# N482DA: Boeing 727-232, registration cancelled 2000-03-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 22, 2000
- Status when cancelled: Sale reported
- 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: 20862
- Type of aircraft: Fixed wing multi engine
- Last registry action: January 11, 2000
- Mode S code: A5F053
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Individual
- Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N482DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=482DA
- Page: https://openairdocs.org/deregistered/N482DA-2000-03-22

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.

ADs and bulletins for the Boeing 727-232: https://openairdocs.org/model/boeing-727-232.md

## Service difficulty reports (25)

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

- [SDR DL72S992195](https://openairdocs.org/sdr/DL72S992195), Oct 3, 1999: BATTERY. DISCHARGED. LEFT AFT EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS NOW OK .
- [SDR DL72S990883](https://openairdocs.org/sdr/DL72S990883), Apr 20, 1999: FRAME. CRACKED. FUSELAGE FRAME C1 DOOR CUTOUT AFT FRAME WEB, CRACK REPAIR. THE AFT FRAME OF THE C1 DOOR CUTOUT WAS FOUND WITH A 1.5 CRACK IN THE FRAME WEB JUST INBD OF THE DOOR
- [SDR DL72S990865](https://openairdocs.org/sdr/DL72S990865), Apr 20, 1999: ANGLE. CRACKED. FOUND ON E-1 LETTER CK, NR 3 SPOILER O/B ACTUATOR ATTACH CASTING CRACKED. REPAIRED PER MM 57-42-0.
- [SDR DL72S990864](https://openairdocs.org/sdr/DL72S990864), Apr 20, 1999: FRAME. CRACKED. FOUND AT E-1 LETTER CK, RT AFT ENTRY DOOR FRAME HAS VISABLE CRACK AT UPPER CUT OUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990593](https://openairdocs.org/sdr/DL72S990593), Mar 17, 1999: FRAME. CRACKED. DURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-61904-12AD, A CRACK WAS NOTED IN THE 2ND FAST HOLE ABOVE THE FLOORLINE. ALSO, THE 4TH FASTENER HOLE ABOVE THE FLOO
- [SDR DL72S990559](https://openairdocs.org/sdr/DL72S990559), Mar 17, 1999: SKIN. CRACKED. PERFORMING INSPECTIONS PER SI 4-74176-12AD, 12 CRACK INDICATIONS WERE FOUND BETWEEN BS 380 TO 460 IN THE SKIN LAP JOINT AT S4L. REPAIRED PER ERA 332914-14AD.
- [SDR DL72S990558](https://openairdocs.org/sdr/DL72S990558), Mar 17, 1999: SKIN. CRACKED. PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP JOINT BETWEEN BS 560 TO 580. THE CRACK INDICATION WAS LOCATED AT FASTENE
- [SDR DL72S990557](https://openairdocs.org/sdr/DL72S990557), Mar 17, 1999: SKIN. CRACKED. PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATIONS WAS NOTED IN THE S4R LAP JOINT BETWEEN BS 620 AND 640. THE INDICATION WAS LOCATED IN FASTENER RO
- [SDR DL72S990553](https://openairdocs.org/sdr/DL72S990553), Mar 16, 1999: KEEL BEAM. CRACKED. KEEL BEAM LT LWR CHORD WAS FOUND CRACKED IN THE UPPER FLANGE TYPICAL OF THAT DESCRIBED BY SB 727-53-0208, REV 1. REPAIRED PER ERA 332906-14.
- [SDR DL72S982355](https://openairdocs.org/sdr/DL72S982355), Nov 14, 1998: BATTERY PACK. DISCHARGED. AFT SERVIVCE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY RACK.
- [SDR DL72S982354](https://openairdocs.org/sdr/DL72S982354), Nov 14, 1998: BATTERY. DISCHARGED. AFT GALLEY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY.
- [SDR DL72S981881](https://openairdocs.org/sdr/DL72S981881), Sep 10, 1998: FRAME. CRACKED. REF SHIP NR 482, TPA, LETTER CHK D2, CRACK AT STA 910 FRAME FWD OUTBOARD RADIUS. REPAIRED PER MM 53-11-0.
- [SDR DL72S981880](https://openairdocs.org/sdr/DL72S981880), Sep 10, 1998: RIB. CRACKED. LT ELEV HINGE SUPPORT RIB CRACKED, ELEV STA 99.79 AFT I/B END. REPAIRED PER MM 55-10-31 FIG 802.
- [SDR DL72S981277](https://openairdocs.org/sdr/DL72S981277), Jun 14, 1998: SPAR WEB. CRACKED. WING CENTER SECTION REAR SPAR WEB, RBL 3 AND LBL 10 : REPAIR FOR WEB CRACK. THE WING CENTER SECTION REAR SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER C
- [SDR DL72S971360](https://openairdocs.org/sdr/DL72S971360), Jul 11, 1997: DOWNLOCK SENSOR. MALFUNCTIONED. AFTER GEAR RETRACTION RIGHT MAIN GEAR INDICIATION WAS BOTH THE RED AND GREEN RIGHT GEAR INDICATORS ILLUMINATED WITH GEAR HANLDE UP. WITH HANDLE DOWN ALL GEAR IN
- [SDR DL72S962622](https://openairdocs.org/sdr/DL72S962622), Dec 2, 1996: STIFFENER. CRACKED. FOUND ON C1 LETTER CK, 2 INCH CRACK IN WING FWD SPAR STIFFNER AT THE NR 7 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.
- [SDR DL72S961164](https://openairdocs.org/sdr/DL72S961164), May 15, 1996: DOOR. CRACKED. A .25 INCH VISIBLE CRACK UPPER FWD END OF RT AFT SERVICE DOOR. REPAIRED PER SRM 52-40-2 FIG 4, INSTALLED DOOR ON AIRCRAFT AND LEAK OPS CHECK OK.
- [SDR DL72S961609](https://openairdocs.org/sdr/DL72S961609), Oct 17, 1995: TRANSVERSE BEAM. CRACKED. THERE IS A CRACK IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTIO
- [SDR DL72S954039](https://openairdocs.org/sdr/DL72S954039), Oct 16, 1995: SKIN. CRACKED. FOUND ON B1 LETTER CK, RT ELEVATOR LWR SKIN CRACKED TWO PLACES, ONE INCH EACH, 12 INCHES FWD OF TAB OUTBD END. REPAIRED PER SRM 55-20-3 FIG 4.
- [SDR DL72S953255](https://openairdocs.org/sdr/DL72S953255), Jul 31, 1995: WINDOW. SHATTERED. DURING CRUISE, RIGHT FORWARD OVERING EXIT DOOR WINDOW OUTER PANE SHATTERED AND DEPARTED AIRCRAFT, LANDED DEN. WINDOW WAS REPLACED. REMAINS OF SHATTERED WINDOW R
- [SDR DL72S953175](https://openairdocs.org/sdr/DL72S953175), Jul 22, 1995: SEPARATOR ASSY. BURST. ON CLIMBOUT AT FL 2,500, HEARD LOUD BANG FOLLOWED BY VIBRATION AND RISING CABIN ALTITUDE, RETURNED ATL. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY BURST. REPLACED
- [SDR DL72S952462](https://openairdocs.org/sdr/DL72S952462), Jun 2, 1995: FUEL CONTROL. MALFUNCTIONED. DURING CRUISE, NR 3 ENGINE HAD FLUCTUATING FUEL FLOW AND N1, AND EPR. RETARDED THROTTLE, THEN ENGINE FLAMED-OUT. LANDED PHL WITHOUT INCIDENT. ENGINE WAS CHECKED
- [SDR DL72S951312](https://openairdocs.org/sdr/DL72S951312), Mar 28, 1995: RIB. CRACKED. THE NR 4 L/E SLAT RIB CRACKED .5 INCHES O/B SIDE. FOUND DURING A-2 LTR CHECK. REPAIRED PER MM 57-54-0 PG 803.
- [SDR DL72S951311](https://openairdocs.org/sdr/DL72S951311), Mar 28, 1995: SKIN. CRACKED. A FIVE INCH CRACK AT LOWER SKIN OF LT ELEV SKIN O/B SIDE. FOUND DURING A-2 LTR CK, TPAMM 3/28/95. REPAIRED PER SRM 55-20-3 FIG 5.
- [SDR DL72S951310](https://openairdocs.org/sdr/DL72S951310), Mar 28, 1995: SKIN. CRACKED. FOUND DURING E-2 LETTER CHECK, BOLT SHEARED AND UPPER SKIN WEDGE CRACKD 1 INCH NR 6 SLAT I/B GUIDE HOOK. REPAIRED PER SRM 57-50-3 FIG 10.

## 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 ATL87IA179](https://openairdocs.org/ntsb/ATL87IA179), Jun 19, 1987: Boeing 727-232 (N482DA), Nashville, TN, incident, no damage

## FAA accident and incident reports (3)

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 19900423041179I](https://openairdocs.org/incident/19900423041179I), Apr 23, 1990: Boeing 727232 (N482DA), Covington - Cin, OH. A system hydraulic failure on climb. Returned. Found right gear door sequence valve cracked.
- [Incident 19800709060249I](https://openairdocs.org/incident/19800709060249I), Jul 9, 1980: Boeing 727232 (N482DA), Detroit, MI, Minor damage. 2 Tires blownout on landing,fuse plugs may have melted as result of previous rejected takeoff.
- [Incident 19790419024299I](https://openairdocs.org/incident/19790419024299I), Apr 19, 1979: Boeing 727232 (N482DA), Portland, ME. Zk leading edge slat indicated unsafe for landing, pilot had no control problem.

## Other aircraft with N482DA

- [Cancelled 2019-12-16](https://openairdocs.org/deregistered/N482DA-2019-12-16): Cirrus Design SR20, S/N 1824, built 2007. Sale reported, canceled. Owner: [Crystal, MN](https://openairdocs.org/faa-place/MN/Crystal)

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