N215AS

Cancelled 2001

Deregistered aircraft · 1985 Embraer EMB-120RT · Pratt & Whitney Canada PW115

Cancelled
October 19, 2001
Status when cancelled
Valid registration
Serial number
120.010
Year built
1985
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
November 28, 1985
Certificate issued
September 10, 2001
Last registry action
September 10, 2001
Mode S code
A1CC26
Owner type
Corporation

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 · 9

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

SDR ASOA99108Warning Light · illuminatedFLT 4241 - APPROX 15 MINUTES AFTER DEPARTING ATL AND 30 NM WEST THE RIGHT ENGINE BLEED AIR 'DUCT LEAKAGE' WARNING LIGHT ILLUMINATED. WE WENT THROUGH THE 'DUCT LEAK LIGHT ILLUMINATED' CHECKLIST WHILE BEING VECTORED BACK TO ATL. THE LIGHT FAILED TO EXTINGUISH,Sep 29, 1999 · N215AS · Emb EMB120RT · Pneumatic Indicating SystemSDR ASOA99058Seal · failedFLT 4912 - RAPID DECOMPRESSURIZATION AT 20,000 FEET. MANUAL MODE DID NOT CONTROL RATE AT THIS ALTITUDE. AT 10,000 FEET, MANUAL MODE WAS ABLE TO CONTROL RATE. PASSENGER MASKS DID DEPLOY DURING DEPRESSURIZATION. FLIGHT LANDED SAFELY. MAINTENANCE FOUND BOTTOJul 7, 1999 · N215AS · Emb EMB120RT · Cargo/Baggage DoorsSDR ASOA99041Clamp · looseDURING CLIMB-OUT CSG-ATL, RIGHT ENGINE 'DUCT LEAKAGE' LIGHT ILLUMINATED. LIGHT REMAINED ON FOR 3 MINUTES AFTER CLOSRING RIGHT ENGINE BLEED. DUCT LEAK LIGHT WENT OUT 4 MINUTES AFTER RIGHT ENGINE WAS SHUTDOWN. DECLARED AN EMERGENCY AND RETURNED TO CSG. MAINTApr 28, 1999 · N215AS · Emb EMB120RT · Pneumatic Distribution SystemSDR ASOA99024Angle · brokenDURING C-CHECK INSPECTION, THE FRAME 2 ANGLE ON LEFT ENGINE NACELLE WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLE ON LEFT ENGINE NACELLE. (M)Feb 11, 1999 · N215AS · Emb EMB120RT · Nacelle/Pylon StructureSDR ASOA99023Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)Feb 11, 1999 · N215AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR 99ZZZX1134Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB, BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. ON THE RT Feb 11, 1998 · N215AS · Emb EMB120RT · Nacelle/Pylon, Main FrameSDR 99ZZZX1133Frame · crackedRECOMMEND REPLACING BOTH FRAMES, AND CONTINUE MOINITORING IAW EXISTING MAINTENANCE CHECKS.Feb 11, 1998 · N215AS · Emb EMB120RT · Nacelle/Pylon, Main FrameSDR ASOA96013Hydraulic Line · chaffedDURING CRUISE FLIGHT ROA-ATL, AIRCRAFT LOST BLUE HYDRAULIC SYSTEM PRESSURE. THE CREW SHUT OFF THE ELECTRIC DRIVEN PUMP AND ADVISED ATC, WHO DECLARED AN EMERGENCY. THE AIRCRAFT LANDED ZERO FLAPS IN ATL SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED THE RIApr 15, 1996 · N215AS · Emb EMB120RT · Hydraulic System, MainSDR ASOA95002Prox Switch · failedATL/LYH - FLT 7248 - UPON SELECTING GEAR DOWN TO LAND, LANDING GEAR WOULD NOT EXTEND. HAD TO USE ELECTRIC OVERRIDE TO EXTEND GEAR SUCCESSFULLY. CONTINUED APPROACH AND LANDED SAFELY AND WITHOUT INCIDENT. A/C WAS FERRIED LYH-ATL GEAR DOWN. IN ATL, REPLACED RJan 21, 1995 · N215AS · Emb EMB120RT · Landing Gear Retraction/Extension System

Other aircraft with N215AS · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N215AS is registered now to the first aircraft listed.