# N510DA: 1978 Boeing 727-232, registration cancelled 2013-06-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 7, 2013
- Status when cancelled: Sale reported, canceled
- 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: 21312
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 28, 1978
- Last registry action: April 2, 2010
- Mode S code: A661BB
- Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City)
- Owner type: Individual
- Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N510DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=510DA
- Page: https://openairdocs.org/deregistered/N510DA-2013-06-07

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 (44)

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

- [SDR DL72L011206](https://openairdocs.org/sdr/DL72L011206), Jul 19, 2001: SPLICE. CRACKED. LFEC OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED A CRACK IN THE LOWER FASTENER ROW OF THE LOWE
- [SDR DL72L011128](https://openairdocs.org/sdr/DL72L011128), Jul 7, 2001: BATTERY. DISCHARGED. LEFT AFT OVERWING EMERGENCY EXIT LIGHT ON MCO. REPLACED M955 BATTERY CHARGER AND BATTERY.
- [SDR DL72L011097](https://openairdocs.org/sdr/DL72L011097), Jul 1, 2001: BATTERY. DISCHARGED. ON L/O, FOUND INTERIOR OVERWING EXIT LIGHTS ON RIGHT SIDE FLICKERING. T/S, REPLACED BATTERY CARTRIDGE ASSY. OPS CHECK NORMAL.
- [SDR DL72L010634](https://openairdocs.org/sdr/DL72L010634), Apr 17, 2001: SEAL. WORN. LT FWD ENTRY DOOR SEAL MADE ALOUD SQUEAL UPON A/C PRESSURIZING AFTER TAKEOFF SQUEALED UNTIL 4.0 PSI DIFF.AND CEASED AT .5 PSI DIFF. REPAIRED SEAL AREA PRESSURIZ
- [SDR DL72L010530](https://openairdocs.org/sdr/DL72L010530), Apr 1, 2001: SEAT BELT. WORN. EXIT PATH LITE AT SEAT ROW 11 DEF INOPERATIVE. REPLACED SEAT HARNESS. CKS NML.
- [SDR DL72L010324](https://openairdocs.org/sdr/DL72L010324), Feb 23, 2001: FLAP TRACK. CORRODED. DURING OVERHAUL AT BF GOODRICH THE INBOARD FLAP, NR 4 INBOARD TRACK WAS FOUND WITH WEAR AND CORROSION AT THE MLG AND SPOILER BEAM ATTACH PADS, THE MLG DOOR FWD 
- [SDR DL72L010130](https://openairdocs.org/sdr/DL72L010130), Jan 23, 2001: LIGHT. INOPERATIVE. BOTH AFT CABIN DOORS OUTSIDE LIGHTS ARE INOP. RELAMPED BOTH DOORS. OPERATION NORMAL.
- [SDR DL72L002461](https://openairdocs.org/sdr/DL72L002461), Dec 15, 2000: SENSOR. FAULTY. ON LIFT OFF A/C ROLLED TO THE RT - REQUIRED LEFT YOKE TO LEVEL WINGS - SUSPECT FUEL IMBALANCE - FOUND NR 1 FUEL QTY SYSTEM IN ERROR - REPLACED COMPENSATOR
- [SDR DL72L001925](https://openairdocs.org/sdr/DL72L001925), Oct 2, 2000: OXYGEN MASK. DISCONNECTED. S/O OXYGEN MASK HEAD PIECE DISCONNECTED FROM HOSE. REPLACED O2 MASK ASSY, OPS CHECK OK.
- [SDR DL72L001201](https://openairdocs.org/sdr/DL72L001201), Jun 23, 2000: BATTERY PACK. INOPERATIVE. LEFT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS NORMAL
- [SDR DL72L001090](https://openairdocs.org/sdr/DL72L001090), Jun 3, 2000: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK PER MM.
- [SDR DL72L000725](https://openairdocs.org/sdr/DL72L000725), Apr 16, 2000: FRAME. CORRODED. THE 1166 FRAME AND BONDED DOUBLER WERE FOUND WITH CORROSION DAMAGE BETWEEN STRINGER 30 AND STRINGER 29R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 334245-14AD
- [SDR DL72L000663](https://openairdocs.org/sdr/DL72L000663), Apr 7, 2000: SKIN. CORRODED. AN UNIDENTIFIED REPAIR WAS FOUND AT FS 1010 BETWEEN STR 29L AND 29R. THE DOUBLER WAS REMOVED AND ADDITIONAL CORROSION WAS FOUND. THE DAMAGE WAS REMOVED RESULTIN
- [SDR DL72L000653](https://openairdocs.org/sdr/DL72L000653), Apr 7, 2000: FRAME. CRACKED. A CRACK WAS FOUND ON THE FS 700 FRAME BETWEEN STRINGER 22L AND 23L. THE FRAME WAS CUT AT STRINGER 22L AND A NEW SECTION WAS SPLICED. THE DAMAGE WAS REPAIRED PER
- [SDR DL72L000651](https://openairdocs.org/sdr/DL72L000651), Apr 7, 2000: FRAME. CORRODED. THE C2 DOOR SILL WAS FOUND WITH CORROSION JUST FORWARD OF THE FS 990 FRAME. CORROSION WAS FOUND ON THE OUTBAORD HOR. FLANGE AND BLENDED AWAY TO A MAXIMUM DEPTH 
- [SDR DL72L000588](https://openairdocs.org/sdr/DL72L000588), Mar 28, 2000: SKIN. DAMAGED. AN OPEN PILOT HOLE WAS FOUND IN THE FUSELAGE SKIN AT FS 826 JUST ABOVE STRINGER 18A, UNDER THE WING TO BODY FAIRING. THE HOLE WAS .125 IN DIAMETER. ERA 334223-1
- [SDR DL72L000620](https://openairdocs.org/sdr/DL72L000620), Mar 16, 2000: WEB. CRACKED. WEB CRACKED LT LOWER CORNER INSIDE OF VERT, MARKED. STOP DRILLED CRACK AND MADE REPAIR PARTS PER SRM 53-10-4D. CHEMICAL TREAT PER PS 900-2-4-1 NR 2. OK TO IST D
- [SDR DL72L000214](https://openairdocs.org/sdr/DL72L000214), Jan 29, 2000: FCU. FAILED. NR 3 THROTTLE BINDING IN FLT. NO THROTTLE/ENG RESPONSE IN UPPER ONE-THIRD OF TRAVEL. BINDING THEN RELOCATED TO LWR ONE-THIRD OF THROTTLE MOVEMENT. WHEN THROTTLE
- [SDR DL72L992357](https://openairdocs.org/sdr/DL72L992357), Sep 20, 1999: INSULATION. DAMAGED. ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIR
- [SDR DL72L992356](https://openairdocs.org/sdr/DL72L992356), Sep 20, 1999: INSULATION. DAMAGED. ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FOR SPLICES IN LT 48 SEC TO FIRE
- [SDR DL72L991887](https://openairdocs.org/sdr/DL72L991887), Aug 24, 1999: BATTERY PACK. DISCHARGED. ON L/O, FOUND RIGHT EXTERIOR OVERWING EMERGENCY LIGHT FLASHING DURING TEST. REPLACED BATTERY PACK.
- [SDR DL72L990034](https://openairdocs.org/sdr/DL72L990034), Jan 7, 1999: BRACKET. CRACKED. THE ACTUATOR SUPPORT BRACKET DOUBLERS WERE FOUND CRACKED FOR THE NR 7 SLAT. THE CRACKS ARE TYPICAL OF BAC S/B 727-57- 0130. THE BRACKETS WERE MODIFIED PER THE I
- [SDR DL72L990013](https://openairdocs.org/sdr/DL72L990013), Jan 4, 1999: FRAME. CRACKED. A .25 INCH VISIBLE CRACK LOWER FWD CORNER NR 5 FLAP ACT MOUNT BOX I/B FRAME. REPAIRED PER MM 57-20-21.
- [SDR DL72L990011](https://openairdocs.org/sdr/DL72L990011), Jan 4, 1999: BRACKET. CRACKED. FOUND ON D1 LETTER CK, .25 INCH CRACK NR 5 L/E FLAP ACTUATOR OUTBOARD ATTACH BRACKET. REPAIRED PER MM 57-20-21.
- [SDR DL72L982644](https://openairdocs.org/sdr/DL72L982644), Dec 24, 1998: DUCT. FAILED. ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. ALL CK LIST WERE RUN AND LIGHT DID NOT GO OUT. SHUT DOWN NR 1 ENG AND DUMP FUEL. RETURNED TO SEA. REPLAC
- [SDR DL72L982358](https://openairdocs.org/sdr/DL72L982358), Nov 14, 1998: BATTERY. DISCHARGED. AFT AIRSTAIR EMERGENCY LIGHTS FAILED TO TEST. REPLACED BATTERY.
- [SDR DL72L981963](https://openairdocs.org/sdr/DL72L981963), Sep 21, 1998: WIRE. BROKEN. WHEN LANDING GEAR WAS LOWERED THE RLG GREEN DOWN AND LOCKED DIDN'T ILUMINATE. LIGHT DIDN'T PRESS TO TEST. CHANGED BULBS, NO HELP. WENT TO BRIGHT ON BRIGHT/DIM S
- [SDR DL72L981147](https://openairdocs.org/sdr/DL72L981147), May 29, 1998: WEB. CRACKED. RT VERT TORQUE BOX WEB CRACKED .875 INCH AT UPPER LIGHTENING HOLE STA 1300 RT. REPAIRED PER MM 53+11+0 P 828.
- [SDR DL72L972666](https://openairdocs.org/sdr/DL72L972666), Dec 17, 1997: RIB. CRACKED. O/B ACTUATOR RIB CRACKED. REPAIRED RIB PER SRM 57-54-0.
- [SDR DL72L972678](https://openairdocs.org/sdr/DL72L972678), Dec 13, 1997: RIB. CRACKED. RIB NR 18 CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72L972164](https://openairdocs.org/sdr/DL72L972164), Oct 27, 1997: MEGAPHONE. INOP. ON PREDEPARTURE CK, FOUND F/C MEGAPHONE INOP. REPLACED F/C MEGAPHONE.
- [SDR DL72L972153](https://openairdocs.org/sdr/DL72L972153), Oct 25, 1997: ANGLE. CRACKED. FROM MV1C1, .25 INCH VISIBLE CRACK KEEL BEAM VERTICAL ANGLE INBD OF APU LOAD CONTROL VALVE. REPAIRED PER SRM 53-10-9.
- [SDR DL72L972151](https://openairdocs.org/sdr/DL72L972151), Oct 25, 1997: SUPPORT. CRACKED. FROM MV1C, NR 7 SLAT ACTUATOR O/B SUPPORT STRUCTURE CRACKED. REPAIR PER M/M 57-42-0.
- [SDR DL72L972189](https://openairdocs.org/sdr/DL72L972189), Oct 24, 1997: FRAME. CORRODED. FUSELAGE C3 DOOR SURROUND FS 1142.7 FRAME STRG 28R. REPAIR FOR CORRODED SKIN ATTACH FLANGE. C3 AFT DOOR JAMB FRAME (FS 1142.7) WAS FOUND CORRODED AT STRG 28R. T
- [SDR DL72L972152](https://openairdocs.org/sdr/DL72L972152), Oct 24, 1997: SKIN. CRACKED. FROM MV1C1, .5 INCH CRACK IN VERTICAL SKIN AT UPPER RIVET ROW OF LT TORQUE BOX AT STA 1223. REPAIR PER M/M 53-11-0.
- [SDR DL72L972180](https://openairdocs.org/sdr/DL72L972180), Oct 23, 1997: SKIN. CORRODED. FUSELAGE SKIN FS 480-500, STRG 28L, SKIN CUT OUT DUE TO CORROSION. REPAIRED PER ER/A 362981-14.
- [SDR DL72L972075](https://openairdocs.org/sdr/DL72L972075), Oct 16, 1997: CHORD. CORRODED. CORROSION FOUND ON O/B FLANGE OF NOSE WHEEL WELL SIDE PANEL T-CHORD RT WALKWAY BEAM AFT OF STA 312 AND 344. CLEANED CORROSION WITHIN LIMITS PER SRM 53-10-4 FIG 
- [SDR DL72L972076](https://openairdocs.org/sdr/DL72L972076), Oct 14, 1997: RIB. CRACKED. A .25 INCH CRACK IN NR 4 SLAT I/B ACTUATOR ATTACH NOSE RIB. REPAIRED PER MM 57-40-0.
- [SDR DL72L970260](https://openairdocs.org/sdr/DL72L970260), Feb 12, 1997: BATTERY. DISCHARGED. DOOR EXIT LIGHT ABOVE COCKPIT DOOR DOES NOT ILLUMINATE WITH STANDBY POWER. REPLACED BATTERIES.
- [SDR DL72L960257](https://openairdocs.org/sdr/DL72L960257), Feb 1, 1996: STRINGER. CRACKED. STRINGERS CRACKED 3RD BAY UP IN VERT STAB ON LT AND RT SIDE UPPER END AND 3RD BAY UP RT LOWER. FOUND DURING A-2 LTR CK TPAMM AND REPAIRED PER SRM 55-30-0.
- [SDR DL72L954440](https://openairdocs.org/sdr/DL72L954440), Nov 19, 1995: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOP 2R AND AFT AISLE. REPLACED BATTERY PACK, OPERATION NORMAL.
- [SDR DL72L952919](https://openairdocs.org/sdr/DL72L952919), Jul 1, 1995: ANGLE. CRACKED. DURING LETTER CHECK, A 1 INCH CRACK WAS FOUND IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. REPLACED DAMAGED PART IN ACCORDANCE WITH S/B 727-53-01
- [SDR DL72L950756](https://openairdocs.org/sdr/DL72L950756), Feb 20, 1995: ACTUATOR. CRACKED. ON LANDING GEAR EXTENSION, LOST ALL A SYSTEM HYDRAULIC FLUID, LANDED SAN WITHOUT INCIDENT, FOUND NOSE LANDING GEAR DOWN LOCK ACTUATOR CRACKED. REPLACED ACTUATOR
- [SDR DL72L950605](https://openairdocs.org/sdr/DL72L950605), Feb 11, 1995: ANTI-ICE VALVE. LEAKING. DURING CLIMB, HAD NR 3 STRUT OVERHEAT LIGHT ON, LIGHT WENT OUT WITH REDUCTION OF POWER. RETURNED ATL. REPLACED NR 3 ENGINE ANTI-ICE VALVE AND UPPER ANTI-ICE DUC

## 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 19930929043329I](https://openairdocs.org/incident/19930929043329I), Sep 29, 1993: Boeing 727277 (N510DA), Kansas City, MO. NR3 engine shut down due to low oil pressure. Landed at destination safely. Replaced engine.
- [Incident 19911031061149I](https://openairdocs.org/incident/19911031061149I), Oct 31, 1991: Boeing 727277 (N510DA), Portland, OR. NR3 engine failed on takeoff roll. Aborted. Returned to gate. Replaced engine.
- [Incident 19800918068919I](https://openairdocs.org/incident/19800918068919I), Sep 18, 1980: Boeing 727232 (N510DA), Dallas, TX. Flight returned when nose gear door stayed open. Replaced nose gear door pulley and nos gear assembly.
- [Incident 19790304010059I](https://openairdocs.org/incident/19790304010059I), Mar 4, 1979: Boeing 727232 (N510DA), Dallas, TX. Engine shutdown due to low oil pressure light. Low oil pressure light deactivatd after checking screens

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