# Service difficulty reports: N14341, cancelled Mar 30, 2009

A list on [N14341, cancelled Mar 30, 2009](https://openairdocs.org/deregistered/N14341-2009-03-30.md).

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

- [SDR CALA0700416](https://openairdocs.org/sdr/CALA0700416.md): Landing Gear · malfunctioned · Aug 9, 2007 · N14341 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > ALL LANDING GEAR EXTENDED ON ITS OWN WITH GEAR HANDLE IN OFF POSITION DURING CLIMBOUT AT 18,000 FEET AND 290 KNOTS. THE GEAR LIGHTS INDICATED THREE GREEN AND THREE RED. THE GEAR HANDLE WAS PLACED TO UP AND THE GEAR RETRACTED WITH NORMAL INDICATIONS. NO ABNOR
- [SDR CALA0600373](https://openairdocs.org/sdr/CALA0600373.md): Frame · cracked · Sep 28, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 794.3. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-2.
- [SDR CALA0600370](https://openairdocs.org/sdr/CALA0600370.md): Keelbeam · corroded · Sep 27, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED AT STA 520-530, S28R. THE CORROSION WAS REMOVED AND THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12 AND 51-40-02.
- [SDR CALA0600364](https://openairdocs.org/sdr/CALA0600364.md): Hinge Fitting · corroded · Sep 24, 2006 · N14341 · Boeing 7373T0 · Fuselage, Door Hinge
  > INSPECTION FOUND L-1 DOOR HINGE FITTING CORRODED AROUND BOLT HOLE AT STA 303.9. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600363](https://openairdocs.org/sdr/CALA0600363.md): Skin · cracked · Sep 23, 2006 · N14341 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN NR 6 FIXED L/E SKIN AT WS 255-389. REPAIRED IAW SRM 51-70-17 AND 51-40-02.
- [SDR CALA0600362](https://openairdocs.org/sdr/CALA0600362.md): Skin · cracked · Sep 23, 2006 · N14341 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN AFT CARGO DOOR SKIN AT LIGHTENING HOLE IN CENTER OF DOOR. A DOUBLER WAS INSTALLED IAW ECRA 5232-01082.
- [SDR CALA0600358](https://openairdocs.org/sdr/CALA0600358.md): Floorbeam · corroded · Sep 22, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 34 TO LBL 27. THE FLOORBEAM TOP CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV C.
- [SDR CALA0600347](https://openairdocs.org/sdr/CALA0600347.md): Seat Track · corroded · Sep 17, 2006 · N14341 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 328-343, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600346](https://openairdocs.org/sdr/CALA0600346.md): Angle · corroded · Sep 17, 2006 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN CABIN L-1 DOOR Z-ANGLE CORRODED AT STA 306-350, LBL 54. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0600345](https://openairdocs.org/sdr/CALA0600345.md): Seat Track · corroded · Sep 16, 2006 · N14341 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 277-291, RBL 42. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02 AND 51-20-01.
- [SDR CALA0600344](https://openairdocs.org/sdr/CALA0600344.md): Floorbeam · corroded · Sep 16, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 295, RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 201B, REPAIR NR 5.
- [SDR CALA0600341](https://openairdocs.org/sdr/CALA0600341.md): Floorbeam · corroded · Sep 15, 2006 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON TOP AND BOTTOM AT STA 986.5, RBL 43. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 201, REPAIR 3.
- [SDR CALA0300709](https://openairdocs.org/sdr/CALA0300709.md): Pressure Panel · cracked · Dec 11, 2003 · N14341 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A 12 INCH CRACK IN RT PRESSURE DECK AT STA 670, RBL 43, WL 200. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01031 AND SRM 53-60-51.
- [SDR CALA0200484](https://openairdocs.org/sdr/CALA0200484.md): Skin · cracked · Oct 3, 2002 · N14341 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.050" CRACK AT EDGE OF LIGHTENING HOLE IN C-2 DOOR INTERIOR SKIN. SECOND ROW FROM LEADING EDGE CENTER OF DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01019.
- [SDR CALA0200483](https://openairdocs.org/sdr/CALA0200483.md): Skin · cracked · Oct 3, 2002 · N14341 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.040" CRACK AT EDGE OF LIGHTENING HOLE IN C-1 DOOR INTERIOR SKIN. SECOND ROW AFT OF LEADING EDGE, CENTER OF DOOR INTERIOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01018.
- [SDR CALA0200478](https://openairdocs.org/sdr/CALA0200478.md): Frame · cracked · Sep 28, 2002 · N14341 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1" CRACK IN FRAME AND FRAME WAS BENT IN AFT PIT AT STA 807 BETWEEN STRINGER 23L AND 24L. A FRAME REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0200477](https://openairdocs.org/sdr/CALA0200477.md): Web · corroded · Sep 27, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO PIT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200475](https://openairdocs.org/sdr/CALA0200475.md): Support · corroded · Sep 25, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD FORWARD WEB SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200474](https://openairdocs.org/sdr/CALA0200474.md): Web · corroded · Sep 25, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAG BIN THRESHOLD LOWER SUPPORT WEB CORRODED IN SEVERAL SPOTS AT STA 794-847, S26R. THE SUPPORT WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0200473](https://openairdocs.org/sdr/CALA0200473.md): Intercostal · corroded · Sep 25, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R/H INTERCOSTAL IN AFT CARGO AREA CORRODED AT STA 747-767, RBL 22. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200472](https://openairdocs.org/sdr/CALA0200472.md): Web · corroded · Sep 24, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD PIT DOOR CUTOUT AFT JAMB R/H LOWER WEB CORRODED ON UNDERSIDE AT STA 500. A WEB SPLICE REPAIR WAS INSTALLED IAW SRM 51-70-13, FIGURE 1.
- [SDR CALA0200471](https://openairdocs.org/sdr/CALA0200471.md): Seat Track · corroded · Sep 24, 2002 · N14341 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 500. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200470](https://openairdocs.org/sdr/CALA0200470.md): Floor Support · corroded · Sep 22, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200469](https://openairdocs.org/sdr/CALA0200469.md): Stringer · cracked · Sep 20, 2002 · N14341 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R FORWARD OF ICE LIGHT AT BS 500C. THE STRINGER SECTION WAS REPLACED IAW SRM 53-00-03, FIGURE 202.
- [SDR CALA0200468](https://openairdocs.org/sdr/CALA0200468.md): Frame · cracked · Sep 19, 2002 · N14341 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND LEFT AND RIGHT MAIN BS 616 FRAME INNER CHORDS CRACKED BELOW MAIN CABIN FLOOR. THE CRACKS WERE 1 INCH EACH. THE CRACKED AREAS WERE CUT OUT AND FILLERS AND STIFFENERS WERE INSTALLED IAW ECRA 5311-01134.
- [SDR CALA0200466](https://openairdocs.org/sdr/CALA0200466.md): Angle · cracked · Sep 18, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2" CRACK IN WEB L-ANGLE AT STA 927-947. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200462](https://openairdocs.org/sdr/CALA0200462.md): Floorbeam · corroded · Sep 15, 2002 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 52 TO RBL 52. THE UPPER CAP WAS REMOVED AND A NEW "T" CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03851.
- [SDR CALA0200457](https://openairdocs.org/sdr/CALA0200457.md): Floor Support · corroded · Sep 10, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006-1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200456](https://openairdocs.org/sdr/CALA0200456.md): Floor Support · corroded · Sep 10, 2002 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0000058](https://openairdocs.org/sdr/CALA0000058.md): Skin · cracked · Jan 21, 2000 · N14341 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN FUSELAGE SKIN CUTOUT AT STA 380, AFT END OF EQUIPMENT COOLING EXHAUST. REPAIRED IAW ECRA 5330-02894.
- [SDR CALA9800149](https://openairdocs.org/sdr/CALA9800149.md): Floorbeam · corroded · Jan 30, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 500C TO 500D BETWEEN STRINGERS 26L AND 27L. THE CORRODED AREA WAS REMOVED, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5320-01502.
- [SDR CALA9800130](https://openairdocs.org/sdr/CALA9800130.md): Socket · inoperative · Jan 27, 1998 · N14341 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND, RT FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INTERMITTENT. THE LIGHT SOCKET WAS REPLACED IAW MM 33-51-00.
- [SDR CALA9800097](https://openairdocs.org/sdr/CALA9800097.md): Floorbeam · corroded · Jan 22, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 15. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9800096](https://openairdocs.org/sdr/CALA9800096.md): Floorbeam · corroded · Jan 22, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 29. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9800095](https://openairdocs.org/sdr/CALA9800095.md): Support · corroded · Jan 21, 1998 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 947-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9800094](https://openairdocs.org/sdr/CALA9800094.md): Support · corroded · Jan 20, 1998 · N14341 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1006 TO 1016, LBL 6 TO 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9800086](https://openairdocs.org/sdr/CALA9800086.md): Floorbeam · corroded · Jan 18, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 947, LBL 6. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.
- [SDR CALA9800085](https://openairdocs.org/sdr/CALA9800085.md): Floorbeam · corroded · Jan 17, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BBL 0 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9800084](https://openairdocs.org/sdr/CALA9800084.md): Floorbeam · corroded · Jan 17, 1998 · N14341 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9700494](https://openairdocs.org/sdr/CALA9700494.md): Fire Detect Unit · inoperative · Apr 6, 1997 · N14341 · Boeing 7373T0 · Fire Detection
  > THE APU FIRE BELL SOUNDED WHILE STARTING THE APU ON SHORT FINAL. THE OVERSPEED LIGHT CAME ON AND THE BOTTLE DISCHARGE LIGHT DID NOT ILLUMINATE. THE FIRE LIGHT REMAINED ILLUMINATED ALL THE WAY TO THE GATE. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 2 ENG
- [SDR CALA9601211](https://openairdocs.org/sdr/CALA9601211.md): Ap Accy Unit · inoperative · Aug 23, 1996 · N14341 · Boeing 7373T0 · Autopilot System
  > UPON SELECTING THE APP MODE AIRCRAFT LOST ALL FLIGHT DIRECTION, NR 1 AIRSPEED BUG, YAW DAMPER, BOOST PUMPS, BUT NO BUSS OFF LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT ACCESSORY UNIT AND THE
- [SDR CAL960469](https://openairdocs.org/sdr/CAL960469.md): Skin · punctured · Apr 11, 1996 · N14341 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > EWR - INSPECTION FOUND A 2 INCH BY 2 INCH PUNCTURE IN RT FUELAGE SKIN ABOVE WINDOW NR 8 AT STA 480. THE AREA WAS REPAIRED IAW SRM 53-00-01, FIGURE 202. (X)
- [SDR CAL960079](https://openairdocs.org/sdr/CAL960079.md): Battery Pack · discharged · Jan 21, 1996 · N14341 · Boeing 7373T0 · Emergency Lighting
  > HOU - THE LEFT AFT EMERGENCY CEILING LIGHT BATTERY PACK FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REPLACED. (M)
- [SDR CAL950734](https://openairdocs.org/sdr/CAL950734.md): Uplock Actuator · inoperative · Aug 20, 1995 · N14341 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > BUF - FLT 0640 - THE RT MLG GAVE AN UNSAFE GEAR INDICATION WHEN GEAR WAS EXTENDED ON APPROACH TO BUF. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY WAS CONDUCTED. THE GEAR WAS CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAIN
- [SDR CAL950621](https://openairdocs.org/sdr/CAL950621.md): Coupler · rate gyro failed · Jul 27, 1995 · N14341 · Boeing 7373T0 · Autopilot System
  > FLT 0131-MEX-THE YAW DAMPER WENT FULL SCALE RT WITH RUDDER MOVEMENT TO THE RT AT APPROX 11,000 FT WITH AIRSPEED BETWEEN 180 AND 170. THE YAW DAMPER WAS TURNED OFF AND RUDDER WENT BACK TO NORM. THE AUTOPILOT ACCY UNIT WAS REMOVED DURING T/S AND TESTED GOOD PE

## 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 = 'N14341' AND deregistration_id = 'N14341-2009-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14341-2009-03-30/reports

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