# N410DA: 1976 Boeing 727-232, registration cancelled 2010-07-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 20, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21222
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 1976
- Certificate issued: June 29, 2004
- Last registry action: June 15, 2010
- Mode S code: A4D46C
- Owner when cancelled: [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC)
- Location: [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul)
- Owner type: Corporation
- Owner's area on the map: 38.5420° N, 95.1245° W: Placed by OpenAirDocs at the center of ZIP code 66079, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N410DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=410DA
- Page: https://openairdocs.org/deregistered/N410DA-2010-07-20

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 (63, newest 50)

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

- [SDR DL72S030143](https://openairdocs.org/sdr/DL72S030143), Feb 11, 2003: SKIN. DAMAGED. UPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD.
- [SDR DL72S011025](https://openairdocs.org/sdr/DL72S011025), Jun 21, 2001: WARNING LIGHT. FALSE INDICATION. R-2 DOOR IND ILLUM ON T/O ROLL. ABORTED T/O BELOW 100 KTS. INSPECTED DOOR, NO PROBLEM NOTED. DOOR OPS NORM. CYCLED NUMEROUS TIMES, UNABLE TO DUPLICATE.
- [SDR DL72S010516](https://openairdocs.org/sdr/DL72S010516), Mar 29, 2001: ANGLE. CRACKED. 1/2 INCH CRACK IN NR 8 L/E SLAT COVE SKIN ANGLE AT ANTI-ICE DUCT CUTOUT REPAIRED PER MM 57-54-000-8
- [SDR DL72K001734](https://openairdocs.org/sdr/DL72K001734), Sep 8, 2000: SIGN. INOPERATIVE. FOUND AFT SERVICE DOORS OVERHEAD EXIT SIGN IN AFT GALLEY. REINSTALLED EXIT SIGN. LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY PACK AND BASE, NO HELP. FOUND WIRE 
- [SDR DL72K001291](https://openairdocs.org/sdr/DL72K001291), Jul 7, 2000: RELAY. FAILED. AFTER TAKEOFF PRESSURIZATION AUTO FAILED TO STBY. ATTEMPTED OPERATION IN STBY AND MANUAL. CABIN DIDN''T PRESSURIZE. FOUND PACK VALVE C/B POPPED. LEVELED AT 8,00
- [SDR DL72K000920](https://openairdocs.org/sdr/DL72K000920), May 8, 2000: PUMP. DAMAGED. AS ENG POWER WAS ADVANCED FOR TAKEOFF NR 1 ENG FLAMED OUT. EPR ON NR 1 ENG REACHED 1.3 BEFORE ENGINE INST. ROLLED BACK, NO TAKEOFF WAS INITIATED. FOUND ENG FUEL
- [SDR DL72K000769](https://openairdocs.org/sdr/DL72K000769), Apr 20, 2000: SIGN. INOPERATIVE. AFT EMERGENCY EXIT SIGN INOP AT CENTER AISLE STA 1046. REPLACED BATTERY RACK, CKS NORMAL.
- [SDR DL72K000728](https://openairdocs.org/sdr/DL72K000728), Apr 16, 2000: FRAME. CRACKED. A PREVIOUS REPAIR WAS FOUND ON THE FS 910 FRAME AT STR 18A ON THE RIGHT SIDE OF THE AIRCRAFT. THE REPAIR WAS REMOVED, INSPECTED AND A NEW REPAIR INSTALLED PER E
- [SDR DL72K000727](https://openairdocs.org/sdr/DL72K000727), Apr 16, 2000: FRAME. CORRODED. CORROSION WAS FOUND ON THE FS 1142.7 CARGO DOOR OPENING FRAME ON THE FORWARD SIDE OF THE WEB. THE CORROSION WAS BLENDED AND A DOUBLER INSTALLED PER ERA 334273-1
- [SDR DL72K000723](https://openairdocs.org/sdr/DL72K000723), Apr 16, 2000: SKIN. GOUGED. A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-2 DOOR AT FS 990. THE DAMAGE WAS LOCATED APPROX 1 INCH ABOVE STRINGER 24R. THE SKIN, DOUBLER AND
- [SDR DL72K000668](https://openairdocs.org/sdr/DL72K000668), Apr 7, 2000: DOOR FRAME. CRACKED. THE RT FRAME OF THE AFT ENTRY DOOR WAS FOUND CRACKED IN THE FORWARD FLANGE AT WL 276. THE BEAM WAS CUT AND A NEW SECTION SPLICED IN PER ERA 334236-14. THE DAMAG
- [SDR DL72K000667](https://openairdocs.org/sdr/DL72K000667), Apr 7, 2000: FRAME. WORN. THE FS 1148 FRAME INNER CHORD WAS WORN AT STRINGER 5R. THE DAMAGE WAS BLENDED SMOOTH AND A REPAIR WAS INSTALLED PER ERA334258-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000656](https://openairdocs.org/sdr/DL72K000656), Apr 7, 2000: STIFFENER. CRACKED. CRACKS WERE FOUND ON BOTH THE LBL 8 AND RBL 8 STIFFENERS OF THE 1183 BULKHEAD AT WL 182. THE CRACKS ARE IN THE TYPICAL LOCATIONS AS THOSE DESCRIBED IN S/B 727-5
- [SDR DL72K000655](https://openairdocs.org/sdr/DL72K000655), Apr 7, 2000: SKIN. CRACKED. A CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK IS THROUGH THE SKIN, DOUBLER AND BEARSTRAP AND IS APPROXIMATELY 2 INCHES LONG. THE CR
- [SDR DL72K000654](https://openairdocs.org/sdr/DL72K000654), Apr 7, 2000: SKIN. GOUGED. A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT FS 360 BETWEEN STRINGER 17L AND 18L JUST BELOW AND AFT OF THE L1 DOOR CUTOUT. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED
- [SDR DL72K000589](https://openairdocs.org/sdr/DL72K000589), Mar 28, 2000: SKIN. CRACKED. SEVERAL CRACKS WERE FOUND IN THE LAP JOINT OF THE FUSELAGE SKIN AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE LAP JOINT WAS REPLACED PER ERA 334230-14AD AT HMV.
- [SDR DL72K000568](https://openairdocs.org/sdr/DL72K000568), Mar 24, 2000: BEAM. CORRODED. DURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS AND WEAR AT THE FWD ATTACH LUGS AND TOGGL
- [SDR DL72K000753](https://openairdocs.org/sdr/DL72K000753), Mar 23, 2000: ANGLE. CRACKED. DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 3 PLACES. A SECTION OF THE ANGLE WAS REPLACED AND NEW SECTION SPLICED IN PER MM 5752-01, FIG 80
- [SDR DL72K000638](https://openairdocs.org/sdr/DL72K000638), Mar 23, 2000: SKIN. WORN. AT HMV THE 5 SLAT LEADING EDGE WAS FOUND WORN AT FENCE. DRILLED REPAIR DOUBLER PER MM 57-54-0. DYE PEN INSP AREA UNDER FENCE FOUND 2 CRACKS STOP DRILLED. INSTAL
- [SDR DL72K000585](https://openairdocs.org/sdr/DL72K000585), Mar 23, 2000: RIB. CRACKED. NR 5 SLAT I/B RIB CRACKED. INSTALLED REPAIR DOUBLER PER B727 MM 57-54-0, FIG 814.
- [SDR DL72K001976](https://openairdocs.org/sdr/DL72K001976), Mar 22, 2000: SKIN. DAMAGED. DURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B LOWER CORNER. THE SKIN WAS REPAIRED PER 727 M/M 57-52-0 FIG 803, BY REMOVING THE DAMAGE AND IN
- [SDR DL72K000641](https://openairdocs.org/sdr/DL72K000641), Mar 22, 2000: SKIN. WORN. AT HMV THE SKIN ON 4 L/E SLAT WAS WORN ON UPPER AND LWR SURFACES I/B TRACK. AREA BURNISHED REPAIR DOUBLER MANUF INSTALLED DOUBLER PER MM 57-54-0 FIG 813.
- [SDR DL72K000640](https://openairdocs.org/sdr/DL72K000640), Mar 22, 2000: RIB. CRACKED. AT HMV A RIB WAS FOUND CRACKED ON 4 L/E SLAT I/B END. REPAIRED PER 57-54-0 FIG 814.
- [SDR DL72K000639](https://openairdocs.org/sdr/DL72K000639), Mar 22, 2000: RIB. CRACKED. AT HMV 4 L/E SLAT RIB WAS FOUND CRACKED ON O/B END. REPLACED PER MM 57-54-0 FIG 814. DYE CHECKED, FOUND NO CRACKS.
- [SDR DL72K000756](https://openairdocs.org/sdr/DL72K000756), Mar 21, 2000: ANGLE. CRACKED. DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. A SECTION OF THE ANGLE WAS REPLACED AND SPLICED TO OLD SECTION PER MM 57-52-0, FIG 802.
- [SDR DL72K000755](https://openairdocs.org/sdr/DL72K000755), Mar 21, 2000: ANGLE. CRACKED. DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. THE CHORD WAS REPAIRED PER MM 57-52-0, FIG 802.
- [SDR DL72K000744](https://openairdocs.org/sdr/DL72K000744), Mar 20, 2000: RIB. CRACKED. DURING SHOP VISIT THE I/B AFT RIB WAS FOUND CRACKED IN THE LOWER RADIUS AT THE AFT END. THE CRACK WAS STOP DRILLED AND A DOUBLER INSTALLED PER 727 MM 57-52-0, F
- [SDR DL72K000624](https://openairdocs.org/sdr/DL72K000624), Mar 20, 2000: SKIN. CRACKED. AT HMV THE VERT SKIN WAS CRACKED AT PANEL 9523 LT FWD SIDE OF VERT STAB. REPAIR WAS FABRICATED PER MM 54-30-0 FIG 903 AND REPAIR WAS INSTALLED.
- [SDR DL72K000621](https://openairdocs.org/sdr/DL72K000621), Mar 20, 2000: PANEL. DAMAGED. AT HMV A TEMP REPAIR WAS INSTALLED ON LT SIDE OF VERT STAB AT L/E STA 1298 JUST FWD OF L/E PNL 9525. TEMP REPAIR WAS REMOVED AND DAMAGE CUT OUT AND PERM REPAIR 
- [SDR DL72K000580](https://openairdocs.org/sdr/DL72K000580), Mar 20, 2000: FLAP TRACK. CORRODED. HMV- ATTACH LUG HOLE FORWARD FITTING MLG WING DOOR CORRODED. REPAIRED PER MM 57-43-01.
- [SDR DL72K991576](https://openairdocs.org/sdr/DL72K991576), Jul 11, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN 
- [SDR DL72K991575](https://openairdocs.org/sdr/DL72K991575), Jul 11, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 480-500, STRG 4L, SKIN LAP SPLICE, CRACK REPAIR. HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETW
- [SDR DL72K991574](https://openairdocs.org/sdr/DL72K991574), Jul 11, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 700-720, STRG 4R, SKIN LAP SPLICE : CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN
- [SDR DL72K991573](https://openairdocs.org/sdr/DL72K991573), Jul 11, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 720A-720B, STRG 4R SKIN LAP SPLICE CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN 
- [SDR DL72K991111](https://openairdocs.org/sdr/DL72K991111), May 19, 1999: LIGHT. INOPERATIVE. L2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.
- [SDR DL72K990966](https://openairdocs.org/sdr/DL72K990966), Apr 30, 1999: ANGLE. CORRODED. WHILE PERFORMING HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLES CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLES WITH ANGLES OF NEW MFG.
- [SDR DL72K990740](https://openairdocs.org/sdr/DL72K990740), Apr 5, 1999: ANGLE. CRACKED. A .25 INCH CRACK ON ANGLE FWD SIDE OF FS 910 RT ABOVE AND FWD OF H BRACKET. REPAIRED PER MM 53-11-0, TIME LIMITED REPAIR.
- [SDR DL72K990512](https://openairdocs.org/sdr/DL72K990512), Mar 11, 1999: ACTUATOR. LEAKING. ON WALKAROUND INSPECTION, FOUND NR 14 SPOILER ACTUATOR LEAKING.
- [SDR DL72K981031](https://openairdocs.org/sdr/DL72K981031), May 12, 1998: SKIN. DAMAGED. DURING BUYBACK OF N/R 218, FOUND NUT PLATE EMBEDDED AT RT ELEVATOR LOWER SKIN. SKIN HAS .3125 INCH IN HOLE REPAIRED PER SRM 55-20-3.
- [SDR DL72K980992](https://openairdocs.org/sdr/DL72K980992), May 8, 1998: STRINGER. CRACKED. THE OUTER CHORD OF THE STRINGER 17L CREASE BEAM WAS FOUND WITH A .5 CRACK AT STA 848.95. THE CRACK WAS IN THE HORIZONTAL FLANGE OF THE TEE WHERE THE FLANGE WAS 
- [SDR DL72K981030](https://openairdocs.org/sdr/DL72K981030), May 4, 1998: REAR SPAR. CRACKED. AN .375 INCH CRACK RT ELEVATOR REAR SPAR AT 2ND FROM O/B TAB, HINGE. REPLACED REAR SPAR UNDER EO 4-70183-3AD ME 02 AND ME 03.
- [SDR DL72K980894](https://openairdocs.org/sdr/DL72K980894), Apr 26, 1998: BEAR STRAP. CRACKED. FUSELAGE/SKIN ASSY, R1 DOOR SURROUND DOUBLER, UPPER HINGE CUTOU. REPAIR FOR CRACK IN REINFORCING DOUBLER. THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) 
- [SDR DL72K980950](https://openairdocs.org/sdr/DL72K980950), Apr 22, 1998: SKIN. CRACKED. THREE EACH .125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER MM 54-30-0.
- [SDR DL72K980937](https://openairdocs.org/sdr/DL72K980937), Apr 21, 1998: FLOORBEAM. CORROSION. CORROSION FLOORBEAM STA 1030 BL 0. REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-20-11.
- [SDR DL72K980914](https://openairdocs.org/sdr/DL72K980914), Apr 21, 1998: BEAR STRAP. CRACKED. FOUND ON MV2 CORROSION VISIT, CRACK IN EDGE OF BEARSTRAP AT RT FWD SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REFERENCE SUPPLEMENTAL CARD FOR SI 4-72762-
- [SDR DL72K981029](https://openairdocs.org/sdr/DL72K981029), Apr 20, 1998: BRACKET. CRACKED. NR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812.
- [SDR DL72K980902](https://openairdocs.org/sdr/DL72K980902), Apr 20, 1998: STRINGER. CRACKED. FOUND ON MV2 CORROSION VISIT, 1 VISABLE CRACK STR 18A RT, AFT OF STA 940 FITTING UPPER AFT ATTACH BOLT. REPAIRED PER M/M 53-12-0.
- [SDR DL72K980900](https://openairdocs.org/sdr/DL72K980900), Apr 20, 1998: BRACKET. CRACKED. FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21.
- [SDR DL72K980899](https://openairdocs.org/sdr/DL72K980899), Apr 20, 1998: BRACKET. CRACKED. FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.
- [SDR DL72K980898](https://openairdocs.org/sdr/DL72K980898), Apr 20, 1998: BRACKET. CRACKED. FOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21.

All 63: https://openairdocs.org/deregistered/N410DA-2010-07-20/reports.md

## FAA accident and incident reports (1)

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 19810824083149I](https://openairdocs.org/incident/19810824083149I), Aug 24, 1981: Boeing 727 (N410DA), Washington, DC. Two cabin crew not properly seated. Injured during landing. Operator to change training procedures.

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