N1972

Cancelled 2017

Deregistered aircraft · 1963 Boeing 727-23 · Pratt & Whitney JT8D series

Cancelled
February 28, 2017
Status when cancelled
Registration expired, pending cancellation
Serial number
18428
Year built
1963
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Experimental, research and development
Airworthiness date
December 8, 1995
Certificate issued
March 23, 1999
Last registry action
August 8, 2005
Mode S code
A184CA
Owner when cancelled
Aircraft Support And Parts Inc
Location
Davie, FL
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.

NTSB investigations · 1

Matched to this aircraft by N1972 and the event date: after January 15, 1940, when the previous aircraft’s registration ended, through this one’s cancellation.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N1972 and the event date: after January 15, 1940, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 12

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

SDR 97ZZZX4646Spar · crackedDURING ROUTINE INSPECTION OF AIRCRAFT, TWO CRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER'S AFT SPAR LOWER CHORD. EACH CRACK WAS APPROXIMATELY 1.5 INCH LONG. ONE CRACK WAS AT STABILIZER STA 169 AND THE OTHER WAS AT STABILIZER STA 179.Sep 16, 1997 · N1972 · Boeing 72723 · Horizontal Stabilizer, Spar/RibSDR 95ZZZX7070Rib · crackedWHILE INSPECTING AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT RT WS 546.5 WAS FOUND CRACKED ON LOWER FLANGE ADJACENT TO THE SECOND FASTENER HOLE FROM FORWARD END OF RIB. SUSPECT CAUSE: FATIGUE.Nov 28, 1995 · N1972 · Boeing 72723 · Wing, Rib/BulkheadSDR 95ZZZX7069Skin · corrodedWHILE INSPECTING AIRCRAFT PER AD 91-06-06 (SB 727-53-0072), THE FUSELAGE SKINS AT THE LAP JOINT AT STR 19R, BS 360 WERE FOUND CORRODED INSIDE THE LAP JOINT. SUSPECT CAUSE: DELAMINATION OF COLD BOND LAP JOINT.Nov 28, 1995 · N1972 · Boeing 72723 · Fuselage Main, Plate/SkinSDR 95ZZZX7068Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 601.5 WAS FOUND CRACKED IN 4 PLACES. THE UPPER FLANGE WAS CRACKED AT THE 2ND FASTENER HOLE FORWARD OF THE AFT END. THE LOWER FLANGE WAS CRACKED AT THE 3RD, 4TH,Nov 28, 1995 · N1972 · Boeing 72723 · Wing, Rib/BulkheadSDR 95ZZZX7067Stringer · corrodedDURING THE COURSE OF ROUTINE MAINTENANCE, FUSELAGE STR 21R WAS FOUND EXFOLIATED, REQUIRING SRM REPAIR. SUSPECT CAUSE: AREA IS DIRECTLY BELOW GALLEY, ALTHOUGH NO DIRECT EVIDENCE OF LEAKAGE WAS FOUND.Nov 28, 1995 · N1972 · Boeing 72723 · Fuselage Main, Longeron/StringerSDR 95ZZZX7066Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 686.5 WAS FOUND CRACKED IN 2 PLACES AT THE LOWER FLANGE. ONE CRACK WAS AT THE AFTMOST FASTENER HOLE, THE OTHER WAS AT THE THIRD FASTENER HOLE FORWARD FROM THE AFNov 28, 1995 · N1972 · Boeing 72723 · Wing, Rib/BulkheadSDR 95ZZZX7065Closure Rib · corrodedWHILE PERFORMING CPC TASK CARD C55-391-30, THE VERTICAL STABILATOR'S UPPER RT CLOSURE RIB WAS FOUND EXFOLIATED ON ITS OUTBOARD SIDE JUST FORWARD OF THE FORKED END OF THE AFT HINGE POINT FITTING FOR THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED AND FOUND TONov 28, 1995 · N1972 · Boeing 72723 · Vertical Stabilizer, Spar/RibSDR 95ZZZX7064Rib · crackedWHILE INSPECTING AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 546.5 WAS FOUND CRACKED ON ITS LOWER FLANGE ADJACENT TO THIRD FASTENER HOLE FORWARD OF THE AFT END OF RIB. SUSPECT CAUSE: FATIGUE.Nov 28, 1995 · N1972 · Boeing 72723 · Wing, Rib/BulkheadSDR 95ZZZX7063Shear Web · corrodedDURING INSPECTION OF AIRCRAFT PER CPC TASK CARD C53-224-04, THE FLOOR STRUCTURE SHEAR WEB WAS FOUND CORRODED BEYOND SRM LIMITS BETWEEN BS 1168 -BS 1178 AND LBL 30-LBL 36 (UNDER LT AFT LAVATORY).Nov 28, 1995 · N1972 · Boeing 72723 · Fuselage Miscellaneous StructureSDR 95ZZZX7062Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED RIB AT RT WS 601.5 WAS FOUND CRACKED IN 2 PLACES ON THE LOWER FLANGE. ONE CRACK WAS AT THE AFT END FASTENER HOLE AND THE OTHER WAS AT THE THIRD FASTENER HOLE FORWARD OF THE AFT ENNov 28, 1995 · N1972 · Boeing 72723 · Wing, Rib/BulkheadSDR 95ZZZX7061Skin · corrodedWHILE PERFORMING INSPECTION OF THE BONDED CIRCUMFERENTIAL DOUBLER AT BS 481 PER AD 90-26-09 (SB 727-53-0084), MATERIAL LOSS RANGING FROM 10-30 PERCENT WAS DETECTED IN THE AREA BOUNDED BY STR 4L TO STR 4R. UPON OPENING UP OF AREA FOR REPAIR, PHYSICAL MEASUREMENov 28, 1995 · N1972 · Boeing 72723 · Fuselage Main, Plate/SkinSDR 96ZZZX187Stringer · corrodedDURING AN INTERNAL VISUAL INSPECTION PER AD 90-26-09*, THE STRINGER SPLICE ON STR 28R AT BS 480 WAS FOUND SEVERELY CORRODED (EXFOLIATED). REMOVAL OF STRINGER SPLICE REVEALED CORROSION ON STRINGER END AFT OF SPLICE. AIRCRAFT HAS BEEN IN STORAGE SINCE 9/92 IN Aug 22, 1995 · N1972 · Boeing 72723 · Fuselage Main, Longeron/Stringer

Other aircraft with N1972 · 2

The FAA can assign a mark to another aircraft once a registration is cancelled. N1972 is registered now to the first aircraft listed.