N12532

Cancelled 2018

Deregistered aircraft · 1968 Mcdonnell Douglas DC-9-32 · Pratt & Whitney JT8D series

Cancelled
January 11, 2018
Status when cancelled
Registration expired, pending cancellation
Serial number
45791
Year built
1968
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard, transport
Airworthiness date
December 19, 1980
Certificate issued
February 26, 1998
Last registry action
April 2, 2012
Mode S code
A06921
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 · 1

FAA accident and incident reports matched to this aircraft by N12532 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 20000502SH002Power Supply · dirtyDURING ACCOMPLISHMENT OF B-CHECK WORK CARD 0617, DISCOVERED WHEN THE EMERGENCY LIGHTS WERE SELECTED TO THE ON POSITION, THE EMERGENCY LIGHTS ABOVE THE AFT OVERWING EXITS WERE INOPERATIVE. THE PROBLEM WAS TROUBLESHOT TO THE B5-25 BATTERY PACK. THE BATTERY PACKMar 26, 2000 · N12532 · Doug DC932 · Emergency LightingSDR 2000ZZZM87Angle · out of adjustAFTER ARRIVING AT SFB AIRPORT AND PRIOR TO THE DISEMBARKATION OF PASSENGERS AN INADVERTENT DEPLOYMENT OF THE L-1 DOOR SLIDE OCCURRED. THE FLT ATTENDANT HAD OPENED THE L1 DOOR AND SECURED THE DOOR IN THE OPEN POSITION WHEN THE SLIDE PACK COVER FELL OFF. THIS Nov 20, 1999 · N12532 · Doug DC932 · Escape SlideSDR 2000ZZZX89Battery · dischargedDURING ACCOMPLISHMENT OF B-CHECK WORK CARD 0617, DISCOVERED WHEN THE EMERGENCY LIGHTS WERE SELECTED TO THE ON POSITION, THE AFT EMERGENCY LIGHTS ABOVE THE TALL CONE SLIDE DID NOT ILLUMINATE. TROUBLESHOOTING PROCEDURES DETERMINED THE BATTERY POWER SUPPLY WAS Oct 13, 1999 · N12532 · Doug DC932 · Emergency LightingSDR CALA9800899Relay · inoperativeWHEN GEAR WAS EXTENDED ON APPROACH, ONLY UPPER HALF OF GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. THE GEAR WAS RECYCLED AND CIRCUIT BREAKERS WERE CHECKED. A GO-AROUND WAS PERFORMED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED THROUGH VIEW PORT. THE AIRCRAFT LAMay 25, 1998 · N12532 · Doug DC932 · Landing Gear Position and WarningSDR CALA9700228Skin · gougedINSPECTION FOUND SKIN GOUGED AT OUTBOARD NR 3 HINGE OF LT ELEVATOR UPPER SURFACE. THE GOUGE WAS REMOVED AND REPAIRED IAW SRM 55-03, FIGURE 14.Feb 11, 1997 · N12532 · Doug DC932 · Elevator, Plate/SkinSDR CALA9700225Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN TOP RIB AND A .25 INCH CRACK IN 7TH RIB FROM BOTTOM OF VERTICAL STABILIZER LEADING EDGE. BOTH CRACKS WERE STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 55-01, FIGURE 2.Feb 11, 1997 · N12532 · Doug DC932 · Vertical Stabilizer, Spar/RibSDR CALA9700226Frame · dentedINSPECTION FOUND AFT CARGO PIT BELTFRAME UPPER FLANGE DENTED AT F.S. 917, STRINGER 29L TO 30L. THE DENT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 5, PAGE 6.Feb 6, 1997 · N12532 · Doug DC932 · Fuselage Main, FrameSDR CALA9700227Bracket · corrodedINSPECTION FOUND CORROSION ON AFT CARGO INTERCOSTAL ATTACH BRACKET AT STA 775, STRINGER 26L. THE ATTACH BRACKET WAS REPLACED WITH A NEW BRACKET IAW SRM 53-21-0 AND 51-30-2.Feb 4, 1997 · N12532 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700224Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON WEB AT STA 1021. THE CRACK WAS LOCATED AT INTERSECTION WITH UPPER SKIN. THE CRACKED AREA WAS REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.Jan 28, 1997 · N12532 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9700223Strip · crackedINSPECTION FOUND NR 1 ENGINE PYLON STRIP ON LOWER STRUCTURE CRACKED FORWARD OF STA 1039.5. THE CRACK WAS 2 INCHES LONG. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-20-0.Jan 28, 1997 · N12532 · Doug DC932 · Nacelle/Pylon StructureSDR CAL960279Skin · crackedHOU - INSPECTION FOUND A 4.5 INCH CRACK IN LEFT UPPER RUDDER SKIN. THE CRACKED AREA WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 55-03. (M)Feb 27, 1996 · N12532 · Doug DC932 · Rudder, Plate/SkinSDR CAL960278Skin · crackedHOU - INSPECTION FOUND A 2 INCH CRACK BETWEEN FOUR RIVETS AT RIVET LINE FOR UPPER CAP AND A .5 INCH CRACK BETWEEN TWO RIVETS AT RIVET LINE FOR UPPER CAP IN RIGHT UPPER RUDDER SKIN. THE CRACKS WERE REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM 55-01Feb 27, 1996 · N12532 · Doug DC932 · Rudder, Plate/SkinSDR CAL950350Vent Valve · malfunctionedFLT NR 1454 - IAH - ON CLIMB-OUT FUEL VENTING OVERBOARD OUT LEFT WING. AIRCRAFT RETURNED TO IAH. FOUND THAT CLIMB VENT VALVE NEEDED TO BE REPLACED. REMOVED AND REPLACED VENT VALVE P/N 770400. FILLED RT WING TO 9300 LBS AND OPS CHECK GOOD. (W)Apr 5, 1995 · N12532 · Doug DC932 · Aircraft Fuel Distribution System