# N130AM: 1989 Embraer EMB-120RT, registration cancelled 2004-02-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 25, 2004
- Status when cancelled: Sale reported
- Airframe: [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt) (registry code 3260202)
- Engine: [Pratt & Whitney Canada PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118) (registry code 52116)
- Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 120.134
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 19, 1989
- Last registry action: December 18, 2003
- Mode S code: A07B3D
- Location: [Lewisville, TX](https://openairdocs.org/faa-place/TX/Lewisville)
- Owner type: Individual
- Owner's area on the map: 33.0506° N, 96.9727° W: Placed by OpenAirDocs at the center of ZIP code 75057, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N130AM
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=130AM
- Page: https://openairdocs.org/deregistered/N130AM-2004-02-25

From the FAA registry file of October 29, 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 Embraer EMB-120RT: https://openairdocs.org/model/embraer-emb-120rt.md

## Service difficulty reports (12)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA99014S](https://openairdocs.org/sdr/ASOA99014S), Jan 23, 1999: ENGINE. FAILED. FLT 4825 - EN ROUTE DFW-AMA, A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT VIBRATION, SMOKE IN CABIN AND COCKPIT, AND REDUCED POWER IN LEFT ENGINE (20 PERCENT TORQ
- [SDR 98ZZZX4722](https://openairdocs.org/sdr/98ZZZX4722), Nov 10, 1998: BOLT. SHEARED. DURING INSTALLATION OF PROPELLER ASSEMBLY ON THE RIGHT ENGINE OF S/N 120134, ONE ATTACHMENT BOLT SHEARED PRIOR TO REACHING TORQUE OF 140 FEET/POUNDS.
- [SDR 98ZZZX4831](https://openairdocs.org/sdr/98ZZZX4831), Nov 9, 1998: BRACKET. CORRODED. AT STA 4825.5, THE LEFT HAND FLOOR SUPPORT BRACKET BETWEEN THE LEFT HAND OMEGA BEAM AND THE FUSELAGE, WAS FOUND SEVERELY EXFOLIATED. THIS AREA IS EXPOSED TO MOI
- [SDR 98ZZZX4721](https://openairdocs.org/sdr/98ZZZX4721), Nov 9, 1998: SKIN. CORRODED. AT STA 7257.6 UNDERNEATH FRAME 22 IN BETWEEN STR 21L AND STR 20R, CORROSION DETECTED WHICH EXCEEDED THE MANUFACTURER'S RECOMMENDATION FOR ALLOWABLE DAMAGE. THE 
- [SDR 98ZZZX4174](https://openairdocs.org/sdr/98ZZZX4174), Nov 3, 1998: ANGLE. CRACKED. AFT FUSELAGE-TO-FIN CONNECTING ANGLE AT THE BASE OF THE VERTICAL STABILIZER AT FS 16128.0, A CRACK WAS DISCOVERED TRAVELING BETWEEN TWO FASTENERS. SUBMITTER STA
- [SDR 98ZZZX4173](https://openairdocs.org/sdr/98ZZZX4173), Nov 2, 1998: NUT. CRACKED. TWO OF THE THREE ATTACHMENT BOLTS FOR THE OUTBOARD TORQUE MOUNT P/N LM-430-SA7 NUTS WERE FOUND CRACKED DURING C-CHECK INSPECTION. SUBMITTER STATED POSSIBLY OVER
- [SDR ASOA97012](https://openairdocs.org/sdr/ASOA97012), Mar 5, 1997: SEAL. DEFECTIVE. EN ROUTE ATL-MYR - AT FL 190, THE CABIN STARTED TO CLIMB. THE CREW ATTEMPTED TO REGAIN CONTROL CABIN PRESSURE TO NO AVAIL. DESCENDED TO 8,000 FEET AND RETURNED 
- [SDR ASOA96046](https://openairdocs.org/sdr/ASOA96046), Oct 16, 1996: OIL PUMP. FALIED. APPROXIMATELY 60 MILES OUT ON APPROACH ICT-DFW, RIGHT NP BEGAN FLUCTUATING FROM 83 PECENT TO 87 PERCENT. ATTEMPTED 100 PERCENT NP, AND NP ROSE TO 101.5 PERCENT.
- [SDR RAIA950512](https://openairdocs.org/sdr/RAIA950512), May 17, 1995: SENSOR. MOISTURE. STL - FLT 7215 - DUCT LEAK LIGHT ILLUMINATED ON 'MAP' PANEL. MAINTENANCE INSPECTED AND CLEANED WATER/MOISTURE FROM DUCT LEAK SENSORS. PERFORMED GROUND RUNS WITH
- [SDR RAIA950501](https://openairdocs.org/sdr/RAIA950501), May 2, 1995: CONTROL UNIT. FAILED. STL - FLT 7213 - NACELLE FLAP FAULT IN FLIGHT. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM CHECK GOOD. (W)
- [SDR RAIA950245](https://openairdocs.org/sdr/RAIA950245), Feb 27, 1995: EJECTOR VALVE. STICKY. STL - FLT 7502 - THE LT AND RT WING I/B DE-ICE BOOT FAULTED ALONG WITH LT AND RT HORIZONTAL STAB. THE I/B DE-ICE BOOTS. MAINTENANCE CLEANED DE-ICE EJECTOR VALVE
- [SDR RAIA950242](https://openairdocs.org/sdr/RAIA950242), Feb 23, 1995: CONTROL UNIT. FAILED. BHM - FLT 7461 - THE FLAP ASSYMETRY OCCURRED, RT FLAP WENT UP AND DOWN. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM TEST GOOD. (W)

## Other aircraft with N130AM

- [Registered now](https://openairdocs.org/aircraft/N130AM): Yakovlev YAK-3U, S/N 170101, built 1995

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