# Service difficulty reports: N15525, cancelled Oct 18, 2000

A list on [N15525, cancelled Oct 18, 2000](https://openairdocs.org/deregistered/N15525-2000-10-18.md).

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

- [SDR CALA9900091](https://openairdocs.org/sdr/CALA9900091.md): Power Supply · inop · Jan 28, 1999 · N15525 · Doug DC932 · Emergency Lighting
  > THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE B5-25 POWER SUPPLY AT STA 635 WAS REMOVED AND REPLACED.
- [SDR CALA9801390](https://openairdocs.org/sdr/CALA9801390.md): Skin · cracked · Aug 5, 1998 · N15525 · Doug DC932 · Cargo Compartments
  > INSPECTION FOUND AFT CARGO BARRIER DOOR SKIN CRACKED AND DELAMINATED ON INBOARD SIDE WITH A PUNCTURE ON OUTBOARD SIDE. THE DOOR WAS DISASSEMBLED. THE OUTER SKIN WAS REMOVED AND THE PUNCTURED AREA WAS TRIMMED OUT. NEW SKIN AND DOUBLERS WERE FABRICATED AND INS
- [SDR CALA9801388](https://openairdocs.org/sdr/CALA9801388.md): Skin · cracked · Aug 5, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, 51-10-3, 51-30-2.
- [SDR CALA9801389](https://openairdocs.org/sdr/CALA9801389.md): Skin · corroded · Aug 4, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-0, 51-30-8, AND 51-30-2.
- [SDR CALA9801382](https://openairdocs.org/sdr/CALA9801382.md): Strap · cracked · Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-0.
- [SDR CALA9801381](https://openairdocs.org/sdr/CALA9801381.md): Bracket · gouged · Jul 31, 1998 · N15525 · Doug DC932 · Engine Thrust Reverser
  > INSPECTION FOUND NR 1 THRUST REVERSER PANEL BRACKET GOUGED. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2A, AND 51-30-2.
- [SDR CALA9801380](https://openairdocs.org/sdr/CALA9801380.md): Angle · cracked · Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon Structure
  > INSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, AND 51-00.
- [SDR CALA9801370](https://openairdocs.org/sdr/CALA9801370.md): Panel · corroded · Jul 30, 1998 · N15525 · Doug DC932 · Wing, Plate/Skin
  > INSPECTION FOUND CORROSION ON TOP SIDE LEFT WING PANEL NR 1122A. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, PAGE 8, 57-31-1, 51-10-3, AND 51-30-2.
- [SDR CALA9801365](https://openairdocs.org/sdr/CALA9801365.md): Splice · corroded · Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR PANEL SPLICE PLATE IN AFT CARGO PIT AT STA 935 CORRODED. A NEW FLOOR PANEL SPLICE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.
- [SDR CALA9801364](https://openairdocs.org/sdr/CALA9801364.md): Panel · gouged · Jul 29, 1998 · N15525 · Doug DC932 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LEADING EDGE PANEL NR 1248 GOUGED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2.
- [SDR CALA9801363](https://openairdocs.org/sdr/CALA9801363.md): Angle · cracked · Jul 29, 1998 · N15525 · Doug DC932 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.
- [SDR CALA9801362](https://openairdocs.org/sdr/CALA9801362.md): Floor · cracked · Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION FOUND AFT CARGO FLOOR PANEL AT STA 756-935 CRACKED AND WORN IN SEVERAL PLACES. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0.
- [SDR CALA9701227](https://openairdocs.org/sdr/CALA9701227.md): Longeron · cracked · Aug 14, 1997 · N15525 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 CRACK IN LONGERON 17R AT STA 965. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18.
- [SDR CAL960042](https://openairdocs.org/sdr/CAL960042.md): Drive Mechanism · broken · Jan 14, 1996 · N15525 · Doug DC932 · Leading Edge Slat Control System
  > FLT NR 1787 - IAH - LEFT LEADING EDGE SLAT WOULD NOT RETRACT AFTER LANDING AT IAH. NO IN FLIGHT ABNORMALITIES WERE OBSERVED. MAINTENANCE FOUND THE LEFT OUTBOARD SLAT DRIVE MECHANISM BROKEN. THE SLAT DRIVE MECHANISM WAS REMOVED AND REPLACED IAW MM 27-80-4.
- [SDR CAL950844](https://openairdocs.org/sdr/CAL950844.md): Jamb Door · dented · Sep 20, 1995 · N15525 · Doug DC932 · Fuselage Main, Attach Fittings
  > HOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M)
- [SDR CAL950842](https://openairdocs.org/sdr/CAL950842.md): Skin · cracked · Sep 17, 1995 · N15525 · Doug DC932 · Fuselage Main, Plate/Skin
  > HOU - INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038 BETWEEN LONGERON 10R AND 11R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 8. (M)
- [SDR CAL950845](https://openairdocs.org/sdr/CAL950845.md): Longeron · corroded · Sep 16, 1995 · N15525 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > HOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-02, FIG 16. (M)
- [SDR CAL950852](https://openairdocs.org/sdr/CAL950852.md): Blkhd Web · cracked · Sep 15, 1995 · N15525 · Doug DC932 · Fuselage Main, Bulkhead
  > HOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M)
- [SDR CAL950833](https://openairdocs.org/sdr/CAL950833.md): Angle · cracked · Sep 8, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT WHEEL WELL ATTACH ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30. (M)
- [SDR CAL950843](https://openairdocs.org/sdr/CAL950843.md): Bracket · cracked · Sep 7, 1995 · N15525 · Doug DC932 · Trailing Edge Flaps
  > HOU - INSPECTION FOUND A.75 INCH CRACK IN NR 4 LEFT FLAP HINGE OUTBOARD BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)
- [SDR CAL950839](https://openairdocs.org/sdr/CAL950839.md): Cusp · corroded · Sep 7, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 165 JUST FORWARD OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)
- [SDR CAL950838](https://openairdocs.org/sdr/CAL950838.md): Cusp · corroded · Sep 7, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 200 JUST AFT OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)
- [SDR CAL950834](https://openairdocs.org/sdr/CAL950834.md): Bracket · cracked · Sep 7, 1995 · N15525 · Doug DC932 · Trailing Edge Flaps
  > HOU - INSPECTION FOUND A.5 INCH CRACK IN THE RIGHT FLAP NR 4 FLAP HINGE INBOARD AND OUTBOARD BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-5. (M)
- [SDR CAL950832](https://openairdocs.org/sdr/CAL950832.md): Jamb · corroded · Sep 6, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND CORROSION ON FORWARD BAGGAGE BIN DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44, PAGE 105. (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 = 'N15525' AND deregistration_id = 'N15525-2000-10-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15525-2000-10-18/reports

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