# N936L: 1985 Mcdonnell Douglas DC-9-34, registration cancelled 2018-01-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 30, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas DC-9-34](https://openairdocs.org/model/mcdonnell-douglas-dc-9-34) (registry code 302207E) - 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: 47711 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 21, 1985 - Certificate issued: November 12, 1999 - Last registry action: March 16, 2010 - Mode S code: ACFCED - Owner when cancelled: [American Aircarriers Support Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRCARRIERS%20SUPPORT%20INC) - Location: [Fort Mill, SC](https://openairdocs.org/faa-place/SC/Fort%20Mill) - Owner type: Corporation - Owner's area on the map: 35.0482° N, 80.9867° W: Placed by OpenAirDocs at the center of ZIP code 29708, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N936L - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936L - Page: https://openairdocs.org/deregistered/N936L-2018-01-30 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-9-34: https://openairdocs.org/model/mcdonnell-douglas-dc-9-34.md ## Service difficulty reports (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA9911101](https://openairdocs.org/sdr/TWAA9911101), Aug 8, 1999: CABLE. FAILED. THE FIRST SECTION OF EGRESS LIGHTS IN THE COACH CABIN WERE INOPERATIVE. REPLACED THE FEEDER STRIP. CHECK-C 6-17-98 STL. - [SDR TWAA9907502](https://openairdocs.org/sdr/TWAA9907502), May 20, 1999: BATTERY PACK. DISCHARGED. DURING PREFLIGHT CHECK, ROW 8-20 EGRESS LIGHTS WERE FOUND INOP. THE PROBLEM WAS LOW BATTERY PACKS. TWO PACKS WERE CHANGED. CHECK -C 06-17-98 STL. - [SDR TWAA9906601](https://openairdocs.org/sdr/TWAA9906601), May 6, 1999: POWER SUPPLY. INOPERATIVE. THE FORWARD OVERHEAD COACH EMERGENCY LIGHTS WERE DIM. REPLACED THE POWER SUPPLY FOR FORWARD OVERHEAD LIGHTS, AND SECURED THE GROUND STUD FOR LIGHT AT ROW 8. CHE - [SDR TWAA9816102](https://openairdocs.org/sdr/TWAA9816102), Oct 5, 1998: DUCT. FAILED. COULD NOT MAINTAIN CABIN PRESSURIZATION AT ALTITUDE. DESCENDED TO 10,000 FT AND PRESSURIZATION NORMAL FOR REMAINDER OF FLIGHT. REPLACED THE LEFT WATER SEPARATOR - [SDR TWAA9714501](https://openairdocs.org/sdr/TWAA9714501), Dec 5, 1997: DOUBLER. CRACKED. STL - DURING LAYOVER, MAINTENANCE FOUND .50 INCH CRACK IN DOUBLER NR 5910130-13 AT L1 DOOR UPPER AFT DOOR JAMB. REPAIRED PER ENGINEERING MAINTENANCE LIASION REC - [SDR TWAA9806006](https://openairdocs.org/sdr/TWAA9806006), Mar 27, 1997: PAN. CRACKED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND THE AFT CARGO COMPT DOOR WITH 2 CRACKS IN DOOR PAN AT FWD LOWER DOOR PRESSURE STOP. FIRST CRACK WAS .5 INCH LONG IN - [SDR TWAA9806005](https://openairdocs.org/sdr/TWAA9806005), Mar 27, 1997: PAN. CRACKED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO COMPT DOOR WITH A CRACK AND TEAR IN INNER PAN AND SEAL PAN AT FWD LOCK INTO PAN RADIUS. INSTALLED DOUBLER - [SDR TWAA9805508](https://openairdocs.org/sdr/TWAA9805508), Mar 27, 1997: SKIN. CRACKED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN AFT LAV SKIN CRACKED AT RIVET LOCATED 6 INCHES FORWARD OF STATION 996, AND 2 IN BELOW LONGERON 15R. TWO EACH C - [SDR TWAA9805502](https://openairdocs.org/sdr/TWAA9805502), Mar 27, 1997: SKIN. CORRODED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT LOWER FUSELAGE SKIN BULGED AND RIVET HEADS POPPED AND PULLED FORWARD OF FS 996 LONGERON 27L. REMOVED CORROSION P - [SDR TWAA9805501](https://openairdocs.org/sdr/TWAA9805501), Mar 27, 1997: SKIN. CORRODED. MCI - DURING OP 15 MAINTENANCE CHECK, FOUND THE AFT LOWER FUSELAGE SKIN BULGED AND RIVET HEADS POPPED AND PULLED FORWARD OF FS 996, LONGERON 28L. REMOVED CORROS - [SDR TWAA9614401](https://openairdocs.org/sdr/TWAA9614401), Nov 21, 1996: POWER SUPPLY. INOPERATIVE. STL - FLT 459 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 10 TO 15. FOUND MALFUNCTIONING POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPL - [SDR 96ZZZM1196](https://openairdocs.org/sdr/96ZZZM1196), Jul 8, 1996: SEAT TRACK. CORRODED. STL - DURING OP-19, FOUND CORROSION ON LEFT INBOARD SEAT TRACK, STATION 200-206. REPLACED SEAT TRACK PER SRM 53-03, PAGE 10G, SHEET 1, FIGURE 4F. (M) - [SDR 96ZZZM906](https://openairdocs.org/sdr/96ZZZM906), Apr 15, 1996: BATTERY PACK. DISCHARGED. STL - FLT 501 - DURING CRUISE EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, OPERATIONAL CHECK NORMAL. (M) - [SDR 95ZZZM381](https://openairdocs.org/sdr/95ZZZM381), Aug 10, 1995: EEL CABLE. FAILED. STL - DURING CRUISE, EGRESS LIGHTS, FROM SEAT ROW 8 TO ROW 14, CAME ON. CYCLED EMERGENCY LIGHT SWITCH TO OFF, TO ARMED, EXTINGUISHED LIGHTS. FOUND OPEN FEEDER C - [SDR 95ZZZW222](https://openairdocs.org/sdr/95ZZZW222), Feb 3, 1995: DOOR JAMB. CRACKED. STL - DURING C-CHECK, FOND A .875 INCH CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD PASSENGER DOOR JAMB. STOP DRILLED CRACK AND REPAIRED PER S/B 53-137. ## FAA accident and incident reports (1) 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 19850721041369I](https://openairdocs.org/incident/19850721041369I), Jul 21, 1985: Doug DC934 (N936L), St Louis, MO, Minor damage. Smoke and fire in compartment panel near galley. Halon used. Bonding strap too long and shorted galley terminal. --- 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.