# Service difficulty reports: N930FT, cancelled Aug 8, 2006

A list on [N930FT, cancelled Aug 8, 2006](https://openairdocs.org/deregistered/N930FT-2006-08-08.md).

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

- [SDR NACA20030103](https://openairdocs.org/sdr/NACA20030103.md): Pressure Switch · false indication · Aug 6, 2003 · N930FT · Boeing 727100 · Engine Oil Indicating System
  > NR 1 ENGINE OIL PRESSURE WARNING LIGHT(BYPASS), FLICKERING DURING CLIMB. INSPECTED NR 1 ENGINE MAIN OIL FILTER. NO METAL FOUND, INSTALLED NEW FILTER. DEFERRED OIL FILTER BYPASS INDICATION. OIL FILTER ON 12 HOUR INPECTION INTERVAL I.A.W. 727 MEL 79-2.
- [SDR NACA20030101](https://openairdocs.org/sdr/NACA20030101.md): Warning Light · malfunctioned · Aug 1, 2003 · N930FT · Boeing 727100 · Smoke Detection
  > AFTER TAKE-OFF THE WHEEL WELL FIRE WARNING ILLUMINATED AND BELL SOUNDED. BOTH EXTINGUISHED UPON GEAR EXTENSION. CREW REPORTED HEAVY BRAKING AT PAEN. INSPECTED WHEEL WELL AND LOOPS. NO EVIDENCE OF FIRE NOTED. OPERATED WHEEL WELL FIRE WARNING TEST MULTIPLE TIMES
- [SDR NACA20030096](https://openairdocs.org/sdr/NACA20030096.md): Switch · false indication · Jul 22, 2003 · N930FT · Boeing 727100 · Leading Edge Slat Actuator
  > NR 2 SLAT INDICATES FORWARD AMBER LIGHT AND F.E. TRANSITE LIGHT WITH FLAPS UP. REPLACED NR 2 SLAT EXTEND SWITCH.
- [SDR NACA20030095](https://openairdocs.org/sdr/NACA20030095.md): Actuator · false indication · Jul 21, 2003 · N930FT · Boeing 727100 · Leading Edge Slat Actuator
  > NR 2 SLAT LIGHT ON IN FLT WITH FLAPS IN UP POSITION. REPLACED SLAT ACTUATOR.
- [SDR NACA20030085](https://openairdocs.org/sdr/NACA20030085.md): Hinge · corroded · May 8, 2003 · N930FT · Boeing 72723 · Leading Edge Devices
  > LT WING KRUEGER FLAP MOUNT BRACKET HINGE ASSEMBLY CORRODED. REMOVED AND REPLACED HINGE ASSEMBLY.
- [SDR NACA20030082](https://openairdocs.org/sdr/NACA20030082.md): Coupler · oscillates · Apr 3, 2003 · N930FT · Boeing 727100 · Autopilot System
  > RIGHT ON TAKE-OFF, UPPER YAW DAMPER OSCILATE AUTO PILOT DISENGAGE, LIGHT STAYED ON, WIND SHEAR CAUTION LIGHT STAYS ON. REPLACED UPPER YAW DAMPER COUPLER AND TESTED GOOD.
- [SDR NACA20030076](https://openairdocs.org/sdr/NACA20030076.md): Engine · shorted · Feb 11, 2003 · N930FT · Boeing 727100 · Engine Oil System Wiring
  > DISCREPANCY: ABORTED TAKE OFF DUE TO #1 ENGINE OIL PRESSURE LIGHT ILLUMINATED.CORRECTIVE ACTION: REMOVED MOISTURE FROM OIL DIFFERENTIAL PRESSURE SWITCH CANNON PLUG.
- [SDR NACA20030073](https://openairdocs.org/sdr/NACA20030073.md): Volt Regulator · tripped · Feb 6, 2003 · N930FT · Boeing 727100 · AC Power Distribution System
  > DISCREPANCY: ON TAKE OFF ROLL LOST #1 ENG GEN ESSENTIAL POWER WITH #3 ENGINE GENERATOR SELECTED.CORRECTIVE ACTION: REPLACED #1 VOLTAGE REGULATOR.
- [SDR NACA20020021](https://openairdocs.org/sdr/NACA20020021.md): Spar Cap · corroded · May 21, 2002 · N930FT · Boeing 72723 · Wing Main, Frame Structure
  > DISCREPANCY: During "C" inspection, I.G. corrosion was discovered on the L/H wing aft spar lower chord, from w.s. 224.5 TO w.s. 241.0.CORRECTIVE ACTION: Lower spar cap being replaced from LBL 70.5 to W.S. 259.
- [SDR NACA20020036](https://openairdocs.org/sdr/NACA20020036.md): Attach Fitting · Mar 14, 2002 · N930FT · Boeing 72723 · Fuselage Main, Structure
  > DURING "C" CHECK INSPECTION FOUND 2 EA STARTED DRILL HOLES IN THE ATTACH FITTING AT B.S. 1183, WL 278, AND RBL 27. CORRECTED BY INSTALLING 2 PIECE FREEZE PLUG, AND DOUBLER PER BOEING PROVIDED REPAIR PLAN NAC-ANC-02-00003H AND REIVISION NAC-ANC-02-00004H.
- [SDR NACA20010038](https://openairdocs.org/sdr/NACA20010038.md): Smoke Detector · malfunctioned · Nov 10, 2001 · N930FT · Boeing 72723 · Smoke Detection
  > MECHANICAL INTERRUPTION IN ANCHORAGE AT 1522Z DUE TO LOWER CARGO FIRE WARNING HORN WENT OFF 3 TIMES. OPENED BOTH BELLY DOORS IMMEDIATELY UPON AIRCRAFT RETURN. FOUND NO SMOKE OR FIRE. UNLOADED BELLY'S AND PERFORMED LOWER CARGO SMOKE/FIRE PROTECTOR TEST, IAW
- [SDR NACA2001018](https://openairdocs.org/sdr/NACA2001018.md): Disk · vibration · Apr 30, 2001 · N930FT · Boeing 72723 · Turbine Section
  > MI AT ANC AT 2102Z, ENGINE SHUTDOWN DUE TO SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE.
- [SDR NACA20010005](https://openairdocs.org/sdr/NACA20010005.md): Control Unit · malfunctioned · Jan 23, 2001 · N930FT · Boeing 72723 · Brake Anti-Skid Section
  > WITH ANTI SKID ON BRAKES RELEASED ON ROLLOUT. REPLACED ANTI SKID CONTROL MODULE.
- [SDR NACA20010004](https://openairdocs.org/sdr/NACA20010004.md): Switch · dirty · Jan 20, 2001 · N930FT · Boeing 72723 · Landing Gear Position and Warning
  > ON LANDING AT ANCHORAGE LOSS OF BRAKE, LOSS OF LEFT PACK, LOSS OF APU, GPWS, AND STICK SHAKER CAME ON. CLEANED NOSE GEAR SAFETY WARNING SWITCH.
- [SDR NACA200000018](https://openairdocs.org/sdr/NACA200000018.md): Brake · overheated · Aug 16, 2000 · N930FT · Boeing 72723 · Overheat Detection
  > ON DOWN WIND AT AKN, WHEEL WELL WARNING LIGHT AND BELL SOUNDED. AS SOON AS THE GEAR WENT OUT AS PER PROCEDURES THE BELL AND LIGHT WENT OUT, VISUAL VERIFICATION WITH CONTROL TOWER EVERYTHING LOOKED NORMAL WITH THEM. INSPECTED MAIN GEAR BRAKES FOR LEAKAGE AND
- [SDR 98ZZZM502](https://openairdocs.org/sdr/98ZZZM502.md): Longeron · worn · Jun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION DISCOVERED WEAR MARKS ON THE LEFT AND RIGHT KEEL BEAM LONGERONS AT THE MAIN LANDING GEAR DOOR HINGES, STATION 947 LEFT AND STATION 910 RIGHT. REPAIRED BY BLENDING AWAY THE DAMAGED AREAS, FLAP PEENED, ALODINED, PRIMED AND CORROSION PR
- [SDR 98ZZZM501](https://openairdocs.org/sdr/98ZZZM501.md): Skin · cracked · Jun 1, 1998 · N930FT · Boeing 72723 · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION DISCOVERED A CRACK IN THE FIXED LEADING EDGE SKIN AT RIGHT WING LEADING EDGE STATION 155. REPAIRED BY TRIMMING OUT THE CRACK, HFEC NDT INSPECTING, FABRICATING AND INSTALLING A REPAIR DOUBLER AND FILLER WITH BLUEPRINT TYPE FASTENERS.
- [SDR 98ZZZM500](https://openairdocs.org/sdr/98ZZZM500.md): Bulkhead Fitting · corroded · Jun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, Bulkhead
  > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT BULKHEAD TERMINAL FITTING AT STATION 870. REPAIRED BY BLENDING AWAY THE CORROSION, HFEC NDT INSPECTING, FLAP PEENING BLENDED AREA, ALODINING AND DOUBLE PRIMING BARE ALUMINUM AREAS. REPAIRED IAW EVI
- [SDR 97ZZZX3523](https://openairdocs.org/sdr/97ZZZX3523.md): Actuator · inaccurate · Jul 12, 1997 · N930FT · Boeing 72723 · Leading Edge Slat Actuator
  > ANC - FLT 74 - RETURNED TO ANC AT 0235Z DUE TO NR 7 LEADING EDGE SLAT INDICATING IN-TRANSIT. MAINTENANCE REPLACED NR 7 LEADING EDGE SLAT ACTUATOR DUE TO FAULTY INDICATION AND RETURNED AIRCRAFT TO SERVICE. (X)
- [SDR 97ZZZX3517](https://openairdocs.org/sdr/97ZZZX3517.md): Slat Actuator · leaking · Jun 8, 1997 · N930FT · Boeing 72723 · Leading Edge Slat Actuator
  > ON TAKEOFF ROLL, A-SYSTEM LOW LEVEL LIGHT CAME ON, TAXIED OFF AT BRAVO TO COMPANY RAMP. MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT ACTUATOR AND RETURNED AIRCRAFT TO SERVICE. (X)
- [SDR 96ZZZX1465](https://openairdocs.org/sdr/96ZZZX1465.md): Windshield · cracked · Jan 10, 1996 · N930FT · Boeing 72723 · Flight Compartment Windows
  > ANC - FLT 105 - RETURNED TO ANC DUE TO FAILURE OF CAPTAIN'S WINDSHIELD OUTER PANEL. MAINTENANCE REPLACED L1 WINDOW. REPLACED WINDSHIELD HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. ACFT RETURNED TO SERVICE.

## 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 = 'N930FT' AND deregistration_id = 'N930FT-2006-08-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N930FT-2006-08-08/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.