# N930RC: 1965 Douglas DC-9-14, registration cancelled 2003-06-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 20, 2003 - Status when cancelled: Triennial form not returned - Airframe: [Douglas DC-9-14](https://openairdocs.org/model/douglas-dc-9-14) (registry code 3022034) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 45729 - Year built: 1965 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: February 27, 1970 - Certificate issued: December 22, 1986 - Last registry action: January 16, 2001 - Mode S code: ACE723 - Owner when cancelled: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC) - Location: [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul) - Owner type: Corporation - Owner's area on the map: 44.8873° N, 93.1924° W: Placed by OpenAirDocs at the center of ZIP code 55111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N930RC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930RC - Page: https://openairdocs.org/deregistered/N930RC-2003-06-20 From the FAA registry file of October 28, 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 Douglas DC-9-14: https://openairdocs.org/model/douglas-dc-9-14.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0202359140](https://openairdocs.org/sdr/0202359140), Jun 24, 2002: DUCT. DISCONNECTED. AT 14,000 FEET, THE CABIN PRESSURE ANNUNCIATOR ILLUMINATED. CABIN ALTITUDE WAS 10,000 FEET. VERY SOON AFTER THE WARNING LIGHT CAME ON AND CABIN WENT TO 15,000 F - [SDR 0101399140](https://openairdocs.org/sdr/0101399140), Apr 11, 2001: CARBON SEAL. LEAKING. AIRCRAFT DIVERTED TO MSP DUE LOSS OF OIL QUANTITY. DURING CRUISE, THE RIGHT ENGINE OIL QUANTITY STEADILY DROPPED FROM 16 QTS TO 0 QTS WHILE THE OIL TEMPERATURE - [SDR 0001409140](https://openairdocs.org/sdr/0001409140), Apr 17, 2000: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY ESCAPE LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 0001399140](https://openairdocs.org/sdr/0001399140), Apr 17, 2000: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9905029140](https://openairdocs.org/sdr/9905029140), Nov 14, 1999: ANGLE. PITTED. DURING M-CHECK, FOUND LEFT LEADING EDGE ATTACH ANGLE FOR LEADING EDGE NR 6321 PITTED. REPAIRED PER EA 91-169335. - [SDR 9904129140](https://openairdocs.org/sdr/9904129140), Oct 4, 1999: BATTERIES. DISCHARGED. TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9902899140](https://openairdocs.org/sdr/9902899140), Jul 12, 1999: BATTERIES. DISCHARGED. DURING PERIODIC CHECK, TAIL COMPARTMENT CATWALK EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9901759140](https://openairdocs.org/sdr/9901759140), May 19, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9900019140](https://openairdocs.org/sdr/9900019140), Jan 1, 1999: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9721809140](https://openairdocs.org/sdr/9721809140), Nov 19, 1997: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 8 THROUGH 13. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK OK. - [SDR 9718149140](https://openairdocs.org/sdr/9718149140), Sep 28, 1997: VOR RECEIVER. INOPERATIVE. DURING CLIMB, THE NR 2 VOR/LOC FLAG APPEARED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 VOR RECEIVER, OPERATIONAL CHECK GOOD. - [SDR 9714819140](https://openairdocs.org/sdr/9714819140), Aug 3, 1997: BUNGEE CYL. MALFUNCTIONED. DURING DESCENT UPON INITIAL GEAR EXTENSION, GREEN NOSE GEAR LIGHT FAILED TO ILLUMINATE. ASSOCIATED RED UNSAFE LIGHT DID NOT ILLUMINATE. AFTER THIRD CYCLE OF GEA - [SDR 9714709140](https://openairdocs.org/sdr/9714709140), Jul 27, 1997: CONTROLLER. FAILED. AT FL350, CABIN PRESSURE BEGAN TO CLIMB AT APPROXIMATELY 200 FPM. AT 10,000 FEET MASKS DEPLOYED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND CONTINUED TO CM - [SDR 9712299140](https://openairdocs.org/sdr/9712299140), Jun 22, 1997: RADAR TR UNIT. FAILED. RADAR BECAME INOPERATIVE AFTER TAKEOFF. THERE WAS NO PAINTING OR TEST PATTERN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FLIGHT RETURNED TO MSP AND LA - [SDR 9710169140](https://openairdocs.org/sdr/9710169140), May 26, 1997: SWITCH. FAILED. ON APPROACH UPON GEAR EXTENSION, THE GREEN NOSE GEAR LIGHT DID NOT ILLUMINATE. FOLLOWED COM PROCEDURES. RECYCLED GEAR AND RECEIVED NORMAL INDICATIONS. FLIGHT LA - [SDR 9709299140](https://openairdocs.org/sdr/9709299140), May 11, 1997: WIRE. BROKEN. DURING APPROACH, NO RED TRANSITION LIGHT ON RIGHT GEAR AND NO GREEN DOWN LIGHT ON NOSE GEAR. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOU - [SDR 9707769140](https://openairdocs.org/sdr/9707769140), Apr 4, 1997: CONNECTOR. LOOSE. NOSE GEAR DOWN AND LOCKED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR WITH SAME RESULT. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. - [SDR 9706129140](https://openairdocs.org/sdr/9706129140), Mar 22, 1997: UPLIMIT SWITCH. MALFUNCTIONED. DURING APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND CHANGED BULBS WITH SAME RESULTS. VISUAL - [SDR 9704869140](https://openairdocs.org/sdr/9704869140), Mar 7, 1997: CLIPS. OUT OF ADJUST. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK. - [SDR 9627449140](https://openairdocs.org/sdr/9627449140), Dec 26, 1996: BUNGEE CYLINDER. FAILED. DURING CLIMBOUT, THE NOSE GEAR HAD TO BE RECYCLED TO GET GREEN INDICATION. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR BUNGEE CYLIND - [SDR 9626999140](https://openairdocs.org/sdr/9626999140), Dec 24, 1996: INDICATION. MALFUNCTIONED. DURING DESCENT UPON GEAR EXTENSION, NOSE WHEEL GREEN LIGHT WOULD NOT ILLUMINATE. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE. RECYCLED GEAR AND GREEN ILLUMINAT - [SDR 9624589140](https://openairdocs.org/sdr/9624589140), Nov 12, 1996: BULKHEAD PANEL. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 105 AT THE LEFT INBOARD AND OUTBOARD VERTICAL BEAM FITTINGS AND - [SDR 9623979140](https://openairdocs.org/sdr/9623979140), Nov 8, 1996: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTS FAILED 10 MINUTE TEST. INSTALLED NEW BATTERIES IN BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9623879140](https://openairdocs.org/sdr/9623879140), Nov 6, 1996: TRAP PANEL. CRACKED. DURING H-CHECK, FOUND A 3 INCH CRACK IN THE LEFT MAIN LANDING GEAR WHEEL WELL TRAPEZOIDAL PANEL ON THE UPPER OUTBOARD FLANGE. REPAIRED PER SRM 57-09. - [SDR 9623839140](https://openairdocs.org/sdr/9623839140), Nov 4, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND THE LONGERON 28L END FITTING CRACKED AT FS 490. REPLACED FITTING PER SRM 51-30-2, 51-30-5. - [SDR 9623819140](https://openairdocs.org/sdr/9623819140), Oct 31, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND CRACKS IN BOTH THE LONGERON 26L AND 26R END FITTINGS AT FS 491. REPLACED FITTINGS PER SRM 51-30-5. - [SDR 9617179140](https://openairdocs.org/sdr/9617179140), Aug 6, 1996: LIGHT. INOPERATIVE. DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9610519140](https://openairdocs.org/sdr/9610519140), May 13, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND INTERIOR TAIL CONE EMERGENCY SLIDE LIGHTS AND NACELLE LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IN POWER SUPPLIES B5-49 AND B5-50, OPE - [SDR 9610529140](https://openairdocs.org/sdr/9610529140), May 10, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9610219140](https://openairdocs.org/sdr/9610219140), May 6, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK GOOD. - [SDR 9521169140](https://openairdocs.org/sdr/9521169140), Dec 22, 1995: OIL PRESS TRANS. FAILED. NR 1 ENGINE OIL PRESSURE INDICATION FAILED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE - [SDR 9520399140](https://openairdocs.org/sdr/9520399140), Dec 12, 1995: DOOR. OUT OF ADJUST. FORWARD ACCESSORY COMPARTMENT DOOR WARNING LIGHT ILLUMINATED DURING INITIAL TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. ADJUSTED DOOR. OPERATIONAL C - [SDR 9508769140](https://openairdocs.org/sdr/9508769140), May 26, 1995: RELEASE MECH. OUT OF ADJUST. DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE, CHEC - [SDR 9508429140](https://openairdocs.org/sdr/9508429140), May 20, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL TO MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING FS 585. REPLACED FITTING P/N 9915511-5 PER DWG 991016 - [SDR 9508399140](https://openairdocs.org/sdr/9508399140), May 19, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL FITTING FS 525. REPLACED FITTING PER SRM 51-30-5. - [SDR 9508189140](https://openairdocs.org/sdr/9508189140), May 17, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL KEEL FITTING LONGERON 29L AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5. - [SDR 9508179140](https://openairdocs.org/sdr/9508179140), May 17, 1995: FITTING. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WHEEL WELL LONGERON 30 END FITTING AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5. - [SDR 9508169140](https://openairdocs.org/sdr/9508169140), May 17, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND A .25 CRACK IN THE AFT CARGO DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING. ## Other aircraft with N930RC - [Registered now](https://openairdocs.org/aircraft/N930RC): Socata TBM 700, S/N 1171, built 2017 --- 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.