# N476DA: Boeing 727-232, registration cancelled 1999-11-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 23, 1999 - 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: 20753 - Type of aircraft: Fixed wing multi engine - Last registry action: November 23, 1999 - Mode S code: A5D7B0 - 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/N476DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=476DA - Page: https://openairdocs.org/deregistered/N476DA-1999-11-23 From the FAA registry file of October 31, 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 (49) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL72S991291](https://openairdocs.org/sdr/DL72S991291), Jun 5, 1999: TRACK. CORRODED. AN I/B FLAP TRACK WAS FOUND WITH CORROSION IN TWO BOLT HOLES WHICH ARE THE SUBJECT OF AD 90-07-05. THE CORROSION WAS CLEANED UP BY OVERSIZING THE HOLES WITHIN T - [SDR DL72S991083](https://openairdocs.org/sdr/DL72S991083), May 16, 1999: BATTERY. DISCHARGED. AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. - [SDR DL72S990137](https://openairdocs.org/sdr/DL72S990137), Jan 21, 1999: FRAME. CRACKED. FOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT FRAME OF R-1 DOOR AT FWD SIDE OF LWR STOP CASTING. REPAIRED PER MM 52-12-0. - [SDR DL72S990136](https://openairdocs.org/sdr/DL72S990136), Jan 21, 1999: FRAME. CRACKED. FOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9. - [SDR DL72S982136](https://openairdocs.org/sdr/DL72S982136), Oct 13, 1998: SKIN. DAMAGED. THE FUSELAGE SKIN AT STRINGER 22L BETWEEN FS 1110 AND 1166 WAS TORN AND GOUGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGE WAS REMOVED FROM THE SKIN WITH T - [SDR DL72S981306](https://openairdocs.org/sdr/DL72S981306), Jun 19, 1998: SKIN. CRACKED. LT ELEVATOR CRACKED ADJACENT PREVIOUS REPAIR LOWER SIDE AFT OF NR 3 BALANCE BOARD PANEL SRM 55-20-3. - [SDR DL72S980135](https://openairdocs.org/sdr/DL72S980135), Jan 17, 1998: BATTERY PACK. DISCHARGED. AFT LT EXT EMERG LIGHT INOP. REPLACED BATTERY PACK M955, CHKS GOOD. - [SDR DL72S972643](https://openairdocs.org/sdr/DL72S972643), Dec 12, 1997: DOUBLER. CRACKED. FUSELAGE, FWD GALLEY DOOR SURROUND DOUBLER, UPPER HINGE: REPAIR FOR CRACK AT HINGE CUTOUT. THE FWD GALLEY DOOR SURROUND DOUBLER WAS FOUND WITH A 1.8 CRACK AT TH - [SDR DL72S972360](https://openairdocs.org/sdr/DL72S972360), Nov 13, 1997: FRAME. CRACKED. A 1.5 INCH CRACK IN UPPER AFT RADIUS OF R-1 DOOR AFT FRAME. REPAIRED PER ERA 363204-14 AND M/M 52-12-0. - [SDR DL72S972358](https://openairdocs.org/sdr/DL72S972358), Nov 13, 1997: BRACKET. CRACKED. FOUND DURING F-1 LETTER CHECK, 2 INCH CRACK NR 8 SPOILER ACTUATOR MOUNT CASTING LWR ATTACH BRACKET. REPAIRED PER M/M 57-20-22. - [SDR DL72S972099](https://openairdocs.org/sdr/DL72S972099), Oct 19, 1997: FITTING. WORN. RT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807, IPC REF 65-26763-10 ITEM 350. - [SDR DL72S972098](https://openairdocs.org/sdr/DL72S972098), Oct 19, 1997: FITTING. WORN. LT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807 IPC LOC 32-10-00-10 ITEM 345. - [SDR DL72S971716](https://openairdocs.org/sdr/DL72S971716), Aug 29, 1997: LIGHT. INOPERATIVE. AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOP. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSY AND BATTERY. - [SDR DL72S971395](https://openairdocs.org/sdr/DL72S971395), Jul 3, 1997: STOP PAD. CRACKED. DOUBLER CRACKED AT LWR COVER SKIN ANGLE AT NR 7 SLAT I/B STOP PAD. REPAIRED PER DELTA ER/A 362251-14. - [SDR DL72S971394](https://openairdocs.org/sdr/DL72S971394), Jul 3, 1997: VERT WEB. CRACKED. VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 EA CRACKS ONE AT LWR RT CORNER AND ONE AT LWR LT CORNER. INSTALLED REPAIR PER SRM 53-10-4. - [SDR DL72S971311](https://openairdocs.org/sdr/DL72S971311), Jul 3, 1997: SKIN. CRACKED. A .25 INCH VISIBLE CRACK AT NR 2 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0. - [SDR DL72S971310](https://openairdocs.org/sdr/DL72S971310), Jul 3, 1997: WEB. CRACKED. LT VERT TORQUE BOX WEB CRACKED AT LIGHTENING HOLE STA 1230. REPAIRED PER MM 53-11-0. - [SDR DL72S971374](https://openairdocs.org/sdr/DL72S971374), Jul 2, 1997: TORQUE BOX. CRACKED. TORQUE BOX CHORD CRACKED STA 1273R. CRACK HORIZ TORQUE BOX ANGLE STA 1273. REPAIRED PER SRM 53-10-10. - [SDR DL72S971354](https://openairdocs.org/sdr/DL72S971354), Jul 2, 1997: TORQUE BOX. CRACKED. A .75 INCH CRACK IN UPPER LT TORQUE BOX WEB STA 1215 CRACKED AT CHORD ATTACH POINT, MARKED. STOP DRILLED CRACKS, DRILLED REPAIR DOUBLER PER M/M 53-11-0, INSTALL - [SDR DL72S971280](https://openairdocs.org/sdr/DL72S971280), Jul 1, 1997: FLOORBEAM. CORRODED. CORROSION FOUND ON FLOORBEAM STA 344 AND RBL 2. INSTALLED REPAIR PER SRM 53-10-8 FIG 11. - [SDR DL72S970770](https://openairdocs.org/sdr/DL72S970770), Apr 25, 1997: SKIN. CRACKED. A 1 INCH CRACK ACROSS RIVET HOLE AT RT SIDE OF VERT STAB BELOW ACCESS PANEL APPROX 10 FT AFT OF L/E. REPAIRED PER SRM 54-30-0. - [SDR DL72S970769](https://openairdocs.org/sdr/DL72S970769), Apr 25, 1997: SKIN. CRACKED. FOUND 1 INCH CRACK FUSELAGE SKIN COMING FROM R-5 COCKPIT WINDOW CUTOUT UPPER AFT CORNER. REPAIRED PER SRM 53-30-3. - [SDR DL72S970768](https://openairdocs.org/sdr/DL72S970768), Apr 25, 1997: WEB. CRACKED. A .375 AND .3125 INCH CRACK RT TORQUE BOX VERT WEB LIGHTENING HOLE AT STA 1235. REPAIRED PER MM 53-11-0. - [SDR DL72S970767](https://openairdocs.org/sdr/DL72S970767), Apr 25, 1997: SKIN. CRACKED. FOUND 3 CRACKS EXTENDING FROM RIVET HOLE AT BASE OF VERTICAL STABILIZER LT SIDE APPROX 10 FT AFT OF L/E. REPAIR PER MM 54-30-0. - [SDR DL72S970243](https://openairdocs.org/sdr/DL72S970243), Feb 7, 1997: AIR DISTRIBUTION. SMOKE. IN CRUISE, FLT ATT REPORTED SMOKE IN MID CABIN AREA WITH ELECTRICAL SMELL. UNABLE TO DUPLICATE PROBLEM OR FIND ANY DESCREPENCIES THAT MAY HAVE CAUSED PROBLEM. - [SDR DL72S962213](https://openairdocs.org/sdr/DL72S962213), Oct 2, 1996: LIGHT. INOPERATIVE. ESCAPE PATH LIGHTING LENS CRACKED AND LIGHT INOP. REPLACED LENS AND LIGHT, OPS CHECK NORMAL. - [SDR DL72S961755](https://openairdocs.org/sdr/DL72S961755), Jul 22, 1996: LIGHT. INOPERATIVE. LT AFT SERVICE DOOR OVERHEAD EMERGNECY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES, CHECKS NORMAL. - [SDR DL72S960998](https://openairdocs.org/sdr/DL72S960998), Apr 25, 1996: WHEEL BEARING. FAILED. ON TAXI IN TO GATE, NR 1 MAIN WHEEL ASSY LOCKED UP. FOUND NR 1 WHEEL ASSY DAMAGED. INBOARD WHEEL BEARING DESTROYED, AXLE CRACKED AND BROKEN AT INBOARD BEARING R - [SDR DL72S960461](https://openairdocs.org/sdr/DL72S960461), Feb 28, 1996: SKIN. CRACKED. THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A .25 INCH CRACK IN THE UPPER FORWARD CORNER OF THE L-1 DOOR CUTOUT. A TIME LIMITED REPAIR HAS BEEN I - [SDR DL72S961607](https://openairdocs.org/sdr/DL72S961607), Feb 27, 1996: WEB. CRACKED. THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 2.5 INCH CRACK BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE WEB AT THIS LOCATION IS 0.040 CLAD 2024 - [SDR DL72S960437](https://openairdocs.org/sdr/DL72S960437), Feb 26, 1996: WEB. CRACKED. TWO LIGHTENING HOLES IN RT VERT WEB OF AFT AIR STAIR TORQUE BOX WERE FOUND WITH CRACKS ROUTED PAST LIMITS. FOUND AT D-2 LTR CHECK AND REPAIRED PER MM 53-11-0. - [SDR DL72S954104](https://openairdocs.org/sdr/DL72S954104), Oct 25, 1995: BATTERY. DISCHARGED. L-2 PORTABLE EMERGENCY LIGHT INOP, REPLACED BATTERIES, OPERATION NORMAL. - [SDR DL72S953292](https://openairdocs.org/sdr/DL72S953292), Aug 5, 1995: LIGHT BALLAST. FAILED. AFTER STOPPING AT GATE AND DEPLANING, SMOKE STARTED COMING OUT OF OVERHEAD PANEL ABOVE 21A. PULLED ALL CABIN LIGHTING C/BS. FOUND CEILING LIGHT BALLAST BETWEEN - [SDR DL72S951523](https://openairdocs.org/sdr/DL72S951523), Apr 12, 1995: CLIP. CORROSION. FOUND DURING CV-2 CHECK, CORROSION FWD OF FORMER 950F WHERE IT ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 FIG 825. - [SDR DL72S951522](https://openairdocs.org/sdr/DL72S951522), Apr 12, 1995: CLIP. CORROSION. FOUND DURING CV-2 CHECK, CORROSION WHERE FORMER 970 ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 PG 825. - [SDR DL72S951521](https://openairdocs.org/sdr/DL72S951521), Apr 12, 1995: STRINGER. CORROSION. FOUND DURING CV-2 CHECK, CORROSION AROUND RIVETS IN STRINGER 25L BETWEEN STA 950D AND 950E. REPAIRED PER MM 53-11-0. - [SDR DL72S951578](https://openairdocs.org/sdr/DL72S951578), Apr 6, 1995: SIDEWALL. CRACKED. THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1 INCH CRACK BET STA 294.5 AND 285.5 APPROX AT WL 170. THE WEB AT THIS LOCATION IS 0.040 INCH THK 2024-T3 CLAD. - [SDR DL72S951449](https://openairdocs.org/sdr/DL72S951449), Apr 3, 1995: WEB. CRACKED. FOUND ON CV2 CHECK .25 INCH CRACK LIGHTNING HOLE TORQUE BOX SIDE WEBB STA 1263 LT SIDE. REPAIR: ROUTE OUT DAMAGED AREA PER M/M 53-11-0. - [SDR DL72S951444](https://openairdocs.org/sdr/DL72S951444), Apr 3, 1995: SKIN. CORRODED. FOUND ON CV2 CHECK, CORROSION ON SKIN BETWEEN STA 480 AND 500 AT BL 0. REPAIRED PER SRM 53-30-3 FIG 1. - [SDR DL72S951495](https://openairdocs.org/sdr/DL72S951495), Apr 2, 1995: STRINGER. CORRODED. FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STRINGER 25L FROM 950A TO 950B. REPAIRED PER SRM 53-10-3 AND PER PS 900-5-1. - [SDR DL72S951451](https://openairdocs.org/sdr/DL72S951451), Apr 2, 1995: CLIP. CRACKED. FOUND ON CV2 CHECK, ONE INCH CRACK IN SKIN CLIP BETWEEN STR 28L AND 29L FWD SIDE STA 990. REPAIR: REPAIRED PER M/M 53-11-0. - [SDR DL72S951445](https://openairdocs.org/sdr/DL72S951445), Apr 2, 1995: STRINGER. CORRODED. FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STR 27L STA 1030 TO STA 1050. REPAIRED PER ERA 301506-14 CODE 4-53-14. - [SDR DL72S951441](https://openairdocs.org/sdr/DL72S951441), Apr 1, 1995: SEAT TRACK. CORRODED. FOUND ON CV2 CHECK, CORROSION AT O/B GALLEY ATTACH TRACK LBL 56 BETWEEN STA 1070 AND STA 1115. REPLACED SEAT TRACK FROM STA 1070 TO STA 1110 PER SRM 53-10-5 FIG - [SDR DL72S951450](https://openairdocs.org/sdr/DL72S951450), Mar 31, 1995: ANGLE. CRACKED. FOUND ON CV2 CHECK, ONE INCH CRACK IN ATTACH ANGLE LOWER END OF NR 7 SPOILER ACTUATOR ATTACH FITTING. REPAIR: REPAIRED PER M/M 57-20-22 PAR 10. - [SDR DL72S951447](https://openairdocs.org/sdr/DL72S951447), Mar 31, 1995: SKIN. CRACKED. FOUND ON CV2 CHECK RT FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED .50 INCH. REPAIR: REPAIRED PER M/M 52-11-0 PG 808. - [SDR DL72S951446](https://openairdocs.org/sdr/DL72S951446), Mar 31, 1995: ANGLE. CRACKED. FOUND ON CV2 NR 8 SLAT ANGLE CRACKED UNDER TELESCOPING TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. - [SDR DL72S951443](https://openairdocs.org/sdr/DL72S951443), Mar 31, 1995: SEAT TRACK. CORRODED. FOUND ON CV2 CHECK, CORROSION ON RT INBD SEAT TRACK STA 380 TO 480. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7. - [SDR DL72S951442](https://openairdocs.org/sdr/DL72S951442), Mar 31, 1995: SEAT TRACK. CORRODED. FOUND ON CV2 CHECK, CORROSION ON RT CENTER SEAT TRACK STA 344 TO 480. CLEANED TREATED AND PAINTED FROM STA 460 TO 480 PER SRM 53-10-1, FROM STA 344 TO 460 REPLA - [SDR DL72S950371](https://openairdocs.org/sdr/DL72S950371), Jan 26, 1995: WEB. CORROSION. CORROSION WAS FOUND ON THE SKIN CLIP AND WEB JUST O/B OF THE LT NOSE CHORD AT STA 303.9. THE DAMAGE WAS REPAIRED PER MM 53-30-0 FIG 806. DAMAGE FOUND DURING SPE ## Other aircraft with N476DA - [Registered now](https://openairdocs.org/aircraft/N476DA): Cirrus Design SR20, S/N 1818, built 2007 --- 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.