# Service difficulty reports: N195AT, cancelled Apr 25, 2006

A list on [N195AT, cancelled Apr 25, 2006](https://openairdocs.org/deregistered/N195AT-2006-04-25.md).

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

- [SDR AMTA200300575](https://openairdocs.org/sdr/AMTA200300575.md): Light · overheated · Apr 29, 2003 · N195AT · Lkheed 1011 · Passenger Compartment Lighting
  > BURNED ELECTRICAL ODOR EMINATING FROM RIGHT FORWARD LAVATORY. FOUND X-FORMER ON OVERHEAD LIGHT ASSEMBLY OVERHEATED. REMOVED AND REPLACED RIGHT FORWARD LAVATORY OVERHEAD LIGHT ASSEMBLY PER MM 33-27-01. OPS CHECK NORMAL. (M)
- [SDR AMTA200300492](https://openairdocs.org/sdr/AMTA200300492.md): Cover · missing · Apr 10, 2003 · N195AT · Lkheed 1011 · Emergency Lighting
  > EGRESS TRACK MISSING COVER PLATES AT SEATS 4 ABC, 5ABC, 4HJK, AND 12HJK. INSTALLED COVER PLATES AS REQUIRED. (M)
- [SDR AMTA200201456](https://openairdocs.org/sdr/AMTA200201456.md): Sign · inoperative · Dec 1, 2002 · N195AT · Lkheed 1011 · Emergency Lighting
  > R-3 DOOR EMERGENCY EXIT SIGN OUT.
- [SDR 2002F00992](https://openairdocs.org/sdr/2002F00992.md): Panel · gouged · Oct 12, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Plate/Skin
  > NR 2 RAM AIR INLET UPPER AND LOWER WEB PANELS GOUGED.
- [SDR AMTA200201286](https://openairdocs.org/sdr/AMTA200201286.md): Stringer · cracked · Oct 10, 2002 · N195AT · Lkheed 1011 · Wing, Longeron/Stringer
  > LT WING, LWR SKIN AT IWS 425.70 AND STR NR 3 HAS A CRACK EXTENDING FWD AND AFT OUT OF THE OUTBD FASTNER OF THE STRINGER, VERIFIED BY EDDY CURRENT. COMPLIED WITH ERA L10-57R-4909. CRACK LENGTH 2.0 INCHES
- [SDR AMTA200201228](https://openairdocs.org/sdr/AMTA200201228.md): Floor Support · corroded · Sep 26, 2002 · N195AT · Lkheed 1011 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT, AT F.S. 1212 FOUND CANTED BULKHEAD SUPPORT WEB CRACKED 2 INCHES AT CORNER OF WEB, WEB LOCATED APPROXIMATELY 2 FEET INBD. FROM RT SIDEWALL. REPAIRED DAMAGE AREA PER ERA L10-53R-4972, REV IR.
- [SDR 2002F01004](https://openairdocs.org/sdr/2002F01004.md): Frame · cracked · Sep 20, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Frame
  > FRAME HAS CRACKS AROUND FWD BOLT HOLE OF FS 1263 FRAME AND PORK CHOP FITTING. REPAIRED PER ERA L10-53R-4927, CRACK LENGTH 0.125, 2 CRACKS. BUTTLINE FROM 113 TO 113.
- [SDR 2002F00994](https://openairdocs.org/sdr/2002F00994.md): Shear Tie · corroded · Sep 8, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Structure
  > FESC SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW SRM 53-12-00, FIG. 805 BS 297, STRINGER 39 TO 40 LT. FROM LBL 46 TO LBL 53, LEVEL 2 CORROSION.
- [SDR AMTA200201241](https://openairdocs.org/sdr/AMTA200201241.md): Longeron · cracked · Sep 2, 2002 · N195AT · Lkheed 1011 · Fuselage Miscellaneous Structure
  > FUSELAGE FORWARD SECTION, LT RAM AIR SCOOP UPPER LONGERON CRACKED AT RADIUS F.S 267 TO F.S 281 W.L 150, 4 INCHES IN LENGTH.
- [SDR 2002F01002](https://openairdocs.org/sdr/2002F01002.md): Structure · damaged · Aug 23, 2002 · N195AT · Lkheed 1011 · Leading Edge Devices
  > HOLE IN 7 RT SLAT OUTBD END LOWER SIDE. REPAIRED AREA IAW SRM 57-51-00. WING STATION, FROM OWS 464.5 TO OWS 464.5
- [SDR AMTA200201083](https://openairdocs.org/sdr/AMTA200201083.md): Bulkhead · corroded · Aug 21, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Bulkhead
  > FWD FUSELAGE SECTION, STA 328 PRESSURE BULKHEAD RBL 24 IN FESC 8 INCHES ABOVE SKIN FLOOR HAS EXFOLATION CORROSION ON BULKHEAD AND PROTUDING ALONG AND UNDER STRAP. REPAIRED DAMAGE AREA PER ERA L10-53R-4922 REV IR.
- [SDR 2002F01003](https://openairdocs.org/sdr/2002F01003.md): Structure · lightning strike · Aug 19, 2002 · N195AT · Lkheed 1011 · Ailerons
  > LIGHTNING STRIKE DISCHARGE AT RT OUTBD AILERON TOP SURFACE. REPAIRED AILERON IAW SRM 51-50-01. WING STATION OWS 502 TO OWS 502.
- [SDR AMTA200201097](https://openairdocs.org/sdr/AMTA200201097.md): Floorbeam · corroded · Aug 13, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Floor Beam
  > AT 53 - FUSELAGE, 60 - MID FUSELAGE SECTION, LOWER GALLEY FLOORBEAM FS 901, RBL 23 TO RBL 28 IS CORRODED. REPLACED CORRODED T-CAP SECTION IN EXISTING REPAIR PER SRM 51-40-02 AND 53-23-00.
- [SDR AMTA200201152](https://openairdocs.org/sdr/AMTA200201152.md): Splice · corroded · Aug 9, 2002 · N195AT · Lkheed 1011 · Fuselage Miscellaneous Structure
  > FUSELAGE, 10 - MAINFRAME, FWD CENTER SPLICE ANGLE AT FS 328 CAP BL 0 CORRODED. INSTALLED NEW SPLICE ANGLE AT BL 0 FWD SIDE OF FS 328 CHORD PER L-1011 SRM 51-40-0.
- [SDR AMTA200201059](https://openairdocs.org/sdr/AMTA200201059.md): Door Frame · cracked · Aug 9, 2002 · N195AT · Lkheed 1011 · Fuselage Main, Structure
  > FWD FUSELAGE SECTION, RT ECS BAY CUTOUT FRAME FOR ACCESS DOOR CRACKED WITH CORROSION AT STAND OFF ATTACH POINT JUST FORWARD OF FORWARD HINGE ARM ATTACH POINT, TOP FWD OF O/B FRAME FORMER, TM3. REMOVED AND REPLACED CRACKED AND CORRODED CHORD ON O/B SIDE OF RT
- [SDR 99ZZZM273](https://openairdocs.org/sdr/99ZZZM273.md): Brake · failed · Feb 5, 1999 · N195AT · Lkheed 10113851 · Landing Gear Brake System
  > AFTER TAXI SET PARKING BRAKES, WHEN TRYING TO RELEASE BRAKES, BRAKES WOULD NOT RELEASE. FOUND 2F BRAKE WOULD NOT RELEASE. REMOVED AND REPLACED BRAKE ASSEMBLY. (M)
- [SDR 99ZZZM16](https://openairdocs.org/sdr/99ZZZM16.md): Switch · intermittent · Nov 1, 1998 · N195AT · Lkheed 10113851 · Aircraft Fuel Distribution System
  > DURING DESCENT, THE NR 3 ENGINE MADE UNSCHEDULED RUN DOWN WHEN TANK NR 3 QTY WENT EMPTY. ENGINE NR 3 WAS ON CROSSFEED FROM TANK 2L AND 2R. LANDED SAFELY. REPLACED RIGHT CROSSFEED SWITCH LIGHT ASSY, CROSSFEED VALVE WAS ALSO REPLACED FOR PRECAUTIONARY MEASURE
- [SDR 95ZZZX1194](https://openairdocs.org/sdr/95ZZZX1194.md): Retract Mech · failed · Feb 13, 1995 · N195AT · Lkheed 10113851 · Landing Gear Door Retract Section
  > MKE - FLT 55 - DURING TAKEOFF AND CLIMB, RT GEAR OR DOOR INTRANSIT FAILED TO COME UP. AIR TURN-BACK. SWAPPED RT AND LT PRESS. CONT. CHECK VALVES PER MM 32-33-04, RT DOOR OPS CHECK NORMAL. LEAK CK GOOD.

## 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 = 'N195AT' AND deregistration_id = 'N195AT-2006-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N195AT-2006-04-25/reports

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