# N941ML: Mcdonnell Douglas DC-9-32, registration cancelled 2000-11-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 17, 2000
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 47131
- Type of aircraft: Fixed wing multi engine
- Certificate issued: October 31, 2000
- Last registry action: October 31, 2000
- Mode S code: AD11FD
- Owner when cancelled: [Interglobal Inc](https://openairdocs.org/faa-owner/INTERGLOBAL%20INC)
- Location: [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City)
- Owner type: Corporation
- Owner's area on the map: 39.2227° N, 119.7016° W: Placed by OpenAirDocs at the center of ZIP code 89706, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N941ML
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=941ML
- Page: https://openairdocs.org/deregistered/N941ML-2000-11-17

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-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md

## Service difficulty reports (86, newest 50)

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

- [SDR GTIA000263](https://openairdocs.org/sdr/GTIA000263), Jul 22, 2000: SLIDE. DISLODGED. UPON ARRIVAL OF A/C, FLIGHT ATTENDANT OPENED FORWARD L-1 DOOR AND ESCAPE SLIDE FELL TO GROUND. INSPECTED SLIDE PACK, NOTIFIED M/C AND INSPECTION. RE-INSTALLED S
- [SDR GTIA000261](https://openairdocs.org/sdr/GTIA000261), Jul 17, 2000: LIGHT. INOPERATIVE. DTW - FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROW 6 THROUGH ROW 12. FOUND BATTERIES IN EMERGENCY LIGHTING BATTERY PACK FOR ROWS 6-12 LOOSE. RE-SEATED B
- [SDR GTIA000258](https://openairdocs.org/sdr/GTIA000258), Jul 15, 2000: LIGHT. INOPERATIVE. FLT 856 - ACY - EMERGENCY LIGHTS WILL NOT OPERATED IN CABIN. FOUND BATTERY PACK GOOD, EMERGENCY PATH LIGHTING IS NOT PROPERLY MAKING CONTACT, RESECURED IAW MM 3
- [SDR GTIA000194](https://openairdocs.org/sdr/GTIA000194), May 4, 2000: LIGHT. INOPERATIVE. MLG - FLT 403 - EMERGENCY PATH LIGHTING FORWARD OF ROW 7 INOPERABLE. COULD NOT DUPLICATE INOPERATIVE PATH LIGHTING. SYSTEM OPS CHECKED NORMALLY IAW DC-9 MM 33-0
- [SDR GTIA000190](https://openairdocs.org/sdr/GTIA000190), May 2, 2000: LIGHT. INOPERATIVE. MLB - FLT 718 - EMERGENCY FLOOR EXIT LIGHTS INOPERABLE. CLEANED CONNECTION AND BATTERY PACK AT STA 160. OPS CHECK OK IAW MM 33-00. (X)
- [SDR GTIA000095](https://openairdocs.org/sdr/GTIA000095), Feb 10, 2000: LIGHT. OBSTRUCTED. ACY - LAST ROW 24 D, E, F CARPET IS COVERING UP EMERGENCY TRACK LIGHTING. ADJUST CARPET ALONG EMERGENCY FLOOR TRACK LIGHT OPS CHECK GOOD PER DC9 MM 33-53-0. (M)
- [SDR GTIA000094](https://openairdocs.org/sdr/GTIA000094), Feb 10, 2000: COVER. DISPLACED. EMERGENCY TRACK LIGHTING COVER HAS MOVED EXPOSING THE FLOOR WIRES. SECURED FLOOR TRACK THAT SLID FORWARD. CHECKS GOOD PER DC-9 MM 33-53-0. (M)
- [SDR GTIA0000007](https://openairdocs.org/sdr/GTIA0000007), Dec 28, 1999: SWITCH. INOPERATIVE. CLE - FLOOR TRACK LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO 'ON' POSITION IN COCKPIT. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. OPS CHECK GOOD. (M)
- [SDR GTIA9901098](https://openairdocs.org/sdr/GTIA9901098), Aug 28, 1999: CONNECTOR. LOOSE. DTW - CABIN EMERGENCY FLOOR LIGHTS INTERMITTENTLY OFF IN FIRST 6 ROWS. CLEANED AND RESEATED CANNON PLUGS ON BATTERY PACKS PERFORMED OPS CHECK IAW MM 33-50-00. O
- [SDR GTIA9900636](https://openairdocs.org/sdr/GTIA9900636), Apr 1, 1999: BULB. FAILED. MLB - CO-PILOTS EMERGENCY FLOOR LIGHTS DO NOT COME ON. RELAMPED FIRST OFFICERS EMERGENCY FLOOD LIGHTS. OPERATIONS CHECK GOOD PER DC-9 MM 33-11-2. NO OTHER DISCR
- [SDR GTIA9800056](https://openairdocs.org/sdr/GTIA9800056), May 9, 1998: BULB. FAILED. DTW - ROW 8 EMERGENCY TRACK LIGHT INOPERATIVE. RELAMPED ROW 8 EMERGENCY LIGHT OPERATIONAL CHECK GOOD. (M)
- [SDR GTIA9800018](https://openairdocs.org/sdr/GTIA9800018), Jan 23, 1998: BATTERY PACK. DISCHARGED. FOUND ON 'A' CHECK, LEFT EMERGENCY OVERWING EVACUATION LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AS REQUIRED IAW DC-9 MM CHAPTER 33-53-0, OPS CHECKED NORMAL
- [SDR GTIA9700389](https://openairdocs.org/sdr/GTIA9700389), Oct 27, 1997: TIRE. FAILED. ACY - FLT 201 - NR 2 MAIN WHEEL BLEW ON LANDING. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSEMBLY PER MM 32-40-1. (M)
- [SDR GTIA9700382](https://openairdocs.org/sdr/GTIA9700382), Oct 12, 1997: PUSHROD. OUTOF ADJUST. MYR - FLT 1703 - WHEN DEPLOYING FLIGHT SPOILER, A/C ROLLED. FOUND LEFT OUTBOARD SPOILER CONTROL VALVE LINK, PUSHROD OUT OF ADJUSTMENT. ADJUSTED PUSHROD IAW DC-9
- [SDR GTIA9700377](https://openairdocs.org/sdr/GTIA9700377), Sep 26, 1997: FAIRING. LOOSE. ACY - FLT 177 - JUST PASSED DOWNWING WITH FLAPS 25 AND GEAR DOWN NOTICED A PRONOUNCED LOW FREQUENCY VIBRATION. PASSENGERS IN AFT ALSO NOTICED THIS VIBRATION UPO
- [SDR GTIA9700340](https://openairdocs.org/sdr/GTIA9700340), Jul 7, 1997: SOCKET. BROKEN. DTW - ON DAILY FOUND EMERGENCY FLOOR TRACK LIGHT INOP BY SEAT 8A, SOCKET TORN APART. TRANSFERRED TO DMI LOG IAW MEL 33-24, CAT 'C' DMI NR 00711. BOS - INSTALL N
- [SDR GTIA9700321](https://openairdocs.org/sdr/GTIA9700321), Jun 28, 1997: LENS. MISSING. MYR - FLT 1606 - RED LENS MISSING FROM EMERGENCY FLOOR LIGHTING (THIRD FROM THE FRONT). REPLACED MISSING LENSES AND BULB FOR EMERGENCY FLOOR LIGHTING. OPS CHECK
- [SDR GTIA9700320](https://openairdocs.org/sdr/GTIA9700320), Jun 28, 1997: LAMP. MISSING. MYR - FLT 1606 - EMERGENCY LIGHT IN FLOR TRACK LIGHTING (ROW 2) OUT. REPLACED MISSING LAMP AND WHITE COER. OPS CHECK GOOD. (M)
- [SDR GTIA9700288](https://openairdocs.org/sdr/GTIA9700288), May 19, 1997: TIRE. FAILED. EWR - FLT 1600 - NR 2 MAIN TIRE REQUIRED REPLACMENT DUE NR 1 MAIN TIRE BLOWOUT. CARRY OVER ITEM NR 2 TIRE REPLACMENT PER GTIA GMM CH 4 PG 7.5, PARA 2A2. CARRY O
- [SDR GTIA9700278](https://openairdocs.org/sdr/GTIA9700278), Apr 24, 1997: HINGE. BROKEN. DTW - DURING COMPLIANCE WITH AD 91-22-07 (AS PER WORK CARD N-3298) THE LEFT AND RT MLG OUTBOARD DOORS AND HINGES WERE INSPECTED AND THE FOLLOWING DISCREPANCY WA
- [SDR GTIA9700247](https://openairdocs.org/sdr/GTIA9700247), Mar 15, 1997: TIRE. FAILED. EWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLAC
- [SDR 97ZZZM485](https://openairdocs.org/sdr/97ZZZM485), Mar 15, 1997: TIRE. FAILED. EWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLAC
- [SDR GTIA9700246](https://openairdocs.org/sdr/GTIA9700246), Mar 10, 1997: SWITCH. FAILED. MDW - FLT 1704 - AFTER PUSH BACK AT MYR, SPOILER DEPLOYED LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURE AS PER MEL 27-32, CONTINUED FLIGHT AS PER MEL. LIGHT EXTINGU
- [SDR GTIA9700231](https://openairdocs.org/sdr/GTIA9700231), Mar 10, 1997: WARNING LIGHT. ILLUMINATED. MDW - FLT 1701 - AFTER PUSH-BACK AT MYR, SPOILER DEPLOYED, LIGHT ILLUMINATED. ACCOMPLISHED PROCEDURE PER MEL 27-32, CONTINUED FLIGHT PER MEL. LIGHT EXTINGUISHED
- [SDR GTIA9700230](https://openairdocs.org/sdr/GTIA9700230), Mar 10, 1997: PRESS SYSTEM. MALFUNCTIONED. BOS - FLT 248 - ON TAKEOFF, AUTO PORTION OF CABIN PRESSURIZATION DID NOT WORK. MANUAL WORKED WELL FOR REMAINDER OF FLIGHT USING FCOM PROCEDURES. DEFERRED PER ME
- [SDR GTIA9700179](https://openairdocs.org/sdr/GTIA9700179), Mar 3, 1997: WHEEL. RATTLES. DTW - FLT 626 - NOSE WHEEL RATTLES DURING TURNS AT SLOW SPEED. REMOVED BOTH NOSE WHEEL ASSEMBLIES AND INSPECTED. NO FAULTS FOUND. RE-INSTALLED TIRE ASSEMBLIES I
- [SDR GTIA9700184](https://openairdocs.org/sdr/GTIA9700184), Feb 28, 1997: TIRE. FAILED. ACY - FLT 700 - NR 2 MAIN TIRE REQUIRES REPLACMENT DUE TO NR 1 MAIN TIRE BLOW OUT. TRANSFERRED TO CARRY OVER LOG ITEM 0019 IAW GTIA GMM CHAPTER 4, PAGE 7.5, PAR
- [SDR GTIA9700183](https://openairdocs.org/sdr/GTIA9700183), Feb 28, 1997: TIRE. FAILED. ACY - FLT 700 - NR 1 MAIN TIRE EXPERIENCED A BLOW OUT. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW DC9 MM CHAPTER 32. OK FOR SERVICE. (X)
- [SDR GTIA9700164](https://openairdocs.org/sdr/GTIA9700164), Feb 7, 1997: AOA TRANSDUCER. FAILED. DTW - FLT 428 - STALL WARNING FAILURE LIGHT COMES ON INTERMITTENTLY AND SHAKER ACTIVATES. REMOVED AND REPLACED LEFT ANGLE OF ATTACH TRANSDUCER IAW DC-9-MM 94-14
- [SDR GTIA96NK217](https://openairdocs.org/sdr/GTIA96NK217), Nov 5, 1996: TRAPEZOIDAL PNL. CRACKED. DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FROM LEADING EDGE OF PANEL TO SECOND FASTEN
- [SDR GTIA96NK216](https://openairdocs.org/sdr/GTIA96NK216), Nov 5, 1996: TRAPEZOIDAL PNL. CRACKED. DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER S/B 53-182. LEFT TRAP PANEL CRACKED EXTENDED BEYOND EXISTING APPROVED SRM 57-09 FIGURE 6 SHEET 4 REPAI
- [SDR GTIA96NK210](https://openairdocs.org/sdr/GTIA96NK210), Sep 30, 1996: DOOR LOCK. OUT OF ADJUST. REF - CABIN LOG ENTRY NR 1 FROM C/N 8113 EMERGENCY EXIT HATCH ROW 15. AIRCRAFT RIGHT COMES LOOSE ON LANDING. INSPECTED AND ADJUSTED DOOR LOCK BAR IAW DC-9 MM 52
- [SDR GTIANK198](https://openairdocs.org/sdr/GTIANK198), Sep 16, 1996: CONNECTOR. LOOSE. FOUND ON DAILY, NR 1 ENGINE FIRE DETECTOR B-LOOP INOP. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 
- [SDR GTIA96NK201](https://openairdocs.org/sdr/GTIA96NK201), Sep 13, 1996: OXY HOSE. FAILED. DURING CLIMB-OUT OF 18,000 FEET, CREW OXYGEN BOTTLE INDICATED JUST BELOW 1500 PSI. RETURNED TO DTW. SHUT OFF BOTTLE AT 1300 PSI. WITH BOTTLE OFF, OXYGEN STILL D
- [SDR GTIA96NK198](https://openairdocs.org/sdr/GTIA96NK198), Sep 7, 1996: CONNECTOR. INOP. NR 1 ENGINE FIRE DETECTOR B-LOOP INOP, FOUND ON DAILY. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 
- [SDR GTIA96NK191](https://openairdocs.org/sdr/GTIA96NK191), Aug 18, 1996: WIRE. DETERIORATED. RIGHT LANDING GEAR UNSAFE LIGHT FLICKERS INTERMITTENTLY DURING TRANSIT OF LANDING GEAR BOTH IN RETRACTION AND EXTENSION. REPAIRED WIRING AT AND REPLACE CANNON P
- [SDR GTIA96NK184](https://openairdocs.org/sdr/GTIA96NK184), Jul 30, 1996: WIRE. BROKEN. LEFT MAIN INTRANSIT RED LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. FOUND BROKEN WIRES IN LEFT MAIN WHEEL WELL, REPAIRED SAME. (M)
- [SDR 96NK171](https://openairdocs.org/sdr/96NK171), May 24, 1996: FUEL CONTROL. OUT OF ADJUST. LOG PAGE 7770. ABORTED TAKEOFF. ON TAKEOFF, LEFT ENGINE DEVELOPED ONLY 1.8 EPR AT 90 PERCENT N1, RIGHT ENGINE DEVELOPED 1.78 EPR AT 88 PERCENT N1, BOTH POWER LE
- [SDR GTIA96NK001](https://openairdocs.org/sdr/GTIA96NK001), Jan 1, 1996: PAX DOOR. WOULD NOT CLOSE. MAIN CABIN DOOR WOULD NOT CLOSE. CLOSED FORWARD AIR STAIR DOOR IAW DC-9MM 52-11-0. (M)
- [SDR GTIANK018](https://openairdocs.org/sdr/GTIANK018), Nov 21, 1995: LONGERON. CRACKED. DURING C-CHECK, FOUND THE FUSELAGE LONGERON 25 LEFT BETWEEN STATION Y446 TO Y465 CRACKED. REPAIRED THE LONGERON 25 IAW SRM 53-02 FIG 2A. (M)
- [SDR GTIA96NK115](https://openairdocs.org/sdr/GTIA96NK115), Nov 21, 1995: SKIN. CORRODED. DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH LIGHT CORROSION BETWEEN Y756 AND Y775, LONGERON 26 LEFT AND LONGERON 28 LEFT. REMOVED CORROSION AND TREATE
- [SDR GTIA96NK114](https://openairdocs.org/sdr/GTIA96NK114), Nov 21, 1995: SUPPORT. CORRODED. DURING C-CHECK, FOUND AFT CARGO COMPT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y815 BETWEEN LONGERON 27 RT AND 28 RT. REMOVED CORROSION AND TREATED METAL 
- [SDR GTIA96NK113](https://openairdocs.org/sdr/GTIA96NK113), Nov 21, 1995: FLOOR BEAM. CORRODED. DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM Y965.09 WITH CORROSION BETWEEN XO AND PLUS X58. REPAIRED FLOOR BEAM LOWER CHORD AT Y965.09 BETWEEN PLUS X
- [SDR GTIA96NK074](https://openairdocs.org/sdr/GTIA96NK074), Nov 21, 1995: LONGERON. CRACKED. DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION, P/N 592030350, IN BETWEEN STATION Y756 TO STATION Y802 CRACKED. REPLACED LONGERON 30 IAW SRM 51-01 PARA C, S
- [SDR GTIA96NK019](https://openairdocs.org/sdr/GTIA96NK019), Nov 21, 1995: FLOOR BEAM. CORRODED. DURING C-CHECK, FOUND THE PAX/FLOOR BEAM LOWER CHORD AT STATION Y965.09 BETWEEN PLUS X6.7 TO PLUS X18 AND BETWEEN PLUS X21.5 TO PLUS 53.5 CORRODED. REPAIRED PAX
- [SDR GTIA96NK017](https://openairdocs.org/sdr/GTIA96NK017), Nov 21, 1995: FITTING. CORRODED. DURING C-CHECK, FOUND FUSELAGE LONGERON 20 RIGHT END FITTING AT STATION Y996 CORRODED. REPLACED LONGERON 20 END FITTING IAW SRM 51-01 PARAGRAPH C AND SRM 51-10-
- [SDR GTIA96NK016](https://openairdocs.org/sdr/GTIA96NK016), Nov 21, 1995: LONGERON. CORRODED. DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION BETWEEN STATION Y356.7 TO STATION Y415 CORRODED. REPLACED LONGERON 30 SECTION IAW SRM 51-01 PARAGRAPH C, SRM 
- [SDR GTIA96NK015](https://openairdocs.org/sdr/GTIA96NK015), Nov 21, 1995: FRAME. CRACKED. DURING C-CHECK, FOUND RIGHT CENTER OVER WHEEL FRAME, P/N 9919618-2N, AT STATION Y718, CRACKED. REPLACED RIGHT CENTER FRAME IAW MD S/B 53-131 REV 3, DATED FEB 11
- [SDR GTIA96NK014](https://openairdocs.org/sdr/GTIA96NK014), Nov 21, 1995: SKIN. CORRODED. DURING C-CHECK, FOUND FUSELAGE SKIN SECTION AT PITOT STATIC PORT AREA BETWEEN STATION Y451 TO STATION Y465, LONGERONS 23 LEFT TO 26 LEFT CORRODED. REPAIRED FUSE
- [SDR GTIA96NK013](https://openairdocs.org/sdr/GTIA96NK013), Nov 21, 1995: LONGERON. CORRODED. DURING C-CHECK, FOUND FUSELAGE LONGERON 14 LEFT BETWEEN STATION Y1109 TO STATION Y1114 CORRODED. REPAIRED LONGERON 14 LEFT IAW SRM 53-02, FIG 2A. (M)

All 86: https://openairdocs.org/deregistered/N941ML-2000-11-17/reports.md

## 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 19940210004499I](https://openairdocs.org/incident/19940210004499I), Feb 10, 1994: Doug DC932 (N941ML), Albany, NY. Narratvie: on approach to r/w 01 at alb pilot experienced right hand main gear down & locked light not illuminated. Performed emergency checklist, landed on…
- [Incident 19891031055419I](https://openairdocs.org/incident/19891031055419I), Oct 31, 1989: Doug DC932 (N941ML), New York, NY, Minor damage. NR1 engine had fire warning on takeoff. Returned. Engine starter had disintegrated and fuel line had a hole.

## Other aircraft with N941ML

- [Registered now](https://openairdocs.org/aircraft/N941ML): Berthoud Claude RV-8, S/N 81743, built 2003

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