# N519DA: 1978 Boeing 727-232, registration cancelled 2013-04-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 1, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21470
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 1978
- Certificate issued: August 26, 2004
- Last registry action: January 2, 2008
- Mode S code: A6832A
- Owner when cancelled: [Aventura Aviation LLC](https://openairdocs.org/faa-owner/AVENTURA%20AVIATION%20LLC)
- Location: [Aventura, FL](https://openairdocs.org/faa-place/FL/Aventura)
- Owner type: Corporation
- Owner's area on the map: 25.9660° N, 80.1399° W: Placed by OpenAirDocs at the center of ZIP code 33180, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N519DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=519DA
- Page: https://openairdocs.org/deregistered/N519DA-2013-04-01

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 (70, newest 50)

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

- [SDR DL72S021251](https://openairdocs.org/sdr/DL72S021251), Oct 27, 2002: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT ROW 16 INOP AND LENS MISSING. RELAMPED AND REPLACED LENS-OPS NORMAL.
- [SDR DL72S021072](https://openairdocs.org/sdr/DL72S021072), Sep 12, 2002: BATTERY PACK. DISCHARGED. AFT EMERGENCY EXIT IDENTIFIER INOP. REPLACED BATTERY PACK.
- [SDR DL72S020917](https://openairdocs.org/sdr/DL72S020917), Aug 6, 2002: VALVE. WORN. AIR RETURN TO CVG FOR HIGH OIL TEMP NUMBER 1 ENG. REPLACED FUEL HEAT VALVE, OP CHECKS NORMAL.
- [SDR DL72S020464](https://openairdocs.org/sdr/DL72S020464), Apr 21, 2002: CHARGER. INOPERATIVE. FOUND AFT OVERHEAD EMERGENCY LIGHT INOP FWD OF AIRSTAIR DOOR. REMOVED AND REPLACED BATTERY PACK CHARGING RACK. CHECKS GOOD.
- [SDR DL72S020258](https://openairdocs.org/sdr/DL72S020258), Mar 5, 2002: BATTERY PACK. DISCHARGED. FORWARD AISLE EMERGENCY SIGN INOPERATIVE. REPLACED BATTERY PACK AND RACK ASSEMBLY PER MM, OPS GOOD.
- [SDR DL72S020202](https://openairdocs.org/sdr/DL72S020202), Feb 16, 2002: STIFFENER. CRACKED. INSPECTION OF THE WL 283 FASTENER HOLES ON THE RBL & LBL 17.8 BEAMS OF THE FS 1183 BULKHEAD REVEALED TOOLING DAMAGE IN THE TWO RT HOLES AND A CRACK INDICATION I
- [SDR DL72S020164](https://openairdocs.org/sdr/DL72S020164), Feb 9, 2002: BATTERY PACK. DISCHARGED. ON LAYOVER FOUND EMERGENCY LIGHT IN AFT STAIRWAY INOP. REPLACED BATTERY PACK.
- [SDR DL72S020163](https://openairdocs.org/sdr/DL72S020163), Feb 9, 2002: BATTERY PACK. DISCHARGED. ON LAYOVER FOUND EXTERIOR LIGHT FLASHING LEFT AFT FUSELAGE EMERGENCY LIGHT. REPLACED BATTERY PACK.
- [SDR DL72S020133](https://openairdocs.org/sdr/DL72S020133), Feb 2, 2002: APU. MALFUNCTIONED. ON APU SHUTDOWN FOUND APU EXHAUST FIRE OVER RIGHT WING COULD NOT PUT OUT HAD TO CALL FIRE DEPT TO PUT OUT FIRE. ALSO, FIRE BLISTERED WING TO FUSELAGE PANEL ABOV
- [SDR DL72S020097](https://openairdocs.org/sdr/DL72S020097), Jan 26, 2002: BATTERY PACK. DISCHARGED. FIRST CLASS EXIT LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S010821](https://openairdocs.org/sdr/DL72S010821), May 22, 2001: DOOR. MISSING. PANEL NR 3 ENGINE OIL SERVICE DOOR MISSING. REPLACED NR 3 OIL SERVICE DOOR.
- [SDR DL72S010738](https://openairdocs.org/sdr/DL72S010738), May 9, 2001: ATTACH ANGLE. CRACKED. A 1 INCH CRACK COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIR PER M/M 57-54-000-8.
- [SDR DL72S010737](https://openairdocs.org/sdr/DL72S010737), May 9, 2001: STIFFENER. CRACKED. A 2 INCH CRACK WING L/E SPAR STIFFENER I/B TRACK NR 2 SLAT I/B STIFFENER. REPLACED ANGLE PER M/M 57-200021-8.
- [SDR DL72S001626](https://openairdocs.org/sdr/DL72S001626), Aug 21, 2000: ACTUATOR. FAILED. WITH GEAR HANDLE DOWN AND MAIN GEAR LOCKED DOWN (GREEN LIGHTS) - EXCESSIVE TIME DELAY BEFORE NOSE GEAR SHOWED LOCKED DOWN AND GREEN LIGHT. NOTE: RED DOOR LIGHT 
- [SDR DL72S001568](https://openairdocs.org/sdr/DL72S001568), Aug 3, 2000: STRAP. CORRODED. THE BEAR STRAP AT THE C-3 DOORWAY WAS FOUND CORRODED ON THE INTERIOR SURFACE AT THE LOWER FWD CORNER OF THE DOORWAY CUTOUT. ER/A 334752-14AD REV A.
- [SDR DL72S001514](https://openairdocs.org/sdr/DL72S001514), Aug 3, 2000: STRAP. TOOL DAMAGE. TOOLING DAMAGE FOUND ON THE STA 784 LT FRAME REINFORCING STRAP. THE DAMAGE IS AT THE FOURTH FASTENER HOLE ABOVE THE FLOOR LINE. NO DAMAGE TO THE FRAME ITSELF. E
- [SDR DL72S001513](https://openairdocs.org/sdr/DL72S001513), Aug 3, 2000: FRAME. TOOL DAMAGE. TOOLING DAMAGE IN THE LT AND RT OVERWING EXIT FRAMES AT FS 761, DAMAGE FOUND IN BOTH THE I/B AND O/B CHORDS. THE LT FRAME DAMAGE AT THE 4TH FASTENER ABOVE THE F
- [SDR DL72S001512](https://openairdocs.org/sdr/DL72S001512), Aug 3, 2000: BEAM. MISINSTALLED. LBL AND RBL 17.8 VERTICAL BEAMS OF THE STA 1183 BULKHEAD HAVE SEVERAL FASTENERS INSTALLED FLUSH IN LIEU OF THE DRAWING REQUIRED BUTTON HEAD. ER/A 334720-14AD.
- [SDR DL72S001511](https://openairdocs.org/sdr/DL72S001511), Aug 2, 2000: FRAME. CRACKED. STA 1142.7 RT FRAME CRACKED/CORRODED JUST ABOVE C3 DOOR LOWER SILL. ER/A 334693-14AD REV A.
- [SDR DL72S001374](https://openairdocs.org/sdr/DL72S001374), Jul 20, 2000: FLAP TRACK. CORRODED. NUMBER 1 FLAP TRACK LT WING WAS CORRODED IN THE BARREL NUT HOLE. TRACK CLEANED UP AND REPAIRED PER MM 57-52-0.
- [SDR DL72S001372](https://openairdocs.org/sdr/DL72S001372), Jul 20, 2000: FLAP TRACK. CORRODED. NUMBER 2 FLAP TRACK LT WING WAS CORRODED IN THE BARREL NUT HOLE. TRACK CLEANED UP AND REPAIRED PER MM 57-52-0.
- [SDR DL72S001366](https://openairdocs.org/sdr/DL72S001366), Jul 20, 2000: CHANNEL. WORN. FIREWALL CHANNEL WORN AT 5:30 POSITION FS 1343 AT MATING SURFACE FOR NR 2 ENG COWLING. REPAIRED PER 53-11-0.
- [SDR DL72S001478](https://openairdocs.org/sdr/DL72S001478), Jul 12, 2000: FLAP TRACK. CORRODED. NR 3 FLAP TRACK CORRODED NR 116. REPAIRED PER M/M.
- [SDR DL72S001476](https://openairdocs.org/sdr/DL72S001476), Jul 12, 2000: FLAP TRACK. CORRODED. NR 2 FLAP TRACK CORRODED CARD NR 115. REPAIRED PER M/M.
- [SDR DL72S000881](https://openairdocs.org/sdr/DL72S000881), May 4, 2000: SWITCH. FAILED. INFLIGHT SHUTDOWN DUE TO NR 2 ENG FILTER BYPASS LIGHT ON. REMOVED AND INSPECTED MAIN OIL FILTER. NO CONTAMINENTS FOUND. CHIP DET CHECKS CLEAN. REPLACED FILTER B
- [SDR DL72S000676](https://openairdocs.org/sdr/DL72S000676), Apr 8, 2000: PCU. MALFUNCTIONED. RUDDER LOAD LIMITER FOLLOWING MEL PROCEDURES WHEN REENGAGED SYSTEM A RUDDER BEFORE FLAP EXTENSION RECEIVED UNCOMMANDED LOWER RUDDER YAW 1 INDICE RT SYS A RUDDER
- [SDR DL72S000797](https://openairdocs.org/sdr/DL72S000797), Mar 20, 2000: SKIN. CRACKED. NR 5 SLAT LOWER SKIN WORN O/B OF O/B ALIGNMENT SPADE. CUT INNER SKIN MADE NEW SKIN DOUBLERS. REPAIRED PER MM 57-54-0 FIG 801.
- [SDR DL72S000551](https://openairdocs.org/sdr/DL72S000551), Mar 20, 2000: SKIN. CRACKED. A .5 INCH CRACK ON NR 2 MIDFLAP LOWER COVE SKIN AT THE I/B ROD CUTOUT.
- [SDR DL72S000305](https://openairdocs.org/sdr/DL72S000305), Feb 13, 2000: BATTERY. DISCHARGED. R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK.
- [SDR DL72S992514](https://openairdocs.org/sdr/DL72S992514), Nov 14, 1999: BATTERY PACK. DISCHARGED. FOUND ON LAYOVER AFT EMERGENCY CEILING LIGHT STROBING. REPLACED BATTERY CHARGER AND BATTERY.
- [SDR DL72S991594](https://openairdocs.org/sdr/DL72S991594), Jul 15, 1999: BRAKE. FAILED. AFTER TAXI TO RUNWAY, A/C REQUIRED APPROX 1.4 EPR TO INITIATE TAXI. WHEN A/C MOVED A VERY LOUD SHUDDER WAS FELT ON LT SIDE OF A/C. MAINT TOW BACK TO GATE. REPLA
- [SDR DL72S991512](https://openairdocs.org/sdr/DL72S991512), Jul 4, 1999: BULB. FAILED. ON L/O 2 CK, FOUND NO SMOKING LIGHTS INOP AT 4CD, 14DEF, 19DEF, 23DEF. ALSO, FOUND FASTEN SEAT BELT LIGHTS AT 4CD, 2AB, 20DEF INOP. RELAMPED, ALL CHECK GOOD.
- [SDR DL72S990595](https://openairdocs.org/sdr/DL72S990595), Mar 19, 1999: POWER SUPPLY. INOPERATIVE. ON S/C FOUND E PATH LIGHTING AT SECTION 20 TO 26 INOP. FOUND BAD FUSE ON AFT PWR SUPPLY. REPLACED AFT PWR SUPPLY, OPS NORMAL NOW.
- [SDR DL72S990294](https://openairdocs.org/sdr/DL72S990294), Feb 14, 1999: LIGHT. INOP. LEFT AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED RACK, NOW CKS NORMAL.
- [SDR DL72S990293](https://openairdocs.org/sdr/DL72S990293), Feb 14, 1999: BATTERY PACK. DISCHARGED. MID CABIN SEAT EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK AND BATTERY PACK, ALL OPS NORMAL.
- [SDR DL72S990273](https://openairdocs.org/sdr/DL72S990273), Feb 9, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 360-481, STRG 4L, SKIN LAP SPLICE, REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE STRINGER 4L 
- [SDR DL72S990272](https://openairdocs.org/sdr/DL72S990272), Feb 9, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 360-481, STRG 4R, SKIN LAP SPLICE REPAIR FOR CRACKED FASTENER HOLES. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360-481 REVE
- [SDR DL72S990258](https://openairdocs.org/sdr/DL72S990258), Feb 6, 1999: SKIN. CRACKED. FUSELAGE SKIN, FS 528, STRG 4, REPAIR FOR SKIN CRACK. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE GAVE A CRACK INDICATION. HFEC INTERNAL INSPECTION WAS T
- [SDR DL72S990065](https://openairdocs.org/sdr/DL72S990065), Jan 11, 1999: SKIN. CRACKED. 4.5 INCH CRACK IN NR 8 SLAT COVE SKIN ANGLE AT O/B UPSTOP PAD. REPAIR PER MM 57-54-0 PG 816.
- [SDR DL72S982341](https://openairdocs.org/sdr/DL72S982341), Nov 12, 1998: STOP. LOOSE. DURING INSPECTION PER REQUIREMENTS OF AD 94-07-08, LOOSE SLAT STOP ATTACH BOLTS WERE FOUND LOOSE FOR THE NR 6, 7 & 8 SLATS. EACH OF THESE SLAT LOCATIONS WERE MO
- [SDR DL72S981278](https://openairdocs.org/sdr/DL72S981278), Jun 14, 1998: SPAR WEB. CRACKED. WING CENTER SECTION REAR SPAR, WEB RBL 3 AND RBL 9 : REPAIR FOR WEB CRACKS. THE WING CENTER SECTION SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER SPAR C
- [SDR DL72S981175](https://openairdocs.org/sdr/DL72S981175), Jun 2, 1998: SKIN. CRACKED. FOUND AT B2 LETTER CHECK, 2 CRACKS .75 INCH AND 2 INCH AT NR 4 L/E FLAP O/B HINGE CUTOUT. REPAIRED PER ERA 364950-14 AND M/M 57-53-0.
- [SDR DL72S972133](https://openairdocs.org/sdr/DL72S972133), Oct 22, 1997: SKIN. HOLE. HOLE IN LT L/E SKIN, 34 INCH FROM BOTTOM. INSTALLED REPAIR DOUBLER PER SRM 55-40-3 FIG. 1.
- [SDR DL72S972132](https://openairdocs.org/sdr/DL72S972132), Oct 22, 1997: SKIN. HOLE. HOLE IN LEFT L/E SKIN ON LOWER RUDDER. REPAIRED PER SRM 55-40-3.
- [SDR DL72S972131](https://openairdocs.org/sdr/DL72S972131), Oct 22, 1997: SKIN. GOUGED. SKIN GOUGED AT LOWER END OF LOWER RUDDER. INSTALLED DOUBLER PER SRM 55-40-3, FIG 1.
- [SDR DL72S972245](https://openairdocs.org/sdr/DL72S972245), Oct 21, 1997: ANGLE. CRACKED. THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION AT HMV VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY STOP DRILLING CRACK AND INSTALLING
- [SDR DL72S972186](https://openairdocs.org/sdr/DL72S972186), Oct 14, 1997: STRINGER. CRACKED. STRINGER TO RIB CRACK LEFT WING STA 686.5 AT STR 12. REPAIRED PER M/M57-13-0 FIG 804.
- [SDR DL72S972056](https://openairdocs.org/sdr/DL72S972056), Oct 13, 1997: STRINGER. CRACKED. HFEC INSPECTION PER OPN NO 8602 AS SHOWS CRACK ON STRINGER TO RIB AT STA 686.5 5-10. PERFORMED DYE CHECK TO IDENTIFY CRACK. NO STOP DRILL HOLE REQUIRED. DISCONN
- [SDR DL72S972119](https://openairdocs.org/sdr/DL72S972119), Oct 10, 1997: BRACKET. CRACKED. THE NR 2 L/E FLAP ACTUATOR SUPPORT BRACKETS I/B AND O/B ARE CRACKED. REMOVED SUPPORT BRACKETS AND BEGAN REPAIRS PER M/M 57-20-21 FIG 807, FINISHED REPAIR PER MM
- [SDR DL72S972078](https://openairdocs.org/sdr/DL72S972078), Oct 9, 1997: ANGLE. CRACKED. AFT LOWER CHORD ANGLE IS CRACKED AT I/B AFT FLAP TRACK CUTOUT I/B AND O/B CORNERS. INSTALLED DOUBLER PER M/M 57-52-0 FIG 802.

All 70: https://openairdocs.org/deregistered/N519DA-2013-04-01/reports.md

## 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 MIA86MA048](https://openairdocs.org/ntsb/MIA86MA048), Dec 28, 1985: Boeing 727-232 (N519DA), Fort Lauderdale, FL, incident, 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 19980119003059I](https://openairdocs.org/incident/19980119003059I), Jan 19, 1998: Boeing 727232 (N519DA), Salt Lake City, UT, Minor damage. Narrative: a southwest de-ice truck backed into the left wing tip of a delta B-727 which was inbound to the gate. Minor damage to the light cover only (approx.…
- [Incident 19851228071879I](https://openairdocs.org/incident/19851228071879I), Dec 28, 1985: Boeing 727232 (N519DA), Ft Lauderdale, FL, Minor damage. Engine failed at rotation blowing all 4 front and rear cowl doors onto runway. Crack in combustion chamber case.

## Other aircraft with N519DA

- [Registered now](https://openairdocs.org/aircraft/N519DA): Diamond Aircraft Ind DA 62, S/N 62.C098, built 2025

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