# Service difficulty reports: N93738, cancelled Apr 12, 2000

A list on [N93738, cancelled Apr 12, 2000](https://openairdocs.org/deregistered/N93738-2000-04-12.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 3 · 101 reports

- [SDR CALA9802082](https://openairdocs.org/sdr/CALA9802082.md): Bearing · worn · Nov 17, 1998 · N93738 · Boeing 727224 · Landing Gear Door Retract Section
  > THE NOSE GEAR DOORS OPEN LIGHT ON BOTH THE FORWARD AND SECOND OFFICER'S PANELS WERE ILLUMINATED AFTER GEAR RETRACTION DEPARTING BWI. THE WARNING LIGHTS WERE ACCOMPANIED BY RUMBLING AIR NOISE. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT WAS DIVERTED TO
- [SDR CALA9801933](https://openairdocs.org/sdr/CALA9801933.md): Floorbeam · corroded · Oct 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor Beam
  > FLOORBEAM TOP HAS SURFACE CORROSION FS 1130 RBL 12-12. REMOVED FASTENERS. CUT OUT ANGLE DAMAGE. FABRICATED NEW ANGLE, SPLICES. FABRICATED NEW FLOORBEAM TREATED AND INSTALLED PER SRM 51-10-2 AND 51-40-3.
- [SDR CALA9801932](https://openairdocs.org/sdr/CALA9801932.md): Skin · worn · Oct 9, 1998 · N93738 · Boeing 727224 · Spoilers
  > RT WING NR 8 SPOILER CENTER CHAFE PAD WORN AND TE WORN/MISSING. DENTS OUT OF LIMITS PER SRM 57-50-1 FIG 5. REMOVED SPOILER PANEL AND SENT OUT FOR REPAIR PER MM 27-62-1.
- [SDR CALA9801931](https://openairdocs.org/sdr/CALA9801931.md): Fitting · corroded · Oct 9, 1998 · N93738 · Boeing 727224 · Wing, Fuselage Attach Fittings
  > RIGHT WING TO FUSELAGE AT BS 870 FACE AND BORE HAVE CORROSION. ACCOMPLISHED REPAIR BY OVERSIZE HOLE TO REMOVE CORROSION PER ECRA 5310-63775.
- [SDR CALA9801929](https://openairdocs.org/sdr/CALA9801929.md): Fitting · corroded · Oct 9, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND THE NR 2 AND NR 3 FLAP TRACK FORWARD MOUNT FITTINGS CORRODED. THE FLAP TRACK FITTINGS WERE REPAIRED IAW ECRA 5740-01277.
- [SDR CALA9801928](https://openairdocs.org/sdr/CALA9801928.md): Fitting · corroded · Oct 9, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 6 AND NR 8 FLAP TRACK ATTACH FITTINGS CORRODED. THE CORROSION WAS REMOVED AND THE FITTINGS WERE REPAIRED IAW ECRA 5740-01277.
- [SDR CALA9801912](https://openairdocs.org/sdr/CALA9801912.md): Bottle Pin · corroded · Oct 5, 1998 · N93738 · Boeing 727224 · Wing, Fuselage Attach Fittings
  > INSPECTION FOUND RT WING TO FUSELAGE BOTTLE PIN, BUSHING, AND RETAINING BOLT CORRODED AT BS 870. THE BOTTLE PIN, BUSHING, AND RETAINING BOLT WERE REMOVED AND REPLACED IAW MM 57-41-1, PAGE 403 AND 57-41-11, PAGE 404.
- [SDR CALA9801911](https://openairdocs.org/sdr/CALA9801911.md): Aileron Tab · dented · Oct 5, 1998 · N93738 · Boeing 727224 · Aileron Tabs
  > INSPECTION FOUND LT INBOARD AILERON TAB DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-31.
- [SDR CALA9801809](https://openairdocs.org/sdr/CALA9801809.md): Skin · delaminated · Sep 18, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND RT INBOARD FOREFLAP SKIN DELAMINATED AT LOWER SURFACE INBOARD MOST END. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9801795](https://openairdocs.org/sdr/CALA9801795.md): Skin · corroded · Sep 16, 1998 · N93738 · Boeing 727224 · Elevator, Plate/Skin
  > INSPECTION FOUND CORROSION IN LT ELEVATOR UPPER TRAILING EDGE SKIN BETWEEN STATIC WICKS. THE CORROSION WAS REMOVED, DOUBLERS WERE INSTALLED IAW SRM 55-20-03.
- [SDR CALA9801794](https://openairdocs.org/sdr/CALA9801794.md): Panel · cracked · Sep 16, 1998 · N93738 · Boeing 727224 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10, 51-10-2 AND 51-30-2.
- [SDR CALA9801793](https://openairdocs.org/sdr/CALA9801793.md): Fitting · corroded · Sep 16, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND FITTING CORRODED WHERE RT WING NR 5 FLAP TRACK MOUNTS. THE FITTING AND BUSHING WERE REMOVED AND REPLACED IAW MM 32-11-51, PAGE 401 TO 403 AND MM 20-70-7.
- [SDR CALA9801792](https://openairdocs.org/sdr/CALA9801792.md): Channel · corroded · Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT LAV FLOOR WAS HAT CHANNEL CORRODED AT FS 1140, RBL 24 TO 60. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2, 51-30-1, AND 51-20-1.
- [SDR CALA9801780](https://openairdocs.org/sdr/CALA9801780.md): Seat Track · corroded · Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 348, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5 AND 51-10-2.
- [SDR CALA9801779](https://openairdocs.org/sdr/CALA9801779.md): Floorbeam · corroded · Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND MOUNT HOLES AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8.
- [SDR CALA9801769](https://openairdocs.org/sdr/CALA9801769.md): Angle · cracked · Sep 15, 1998 · N93738 · Boeing 727224 · Vertical Stabilizer
  > INSPECTION FOUND A.25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.
- [SDR CALA9801768](https://openairdocs.org/sdr/CALA9801768.md): Intercostal · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK AT TOP FLANGE OF INTERCOSTAL THREE INCHES AFT OF FLOOR FRAME FS 970, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.
- [SDR CALA9801767](https://openairdocs.org/sdr/CALA9801767.md): Support · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL AT FS 1120, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-20-1 FIGURE 7.
- [SDR CALA9801766](https://openairdocs.org/sdr/CALA9801766.md): Stringer · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 683 TO 688. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3, FIGURE 6. A REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 6 AND 51-10-2.
- [SDR CALA9801765](https://openairdocs.org/sdr/CALA9801765.md): Support · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1034, RBL 12-24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-00 AND 51-10-2.
- [SDR CALA9801745](https://openairdocs.org/sdr/CALA9801745.md): Panel · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Wing, Plate/Skin
  > INSPECTION FOUND A.375 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 12 SPOILER INBOARD HINGE AREA. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4 AND 51-30-2.
- [SDR CALA9801744](https://openairdocs.org/sdr/CALA9801744.md): Angle · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT RT INBOARD MIDFLAP JUST OUTBOARD OF NR 5 FLAP CARRIAGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9801743](https://openairdocs.org/sdr/CALA9801743.md): Pad · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND CORROSION AT RT WING AFT FALSE SPAR PAD WHERE NR 5 AND NR 6 FLAP TRACKS MOUNT. THE FLAP TRACK MOUNT PADS WERE REMOVED IAW SRM 51-30-2. NEW MOUNT PADS WERE INSTALLED IAW SRM 51-10-6, 51-10-1, AND 51-30-2.
- [SDR CALA9801742](https://openairdocs.org/sdr/CALA9801742.md): Skin · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Elevator, Plate/Skin
  > INSPECTION FOUND LT ELEVATOR SKIN UPPER SURFACE CORRODED AROUND STATIC WICK BASE. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-20-03.
- [SDR CALA9801741](https://openairdocs.org/sdr/CALA9801741.md): Skin · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND A.75 INCH AND.1093 INCH CRACK IN RT WING LOWER TRAILING EDGE OF INBOARD MIDFLAP, 34 INCHES FROM INBOARD END. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 57-50-4, FIGURE 1.
- [SDR CALA9801740](https://openairdocs.org/sdr/CALA9801740.md): Skin · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND A.3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHES FROM INBOARD END. A DOUBLER WAS INSTALLED IAW SRM 57-50-4, FIGURE 1, 51-10-6, AND 51-10-2.
- [SDR CALA9801739](https://openairdocs.org/sdr/CALA9801739.md): Channel · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LAV FLOOR HAT CHANNEL CORRODED AT FS 1140-1170, RBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-2, AND 51-40-5.
- [SDR CALA9801738](https://openairdocs.org/sdr/CALA9801738.md): Angle · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Leading Edge Devices
  > INSPECTION FOUND A.375 INCH CRACK IN NR 2 SLAT PANEL ATTACH ANGLE BY ANTI-ICE DUCT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, FIGURE 4.
- [SDR CALA9801737](https://openairdocs.org/sdr/CALA9801737.md): Angle · cracked · Sep 14, 1998 · N93738 · Boeing 727224 · Leading Edge Devices
  > INSPECTION FOUND A.375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3.
- [SDR CALA9801736](https://openairdocs.org/sdr/CALA9801736.md): Track · corroded · Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND NR 4 FLAP TRACK FORWARD CLEVIS CORRODED ON BOTH SIDES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801705](https://openairdocs.org/sdr/CALA9801705.md): Angle · cracked · Sep 10, 1998 · N93738 · Boeing 727224 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-3, F
- [SDR CALA9801704](https://openairdocs.org/sdr/CALA9801704.md): Bracket · cracked · Sep 10, 1998 · N93738 · Boeing 727224 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2.
- [SDR CALA9801703](https://openairdocs.org/sdr/CALA9801703.md): Doubler · cracked · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN DOUBLER INSIDE LT INBOARD FLAP AT AFT END OF INBOARD FLAP TRACK CARRIAGE SPINDLE CUTOUT. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2.
- [SDR CALA9801702](https://openairdocs.org/sdr/CALA9801702.md): Rib · cracked · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND A 1.5 INCH CRACK IN LT O/B MIDFLAP O/B END RIB FORWARD OF MID SPAR. THE CRACK WAS STOP DRILLED. A DOUBLER ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.
- [SDR CALA9801701](https://openairdocs.org/sdr/CALA9801701.md): Skin · dented · Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN AND RIB DENTED JUST AFT OF NLG AFT DOOR. THE RIB AND SKIN WERE REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9801700](https://openairdocs.org/sdr/CALA9801700.md): Pad · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Wing Miscellaneous Structure
  > INSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PAGE 1 AND 51-30-2, PAGE 14.
- [SDR CALA9801699](https://openairdocs.org/sdr/CALA9801699.md): Track · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801695](https://openairdocs.org/sdr/CALA9801695.md): Track · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 8 FLAP TRACK FORWARD ATTACH LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801694](https://openairdocs.org/sdr/CALA9801694.md): Bracket · cracked · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flap Actuator
  > INSPECTION FOUND A.5 INCH CRACK IN OUTBOARD BRACKET WHERE RT WING NR 5 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.
- [SDR CALA9801693](https://openairdocs.org/sdr/CALA9801693.md): Hat Channel · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND HAT CHANNEL CORRODED AT FS 1150, LBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.
- [SDR CALA9801692](https://openairdocs.org/sdr/CALA9801692.md): Support · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801691](https://openairdocs.org/sdr/CALA9801691.md): Skin · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Elevator, Plate/Skin
  > INSPECTION FOUND RT ELEVATOR SKIN LOWER SURFACE CORRODED. THE CORRODED AREA WAS CUT OUT AND A NEW FITTING AND DOUBLER WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2, 51-10-2, AND 51-40-5.
- [SDR CALA9801690](https://openairdocs.org/sdr/CALA9801690.md): Carriage · corroded · Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flaps
  > INSPECTION FOUND NR 7 FLAP OUTBOARD FLAP INBOARD CARRIAGE CORRODED. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 57-53-2.
- [SDR CALA9801679](https://openairdocs.org/sdr/CALA9801679.md): Floorbeam · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 22.5 TO 24.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-8 AND 51-30-2.
- [SDR CALA9801678](https://openairdocs.org/sdr/CALA9801678.md): Angle · cracked · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.375 CRACK IN ANGLE AT INTERCOSTAL AT BS 950A-950B, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.
- [SDR CALA9801677](https://openairdocs.org/sdr/CALA9801677.md): Support · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1067, RBL 12-24 AND RBL 45-65. THE FLOOR SUPPORTS WERE REMOVED AND A NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1AND 51-10-2.
- [SDR CALA9801676](https://openairdocs.org/sdr/CALA9801676.md): Support · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 24-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.
- [SDR CALA9801675](https://openairdocs.org/sdr/CALA9801675.md): Web · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT WEB CORRODED AT FS 1122, RBL 65. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-2, 51-10-1, PAGE 4, AND 51-30-2.
- [SDR CALA9801674](https://openairdocs.org/sdr/CALA9801674.md): Floorbeam · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT TOP FLANGE SCREW HOLE FS 1050, RBL 35. THE CORRODED AREA WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 53-10-5, FIGURE 7.
- [SDR CALA9801673](https://openairdocs.org/sdr/CALA9801673.md): Support · corroded · Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-1, AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N93738-2000-04-12/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 = 'N93738' AND deregistration_id = 'N93738-2000-04-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N93738-2000-04-12/reports

---
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