# N195US: 1967 Douglas DC-9-15F, registration cancelled 2025-12-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 9, 2025 - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-15F](https://openairdocs.org/model/douglas-dc-9-15f) (registry code 3022037) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47017 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 20, 1994 - Certificate issued: April 18, 2023 - Last registry action: May 2, 2023 - Mode S code: A17C91 - Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC) - Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) - Owner type: Individual - Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N195US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=195US - Page: https://openairdocs.org/deregistered/N195US-2025-12-09 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 Douglas DC-9-15F: https://openairdocs.org/model/douglas-dc-9-15f.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR Y2PA2018072700025](https://openairdocs.org/sdr/Y2PA2018072700025), Jul 23, 2018: CONTROLLER. MALFUNCTIONED. DURING THE DESCENT, WE HAD THE MASTER WARNING LIGHT FOR CABIN PRESSURIZATION. SECURED OUR OXYGEN, RAN THE EMERGENCY PROCEDURE AND DECLARED EMERGENCY. WE REQUIRE - [SDR Y2PA2016112200027](https://openairdocs.org/sdr/Y2PA2016112200027), Nov 22, 2016: SKIN. CORRODED. DURING C-CHECK, FOUND MARKER BEACON ANTENNA SKIN CORRODED. REPAIRED THE SKIN IAW DRAWING 53-16146-1. - [SDR 7AHR201611210004](https://openairdocs.org/sdr/7AHR201611210004), Nov 21, 2016: DOOR FRAME. CRACKED. CRACK AFT PRESSURE DOOR JAMB RIGHT HAND CORNER 3 INCHES DOWN FROM 9, AND 3 INCHES DOWN FROM JAMB. REPAIRED CRACK IN AFT PRESSURE BULKHEAD SKIN BY INSTALLLING MO - [SDR 7AHR2016112100003](https://openairdocs.org/sdr/7AHR2016112100003), Nov 21, 2016: CARGO TRACK. DAMAGED. CARGO TRACK AT BS 358.5, LBL 54.5 DAMAGED. REPAIRED THE CARGO TRACK IAW DRAWING 53-16142-1 AND SRM 53-05. - [SDR 7AHR2016112100002](https://openairdocs.org/sdr/7AHR2016112100002), Nov 21, 2016: SEAT TRACK. CORRODED. SEVERAL AREAS OF CORROSION ON THE SEAT TRACK BS 294 TO 408. REPAIRED IAW DRAWING 53-16124-1 AND 53-16124-2 PAGES 1-3. - [SDR 7AHR2016112100001](https://openairdocs.org/sdr/7AHR2016112100001), Nov 21, 2016: DOOR FRAME. CHAFED. FWD ENTRY DOOR UPPER AFT FRAME CHAFED. REPAIRED FWD ENTRY DOOR UPPER AFT JAM (SEAL DEPRESSOR) PER FLIGHT VEHICLES CONSULTING DRAWING 53-16151-1, AND DC-9/MD-80 - [SDR 7AHR201611212069](https://openairdocs.org/sdr/7AHR201611212069), Nov 21, 2016: DOUBLER. CORRODED. FWD EDGE OF MARKER BEACON ANTENNA DOUBLER ERRODED. REPAIRED IAW DRAWING 53-16146-1. REPLACED THE ANTENNA IAW MM 34-35-1, STEPS 2.B.(1) TO 2.B.(8). - [SDR Y2PA20140303002](https://openairdocs.org/sdr/Y2PA20140303002), Mar 2, 2014: GAUGE. UNSERVICEABLE. CREW REPORTED, DURING CLIMB THROUGH ABOUT FL230, LEFT OIL TEMPERATURE GAUGE ROSE TO A READING BEYOND THE RED RADIAL. COM PROCEDURE FOLLOWED AND CALL FOR PRECAUT - [SDR Y2PA20120206004](https://openairdocs.org/sdr/Y2PA20120206004), Feb 6, 2012: LAMP. INOPERATIVE. ON PREFLIGHT MX, FOUND THE RT EXIT ROW GROUND EMERGENCY LIGHT INOPERATIVE. MX R & R THE RT EXIT ROW GROUND EMERGENCY LIGHT (LAMP) IAW THE INSTALLATION MANUAL, C - [SDR FOTR2110410227](https://openairdocs.org/sdr/FOTR2110410227), Jun 17, 2011: PAN. CRACKED. C2 DOOR PAN IS CRACKED UNDERNEATH NR 2 BEAM END FITTING. - [SDR FOTR2110410228](https://openairdocs.org/sdr/FOTR2110410228), Jun 17, 2011: PAN. CRACKED. C2 DOOR PAN IS CRACKED AT NR 5 AFT BEAM END FITTING. - [SDR FOTR2110410175](https://openairdocs.org/sdr/FOTR2110410175), Jun 17, 2011: LONGERON. CORRODED. BS 738 LONGERON 19L IS EXFOLIATED. - [SDR FOTR2110410017](https://openairdocs.org/sdr/FOTR2110410017), Jun 15, 2011: DOOR. CRACKED. NLG RT AFT STRUT DOOR, EXTERIOR AFT HINGE CUT OUT SKIN IS BENT IN AND CRACKED AT EDGE. - [SDR FOTR2110410077](https://openairdocs.org/sdr/FOTR2110410077), Jun 15, 2011: SKIN. CORRODED. CORROSION ON LT ELEVATOR- LOWER OTBD T/E. - [SDR FOTR2110409916](https://openairdocs.org/sdr/FOTR2110409916), Jun 15, 2011: SKIN. DENTED. DENT AT RT FUSELAGE SKIN BS 213 JUST BELOW LONGERON 18R. - [SDR FOTR2110410149](https://openairdocs.org/sdr/FOTR2110410149), Jun 14, 2011: FRAME. CRACKED. LEFT FS 642 MAIN FRAME IS CRACKED PT E TO PT D AND PT D TO PT C, ALSO CRACK EXTENDS 2" OTBD FROM POINT D/E AND 1" BELOW PT E AND 2" ABOVE PT D. - [SDR FOTR2110410158](https://openairdocs.org/sdr/FOTR2110410158), Jun 10, 2011: LONGERON. CRACKED. UPPER CABIN LONGERON 3 RT IS CRACKED AT FS 314. - [SDR FOTR2110410092](https://openairdocs.org/sdr/FOTR2110410092), Jun 10, 2011: LONGERON. CORRODED. E/E, LONGERON 30 IS CORRODED AT SPLICE BETWEEN BS 160-180. - [SDR FOTR2110410125](https://openairdocs.org/sdr/FOTR2110410125), Jun 8, 2011: SKIN. CORRODED. BS 948 APPROX LT SIDE, BELOW NR1 PYLON AFT FAIRING, FUSELAGE SKIN HAS A BULGE. - [SDR FOTR2110410171](https://openairdocs.org/sdr/FOTR2110410171), Jun 6, 2011: FRAME. CHAFED. BS 798 FRAME BETWEEN LONGERON 12 AND 13R, HAS A HOLE CHAFED INTO IT. - [SDR Y2PA200600015](https://openairdocs.org/sdr/Y2PA200600015), Aug 2, 2006: STRUCTURE. CORRODED. CORROSION FOUND AT STATION 897, LONGERON 24L TO BE OUT OF LIMITS. REQUIRES ADDITIONAL REVIEW TO DETERMINE REPAIR. - [SDR Y2PA060004](https://openairdocs.org/sdr/Y2PA060004), Feb 13, 2006: CSD. UNSERVICEABLE. RIGHT CSD DISCONNECTED IN FLIGHT DUE TO AN OVERHEAT INDICATION (LIGHT AND TEMP INDICATION) AND GENERATOR LOW FREQUENCY. CREW DECLARED EMERGENCY REQUESTING DIVER - [SDR ZIAA02004](https://openairdocs.org/sdr/ZIAA02004), Nov 8, 2002: DOUBLER. CRACKED. WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, OBSERVED CRACK INDICATION IN REPAIR DOUBLER AT FORWARD SIDE NR 4 BEAM OUTER PAN OF FORWARD - [SDR ZIAA02003](https://openairdocs.org/sdr/ZIAA02003), Nov 8, 2002: DOUBLER. CRACKED. WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, OBSERVED CRACK INDICATION IN REPAIR DOUBLER AT FORWARD SIDE NR 1 BEAM OUTER PAN OF FORWARD - [SDR ZIAA02002](https://openairdocs.org/sdr/ZIAA02002), Nov 8, 2002: PAN. CRACKED. WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, RECEIVED CRACK INDICATION OF .75 INCH IN OUTER PAN RADIUS LOWER AFT STOP. (M) - [SDR ZIAA02001](https://openairdocs.org/sdr/ZIAA02001), Nov 8, 2002: PAN. CRACKED. RECEIVED CRACK INDICATION OF .75 INCH WHILE CONDUCTING EDDY CURRENT INSPECTION OF AFT LOWER CARGO DOOR, OUTER PAN RADIUS AFT SIDE AT BEAM 5. (M) - [SDR Y2PA96044](https://openairdocs.org/sdr/Y2PA96044), Jun 22, 1996: RETRACT MECH. OUT OF ADJUST. GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR DOWN AND LOCKED, FOLLOWED EMERGENCY PROCEDURE 2-32-6. AIRCRAFT FERRIED TO DFW FOR MX BOTH MAIN LANDING GEAR DOORS SCUFF - [SDR Y2PA96038](https://openairdocs.org/sdr/Y2PA96038), Jun 3, 1996: HINGE. OUT OF POSITION. YIP - GEAR DOOR LIGHT ON WITH GEAR DOWN INDICATION. FOUND RIGHT HAND HINGE PIN PROTRUDING OUT OF HINGE. REINSTALLED HINGE PIN. DOOR SYSTEM OPS CHECK IAW MM 32-3 - [SDR Y2PA96037](https://openairdocs.org/sdr/Y2PA96037), May 21, 1996: POSITION SWITCH. OUT OF ADJUST. YIP - INBOUND TO YIP THE LANDING GEAR WAS SELECTED DOWN. INDICATION WAS 3 GREEN LIGHTS WITH A GEAR DOOR UNSAFE LIGHT. THE LANDING GEAR WAS RECYCLED AND THE GEAR - [SDR Y2PA96022](https://openairdocs.org/sdr/Y2PA96022), Apr 8, 1996: SKIN PANEL. CRACKED. YIP - FOUND ONE .25 INCH CRACK IN THE LT SIDE OF NLG WHEELWELL SKIN AT STA 108. NOTE: THIS SAME AREA WAS DISCOVERED CRACKED ON RT SIDE OF 195US (SN 47017) ON 3- - [SDR Y2PA96016](https://openairdocs.org/sdr/Y2PA96016), Apr 2, 1996: DOOR SWITCH. MALFUNCTIONED. YIP - FLT 13336 - ON DESCENT INTO YIP WITH GEAR UP, THE DOOR LIGHT CAME ON AND REMAINED ON. REPLACED LEFT AND RIGHT GEAR DOOR SWITCHES AND REPAIRED WIRING ON LE - [SDR Y2PA96014](https://openairdocs.org/sdr/Y2PA96014), Mar 27, 1996: SKIN. CRACKED. TWO 1 INCH CRACKS IN THE RIGHT SIDE OF THE NLG WHEELWELL SKIN AT STA 108. REMOVED DAMAGED SKIN AREA. FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR DOUBLER P ## 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 CHI99FA102](https://openairdocs.org/ntsb/CHI99FA102), Mar 5, 1999: Douglas DC-9-15F (N195US), Kansas City, MO, substantial damage. Probable cause: ingestion of birds into both engines, resulting in foreign object damage and the subsequent partial power loss to both engines. A factor relating to this accident was the dark night. ## 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. - [Accident 19990304002009A](https://openairdocs.org/incident/19990304002009A), Mar 4, 1999: Doug DC915F (N195US), Kansas City, MO, Substantial damage. (.4)The airplane was cleared to land on runway 19R at the Kansas City International Airport. The first officer said that the airplane was on speed and on… --- 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.