# N407DA: Boeing 727-232, registration cancelled 2001-01-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 31, 2001
- 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: 21151
- Type of aircraft: Fixed wing multi engine
- Certificate issued: February 10, 1997
- Last registry action: February 16, 2000
- Mode S code: A4C6EE
- 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/N407DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407DA
- Page: https://openairdocs.org/deregistered/N407DA-2001-01-31

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 (51, newest 50)

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

- [SDR DL72S002028](https://openairdocs.org/sdr/DL72S002028), Oct 16, 2000: ENGINE. BIRD STRIKE. DURING TAKEOFF, A/C SUFFERED BIRD STRIKE, FODDING OUT NR 1 ENGINE. REPLACED ENGINE.
- [SDR DL72S001699](https://openairdocs.org/sdr/DL72S001699), Sep 3, 2000: LIGHT. INOPERATIVE. ON L/O, FOUND L-2 OVER DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S001169](https://openairdocs.org/sdr/DL72S001169), Jun 16, 2000: BATTERY. DISCHARGED. AFT CABIN DOOR OVERHEAD EMERG LIGHT INOP. C/W REPLACED BATTERIES, OPS NOW OK.
- [SDR DL72S000300](https://openairdocs.org/sdr/DL72S000300), Feb 13, 2000: ENGINE. FAILED. RIGHT ENGINE OIL PRESS HIGH WITH NR 3 OIL BYPASS LIGHT. ENGINE SUBSEQUENTLY FAILED. REPLACED ENGINE.
- [SDR DL72S992706](https://openairdocs.org/sdr/DL72S992706), Dec 10, 1999: BRACKET. CRACKED. A 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21.
- [SDR DL72S992688](https://openairdocs.org/sdr/DL72S992688), Dec 9, 1999: LIGHT. INOPERATIVE. FLIGHT DECK EMERGENCY PORTABLE EXIT IDENTIFIER LIGHT WOULD NOT TEST. REPLACED BATTERY PACK, OP CKS GOOD.
- [SDR DL72S991433](https://openairdocs.org/sdr/DL72S991433), Jun 23, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION 
- [SDR DL72S991178](https://openairdocs.org/sdr/DL72S991178), May 25, 1999: CSD. REQUIRED SERVICE. CSD LOW PRESSURE LIGHT FLICKERED AND THEN STAYED ON, LOST MAIN AC NR 2. FOUND CSD LOW. SERVICED CSD, RAN ENG AND NO LEAKS NOTED.
- [SDR DL72S991124](https://openairdocs.org/sdr/DL72S991124), May 20, 1999: WEB. CRACKED. TPA LTR CHK B-2, LT VERT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0 PG 828, LT VERT TORQUE BOX WEB LWR LIGHTE
- [SDR DL72S991122](https://openairdocs.org/sdr/DL72S991122), May 20, 1999: FRAME. CRACKED. FOUND AT B-2 LETTER CHECK, LT AFT ENTRYWAY DOOR FRAME HAS .375 INCH VISIBLE CRACK. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990588](https://openairdocs.org/sdr/DL72S990588), Mar 15, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION
- [SDR DL72S990546](https://openairdocs.org/sdr/DL72S990546), Mar 13, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTIO
- [SDR DL72S990566](https://openairdocs.org/sdr/DL72S990566), Mar 11, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CO
- [SDR DL72S990565](https://openairdocs.org/sdr/DL72S990565), Mar 11, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 TO 740 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION
- [SDR DL72S990562](https://openairdocs.org/sdr/DL72S990562), Mar 11, 1999: SKIN. CRACKED. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION 
- [SDR DL72S990348](https://openairdocs.org/sdr/DL72S990348), Feb 21, 1999: PUMP. FAILED. B-SYSTEM HYD WENT TO 0, FOLLOWED PROCEDURES. WHEN GEAR EXTENDED HYD PRESS WENT TO 1700 PSI. OPERATED BRAKE INTERCONNECT, USED PNEUMATIC BRAKES TO STOP. TOWED AC
- [SDR DL72S982564](https://openairdocs.org/sdr/DL72S982564), Dec 15, 1998: ACTUATOR. LEAKING. AIRCRAFT LOST 'A SYSTEM HYDRAULICS WHILE TAXING TO THE GATE AFTER LANDING IN CVG. MTC FOUND THAT THE NUMBER 7 LEADING EDGE SLAT ACTUATOR HAD FAILED. REPLACED AC
- [SDR DL72S982154](https://openairdocs.org/sdr/DL72S982154), Oct 16, 1998: STRINGER. CRACKED. S18 TAB ON THE RT WING VENT BOX AT WS 171.5 WAS FOUND CRACKED. ADDITIONAL DAMAGE INCURRED WHILE INSTALLING THE SRM REPAIR. REPAIRED PER ERA 332288-14.
- [SDR DL72S982151](https://openairdocs.org/sdr/DL72S982151), Oct 16, 1998: STRINGER. CRACKED. FUSE STR 29R WAS FOUND CRACKED AT FS 950E. REPAIRED PER ERA 332275-14.
- [SDR DL72S982150](https://openairdocs.org/sdr/DL72S982150), Oct 16, 1998: STRINGER. CRACKED. RT WING UPPER SURFACE S18 AT WS 304 WAS FOUND CRACKED, REQUIRING A 2.5 INCH CUTOUT. REPAIRED PER ERA 332341-14.
- [SDR DL72S982149](https://openairdocs.org/sdr/DL72S982149), Oct 16, 1998: FRAME. CRACKED. CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED PER ERA 332283-14AD.
- [SDR DL72S982139](https://openairdocs.org/sdr/DL72S982139), Oct 14, 1998: SKIN. CRACKED. FUSELAGE SKIN WAS FOUND WITH A TIME LIMITED EXT REPAIR DOUBLER FOR A CRACK IN THE SKIN AT FS 294.5, BELOW S15R. THE TIME LIMITED REPAIR WAS REMOVED AND ADDITION
- [SDR DL72S982094](https://openairdocs.org/sdr/DL72S982094), Oct 8, 1998: SKIN. CRACKED. FUSE SKIN HAD A TIME LIMITED REPAIR REMOVED AT FS294, S15R; AND ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332347-14.
- [SDR DL72S982085](https://openairdocs.org/sdr/DL72S982085), Oct 8, 1998: SPAR. DAMAGED. DURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO TOOLING DAMAGE. REPAIRED PER ERA 332359-1
- [SDR DL72S982063](https://openairdocs.org/sdr/DL72S982063), Oct 6, 1998: FRAME. CRACKED. A CRACK WAS FOUND IN THE FS 784 RT FRAME INBD FLANGE. THE CRACK PROPAGATES FROM THE FIRST FASTENER HOLE ABOVE THE FLOOR LINE. REPAIRED PER ERA 300891-14AD, REV 
- [SDR DL72S982112](https://openairdocs.org/sdr/DL72S982112), Oct 1, 1998: TRACK. CORRODED. CORROSION FOUND AT FWD ATTACH LUG FACES AND BORE AND TO MLG BEAM ATTACH HOLES. BUSH LUG HOLES AND INSTALLED SPLICE PLATE REPAIR FOR MLG BEAM ATTACH HOLES.
- [SDR DL72S982318](https://openairdocs.org/sdr/DL72S982318), Sep 30, 1998: ANGLE. CRACKED. DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 18 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802 BY REPLACING A SECTI
- [SDR DL72S982316](https://openairdocs.org/sdr/DL72S982316), Sep 30, 1998: SKIN. CRACKED. DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809 BY REMOVING THE DAMAGE AND
- [SDR DL72S982315](https://openairdocs.org/sdr/DL72S982315), Sep 30, 1998: ANGLE. REPAIRED. DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802
- [SDR DL72S982053](https://openairdocs.org/sdr/DL72S982053), Sep 29, 1998: RIB. CRACKED. INBOARD AFT CLOSE OUT RIB CRACKED AT LWR AFT CORNER. DAMAG REPAIRED PER MM 57-52-0 ON SHOP ORDER 582612.
- [SDR DL72S981998](https://openairdocs.org/sdr/DL72S981998), Sep 25, 1998: PIN. CORRODED. BORE CORRODED LEFT AFT BTL PIN IS CORRODED. CLEANED CORROSION PER SRM 53-40-1 FIG 4 DAMAGE WITHIN LIMITS OK TO TREAT. TREATED BORE PER PS 900-2-4-1 NO O2.
- [SDR DL72S982218](https://openairdocs.org/sdr/DL72S982218), Sep 23, 1998: ANGLE. CRACKED. DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 21 AND 34 FR OM IB END OF FLAP. THE ANGLE WAS REPAIRED BY SPLICING IN A NE W SECTION OF ANGLEPER M
- [SDR DL72S982060](https://openairdocs.org/sdr/DL72S982060), Sep 23, 1998: SUPPORT. WORN. ITEM: NR 2 ENG FWD COWL SUPPORT RING IS WORN AT THE 9 O'CLOCK POS LOC ON FUSELAGE. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER PER M/M 53-11-0 PG 801. O
- [SDR DL72S981764](https://openairdocs.org/sdr/DL72S981764), Aug 24, 1998: BATTERY PACK. DISCHARGED. ON L/O, AFT OVERWING ESCAPE LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S971562](https://openairdocs.org/sdr/DL72S971562), Aug 8, 1997: CONTROL MECH. MALFUNCTIONED. ON APPROACH OUTBD FLAPS WOULD NOT EXTEND. MADE MISSED APPROACH. FLAPS EXTENDED NORMAL ON SECOND ATTEMP. FLAP OPERATIONAL TEST NORMAL ON GROUND AND VISUALLY INSP
- [SDR DL72S970745](https://openairdocs.org/sdr/DL72S970745), Apr 22, 1997: SEQUENCE VALVE. DAMAGED. AFTER T/O DURING GEAR RETRACTION, SYS-A PRESSURE/QUANTITY WENT TO 0, A-SYSTEM PUMPS TURNED OFF 1 MIN LATER. CASTING DAMAGED ON LT GEAR DOOR SEQUENCE VALVE. REPL
- [SDR DL72S970292](https://openairdocs.org/sdr/DL72S970292), Feb 12, 1997: SKIN. CORRODED. CORROSION REMOVED AROUND RADIO ALTIMETER ANTENNA CUTOUT BTWN FS 520 TO 540, STR 28L AND 29R. INTERNAL REPAIR WILL BE INSTALLED. ADDITIONAL DAMAGE WAS FOUND AT L
- [SDR DL72S962654](https://openairdocs.org/sdr/DL72S962654), Dec 6, 1996: POWER SUPPLY. INOPERATIVE. LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, OPS CHECKS GOOD.
- [SDR DL72S962437](https://openairdocs.org/sdr/DL72S962437), Nov 2, 1996: BRACKET. CRACKED. FOUND ON F1 LETTER CK, NR 1 SLAT ACTUATOR ATTACH BRACKETS CRACKED INBD AND OUTBD SIDES. REPAIRED PER MM 57-20-21.
- [SDR DL72S961425](https://openairdocs.org/sdr/DL72S961425), Jun 12, 1996: SWIVEL. LEAKING. DURING CLIMB, A-HYD QTY WENT TO ZERO AND A PUMP LIGHT FLICKERED, RETURNED TO SHV. REPLACED CASE DRAIN FILTERS, NO METAL FOUND. FOUND THE NR 4 SLAT ACTUATOR SWIV
- [SDR DL72S961145](https://openairdocs.org/sdr/DL72S961145), Apr 12, 1996: BULKHEAD WEB. CRACKED. THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 
- [SDR DL72S960876](https://openairdocs.org/sdr/DL72S960876), Apr 12, 1996: SKIN. CORROSION. CORROSION DAMAGE WAS REMOVED FROM AROUND THE HOLE CUTOUT FOR THE RADIO ALTIMETER ANTENNA BETWEEN STATION 520 AND STATION 540, BETWEEN STRINGER 28 LEFT AND STRIN
- [SDR DL72S960875](https://openairdocs.org/sdr/DL72S960875), Apr 12, 1996: SKIN. CORROSION. CORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING STRINGER SPLICE AT BS 490 AND A NEW SPLICE 
- [SDR DL72S960843](https://openairdocs.org/sdr/DL72S960843), Apr 11, 1996: ANGLE. CRACKED. FOUND ON E-2 LETTER CHECK, LWR T-ANGLE CRACKED AT AFT HINGE FOR LWR FUS PANEL 3448R. REPAIRED PER M/M 53-30-1 PG 807.
- [SDR DL72S960512](https://openairdocs.org/sdr/DL72S960512), Mar 4, 1996: LIGHT. LOOSE. ON PRE-FLIGHT, FOUND SECTION OF TRACK LIGHTING LOOSE WITH EXPOSED WIRING. REPAIRED WIRING SECURED TRACK, OPERATION NORMAL.
- [SDR DL72S960291](https://openairdocs.org/sdr/DL72S960291), Feb 6, 1996: SENSOR. DIRTY. ON GEAR RETRACTION, RED RT GEAR AND GREEN RT GEAR LIGHTS REMAINED ON. COMPLETED LDG GEAR RETRACTION MALFUNCTION CHECK LIST, BOTH LIGHTS REMAINED ON. ABOUT 40 SE
- [SDR DL72S960024](https://openairdocs.org/sdr/DL72S960024), Dec 28, 1995: SKIN. CRACKED. A SKIN CRACK, 1.75 INCH BY 2 INCH WAS DISCOVERED BETWEEN STRINGER 27R AND 28R, FS 481. THE PREVIOUS REPAIR ON THIS SECTION MEASURED 5.5 INCH BY 13 INCH. THE REP
- [SDR DL72S954791](https://openairdocs.org/sdr/DL72S954791), Dec 20, 1995: STRINGER. CRACKED. FORWARD LOWER FUSELAGE BS-480 STRINGER 28R SKIN BULGING AND CRACKED. REPAIRED PER DL ERA 302938-14.
- [SDR DL72S954747](https://openairdocs.org/sdr/DL72S954747), Dec 19, 1995: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT OUT LOWER RT OVERWING FAIRING. REPLACED EMERGENCY LIGHT BATTERY PACK. CKS NORMAL.
- [SDR DL72S954709](https://openairdocs.org/sdr/DL72S954709), Dec 15, 1995: COOLING VALVE. FAILED. DURING CLIMB AND LEVEL AT FL 240, WERE UNABLE TO MAINTAIN, CABIN SLOWEST RATE OF ASSENT WAS 700 FPM. DESCENDED AND RETURNED TO JFK. FOUND EQUIPMENT COOLING VALV

All 51: https://openairdocs.org/deregistered/N407DA-2001-01-31/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 19990401020229I](https://openairdocs.org/incident/19990401020229I), Apr 1, 1999: Boeing 727232 (N407DA), Salt Lake City, UT. On April 1, 1999 delta airlines flight 1137 enroute from new orleans to Salt Lake City was issued ILS rwy 16L approach instructions. Delta flight 1137 was at…
- [Incident 19961205044539I](https://openairdocs.org/incident/19961205044539I), Dec 5, 1996: Boeing 727232 (N407DA), Salt Lake City, UT, Minor damage. Narrative: after dl 2110, a 727-200, was towed to position for engine start, while still connected to the towbar, a baggage cart struck the aircraft at the C-2…
- [Incident 19900507024599I](https://openairdocs.org/incident/19900507024599I), May 7, 1990: Boeing 727232 (N407DA), Covington - Cin, OH. Takeoff warning system failed taxiing for takeoff. Replaced up limit switch for horizontal stabilizer.
- [Incident 19780113002809I](https://openairdocs.org/incident/19780113002809I), Jan 13, 1978: Boeing 727232 (N407DA), Boston, MA. Flight returned after oil pressure light came on. Replaced sensor and fuel heat valve.

## Other aircraft with N407DA

- [Registered now](https://openairdocs.org/aircraft/N407DA): Bell Helicopter Textron Canada 407, S/N 54863, built 2019
- [Cancelled 2010-12-23](https://openairdocs.org/deregistered/N407DA-2010-12-23): Bell 206-L4, S/N 52418, built 2010. Exported to Brazil. Owner: [Bell Helicopter Textron Inc](https://openairdocs.org/faa-owner/BELL%20HELICOPTER%20TEXTRON%20INC), [Ft Worth, TX](https://openairdocs.org/faa-place/TX/Ft%20Worth)

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