# N677MC: 1977 Mcdonnell Douglas DC-9-51, registration cancelled 2018-12-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 6, 2018 - Status when cancelled: First renewal notice - Airframe: [Mcdonnell Douglas DC-9-51](https://openairdocs.org/model/mcdonnell-douglas-dc-9-51) (registry code 3022051) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47756 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 13, 1985 - Certificate issued: December 31, 2009 - Last registry action: March 31, 2016 - Mode S code: A8F6CF - 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: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N677MC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=677MC - Page: https://openairdocs.org/deregistered/N677MC-2018-12-06 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 Mcdonnell Douglas DC-9-51: https://openairdocs.org/model/mcdonnell-douglas-dc-9-51.md ## Service difficulty reports (48) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1223259884](https://openairdocs.org/sdr/DALA1223259884), Apr 12, 2012: DOOR FRAME. DAMAGED. DURING LINE CHECK, MAINTENANCE FOUND THE FORWARD CARGO DOOR FRAME EDGE HAD A LARGE GOUGE. MAINTENANCE REMOVED AND INSTALLED DAMAGED DOUBLER PER EA 98-205669 REV - [SDR DALA1163289884](https://openairdocs.org/sdr/DALA1163289884), Nov 11, 2011: A/C PACK. OVERHEATED. A/C 9884 FLT 1246 FAR-MSP: RIGHT PACK OVERHEATING DID NOT REACT TO AUTO SELECTION, WENT TO MANUAL TO CONTROL. RIGHT PACK HAD OVERHEATED WITH SMOKE IN THE CABIN. - [SDR DALA1108779884](https://openairdocs.org/sdr/DALA1108779884), Feb 5, 2011: STRUCTURE. CRACKED. DURING LEAK CK, 2 CRACKS WERE FOUND AT THE FWD LOWER AND THE UPPER AFT CORNERS OF THE FWD LAV SERVICE DOOR. THE FWD CRACK WAS FOUND TO BE 1.5" LONG AND AFT CRAC - [SDR DALA1108669884](https://openairdocs.org/sdr/DALA1108669884), Feb 5, 2011: DOUBLER. CRACKED. FUSELAGE EXTERIOR FWD LAV SERVICE PANEL LANDING INTERNAL DOUBLER HAS APPROXIMATELY 1.5 INCH CRACK AT FWD LOWER CORNER. ACCOMPLISHED ERA 489353-4 P-192 REQUIRED - [SDR DALA1108319884](https://openairdocs.org/sdr/DALA1108319884), Feb 3, 2011: SKIN. CRACKED. L1 DOOR JAMB, FORWARD UPPER CORNER HAS APPROX .750 CRACK IN OUTER SKIN REPAIR PER SRM 53-05 FIG.25A OR FIG 26 AD FAR INSPECTION. CUT OUT SKIN AND REMOVED CRACK - [SDR DALA1108059884](https://openairdocs.org/sdr/DALA1108059884), Feb 1, 2011: ATTACH BRACKET. CRACKED. LT WING T/E REAR SPAR FWD OF INBD SPOILER ACTUATOR ATTACH BRACKET CRACKED. REMOVED ATTACH BRACKET IAW SRM 51-30-5. LOCATED, DRILLED AND INSTALLED NEW ATTACH BRA - [SDR DALA1107139884](https://openairdocs.org/sdr/DALA1107139884), Jan 29, 2011: SKIN. CRACKED. FUSELAGE EXTERIOR STA 69 BETWEEN L21R AND L22R SKIN CRACKED AT 3EA FASTENERS. CUT OUT CRACKED AREA FROM SKIN AT STA 69 BETWEEN L21R & L22R IAW SRM 53-04, FIG 38 - [SDR DALA1107129884](https://openairdocs.org/sdr/DALA1107129884), Jan 29, 2011: SKIN. CRACKED. FUSELAGE EXTERIOR STA 69 BETWEEN L19R AND L20R SKIN CRACKED AT FASTENER. REMOVED DAMAGE IAW SRM 53-04, FIG 38, FABRICATED 1EA FILLER & 1EA DOUBLER IAW SRM 53-34 - [SDR DALA1108729884](https://openairdocs.org/sdr/DALA1108729884), Jan 21, 2011: HINGE. CRACKED. LT WING FLAP, FLAP HALF OF NR 2 HINGE HAS NDT VERIFIED CRACK. REMOVED & REPLACED LT FLAP NR 2 FLAP HINGE AFT HALF IAW DC-9 OHM 27-50-1 PERFORMED OPS CHECK; OPS - [SDR DALA1108049884](https://openairdocs.org/sdr/DALA1108049884), Jan 20, 2011: SKIN. CRACKED. FUSELAGE EXTERIOR, STA 101 BETWEEN L19R AND L20R SKIN CRACKED AT FASTENER. GAINED ACCESS, CUT OUT DAMAGE 1.55 X 1.55. NDT VERIFIES NO CRACK INDICATION NOTED, FA - [SDR DALA1032969884](https://openairdocs.org/sdr/DALA1032969884), Nov 19, 2010: RIB. DAMAGED. DURING LINE CHECK FOUND FLAP DAMAGE TO LT WING FLAP T/E 4 FT OTBD FROM INBD MOST EDGE. REMOVED T/E PANEL 788 IAW CMM 27-50-1. REMOVED DAMAGED RIB SRM 57-03 INST - [SDR DALA1019879884](https://openairdocs.org/sdr/DALA1019879884), Aug 22, 2010: MOUNT. CRACKED. DURING LINE CHECK, FOUND CRACK IN RT PYLON AFT ENGINE MOUNT SUPPORT FRAME AFT WEB. REPAIRED IAW ERA 484935-14. - [SDR DALA107159884](https://openairdocs.org/sdr/DALA107159884), Apr 5, 2010: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OP - [SDR DALA101699884](https://openairdocs.org/sdr/DALA101699884), Jan 24, 2010: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 23-26 OF THE CABIN WERE TOO DIM TO PROVIDE ESCAPE GUIDANCE. MX REPLACED THE BATTERY PACK - [SDR DALA100249884](https://openairdocs.org/sdr/DALA100249884), Jan 8, 2010: SUPPORT FITTING. CORRODED. DURING LINE CHECK FOUND CORROSION ON RT MLG SUPPORT FITTING. REPLACED FITTING IAW CMM 57-40-01 AND AMDS 3210-9904M-RT. - [SDR NWAA094409884](https://openairdocs.org/sdr/NWAA094409884), Dec 19, 2009: WIRE. DAMAGED. DURING LINE CHECK MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPAIRED THE WIRING AND - [SDR NWAA093939884](https://openairdocs.org/sdr/NWAA093939884), Nov 21, 2009: BATTERY. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND THAT ALL OF THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE - [SDR NWAA091749884](https://openairdocs.org/sdr/NWAA091749884), May 11, 2009: FLOOR PANEL. DEBONDED. DURING "H" CHECK, FOUND FLOOR PANEL NR 17 HAD 10 SUPPORT CHANNELS DISBONDED AT END ATTACH POINTS. REPAIRED PER EA 98-214550. - [SDR NWAA091969884](https://openairdocs.org/sdr/NWAA091969884), May 6, 2009: FLOOR SUPPORT. CRACKED. DURING "H" CHECK FOUND FLOOR PANEL NR 18 HAD 4 SUPPORT CHANNELS CRACKED. REPAIRED PER EA 98-214548. - [SDR NWAA091959884](https://openairdocs.org/sdr/NWAA091959884), May 5, 2009: RIB. CRACKED. DURING "H" CHECK FOUND CRACK IN RT WING LEADING EDGE RIB AT STATION XIS 134. REPAIRED PER EA 98-214545. - [SDR NWAA09819884](https://openairdocs.org/sdr/NWAA09819884), Mar 23, 2009: BATTERY. INOPERATIVE. DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-16 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD. (K) - [SDR NWAA09729884](https://openairdocs.org/sdr/NWAA09729884), Mar 9, 2009: FUSE. FAILED. DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-14 AND THE LT FWD OVERWING EMERGENCY EXIT SIGN WERE INOPERATIVE. MX INSTALLED NEW BATT - [SDR NWAA084139884](https://openairdocs.org/sdr/NWAA084139884), Sep 1, 2008: FUSE. BLOWN. DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE ASSOCIATED FUSE. OPS CHECK WAS GOOD. - [SDR NWAA083439884](https://openairdocs.org/sdr/NWAA083439884), Jul 26, 2008: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-13 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND T - [SDR NWAA082049884](https://openairdocs.org/sdr/NWAA082049884), May 9, 2008: FUSE. FAILED. AS THE AIRCRAFT WAS BEING PUSHED BACK FOR DEPARTURE, THE RIGHT HYDRAULIC SYSTEM LOST ALL FLUID. COM PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT RETURNED TO T - [SDR NWAA081549884](https://openairdocs.org/sdr/NWAA081549884), Apr 10, 2008: FUSE. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE ASSOCIATED - [SDR NWAA071509884](https://openairdocs.org/sdr/NWAA071509884), Apr 15, 2007: FRAME. CRACKED. DURING ENGINE CHANGE, FOUND CRACKS IN NR 1 PYLON HORIZONTAL WEB FRAME AT XN 39.250. REPAIRED PER EA 98-209044. - [SDR 0602779884](https://openairdocs.org/sdr/0602779884), Dec 18, 2006: OVEN. SMOKE. WHEN FLIGHT ATTENDANT ATTEMPTED TO UTILIZE THE OVEN A THICK WHITE SMOKE DEVELOPED FROM THE ELECTRICAL WIRE CONNECTION AREA AT BACK WALL. SMOKE SMELLED OF ELECTR - [SDR 0600039884](https://openairdocs.org/sdr/0600039884), Jan 2, 2006: UNKNOWN. MALFUNCTIONED. FLIGHT CREW REPORTS THAT THE FLIGHT CONTROL PITCH INPUTS WERE SLUGGISH DURING FINAL APPROACH FOR LANDING. AIRCRAFT DID NOT RESPOND IN A TIMELY MANNER AND PITCH - [SDR 0401139884](https://openairdocs.org/sdr/0401139884), Jun 25, 2004: LIMITER. CRACKED. AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID FROM THE LT SYSTEM AFTER RETRACTION OF LANDING GEAR DURING CLIMBOUT. COMPLIED WITH COM PROCEDURES AND THE F - [SDR 0301259884](https://openairdocs.org/sdr/0301259884), Jul 7, 2003: TIRE. SEPARATED. DURING TAKEOFF, THE NR 4 TIRE EXPERIENCED COMPLETE TREAD SEPARATION. DEBRIS FROM THIS FAILED TIRE DAMAGED THE NR 2 ENGINE CAUSING A LOSS OF OIL PRESSURE REQUIRI - [SDR 0200679884](https://openairdocs.org/sdr/0200679884), Mar 18, 2002: SLAT. MALFUNCTIONED. WHILE ON APPROACH FOR LANDING AT MOT, CREW NOTICED THE SLAT DISAGREEMENT LIGHT ON AND THE AIRCRAFT ROLL TO THE RIGHT. FOLLOWED COM PROCEDURES. DUE TO INSUFFICIE - [SDR 9811089884](https://openairdocs.org/sdr/9811089884), Dec 30, 1998: SENSOR. FAILED. DURING APPROACH INTO DTW, THE NOSE LANDING GEAR UNSAFE INDICATOR LIGHT ILLUMINATED WITH LANDING GEAR EXTENSION. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARE - [SDR 9807269884](https://openairdocs.org/sdr/9807269884), Apr 26, 1998: SWITCH. STICKING. DURING TAKEOFF ROLL, THE TAKEOFF AURAL WARNING HORN SOUNDED. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBR - [SDR 9801479884](https://openairdocs.org/sdr/9801479884), Jan 25, 1998: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9712279884](https://openairdocs.org/sdr/9712279884), Jun 20, 1997: TEMP SENSOR. FAILED. AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LIGHT WENT OUT WITH POWER REDUCTION. FLIGHT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. INS - [SDR 9707789884](https://openairdocs.org/sdr/9707789884), Apr 16, 1997: TEMP SENSOR. FAILED. DURING CLIMB-OUT OF DFW PASSING 17,000, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. LIGHT REMAINED ON. LIG - [SDR 9710939884](https://openairdocs.org/sdr/9710939884), Apr 7, 1997: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON LONGERON 22L BETWEEN FS 1151 TO 1167. REPAIRED PER EA 98-111889. - [SDR 9702109884](https://openairdocs.org/sdr/9702109884), Feb 1, 1997: STRUT. REQD SERVICE. AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. FLIGHT RETURNED TO FAR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR STRUT FLAT. SERVICE NOSE GEAR STRUT - [SDR 9622609884](https://openairdocs.org/sdr/9622609884), Oct 20, 1996: RELEASE MECH. INOPERATIVE. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. FOUND THE LOWER CABLE INNER SLEEVE LODGED IN THE CONDUIT. REMOVED THE SLEEVE - [SDR 9619379884](https://openairdocs.org/sdr/9619379884), Sep 8, 1996: FUEL HEAT VALVE. FAILED. WHILE APPLYING TAKEOFF POWER, THE LEFT ENGINE FUEL HEAT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND THE SYSTEM WAS PLACED ON MEL. FLIGHT RESUMED AS SCHEDULED. M - [SDR 9610489884](https://openairdocs.org/sdr/9610489884), May 10, 1996: SOCKET. INOPERATIVE. DURING LINE CHECK, FOUND FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED LIGHT SOCKET, OPERATIONAL CHECK GOOD. - [SDR 9602129984](https://openairdocs.org/sdr/9602129984), Jan 25, 1996: NOSE BULLET. ICED UP. NR 1 ENGINE EPR INDICATION WAS ABNORMALLY HIGH DURING POWER APPLICATION ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENA - [SDR 9521419884](https://openairdocs.org/sdr/9521419884), Dec 25, 1995: STRUT. DEFLATED. LANDING GEAR WOULD NOT RETRACT DUE TO GROUND SHIFT FAILURE AFTER TAKEOFF. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND SERV - [SDR 9521409884](https://openairdocs.org/sdr/9521409884), Dec 22, 1995: STRUT. DEFLATED. AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT TO - [SDR 9520389884](https://openairdocs.org/sdr/9520389884), Dec 13, 1995: STRUT. DEFLATED. NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RED NOSE UNSAFE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND ICE ACC - [SDR 9518819884](https://openairdocs.org/sdr/9518819884), Nov 21, 1995: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS BETWEEN ROWS 6 AND 11 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. - [SDR 9516209884](https://openairdocs.org/sdr/9516209884), Oct 17, 1995: DN LOCK SENSOR. FAILED. DURING CLIMB, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED, CONTINUED TO DTW AND LAND ## 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 20030720013919I](https://openairdocs.org/incident/20030720013919I), Jul 20, 2003: Doug DC951 (N677MC), Kansas City, MO. (-23) Upon approach, after gear extension the nose gear unsafe light remained illuminated. Contacted mx. Cont. Normal indication obtained. Pilot declared an… - [Incident 19980519026519I](https://openairdocs.org/incident/19980519026519I), May 19, 1998: Doug DC951 (N677MC), Cleveland, OH. On may 19, 1998, at approximately 1831 EDT, NWA609 taxied slightly across the 23C hold bar without cel-atct clearance. Although there was no loss of ATC… - [Incident 19881114067959I](https://openairdocs.org/incident/19881114067959I), Nov 14, 1988: Doug DC951 (N677MC), Detroit, MI, Minor damage. Smoke in lavatory from fire in trash bin. Put out fire. Determined fire to be of suspicious origin. - [Incident 19851011055979I](https://openairdocs.org/incident/19851011055979I), Oct 11, 1985: Doug DC951 (N677MC), Las Vegas, NV, Substantial damage. Tire failed at rotation after striking debris on runway. Returned and found strut flying door gone, engine FOD. --- 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.