# N411DA: Boeing 727-232, registration cancelled 2001-02-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 16, 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: 21223
- Type of aircraft: Fixed wing multi engine
- Certificate issued: July 30, 1976
- Last registry action: March 18, 1998
- Mode S code: A4D823
- 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/N411DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=411DA
- Page: https://openairdocs.org/deregistered/N411DA-2001-02-16

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 (97, newest 50)

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

- [SDR DL72S002208](https://openairdocs.org/sdr/DL72S002208), Nov 10, 2000: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER L2 DOOR INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NML.
- [SDR DL72S002149](https://openairdocs.org/sdr/DL72S002149), Nov 2, 2000: ACTUATOR. LEAKING. ON SLAT EXTENSION NR 6 SLAT NO INTRANSIT OR EXTEND LIGHT. CYCLED SLATS AND LOST A SYS HYD QTY. REPLACED NR 6 SLAT ACTUATOR FOR LEAKING.
- [SDR DL72S002129](https://openairdocs.org/sdr/DL72S002129), Oct 28, 2000: BATTERY PACK. DISCHARGED. ON SERVICE CK, EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S001967](https://openairdocs.org/sdr/DL72S001967), Oct 10, 2000: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME.
- [SDR DL72S000947](https://openairdocs.org/sdr/DL72S000947), May 12, 2000: KEELBEAM. CRACKED. FOUND ON C1 LETTER CK, LOWER I/B FWD VERTICAL KEEL BEAM ANGLE CRACKED RT WHEEL WELL STA 870. REPAIRED PER MM 53-10-9D.
- [SDR DL72S000946](https://openairdocs.org/sdr/DL72S000946), May 12, 2000: ATTACH ANGLE. CRACKED. FOUND ON C1 LETTER CK, 1 INCH CRACK NR 11 SPOILER ACTUATOR I/B ATTACH ANGLE. REPAIRED PER MM 57-42-0.
- [SDR DL72S992591](https://openairdocs.org/sdr/DL72S992591), Nov 23, 1999: BATTERY PACK. DISCHARGED. DURING L/O CHECK, FOUND SVL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTS AND PACKS, ALL CHECK OK.
- [SDR DL72S991891](https://openairdocs.org/sdr/DL72S991891), Aug 23, 1999: WIRE. BROKEN. CEILING EMERGENCY EXIT LIGHT NEAR OVERWING EXIT IS INOP. REPAIRED A BROKEN WIRE AT THE LIGHT ASSY CONNECTOR.
- [SDR DL72S991307](https://openairdocs.org/sdr/DL72S991307), Jun 10, 1999: SKIN. CRACKED. DURING LFEC INSPECTION PER SI 4-74176-12AD, NUMEROUS CRACK INDICATIONS WERE FOUND IN THE VARIOUS FRAME BAYS EXTENDING FROM BS 360-480 ALONG S4R. THERE WAS A PRE
- [SDR DL72S991287](https://openairdocs.org/sdr/DL72S991287), Jun 8, 1999: SKIN. CRACKED. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 14 CRACKS ALONG THE PANEL LENGTH. THE SKI
- [SDR DL72S990616](https://openairdocs.org/sdr/DL72S990616), Mar 15, 1999: FLAP TRACK. CORRODED. DURING OUTSIDE REPAIR, OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND TO THE FWD ATTACH LUGS AND THE MLG BEAM AND SPOILER BEAM ATTACH 
- [SDR DL72S990615](https://openairdocs.org/sdr/DL72S990615), Mar 15, 1999: FLAP TRACK. CORRODED. DURING OUTSIDE REPAIR OF COMPONENT AND OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND ON THE MLG BEAM AND SPOILER BEAM ATTACH PAD AND 
- [SDR DL72S990522](https://openairdocs.org/sdr/DL72S990522), Mar 10, 1999: SKIN. CRACKED. WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12 ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 681 AND BS 740. HFEC INSPECTION CONFIRMED 8 
- [SDR DL72S990521](https://openairdocs.org/sdr/DL72S990521), Mar 10, 1999: SKIN. CRACKED. WHILE ACCOMPLISHING LFEC INSP PER SI 4-74176-12, ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. HFEC CONFIRMED 15 CRACK INDICATIONS I
- [SDR DL72S990520](https://openairdocs.org/sdr/DL72S990520), Mar 10, 1999: FRAME. DENTED. TWO DENTED AREAS WERE FOUND ON THE I/B CHORD OF THE BS 950C FRAME BETWEEN S24L AND 27L. REPAIRED PER ERA 332897-14, REV A.
- [SDR DL72S990490](https://openairdocs.org/sdr/DL72S990490), Mar 10, 1999: SKIN. CRACKED. WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R LAP JOINT, 2 CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND 481. HFEC INSP VERIFIED CRACK INDIC
- [SDR DL72S990489](https://openairdocs.org/sdr/DL72S990489), Mar 10, 1999: SKIN. MISDRILLED. FUSELAGE SKIN WAS MISDRILLED AT S11R AT BS 1233. REPAIRED PER ERA 332842-14, REV A.
- [SDR DL72S990488](https://openairdocs.org/sdr/DL72S990488), Mar 10, 1999: FITTING. CORRODED. CORROSION FOUND IN THE RT MLG SUPPORT BEAM O/B BORE AND IN THE FWD AND AFT FITTINGS. REWORKED PER ERA 332851-14.
- [SDR DL72S990487](https://openairdocs.org/sdr/DL72S990487), Mar 10, 1999: FITTING. CORRODED. CORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A.
- [SDR DL72S990486](https://openairdocs.org/sdr/DL72S990486), Mar 10, 1999: FRAME. CORRODED. BS 600 FRAME BELOW THE CARGO FLOOR AT STR 28R WAS FOUND CORRODED. THE UPPER FRAME OF THE LOWER LOBE CTR FRAME SECTION AND SOME EXISTING REPAIRS WERE ALSO FOUND 
- [SDR DL72S990441](https://openairdocs.org/sdr/DL72S990441), Mar 3, 1999: FITTING. WORN. WEAR WAS FOUND ON BOTH ATTACH LUGS FOR THE HORIZ STAB JACK SCREW MECHANISM. WEAR WAS ON BOTH I/B AND O/B FACES OF EACH LUG. REWORKED PER ERA 332860-14, REV A.
- [SDR DL72S990385](https://openairdocs.org/sdr/DL72S990385), Feb 24, 1999: SKIN. TORN. GOUGE IN SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. DAMAGED AREA LOCATED AT 2-24R. SKIN, DOUBLER, TRIPLER AND BEAR STRAP ARE ALL DAMAGED. ACTION TAK
- [SDR DL72S990361](https://openairdocs.org/sdr/DL72S990361), Feb 24, 1999: FRAME. DENTED. FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950B ABOVE STR 26L. REMOVED DAMAGED PER SRM 53-10-4 FIG 27. DYE PENETRANT CHECKED PER PS 900-6-3, NO CRACKS 
- [SDR DL72S990360](https://openairdocs.org/sdr/DL72S990360), Feb 24, 1999: FRAME. DENTED. FRAME DENTED LT FS 1070, STR 26L. REMOVED DAMAGED AREA, DYE CHECKED PER PS 900-6-3 NR 1. NO FURTHER DAMAGE FOUND. FABRICATED DOUBLER, INSTALLED DOUBLER PER SRM 
- [SDR DL72S990461](https://openairdocs.org/sdr/DL72S990461), Feb 23, 1999: FITTING. CORRODED. AT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUS
- [SDR DL72S990398](https://openairdocs.org/sdr/DL72S990398), Feb 23, 1999: FRAME. CRACKED. OVERWING EXIT FRAME STA 761 RT, 784 LT AND 784 RT FOUND CRACKED IN I/B FLANGE. ACTION TAKEN, ERA 361976-14AD.
- [SDR DL72S990397](https://openairdocs.org/sdr/DL72S990397), Feb 23, 1999: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE AT AN EXISTING FASTENER IN THE SKIN BETWEEN S-7R AND S-8R AT STA 277. ACTION TAKEN, ERA 255827-14.
- [SDR DL72S990751](https://openairdocs.org/sdr/DL72S990751), Feb 17, 1999: SKIN. WORN. LOWER L/E SKIN WORN O/B END OF FLAP APPROX 6 INCHES LONG. REPAIRED PER MM 57-52-0 FIG 803.
- [SDR DL72S991362](https://openairdocs.org/sdr/DL72S991362), Feb 16, 1999: SPAR. DAMAGED. AFT SPAR RAIL DAMAGED AT 2ND FROM I/B AFT FLAP TRACK CUT OUT. REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S990477](https://openairdocs.org/sdr/DL72S990477), Feb 15, 1999: SKIN. CRACKED. AT HMV2, FOUND SKIN CRACKED - EMPENNAGE EXIT, LOC AT FWD RT CORNER OF AFT AIRSTAIRS CUTOUT. FABRICATED DOUBLER PER MM 53-30-00 PG 803. STOP DRILLED CRACK, INSTA
- [SDR DL72S990450](https://openairdocs.org/sdr/DL72S990450), Feb 15, 1999: FRAME. DENTED. FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 27L TO 25L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER PER SRM 5
- [SDR DL72S990416](https://openairdocs.org/sdr/DL72S990416), Feb 15, 1999: FRAME. DENTED. FRAME DENTED AFT CARGO COMPT RT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 25R TO STR 26R. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27. DYE PENETRANT INSPECTED 
- [SDR DL72S990379](https://openairdocs.org/sdr/DL72S990379), Feb 15, 1999: SKIN. CRACKED. SKIN CRACKED EMPENNAGE EXT LOC AT AFT I/B CORNER OF ACCESS PNL 3903 CUTOUT. FABRICATED DOUBLER PER M/M 53-30-0 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER PER
- [SDR DL72S990462](https://openairdocs.org/sdr/DL72S990462), Jan 16, 1999: SKIN. CRACKED. DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 72
- [SDR DL72S982455](https://openairdocs.org/sdr/DL72S982455), Nov 29, 1998: RETRACT MECH. LACK OF LUBE. OUTBOARD FLAPS WOULD NOT EXTEND PAST 15 TO 20 DEGS. DIVERTED TO JFK. PERFORMED OPS CHECK, COULD NOT DUPLICATE. DUE PREVIOUS ITEMS, SERVICED TRANS AND JACKSCREW 
- [SDR DL72S982220](https://openairdocs.org/sdr/DL72S982220), Oct 28, 1998: WIRE. SHORTED. FOUND ON MAINT PREFLIGHT ROWS 12-19 EMERGENCY TRACK LIGHTINGINOP REPLACED BLOWN FUSE ON FWD POWER SUPPLY AFTER REPAIRINGBARE WIRES UNDER SEAT ROW 12 DEF LIGHT O
- [SDR DL72S982157](https://openairdocs.org/sdr/DL72S982157), Oct 16, 1998: BATTERY. DISCHARGED. SEAT ROW 25 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NOW OK.
- [SDR DL72S982010](https://openairdocs.org/sdr/DL72S982010), Aug 10, 1998: ANGLE. CRACKED. DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 AND 23 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INST
- [SDR DL72S982009](https://openairdocs.org/sdr/DL72S982009), Aug 10, 1998: ANGLE. CRACKED. DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING 
- [SDR DL72S982008](https://openairdocs.org/sdr/DL72S982008), Aug 10, 1998: ANGLE. CRACKED. DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-
- [SDR DL72S982007](https://openairdocs.org/sdr/DL72S982007), Aug 10, 1998: ANGLE. CRACKED. DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 44 INCHES FROM O/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING 
- [SDR DL72S981085](https://openairdocs.org/sdr/DL72S981085), May 19, 1998: RIB. CRACKED. FOUND ON A-1 LETTER CHECK, NR 6 SLAT NOSE RIB CRACKED I/B SIDE OF ACTUATOR .75 INCH. REPAIRED PER M/M 57-54-0.
- [SDR DL72S981084](https://openairdocs.org/sdr/DL72S981084), May 19, 1998: FITTING. CRACKED. TAIL SECTION TIE BOLT FITTING CRACKED LT I/B FITTING, CRACKED JUST O/B OF BOLT HEAD. REPLACED FITTING PER BOEING DWG 65-17509 REV M.
- [SDR DL72S981083](https://openairdocs.org/sdr/DL72S981083), May 19, 1998: STIFFENER. CRACKED. NR 3 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21 P 813.
- [SDR DL72S981082](https://openairdocs.org/sdr/DL72S981082), May 19, 1998: BRACKET. CRACKED. NR 1 SLAT ACT O/B ATTACH BRACKET CRACKED AT I/B WEB. REPAIRED PER MM 57-20-21 P 812.
- [SDR DL72S981081](https://openairdocs.org/sdr/DL72S981081), May 19, 1998: SKIN. CRCAKED. FOUND AT A-1 LETTER CHECK, 1.125 INCH CRACK AT FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER 53-30-3.
- [SDR DL72S972383](https://openairdocs.org/sdr/DL72S972383), Nov 16, 1997: BATTERY. DISCHARGED. ON PREFLIGHT, COCKPIT EMERGRNCY LIGHT DID NOT ILLUM IN STBY PWR. REPLACED BATTS, OPS NOW OK.
- [SDR DL72S972160](https://openairdocs.org/sdr/DL72S972160), Oct 25, 1997: SKIN. CRACKED. .5 INCH CRACK IN LOWER SKIN OF LT ELEVATOR 5 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3.
- [SDR DL72S972157](https://openairdocs.org/sdr/DL72S972157), Oct 25, 1997: STRINGER. CRACKED. VERT FIN STR 9L IS CRACKED AT FIN STA 133.800. REPAIR PER MM 55-30-0.
- [SDR DL72S972156](https://openairdocs.org/sdr/DL72S972156), Oct 25, 1997: STRINGER. CRACKED. VERT FIN STR 9L CRACKED AT FIN STA 157.200. REPAIR PER MM 55-30-0.

All 97: https://openairdocs.org/deregistered/N411DA-2001-02-16/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 19990105045219I](https://openairdocs.org/incident/19990105045219I), Jan 5, 1999: Boeing 727232 (N411DA), Salt Lake City, UT, Minor damage. (-23)Delta airlines B-727 N411DA departed Salt lake international on January 5, 2000 at approx. 1836 hrs. During departure the flight crew heard a thump. The…
- [Incident 19920918055509I](https://openairdocs.org/incident/19920918055509I), Sep 18, 1992: Boeing 727277 (N411DA), Chicago, IL. Moderate turbulence with severe downdraft. Two unbelted passengers hurt. Fasten seat belt sign on.
- [Incident 19911013049619I](https://openairdocs.org/incident/19911013049619I), Oct 13, 1991: Boeing 727277 (N411DA), Covington - Cin, OH. Outboard flaps in disagreement with inboard one after takeoff. Returned. Replaced indicator. Adjusted transmitter.
- [Incident 19901007059359I](https://openairdocs.org/incident/19901007059359I), Oct 7, 1990: Boeing 727232 (N411DA), Covington - Cin, OH. Tripped auto pack. Both engines failed. Aborted takeoff. Autopack was previous mco item.

## Other aircraft with N411DA

- [Cancelled 2018-03-23](https://openairdocs.org/deregistered/N411DA-2018-03-23): Cessna 411, S/N 411-0035, built 1965. Registration expired, pending cancellation. Owner: [Team Systems LLC](https://openairdocs.org/faa-owner/TEAM%20SYSTEMS%20LLC), [Johns Creek, GA](https://openairdocs.org/faa-place/GA/Johns%20Creek)

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