N18563, cancelled Jun 12, 2002

Service difficulty reports · 25

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA9900337Support · crackedINSPECTION 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.Mar 30, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9900336Angle · crackedINSPECTION 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.Mar 30, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9900329Skin · debondedINSPECTION 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.Mar 26, 1999 · N18563 · Doug DC931 · Wing, Plate/SkinSDR CALA9900328Floorbeam · crackedINSPECTION 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.Mar 26, 1999 · N18563 · Doug DC931 · Fuselage Main, Floor BeamSDR CALA9900327Skin · crackedINSPECTION 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.Mar 26, 1999 · N18563 · Doug DC931 · Elevator, Plate/SkinSDR CALA9900326Strap · corrodedINSPECTION 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 51-3Mar 26, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9900318Skin · debondedINSPECTION FOUND LEFT AILERON TAB DEBONDED. THE LEFT AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-51, PAGE 203.Mar 24, 1999 · N18563 · Doug DC931 · Aileron TabsSDR CALA9900317Fitting · crackedINSPECTION 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.Mar 24, 1999 · N18563 · Doug DC931 · Trailing Edge Flap ActuatorSDR CALA9900315Angle · crackedINSPECTION 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.Mar 24, 1999 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9900015Light · looseFLOOR EMERGENCY EXIT LIGHTS PULLED UP FROM FLOOR. INSTALLED TRACKS AND OPS CHECK OK.Jan 12, 1999 · N18563 · Doug DC931 · Emergency LightingSDR CALA9900005Strut · low pressureTHE 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 WJan 5, 1999 · N18563 · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR CALA9801243Strut · required serviceTHE 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 WASJul 13, 1998 · N18563 · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR CALA9801217Actuator · failedSMOKE 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 RJul 8, 1998 · N18563 · Doug DC931 · Drag Control ActuatorSDR CALA9800089Hyd Line · rupturedAIRCRAFT 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 REPAJan 19, 1998 · N18563 · Doug DC931 · Hydraulic System, MainSDR CALA9700629Spoiler · crackedDURING 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).Apr 19, 1997 · N18563 · Doug DC931 · SpoilersSDR CALA9700626Longeron · crackedDURING 1/2 D-CHECK INSPECTION, FOUND LONGERON .25 INCH CRACKED AT STA 965. REMOVED AND REPLACED CRACKED LONGERON PER SRM 53-02 FIG 2.Apr 9, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/StringerSDR CALA9700628Angle · corrodedDURING 1/2 D-CHECK INSP, FOUND RT WING L-ANGLE HAS CORROSION. REMOVED CORROSION PER SRM 57-03.Apr 8, 1997 · N18563 · Doug DC931 · Wing Miscellaneous StructureSDR CALA9700625Spar · crackedDURING 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.Apr 5, 1997 · N18563 · Doug DC931 · Wing SparSDR CALA9700623Angle · crackedDURING 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).Apr 5, 1997 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9700621Beam · crackedDURING 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.Apr 5, 1997 · N18563 · Doug DC931 · Fuselage Miscellaneous StructureSDR CALA9700639Longeron · crackedINSPECTION 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.Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/StringerSDR CALA9700627Longeron · crackedDURING 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.Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, Longeron/StringerSDR CALA9700624Spar Cap · corrodedDURING 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.Apr 3, 1997 · N18563 · Doug DC931 · Horizontal Stabilizer, Spar/RibSDR CALA9700622Beltframe · crackedDURING 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.Apr 3, 1997 · N18563 · Doug DC931 · Fuselage Main, FrameSDR CALA9700235Downlock Switch · inoperativeTHE 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. TFeb 23, 1997 · N18563 · Doug DC931 · Landing Gear Position and Warning
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