED TO FAI. REPLACED ENGINE OIL PRESSURE XDCR S/N 4 - [SDR ERAA200900002](https://openairdocs.org/sdr/ERAA200900002), Jun 22, 2009: FITTING. CRACKED. WHILE INSPECTING IAW SB27-3928, FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON THE RT AILERON. - [SDR ERAA200900001](https://openairdocs.org/sdr/ERAA200900001), Jun 22, 2009: FITTING. CRACKED. WHILE INSPECTING IAW SB27-3928 FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON LT AILERON. - [SDR ERAA200700003](https://openairdocs.org/sdr/ERAA200700003), Aug 17, 2007: UNKNOWN. ODOR. STRONG BURNING SMELL AT FL190 AND LIGHT SMOKE OBSERVED BY CREW & PAX. RETURNED TO ANC. VISUALLY INSPECTED WIRING & CONNECTIONS AT WINDSHIELD PANELS, CB PANELS, --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.