# N484DA: Boeing 727-232, registration cancelled 1999-12-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 7, 1999 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 20864 - Type of aircraft: Fixed wing multi engine - Certificate issued: September 11, 1974 - Last registry action: May 20, 1998 - Mode S code: A5F7C1 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.7490° N, 84.3880° W: Placed by OpenAirDocs: center of Atlanta, GA, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N484DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=484DA - Page: https://openairdocs.org/deregistered/N484DA-1999-12-07 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. ADs and bulletins for the Boeing 727-232: https://openairdocs.org/model/boeing-727-232.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL72S991785](https://openairdocs.org/sdr/DL72S991785), Aug 10, 1999: SKIN. CRACKED. FOUND ON E1 LETTER CK, 2 CRACKS AT L-4 WINDOW CUTOUT LOWER INBD FASTENER HOLES. REPAIRED PER SRM 53-30-3. - [SDR DL72S990626](https://openairdocs.org/sdr/DL72S990626), Mar 20, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION - [SDR DL72S990624](https://openairdocs.org/sdr/DL72S990624), Mar 20, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION - [SDR DL72S990623](https://openairdocs.org/sdr/DL72S990623), Mar 20, 1999: SKIN. CRACKED. CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HF - [SDR DL72S990606](https://openairdocs.org/sdr/DL72S990606), Mar 19, 1999: SKIN. CORRODED. THE LOWER FUSELAGE SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND CORRODED BETWEEN FS 720 +17 AND FS 740 NEAR AN A/C DUCT CUTOUT. THE DAMAGED SECTION OF SKI - [SDR DL72S990352](https://openairdocs.org/sdr/DL72S990352), Feb 22, 1999: SWITCH. LOOSE. YELLOW AFT AIRSTAIR LIGHT CAME ON DURING TAKEOFF ROLL. FOUND SWITCH (P/N AN3167-1) LOOSE IN BRACKET (P/N 69-20985-6), REFERENCE IPC 52-70-00-49, ITEM 15 AND 20. - [SDR DL72S990031](https://openairdocs.org/sdr/DL72S990031), Jan 6, 1999: BRACKET. CRACKED. LTR CHK D-2 1/6/99, CRACK IN UPPER O/B RADIUS NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-20-21. - [SDR DL72S990030](https://openairdocs.org/sdr/DL72S990030), Jan 6, 1999: STRINGER. CRACKED. VERT FIN STR 9L CRACKED FIN STA 110.400. REPAIRED PER MM 55-30-0. - [SDR DL72S990029](https://openairdocs.org/sdr/DL72S990029), Jan 6, 1999: SKIN. CRACKED. FOUR CRACKS AT FASTENER HOLES FWD OF PNL 9501 RT SIDE. REPAIRED PER MM 54-30-0. - [SDR DL72S990028](https://openairdocs.org/sdr/DL72S990028), Jan 6, 1999: FRAME. CRACKED. FOUND AT D-2 LETTER CHECK, .5 INCH VISIBLE CRACK AT RT FRAME AFT ENTRYWAY APPROX 6 INCHES BELOW UPPER STOP. REPAIRED PER SRM 53-10-9. - [SDR DL72S990027](https://openairdocs.org/sdr/DL72S990027), Jan 6, 1999: FRAME. CRACKED. FOUND ON D2 LETTER CK, .75 INCH CRACK IN R-1 DOOR AFT LOWER FRAME. REPAIRED PER MM 52-12-0. - [SDR DL72S981592](https://openairdocs.org/sdr/DL72S981592), Aug 1, 1998: SKIN. CORRODED. CORROSION WAS FOUND IN THE SKIN AT THE STRINGER 26L LAP SPLICE. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED. THE SKI - [SDR DL72S981593](https://openairdocs.org/sdr/DL72S981593), Jul 31, 1998: SKIN. CORRODED. THE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE. THE CORRODED AREA WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REP - [SDR DL72S981200](https://openairdocs.org/sdr/DL72S981200), Jun 5, 1998: BRACKET. CRACKED. A .5 INCH CRACK NR 2 L/E FLAP ACT ATTACH BRACKET, LOWER FWD END. FOUND ON D1 LTR CHECK. INSTALLED DOUBLER PER M/M 57-20-21. - [SDR DL72S972210](https://openairdocs.org/sdr/DL72S972210), Oct 30, 1997: CASTING. CRACKED. NR 13 SPOILER ACT I/B AND O/B ATTACH CASTINGS ARE BROKEN. REPLACED PER M/M 57-42-0. - [SDR DL72S972041](https://openairdocs.org/sdr/DL72S972041), Oct 10, 1997: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE ROW 26 INOP. REPLACED LIGHT ASSY. - [SDR DL72S970818](https://openairdocs.org/sdr/DL72S970818), May 2, 1997: DOOR FRAME. CRACKED. A .75 IN CRACK L2 DOOR FRAME CUTOUT NEXT TO UPPER FWD STOP CASTING. INSTALLED REPAIR PER MM 53-10-0 PG 808. - [SDR DL72S970804](https://openairdocs.org/sdr/DL72S970804), Apr 29, 1997: BEAM. CRACKED. A CRACK WAS FOUND IN THE UPPER FWD TRANSVERSE BEAM ANGLE AND GUSSET AT FS 1273. THE DAMAGED PARTS ARE LOCATED IN THE TORQUE BOX WHICH IS THE SUBJECT OF THE AD 9 - [SDR DL72S970798](https://openairdocs.org/sdr/DL72S970798), Apr 24, 1997: SEAT TRACK. BROKEN. LT I/B SEAT TRACK BROKEN AT CORNER AROUND BOLT HOLE STA 344. REPAIRED PER SRM 53-10-5 FIG 7 SHEET 4. - [SDR DL72S970663](https://openairdocs.org/sdr/DL72S970663), Apr 14, 1997: LIGHTING. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROW 25 AND AFT. REPAIRED AFT SECTION OF INTERIOR EMERGENCY TRACK LIGHTING SYS. OPS NORMAL. - [SDR DL72S970642](https://openairdocs.org/sdr/DL72S970642), Apr 10, 1997: POWER SUPPLY. INOPERATIVE. EMERGENCY FLOOR LIGHTS OUT FROM ROW 27 TO REAR OF CABIN. REPLACED POWER SUPPLY, CHECKS NORMAL. - [SDR DL72S961432](https://openairdocs.org/sdr/DL72S961432), Jun 14, 1996: PROX SENSOR. MALFUNCTIONED. ON T/O WITH GEAR RETRACTED, HANDLE IN UP POSITION, GOT LT MAIN GEAR RED UNSAFE LIGHT. REPLACED LT MAIN GEAR UP PROX SENSOR. ALSO, AS A PRECAUTIONARY REPLACED LD - [SDR DL72S960283](https://openairdocs.org/sdr/DL72S960283), Feb 6, 1996: ANGLE. CRACKED. FOUND ON B1 LETTER CHECK, NR 7 SPOILER ATTACH CASTING CRACKED AT LOWER WING ATTACH. REPAIRED PER MM 57-20-22. - [SDR DL72S960282](https://openairdocs.org/sdr/DL72S960282), Feb 6, 1996: ANGLE. CRACKED. FOUND ON B-1 LETTER CHECK, TWO L/E SPAR STIFFENERS CRACKED .50 INCH, ONE AT NR 3 SLAT INBD TRACK, THE OTHER AT NR 2 SLAT OUTBD TRACK. REPLACED ANGLES PER MM 57- - [SDR DL72S960281](https://openairdocs.org/sdr/DL72S960281), Feb 6, 1996: STIFFENER. CRACKED. FOUND ON B1 LETTER CHECK, 2 INCH CRACK IN WING L/E SPAR STIFFENER AT NR 6 SLAT INBD TRACK. REPLACED STIFFENER PER MM 57-20-21. - [SDR DL72S954753](https://openairdocs.org/sdr/DL72S954753), Dec 8, 1995: SKIN. PUNCTURED. DURING A SHOP INSPECTION FOUND PUNCTURE DAMAGE TO RT ELEVATOR SKIN AT AT THE OUTBOARD END. REPAIR WAS INSTALLED PER SRM 55-20-3. - [SDR DL72S954636](https://openairdocs.org/sdr/DL72S954636), Dec 6, 1995: ELEVATOR. DAMAGED. DURING SHOP INSPECTION, RT ELEVATOR WAS RESTORED PER SRM 55-20-3. - [SDR DL72S954301](https://openairdocs.org/sdr/DL72S954301), Nov 8, 1995: BATTERY. DISCHARGED. CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CKS NORMAL. - [SDR DL72S954268](https://openairdocs.org/sdr/DL72S954268), Oct 29, 1995: SKIN. CORROSION. CORROSION AT AN EXISTING EXTERNAL REPAIR DOUBLER ON THE LOWER FUSELAGE SKIN PANEL, BETWEEN BS 259.5 AND BS312, AT STRINGER 20R. REMOVAL OF THE DOUBLER REVEALED - [SDR DL72S953148](https://openairdocs.org/sdr/DL72S953148), Jul 11, 1995: ANGLE. CRACKED. CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND THE AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER ERA 302109-14AD. - [SDR DL72S953018](https://openairdocs.org/sdr/DL72S953018), Jul 10, 1995: SKIN. CRACKED. FOUND DURING A-2 LETTER CHECK, NR 6 SLAT COVE SKIN ANGLE, UNDER TAI DUCT CRACKED. REPAIRED PER SRM 57-54-0. - [SDR DL72S953017](https://openairdocs.org/sdr/DL72S953017), Jul 10, 1995: SKIN. CRACKED. FOUND DURING A-2 LETTER CHECK, CRACK IN LWR COVE SKIN SUPPORT ANGLE, BELOW TAI DUCT ON NR 3 SLAT. REPAIRED PER SRM 57-54-0. - [SDR DL72S950216](https://openairdocs.org/sdr/DL72S950216), Jan 10, 1995: RIBS. CRACKED. DURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT WAS FOUND WITH INTERNAL SUPPORT RIBS NR 7 AND NR 9 CRACKED. REPAIRED PER SRM 57-54-0. - [SDR DL72S950190](https://openairdocs.org/sdr/DL72S950190), Jan 5, 1995: STIFFENERS. CRACKED. DURING INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS/BEAMS CRACKED AT BOTH FS 1263 AND FS 1273. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE W - [SDR DL72S950048](https://openairdocs.org/sdr/DL72S950048), Jan 4, 1995: SLAT RIB. CRACKED. DURING LETTER CHECK, FOUND LEFT WING NR 4 LEADING EDGE SLAT WITH A .5 INCH CRACK IN THE NOSE RIB JUST OUTBOARD OF ACTUATOR ROD ATTACH FITTING. REPAIRED PER MM 5 - [SDR DL72S950046](https://openairdocs.org/sdr/DL72S950046), Jan 4, 1995: SLAT. CRACKED. DURING LETTER CHECK, LEFT WING NR 4 LEADING EDGE SLAT WAS FOUND WITH TWO .5 INCH CRACKS ON THE LOWER SKIN IN THE RADIUS OF THE INBOARD SLAT TRACK FAIRING. REPAI - [SDR DL72S950045](https://openairdocs.org/sdr/DL72S950045), Jan 4, 1995: SKIN. CRACKED. DURING LETTER CHECK, THE NR 2 ENGINE S DUCT HOUSING RIGHT SIDE OUTER SKIN WAS FOUND WITH A 1.25 INCH CRACK EXTENDING UP FROM ACCESS PANEL 9524. REPAIRED PER MM - [SDR DL72S950044](https://openairdocs.org/sdr/DL72S950044), Jan 4, 1995: STIFFENER ANGLE. CRACKED. DURING LETTER CHECK, A 3 INCH CRACK WAS FOUND IN THE VERTICAL STIFFENER ANGLE ON THE WING FRONT SPAR ON THE OUTBOARD SIDE OF NR 3 SLAT OUTBOARD TRACK ROLLER FIT ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW78FA076](https://openairdocs.org/ntsb/FTW78FA076), Sep 7, 1978: Boeing B-727 (N484DA), Baton Rouge, LA, minor damage ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19970605017689I](https://openairdocs.org/incident/19970605017689I), Jun 5, 1997: Boeing 727232 (N484DA), Kansas City, MO. Narrative: item: aircraft returned to gate after aborted takeoff due to compressor stall. Details: during takeoff roll at about 80 knots with epr set at 1.6… - [Incident 19880407017219I](https://openairdocs.org/incident/19880407017219I), Apr 7, 1988: Boeing 727232 (N484DA), Covington - Cin, OH, Minor damage. Loud bang on takeoff. Nr 3 engine turbine had failed with parts spraying on runway. Takeoff aborted. No fire. ## Other aircraft with N484DA - [Cancelled 2022-12-31](https://openairdocs.org/deregistered/N484DA-2022-12-31): Cirrus Design SR20, S/N 1829, built 2007. Registration expired, pending cancellation. Owner: [Aerosim Academy Inc](https://openairdocs.org/faa-owner/AEROSIM%20ACADEMY%20INC), [Sanford, FL](https://openairdocs.org/faa-place/FL/Sanford) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.