# N419DA: 1977 Boeing 727-232, registration cancelled 2012-11-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 7, 2012 - Status when cancelled: Sale reported, canceled - Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082) - Engine: [Pratt & Whitney Canada JT15D-1 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-1-series) (registry code 52060) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 21272 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 25, 1977 - Last registry action: February 1, 2001 - Mode S code: A4F5DB - 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/N419DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=419DA - Page: https://openairdocs.org/deregistered/N419DA-2012-11-07 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 (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL72S001005](https://openairdocs.org/sdr/DL72S001005), May 22, 2000: FRAME. CRACKED. FOUND ON A1 LETTER CHECK, 1 INCH CRACK R-1 DOOR AFT FRAME AT LOWER STOP CASTING. REPAIRED PER MM 52-12-0. - [SDR DL72S000795](https://openairdocs.org/sdr/DL72S000795), Mar 7, 2000: RIB. CRACKED. NR 3 SLAT RIB NR 6 CRACKED. INSTALLED DOUBLER PER MM 57-54-00 PG 818. - [SDR DL72S992660](https://openairdocs.org/sdr/DL72S992660), Dec 6, 1999: BULB. FAILED. ON SVC CHECK, FOUND RT R1 EMERGENCY LIGHT INOP. REPLACED BULB, OPS CK GOOD. - [SDR DL72S992323](https://openairdocs.org/sdr/DL72S992323), Oct 21, 1999: STRINGER. CRACKED. STRINGER 18A CRACKED AT LWR AFT BOLT STA 940. REPAIRED PER MM 53-12-0 PG 816. - [SDR DL72S992322](https://openairdocs.org/sdr/DL72S992322), Oct 21, 1999: BRACKET. CRACKED. NR 1 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER M/M 57-20-21 PG 812. - [SDR DL72S992321](https://openairdocs.org/sdr/DL72S992321), Oct 21, 1999: SKIN. CRACKED. TWO .25 INCH CRACKS IN F/S 231 STR 21R. INSTALLED DOUBLER PER SRM 53-30-3 F 26. - [SDR DL72S992320](https://openairdocs.org/sdr/DL72S992320), Oct 21, 1999: WEB. CRACKED. TPA LTR CHECK F-2, LT TORQUE BOX VERT WEB CRACKED 1 AT STA 1235. REPAIRED PER MM 53-11-0. - [SDR DL72S992319](https://openairdocs.org/sdr/DL72S992319), Oct 21, 1999: SKIN. CRACKED. TPA LTR CHECK F-2, 1 CRACK IN VERT STAB SKIN LT SIDE AT LWR SIDE OF CUTOUT FOR ACCESS PANEL 9523. REPAIRED PER MM 54-30-0. - [SDR DL72S992317](https://openairdocs.org/sdr/DL72S992317), Oct 21, 1999: FRAME. CRACKED. FOUND AT F-2 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE BELOW A/C DATA PLATE. REPAIRED PER SRM 53-10-9. - [SDR DL72S991866](https://openairdocs.org/sdr/DL72S991866), Aug 20, 1999: PRBC. INOP. AUTO PACK TRIP ON TAKEOFF. POSSIBLE COMPRESS STALL. OCCURED AFTER BRAKES RELEASE. ABORTED TAKEOFF AT 60 KTS. REPLACED NR 3 ENGINE PRBC FOR OFF IDLE STALL. RAN E - [SDR DL72S990510](https://openairdocs.org/sdr/DL72S990510), Mar 10, 1999: ANGLE. CRACKED. REPAIR ANGLE CRACKED NR 7 SLAT STOP PAD I/B SIDE. REPAIRED PER MM 57-54-0 PG 816. - [SDR DL72S990509](https://openairdocs.org/sdr/DL72S990509), Mar 10, 1999: SKIN. CRACKED. A .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8. - [SDR DL72S990508](https://openairdocs.org/sdr/DL72S990508), Mar 10, 1999: BRACKET. CRACKED. FOUND ON F1 LETTER CK, CRACK IN NR 1 SLAT ACTUATOR SUPPORT BRACKET WEB I/B SIDE. REPAIRED PER MM 57-20-21. - [SDR DL72S990507](https://openairdocs.org/sdr/DL72S990507), Mar 10, 1999: STIFFENER. CRACKED. FOUND ON F1 LETTER CK, L/E SPAR STIFFENER CRACKED AT LOWER END NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21. - [SDR DL72S990505](https://openairdocs.org/sdr/DL72S990505), Mar 10, 1999: SKIN. CRACKED. A .5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT FWD SPAR AREA. REPAIRED PER SRM 55-20-3 FIG 4. - [SDR DL72S990501](https://openairdocs.org/sdr/DL72S990501), Mar 10, 1999: FRAME. CRACKED. FOUND ON F1 LETTER CK, AFT ENTRY DOOR FRAME CRACKED RT SIDE 10 INCHES BELOW THE TOP OF THE DOOR CUTOUT. REPAIRED PER SRM 53-10-9. - [SDR DL72S990313](https://openairdocs.org/sdr/DL72S990313), Feb 16, 1999: BATTERY PACK. DISCHARGED. OVERHEAD EXIT SIGN EMERGENCY LIGHT INOP ON TEST AT OVERWING EXITS. REPLACED M1094 RACK AND BATTERY PACK OP CKS OK. PARTS BORROWED FROM AMERICA WEST PACK LOCATED - [SDR DL72S990312](https://openairdocs.org/sdr/DL72S990312), Feb 16, 1999: BATTERY PACK. DISCHARGED. LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT MOST FWD INOP. REPLACED RACK AND BATTERY PACK, OP CKS OK. - [SDR DL72S982360](https://openairdocs.org/sdr/DL72S982360), Nov 14, 1998: LIGHT. INOP. L2 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY. - [SDR DL72S981594](https://openairdocs.org/sdr/DL72S981594), Jul 31, 1998: SKIN. DENTED. THE FUSELAGE SKIN WAS BADLY DENTED AT FS 295 BETWEEN STR 12L AND 13L DUE TO A BIRD STRIKE. THE DAMAGED AREA WAS CUTOUT AND REPAIRED PER THE B727 SRM 53-30-3, FI - [SDR DL72S980102](https://openairdocs.org/sdr/DL72S980102), Jan 14, 1998: WEB. CRACKED. DURING INSTALLATION OF PREVENTATIVE MOD ON THE LHS KEEL BEAM PER SB727-53-0208 (EO 4-64433-3), A CRACK WAS FOUND IN THE WEB JUST ABOVE THE VERT FLANGE OF THE KE - [SDR DL72S980101](https://openairdocs.org/sdr/DL72S980101), Jan 14, 1998: SKIN. CRACKED. DURING INSPECTION PER EO4-60829-3, A CRACK WAS FOUND IN THE SKIN AND DOUBLER IN THE TYP LOCATION AS WELL AS A CRACK IN THE STRAP, BUT ONE FASTENER ROW HIGHER TH - [SDR DL72S980063](https://openairdocs.org/sdr/DL72S980063), Jan 7, 1998: SKIN. CRACKED. NUMBER 4 L/E SLAT HAD A CRACK FROM THE FENCE MOUNTING BOLT HOLE. INSTALLED A REPAIR DOUBLER PER M/M 57-54-0. - [SDR DL72S971808](https://openairdocs.org/sdr/DL72S971808), Sep 16, 1997: LIGHT. DAMAGED. EMERGENCY TRACK LIGHTING STRIP AT 22DEF, TRACK COVER AND WIRING DAMAGED. REPLACED APPROX 30 INCHES OF LIGHT TRACK INVOLVING 4 RED LIGHTS. REPLACING 1 BULB HOLDE - [SDR DL72S970245](https://openairdocs.org/sdr/DL72S970245), Feb 8, 1997: BATTERY PACK. DISCHARGED. RT CARGO DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT M957, OPS CHKS GOOD. - [SDR DL72S970071](https://openairdocs.org/sdr/DL72S970071), Jan 15, 1997: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT OUT AT ROW 16. REPLACED BATTERY AND RACK. - [SDR DL72S962440](https://openairdocs.org/sdr/DL72S962440), Nov 3, 1996: BATTERY. DISCHARGED. EMERGENCY LIGHT ABOVE L1 DOOR INOP. REPLACED BATTERIES. - [SDR DL72S962414](https://openairdocs.org/sdr/DL72S962414), Oct 29, 1996: WEB. CRACKED. A .75 INCH CRACK AT LIGHTNING HOLE STATION 1243 LT, LOWER TORQUE BOX WEB. INSTALLED DOUBLER PER MM 53-11-0 PG 828. - [SDR DL72S962025](https://openairdocs.org/sdr/DL72S962025), Sep 1, 1996: BATTERY PACK. DISCHARGED. OVERWING EXIT LIGHT AT AFT CARGO DOOR INOP. REPLACED BATTERY CARTRIDGE, OPS CHECK GOOD. - [SDR DL72S960754](https://openairdocs.org/sdr/DL72S960754), Apr 2, 1996: STRINGER. CRACKED. FOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0. - [SDR DL72S960753](https://openairdocs.org/sdr/DL72S960753), Apr 2, 1996: ANGLE. CRACKED. FOUND ON C-2 LETTER CHECK, NR 1 SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0. - [SDR DL72S960555](https://openairdocs.org/sdr/DL72S960555), Feb 29, 1996: RIB. CRACKED. THE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL. - [SDR DL72S960554](https://openairdocs.org/sdr/DL72S960554), Feb 29, 1996: RIB. CRACKED. THE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL. - [SDR DL72S960553](https://openairdocs.org/sdr/DL72S960553), Feb 29, 1996: RIB. CRACKED. THE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL. - [SDR DL72S960389](https://openairdocs.org/sdr/DL72S960389), Feb 20, 1996: RIB. CRACKED. DURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0. - [SDR DL72S960385](https://openairdocs.org/sdr/DL72S960385), Feb 20, 1996: SKIN. CRACKED. DURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813. - [SDR DL72S960463](https://openairdocs.org/sdr/DL72S960463), Jan 29, 1996: RIB. CRACKED. DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0. - [SDR DL72S961604](https://openairdocs.org/sdr/DL72S961604), Jan 20, 1996: FRAME. CORROSION. THE BS 1166 FRAME WAS FOUND CORRODED NEAR STRINGER 29R. THE REMOVED SECTION OF FRAME WAS TOO LARGE TO REPAIR PER THE B727 SRM. THE FRAME WEB IS MANUFACTURED FRO - [SDR DL72S960170](https://openairdocs.org/sdr/DL72S960170), Jan 19, 1996: KEEL BEAM. CORRODED. DURING INSPECTION, THE OUTBD FLANGE OF THE RT KEEL BEAM, STR 29R WAS FOUND WITH CORROSION AT STA 950. DUE TO INTERFERENCE ITEMS IT WAS NECESSARY TO CUT THE FUSE - [SDR DL72S960169](https://openairdocs.org/sdr/DL72S960169), Jan 19, 1996: STRINGER. CRACKED. DURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/B AND I/B SKIN FLANGES, STRINGER 29L BET - [SDR DL72S960129](https://openairdocs.org/sdr/DL72S960129), Jan 11, 1996: FLOOR PAN. CRACKED. FOUND ON MV1 CHECK, LT AND RT LAV FLOOR PAN DITCHING SEAL PANEL CRACKED, VIEWED FROM BAG BIN FWD OF 1183. REPAIRED PER M/M 53-0-11. - [SDR DL72S960475](https://openairdocs.org/sdr/DL72S960475), Jan 9, 1996: RIB. CRACKED. UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON 2ND RIB FROM I/B END. REPAIRED AS PER SRM 57-50-3 FIG 9, FOR NR L/E SLAT. - [SDR DL72S954273](https://openairdocs.org/sdr/DL72S954273), Nov 7, 1995: BATTERY. DISCHARGED. AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL. - [SDR DL72S953685](https://openairdocs.org/sdr/DL72S953685), Sep 12, 1995: BATTERY PACK. DISCHARGED. LT AND RT LOWER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS EACH SIDE. RT SIDE CKS NORMAL. LT SIDE FORWARD TO MCO. - [SDR DL72S953643](https://openairdocs.org/sdr/DL72S953643), Sep 6, 1995: RIB. CRACKED. DURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B U - [SDR DL72S953549](https://openairdocs.org/sdr/DL72S953549), Aug 29, 1995: BEAM. CRACKED. AT A LETTER CHECK IN TPA, A .50 INCH CRACK WAS FOUND IN THE UPPER TRANSVERSE BEAM GUSSET ANGLE AT F.S. 1273. ALSO, A .75 INCH CRACK IN THE ACCOMPANYING UPPER TR - [SDR DL72S953531](https://openairdocs.org/sdr/DL72S953531), Aug 28, 1995: ANGLE. CRACKED. CRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP. - [SDR DL72S953530](https://openairdocs.org/sdr/DL72S953530), Aug 28, 1995: RIB. CRACKED. NR 6 SLAT HAS .50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0. - [SDR DL72S951452](https://openairdocs.org/sdr/DL72S951452), Apr 7, 1995: ACTUATOR. CRACKED. ON APPROACH, LOST SYSTEM A HYDRAULICS. LANDED ATL AND FOUND NR 7 SLAT ACTUATOR CRACKED. REPLACED ACTUATOR, OPERATION NORMAL. - [SDR DL72S950813](https://openairdocs.org/sdr/DL72S950813), Feb 16, 1995: ANGLE. CRACKED. DURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH B727 SB 53-0129 All 57: https://openairdocs.org/deregistered/N419DA-2012-11-07/reports.md ## FAA accident and incident reports (4) 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 19930331011729I](https://openairdocs.org/incident/19930331011729I), Mar 31, 1993: Boeing 727277 (N419DA), Covington - Cin, OH. One hour after departure pilot reported severe vibration. Returned. Replaced NR3 engine fuel control and pump. - [Incident 19930201012029I](https://openairdocs.org/incident/19930201012029I), Feb 1, 1993: Boeing 727277 (N419DA), Atlanta, GA. Maintenance crew instructed by ATC to hold short of runway. Crossed runway. Another aircraft on landing roll. - [Incident 19910405017049I](https://openairdocs.org/incident/19910405017049I), Apr 5, 1991: Boeing 727277 (N419DA), San Antonio, TX. Fuel fumes in cabin after landing. Found 10 containers of stp cleaner in overhead bin. Confiscated from passenger. - [Incident 19800505050849I](https://openairdocs.org/incident/19800505050849I), May 5, 1980: Boeing 727200 (N419DA), Chicago, IL, Minor damage. Wing tip struck runway on hard landing damaging flaps and slats. ## Other aircraft with N419DA - [Registered now](https://openairdocs.org/aircraft/N419DA): Ea Vision EA J100, S/N 85374 --- 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.