N18544, cancelled Aug 30, 1999

Service difficulty reports · 98

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 = 'N18544' AND deregistration_id = 'N18544-1999-08-30'
  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 CALA9900674Skin · dentedINSPECTION FOUND THE LT FUSELAGE SKIN DENTED AT STA 200-237, LONGERON 17L. THE DENTED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-04, FIGURE 47.Jun 15, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900654Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED IN SEVERAL PLACES FROM STA 427 TO 446 BETWEEN LONGERONS 21R TO 25R. THE DENTED AREAS WERE CUT OUT, NEW SKIN AND LONGERON SPLICES WERE INSTALLED IAW DOUGLAS DRAWING SR 09530004.Jun 5, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900633Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BELOW LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, PAGE 218F.Jun 3, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900613Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED BELOW WINDOW NR 12 (STA 437) AT STRINGER 15R. A DOUBLER AND FINGER DOUBLER REPAIR WAS INSTALLED IAW DOUGLAS DRAWING J060109, SRM 51-10-3 AND ECRA 5330-02815.Jun 2, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900612Rib · gougedINSPECTION FOUND TWO GOUGES IN RIB AT LEFT MLG WELL JUST FORWARD OF GEAR DIAGONAL BRACE. THE GOUGED AREA WAS CUT OUT IAW SRM 51-00-00 AND A NEW ANGLE AND SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2.Jun 2, 1999 · N18544 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9900590Skin · dentedINSPECTION FOUND LT FLAP LOWER TRAILING EDGE AREA DENTED INBOARD OF INBOARD ACTUATOR AREA. A DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 51-30-00.May 31, 1999 · N18544 · Doug DC932 · Trailing Edge FlapsSDR CALA9900589Rib · gougedINSPECTION FOUND LT MLG WELL CLOSURE RIB GOUGED JUST ABOVE LOCK DOT NR 2. A NEW PLATE AND SPLICES WERE INSTALLED IAW SRM 51-10-2.May 31, 1999 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900588Light · dimINSPECTION FOUND THREE SELF ILLUMINATING EXIT SIGNS WITH LOW LIGHT LEVEL AT ROW 15-16 AND ROW 25. THE SIGNS WERE REPLACED IAW MM 25-63-0.May 31, 1999 · N18544 · Doug DC932 · Emergency LightingSDR CALA9900564Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 484, LONGERONS 19 AND 20. THE SKIN WAS REPAIRED IAW SRM 53-04-04, FIGURE 38.May 20, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900554Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229 ABOVE LONGERON 17. THE DENTED AREA WAS CUT OUT IAW SRM 53-04-00, PAGE 203. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04-00, PAGE 203 AND 51-10-3.May 17, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900553Doubler · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT CARGO COMPARTMENT DOOR REPAIR DOUBLER AT UPLOCK GUIDE PIN. THE DOUBLER WAS REMOVED IAW SRM 51-10-2, PAGE 1. A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 1 AND 51-10-3, PAGE 1.May 17, 1999 · N18544 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9900551Skin · crackedINSPECTION FOUND A .5 INCH CRACK WITH CORROSION IN LOWER FUSELAGE SKIN JUST FORWARD OF BEACON LIGHT. THE CRACKED AREA WAS CUT OUT, THE CORROSION WAS REMOVED IAW SRM 51-10-3. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, PAGE 218A.May 14, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900550Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 37 AND LONGERON 17. THE DENTED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04-00, FIGURE 38, PAGE 218J, 51-10-3, AND 51-30-2.May 14, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900462Switch · failedIAH - FLT 612 - IMMEDIATELY AFTER TAKEOFF NOTICED ELECTRICAL SMELL IN COCKPIT. SMELL WENT AWAY IN A FEW MINUTES. DURING CLIMB-OUT NOTICED LEFT IGNITION C/B TRIPPED. RESET C/B PER QRH, WOULD NOT RESET. GOT A BEEP NOISE AND SPARKS CAME OUT OF OVERHEAD PANEL Apr 28, 1999 · N18544 · Doug DC932 · Ignition SwitchingSDR CALA9801566Uplatch Mech · out of adjustTHE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED, BUT THE GEAR DOOR OPEN LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO IAH. BOTH THE LT AND RT MLG DOORS WERE DAMAGED ON LANDING.Aug 28, 1998 · N18544 · Doug DC932 · Landing Gear Retraction/Extension SystemSDR CALA9801467Wire · brokenTHE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED, BUT THE GEAR DOOR OPEN LIGHT CAME ON. THE GEAR WAS CYCLED TO UP AND THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE GEAR INDICATIONS WERE NORMAL Aug 17, 1998 · N18544 · Doug DC932 · Landing Gear System WiringSDR CALA9801345Skin · dentedINSPECTION FOUND LT LEADING EDGE SLAT NR 1 SKIN DENTED AT STA XIS 136 AND XIS 132. REPAIRED IAW SRM 57-09, FIGURE 10 AND 10A.Jul 27, 1998 · N18544 · Doug DC932 · Leading Edge DevicesSDR CALA9801344Skin · dentedINSPECTION FOUND A DENT IN LT LOWER WING SKIN AT XRS 530. THE AREA WAS REPAIRED IAW SRM 57-03, PAGE 23.Jul 24, 1998 · N18544 · Doug DC932 · Wing, Plate/SkinSDR CALA9801343Skin · corrodedINSPECTION FOUND LT AND RT WHEEL WELL KEEL SKIN AREA CORRODED AT STA 680 TO 756. THE CORRODED SECTION OF KEEL SKIN WAS REMOVED IAW SRM 53-04, FIGURE 42. A NEW SECTION OF SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 53-04, FIGURE 4Jul 24, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801318Seat Track · corrodedINSPECTION FOUND SEAT TRACKS CORRODED AT STA 237 RT O/B AND STA 803-845, LBL 48. THE CORRODED SECTIONS OF SEAT TRACKS WERE CUT OUT. NEW SEAT TRACKS, SPLICES, AND PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F AND 51-30-1.Jul 21, 1998 · N18544 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801283Skin · crackedINSPECTION FOUND A 1 INCH CRACK COMING FROM RIVET HOLE IN FORWARD CARGO DOOR AT STA 425. THE CRACK WAS STOP DRILLED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 52-03, 52-31-0 AND 51-70-2.Jul 20, 1998 · N18544 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801282Floor Panel · delaminatedINSPECTION FOUND FLOOR PANEL DELAMINATED AT STA 756 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND 51-10-3.Jul 20, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801268Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 294, STRINGER 27R. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW ECRA 5320-01263. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 532Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801267Intercostal · crackedINSPECTION FOUND TWO CRACKS IN INTERCOSTAL AT STA 996 TO 1019, RBL 20. THE CRACKS WERE STOP DRILLED, AN ANGLE STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-30-2, AND 51-30-0.Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801266Skin · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE TO SKIN BELOW FLOOR LINE AT WING SCAN LIGHT AT STA 522. A DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38.Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801265Floor Panel · separatedINSPECTION FOUND FLOOR PANEL SKIN SEPARATING AT STA 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, PAGE 11 AND 53-05, PAGE 122B.Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801264Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 980, RBL 21 AND RBL 34. THE CORRODED AREAS WERE CUT OUT, AN ANGLE, FILLER, AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A.Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801263Stringer · corrodedINSPECTION FOUND STRINGER/FRAME CORRODED AROUND FASTENERS AT KEEL BOX INTERIOR, STA 598, STRINGER 29R. THE KEEL BOX WEB WAS REMOVED. TWO REPAIR ANGLES WERE FABRICATED IAW SRM 53-01, FIGURE 2 AND 51-10-2A. THE ANGLES AND KEEL BOX PANEL WERE INSTALLED IAW SRM Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801261Angle · corrodedINSPECTION FOUND FLOOR GILL LINING ATTACH ANGLE CORRODED IN AFT CARGO COMPARTMENT AT STA 996, BL 0 TO LBL 6. THE CORRODED SECTION OF ANGLE WAS CUT OUT. TWO L-ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30Jul 16, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801257Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT RT DORSAL FIN LOWER FORWARD ACCESS PANEL. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801256Floor Panel · brokenINSPECTION FOUND FLOOR PANEL BROKEN AT STA 522 TO 579. THE FLOOR PANEL WAS REMOVED IAW MM 53-20-0. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-20-0 AND 53-21-0.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801255Floorbeam · crackedINSPECTION FOUND A 4 INCH CRACK IN RADIUS OF FORWARD CARGO FLOORBEAM AT STA 351, BL 0. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 78.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801254Cusp · corrodedINSPECTION FOUND CUSP CORRODED AT FS 986, RBL 62. THE CORRODED AREA OF CUSP WAS CUT OUT. A REPAIR CUSP AND L-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-05, 51-20-2, AND 51-10-30.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801253Bracket · crackedINSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF LT WING SUPPORT BRACKET, XRS 332. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-1, 51-10-2, 51-10-2A, AND 51-10-3.Jul 15, 1998 · N18544 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9801252Floor Panel · corrodedINSPECTION FOUND FORWARD PIT FLOOR PANEL CORRODED AND DELAMINATED AT STA 313 TO 357. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801251Clip · crackedINSPECTION FOUND RT WING LEADING EDGE RIB CLIP CRACKED JUST INBOARD OF WS XOS 429. THE CRACK WAS STOP DRILLED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.Jul 15, 1998 · N18544 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9801250Frame · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE ON WINDOW FRAMES 28 TO 30R. REPAIRED IAW ECRA 5330-02683.Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801248Web · corrodedINSPECTION FOUND WEB CORRODED AT CUSP LINE FORWARD AND AFT OF FRAME FITTING AT STA 237 ON LT SIDE. THE CORRODED AREA OF WEB WAS CUT OUT, A REPAIR WEB AND L-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-01, PAGE 9.Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801247End Caps · corrodedINSPECTION FOUND LONGERON 20R AND 21R END CAPS CORRODED IN AFT CARGO COMPARTMENT AT STA 996. THE END CAPS WERE REMOVED IAW SRM 51-30-2. NEW END CAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801246Floor Panel · delaminatedINSPECTION FOUND FORWARD PIT FLOOR PANEL DELAMINATED AT STA 218 TO 313. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801245Floor Panel · crackedINSPECTION FOUND FORWARD CARGO PIT FLOOR PANEL CRACKED AT ST 427 TO 522. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801239Floor · corrodedINSPECTION FOUND CABIN FLOOR PANEL CORRODED FORWARD OF RT AFT LAV AT STA 945 TO 965, RBL 44. THE FLOOR PANEL WAS REMOVED AND THE CORRODED SECTIONS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-10-3, AND 51-30-2. THE FLOOR PAJul 12, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801241Longeron · crackedINSPECTION FOUND LONGERON 16R CRACKED AT UPPER FLANGE AND LONGERON 16L CRACKED OUT OF UPPER AND LOWER ATTACH CLIP FASTENERS, STA 965. THE CRACKED AREAS OF LONGERONS WERE REMOVED IAW SRM 51-30-2. LONGERONS AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-Jul 11, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801240Longeron · crackedINSPECTION FOUND THREE CRACKS IN LONGERON 17R AT FRAME ATTACH HOLES FROM STA 945 TO 980. THE CRACKS WERE .5 TO 1 INCH LONG. THE CRACKED AREAS OF LONGERON WERE REMOVED IAW SRM 53-02, FIGURE 18. LONGERON REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIJul 11, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801238Fitting · crackedINSPECTION FOUND A 7 INCH CRACK IN KEEL BEAM FITTING AT BS 756, LONGERON 30. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-5 AND 51-30-1, PAGE 6.Jul 11, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801237Floor · corrodedINSPECTION FOUND FLOOR PANEL CORRODED AT STA 229 TO 294, BL 0. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 53-10-4, 51-20-2, 51-10-3, AND 51-30-2.Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR CALA9801236Doubler · bulgedINSPECTION FOUND DOUBLER BULGED WITH FASTENERS PULLING THROUGH AT STA 1019, LONGERON 19L. THE DOUBLER WAS REMOVED IAW SRM 51-10-2. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 53-04, FIGURE 12B.Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801235Channel · crackedINSPECTION FOUND A .5 INCH CRACK AROUND FASTENER HOLE IN CHANNEL AT FORWARD CARGO DOOR FRAME STA 389, S18R, RBL 52. THE CHANNEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801228Skin · corrodedINSPECTION FOUND SKIN CORRODED AT AFT CARGO COMPARTMENT FRAME STA 945 BETWEEN LONGERON 25R AND 26R. THE CORRODED AREA WAS CUT OUT. A REPAIR DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-04, FIGURE 12, SHEEJul 9, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801227Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORROSION AT STA 980, LBL 34, STA 996, LBL 27, AND STA 965, LBL 16. L-ANGLES AND FILLERS WERE FABRICATED AND INSTALLED AT EACH LOCATION IAW SRM 53-05, FIGURE 20A AND 51-10-3.Jul 9, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor Beam
Back to N18544, cancelled Aug 30, 1999