# N782NC: 1980 Mcdonnell Douglas DC-9-51, registration cancelled 2014-11-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 19, 2014
- Status when cancelled: Valid registration
- 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: 48107
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 21, 1980
- Certificate issued: December 31, 2009
- Last registry action: May 1, 2013
- Mode S code: AA9923
- 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/N782NC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=782NC
- Page: https://openairdocs.org/deregistered/N782NC-2014-11-19

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 Mcdonnell Douglas DC-9-51: https://openairdocs.org/model/mcdonnell-douglas-dc-9-51.md

## Service difficulty reports (125, newest 50)

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

- [SDR DALA13056240873](https://openairdocs.org/sdr/DALA13056240873), Oct 27, 2013: FLOORBEAM. DAMAGED. FLOORBEAM AT RBL 4 BS 446 DAMAGED FROM FLOORBOARD. CLEANED AREA IAW SRM 53-05, FIG 20. TREATED AND PRIMED. REPAIRED IAW SRM 53-05.
- [SDR DALA13056230873](https://openairdocs.org/sdr/DALA13056230873), Oct 27, 2013: FLOORBEAM. DAMAGED. FLOORBEAM AT RBL 4 BS 427 DAMAGED FROM FLOORBOARD . CLEANED AREA IAW SRM 53-05, FIG 20A. TREATED AND PRIMED. REPAIRED IAW SRM 53-05.
- [SDR DALA13056220873](https://openairdocs.org/sdr/DALA13056220873), Oct 27, 2013: FLOOR PANEL. DAMAGED. FLOOR HAS SOFT SPOT IN FIRST CLASS AT ROW 4 BETWEEN B & C. REMOVED FLOOR PANEL AND FOUND HAT CHANNEL DAMAGE. REMOVED TWO DAMAGED CHANNELS IAW SRM 51-30-02. FABR
- [SDR DALA13056210873](https://openairdocs.org/sdr/DALA13056210873), Oct 27, 2013: FLOORBEAM. CORRODED. FLOORBEAM RBL 4, BS 408 DAMAGED FROM FLOORBOARD. CLEANED AREA IAW SRM 53-05, FIG 20A. REPAIRED FLOORBEAM IAW SRM 53-05. OK FOR SERVICE.
- [SDR DALA12002300873](https://openairdocs.org/sdr/DALA12002300873), Jun 28, 2012: LANYARD. UNSECURE. DURING LINE CHECK, MAINTENANCE FOUND THE R1 DOOR SLIDE LANYARD TO BE DETACHED FROM THE DOOR SLIDE COVER. MAINTENANCE SECURED THE 1R DOOR SLIDE LANYARD AND RETUR
- [SDR DALA1142569873](https://openairdocs.org/sdr/DALA1142569873), Jul 2, 2011: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL HAS VERY SOFT SPOT IN ISLE AT ROW 11. REMOVED DAMAGED FLOOR PANEL 60C. REPLACED FLOOR PANEL IAW ERA 489362-14.
- [SDR DALA1128399873](https://openairdocs.org/sdr/DALA1128399873), Apr 20, 2011: ACM. OVERSERVICED. ACFT RETURNED TO DEPARTURE DUE TO SMOKE IN THE CABIN. LAV SMOKE DETECTORS SOUNDED AND LT AIR COND SUPPLY TEMP HIGH LIGHT ILLUMINATED. QRH WAS COMPLIED WITH AND 
- [SDR DALA1120659873](https://openairdocs.org/sdr/DALA1120659873), Mar 18, 2011: DOUBLER. CRACKED. FUSELAGE EXTERIOR POTABLE WATER DOOR CUTOUT AFT LOWER CORNER INNER DOUBLER IS CRACKED APPROX .75 INCH. CUT OUT DAMAGED PORTION OF DOUBLER, NO CRACKS NOTED. FABB
- [SDR DALA1119219873](https://openairdocs.org/sdr/DALA1119219873), Mar 15, 2011: SHEAR TIE. CRACKED. THE 1F/62 AFT ACC COMPT STA 1247 BETWEEN L1-L2R SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-11-00 114725. INSTALLED IAW DC9 SRM 53-03 FIG 3.P-1
- [SDR DALA1118749873](https://openairdocs.org/sdr/DALA1118749873), Mar 14, 2011: DOOR FRAME. CORRODED. FWD CARGO DOOR CUTOUT STA 370-427 CORROSION ON WEB REMOVED CORROSION ORIG MAT .040 REMOVED .010 REMAINING .030 OUT OF LIMITS PER SRM 53-01. RECEIVED NEW WITH PA
- [SDR DALA1118529873](https://openairdocs.org/sdr/DALA1118529873), Mar 11, 2011: SKIN. CHAFED. RIGHT WING NR 2 SLAT CENTER SLAT TRACK L/EDGE SKIN CHAFED I/B SIDE OF CUTOUT. BLENDED CHAFE 3"X 2". FOUND TO BE OUT OF LIMITS IAW DC9 SRM 57-01 WITH AN ORIGINAL
- [SDR DALA1117199873](https://openairdocs.org/sdr/DALA1117199873), Mar 10, 2011: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 80 CRACKED ON EDGE. REMOVED DAMAGE ON FLOOR PANEL 1 X 2 INCHES PER ERA 490094-14 AND IAW DC9 SRM 53-01 FIG 4.NDT VERIFIED CRACK IS REMOVE
- [SDR DALA1116419873](https://openairdocs.org/sdr/DALA1116419873), Mar 8, 2011: FLOOR PANEL. CRACKED. MAIN CABIN-FLOOR PANEL, NR 80, AFT END IS CRACKED AND HAS CORROSION AT FASTENER HOLE. REMOVED CORR & CRACK BY CUTTING OUT DAMAGE 11.5" X 5" IAW SRM 51-10-4 & 51
- [SDR DALA1116079873](https://openairdocs.org/sdr/DALA1116079873), Mar 7, 2011: INTERCOSTAL. CRACKED. MAIN CABIN BETWEEN STA 617 AND 636 BL-0 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-30-2. REMOVED CRACK IAW SRM 53-01, FIG 1. HFEC INSP IAW NDT SPM 06-1
- [SDR DALA1115869873](https://openairdocs.org/sdr/DALA1115869873), Mar 5, 2011: VANE. DELAMINATED. LEFT WING CENTER FIXED FLAP VANE DELAMINATED 0N IB END. REMOVED L/WING FLAP CENTER FIXED VANE IAW DC-9 MM 27-51-03. REPLACED FLAP FIXED VANE DUE TO DELAMINATION
- [SDR DALA1115529873](https://openairdocs.org/sdr/DALA1115529873), Mar 4, 2011: FLOOR PANEL. CORRODED. MAIN CABIN METAL FLOOR PANEL NR 21 HAS CORROSION FASTENER HOLES. REMOVED CORROSION FROM FLOOR PANEL IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FABBED FLOOR PAN
- [SDR DALA1115859873](https://openairdocs.org/sdr/DALA1115859873), Mar 3, 2011: VANE. DELAMINATED. RIGHT WING FLAP FIXED VANE NR 2 FROM I/B HAS SOME DELAMINATION ON UPPER SURFACE AT PREVIOUS REPAIR. REPLACED RT WING FLAP NR 2 FIXED VANE WITH NEW SERVICEABLE N
- [SDR DALA1115299873](https://openairdocs.org/sdr/DALA1115299873), Mar 3, 2011: FLOOR PANEL. CORRODED. MAIN CABIN METAL FLOOR PANEL NR 79 HAS CORROSION AROUND EDGES AND 2 EA HAT CHANNELS CRACKED PARTS RACK 22B. REMOVED CORROSION FROM SEVERAL SPOTS IAW SRM 51-10-3
- [SDR DALA1114909873](https://openairdocs.org/sdr/DALA1114909873), Mar 2, 2011: SKIN. DAMAGED. DURING INSPECTION OF LIGHTNING STRIKE MONITORS FOUND AREAS OF PREVIOUS BLENDS ON FASTENER HEADS AND SKIN STA 370 L22R. BLENDED LIGHTNING STRIKE PER DWG NR S6059
- [SDR DALA1114779873](https://openairdocs.org/sdr/DALA1114779873), Mar 2, 2011: FLOOR PANEL. CORRODED. MAIN CABIN METAL FLOOR PANEL NR 17 HAS CORROSION ON SKIN. PARTS RACK 22B. REPLACED FLOOR PANEL NR 17 WITH SERVICEABLE COMPOSITE FLOOR PANEL IAW DC-9 SRM 51-30-1
- [SDR DALA1114769873](https://openairdocs.org/sdr/DALA1114769873), Mar 2, 2011: FLOORBEAM. CRACKED. MAIN PASSENGER CABIN-FLOOR SUPPORT CRACKED STA 617 LBL1 TO LBL18. REMOVED CRACKED FLOOR SUPPORT/ZEE IAW SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT/ZEE FROM .050 
- [SDR DALA1114539873](https://openairdocs.org/sdr/DALA1114539873), Mar 1, 2011: CARGO TRACK. CORRODED. FWD CARGO SURFACE CORROSION ON RT TIE DOWN TRACK FROM STA 427-579. REMOVED CORROSION FROM TIEDOWN TRACK 50 PERCENT MATERIAL LOSS. FABRICATED 2 SPLICES FROM .071
- [SDR DALA1114489873](https://openairdocs.org/sdr/DALA1114489873), Mar 1, 2011: CUSP WEB. CRACKED. MAIN CABIN STA 694 RIGHT SIDE CUSP WEB CRACKED UNDER HORSESHOE COLLAR. REMOVED AND INSTALLED CUSP WEB FROM 693-753 IAW DC9 SRM 51-30-2. FABBED NEW WEB USING 707
- [SDR DALA1114479873](https://openairdocs.org/sdr/DALA1114479873), Mar 1, 2011: CUSP WEB. DAMAGED. FOUND ELONGATED HOLES IN CUSP AT STA 680 RT CUSP AT ZEE SPLICE. REMOVED AND INSTALLED CUSP WEB FROM STA 674-693 IAW SRM 51-30-2. FABRICATED NEW WEB FROM .020 70
- [SDR DALA1114469873](https://openairdocs.org/sdr/DALA1114469873), Mar 1, 2011: ATTACH ANGLE. CRACKED. MAIN PASSENGER CABIN STA 1167 APB RT BOTTOM HORIZ SUPPORT OTBD BOTTOM ATTACH ANGLE CRACKED. REMOVED ATTACH ANGLE FROM HORIZ SUPPORT IAW DC-9 SRM 51-30-02 AND SR
- [SDR DALA1114209873](https://openairdocs.org/sdr/DALA1114209873), Feb 26, 2011: FRAME. CORRODED. STA 579 BET L 26-27 RT CORROSION FOUND UNDER TIE DOWN TRACK ON FRAME. REMOVED CORROSION PER SRM 53-01 FIG 1. MATERIAL LOSS OUT OF LIMITS PER SRM 53-01 FIG 1. RE
- [SDR DALA1114199873](https://openairdocs.org/sdr/DALA1114199873), Feb 26, 2011: ATTACH FITTING. CRACKED. C-1 PIT STATION 579 RT TIE DOWN TRACK ATTACH FITTING CRACKED. REMOVED CRACKED TIE DOWN TRACK ATTACH FITTING IAW SRM 51-30-5. RECEIVED NEW FITTING PN 5956034-557
- [SDR DALA1114189873](https://openairdocs.org/sdr/DALA1114189873), Feb 26, 2011: ATTACH FITTING. CRACKED. C-1 PIT STATION 579 RT TIE DOWN TRACK ATTACH FITTING CRACKED. REMOVED CRACKED TIE DOWN TRACK ATTACH FITTING IAW SRM 51-30-5. RECEIVED NEW FITTING PN 5956034-557
- [SDR DALA1113969873](https://openairdocs.org/sdr/DALA1113969873), Feb 26, 2011: FRAME. CRACKED. AFT ACCESSORY COMPARTMENT STA 1209 L13R FRAME WEB CRACKED. REPAIRED CRACKED WEB AT AFT ACC COMPT IAW DC-9 SRM 51-70-4 FIG 2. REMOVED CRACKED WEB SECTION FROM ST
- [SDR DALA1114029873](https://openairdocs.org/sdr/DALA1114029873), Feb 25, 2011: FLOOR SUPPORT. CORRODED. FORWARD WET AREA STA 256-275 LBL 18 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION 1 INCH BY 3 INCH IAW DC9 SRM 51-10-3 ORIG MATL .060, FOUND TO BE OUT OF LIMIT
- [SDR DALA1114019873](https://openairdocs.org/sdr/DALA1114019873), Feb 25, 2011: FLOOR PANEL. CORRODED. MAIN CABIN METAL FLOOR PANEL NR 99 HAS CORROSION AROUND FASTENER HOLES. PARTS RACK 22B. FABRICATED NEW PANEL FROM .025 7075-T6 SKIN AND HAT CHANNEL PN S2912282F
- [SDR DALA1114009873](https://openairdocs.org/sdr/DALA1114009873), Feb 25, 2011: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 102C CRACKED AT FASTENER HOLE. TRIMMED OUT CRACKED AREA IAW DC-9 SRM 53-05. FABRICATED DOUBLER AND FILLER FROM .032 7075T6 IAW DC-9 SRM 5
- [SDR DALA1113999873](https://openairdocs.org/sdr/DALA1113999873), Feb 25, 2011: SEAT TRACK. DAMAGED. MAIN CABIN-FS 200-240 RBL 22 SEAT TRACK HAS 1 MISDRILLED HOLE. REMOVED DAMAGED SEAT TRACK. RECEIVED NEW SEAT TRACK PN52772660 PO 1022910 IAW DC-9 SRM 53-23 FIG 
- [SDR DALA1113959873](https://openairdocs.org/sdr/DALA1113959873), Feb 25, 2011: FRAME. CHAFED. AFT ACCESSORY COMP LT SIDE CANTED FRAME STA 1139 AFT SIDE HAS DEEP CHAFE. BLENDED CHAFE ON LT SIDE CANTED FRAME IAW DC-9 SRM 51-10-3. ORIG MAT .063 REMOVED OVER
- [SDR DALA1113949873](https://openairdocs.org/sdr/DALA1113949873), Feb 25, 2011: FRAME. CHAFED. AFT ACCESSORY COMP RT SIDE CANTED FRAME STA 1339 AFT SIDE HAS DEEP CHAFE. BLENDED CHAFE AREA ORIG MAT .063 LOST OVER 50 PERCENT MATERIAL. FOUND TO BE OUT OF LIM
- [SDR DALA1113939873](https://openairdocs.org/sdr/DALA1113939873), Feb 25, 2011: LONGERON. CRACKED. MAIN CABIN STA 753 LEFT LONGERON 18 JUST BELOW FLOOR MAIN FRAME CRACKED APPROX 2 INCHES ON FWD SIDE NDT VERIFIED #A2700. REPLACE MAIN FRAME PN 9923407-501N STA 
- [SDR DALA1113729873](https://openairdocs.org/sdr/DALA1113729873), Feb 24, 2011: SUPPORT ANGLE. CRACKED. 6C/161 MAIN CABIN LBL-44 BETWEEN STA 750 AND 770 SUPPORT ANGLE FROM WEB TO CENTER TANK CRACKED AT FASTENERS. REMOVED, ORDERED, AND INSTALLED NEW ANGLE PART NR 5
- [SDR DALA1113719873](https://openairdocs.org/sdr/DALA1113719873), Feb 24, 2011: FLOOR SUPPORT. CRACKED. 6C/299 MAIN CABIN-FS 1136 LBL 1 TO LBL 22 FLOOR SUPPORT IS CRACKED AT INBD END APPROX 1.5 IN. RII: Y. REMOVED DAMAGED ANGLE. FABBED NEW ANGLE IAW DC9 SRM 53-13-
- [SDR DALA1113709873](https://openairdocs.org/sdr/DALA1113709873), Feb 24, 2011: FLOOR PANEL. CORRODED. 6C/203 MAIN CABIN METAL FLOOR PANEL NR 26 HAS CORROSION AROUND FASTENER HOLES PARTS RACK 22B CPCP TASK 58-53303 RII: Y. REMOVED CORROSION FROM END OF PANEL NR 2
- [SDR DALA1113699873](https://openairdocs.org/sdr/DALA1113699873), Feb 24, 2011: CUSP WEB. CRACKED. 6C/194 MAIN CABIN APPROXIMATELY STATION 1134 RT CUSP WEB CRACKED AT AFT HOLE. REMOVED AND REPLACED CUSP WEB STA 1068-1136 IAW DWG SG09537 PN 09-5300-3-3408. REQ
- [SDR DALA1113689873](https://openairdocs.org/sdr/DALA1113689873), Feb 24, 2011: FLOOR PANEL. CRACKED. 6C/298 CABIN FLOOR PANEL NR 98 CRACKED AT AFT INBOARD CORNER. TRIMMED OUT CRACKED AREA 3 1/8 INCH BY 2 3/8 INCH PER DC9 SRM 53-05 FIG 1. HFEC CHECK COMPLETED PE
- [SDR DALA1113679873](https://openairdocs.org/sdr/DALA1113679873), Feb 24, 2011: FLOOR PANEL. CORRODED. 6C/85 COCKPIT FLOOR PANEL NR 14 HAS CORROSION AT AFT END CPCP 46-53303. FABRICATED NEW FLOOR PANEL FROM .025 7075-T6 PO 1120200 AND HAT CHANNELS S2912282 PER ER
- [SDR DALA1113649873](https://openairdocs.org/sdr/DALA1113649873), Feb 24, 2011: FRAME. CORRODED. 1C/30 ACCESS FROM COCKPIT-UPPER FACE OF PRESSURE PANEL BELOW RUDDER PEDAL STA 110 JUNCTURE AT FUSELAGE FRAME HAS CORROSION AT RT END OF ANGLE 4 INCHES BY 3 INCH
- [SDR DALA1113089873](https://openairdocs.org/sdr/DALA1113089873), Feb 23, 2011: SEAT TRACK. CORRODED. MAIN CABIN-FS 218-275 RBL 45 SEAT TRACK HAS CORROSION ON UPPER SURFACE. FOUND CORROSION TO BE BEYOND BLEND OUT LIMITS. REMOVED AND REPLACED TRACK STA RBL 45 AT 
- [SDR DALA1113069873](https://openairdocs.org/sdr/DALA1113069873), Feb 23, 2011: FLOOR PANEL. DAMAGED. MAIN CABIN METAL FLOOR PANEL 60C HAS ELONGATED HOLES AND NO ED PARTS RACK 22B. FABRICATED NEW FLOOR PANEL FROM .025 7075-T6 AND HAT CHANNELS IAW ERA 489362-14.P
- [SDR DALA1112779873](https://openairdocs.org/sdr/DALA1112779873), Feb 22, 2011: FLOOR PANEL. DAMAGED. CABIN COMPOSITE FLOOR PANEL 17 DOES NOT LINE UP WITH HOLES IN A/C. REPAIRED HOLES ON PANEL NR 17 IAW DC9A-53-22-01-801-663A-A AND LOCATED AND DRILLED HOLES IAW 
- [SDR DALA1112409873](https://openairdocs.org/sdr/DALA1112409873), Feb 21, 2011: CUSP WEB. PUNCTURED. MAIN PAX CABIN RT SIDE CUSP WEB HAS 1 PUNCTURE APPROX 1/4 INCH DIA AT FUS FRAME STA 351 RBL 57 IN. REPAIRED PUNCTURE AT STA 351 RBL 57 IAW SRM 53-01 FIG 1 SHEET
- [SDR DALA1112399873](https://openairdocs.org/sdr/DALA1112399873), Feb 21, 2011: LONGERON SPLICE. CORRODED. FORWARD CARGO L29L BETWEEN STA 636 AND 655 LONGERON SPLICE HAS CORROSION. REMOVED CORROSION ON SPLICE. FOUND TO BE OUT OF LIMIT. RECEIVED NEW LONGERON SPLICE ON
- [SDR DALA1112379873](https://openairdocs.org/sdr/DALA1112379873), Feb 21, 2011: LONGERON. CRACKED. MAIN CABIN STATION 484 L17L IS CRACKED. REMOVED DAMAGED L17L STA 455-513. EXISTING SPLICE TO EXISTING SPLICE. REPLACED SECTION L17L WITH NEW. REINSTALLED 2 SPLI
- [SDR DALA1112369873](https://openairdocs.org/sdr/DALA1112369873), Feb 21, 2011: LONGERON. CRACKED. MAIN CABIN STATION 427 L16L IS CRACKED. REMOVED LONGERON SECTION FROM STA 360 TO 434 AT EXISTING SPLICES. INSTALLED NEW SECTION OF LONGERON FROM S2777922-1 AND 

All 125: https://openairdocs.org/deregistered/N782NC-2014-11-19/reports.md

## 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 CEN09LA093](https://openairdocs.org/ntsb/CEN09LA093), Dec 3, 2008: Mcdonnell Douglas DC-9-50 (N782NC), Madison, WI, substantial damage. Probable cause: The collision between the tug and the airplane during towing as a result of sliding on the snow covered runway.

## FAA accident and incident reports (5)

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.

- [Accident 20081203854839A](https://openairdocs.org/incident/20081203854839A), Dec 3, 2008: Doug DC951 (N782NC), Madison, WI, Substantial damage. (-23) On 12/03/08 at about 12:40 CST, northwest airlines (nwa) flight nr 1742 landed in the touchdown zone on runway 36 in Madison, Wisconsin (msn) after…
- [Incident 19960930034209I](https://openairdocs.org/incident/19960930034209I), Sep 30, 1996: Doug DC951 (N782NC), Albany, NY, Substantial damage. Diverted alb due loud bang loss N1 bar and rising EGT left engine. Throttled back. Landed. Turbine blade failure.
- [Incident 19921107053599I](https://openairdocs.org/incident/19921107053599I), Nov 7, 1992: Doug DC951 (N782NC), Atlanta, GA, Minor damage. Left engine failed on climb. Shut down. Returned. Landed safely. Found damage to power turbine section.
- [Incident 19920424015749I](https://openairdocs.org/incident/19920424015749I), Apr 24, 1992: Doug DC951 (N782NC), Miami, FL, Minor damage. On push back from gate aircraft was pushed into a large motorized air conditioning truck. Had two wing walkers.
- [Incident 19900518029979I](https://openairdocs.org/incident/19900518029979I), May 18, 1990: Doug DC951 (N782NC), Buffalo, NY. NR2 hydraulic system lost pressure. Landed safely. Replaced pumps, filters, and a line.

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