# Service difficulty reports: N195US, cancelled Dec 9, 2025

A list on [N195US, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N195US-2025-12-09.md).

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

- [SDR Y2PA2018072700025](https://openairdocs.org/sdr/Y2PA2018072700025.md): Controller · malfunctioned · Jul 23, 2018 · N195US · Doug DC915F · Cabin Pressure Controller
  > DURING THE DESCENT, WE HAD THE MASTER WARNING LIGHT FOR CABIN PRESSURIZATION. SECURED OUR OXYGEN, RAN THE EMERGENCY PROCEDURE AND DECLARED EMERGENCY. WE REQUIRED A LOWER ALTITUDE AND DIVERT TO MMQT AIRPORT, WHERE THE WEATHER WAS CLEAR, LANDED SAFELY. MX PERFOR
- [SDR Y2PA2016112200027](https://openairdocs.org/sdr/Y2PA2016112200027.md): Skin · corroded · Nov 22, 2016 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND MARKER BEACON ANTENNA SKIN CORRODED. REPAIRED THE SKIN IAW DRAWING 53-16146-1.
- [SDR 7AHR201611210004](https://openairdocs.org/sdr/7AHR201611210004.md): Door Frame · cracked · Nov 21, 2016 · N195US · Doug DC915F · Fuselage Main, Structure
  > 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 MODIFIED SERVICE REWORK DRAWING JO60110 DOUBLERS, DATED 10-27-16, ODA-300064-NM
- [SDR 7AHR2016112100003](https://openairdocs.org/sdr/7AHR2016112100003.md): Cargo Track · damaged · Nov 21, 2016 · N195US · Doug DC915F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Nov 21, 2016 · N195US · Doug DC915F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Door Frame · chafed · Nov 21, 2016 · N195US · Doug DC915F · Standard Practices/Structures
  > 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 SRM 51-30-5 PAGES 12-14.
- [SDR 7AHR201611212069](https://openairdocs.org/sdr/7AHR201611212069.md): Doubler · corroded · Nov 21, 2016 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > 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.md): Gauge · unserviceable · Mar 2, 2014 · N195US · Doug DC915F · Engine Oil Temperature
  > 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 PRECAUTIONARY ENGINE SHUTDOWN. EMERGENCY DECLARED WITH ATC AND RETURN TO DEPARTURE INITIATED. AS POWER L
- [SDR Y2PA20120206004](https://openairdocs.org/sdr/Y2PA20120206004.md): Lamp · inoperative · Feb 6, 2012 · N195US · Doug DC915F · Emergency Lighting
  > 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, CHP. 33-21-27. THE SUBSEQUENT OPS CHECK WAS GOOD AND THE ACFT WAS RETURNED TO SERVICE.
- [SDR FOTR2110410227](https://openairdocs.org/sdr/FOTR2110410227.md): Pan · cracked · Jun 17, 2011 · N195US · Doug DC915F · Cargo/Baggage Doors
  > C2 DOOR PAN IS CRACKED UNDERNEATH NR 2 BEAM END FITTING.
- [SDR FOTR2110410228](https://openairdocs.org/sdr/FOTR2110410228.md): Pan · cracked · Jun 17, 2011 · N195US · Doug DC915F · Cargo/Baggage Doors
  > C2 DOOR PAN IS CRACKED AT NR 5 AFT BEAM END FITTING.
- [SDR FOTR2110410175](https://openairdocs.org/sdr/FOTR2110410175.md): Longeron · corroded · Jun 17, 2011 · N195US · Doug DC915F · Fuselage Main, Longeron/Stringer
  > BS 738 LONGERON 19L IS EXFOLIATED.
- [SDR FOTR2110410017](https://openairdocs.org/sdr/FOTR2110410017.md): Door · cracked · Jun 15, 2011 · N195US · Doug DC915F · Landing Gear Doors
  > 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.md): Skin · corroded · Jun 15, 2011 · N195US · Doug DC915F · Elevator, Plate/Skin
  > CORROSION ON LT ELEVATOR- LOWER OTBD T/E.
- [SDR FOTR2110409916](https://openairdocs.org/sdr/FOTR2110409916.md): Skin · dented · Jun 15, 2011 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > DENT AT RT FUSELAGE SKIN BS 213 JUST BELOW LONGERON 18R.
- [SDR FOTR2110410149](https://openairdocs.org/sdr/FOTR2110410149.md): Frame · cracked · Jun 14, 2011 · N195US · Doug DC915F · Fuselage Main, Frame
  > 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.md): Longeron · cracked · Jun 10, 2011 · N195US · Doug DC915F · Fuselage Main, Longeron/Stringer
  > UPPER CABIN LONGERON 3 RT IS CRACKED AT FS 314.
- [SDR FOTR2110410092](https://openairdocs.org/sdr/FOTR2110410092.md): Longeron · corroded · Jun 10, 2011 · N195US · Doug DC915F · Fuselage Main, Longeron/Stringer
  > E/E, LONGERON 30 IS CORRODED AT SPLICE BETWEEN BS 160-180.
- [SDR FOTR2110410125](https://openairdocs.org/sdr/FOTR2110410125.md): Skin · corroded · Jun 8, 2011 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > BS 948 APPROX LT SIDE, BELOW NR1 PYLON AFT FAIRING, FUSELAGE SKIN HAS A BULGE.
- [SDR FOTR2110410171](https://openairdocs.org/sdr/FOTR2110410171.md): Frame · chafed · Jun 6, 2011 · N195US · Doug DC915F · Fuselage Main, Frame
  > BS 798 FRAME BETWEEN LONGERON 12 AND 13R, HAS A HOLE CHAFED INTO IT.
- [SDR Y2PA200600015](https://openairdocs.org/sdr/Y2PA200600015.md): Structure · corroded · Aug 2, 2006 · N195US · Doug DC915F · Fuselage Main, Structure
  > 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.md): Csd · unserviceable · Feb 13, 2006 · N195US · Doug DC915F · Alternator-Generator Drive
  > RIGHT CSD DISCONNECTED IN FLIGHT DUE TO AN OVERHEAT INDICATION (LIGHT AND TEMP INDICATION) AND GENERATOR LOW FREQUENCY. CREW DECLARED EMERGENCY REQUESTING DIVERSION WHEN CSD TEMPERATURE REMAINED AT REDLINE. DURING THE DESCENT THRU FL300 THE CSD COOLED BELOW
- [SDR ZIAA02004](https://openairdocs.org/sdr/ZIAA02004.md): Doubler · cracked · Nov 8, 2002 · N195US · Doug DC915F · Cargo/Baggage Doors
  > 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 LOWER CARGO DOOR. (M)
- [SDR ZIAA02003](https://openairdocs.org/sdr/ZIAA02003.md): Doubler · cracked · Nov 8, 2002 · N195US · Doug DC915F · Cargo/Baggage Doors
  > 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 LOWER CARGO DOOR EMANATING FROM STEEL HI-LOCK FASTENER HOLE. (M)
- [SDR ZIAA02002](https://openairdocs.org/sdr/ZIAA02002.md): Pan · cracked · Nov 8, 2002 · N195US · Doug DC915F · Cargo/Baggage Doors
  > 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.md): Pan · cracked · Nov 8, 2002 · N195US · Doug DC915F · Cargo/Baggage Doors
  > 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.md): Retract Mech · out of adjust · Jun 22, 1996 · N195US · Doug DC915F · Landing Gear Door Retract Section
  > 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 SCUFFED ON LANDING. ADJUSTED LANDING GEAR PUSH/PULL CABLES, CHECKED DOOR LATCH MECHANISM CLEARANCES. P
- [SDR Y2PA96038](https://openairdocs.org/sdr/Y2PA96038.md): Hinge · out of position · Jun 3, 1996 · N195US · Doug DC915F · Landing Gear Doors
  > 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 32-32-0. (M)
- [SDR Y2PA96037](https://openairdocs.org/sdr/Y2PA96037.md): Position Switch · out of adjust · May 21, 1996 · N195US · Doug DC915F · Landing Gear Position and Warning
  > 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 DOOR UNSAFE LIGHT WENT OUT. THE AIRCRAFT LANDED AT ITS INTENDED DESTINATION AT YIP. CHECKED AND
- [SDR Y2PA96022](https://openairdocs.org/sdr/Y2PA96022.md): Skin Panel · cracked · Apr 8, 1996 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > 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 3-27-96 - MRR NR 96014, AND ON THE RT SIDE OF 198US (SN 47045) ON 4-8-96 - MRR NR 96017. ALL CRACKS
- [SDR Y2PA96016](https://openairdocs.org/sdr/Y2PA96016.md): Door Switch · malfunctioned · Apr 2, 1996 · N195US · Doug DC915F · Landing Gear Position and Warning
  > 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 LEFT AND RIGHT DOOR SWITCH CANNON PLUGS. PART TOTAL CYCLES, 78,574. S/N OFF LT, 9471. S/N NR OFF RT
- [SDR Y2PA96014](https://openairdocs.org/sdr/Y2PA96014.md): Skin · cracked · Mar 27, 1996 · N195US · Doug DC915F · Fuselage Main, Plate/Skin
  > 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 PER USA JET AIRLINES ENGINEERING AUTHORIZATION NR 96-53-02. THESE DATA WERE DER APPROVED BY R. MNA

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N195US' AND deregistration_id = 'N195US-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N195US-2025-12-09/reports

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.