# N805EA: 1980 Boeing 727-225, registration cancelled 2006-11-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 8, 2006 - Status when cancelled: Sale reported - Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22436 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 12, 1980 - Last registry action: August 29, 2006 - Mode S code: AAF4D5 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.6544° N, 80.4122° W: Placed by OpenAirDocs at the center of ZIP code 33186, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N805EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805EA - Page: https://openairdocs.org/deregistered/N805EA-2006-11-08 From the FAA registry file of November 5, 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 727-225: https://openairdocs.org/model/boeing-727-225.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 DL72S030340](https://openairdocs.org/sdr/DL72S030340), Apr 4, 2003: SPAR. CRACKED. THE LOWER STRUCTURE AND WEB OF THE LT WING AUX SPAR BEAM WERE FOUND CRACKED NEAR THE NR 7 INBD SPOILER ACTUATOR SUPPORT FITTING. THE LOWER STRUCTURE WAS CUT AND - [SDR DL72S030208](https://openairdocs.org/sdr/DL72S030208), Mar 3, 2003: INDICATOR. MALFUNCTIONED. CAPTS ATTITUDE INDICATOR INTERMITTENT. ROLLS TO 45/90 DEGS WITH AFF FAIL FLAG AND A COMPARITOR ROLL LIGHT. REPLACED CAPTS ADI AND VG PER M/M. SYS CHECKS NORMAL. - [SDR DL72S021413](https://openairdocs.org/sdr/DL72S021413), Dec 5, 2002: ANGLE. CRACKED. NO. 12 SPOILER ACTUATOR ATTACH BRACKET CRACKED OUT BOARD ENDREPLACED ATTACH ANGLE - [SDR DL72S021136](https://openairdocs.org/sdr/DL72S021136), Sep 25, 2002: BATTERY. DISCHARGED. FWD GALLEY DOOR EMERGENCY EXIT LIGHT INOP. WILL NOT TEST, REPLACED BATTERIES AND BULBS OPERATIONAL CHECKS NORMAL. - [SDR DL72S020920](https://openairdocs.org/sdr/DL72S020920), Aug 7, 2002: FUEL CONTROL. MALFUNCTIONED. ON CLIMBOUT AUS NUMBER 3 ENGINE SLOWLY ROLLED BACK TO IDLE. ENGINE SHUTDOWN ON FINAL DFW. REPLACED FUEL PUMP AND FUEL CONTROL RIGGED AND TRIMMED ENGINE, ALL OPS - [SDR DL72S020459](https://openairdocs.org/sdr/DL72S020459), Apr 19, 2002: RIB. CRACKED. L/E NOSE RIB ON NR 5 SLAT I/B SIDE OF ACTUATOR ROD END IS CRACKED. REPAIRED PER M/M 57-54-000-8 AND ERA 382989-14. - [SDR DL72S011506](https://openairdocs.org/sdr/DL72S011506), Sep 8, 2001: SWITCH. CONTAMINATED. NOSE GEAR RED UNSAFE LIGHT ILLUM IN FLT ON GEAR EXTENSION RED AND GREEN NOSE GEAR IND LIGHT ILLUM. MTC FOUND THE NOSE GEAR RED LIGHT ILLUM AT THE GATE CLEANED T - [SDR DL72S011500](https://openairdocs.org/sdr/DL72S011500), Sep 6, 2001: STRINGER. CRACKED. VERT STAB STRINGER 6R CRACKED AT STA 6.372 REPAIRED PER MM 55-30-000-8 FIG 803 - [SDR DL72S011499](https://openairdocs.org/sdr/DL72S011499), Sep 6, 2001: STRINGER. CRACKED. VERT STAB STR 6R CRACKED @ STA 6.372 REPAIRED PER M/M 55-30-000-8 FIG 803 - [SDR DL72S011419](https://openairdocs.org/sdr/DL72S011419), Aug 27, 2001: LIGHT. INOPERATIVE. PAX SEAT 15 & 29 EMERGENCY LIGHTS INOP. RE-ATTACHED CONNECTOR AT SEAT ROW 15 AND RELAMPED SEAT ROW 29. - [SDR DL72S011022](https://openairdocs.org/sdr/DL72S011022), Jun 20, 2001: ACTUATOR. BYPASSING. ON GEAR EXTENSION MAIN GEAR EXTENDED NORMALLY NOSE GEAR DID NOT. FOUND LOCK ACTUATOR BYPASSING INTERNALLY. REPLACED SAME. - [SDR DL72S010915](https://openairdocs.org/sdr/DL72S010915), Jun 5, 2001: ACTUATOR. LEAKING. COMPLETE LOSS OF A SYSTEM HYD UPON GEAR RETRACTION. FOUND RT GEAR DOOR ACTUATOR LEAKING. REPLACED SAME PER M/M. - [SDR DL72S010621](https://openairdocs.org/sdr/DL72S010621), Apr 15, 2001: CONNECTOR. INOPERATIVE. RED EMERGENCY LIGHT INOPERATIVE INBD SIDE OF FWD COAT CLOSET. FOUND WIRE PULLED FRM CONNECTOR. REPAIRED CONNECTOR - [SDR DL72S010167](https://openairdocs.org/sdr/DL72S010167), Jan 29, 2001: ANGLE. CRACKED. FOUND ON C1 LETTER CK, TWO .25 INCH CRACKS IN THE NUMBER 6 SLAT LOWER COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-000-8. - [SDR DL72S001183](https://openairdocs.org/sdr/DL72S001183), Jun 19, 2000: FUEL HEATER. FAILED. NEAR TOP OF CLIMB FL330 NR 1 OIL TEMP WAS 140 DEG CELSIUS. REMAINED IN YELLOW FOR 15 MIN. PERFORMED POM. REPLACED NR 1 FUEL HEAT VALVE, CKS GOOD. - [SDR DL72S001173](https://openairdocs.org/sdr/DL72S001173), Jun 16, 2000: ACTUATOR. FAILED. THE RIGHT MAIN LANDING GEAR WOULD NOT EXTEND NORMALLY. CHECKLIST PROCEDURES FOLLOWED, GEAR WAS MANUALLY EXTENDED (IE CRANKED DOWN). NORMAL INDICATIONS APPEARED - [SDR DL72S000935](https://openairdocs.org/sdr/DL72S000935), May 8, 2000: FRAME. CORRODED. THE VERTICAL LEG OF THE LOWER CHORD OF THE FRONT SPAR ON THE LT WING WAS FOUND CORRODED AT FSS 402. THE CHORD PLATE WAS ALSO FOUND WITH CORROSION DAMAGE ON ITS - [SDR DL72S000719](https://openairdocs.org/sdr/DL72S000719), Apr 15, 2000: SEQUENCE VALVE. CHAFED. AFTER T/O LOST A SYS HYD FLUID. AIR TURNBACK TO ABQ. FOUND LINE IN RT MAIN GEAR FROM SEQUENCE VALVE CHAFED THROUGH. MTC REPLACING SAME. - [SDR DL72S992607](https://openairdocs.org/sdr/DL72S992607), Nov 25, 1999: SEAL. LEAKING. AIRCRAFT WOULD NOT HOLD SCHEDULED CABIN PRESSURE WITH SINGLE PACK OPS AT FL 210. CABIN WAS 8000 FT, CLIMBING 500-700 FEET PER MIN. DESCENDED TO 15,000 TO HOLD L - [SDR DL72S992582](https://openairdocs.org/sdr/DL72S992582), Nov 22, 1999: ANGLE. CRACKED. LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14. - [SDR DL72S992579](https://openairdocs.org/sdr/DL72S992579), Nov 22, 1999: ANGLE. CRACKED. COVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0. - [SDR DL72S992578](https://openairdocs.org/sdr/DL72S992578), Nov 22, 1999: ANGLE. CRACKED. COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0. - [SDR DL72S991772](https://openairdocs.org/sdr/DL72S991772), Aug 9, 1999: CONNECTOR. LOOSE. FIRST CLASS CABIN EMERGENCY LIGHTS WON'T TEST. RESEATED PIN AT QUICK DISCONNECT AT SEAT 4AB. SYSTEM CHECKS NORMAL. - [SDR DL72S991600](https://openairdocs.org/sdr/DL72S991600), Jun 24, 1999: SKIN. DAMAGED. ON SHOP VISIT, DAMAGE WAS FOUND TO THE TOP HALF OF THE C1 DOOR, OUTER SKIN. THE SKIN WAS TRIMMED BETWEEN THE NR 3 AND NR 4 STOP BEAMS AND REMOVED TO THE UPPER E - [SDR DL72S991335](https://openairdocs.org/sdr/DL72S991335), Jun 13, 1999: WIRE. BROKEN. EMERGENCY LIGHT AT SEAT 26D INOP. FOUND BROKEN WIRE AT CONNECTOR. SPLICED WIRE, OPS CHECK GOOD. - [SDR DL72S991212](https://openairdocs.org/sdr/DL72S991212), May 31, 1999: VALVE. INOPERATIVE. WHILE DEPARTING ATL, CENTER FUEL GAUAGE WAS READING 2500 LBS LOWER, WHILE RT WING GAUGE WAS READING HIGHER BY THE SAME. TWO UNITS TRIM REQUIRED FOR LEVEL FLT. A - [SDR DL72S991019](https://openairdocs.org/sdr/DL72S991019), May 9, 1999: BALLAST. FAILED. AFT CABIN AISLE FLUORESCENT LIGHTING (OVERHEAD) WAS SMOKING AND HAD ELECTRICAL SMELL WITH SPARKING. UPON INSPECTION CEILING RAFTER C/B WAS POPPED. REPLACED LIGH - [SDR DL72S991013](https://openairdocs.org/sdr/DL72S991013), May 8, 1999: BATTERY PACK. DISCHARGED. FWD F/C EMER EXIT LIGHT STROBES INOP DURING TEST. REPLACED BATTERY PACK. - [SDR DL72S981932](https://openairdocs.org/sdr/DL72S981932), Sep 17, 1998: WEB. CRACKED. FOUND ON A1 LETTER CK, RT VERTICAL WEB IN LOWER TORQUE BOX AREA CRACKED STA 1223 AND 1233 AT LIGHTENING HOLES. REPAIRED PER MM 53-11-0. - [SDR DL72S981931](https://openairdocs.org/sdr/DL72S981931), Sep 17, 1998: ANGLE. CRACKED. FOUND ON A1 LETTER CK, NR 3 SLAT I/B ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0. - [SDR DL72S980611](https://openairdocs.org/sdr/DL72S980611), Mar 19, 1998: LIGHT. INOPERATIVE. AFT AIRSTAIR EMERG LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY PACK. - [SDR DL72S980363](https://openairdocs.org/sdr/DL72S980363), Feb 10, 1998: STRINGER. CORRODED. FUSELAGE/STRINGER 29R/FS 950D PLUS 10, FS 1007. SPLICE REPAIR A SECTION OF STRINGER 29R NEAR FS 950D PLUS 10 WAS FOUND BADLY CORRODED. THE STRINGER WAS CUT AT S - [SDR DL72S980326](https://openairdocs.org/sdr/DL72S980326), Feb 4, 1998: SKIN. TORN. WHILE ACCOMPLISHING MODIFICATIONS AROUND THE AFT LAV SERVICE PANEL CUTOUT IN THE SKIN, THE BONDED INTERNAL DOUBLER WAS TORN IN SEVERAL LOCATIONS. THE SKIN AND B - [SDR DL72S980278](https://openairdocs.org/sdr/DL72S980278), Feb 2, 1998: SKIN. CORRODED. FUSELAGE SKIN WAS FOUND CORRODED BETWEEN STA 480 AND 500 AND BETWEEN S28L AND BL 0. THE CORROSION WAS TRIMMED AWAY WITH A 9 BY 20 CUTOUT. REPAIRED PER ERA 36369 - [SDR DL72S980203](https://openairdocs.org/sdr/DL72S980203), Jan 20, 1998: SKIN. CORRODED. THE FUSELAGE SKIN BETWEEN STA 490 TO 520 WAS FOUND CORRODED AT STRINGER 27R. THE DAMAGED SKIN WAS CUTOUT AND A DOUBLER AND STRUCTURAL FILLER WERE INSTALLED. THE - [SDR DL72S980205](https://openairdocs.org/sdr/DL72S980205), Jan 19, 1998: BEAM. CORRODED. TYPICAL CORROSION WAS FOUND IN MANY OF THE HOLE BORES OF THE LT AND RT MAIN LANDING GEAR SUPPORT BEAMS AT THE SKIN PANEL ATTACH LOCATIONS. SURFACE CORROSION WAS - [SDR DL72S980144](https://openairdocs.org/sdr/DL72S980144), Jan 18, 1998: SKIN. CORRODED. CORROSION WAS FOUND DURING 4-37113-3 IN THE CENTER WING LWR SKIN. DAMAGE LOCATED BETWEEN S3C AND S7C FROM RBL 15 TO RBL 32 ON THE LWR SURFACE. REPAIRED PER ERA - [SDR DL72S980106](https://openairdocs.org/sdr/DL72S980106), Dec 9, 1997: ANGLE. CRACKED. NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0. - [SDR DL72S980105](https://openairdocs.org/sdr/DL72S980105), Dec 9, 1997: ANGLE. CRACKED. NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR RAIL. DURING SHOP INSPECTION, THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0. - [SDR DL72S980104](https://openairdocs.org/sdr/DL72S980104), Dec 9, 1997: ANGLE. CRACKED. NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0. - [SDR DL72S972668](https://openairdocs.org/sdr/DL72S972668), Dec 8, 1997: SKIN. TORN. .625 INCH LONG CRACK, CONE SKIN 31 FROM I/B END OF FLAP, ALSO COVE SKIN TORN 32 FROM O/B END OF FLAP. BOTH AREAS REPAIRED PER MM 57-52-FIG 809. - [SDR 96ZZZM871](https://openairdocs.org/sdr/96ZZZM871), Apr 21, 1996: ENGINE. FAILED. ON TAKEOFF NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP C - [SDR 96ZZZM1261](https://openairdocs.org/sdr/96ZZZM1261), Apr 21, 1996: BEARING. FAILURE. ON TAKEOFF, NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP - [SDR 95ZZZM700](https://openairdocs.org/sdr/95ZZZM700), Nov 2, 1995: SQUAT SWITCH. MALFUNCTIONED. FLT KIC019 - AKL-SYD - ON LANDING, BOTH RIGHT MAIN TIRES BLEW CAUSING GEAR DOOR AND FLAP TRACK DAMAGE. FOUND NOSE GEAR SQUAT SWITCH (S480) OUT OF RIG. RIGGED SW ## 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 20010801028219I](https://openairdocs.org/incident/20010801028219I), Aug 1, 2001: Boeing 727225 (N805EA), Buffalo, NY, Minor damage. (-23) On August 1, 2001, at 20:17 local time, a Boeing 727 aircraft, bearing registration number N805EA serial number 22436, operating as delta airlines flight… - [Incident 20001126037929I](https://openairdocs.org/incident/20001126037929I), Nov 26, 2000: Boeing 727225 (N805EA), Syracuse, NY. (-23) On Sunday, November 26, 2000, at 2045 EST, a Boeing 727, N805EA, flight 500, operated by delta airlines, blew a tire during landing on runway ten at… - [Incident 19871121073099I](https://openairdocs.org/incident/19871121073099I), Nov 21, 1987: Boeing 727225 (N805EA), Kansas City, MO. Hydraulic in a system. Low and fluctuating. Flaps lowered by alternate system. Emergency equipment requested. - [Incident 19851209065209I](https://openairdocs.org/incident/19851209065209I), Dec 9, 1985: Boeing 727225 (N805EA), Chicago, IL. Leading edge slat NR4 failed to retract when second degree flap position selected. Returned, replaced slat acutator --- 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.