# Service difficulty reports: N14524, cancelled May 31, 2000

A list on [N14524, cancelled May 31, 2000](https://openairdocs.org/deregistered/N14524-2000-05-31.md).

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

- [SDR CALA9900209](https://openairdocs.org/sdr/CALA9900209.md): Wire · broken · Mar 2, 1999 · N14524 · Doug DC932 · Light System Wiring
  > INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND LIGHT WIRE PULLED FROM SPLICE. THE WIRE WAS RESPLICED AND OPERATION CHECKED GOOD.
- [SDR CALA9900208](https://openairdocs.org/sdr/CALA9900208.md): Batteries · discharged · Mar 2, 1999 · N14524 · Doug DC932 · Emergency Lighting
  > INSPECTION FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9900207](https://openairdocs.org/sdr/CALA9900207.md): Batteries · discharged · Mar 1, 1999 · N14524 · Doug DC932 · Emergency Lighting
  > INSPECTION FOUND THE TAIL CONE EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9900105](https://openairdocs.org/sdr/CALA9900105.md): Wire · loose · Feb 2, 1999 · N14524 · Doug DC932 · Light System Wiring
  > THE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE ON SWITCH. THE LOOSE WIRE WAS TIGHTENED AND SYSTEM OPERATION CHECKED GOOD IAW MM 33-50-00, PAGES 203-204.
- [SDR CALA9900104](https://openairdocs.org/sdr/CALA9900104.md): Wire · broken · Feb 2, 1999 · N14524 · Doug DC932 · Light System Wiring
  > THE AFT CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 23 TO TAIL SECTION. MAINTENANCE FOUND WIRING TO BATTERY POWER PACKS BROKEN. THE WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0.
- [SDR CALA9900103](https://openairdocs.org/sdr/CALA9900103.md): Wire · broken · Feb 2, 1999 · N14524 · Doug DC932 · Light System Wiring
  > THE CABIN EMERGENCY LIGHTS FROM COCKPIT TO ROW 13 WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.
- [SDR CALA9900102](https://openairdocs.org/sdr/CALA9900102.md): Wire · broken · Feb 2, 1999 · N14524 · Doug DC932 · Light System Wiring
  > THE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.
- [SDR CALA9900096](https://openairdocs.org/sdr/CALA9900096.md): Connector · dirty · Jan 30, 1999 · N14524 · Doug DC932 · Emergency Lighting
  > INSPECTION FOUND THE L-1 PORTABLE EMERGENCY LIGHT INOPERATIVE. THE CONNECTOR WAS CLEANED AND SECURED AND OPERATION OF THE LIGHT CHECKED GOOD.
- [SDR CALA9900093](https://openairdocs.org/sdr/CALA9900093.md): Wire · broken · Jan 29, 1999 · N14524 · Doug DC932 · Light System Wiring
  > INSPECTION FOUND THE ESCAPE PATH LIGHT INBOARD OF FORWARD FIRST CLASS COAT CLOSET INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING. THE ESCAPE PATH LIGHT WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 501.
- [SDR CALA9900092](https://openairdocs.org/sdr/CALA9900092.md): Fitting · cracked · Jan 28, 1999 · N14524 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR THIRD BEAM END FITTING CRACKED AT AFT SIDE OF DOOR. THE CRACK WAS.1875 INCH LONG. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9900084](https://openairdocs.org/sdr/CALA9900084.md): Fitting · cracked · Jan 27, 1999 · N14524 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN AFT CARGO DOOR BEAM END FITTING AT AFT SIDE OF DOOR. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, PAGE 4.
- [SDR CALA9900037](https://openairdocs.org/sdr/CALA9900037.md): Rib · cracked · Jan 20, 1999 · N14524 · Doug DC932 · Wing, Rib/Bulkhead
  > RIB CRACKED THROUGH FASTENER HOLE INSIDE LEFT WING L/E XRS545 (.5) 12 INCES OUTSIDE OF NR 5 SLAT CENTER TRACK. REMOVED AND INSTALLED NEW RIB PER SRM 51-30-2.
- [SDR CALA9900062](https://openairdocs.org/sdr/CALA9900062.md): Tab · debond · Jan 16, 1999 · N14524 · Doug DC932 · Aileron Tabs
  > RIGHT AILERON INBOARD TAB HAS APPROXIMATELY 1 BY 10 DEBONDED LOWER SKIN. REMOVED AND REPLACED RIGHT AILERON PER MM 27-10-2.
- [SDR CALA9900011](https://openairdocs.org/sdr/CALA9900011.md): Angle · cracked · Jan 13, 1999 · N14524 · Doug DC932 · Wing Miscellaneous Structure
  > RIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51-10-3, AND 51-10-2.
- [SDR CALA9900010](https://openairdocs.org/sdr/CALA9900010.md): Terminal · failed · Jan 11, 1999 · N14524 · Doug DC932 · Emergency Lighting
  > AFT DOOR EMERGENGY EXIT LIGHT INOP. REPAIRED TERMINAL AT LIGHT AND OPS CHECK OK PER MM 33-53-01.
- [SDR CALA9900101](https://openairdocs.org/sdr/CALA9900101.md): Spar · cracked · Jan 2, 1999 · N14524 · Doug DC932 · Wing Spar
  > INSPECTION FOUND A.25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, APPROXIMATELY XRS 164. THE FASTENERS WERE REMOVED AND THE CRACKED SECTION OF SPAR WAS CUT OUT. A NEW SPAR SECTION WAS INSTALLED USING SPLICE
- [SDR CALA9900004](https://openairdocs.org/sdr/CALA9900004.md): Control · inop · Jan 3, 1998 · N14524 · Doug DC932 · Landing Gear Position and Warning
  > THE LT MLG UNSAFE LIGHT ILLUMINATED ON UPLATCH CHECK AFTER TAKEOFF. WHEN THE SLATS AND FLAPS WERE EXTENDED TO FIVE DEGREES AND THE AIRCRAFT WAS SLOWED TO 210 KNOTS FOR A RETURN TO IAH, THE UNSAFE LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE
- [SDR CALA9701678](https://openairdocs.org/sdr/CALA9701678.md): Spar Cap · cracked · Nov 24, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAI
- [SDR CALA9701660](https://openairdocs.org/sdr/CALA9701660.md): Spar Cap · cracked · Nov 20, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF LT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR CAP WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SECTION OF SPAR CA
- [SDR CALA9701659](https://openairdocs.org/sdr/CALA9701659.md): Spar Cap · cracked · Nov 20, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SPAR SECTION WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAIR A
- [SDR CALA9701658](https://openairdocs.org/sdr/CALA9701658.md): Skin · dented · Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 323, LONGERON 24. THE DENTED AREA WAS CUT OUT IAW SRM 53-04. A DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, 51-10-3, 51-30-2, AND 51-30-5.
- [SDR CALA9701657](https://openairdocs.org/sdr/CALA9701657.md): Floorbeam · corroded · Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION ON FLOORBEAM NUT PLATE AT STA 965. A DOUBLER, FILLER, AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-5, AND ECRA 5320-01488.
- [SDR CALA9701656](https://openairdocs.org/sdr/CALA9701656.md): Floor Panel · corroded · Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION FOUND FLOOR PANEL AND HAT CHANNEL CORRODED UNDER PILOT'S SEAT. A NEW PANEL AND HAT CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-20-0.
- [SDR CALA9701655](https://openairdocs.org/sdr/CALA9701655.md): Jamb · corroded · Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND DOOR JAMB AND SUB FLOOR CORRODED AT FS 200 BY R-1 DOOR. THE CORRODED DOOR JAMB PAN AND SUB FLOOR SECTIONS WERE REMOVED IAW SRM 53-05, FIGURE 55. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.
- [SDR CALA9701654](https://openairdocs.org/sdr/CALA9701654.md): Support · corroded · Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOORBOARD SUPPORT AT FORWARD PASSENGER ENTRYWAY CORRODED BETWEEN NR 1 SEAT TRACK AND CENTERLINE FLOORBEAM. THE FLOOR SUPPORT WAS REMOVED, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA9701653](https://openairdocs.org/sdr/CALA9701653.md): Skin · dented · Nov 20, 1997 · N14524 · Doug DC932 · Electrical/Electronic Compartment Doors
  > INSPECTION FOUND DENTS IN E AND E COMPARTMENT DOOR EXTERIOR SKIN. THE SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-3.
- [SDR CALA9701581](https://openairdocs.org/sdr/CALA9701581.md): Longeron · corroded · Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 25R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 218. THE LONGERON WAS REMOVED IAW SRM 53-10-03. A NEW LONGERON AND SPLICE SECTION WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-10-3 AND 51-30-2.
- [SDR CALA9701580](https://openairdocs.org/sdr/CALA9701580.md): Doubler · gouged · Nov 3, 1997 · N14524 · Doug DC932 · Passenger/Crew Doors
  > INSPECTION FOUND GOUGED DOUBLER AT FORWARD PASSENGER DOOR CUTOUT FOR DOOR LATCH HOOK ASSEMBLY. THE OLD DOUBLER WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, 51-10-3, 51-30-1, AND 51-30-2.
- [SDR CALA9701579](https://openairdocs.org/sdr/CALA9701579.md): Longeron · cracked · Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1079. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02. A REPAIR SECTION, SPLICE AND ATTACH BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-30-5 AND ECRA 5310-03589.
- [SDR CALA9701578](https://openairdocs.org/sdr/CALA9701578.md): Cover · cracked · Nov 3, 1997 · N14524 · Doug DC932 · Elevator Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RT ELEVATOR FLIGHT TAB MECHANISM CONTROL COVER AT STA XHS 95. THE CRACKED AREA WAS REMOVED, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-03, 51-10-3, 51-30-2, AND 51-30-8.
- [SDR CALA9701577](https://openairdocs.org/sdr/CALA9701577.md): Skin · dented · Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 360 BETWEEN LONGERON 21R AND 22R. THE DENTED AREA WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2.
- [SDR CALA9701519](https://openairdocs.org/sdr/CALA9701519.md): Intercostal · dented · Oct 30, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL DENTED BETWEEN STA 560 AND 579 AT LONGERON 28R. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-1.
- [SDR CALA9701518](https://openairdocs.org/sdr/CALA9701518.md): Intercostal · corroded · Oct 30, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT STA 680-699, LONGERON 16L. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-11-2, 51-10-3, AND 51-30-2.
- [SDR CALA9701517](https://openairdocs.org/sdr/CALA9701517.md): Intercostal · cracked · Oct 30, 1997 · N14524 · Doug DC932 · Service Doors
  > INSPECTION FOUND INTERCOSTAL CRACKED INSIDE R-1 DOOR AT CENTER OF DOOR BELOW LATCH MECHANISM. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9701516](https://openairdocs.org/sdr/CALA9701516.md): Skin · dented · Oct 29, 1997 · N14524 · Doug DC932 · Leading Edge Devices
  > INSPECTION FOUND RT WING NR 1 LEADING EDGE SLAT SKIN DENTED. THE DENTED AREA WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 57-06 AND 51-10-3.
- [SDR CALA9701515](https://openairdocs.org/sdr/CALA9701515.md): Stiffener · cracked · Oct 29, 1997 · N14524 · Doug DC932 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 2 CRACK IN HORIZONTAL STIFFENER ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT L13R. THE STIFFENER WAS REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5.
- [SDR CALA9701514](https://openairdocs.org/sdr/CALA9701514.md): Skin · dented · Oct 29, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 284, LONGERON 24. THE DENTED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04 AND 53-04, FIGURE 12.
- [SDR CALA9700111](https://openairdocs.org/sdr/CALA9700111.md): Hyd Line · leaking · Jan 29, 1997 · N14524 · Doug DC932 · Hydraulic System, Main
  > THE RT HYDRAULIC SYSTEM LOST ALL QUANTITY DURING FLIGHT. ABNORMAL PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE ON RIGHT THRUST REVERSER VALVE LEAKING. THE LINE WAS REMOVED AND REPLACED.
- [SDR CALA9601541](https://openairdocs.org/sdr/CALA9601541.md): Duct · cracked · Oct 31, 1996 · N14524 · Doug DC932 · Pneumatic Distribution System
  > THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED SHORTLY AFTER TAKEOFF. THE FIRE WARNING CEASED AFTER THE ENGINE THROTTLE WAS RETARDED LESS THAN TEN PERCENT. BOTH FIRE LOOPS TESTED NORMAL AND ALL ENGINE INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED AT
- [SDR CALA9600769](https://openairdocs.org/sdr/CALA9600769.md): Pushrod · bent · Jun 7, 1996 · N14524 · Doug DC932 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND PUSHROD AT GROUND SENSE SECTOR BENT. THE PUSHROD WAS REMOVED AND REPLACED. THE NLG GROUND SENSE WAS TESTED IAW MM 32-23-1, PAGE 204A. THE LANDIN
- [SDR CAL951140](https://openairdocs.org/sdr/CAL951140.md): Floor Web · cracked · Dec 7, 1995 · N14524 · Doug DC932 · Fuselage Miscellaneous Structure
  > IAH - INSPECTION FOUND A 1 INCH CRACK IN COCKPIT FLOOR WEB AT BS 89.050 AND A 2 INCH CRACK FOUND AT BS 83.550. THE FLOOR WEB WAS REPAIRED IAW ECRA 5310-03193 AND ECRA 531003031. (X)
- [SDR CAL950804](https://openairdocs.org/sdr/CAL950804.md): Longeron · corroded · Aug 27, 1995 · N14524 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > HOU - INSPECTION FOUND CORROSION ON LONGERON 26L BETWEEN STATION 945-960. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE INSTALLED IAW SRM 51-30-2. (M)
- [SDR CAL950803](https://openairdocs.org/sdr/CAL950803.md): Longeron · corroded · Aug 27, 1995 · N14524 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > HOU - INSPECTION FOUND CORROSION ON LONGERONS 26L TO 28L IN AFT BAGGAGE BIN BETWEEN STATION 937-945. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE REPLACED IAW SRM 51-30-2. (M)
- [SDR CAL950805](https://openairdocs.org/sdr/CAL950805.md): Rib · cracked · Aug 24, 1995 · N14524 · Doug DC932 · Wing, Rib/Bulkhead
  > HOU - INSPECTION FOUND THREE.25 INCH CRACKS IN WING LEADING EDGE RIB AT STATION XRS 501. A DOUBLER, FILLER, AND CLIP WERE FABRICATED AND INSTALLED IAW ECRA 5720-01260. (M)
- [SDR CAL950762](https://openairdocs.org/sdr/CAL950762.md): Skin · cracked · Aug 23, 1995 · N14524 · Doug DC932 · Nacelle/Pylon Structure
  > HOU - INSPECTION FOUND A.5 INCH CRACK IN SKIN ON TOP SIDE OF NR 2 ENGINE PYLON. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02. (M)
- [SDR CAL950497](https://openairdocs.org/sdr/CAL950497.md): Prox Control Box · inoperative · Jun 17, 1995 · N14524 · Doug DC932 · Landing Gear Position and Warning
  > IAH - FLT 1536 - THE LEFT GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK AFTER DEPARTING IAH. CYCLING THE GEAR AND REPEATING THE UPLATCH CHECK GAVE NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE LANDING GEAR P
- [SDR CAL950472](https://openairdocs.org/sdr/CAL950472.md): Seal · failed · Jun 9, 1995 · N14524 · Doug DC932 · Cabin Cooling System
  > FLT NR 1781 - GSO - THE CABIN BEGAN TO FILL WITH SMOKE DURING TAXI OUT FOR DEPARTURE. THE AIRCRAFT BEGAN A RETURN TO THE GATE AND WAS ACCOMPANIED BY EMERGENCY VEHICLES AS A PRECAUTIONARY MEASURE. NO EVIDENCE OF FIRE WAS OBSERVED. THE PASSENGERS WERE DEPLANE
- [SDR CAL950338](https://openairdocs.org/sdr/CAL950338.md): S/O Valve · leak · Apr 27, 1995 · N14524 · Doug DC932 · Rudder Control System
  > FLT NR 1581 - IAH - UPON LANDING FOUND HYDRAULIC FLUID LEAKING AT RUDDER. FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED SHUTOFF VALVE NO FURTHER ACTION. (W)
- [SDR CAL950153](https://openairdocs.org/sdr/CAL950153.md): Bungee Cyl · inoperative · Feb 26, 1995 · N14524 · Doug DC932 · Landing Gear Retraction/Extension System
  > FLT NR 1647 - CLE - THE LEFT MLG RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND BOTH RED LIGHTS EXTINGUISHED WITH THREE GREEN GEAR LIGHTS INDICATED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDE
- [SDR CAL950148](https://openairdocs.org/sdr/CAL950148.md): Eel Batt · discharged · Feb 23, 1995 · N14524 · Doug DC932 · Emergency Lighting
  > JAX - FLT 1521 - THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE FWD OVERWING EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (W)

## 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 = 'N14524' AND deregistration_id = 'N14524-2000-05-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14524-2000-05-31/reports

---
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