# N935L: 1974 Douglas DC-9-41, registration cancelled 2008-08-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 27, 2008 - Status when cancelled: Triennial form not returned - Airframe: [Douglas DC-9-41](https://openairdocs.org/model/douglas-dc-9-41) (registry code 302207N) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47603 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 22, 1983 - Certificate issued: July 15, 1999 - Last registry action: July 15, 2008 - Mode S code: ACF936 - Owner when cancelled: [Jet Capital LLC](https://openairdocs.org/faa-owner/JET%20CAPITAL%20LLC) - Location: [Lake Zurich, IL](https://openairdocs.org/faa-place/IL/Lake%20Zurich) - Owner type: Corporation - Owner's area on the map: 42.2016° N, 88.0463° W: Placed by OpenAirDocs at the center of ZIP code 60047, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N935L - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=935L - Page: https://openairdocs.org/deregistered/N935L-2008-08-27 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 Douglas DC-9-41: https://openairdocs.org/model/douglas-dc-9-41.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA9915701](https://openairdocs.org/sdr/TWAA9915701), Nov 17, 1999: POWER SUPPLY. INOP. THE FWD SECTION OF COACH CABIN EGRESS LIGHTING WAS INOPERATIVE. REPLACED THE POWER SUPPLY FOR ROWS 8 THRU 14. CHECK-C 9-28-98 STL. - [SDR TWAA9911301](https://openairdocs.org/sdr/TWAA9911301), Aug 16, 1999: MOTOR. FAILED. LONGITUDINAL TRIM CONTROL WHEEL AND SUITCASE HANDLES INOP. REMOVED AND REPLACED LONGITUDINAL PRIMARY TRIM MOTOR TWA STK NR 80374. OPERATIONAL CHECK WAS NORMAL. - [SDR TWAA9902001](https://openairdocs.org/sdr/TWAA9902001), Feb 2, 1999: BATTERY PACK. DISCHARGED. JUST PRIOR TO DEPARTURE FOUND FLOOR EGRESS LIGHTS AT ROW 15 TO 19 REMAINED ON. REPLACED THE BATTERY PACK. CHECK-C 9-28-98 STL. - [SDR TWAA9814101](https://openairdocs.org/sdr/TWAA9814101), Sep 1, 1998: VALVE. WORN. CREW REPORTED SLOW PRESSURIZATION LOSS IN FLIGHT. REGAINED CABIN PRESSURIZATION IN DESCENT FROM BETWEEN 11000 AND 16000 FT. FLIGHT RETURNED TO STL. REPLACED RT - [SDR TWAA9809503](https://openairdocs.org/sdr/TWAA9809503), Jun 14, 1998: FAN. MALFUNCTIONED. STL - FLT 598 - AFATER TAKEOFF, THE RT PACK FILLED CABIN WITH SMOKE. THE PACK FAN WAS WORKING. RAN BOTH ENGINES AND RT PACK AND PACK FAN. NO SMOKE NOTED. GROUND - [SDR TWAA9714603](https://openairdocs.org/sdr/TWAA9714603), Dec 13, 1997: POWER SUPPLY. INOPERATIVE. STL - FLT 689 - DURING CRUISE, L1 AND R1 DOOR EMERGENCY LIGHTS CAME ON. NO FLOOR LIGHTS. REPLACED POWER SUPPLY AND BATTERIES FOR L1 AND R1 EMERGENCY LIGHTS. MFG - [SDR TWAA9795003](https://openairdocs.org/sdr/TWAA9795003), Aug 14, 1997: TRAP PANEL. CRACKED. STL - RIGHT TRAP PANEL HAS CRACK IN PREVIOUS REPAIR. REMOVED AND REPLACED ENTIRE TRAP PANEL. (M) - [SDR TWAA9795002](https://openairdocs.org/sdr/TWAA9795002), Aug 14, 1997: FLOORBEAM. CRACKED. STL - REPAIRED 3 INCH CRACK IN FLOORBEAM AT STATION 237 BY PULLEY BRACKET. (M) - [SDR TWAA9795001](https://openairdocs.org/sdr/TWAA9795001), Aug 14, 1997: SEAT TRACK. CORROSION. STL - REPLACED NR 4 SEAT TRACK FROM STA 200 TO STA 256 DUE TO CORROSION. (X) - [SDR TWAA9753001](https://openairdocs.org/sdr/TWAA9753001), Apr 25, 1997: PUMP. FAILED. STL - FLT 563 - DURING CRUISE LOST RIGHT HYDRAULIC PRESSURE DUE TO WORN RIGHT ENGINE DRIVEN HYDRAULIC PUMP, MFG P/N 314195, MANUFACTURED BY VICKERS INC. OPERATI - [SDR TWAA9753004](https://openairdocs.org/sdr/TWAA9753004), Apr 17, 1997: LONGERON. CRACKED. STL - DURING SPECIAL CHECK, FOUND A .25 INCH CRACK IN LONGERON 4L, AT BELTRING STATION. INSTALLED REPAIR PER SRM 53-02, FIGURE 2. (M) - [SDR TWAA9731002](https://openairdocs.org/sdr/TWAA9731002), Mar 1, 1997: BATTERY PACK. DISCHARGED. STL - FLT 696 - DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED IN FORWARD CABIN. REMOVED AND REPLACED WEAK BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NO - [SDR 97ZZZM104](https://openairdocs.org/sdr/97ZZZM104), Sep 27, 1996: BATTERY PACK. DISCHARGED. STL - FLT 541 - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BATTERY PACK, MFG P/N 2013-1A. OPERATIONAL - [SDR 96ZZZM1469](https://openairdocs.org/sdr/96ZZZM1469), Sep 27, 1996: BATTERY PACK. DISCHARGED. STL - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BATTERY PACK, MFG P/N 2013-1A. OPERATIONAL CHECK NORM - [SDR 96ZZZM1465](https://openairdocs.org/sdr/96ZZZM1465), Sep 24, 1996: POWER SUPPLY. INOPERATIVE. STL - DURING CRUISE, EGRESS LIGHTING ILLUMINATED. FOUND WEAK BATTERIES IN POWER SUPPLY, MFG P/N 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHE - [SDR 96ZZZX3624](https://openairdocs.org/sdr/96ZZZX3624), May 7, 1996: POWER SUPPLY. INOPERATIVE. STL - FLT 661 - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED EMERGENCY EGRESS LIGHT POWER SUPPLY, MFG PN 5822-2. OPERATIONAL CHECK N - [SDR 96ZZZM655](https://openairdocs.org/sdr/96ZZZM655), Mar 11, 1996: BATTERY PACK. DISCHARGED. STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 THROUGH 19 ILLUMINATED. FOUND LIGHTING SYSTEM BATTERIES, MFG P/N 3350-0026-21, WEAK. REPLACED BATTERIES AND EG - [SDR 96ZZZX305](https://openairdocs.org/sdr/96ZZZX305), Jan 4, 1996: BATTERY PACK. DISCHARGED. STL - FLT 141 - DURING LANDING AND TAXI, THE EGRESS LIGHTS FLICKERED ON AND OFF. FOUND BATTERY PACK, MFG PN 5822-2, WEAK. REPLACED BATTERY PACK AND EGRESS LIGHT - [SDR 95ZZZX3404](https://openairdocs.org/sdr/95ZZZX3404), Jun 4, 1995: JAMB. CRACKED. DURING CHECK C, FOUND A 1.25 INCH RADIAL CRACK AT TOP LEFT SIDE OF AFT VENTRAL DOOR JAMB, RUNNING CIRCUMFERENTIALLY IN RADIUS OF DASH 13 ANGLE. STOP DRILLED PER ## 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 19860525033269I](https://openairdocs.org/incident/19860525033269I), May 25, 1986: Doug DC941 (N935L), Las Vegas, NV, Minor damage. After departure,a section of tire tread was found on runway. Safe landing. Damage to gear door and left engine fan. - [Incident 19860411018679I](https://openairdocs.org/incident/19860411018679I), Apr 11, 1986: Doug DC941 (N935L), St Louis, MO, Minor damage. Vibration after takeoff with rubber remaining on runway. Returned to find tread pieces from main tire on runway. --- 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.