# Service difficulty reports: N14564, cancelled Dec 8, 1999

A list on [N14564, cancelled Dec 8, 1999](https://openairdocs.org/deregistered/N14564-1999-12-08.md).

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

- [SDR CALA9901094](https://openairdocs.org/sdr/CALA9901094.md): Control Cable · broken · Aug 26, 1999 · N14564 · Doug DC931 · Landing Gear Door Retract Section
  > A LOUD BANG WAS HEARD UPON GEAR RETRACTION AND THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOOR CABLE BROKEN WITH DAMAGE TO FWD NLG DOOR AND DOO
- [SDR CALA9801571](https://openairdocs.org/sdr/CALA9801571.md): Light · inoperative · Aug 27, 1998 · N14564 · Doug DC931 · Escape Slide
  > THE R-1 DOOR EMERGENCY EVACUATION SLIDE FAILED SLIDE LIGHT TEST. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED.
- [SDR CALA9801568](https://openairdocs.org/sdr/CALA9801568.md): Clips · out of adjust · Aug 27, 1998 · N14564 · Doug DC931 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS WAS LOW AT 15 POUNDS. THE CLIPS WERE REPLACED AND ADJUSTED IAW MM 53-50-3.
- [SDR CALA9801524](https://openairdocs.org/sdr/CALA9801524.md): Skin · corroded · Aug 24, 1998 · N14564 · Doug DC931 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT AFT BAGGAGE BIN STA 775, LONGERON 30 TO 29R. A DOUBLER WAS INSTALLED IAW ECRA 5331-01028.
- [SDR CALA9801499](https://openairdocs.org/sdr/CALA9801499.md): Spar Cap · corroded · Aug 21, 1998 · N14564 · Doug DC931 · Wing Spar
  > INSPECTION FOUND RT WING AFT LOWER SPAR CAP CORRODED AT WS XRS 364.5. THE AFT LOWER SPAR CAP WAS REPAIRED IAW SRM 57-09, FIGURE 11.
- [SDR CALA9801477](https://openairdocs.org/sdr/CALA9801477.md): Longeron · cracked · Aug 18, 1998 · N14564 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A CRACK IN LONGERON 16R AT RT LAV WALL, STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18, PAGE 48.
- [SDR CALA9801476](https://openairdocs.org/sdr/CALA9801476.md): Beltframe · cracked · Aug 18, 1998 · N14564 · Doug DC931 · Fuselage Main, Frame
  > INSPECTION FOUND A 4 INCH CRACK IN BELTFRAME AT STA 408, LONGERON 5L. THE BELTFRAME WAS REPAIRED IAW SRM 53-03, FIGURE 4.
- [SDR CALA9801472](https://openairdocs.org/sdr/CALA9801472.md): Longeron · cracked · Aug 17, 1998 · N14564 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT LT LAV WALL STA 965. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 18.
- [SDR CALA9801470](https://openairdocs.org/sdr/CALA9801470.md): Membrane · corroded · Aug 16, 1998 · N14564 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP MEMBRANE CORRODED AT STA 996, LONGERON 18L. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 25.
- [SDR CALA9801469](https://openairdocs.org/sdr/CALA9801469.md): Longeron · cracked · Aug 16, 1998 · N14564 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN LONGERON 17R AT LAV WALL STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18.
- [SDR CALA9801471](https://openairdocs.org/sdr/CALA9801471.md): Bulkhead Doubler · cracked · Aug 15, 1998 · N14564 · Doug DC931 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 1.5 INCH CRACK IN AFT PRESSURE BULKHEAD DOUBLER ON LT SIDE BELOW DOOR OPENING. REPAIRED IAW SRM 53-05, FIGURE 39.
- [SDR CALA9700671](https://openairdocs.org/sdr/CALA9700671.md): Skin · cracked · May 8, 1997 · N14564 · Doug DC931 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 AND 1.2 CRACK IN FUSELAGE SKIN AT STA 1143, LONGERON 14 AND 16R. THE CRACKS WERE STOP DRILLED AND REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9.
- [SDR CALA9601545](https://openairdocs.org/sdr/CALA9601545.md): Restrictor · clogged · Nov 2, 1996 · N14564 · Doug DC931 · Leading Edge Slat Control System
  > THE SLATS DID NOT EXTEND SYMMETRICALLY ON APPROACH. A SIGNIFICANT ROLL TO THE RIGHT OCCURRED AT SLATS EXTENDED/FLAPS 5 DEGREES, WHICH TOOK 10 DEGREES LEFT TURN TO COUNTERACT, AND THE BLUE SLAT EXTEND LIGHT TOOK 5 TO 6 SECONDS TO ILLUMINATE. THE AIRCRAFT LAND
- [SDR CALA9601262](https://openairdocs.org/sdr/CALA9601262.md): Posn Switch · out of adjust · Sep 2, 1996 · N14564 · Doug DC931 · Landing Gear Position and Warning
  > THE GEAR DOOR OPEN LIGHT REMAINED ON WITH GEAR RETRACTED AFTER TAKEOFF. CYCLING THE GEAR WAS NO HELP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO IAH THE LIGHT EXTINGUISHED. THE AIRCRAFT HAD A BRIEF PROBLEM HISTORY WITH THE DOOR OPEN LIGHT AND THE LEFT GEAR DO
- [SDR CALA9601273](https://openairdocs.org/sdr/CALA9601273.md): Angle · cracked · Aug 22, 1996 · N14564 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK ON REPAIR ANGLE FOR FORMER IN LEFT KEEL BEAM AREA, STA 637.5. A NEW ANGLE WAS INSTALLED IAW SRM 53-03.
- [SDR CALA9601274](https://openairdocs.org/sdr/CALA9601274.md): Fitting · cracked · Aug 21, 1996 · N14564 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN FITTING IN LEFT KEEL BEAM AREA, STA 622. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-03.
- [SDR CALA9601272](https://openairdocs.org/sdr/CALA9601272.md): Bulkhead Frame · cracked · Aug 21, 1996 · N14564 · Doug DC931 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN AFT PIT FORWARD BULKHEAD FRAME AT STA 756, LONGERON 26R. A DOUBLER WAS INSTALLED IAW SRM 53-01.
- [SDR CALA9601271](https://openairdocs.org/sdr/CALA9601271.md): Doubler · cracked · Aug 21, 1996 · N14564 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN DOUBLER JUST AFT OF STA 408, LONGERON 30. A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9601270](https://openairdocs.org/sdr/CALA9601270.md): Beam · cracked · Aug 20, 1996 · N14564 · Doug DC931 · Passenger/Crew Doors
  > INSPECTION FOUND ONE CRACK IN EACH OF MAIN CABIN DOOR BEAMS NR 1, 5 AND 7. THE CRACKS WERE.25 TO 1 INCH IN LENGTH. THE CRACKS WERE REPAIRED IAW SRM 52-05, FIGURE 31.
- [SDR CALA9601266](https://openairdocs.org/sdr/CALA9601266.md): Skin · cracked · Aug 20, 1996 · N14564 · Doug DC931 · Rudder, Plate/Skin
  > INSPECTION FOUND TWO 2 INCH CRACKS IN RUDDER SKIN, LOCATED AT TOP LEFT AND RIGHT SIDE OF RUDDER. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 55-01.
- [SDR CALA9601267](https://openairdocs.org/sdr/CALA9601267.md): Latches · binding · Aug 19, 1996 · N14564 · Doug DC931 · Aerodynamic Fairings
  > THE TAILCONE FAILED DROP CHECK AT 50+ POUNDS WHEN USING THE EXTERIOR RELEASE HANDLE. THE TAILCONE LATCHES WERE LUBRICATED AND OPERATION CHECKED GOOD.
- [SDR CALA9601151](https://openairdocs.org/sdr/CALA9601151.md): Up/Dnlk Switch · inoperative · Aug 11, 1996 · N14564 · Doug DC931 · Landing Gear Position and Warning
  > WHEN GEAR WAS EXTENDED ON APPROACH TO BHM NEITHER THE RED TRANSIT OR GREEN DOWN INDICATION LIGHTS FOR THE NOSE GEAR ILLUMINATED. THE GEAR WAS CYCLED WITH NO CHANGE IN INDICATION. EMERGENCY GEAR EXTENSION WAS USED TWICE BEFORE THE GREEN INDICATION BECAME STEAD
- [SDR CAL960201](https://openairdocs.org/sdr/CAL960201.md): Dnlock Switch · inoperative · Feb 26, 1996 · N14564 · Doug DC931 · Landing Gear Position and Warning
  > FLT NR 1819 - IAH - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG GREEN LIGHT NOT ILLUMINATING WHEN GEAR WAS EXTENDED FOR LANDING. CYCLING THE GEAR CAUSED THE LIGHT TO COME ON. THE NOSE GEAR DOWNLOCK SWITCH WAS REWIRED FROM S3-49 TO P1-133 PER WIRING DIAGRAM 3
- [SDR CAL950932](https://openairdocs.org/sdr/CAL950932.md): Angle · corroded · Oct 7, 1995 · N14564 · Doug DC931 · Fuselage Miscellaneous Structure
  > STA 31J - INSPECTION FOUND CORROSION ON L-ANGLE ATTACHED TO FLOOR BEAM AT FS 926, LBL 25. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05-0 AND SRM 51-40-2. (M)
- [SDR CAL950732](https://openairdocs.org/sdr/CAL950732.md): Receptacle · burned · Aug 18, 1995 · N14564 · Doug DC931 · Passenger Compartment Equipment
  > FLT NR 1579 - FLL - THE CREW REPORTED AN ODOR IN MID CABIN PRIOR TO LANDING AT FLL. MAINTENANCE FOUND PSU RECEPTACLE BETWEEN ROW 12-14 RT BURNED. THE RECEPTACLE AND PSU WERE REMOVED AND REPLACED. THE READING LIGHTS, CALL SWITCH, AND PASSENGER WARNING SIGNS
- [SDR CAL950475](https://openairdocs.org/sdr/CAL950475.md): Transformer Rect · inoperative · Jun 11, 1995 · N14564 · Doug DC931 · DC Rectifier/Converter
  > FLT NR 1279 - IAH - THE NR 2 TRANSFORMER RECTIFIER FAILED ON ROTATION LEAVING IAH (NR 1 RIGHT TRANSFORMER RECTIFIER WAS ON PLACARD). THE DC BUS OFF LIGHT ILLUMINATED AND THE GROUND SERVICE BUS CONTROL BREAKER POPPED. DC BUS TIE WAS CLOSED AND DC BUS WAS RECO

## 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 = 'N14564' AND deregistration_id = 'N14564-1999-12-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14564-1999-12-08/reports

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