# Service difficulty reports: N18544, cancelled Aug 30, 1999

A list on [N18544, cancelled Aug 30, 1999](https://openairdocs.org/deregistered/N18544-1999-08-30.md).

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

Page 1 of 2 · 98 reports

- [SDR CALA9900674](https://openairdocs.org/sdr/CALA9900674.md): Skin · dented · Jun 15, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900654](https://openairdocs.org/sdr/CALA9900654.md): Skin · dented · Jun 5, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900633](https://openairdocs.org/sdr/CALA9900633.md): Skin · dented · Jun 3, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BELOW LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, PAGE 218F.
- [SDR CALA9900613](https://openairdocs.org/sdr/CALA9900613.md): Skin · dented · Jun 2, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900612](https://openairdocs.org/sdr/CALA9900612.md): Rib · gouged · Jun 2, 1999 · N18544 · Doug DC932 · Wing, Rib/Bulkhead
  > INSPECTION 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.
- [SDR CALA9900590](https://openairdocs.org/sdr/CALA9900590.md): Skin · dented · May 31, 1999 · N18544 · Doug DC932 · Trailing Edge Flaps
  > INSPECTION 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.
- [SDR CALA9900589](https://openairdocs.org/sdr/CALA9900589.md): Rib · gouged · May 31, 1999 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9900588](https://openairdocs.org/sdr/CALA9900588.md): Light · dim · May 31, 1999 · N18544 · Doug DC932 · Emergency Lighting
  > INSPECTION 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.
- [SDR CALA9900564](https://openairdocs.org/sdr/CALA9900564.md): Skin · dented · May 20, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 484, LONGERONS 19 AND 20. THE SKIN WAS REPAIRED IAW SRM 53-04-04, FIGURE 38.
- [SDR CALA9900554](https://openairdocs.org/sdr/CALA9900554.md): Skin · dented · May 17, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900553](https://openairdocs.org/sdr/CALA9900553.md): Doubler · cracked · May 17, 1999 · N18544 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION 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.
- [SDR CALA9900551](https://openairdocs.org/sdr/CALA9900551.md): Skin · cracked · May 14, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900550](https://openairdocs.org/sdr/CALA9900550.md): Skin · dented · May 14, 1999 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9900462](https://openairdocs.org/sdr/CALA9900462.md): Switch · failed · Apr 28, 1999 · N18544 · Doug DC932 · Ignition Switching
  > IAH - 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
- [SDR CALA9801566](https://openairdocs.org/sdr/CALA9801566.md): Uplatch Mech · out of adjust · Aug 28, 1998 · N18544 · Doug DC932 · Landing Gear Retraction/Extension System
  > THE 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.
- [SDR CALA9801467](https://openairdocs.org/sdr/CALA9801467.md): Wire · broken · Aug 17, 1998 · N18544 · Doug DC932 · Landing Gear System Wiring
  > THE 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
- [SDR CALA9801345](https://openairdocs.org/sdr/CALA9801345.md): Skin · dented · Jul 27, 1998 · N18544 · Doug DC932 · Leading Edge Devices
  > INSPECTION 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.
- [SDR CALA9801344](https://openairdocs.org/sdr/CALA9801344.md): Skin · dented · Jul 24, 1998 · N18544 · Doug DC932 · Wing, Plate/Skin
  > INSPECTION FOUND A DENT IN LT LOWER WING SKIN AT XRS 530. THE AREA WAS REPAIRED IAW SRM 57-03, PAGE 23.
- [SDR CALA9801343](https://openairdocs.org/sdr/CALA9801343.md): Skin · corroded · Jul 24, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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 4
- [SDR CALA9801318](https://openairdocs.org/sdr/CALA9801318.md): Seat Track · corroded · Jul 21, 1998 · N18544 · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR CALA9801283](https://openairdocs.org/sdr/CALA9801283.md): Skin · cracked · Jul 20, 1998 · N18544 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION 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.
- [SDR CALA9801282](https://openairdocs.org/sdr/CALA9801282.md): Floor Panel · delaminated · Jul 20, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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.
- [SDR CALA9801268](https://openairdocs.org/sdr/CALA9801268.md): Support · cracked · Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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 532
- [SDR CALA9801267](https://openairdocs.org/sdr/CALA9801267.md): Intercostal · cracked · Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801266](https://openairdocs.org/sdr/CALA9801266.md): Skin · damaged · Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR CALA9801265](https://openairdocs.org/sdr/CALA9801265.md): Floor Panel · separated · Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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.
- [SDR CALA9801264](https://openairdocs.org/sdr/CALA9801264.md): Floorbeam · corroded · Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR CALA9801263](https://openairdocs.org/sdr/CALA9801263.md): Stringer · corroded · Jul 17, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION 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
- [SDR CALA9801261](https://openairdocs.org/sdr/CALA9801261.md): Angle · corroded · Jul 16, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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 51-30
- [SDR CALA9801257](https://openairdocs.org/sdr/CALA9801257.md): Angle · cracked · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801256](https://openairdocs.org/sdr/CALA9801256.md): Floor Panel · broken · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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.
- [SDR CALA9801255](https://openairdocs.org/sdr/CALA9801255.md): Floorbeam · cracked · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR CALA9801254](https://openairdocs.org/sdr/CALA9801254.md): Cusp · corroded · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801253](https://openairdocs.org/sdr/CALA9801253.md): Bracket · cracked · Jul 15, 1998 · N18544 · Doug DC932 · Wing Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801252](https://openairdocs.org/sdr/CALA9801252.md): Floor Panel · corroded · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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.
- [SDR CALA9801251](https://openairdocs.org/sdr/CALA9801251.md): Clip · cracked · Jul 15, 1998 · N18544 · Doug DC932 · Wing Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801250](https://openairdocs.org/sdr/CALA9801250.md): Frame · damaged · Jul 15, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON WINDOW FRAMES 28 TO 30R. REPAIRED IAW ECRA 5330-02683.
- [SDR CALA9801248](https://openairdocs.org/sdr/CALA9801248.md): Web · corroded · Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801247](https://openairdocs.org/sdr/CALA9801247.md): End Caps · corroded · Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801246](https://openairdocs.org/sdr/CALA9801246.md): Floor Panel · delaminated · Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION FOUND FORWARD PIT FLOOR PANEL DELAMINATED AT STA 218 TO 313. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.
- [SDR CALA9801245](https://openairdocs.org/sdr/CALA9801245.md): Floor Panel · cracked · Jul 14, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION FOUND FORWARD CARGO PIT FLOOR PANEL CRACKED AT ST 427 TO 522. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.
- [SDR CALA9801239](https://openairdocs.org/sdr/CALA9801239.md): Floor · corroded · Jul 12, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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 PA
- [SDR CALA9801241](https://openairdocs.org/sdr/CALA9801241.md): Longeron · cracked · Jul 11, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION 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-
- [SDR CALA9801240](https://openairdocs.org/sdr/CALA9801240.md): Longeron · cracked · Jul 11, 1998 · N18544 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION 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, FI
- [SDR CALA9801238](https://openairdocs.org/sdr/CALA9801238.md): Fitting · cracked · Jul 11, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801237](https://openairdocs.org/sdr/CALA9801237.md): Floor · corroded · Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION 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.
- [SDR CALA9801236](https://openairdocs.org/sdr/CALA9801236.md): Doubler · bulged · Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801235](https://openairdocs.org/sdr/CALA9801235.md): Channel · cracked · Jul 10, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR CALA9801228](https://openairdocs.org/sdr/CALA9801228.md): Skin · corroded · Jul 9, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION 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, SHEE
- [SDR CALA9801227](https://openairdocs.org/sdr/CALA9801227.md): Floorbeam · corroded · Jul 9, 1998 · N18544 · Doug DC932 · Fuselage Main, Floor Beam
  > INSPECTION 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.

Next page: https://openairdocs.org/deregistered/N18544-1999-08-30/reports.md?page=2

## 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 = 'N18544' AND deregistration_id = 'N18544-1999-08-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18544-1999-08-30/reports

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