N409EA

Cancelled 2005

Deregistered aircraft · 1977 Mcdonnell Douglas DC-9-51 · Pratt & Whitney JT8D-5

Cancelled
June 15, 2005
Status when cancelled
Valid registration
Serial number
47728
Year built
1977
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard, transport
Airworthiness date
July 13, 1977
Last registry action
June 15, 2005
Mode S code
A4CE75
Owner when cancelled
Ram Air Sales Inc
Owner type
Corporation

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.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N409EA and the event date: up to this one’s cancellation.

Service difficulty reports · 13

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

SDR TWAA9819201Switch · looseSPARKS CAME OUT OF THE NOSE TAXI LIGHT SWITCH. TURNED OFF SWITCH. CIRCUIT BREAKER POPPED. SYSTEM WAS PLACARDED INOPERATIVE PER MEL. MAINTENANCE LATER TIGHTENED THE SWITCH. CHECK-C 9-16-98 MCI.Dec 1, 1998 · N409EA · Doug DC951 · Exterior LightingSDR TWAA9814401Bulkhead Tee · damagedDURING CHECK-C, MAINT FOUND UPPER T-CAP AT STA 1147 DAMAGED WHEN LT T-CAP WAS REMOVED AT AFT PRESSURE BULKHEAD. SPLICE STRAP, CLIPS AND SHIMS INSTALLED PER ARA 15382.Sep 3, 1998 · N409EA · Doug DC951 · Fuselage Main, BulkheadSDR TWAA9814203Track · corrodedDURING CHECK-C, MAINT FOUND CORROSION IN AFT CARGO COMPT, LT TIE DOWN TRACK, FROM FWD END TO AFT END OF BIN. TRACK WAS REMOVED AND REPLACED. INSTALLED PER SRM 53-01, PG 10 FIG 2 SHEET 4.Sep 1, 1998 · N409EA · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9814202Bulkhead Cap · crackedDURING CHECK-C, MAINT FOUND CRACK INDICATION BETWEEN STR 10L AND 11L, REAR PRESS BULKHEAD T-CAP. REMOVED AND REPLACED T-CAP. SPLICED IN PER SRM 53-03, FIG 37A.Aug 31, 1998 · N409EA · Doug DC951 · Fuselage Main, BulkheadSDR TWAA9814108Pan · damagedDURING CHECK-C, MAINT FOUND INTERIM REPAIR INSTALLED PER ARA 11885 AT RT AFT EMERGENCY EXIT DOOR PAN. REPLACED SECTION OF PAN PER SRM 52-05, FIG 51.Aug 28, 1998 · N409EA · Doug DC951 · Emergency ExitsSDR TWAA9814107Pan · damagedDURING CHECK-C, MAINT FOUND INTERIM REPAIR INSTALLED PER ARA 11885 AT THE LT AFT EMERGENCY EXIT DOOR PAN. REPLACED SECTION OF PAN PER SRM 52-05, FIG 51.Aug 28, 1998 · N409EA · Doug DC951 · Emergency ExitsSDR TWAA9814109Angle · crackedDURING CHECK C, MAINT FOUND CRACKED SUPPORT ANGLE INSIDE ACCESS PLATE NR 8111A AT UPPER AFT ENG MOUNT. MADE AND INSTALLED NEW SUPPORT ANGLE WITH EXISTING ORIGINAL HARDWARE AFTER PRIMING.Aug 21, 1998 · N409EA · Doug DC951 · Engine Mount SectionSDR TWAA9813604Tie Down Track · corrodedDURING CHECK-C MAINT, FOUND IN AFT CARGO COMPT THE RT TIE DOWN TRACK, AFT OF CARGO DOOR, WITH CORROSION IN CHANNEL. REPLACED RT TIE DOWN TRACK AFT OF DOOR PER SRM 51-01, PAGE 4.Aug 19, 1998 · N409EA · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM1201Longeron · crackedSTL - DURING OP-15, FOUND CRACK APPROXIMATELY ONE INCH LONG IN LONGERON 17R, STATION 1151, TOP AND BOTTOM LEGS. REPAIRED PER SRM 53-02. AIRCRAFT TOTAL TIME 41,764, TOTAL CYCLES 37,652.Apr 12, 1996 · N409EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 96ZZZM50Oil Cap · missingSTL - DURING CRUISE, SHUTDOWN NR 2 ENGINE, S/N 1526, DUE TO DECREASING OIL PRESSURE AND OIL QUANTITY. FOUND OIL CAP MISSING, REPLACED OIL CAP, INSPECTED OIL SCREEN, SERVICED OIL, RAN AND LEAK CHECKED ENGINE. OPERATIONS CHECKED NORMAL. (M)Dec 21, 1995 · N409EA · Doug DC951 · Turbine Engine Oil SystemSDR 96ZZZM49Turbine Blade · failedIND - FLT NR 275 - DURING CLIMB, SHUT DOWN NR 1 ENGINE. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION CHECKS NORMAL. INVESTIGATION OF METAL PARTICLES IN TAILPIPE AFTER SHUTDOWN OF NR 1 ENGINE, REVEALED THAT A FIRST STAGE TURBINE BLADDec 21, 1995 · N409EA · Doug DC951 · Turbine SectionSDR 95ZZZW738Doubler · crackedSTL - DURING SPECIAL CHECK, FOUND ONE .1875 INCH CRACK IN -85 LOWER LEFT CORNER, STATION 1167. STOP DRILLED CRACK AND REPAIRED PER SERVICE BULLETIN 137 AND EMLR 65694. (W)Apr 24, 1995 · N409EA · Doug DC951 · Fuselage Miscellaneous StructureSDR 95ZZZX860Attach Angle · crackedSTL - DURING CHECK C, FOUND A .25 INCH CRACK IN VERTICAL STABILIZER RIGHT DORSAL FIN ATTACH ANGLE, FROM FASTENER HOLE TO EDGE. REPAIRED PER SRM 51-30 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 38,864 HOURS; 35,359 CYCLES.Jan 20, 1995 · N409EA · Doug DC951 · Vertical Stabilizer

Other aircraft with N409EA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N409EA is registered now to the first aircraft listed.