# Service difficulty reports: N18563, cancelled Jun 12, 2002

A list on [N18563, cancelled Jun 12, 2002](https://openairdocs.org/deregistered/N18563-2002-06-12.md).

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

- [SDR CALA9900337](https://openairdocs.org/sdr/CALA9900337.md): Support · cracked · Mar 30, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO,.5 INCH CRACKS IN AFT ACCESSORY COMPARTMENT SUPPORT AT STA 1038, RT SIDE. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-11-4 PAGE 5.
- [SDR CALA9900336](https://openairdocs.org/sdr/CALA9900336.md): Angle · cracked · Mar 30, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.625 INCH CRACK, RT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA9900329](https://openairdocs.org/sdr/CALA9900329.md): Skin · debonded · Mar 26, 1999 · N18563 · Doug DC931 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER SKIN PANEL FORWARD OF RIGHT GEAR DEBONDED. THE PANEL WAS REMOVED, REPAIRED AND INSTALLED IAW SRM 51-30-2, PAGE 4.
- [SDR CALA9900328](https://openairdocs.org/sdr/CALA9900328.md): Floorbeam · cracked · Mar 26, 1999 · N18563 · Doug DC931 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT OVERHEAD FLOORBEAM AT STA 237, LBL 8. THE CRACKED AREA WAS CUT OUT IAW SRM 53-05, PAGE 216A. A DOUBLER AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-05, PAGE 216A.
- [SDR CALA9900327](https://openairdocs.org/sdr/CALA9900327.md): Skin · cracked · Mar 26, 1999 · N18563 · Doug DC931 · Elevator, Plate/Skin
  > INSPECTION FOUND A 2.5 INCH CRACK IN LT ELEVATOR O/B TRAILING EDGE SKIN (JUST I/B OF STATIC WICK). THE CRACK WAS STOP DRILLED AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-70-1, PAGE 12. WEIGHT AND BALANCE WAS WITHIN LIMITS IAW SRM 55-20-1, FIGURE 4.
- [SDR CALA9900326](https://openairdocs.org/sdr/CALA9900326.md): Strap · corroded · Mar 26, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO COMPARTMENT LONGERON 23L STRAP BETWEEN STA 937 AND 967 CORRODED. THE FASTENERS AND STRAP WERE REMOVED IAW SRM 51-30-2. THE SURFACE CORROSION WAS REMOVED IAW SRM 51-10-3. A NEW STRAP WAS INSTALLED IAW SRM 51-01-0, 51-10-3, AND 51-3
- [SDR CALA9900318](https://openairdocs.org/sdr/CALA9900318.md): Skin · debonded · Mar 24, 1999 · N18563 · Doug DC931 · Aileron Tabs
  > INSPECTION FOUND LEFT AILERON TAB DEBONDED. THE LEFT AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-51, PAGE 203.
- [SDR CALA9900317](https://openairdocs.org/sdr/CALA9900317.md): Fitting · cracked · Mar 24, 1999 · N18563 · Doug DC931 · Trailing Edge Flap Actuator
  > INSPECTION FOUND A 1.6 CRACK IN LEFT FLAP O/B ACTUATOR AFT HINGE FITTING. THE LEFT FLAP O/B ACTUATOR AFT HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-50-01, PAGE 505.
- [SDR CALA9900315](https://openairdocs.org/sdr/CALA9900315.md): Angle · cracked · Mar 24, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO.5 INCH CRACKS IN LEFT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604, APPROXIMATELY LEFT LOWER BELLY FORWARD ADF SENSE ANTENNA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-45.
- [SDR CALA9900015](https://openairdocs.org/sdr/CALA9900015.md): Light · loose · Jan 12, 1999 · N18563 · Doug DC931 · Emergency Lighting
  > FLOOR EMERGENCY EXIT LIGHTS PULLED UP FROM FLOOR. INSTALLED TRACKS AND OPS CHECK OK.
- [SDR CALA9900005](https://openairdocs.org/sdr/CALA9900005.md): Strut · low pressure · Jan 5, 1999 · N18563 · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
  > THE LANDING GEAR HANDLE WOULD NOT RAISE PAST UP LATCH CHECK POSITION AND GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE NOSE GEAR STRUT WAS SERVICED IAW MM 32-21-2 AND THE GROUND SHIFT MECHANISM W
- [SDR CALA9801243](https://openairdocs.org/sdr/CALA9801243.md): Strut · required service · Jul 13, 1998 · N18563 · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING PIT. THE AIRCRAFT WAS RETURNED TO PIT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE NOSE STRUT WAS SERVICED IAW MM 32-21-02. THE NOSE GEAR WAS
- [SDR CALA9801217](https://openairdocs.org/sdr/CALA9801217.md): Actuator · failed · Jul 8, 1998 · N18563 · Doug DC931 · Drag Control Actuator
  > SMOKE BEGAN COMING FROM TOP OF FIRST OFFICER'S GLARESHIELD/WINDOW AREA DURING CLIMB-OUT OF IAH BOUND FOR ORD. THE AIRCRAFT WAS DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO GROUND SPOILER ACTUATOR LOCKED UP. THE ACTUATOR WAS R
- [SDR CALA9800089](https://openairdocs.org/sdr/CALA9800089.md): Hyd Line · ruptured · Jan 19, 1998 · N18563 · Doug DC931 · Hydraulic System, Main
  > AIRCRAFT LOST THE LEFT SYSTEM HYDRAULIC QUANTITY DURING CLIMB-OUT OF IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE THRUST REVERSER CONTROL VALVE HYDRAULIC LINE RUPTURED. THE HYDRAULIC LINE WAS REPA
- [SDR CALA9700629](https://openairdocs.org/sdr/CALA9700629.md): Spoiler · cracked · Apr 19, 1997 · N18563 · Doug DC931 · Spoilers
  > DURING 1/2 D-CHECK INSP, FOUND ACTUATOR ATTACH POINT CUTOUT CRACKED 1.5 INCH LONG. REMOVED AND INSTALLED RIGHT I/B FLT SPOILER PANEL (P/N 5910053-01).
- [SDR CALA9700626](https://openairdocs.org/sdr/CALA9700626.md): Longeron · cracked · Apr 9, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING 1/2 D-CHECK INSPECTION, FOUND LONGERON.25 INCH CRACKED AT STA 965. REMOVED AND REPLACED CRACKED LONGERON PER SRM 53-02 FIG 2.
- [SDR CALA9700628](https://openairdocs.org/sdr/CALA9700628.md): Angle · corroded · Apr 8, 1997 · N18563 · Doug DC931 · Wing Miscellaneous Structure
  > DURING 1/2 D-CHECK INSP, FOUND RT WING L-ANGLE HAS CORROSION. REMOVED CORROSION PER SRM 57-03.
- [SDR CALA9700625](https://openairdocs.org/sdr/CALA9700625.md): Spar · cracked · Apr 5, 1997 · N18563 · Doug DC931 · Wing Spar
  > DURING 1/2 D-CHECK INSPECTION, FOUND RT WING REAR SPAR CRACKED 1.75 INCH BELOW I/B LOWER MOUNT FOR NR 2 FLAP HINGE. REPAIRED PER ECRA 5761-01001.
- [SDR CALA9700623](https://openairdocs.org/sdr/CALA9700623.md): Angle · cracked · Apr 5, 1997 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING 1/2 D-CHECK INSPECTION, FOUND 3 INCH CRACK AT SUPPORT ANGLE STA 37. REMOVED AND INSTALLED NEW FITTING PER SRM 51-30-0, NEW (P/N 9957899-11).
- [SDR CALA9700621](https://openairdocs.org/sdr/CALA9700621.md): Beam · cracked · Apr 5, 1997 · N18563 · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING 1/2 D-CHECK INSPECTION, FOUND CRACKS AT TOP OF VERTICAL SUPPORT BEAM I/B RADIUS.625 INCH LONG O/B RADUIS 1 INCH LONG. FABRICATED AND INSTALLED DOUBLERS PER SRM 53-01 FIG 2.
- [SDR CALA9700639](https://openairdocs.org/sdr/CALA9700639.md): Longeron · cracked · Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND TWO 1 INCH CRACKS IN LONGERON 2L AT STA 756. THE CRACKED SECTION WAS REMOVED AND A REPAIR WAS SPLICED IN IAW SRM 53-02.
- [SDR CALA9700627](https://openairdocs.org/sdr/CALA9700627.md): Longeron · cracked · Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING 1/2 D-CHECK INSP, FOUND LONG 3R CRACKED APPROX.5 INCH AT STA 699. REMOVED CRACKED SECTION (P/N 2777922-3), REPAIRED SPLICE PER SRM 53-02.
- [SDR CALA9700624](https://openairdocs.org/sdr/CALA9700624.md): Spar Cap · corroded · Apr 3, 1997 · N18563 · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING 1/2 D-CHECK INSPECTION, FOUND CORROSION AT UPPER T-CAP AFT SPAR APPROX 2 INCH LONG ABOUT 5 FT FROM O/B END. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLERS REFERENCE ECRA 5510-01356.
- [SDR CALA9700622](https://openairdocs.org/sdr/CALA9700622.md): Beltframe · cracked · Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, Frame
  > DURING 1/2 D-CHECK INSPECTION, FOUND.5 INCH CRACK AT BELTFRAME STA 408 LT CABIN STRUCTURE AT LONG 5L. INSTALLED AND REPAIRED PER SRM 53-03 FIG 4.
- [SDR CALA9700235](https://openairdocs.org/sdr/CALA9700235.md): Downlock Switch · inoperative · Feb 23, 1997 · N18563 · Doug DC931 · Landing Gear Position and Warning
  > THE NOSE LANDING GEAR GREEN LIGHT ILLUMINATED INTERMITTENTLY AFTER GEAR WAS EXTENDED FOR LANDING ON APPROACH. THE GEAR WAS VISUALLY CONFIRMED DOWN IAW PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG DOWNLOCK SWITCH AT FAULT. T

## 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 = 'N18563' AND deregistration_id = 'N18563-2002-06-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18563-2002-06-12/reports

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