# Service difficulty reports: N43537, cancelled Jul 30, 2002

A list on [N43537, cancelled Jul 30, 2002](https://openairdocs.org/deregistered/N43537-2002-07-30.md).

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

- [SDR CALA9901100](https://openairdocs.org/sdr/CALA9901100.md): Wire · broken · Aug 29, 1999 · N43537 · Doug DC932 · Light System Wiring
  > INSPECTION FOUND FORWARD SECTION OF EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE FOUND A BROKEN LIGHT SOCKET WIRE. A NEW SOCKET ASSEMBLY WAS SPLICED IN AND FUNCTIONAL CHECK WAS GOOD.
- [SDR CALA9900708](https://openairdocs.org/sdr/CALA9900708.md): Batteries · discharged · Jun 18, 1999 · N43537 · Doug DC932 · Emergency Lighting
  > INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERIES IN BATTERY PACK WERE REPLACED AND EMERGENCY LIGHT OPERATION CHECKED GOOD.
- [SDR CALA9900194](https://openairdocs.org/sdr/CALA9900194.md): Wire · broken · Feb 25, 1999 · N43537 · Doug DC932 · Light System Wiring
  > THE EMERGENCY AISLE PATH LIGHTS DID NOT ILLUMINATE WHEN ON POSITION WAS SELECTED DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A BROKEN WIRE ON SWITCH IN COCKPIT. THE SWITCH WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED.
- [SDR CALA9900162](https://openairdocs.org/sdr/CALA9900162.md): Vane · corroded · Feb 17, 1999 · N43537 · Doug DC932 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING FLAP O/B FIXED VANE I/B END LOWER SURFACE CORRODED WITH RIVETS PULLING THROUGH. THE LT O/B FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-51-3.
- [SDR CALA9900156](https://openairdocs.org/sdr/CALA9900156.md): Blkhd Bracket · cracked · Feb 15, 1999 · N43537 · Doug DC932 · Fuselage Main, Bulkhead
  > INSPECTION FOUND TWO AFT CARGO FORWARD BULKHEAD SPLICE BRACKETS WITH.5 INCH CRACKS. NEW FITTINGS WERE INSTALLED IAW SRM 51-10-1 AND 51-00-00.
- [SDR CALA9900155](https://openairdocs.org/sdr/CALA9900155.md): Support · corroded · Feb 15, 1999 · N43537 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT TEE CHANNEL CORRODED AT STA 160, LBL 8. THE FLOOR SUPPORT T CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0.
- [SDR CALA9900154](https://openairdocs.org/sdr/CALA9900154.md): Wire · broken · Feb 15, 1999 · N43537 · Doug DC932 · Light System Wiring
  > EMERGENCY LIGHT BATTERY PACKS FAILED TEST AT LT LAV AND FORWARD ENTRY. REPAIRED BROKEN WIRES, SECURED LOOSE GROUND, AND TIGHTENED BATTERY CONTACTS. OPERATION CHECKED NORMAL IAW MM 33-50-00, PAGE 203.
- [SDR CALA9900151](https://openairdocs.org/sdr/CALA9900151.md): Floorbeam · chafed · Feb 13, 1999 · N43537 · Doug DC932 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A HOLE CHAFED IN LOWER CHORD OF FORWARD CARGO COMPARTMENT FLOORBEAM AT FS 389, RBL 2. A REPAIR WAS INSTALLED IAW SRM 53-05-00, FIGURE 20A, PAGE 31.
- [SDR CALA9900150](https://openairdocs.org/sdr/CALA9900150.md): Skin · debonded · Feb 13, 1999 · N43537 · Doug DC932 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING LOWER SKIN PANEL DEBONDED AROUND SCREW HOLE FORWARD OF OUTER WHEEL WELL AREA. THE SKIN PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2.
- [SDR CALA9900149](https://openairdocs.org/sdr/CALA9900149.md): Panel · debonded · Feb 13, 1999 · N43537 · Doug DC932 · Wing, Plate/Skin
  > INSPECTION FOUND THE LT WING UPPER T/E FIXED PANEL DEBONDED WITH SURFACE CORROSION ON BOTTOM, JUST I/B OF AILERON. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2 AND 51-30-1.
- [SDR CALA9900148](https://openairdocs.org/sdr/CALA9900148.md): Vane · dented · Feb 13, 1999 · N43537 · Doug DC932 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING FLAP AFT MOVEABLE VANE DENTED AND ONE SPOT WORN THROUGH AT LOWER SURFACE NEAR I/B END. THE FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-51-2.
- [SDR CALA9900141](https://openairdocs.org/sdr/CALA9900141.md): Rib · cracked · Feb 12, 1999 · N43537 · Doug DC932 · Auxiliary Power Unit (APU) Doors
  > INSPECTION FOUND A.5 INCH CRACK IN RT APU DOOR INNER RIB. THE RIB WAS REPAIRED IAW SRM 52-01-00, FIGURE 2 AND 51-10-3.
- [SDR CALA9900140](https://openairdocs.org/sdr/CALA9900140.md): Tab · delaminated · Feb 12, 1999 · N43537 · Doug DC932 · Elevator, Tab Structure
  > INSPECTION FOUND LT ELEVATOR CONTROL TAB DELAMINATED ON UPPER SURFACE. THE LT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-00 AND 27-30-3.
- [SDR CALA9900139](https://openairdocs.org/sdr/CALA9900139.md): Fitting · cracked · Feb 12, 1999 · N43537 · Doug DC932 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN FITTING OF FORWARD ENTRY DOOR AT UPPER AFT STOP PAD AREA. THE FASTENERS AND FITTING WERE REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 52-03-00, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 52-03-00, PAGE 5, 51-10-3, AND 51-1
- [SDR CALA9900138](https://openairdocs.org/sdr/CALA9900138.md): Support · corroded · Feb 12, 1999 · N43537 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT T CHANNEL CORRODED BETWEEN STA 160 AND 229, BL 0. THE CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0.
- [SDR CALA9900121](https://openairdocs.org/sdr/CALA9900121.md): Door · out of adjust · Feb 8, 1999 · N43537 · Doug DC932 · Emergency Exits
  > THE LT AFT OVERWING EMERGENCY EXIT DOOR FAILED UNLOCK FORCE TEST. THE LATCH BAR SCREWS WERE ADJUSTED TO OBTAIN THE REQUIRED FORCE TO UNLOCK THE EXIT DOOR IAW MM 52-21-0, PAGE 504.
- [SDR CALA9801934](https://openairdocs.org/sdr/CALA9801934.md): Light · cracked · Oct 9, 1998 · N43537 · Doug DC932 · Emergency Lighting
  > FWD AISLE PATH LIGHTING COVER IN FIRST CLASS NEEDS TO BE RE-SECURED. REPLACED FWD SECTION OF BASE AND END CAP ASSY.
- [SDR CALA9601530](https://openairdocs.org/sdr/CALA9601530.md): Skin · punctured · Oct 25, 1996 · N43537 · Doug DC932 · Fuselage Main, Plate/Skin
  > A MAINTENANCE LIFT TRUCK STRUCK THE FUSELAGE CREATING A HOLE THROUGH SKIN AT STA 140.038, 3 INCHES BELOW LONGERON 20R. THE HOLE WAS APPROXIMATELY.875 L BY.5 W. THE AREA WAS REPAIRED IAW SRM 53-04 FIGURE 12B PAGE 608A SHEET 15.
- [SDR CALA9601298](https://openairdocs.org/sdr/CALA9601298.md): Relay · cracked · Sep 10, 1996 · N43537 · Doug DC932 · Ground Proximity System
  > THE AIRCRAFT HAD A HISTORY OF THE GPWS GIVING A TOO LOW GEAR WARNING AT LOW ALTITUDES DURING LANDING, WHICH RESULTED IN TWO INSTANCES OF A GO-AROUND. THE WARNING WAS ACCOMPANIED BY DIM LOWER HALF OF GREEN DOWN AND LOCKED LIGHTS. TROUBLESHOOTING BY MAINTENANC
- [SDR CAL960610](https://openairdocs.org/sdr/CAL960610.md): Batteries · discharged · May 14, 1996 · N43537 · Doug DC932 · Emergency Lighting
  > CLE - FLT 1144 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY BATTERIES WERE FOUND AT FAULT. THE NICAD BATTERIES IN POWER SUPPLY WERE REPLACED. (X)
- [SDR CAL951034](https://openairdocs.org/sdr/CAL951034.md): Skin · cracked · Nov 5, 1995 · N43537 · Doug DC932 · Fuselage Main, Plate/Skin
  > IAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, FIGURE 27. (X)
- [SDR 97ZZZX4197](https://openairdocs.org/sdr/97ZZZX4197.md): Steering Piston · pin sheared · Oct 19, 1995 · N43537 · Doug DC932 · Landing Gear Steering System
  > ONE EACH OF TWO STEERING PISTON PINS THAT GO THROUGH COLLAR, PN 5920605-503, WAS SHEARED INSIDE THE COLLAR. THE BREAK WAS IN THE BOTTOM THIRD OF THE SHANK. THERE WAS A HEAVY COATING OF RUST ACROSS THE SHEARED SURFACE. THIS DEFECT WAS DISCOVERED DURING THE P
- [SDR CAL950939](https://openairdocs.org/sdr/CAL950939.md): Actuator Pin · sheared · Oct 18, 1995 · N43537 · Doug DC932 · Landing Gear Steering System
  > DHN - INSPECTION FOUND THE NLG RIGHT NOSE STEERING ACTUATOR PIN SHEARED. THE STEERING CONTROL LEVER ASSEMBLY AND RIGHT NOSE STEERING CYLINDER ASSEMBLY WERE REMOVED AND REPLACED. (M)

## 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 = 'N43537' AND deregistration_id = 'N43537-2002-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N43537-2002-07-30/reports

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