# N675MC: 1975 Mcdonnell Douglas DC-9-51, registration cancelled 2019-07-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 26, 2019
- Status when cancelled: Third renewal notice
- Airframe: [Mcdonnell Douglas DC-9-51](https://openairdocs.org/model/mcdonnell-douglas-dc-9-51) (registry code 3022051)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 47651
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: April 3, 1985
- Certificate issued: December 31, 2009
- Last registry action: March 31, 2016
- Mode S code: A8EF61
- 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/N675MC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=675MC
- Page: https://openairdocs.org/deregistered/N675MC-2019-07-26

From the FAA registry file of October 31, 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 (101, newest 50)

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

- [SDR DALA13033600880](https://openairdocs.org/sdr/DALA13033600880), Jun 30, 2013: WIRE. BROKEN. SEAT 12DEF EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT SEAT TRACK. REPAIRED WIRE IAW SWPM 20-10. OPS CHECKED GOOD.
- [SDR DALA13033400880](https://openairdocs.org/sdr/DALA13033400880), Jun 30, 2013: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT SIGNS INOPERATIVE. R & R 14A EXIT SIGN BATTERIES IAW AMM, OPS CHECKED NORMAL.
- [SDR DALA13024580880](https://openairdocs.org/sdr/DALA13024580880), May 21, 2013: LAMP. INOPERATIVE. DURING SERVICE CHECK FOUND ESCAPE PATH LIGHTS INOPERATIVE AT ROWS 6-8 AND 3 OF 4 RT SIDE OVERWING EXIT BULBS INOPERATIVE. REPLACED LAMPS AND REPLACED FUSE IAW A
- [SDR DALA13017960880](https://openairdocs.org/sdr/DALA13017960880), Apr 17, 2013: BUSHING. CORRODED. FOUND THAT INBD BUSHING IS OUT OF LIMITS FOR STANDARD BUSHING. RT MLG REF N/R 3. REAMED INBD BORE TO 2.136 FOR .010 OVER BUSHING IAW CMM 57-40-1. REPAIR GENERAL
- [SDR DALA13016970880](https://openairdocs.org/sdr/DALA13016970880), Apr 12, 2013: WIRE. BROKEN. ROW 8B EMERGENCY LIGHTS INOPERATIVE. SPLICED BROKEN WIRE IAW SWPM 20. OPS CHECKED GOOD.
- [SDR DALA13014730880](https://openairdocs.org/sdr/DALA13014730880), Apr 1, 2013: LIGHT. DAMAGED. FWD GALLEY FLOOR LEVEL EMERGENCY EXIT LIGHT DAMAGED. REPLACED LIGHT ASSY IAW AMM 33-53. OPS CHECKED NORMAL.
- [SDR DALA12009910880](https://openairdocs.org/sdr/DALA12009910880), Oct 10, 2012: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED FORWARD RT CABIN, 4" FWD OF STA 160 AT LONGERON R-9 . REMOVED 1 EA GUSSET TO FOM & DAMAGED ANGLE, 4" FWD OF STA 160 AT L-9R, FABRICATED TOP 
- [SDR DALA12009900880](https://openairdocs.org/sdr/DALA12009900880), Oct 9, 2012: STRINGER. CRACKED. FUSELAGE CENTER SECTION FUEL AUXILIARY TANK LOWER STRINGER CRACKED, VIEWED THRU NR 5115A AND RBL 8. DOT 21-02. ACCOMPLISHED PERMANENT REPAIR ON CENTER FUEL AUXI
- [SDR DALA12009420880](https://openairdocs.org/sdr/DALA12009420880), Oct 7, 2012: STRINGER. CRACKED. FUSELAGE CENTER SECTION FUEL AUXILIARY TANK LOWER STRINGER CRACKED VIEWED THRU 5115A & RBL6. CUT OUT DAMAGE IAW SRM 53-05, FIG 46. NDT VERIFY NO CRACKS NOTED AT
- [SDR DALA12009350880](https://openairdocs.org/sdr/DALA12009350880), Oct 4, 2012: FLOOR PANEL. CRACKED. MAIN CABIN ALUMINUM FLOOR PANEL 72A FWD EDGE BENT, BUCKLED, CRACKED BS 734. FABRICATED STIFFENER AND FLOOR PANEL 72, IAW SRM 53-23-0, FIG 5.
- [SDR DALA1166679880](https://openairdocs.org/sdr/DALA1166679880), Nov 29, 2011: SKIN. DAMAGED. WATER LEAKING FROM CEILING AT ROW 25. REPAIRED FUSELAGE SKIN LAP PER ERA 498220-14. (L/P 8497670, 0402767)
- [SDR DALA1161009880](https://openairdocs.org/sdr/DALA1161009880), Oct 29, 2011: O-RING. LEAKING. DURING CLIMBOUT, AFTER A REQUEST FOR INCREASED CABIN TEMP INBACK OF AIRCRAFT, STRONG ODOR (OIL SMELL) ENTERED CABIN, CAUSING FLIGHT ATTENDANTS TO GET SICK. WITH
- [SDR DALA1149509880](https://openairdocs.org/sdr/DALA1149509880), Aug 22, 2011: PIN. LOOSE. MAINTENANCE FOUND SEAT 1C EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE RECONNECTED LOOSE PIN ON SEAT BOTTOM. AIRCRAFT OK FOR SERVICE.
- [SDR DALA1149219880](https://openairdocs.org/sdr/DALA1149219880), Aug 20, 2011: SKIN. CRACKED. CRACK IN SKIN AT CANTED FRAME STA 1303 JUST ABOVE STRINGER 14 LT SIDE. CRACK IS APPROXIMATELY 2.6 INCHES IN LENGTH. REPAIRED CRACK IN SKIN PER DC-9 SRM 53-01 FI
- [SDR DALA1146399880](https://openairdocs.org/sdr/DALA1146399880), Jun 9, 2011: SKIN. GOUGED. RT WING NR 1 SLAT PANEL INBOARD LOWER SKIN WITH GOUGE DUE TO CHAFING WITH L/E (MMO89) BLENDED AREA ON LWR SKIN INBD ON RT WING NR 1 SLAT REF DC9 SRM 57-01 FIG 1
- [SDR DALA1138819880](https://openairdocs.org/sdr/DALA1138819880), Jun 9, 2011: SKIN. DENTED. LT WING AILERON UPPER SKIN WITH SEVERAL (7) DENTS FROM STA XRS 383 TO XRS 509 (MM067) RII: Y. PROCURED SERVICEABLE AILERON. AILERON REMOVED, REPLACED, AND ADJUS
- [SDR DALA1138809880](https://openairdocs.org/sdr/DALA1138809880), Jun 9, 2011: SKIN. WORN. RT SIDE VERTICAL STABILIZER LEADING EDGE TIP SKIN HAS A DEEP WEAR AREA APPROX 22 INCH LONG, CAUSED BY BANANA FAIRING. BLENDED AREA REF SRM 55-01 FIG 1. LOWER BL
- [SDR DALA1138799880](https://openairdocs.org/sdr/DALA1138799880), Jun 9, 2011: SKIN. DENTED. LWR FUSELAGE STA Y351, BETWEEN LONG 29LT AND LONG 30. EXT SKIN WITH DENT. RII: Y. DENT AT FUSELAGE AT STA Y351 BETWEEN LONG 29L AND LONG 30, OUT OF LIMITS. CUT 
- [SDR DALA1138769880](https://openairdocs.org/sdr/DALA1138769880), Jun 9, 2011: FLOOR PANEL. DAMAGED. CABIN FLOOR PNL 37 FWD END TOP SKIN IS CRACKED, DENTED, AND CORRODED. RII: Y. REMOVED EXISTING REPAIR WITH CRACK AT CENTER PORTION OF PANEL 37. FURTHER EVALUATI
- [SDR DALA1138829880](https://openairdocs.org/sdr/DALA1138829880), Jun 8, 2011: SKIN. DAMAGED. RT WING AILERON INBOARD LATERAL FACE SKIN WITH HOLES ELONGATED (MM095). RII: Y PROCURED SERVICIABLE AILERON, AILERON REMOVED, REPLACED AND ADJUSTED. AILERON, RI
- [SDR DALA1138789880](https://openairdocs.org/sdr/DALA1138789880), Jun 2, 2011: SKIN PANEL. DENTED. DURING MCK AT SAT, 9 DENTS WERE FOUND IN THE FUSELAGE SKIN PANEL BETWEEN RT STA 297 - 333 AND L23R - L25R. ACCOMPLISHED PERMANENT REPAIR AT STA 298 TO STA 333.5
- [SDR DALA1137589880](https://openairdocs.org/sdr/DALA1137589880), Jun 2, 2011: STRINGER. CRACKED. STRINGER 17L CRACKED ON RADIUS NEAR UPPER ATTACHMENT FASTENER OF FRAME STA 237. REMOVED DAMAGED SECTION PER SRM 53-02 FIG 18, NDT NO DAMAGE NOTED. FABBED STRING
- [SDR DALA1137349880](https://openairdocs.org/sdr/DALA1137349880), May 31, 2011: CUSP WEB. CRACKED. RT CUSP WEB AT STA 215 LIGHTENING HOLE HAS CRACK. STOP DRILLED CRACK AT FLOOR WEB BY LIGHTENING HOLE STA 218 IAW DC9 SRM 53-01 FIG 2. FABRICATED REPAIR DOUBLER 
- [SDR DALA1137179880](https://openairdocs.org/sdr/DALA1137179880), May 30, 2011: SKIN. DENTED. LOWER FUSELAGE STA Y1115.5 BETWEEN LONGERON 27R AND 28R, EXTERNAL SKIN WITH DENT. COMPLIED WITH PERMANENT REPAIR PER ERA#492136-14 REV ORIGINAL AT FUSELAGE STA 
- [SDR DALA1137089880](https://openairdocs.org/sdr/DALA1137089880), May 28, 2011: WEB. CRACKED. FLOOR WEB HAS CRACK INBD EDGE AT FS STA 261 RBL44. CUT OUT DAMAGED SECTION IAW SRM 51-70-4 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-70-4 FIG 2. IN
- [SDR DALA1137069880](https://openairdocs.org/sdr/DALA1137069880), May 28, 2011: FLOOR PANEL. DAMAGED. PASS CABIN FLOOR PANEL NR 66 WITH ELONGATED HOLES. FABRICATED DOUBLER REPAIR WASHER IAW DC9 SRM 53-05 PG: 12 FIG 3 SRM 51-60-0 PG: 6 FIG 1 AND INSTALLED 3 DOUBL
- [SDR DALA1146299880](https://openairdocs.org/sdr/DALA1146299880), May 27, 2011: SKIN. DENTED. UPPER FUSELAGE STA 251 BETWEEN LONG 17 LT AND 18 LT EXTERNAL SKIN WITH DENT. RII:Y. CUT OUT DAMAGED AREA, NDT NO DAMAGE NOTED, FABRICATED TREATED AND INSTALLED 
- [SDR DALA1136769880](https://openairdocs.org/sdr/DALA1136769880), May 26, 2011: FLOOR PANEL. DAMAGED. PASS CABIN, FLOOR PANEL NR 67B, ELONGATED HOLES OFF A/C PART(JG022). FABRICATED AND INSTALLED 3 DOUBLER REPAIR WASHERS AND PERMACEL TAPE AT PASS CABIN FLOOR PAN
- [SDR DALA1136759880](https://openairdocs.org/sdr/DALA1136759880), May 26, 2011: FLOOR PANEL. DAMAGED. PASS CABIN FLOOR PANEL NR 72B, ELONGATED HOLES OFF A/C PART. FABRICATED AND INSTALLED 3 DOUBLER REPAIR WASHERS AND PERMACEL TAPE IAW AMM DC-9-A-53-20-01-201-925
- [SDR DALA1136749880](https://openairdocs.org/sdr/DALA1136749880), May 26, 2011: FLOOR PANEL. DAMAGED. PASS CABIN FLOOR PANEL NR 29 ELONGATED HOLES. FABRICATED AND INSTALLED 2 DOUBLER REPAIR WASHERS AND PERMACEL TAPE AT PASS CABIN FLOOR PANEL NR 29 IAW AMM DC9-A-
- [SDR DALA1138679880](https://openairdocs.org/sdr/DALA1138679880), May 25, 2011: FLOORBOARD. CORRODED. FLOORBOARD 19 HAS CORROSION (DT-09). REMOVED, FABRICATED, AND INSTALLED FLOORBOARD PANEL SKIN 19 AND 2 EA U-CHANNELS AT FLOORBOARD PANEL 19 IAW DC-9 SRM 53-23-0
- [SDR DALA1138649880](https://openairdocs.org/sdr/DALA1138649880), May 25, 2011: CONNECTOR. BROKEN. MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR BROKEN AT FORWARD LEFT OVERWING EXIT SIDEWALL PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT CONNECTOR. OPE
- [SDR DALA1136739880](https://openairdocs.org/sdr/DALA1136739880), May 24, 2011: FLOORBOARD. DAMAGED. MAIN CABIN FLOOR BOARD NR 23, ENLONGATED HOLES, (5). FABRICATED 5 DOUBLER REPAIR WASHERS IAW DC9 SRM 53-05, PG 12, FIG 3, SRM 51-60-0, FIG 1, AND INSTALLED 5 DO
- [SDR DALA1137119880](https://openairdocs.org/sdr/DALA1137119880), May 19, 2011: VANE. DENTED. LT FLAP, MOVABLE VANE LWR SURFACE HAS A DENT. REPAIRED DENT IAW DC9 SRM 57-03, FIG 11, DC9 SRM 51-70-2, DC9 SRM 57-50-9, ITEM 2, FIG 1A, PG 3, DC9 SRM 57-03, PA
- [SDR DALA1137109880](https://openairdocs.org/sdr/DALA1137109880), May 11, 2011: FLOORBOARD. CRACKED. FLOORBOARD PANEL NR 69 LOWER STIFFENER CRACKED AT SCREW HOLES. REMOVED AND REPLACED LOWER STIFFENER "SUPPORT" ON FLOORBOARD PANEL NR 69 IAW SRM 51-30-2, PG 1-24
- [SDR DALA1137059880](https://openairdocs.org/sdr/DALA1137059880), May 11, 2011: FLOOR PANEL. DAMAGED. PASS CABIN FLOOR PANEL NR 65, ENLONGATED HOLES. FABRICATED DOUBLER REPAIR WASHERS IAW DC9 SRM 53-05, PG 12, FIG 3, SRM 51-60-0, PG 6 FIG 1, AND INSTALLED 3 DOUB
- [SDR DALA1146409880](https://openairdocs.org/sdr/DALA1146409880), May 9, 2011: FLOOR SUPPORT. CORRODED. CORROSION LEVEL: 2. LAV FLOOR SUPPORT FITTING HAS HEAVY CORROSION AND ATTACH BOLT HOLE THREADS DAMAGED IN FITTING, STA 200, LBL 44 RL005. REMOVED AND REPLACED L
- [SDR DALA1138779880](https://openairdocs.org/sdr/DALA1138779880), May 9, 2011: TIE CLIP. CRACKED. TIE CLIP CRACKED AT LT SIDE AFT WALL STA 1136, BELOW LONGERON 14L (MAJOR REPAIR) RII: Y FOUND IN COMING ELONGATED HOLE ON SKIN. EXTERNAL REPAIR DOUBLER AND FILL
- [SDR DALA1137869880](https://openairdocs.org/sdr/DALA1137869880), May 9, 2011: FLOOR PANEL. DAMAGED. CABIN FLOOR PNL 81B TOP SKIN IS TORN OUT AT ATTACH SCREWS. CUT OUT DAMAGE FROM PANEL 81B TOP SKIN IAW SRM 53-05, PTG 10, FIG 1, NO CRACKS NOTED, FABRICATED DOUB
- [SDR DALA1137049880](https://openairdocs.org/sdr/DALA1137049880), May 9, 2011: FLOOR PANEL. DAMAGED. CABIN FLOOR PNL 89 TOP SKIN TORN WITH PULLED THRU SCREW. CUTOUT DAMAGE FROM TOP SKIN AND FABRICATED DOUBLER FROM SHT 7075T6, .040, BATCH #0001590589, IAW SRM 51
- [SDR DALA1137039880](https://openairdocs.org/sdr/DALA1137039880), May 9, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315, RBL-44. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-05, FIG 4B FROM STA 284 TO STA 200, RB
- [SDR DALA1137029880](https://openairdocs.org/sdr/DALA1137029880), May 9, 2011: FLOOR PANEL. CRACKED. CABIN FLOOR PNL 76 TOP SKIN HAS CRACK AT EDGE REMOVED EDGE DAMAGE AT CABIN FLOOR PANEL 76, ORG MAT 18 INCHES LONG, MAT LOSS .35, WITHIN LIMITS IAW SRM 53-01, PG
- [SDR DALA1136729880](https://openairdocs.org/sdr/DALA1136729880), May 9, 2011: FLOOR PANEL. PUNCTURED. CABIN FLOOR PNL 102B HAS PUNCTURES 77-27. CUT OUT DAMAGE ON FLOOR BOARD PANEL NR 102B IAW DC9 SRM 53-05, PG 11, SEC. B-B. FABRICATED AND INSTALLED FLOOR BOARD P
- [SDR DALA1136539880](https://openairdocs.org/sdr/DALA1136539880), May 9, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315,LBL 44. BLENDED CORROSION AT 3 AREAS STA 210, 245, AND 260 ON SEAT TRACK LBL 44- OUT OF LIMITS, PER 
- [SDR DALA1136439880](https://openairdocs.org/sdr/DALA1136439880), May 9, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315,LBL -22. BLENDED OUT CORROSION AREAS OUT LIMITS PER SRM 53-05, FIG 4B, SHEET 1. REMOVED AND REPLACED
- [SDR DALA1136059880](https://openairdocs.org/sdr/DALA1136059880), May 9, 2011: FLOOR PANEL. CORRODED. CABIN FLOOR PNL 36 FWD END TOP SKIN IS CORRODED, 77-40. BLENDED CORROSION AT MAIN CABIN FLOOR PNL 36 FWD END OF TOP SKIN ORG MAT. .040 IAW SRM 53-23-0, FIG 4 OU
- [SDR DALA1136049880](https://openairdocs.org/sdr/DALA1136049880), May 9, 2011: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT ANGLE HAS CORROSION AND LAV ATTACH BOLT SHEARED IN FITTING, FROM STA 200 TO 218, RBL-19. REMOVED AND REPLACED FLOOR SUPPORT ANGLE WITH "EXTRUSION"
- [SDR DALA1135929880](https://openairdocs.org/sdr/DALA1135929880), May 9, 2011: FLOORBOARD. DAMAGED. FLOORBOARD, NR 102C LT AFT CORNER IS BROKEN CUT OUT DAMAGED AREA OF FLOORBOARD NR 102C IAW SRM 51-70-4, FABED (1) EA DOUBLER AND (1) EA SPLICE MAT, IAW SRM 51-7
- [SDR DALA1135619880](https://openairdocs.org/sdr/DALA1135619880), May 9, 2011: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT ANGLE HAS CORROSION FROM BS 160 TO 313 AT BL-0. BLENDED OUT CORROSION MAIN CABIN FLOOR SUPPORT ANGLE AT BL0 BS 160 TO BS 313 IAW SRM 51-10-3
- [SDR DALA1135609880](https://openairdocs.org/sdr/DALA1135609880), May 9, 2011: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT ANGLE HAS CORROSION STA 160 TO 200, LBL 44. BLENDED CORROSION ON FLOOR SUPPORT, OUT OF LIMITS, PER SRM 53-01, FIG 1, SHEET 3. REMOVED AND RE

All 101: https://openairdocs.org/deregistered/N675MC-2019-07-26/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 19950813031479I](https://openairdocs.org/incident/19950813031479I), Aug 13, 1995: Doug DC951 (N675MC), Raleigh-Durham, NC. Loud noise during gear retraction. Vibration. Unsafe nose gear. Landed. Nose gear was locked. Problem unresolved.

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