# N676MC: 1975 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: 47652
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 25, 1985
- Certificate issued: December 31, 2009
- Last registry action: March 31, 2016
- Mode S code: A8F318
- 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/N676MC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=676MC
- Page: https://openairdocs.org/deregistered/N676MC-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 (47)

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

- [SDR DALA12000030881](https://openairdocs.org/sdr/DALA12000030881), May 1, 2012: LIGHT. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 6D TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE LIGHT RETURNED TO AN OPER
- [SDR DALA1219179881](https://openairdocs.org/sdr/DALA1219179881), Mar 23, 2012: SIGN. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY EXIT SIGN ON THE LEFT SIDE OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT
- [SDR DALA1154689881](https://openairdocs.org/sdr/DALA1154689881), Sep 19, 2011: BATTERY. DISCHARGED. MAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES PER AMM. AIRCRAFT OK FOR SERVICE.
- [SDR DALA1147039881](https://openairdocs.org/sdr/DALA1147039881), Aug 6, 2011: FAN BLADE. BROKEN. DURING TAKEOFF ROLL JUST ABOVE 80 KNOTS A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT SHIMMY. FLIGHT CREW ABORTED TAKEOFF AND NOTICED ENGINE NR 2 VIBRATION. ENGINE
- [SDR DALA1139919881](https://openairdocs.org/sdr/DALA1139919881), Jun 15, 2011: FUEL LINE. DISCONNECTED. AIRCRAFT RETURNED TO ATL DUE TO UNCOMMANDED FUEL VENTING FROM LEFT WING TIP IN FLIGHT. FUEL VENTING STOPPED ONLY AFTER CENTER TANK WENT DRY. MAINTENANCE FOUND F
- [SDR DALA1112849881](https://openairdocs.org/sdr/DALA1112849881), Feb 22, 2011: SKIN. CRACKED. MONITOR BLIND FASTENERS-AD-FAR FUSELAGE EXTERIOR FORWARD SERVICE DOOR JAMB AFT LOWER CORNER HAS NDT VERIFIED CRACK AT FASTENER. REPAIR PER 5330-01134-02D. CUT O
- [SDR DALA1112829881](https://openairdocs.org/sdr/DALA1112829881), Feb 22, 2011: SKIN. CRACKED. DURING LCK IN DHN, AN 0.125 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE FWD CARGO DOOR JAMB CUTOUT, UPPER FORWARD CORNER. WORK PER ER/A 475544-14AD AS
- [SDR DALA1112809881](https://openairdocs.org/sdr/DALA1112809881), Feb 22, 2011: SKIN. CRACKED. DURING LCK AT DHN, A 0.25 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB CUTOUT, AFT LOWER CORNER. DFRD STA ATL 22FEB11 ATA 5331. WORK P
- [SDR DALA1112619881](https://openairdocs.org/sdr/DALA1112619881), Feb 21, 2011: ANGLE. CRACKED. MONITOR BLIND FASTENER-LEFT ENGINE PYLON STA 1151 UPPER PYLON TO FUSELAGE ANGLE CRACKED APPROX 1 INCH CUT OUT DAMAGED AREA 2.5 INCH BY 1 INCH. NDT VERIFIED DAMA
- [SDR DALA1112389881](https://openairdocs.org/sdr/DALA1112389881), Feb 21, 2011: CHANNEL. CRACKED. NOSE LANDING GEAR STA 106 LEFT LONG 28 CHANNEL CRACKED ON OTBD END APPROX 1/2 INCH. REMOVED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5. LOCATED, DRILLED AND INSTALL
- [SDR DALA1112249881](https://openairdocs.org/sdr/DALA1112249881), Feb 19, 2011: CHANNEL. CRACKED. LT MLG W/W DOOR INTERIOR SIDE FWD ZEE CHANNEL IS CRACKED AT INBOARD END. REMOVED CHANNEL IAW DC-9 SRM 51-30-2,51-30-5 AND 51-30-6. LOCATED DRILLED AND INSTALLED
- [SDR DALA1111889881](https://openairdocs.org/sdr/DALA1111889881), Feb 17, 2011: SHEAR TIE. CRACKED. STA 1190 L14R SHEAR TIE CLIP CRACKED. REMOVED CRACKED SHEAR TIE CLIP IAW DC9 SRM 51-30-5. RECEIVED MATERIAL FOR NEW CLIP. FABRICATED NEW CLIP IAW DC9 SRM 51-10-
- [SDR DALA1111779881](https://openairdocs.org/sdr/DALA1111779881), Feb 17, 2011: SHEAR TIE. CRACKED. AFT ACCESSORY COMPARTMENT-UPON REMOVAL OF CRACKED CLIP UNDERNEATH FOUND SHEAR TIE CRACKED AT LONG 14R FRAME STA 1190. REMOVED CRACKED/DAMAGED SHEAR TIE IAW DC9 
- [SDR DALA1113119881](https://openairdocs.org/sdr/DALA1113119881), Feb 11, 2011: FRAME. CRACKED. FUSELAGE EXTERIOR AT CANTED FRAME STA 1292 BETWEEN L14L AND L15L SKIN CRACKED. REMOVED EXISTING DOUBLER IAW SRM 51-30-2. REMOVED CRACKED SKIN BY EXTENDING EXIST
- [SDR DALA1112789881](https://openairdocs.org/sdr/DALA1112789881), Feb 10, 2011: SKIN. CRACKED. FORWARD CARGO DOORJAMB, FORWARD UPPER CORNER HAS APPROX 1/8 INCH CRACK AT FASTENER. CUTOUT DAMAGED SECTION OF SKIN IAW DRAWING SR09530117. HFEC INSPECTED CUTOUT
- [SDR DALA1112609881](https://openairdocs.org/sdr/DALA1112609881), Feb 10, 2011: ANGLE. CRACKED. LEFT ENGINE PYLON STA 1116 UPPER PYLON TO FUSELAGE ANGLE CRACKED APPROX 2 INCHES. REMOVED CRACKED ANGLE AND EXISTING SPLICES IAW DC-9 SRM 51-30-2 AND 51-30-5. F
- [SDR DALA1015779881](https://openairdocs.org/sdr/DALA1015779881), Jul 7, 2010: BATTERY PACK. DISCHARGED. DURING LINE CHECK MAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK AT R1 EMERGENCY EXIT SIGN. OPERATIONAL CHECK OF LIGHTS 
- [SDR DALA1015769881](https://openairdocs.org/sdr/DALA1015769881), Jul 7, 2010: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK MAINTENANCE FOUND L1 & R1 EMERGENCY DOOR LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY AT L1 DOOR. OPERATIONAL CHECK OF LIGHTS NOW CHECK GOOD
- [SDR DALA1012119881](https://openairdocs.org/sdr/DALA1012119881), Jun 1, 2010: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS INOP IN ROW 5-8, 19-22, AND 23-26 INOP. MX REPLACED BATTERY PACKS FOR ROWS 19-22 AND USED SPARE BATTERIES FOR ROWS 
- [SDR NWAA094499881](https://openairdocs.org/sdr/NWAA094499881), Dec 28, 2009: STUD. FAILED. DURING PREFLIGHT CHECK, THE PILOT FOUND THAT THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FAILED STUD AND HARDWARE IN THE EXTERIOR EME
- [SDR NWAA092349881](https://openairdocs.org/sdr/NWAA092349881), Jun 17, 2009: RIB. CRACKED. DURING "M" CHECK FOUND CRACK IN RT WING LEADING EDGE RIB FASTENER HOLE AT STA XCW 124. REPAIRED PER EA 98-215902.
- [SDR NWAA084769881](https://openairdocs.org/sdr/NWAA084769881), Oct 25, 2008: BATTERY PACK. DISCHARGED. DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE OR TOO DIM TO BE FUNCTIONAL. MX CHARGED T
- [SDR NWAA085029881](https://openairdocs.org/sdr/NWAA085029881), Oct 9, 2008: O-RING. LEAKING. SHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED STRONG FUEL ODOR IN CABIN. A SLIGHT FUEL ODOR WAS NOTICED IN THE COCKPIT. FLIGHT CREW LANDED AT DESTINATION. MX 
- [SDR NWAA082669881](https://openairdocs.org/sdr/NWAA082669881), Jun 6, 2008: ATTACH ANGLE. CRACKED. DURING LINE CHECK FOUND CRACK IN THE RT DORSAL FIN ATTACH ANGLE AT BS 1266. REPAIRED PER EA 98-213301. (A)
- [SDR NWAA082659881](https://openairdocs.org/sdr/NWAA082659881), Jun 6, 2008: SKIN. CRACKED. DURING LINE CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1266 LT BELOW VERTICAL STABILIZER ATTACH ANGLE. REPAIRED PER EA 98-213119. (A)
- [SDR NWAA080529881](https://openairdocs.org/sdr/NWAA080529881), Feb 14, 2008: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR THE TAIL COMPARTMENT WERE INOPERATIVE. BOTH LEFT AND RIGHT LAMPS WERE CHANGED BUT DID NO
- [SDR 0600979881](https://openairdocs.org/sdr/0600979881), May 13, 2006: LINE. LEAKING. WHILE EN ROUTE TO DESTINATION, THE CREW RECEIVED INDICATIONS THAT ALL OF THE HYDRAULIC FLUID IN THE RIGHT HAND SYSTEM HAD BEEN LOST. COM PROCEDURES WERE COMPLIE
- [SDR 0600149881](https://openairdocs.org/sdr/0600149881), Jan 12, 2006: ROD END. FAILED. WHEN THE LEADING EDGE SLATS WERE SELECTED FOR EXTENSION DURING APPROACH, THE AIRCRAFT ROLLED TO THE RIGHT. CREW NOTED THAT THE BLUE -SLAT EXTEND- LIGHT DID NOT 
- [SDR 0600099881](https://openairdocs.org/sdr/0600099881), Jan 9, 2006: DUCT. LOOSE. WHEN THE LEADING EDGE SLATS WERE SELECTED FOR EXTENSION DURING APPROACH, THE AIRCRAFT ABRUPTLY ROLLED TO THE RIGHT AND THE -SLAT DISAGREE- LIGHT MOMENTARILY ILL
- [SDR 0500989881](https://openairdocs.org/sdr/0500989881), Jul 5, 2005: PACKING. LEAKING. WHILE INBOUND FOR LANDING AT MYR, THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO AND THE PRESSURE DROPPED. COM PROCEDURES WERE COMPLIED WITH AND THE RIGH
- [SDR 0500739881](https://openairdocs.org/sdr/0500739881), May 13, 2005: O-RING. WORN. DURING APPROACH FOR LANDING AT DTW, THE CREW NOTICED THAT THE LEFT HYDRAULIC SYSTEM FLUID DROPPED TO ZERO QUANTITY INDICATION. COMPLIED WITH COM PROCEDURES AND 
- [SDR 0204149881](https://openairdocs.org/sdr/0204149881), Dec 22, 2002: ENGINE. MALFUNCTIONED. CLIMBING THROUGH 8000 FEET, MASTER CAUTION ILLUMINATED. ENGINE NR 1 OIL QUANTITY WAS ZERO AND OIL PRESSURE LIGHT WAS ILLUMINATED. ENGINE NR 1 WAS SHUTDOWN. FLIG
- [SDR 0203659981](https://openairdocs.org/sdr/0203659981), Oct 22, 2002: STABILIZER. CRACKED. Duting Hck in ATL, a .25" crack was found in the upper plate of the horizontal stabilizer center section. Repaired per EA 98-190787.
- [SDR 0202069881](https://openairdocs.org/sdr/0202069881), Jun 24, 2002: SWITCH. WHILE CRUISING AT ALTITUDE, CREW AND PASSENGERS NOTICED A VERY STRONG RUBBER SMELL IN THE CABIN AND COCKPIT. ALSO, THERE WAS EXCESSIVE HEAT COMING FROM OVERHEAD
- [SDR 0003759881](https://openairdocs.org/sdr/0003759881), Oct 6, 2000: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, FOUND EMERGENCY LIGHT IN AFT CEILING AND TAIL CONE RELEASE HANDLE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMA
- [SDR 0003189881](https://openairdocs.org/sdr/0003189881), Sep 10, 2000: BULKHEAD. CRACKED. TAIL INTERIOR- CRACKED LIGHTENING HOLE IN WEB OF LEFT PYLON BULKHEAD AT STA 1209 BETWEEN L11 AND L14. CUT OUT DAMAGED WEB, DRILLED REPLACEMENT WEB FABRICATED DO
- [SDR 0000749881](https://openairdocs.org/sdr/0000749881), Apr 2, 2000: WARNING LIGHT. ILLUMINATED. THE LEFT ENGINE REVERSER UNLOCK LIGHT INDICATION ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED AT 101 KNOTS. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. M
- [SDR 9901059881](https://openairdocs.org/sdr/9901059881), Mar 17, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTING IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHEC
- [SDR 9808279881](https://openairdocs.org/sdr/9808279881), May 4, 1998: WINDSHIELD. CRACKED. DURING CLIMB THROUGH FL250, 280 KIAS, CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 
- [SDR 9721169881](https://openairdocs.org/sdr/9721169881), Nov 11, 1997: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 2 AND 4. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK B5-24, OPERATIONAL CHECK NORMAL.
- [SDR 9718269881](https://openairdocs.org/sdr/9718269881), Sep 27, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND 3 EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD.
- [SDR 9706469881](https://openairdocs.org/sdr/9706469881), Mar 26, 1997: SLIDE. LOW PRESSURE. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE SLIDE PRESSURE LOW. REPLACED SLIDE.
- [SDR 9622399881](https://openairdocs.org/sdr/9622399881), Oct 17, 1996: SWITCH. MALFUNCTIONED. TAKEOFF WARNING HORN SOUNDED AS TAKEOFF POWER WAS APPLIED. ABORTED TAKEOFF AT 5 KTS AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT SLAT SWITCH, OPERAT
- [SDR 9611979881](https://openairdocs.org/sdr/9611979881), May 30, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND AFT ENTRY DOOR AND TAIL CONE EMERGENCY LIGHTS OUT. REPLACED BATTERIES AND PACKS, OPERATIONAL CHECK OK.
- [SDR 9514439881](https://openairdocs.org/sdr/9514439881), Sep 21, 1995: TORQUE LINKS. FAILED. DURING TAKEOFF ROLL, EXCESSIVE VIBRATION FROM NOSE GEAR AREA WAS EXPERIENCED. ABORTED TAKEOFF AT APPROXIMATELY 30 KNOTS AND RETURNED TO GATE. REPLACED THE UPPER
- [SDR 9510069881](https://openairdocs.org/sdr/9510069881), Jun 24, 1995: CLIPS. OUT OF ADJUST. DURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE TAILCONE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS.
- [SDR 9508719881](https://openairdocs.org/sdr/9508719881), May 30, 1995: TIRES. OUT OF ROUND. ABORTED TAKEOFF AT 60 KNOTS DUE TO EXCESSIVE VIBRATION FROM NOSE GEAR AREA. FOUND BOTH NOSE TIRES WITH OUT OF ROUND CONDITION. REPLACED BOTH TIRES. AIRCRAFT RET

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG11IA043](https://openairdocs.org/ntsb/ENG11IA043), Aug 6, 2011: Mcdonnell Douglas DC-9-51 (N676MC), Atlanta, GA, incident, minor damage. Probable cause: The probable cause of the No. 2 engine failure and subsequent aborted takeoff was the high cycle fatigue failure of a fan blade near the blade root that resulted in extensive low pressure compressor…

## FAA accident and incident reports (2)

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 20020624021139I](https://openairdocs.org/incident/20020624021139I), Jun 24, 2002: Doug DC951 (N676MC), Grand Rapids, MI. (-23) On June 24, 2002, at 1450Z, northwest airline, DC-9-51, N676MC, experienced a rubber smell in cabin and cockpit and was very strong with excessive heat…
- [Incident 20011116032879I](https://openairdocs.org/incident/20011116032879I), Nov 16, 2001: Doug DC951 (N676MC), Kansas City, MO. (-23) On November 16, 2001 at approx. 1628 CST an northwest airlines DC9-51 flight 211 reported to ATC that it had a flap problem. The aircraft executed a…

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