N130AM

Cancelled 2004

Deregistered aircraft · 1989 Embraer EMB-120RT · Pratt & Whitney Canada PW118

Cancelled
February 25, 2004
Status when cancelled
Sale reported
Serial number
120.134
Year built
1989
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, transport
Airworthiness date
June 19, 1989
Last registry action
December 18, 2003
Mode S code
A07B3D
Owner when cancelled
Sale Reported
Owner type
Individual

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 12

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

SDR ASOA99014SEngine · failedFLT 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 TORQUE). CREW FOLLOWED THE ENGINE FAILURE CHECKLIST, DECLARED AN EMERGENCY AND DIVERTED TO SPS WHERE SIJan 23, 1999 · N130AM · Emb EMB120RT · Engine (Turbine/Turboprop)SDR 98ZZZX4722Bolt · shearedDURING INSTALLATION OF PROPELLER ASSEMBLY ON THE RIGHT ENGINE OF S/N 120134, ONE ATTACHMENT BOLT SHEARED PRIOR TO REACHING TORQUE OF 140 FEET/POUNDS.Nov 10, 1998 · N130AM · Emb EMB120RT · Propeller AssemblySDR 98ZZZX4831Bracket · corrodedAT 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 MOISTURE FROM THE PASSENGER DOOR ENTRY WAY, AND ACIDIC SOFT DRINKS FROM THE GALLERY. SUBMITTER RECOMMNov 9, 1998 · N130AM · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 98ZZZX4721Skin · corrodedAT 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 AREA OF CORROSION WAS EXTENSIVE ENOUGH THAT THE MECHANIC HAD TO CUT A 9.25 INCH BY 1.52 INCH SECTIONov 9, 1998 · N130AM · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 98ZZZX4174Angle · crackedAFT 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 STATED POSSIBLY CAUSE AS FATIGUE AND RECOMMENDED A DETAILED VISUAL INSPECTION BE CALLED OUT DURING C-CNov 3, 1998 · N130AM · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 98ZZZX4173Nut · crackedTWO 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 OVERTORQUED, EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE REMAINING NUT AND RECOMMENDED INSPECTION AT EVENov 2, 1998 · N130AM · Emb EMB120RT · Engine Mount SectionSDR ASOA97012Seal · defectiveEN 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 TO ATL. REMOVED RTV FROM LEFT BOTTOM AIRSTAIR DOOR SEAL AND SHIMMED RIGHT SIDE OF AIRSTAIR DOOR. Mar 5, 1997 · N130AM · Emb EMB120RT · Passenger/Crew DoorsSDR ASOA96046Oil Pump · faliedAPPROXIMATELY 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. CAPTAIN BROUGHT THE POWER LEVER BACK TO CONTROL THE NP, FLUCTUATION CONTINUED (WENT TO 105 PERCEOct 16, 1996 · N130AM · Emb EMB120RT · Propeller Controlling SystemSDR RAIA950512Sensor · moistureSTL - FLT 7215 - DUCT LEAK LIGHT ILLUMINATED ON 'MAP' PANEL. MAINTENANCE INSPECTED AND CLEANED WATER/MOISTURE FROM DUCT LEAK SENSORS. PERFORMED GROUND RUNS WITH BLEED AIR ON, NO LEAK LIGHT ILLUMINATED. SYSTEM CHECK NORMAL.May 17, 1995 · N130AM · Emb EMB120RT · Pneumatic Distribution SystemSDR RAIA950501Control Unit · failedSTL - FLT 7213 - NACELLE FLAP FAULT IN FLIGHT. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM CHECK GOOD. (W)May 2, 1995 · N130AM · Emb EMB120RT · Trailing Edge Flap Control SystemSDR RAIA950245Ejector Valve · stickySTL - 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 VALVES. OPERATION CHECK GOOD. (W)Feb 27, 1995 · N130AM · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR RAIA950242Control Unit · failedBHM - FLT 7461 - THE FLAP ASSYMETRY OCCURRED, RT FLAP WENT UP AND DOWN. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM TEST GOOD. (W)Feb 23, 1995 · N130AM · Emb EMB120RT · Trailing Edge Flap Control System

Other aircraft with N130AM · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N130AM is registered now to the first aircraft listed.