# N762NC: 1976 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: 47710
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 26, 1991
- Certificate issued: December 31, 2009
- Last registry action: April 21, 2016
- Mode S code: AA4A25
- 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/N762NC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=762NC
- Page: https://openairdocs.org/deregistered/N762NC-2018-12-06

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 (197, newest 50)

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

- [SDR DALA13043200853](https://openairdocs.org/sdr/DALA13043200853), Sep 4, 2013: BATTERY PACK. INOPERATIVE. LAST 4 ROWS OF SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERIES IAW AMM 33-52, OPS CHECKED GOOD.
- [SDR DALA13020860853](https://openairdocs.org/sdr/DALA13020860853), May 2, 2013: WIRE. BROKEN. SEAT MOUNTED EMERGENCY LIGHT AT 23DEF INOPERATIVE. FOUND BROKEN WIRE & REPAIRED IAW SPWM 20 AND EWIS. OPS CHECKED GOOD.
- [SDR DALA13009290853](https://openairdocs.org/sdr/DALA13009290853), Feb 24, 2013: LAMP. INOPERATIVE. LAST TWO EMERGENCY LIGHTS ON CATWALK INOPERATIVE. REPLACED LAMPS NEXT TO LAST CATWALK EMERGENCY LIGHT AND REPLACED LIGHT ASSY AT LAST EMERGENCY LIGHT IAW WDM. O
- [SDR DALA12012770853](https://openairdocs.org/sdr/DALA12012770853), Nov 15, 2012: PLACARD. MISSING. RED/WHITE EMERGENCY EXIT SIGN ON OUTSIDE OF COCKPIT DOOR IS MISSING. REPLACED MISSING EXIT SIGN ON COCKPIT DOOR.
- [SDR DALA12004180853](https://openairdocs.org/sdr/DALA12004180853), Aug 1, 2012: STOP FITTING. CRACKED. DETECTED A CRACK ON THE NR 4 AFT DOOR STOP APPROXIMATELY .125 IN LENGTH STARTING AT DOOR STOP HOLE AND EXTENDING FORWARD. REMOVED DAMAGE PER DRAWING SR095302 52
- [SDR DALA12004170853](https://openairdocs.org/sdr/DALA12004170853), Aug 1, 2012: DOOR FRAME. CORRODED. FORWARD CARGO DOOR FRAME LOWER EDGE HAS CORROSION AND IS BULGED. REMOVED AND REPLACED DOOR FRAME IAW SRM 53-05 FIG 44 AND SRM 51-30-2 SRM 51-30-8 .
- [SDR DALA1243449853](https://openairdocs.org/sdr/DALA1243449853), Jul 26, 2012: SKIN. TORN. ON ARRIVAL, FOUND SKIN TORN APPROX 0-12 INCHES FROM LOWER FWD CORNER OF FWD BAGGAGE BIN FWD DOOR FRAME. INSTALLED INTERNAL REPAIR, EXTERNAL REPAIR DOUBLER AND F
- [SDR DALA11000300853](https://openairdocs.org/sdr/DALA11000300853), Oct 11, 2011: CONNECTOR. DIRTY. THE FORWARD AND MIDDLE EMERGENCY EGRESS CATWALK PATH LIGHTS ARE INOP. CLEANED LIGHTING CONNECTORS AND RECONNECTED, CHECKS OK.
- [SDR DALA1146829853](https://openairdocs.org/sdr/DALA1146829853), Aug 2, 2011: PROXIMITY SENSOR. FAULTY. ON APPROACH, GOT A NORMAL GEAR DOWN INDICATION. ON SHORT FINAL, THE RIGHT GEAR RED UNSAFE LIGHT STARTED FLICKERING AND THE GREEN LIGHT FLICKERED. CREW DECLARED 
- [SDR DALA1035439853](https://openairdocs.org/sdr/DALA1035439853), Dec 12, 2010: SKIN. CRACKED. DURING M-CHECK, FOUND FUSELAGE EXTERIOR STA 200 BETWEEN L20L AND L21L SKIN CRACKED AT FASTENER. TRIMMED SKIN CRACKED AREA IAW DWG SR09530219. FABRICATED 4 EA FI
- [SDR DALA1035449853](https://openairdocs.org/sdr/DALA1035449853), Dec 11, 2010: FRAME. CRACKED. DURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT RT SIDE STA 1209 BETWEEN STRINGER 13-14, LARGE CRACK IN WEB. CUTOUT SECTION OF WEB FROM LONGERON 7 TO 14 IAW SRM 
- [SDR DALA1035629853](https://openairdocs.org/sdr/DALA1035629853), Dec 10, 2010: LONGERON. CORRODED. DURING MX, CORROSION WAS FOUND ON LONGERON L17R BETWEEN STA 1136 AND STA 1117. WHEN THE FASTENERS IN THE SKIN PANEL WERE REMOVED, THE FASTENER HOLES WERE ELONGA
- [SDR DALA1035619853](https://openairdocs.org/sdr/DALA1035619853), Dec 9, 2010: SKIN. CRACKED. WHILE ACCOMPLISHING A SID INSP OF PSE 53.09.028, IAW AD2006-21-06, EM5330-01148-01B, A 1.8" LONG CRACK WAS FOUND IN THE SKIN, STA 1247, L1 TO L2R. WORK IAW ER/A
- [SDR DALA1035369853](https://openairdocs.org/sdr/DALA1035369853), Dec 9, 2010: FLOOR PANEL. CORRODED. DURING M-CHECK FOUND COCKPIT FLOOR PANEL NR 14B HAS CORROSION IN SEVERAL PLACES ON TOP OF PANEL. REMOVED AND FABRICATED, INSTALLED NEW PANEL IAW ERA 4861146-14.
- [SDR DALA1035359853](https://openairdocs.org/sdr/DALA1035359853), Dec 9, 2010: FLOOR PANEL. LOOSE. DURING M-CHECK, FOUND MAIN PASSENGER CABIN FLOOR PANEL NR 60C AFT END OLD REPAIR LOOSE. FABRICATED NEW FLOOR PANEL AND HAT CHANNELS IAW ERA 482363-14.
- [SDR DALA1035349853](https://openairdocs.org/sdr/DALA1035349853), Dec 9, 2010: WEB. CHAFED. DURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT LT SIDE STA 1209, STR 5 JUST AFT OF ACTUATOR WEB REPAIR CHAFED THROUGH. REMOVED OLD REPAIR. FABRICATED NEW WEB AN
- [SDR DALA1035109853](https://openairdocs.org/sdr/DALA1035109853), Dec 7, 2010: HINGE. CORRODED. DURING M-CHECK FOUND FWD AIRSTAIR DOOR HINGE AND ATTACH FASTENERS CORRODED. CORROSION WAS REMOVED IAW SRM 51-10-3. ORIG MAT .071 IAW SRM 53-33-0. REMOVED .026 R
- [SDR DALA1035089853](https://openairdocs.org/sdr/DALA1035089853), Dec 7, 2010: CHANNEL. CRACKED. DURING M-CHECK FOUND CABIN FLOOR PANEL NR76 HAS 1EA HAT CHANNEL CRACKED AND 1EA CHAFED THRU FABRICATED NEW PANEL IAW ERA 486157-14. REMOVED HAT CHANNELS FROM PA
- [SDR DALA1035079853](https://openairdocs.org/sdr/DALA1035079853), Dec 7, 2010: CHANNEL. CRACKED. DURING M-CHECK (AD-FAR) AFT ACCY COMPARTMENT-APB RT LOWER CORNER -37 SEAL CHANNEL HAS APPROX 2 INCH CRACK. FABRICATED REPAIR CHANNEL. TREATED AND PRIMED AND INS
- [SDR DALA1034899853](https://openairdocs.org/sdr/DALA1034899853), Dec 6, 2010: SUPPORT ANGLE. CRACKED. DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 750, LBL44 SUPPORT ANGLE ON TOP OF CTR WING TANK IS CRACKED. REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR 
- [SDR DALA1034929855](https://openairdocs.org/sdr/DALA1034929855), Dec 4, 2010: FLOOR PANEL. DAMAGED. DURING M-CHECK, FOUND HOLE IN MAIN PASSENGER CABIN FLOOR PANEL NR98 AT BS1138. REMOVED DAMAGE IAW SRM 51-70-4 FIG 1. 9.2500"X 1.6250" ORIGINAL MATERIAL .020. FA
- [SDR DALA1034869853](https://openairdocs.org/sdr/DALA1034869853), Dec 3, 2010: FLOOR SUPPORT. GOUGED. DURING M-CHECK, FOUND MAIN PASSENGER CABIN LBL 18 TO RBL 18 AFT ENTRY DOORJAMB LOWER FLOOR PANEL SUPPORT ANGLE HAS 2EA GOUGES. R & R BOTTOM SECTION OF FRAME R &
- [SDR DALA1034859853](https://openairdocs.org/sdr/DALA1034859853), Dec 3, 2010: PAN. CORRODED. DURING M-CHECK FOUND AFT CARGO DOOR PAN HAS CORROSION FROM STA 1070-1100. REMOVED AFT CARGO DOOR PAN & WEB AND REPLACED WITH NEW CUSTOMER FURNISHED PARTS IAW DW
- [SDR DALA1034849853](https://openairdocs.org/sdr/DALA1034849853), Dec 3, 2010: STRAP. CORRODED. DURING M-CHECK, FOUND AFT CARGO DOOR PAN WEB FWD OTBD STRAP HAS CORROSION. R & R AFT CARGO DOOR PAN WEB OTBD STRAP GUSSETT AND INSTALLED NEW OTBD STRAP GUSSETT 
- [SDR DALA1034839853](https://openairdocs.org/sdr/DALA1034839853), Dec 3, 2010: STRAP. CORRODED. DURING M-CHECK, FOUND AFT CARGO DOOR PAN WEB AFT INBD STRAP CORRODED. R & R AFT CARGO DOOR PAN WEB AFT INBD STRAP. INSTALLED NEW CUSTOMER FURNISHED PART IAW SRM
- [SDR DALA1034759853](https://openairdocs.org/sdr/DALA1034759853), Dec 2, 2010: STRUCTURE. DAMAGED. DURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT, LT SIDE, BETWEEN CANTED FRAMES 1275 & 1292 UNDER INBD ATTACH POINTS FOR AIRSTAIR RELEASE MOUNT FITTING. PREVIOUS
- [SDR DALA1034549853](https://openairdocs.org/sdr/DALA1034549853), Dec 1, 2010: DOOR. CORRODED. DURING M-CHECK, FOUND FUSELAGE EXTERIOR AIR STAIR DOOR HAS CORROSION ALONG BOTTOM EDGE IN CHANNEL. REMOVED CORROSION FROM DOOR EDGE IN CHANNEL. FOUND TO BE OUT 
- [SDR DALA1034359853](https://openairdocs.org/sdr/DALA1034359853), Nov 30, 2010: SKIN. DAMAGED. DURING M-CHECK FUSELAGE EXTERIOR AFT CARGO DOOR JAMB FWD LOWER CORNER HAS ELONGATED FASTENER HOLE THRU SKIN AND INTERNAL DOUBLERS AND DOOR PAN AND PAN SPLICE HO
- [SDR DALA1034369853](https://openairdocs.org/sdr/DALA1034369853), Nov 30, 2010: INTERCOSTAL. CORRODED. DURING M-CHECK, FOUND FWD CARGO BETWEEN STA 218 AND 237 JUST OTBD OF LT LONG 28 INTERCOSTAL HAS CORROSION AND CRACKS APPROX 1 INCH. REMOVED CORROSION ORIGINAL M
- [SDR DALA1034039853](https://openairdocs.org/sdr/DALA1034039853), Nov 29, 2010: DOUBLER. CRACKED. DURING M-CHECK FOUND CABIN/HORSE SHOE DOUBLER CRACKED FWD SIDE OF STA 712 FRAME AT CUSP WEB. REMOVED CRACKED HORSESHOE DOUBLER AT STA 712 IAW DC9 51-305. DRILLE
- [SDR DALA1033959853](https://openairdocs.org/sdr/DALA1033959853), Nov 29, 2010: ANGLE. CRACKED. DURING M-CHECK FOUND AFT ACC COMPT STA 1209 AT L12L FRAME SHEAR ANGLE CRACKED. REMOVED 5 EA ANGLES AND CRACKED SHEAR TIE BETWEEN LONGERON 10 AND 14 RH STA 1209.
- [SDR DALA1034029853](https://openairdocs.org/sdr/DALA1034029853), Nov 28, 2010: FLOOR PANEL. DAMAGED. DURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 33 STA 351 I/B SIDE HOLE IN SKIN. REMOVED AND RECEIVED NEW FLOOR PANEL AND COUNTERSUNK ALL HOLES INSTALLED
- [SDR DALA1034019853](https://openairdocs.org/sdr/DALA1034019853), Nov 28, 2010: FLOOR PANEL. CRACKED. DURING M=CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 32 CRACKED ON FORWARD INBOARD END. REMOVED CABIN FLOOR PANEL 32. RECEIVED NEW FLOOR PANEL AND COUNTERSUNK 
- [SDR DALA1034009853](https://openairdocs.org/sdr/DALA1034009853), Nov 28, 2010: FLOOR SUPPORT. BROKEN. DURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL SUPPORT STA 617 LBL 22-44 IS BROKEN. FABRICATED 1 EA FLOOR SUPPORT IAW DC9 SRM 53-10-3 FIG 10. INSTALL 1EA
- [SDR DALA1033939853](https://openairdocs.org/sdr/DALA1033939853), Nov 28, 2010: ATTACH ANGLE. CRACKED. DURING M-CHECK, FOUND MAIN PASSENGER CABIN APB LT NR2 FORMER FROM FLOOR LEVEL UPPER OTBD ATTACH ANGLE IS CRACKED. REMOVED CRACKED ATTACH ANGLE IAW DC-9A53-10-25
- [SDR DALA1034059853](https://openairdocs.org/sdr/DALA1034059853), Nov 27, 2010: HINGE. GOUGED. DURING M-CHECK FOUND LT HORIZONTAL STAB T/E NR 6 ELEVATOR HINGE GOUGED AT UPPER ATTACH POINT TO REAR SPAR. REMOVED, REPAIRED AND RE-INSTALLED IAW DC-9 MM 20-16-
- [SDR DALA1034049853](https://openairdocs.org/sdr/DALA1034049853), Nov 27, 2010: CARGO TRACK. CORRODED. DURING M-CHECK FOUND AFT CARGO RT TRACK HAS CORROSION AT STA 1068. RT AFT CARGO TRACK FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-05, LOCATED, DRILLED AND INSTALLE
- [SDR DALA1033999853](https://openairdocs.org/sdr/DALA1033999853), Nov 27, 2010: CUSP WEB. CRACKED. DURING M-CHECK FOUND MAIN CABIN STA 706 LBL 50 CUSP WEB CRACKED CUT OUT DAMAGED AREA .5 X 1.5 IAW DC9 A-53-10-16-801-663A-A. CUSP WEB REMOVED AND REPLACED ON PE
- [SDR DALA1033989853](https://openairdocs.org/sdr/DALA1033989853), Nov 27, 2010: FLOOR PANEL. DAMAGED. DURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 55 FORWARD END SKIN CHAFED AND TORN AROUND FASTENER HOLES. REMOVED CABIN FLOOR PANEL.RECEIVED NEW FLOOR PA
- [SDR DALA1033979853](https://openairdocs.org/sdr/DALA1033979853), Nov 27, 2010: FLOOR SUPPORT. CRACKED. DURING M-CHECK FOUND MAIN CABIN STA 655 LBL 22-42 FLOOR SUPPORT CRACKED. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE IAW DC9 SRM 53-10-3 FIG 10 PG 19 
- [SDR DALA1033969853](https://openairdocs.org/sdr/DALA1033969853), Nov 27, 2010: FLOOR PANEL. CORRODED. DURING M CHECK FOUND MAIN CABIN FLOOR PANEL 77 EXPANSION PANEL HAS CORROSION. REMOVED AND REPLACED EXPANSION CHANNEL IAW DC9 SRM 51-10-4, 51-30-2, 53-01 FIG 1 S
- [SDR DALA1033949853](https://openairdocs.org/sdr/DALA1033949853), Nov 27, 2010: INTERCOSTAL. DAMAGED. DURING M-CHECK FOUND INTERCOSTAL BL-0 FROM STA 218-237 HAS CORROSION AND ELONGATED HOLES. REMOVED AND INSTALLED NEW INTERCOSTAL AT BL 0 BETWEEN STA 218 TO STA 2
- [SDR DALA1035429853](https://openairdocs.org/sdr/DALA1035429853), Nov 26, 2010: SKIN. CRACKED. DURING M-CHECK FOUND VERTICAL STAB, TOP AFT T/E OF RUDDER IS CRACKED, RUDDER ASSY OFF 09-5541-9-9003. UPON EVALUATION VERT STAB TOP AFT T/E OF RUDDER HAS SEPARA
- [SDR DALA1033859853](https://openairdocs.org/sdr/DALA1033859853), Nov 26, 2010: ATTACH ANGLE. CORRODED. DURING M-CHECK FOUND AFT CARGO DOOR PAN DOOR STOP 2 EA INNER ATTACH ANGLES CORRODED. REMOVED 2 EA INNER ATTACH ANGLES FROM AFT CARGO DOOR PAN DOOR STOP IAW DC9 
- [SDR DALA1033849853](https://openairdocs.org/sdr/DALA1033849853), Nov 26, 2010: CARGO TRACK. CORRODED. DURING M-CHECK FOUND FORWARD CARGO COMPT, RT TIE DOWN TRACK CORRODED IN SEVERAL PLACES FROM STATION 218-370. REMOVED AND REPLACED TRACK. SCALLOPED TRACK IAW DRA
- [SDR DALA1033839853](https://openairdocs.org/sdr/DALA1033839853), Nov 26, 2010: WEB. CRACKED. DURING M-CHECK FOUND LEFT PYLON INTERIOR WEB CRACKED IN O/B LOWER RADIUS JUST AFT OF 8TH STAGE DUCT. STOP DRILLED 1 INCH CRACK IAW DC-9 SRM 54-01, INSTALLED 2 E
- [SDR DALA1033599853](https://openairdocs.org/sdr/DALA1033599853), Nov 23, 2010: FRAME. CRACKED. DURING M-CHECK PER AD-FAR MAIN CABIN STA 712 LT MAIN FRAME IS CRACKED INRADIUS BELOW FLOOR. REPAIR PRIOR TO FURTHER FLIGHT REPAIR REQUIRES REQUIRES FAA MANAGER 
- [SDR DALA1033589853](https://openairdocs.org/sdr/DALA1033589853), Nov 23, 2010: FRAME. GOUGED. DURING M-CHECK, FOUND AFT ACCESSORY COMPARTMENT RT SIDE CANTED STA 1243, BETWEEN STRINGER 13-14, FRAME GOUGED ON BOTH SIDES COMPLETELY THROUGH. RT CANTED FRAME 
- [SDR DALA1033579853](https://openairdocs.org/sdr/DALA1033579853), Nov 23, 2010: BULKHEAD. CRACKED. DURING M-CHECK AND IAW AD-FAR AFT ACCY COMPARTMENT-AFT PRESSURE BULKHEAD RT LOWER CORNER HAS CRACK IN 5910130-85 GUSSET AND 5910130-87 DOUBLER, JUST ABOVE -37 S
- [SDR DALA1033569853](https://openairdocs.org/sdr/DALA1033569853), Nov 23, 2010: INTERCOSTAL. CRACKED. DURING M-CHECK FOUND FUSELAGE EXTERIOR BETWEEN WHEEL WELL DOORS STA 792 RBL 10 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW DC9 SRM 51-30-5 FABRICATED, LOCATED,

All 197: https://openairdocs.org/deregistered/N762NC-2018-12-06/reports.md

## FAA accident and incident reports (3)

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 20081215855079I](https://openairdocs.org/incident/20081215855079I), Dec 15, 2008: Doug DC951 (N762NC), Minot, ND, No damage. (-23) During taxi to the ramp after a normal landing, the captain and first officer on northwest airlines flight 1471 had difficulty distinguishing the…
- [Incident 19910318009599I](https://openairdocs.org/incident/19910318009599I), Mar 18, 1991: Doug DC951 (N762NC), Milwaukee, WI. Right engine power loss and compressor stall takeoff. Aborted. Crew observed flames and smoke from engine.
- [Incident 19880418024589I](https://openairdocs.org/incident/19880418024589I), Apr 18, 1988: Doug DC951 (N762NC), Memphis, TN, Minor damage. Powered back from gate then stowed thrust reversers. Late signal to come forward. Rolled backward. Hit aircraft.

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