# Service difficulty reports: N10251, cancelled Apr 17, 1999

A list on [N10251, cancelled Apr 17, 1999](https://openairdocs.org/deregistered/N10251-1999-04-17.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 · 59 reports

- [SDR CALA9801570](https://openairdocs.org/sdr/CALA9801570.md): Power Supply · inoperative · Aug 27, 1998 · N10251 · Boeing 737291 · Emergency Lighting
  > INSPECTION FOUND SECTION OF EMERGENCY FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE FOUND THE M913 POWER SUPPLY AT STA 776 AT FAULT. THE M913 POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY FLOOR PATH LIGHTING WAS RESTORED.
- [SDR CALA9800999](https://openairdocs.org/sdr/CALA9800999.md): Frame · cracked · Jun 9, 1998 · N10251 · Boeing 737291 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3 INCH CRACK AT FORWARD LOWER CORNER OF DOOR FRAME JUST BELOW OPEN LATCH ASSEMBLY OF FORWARD CARGO DOOR. THE AREA WAS REPAIRED IAW SRM 51-10-2.
- [SDR CALA9800919](https://openairdocs.org/sdr/CALA9800919.md): Fire Detector · inoperative · May 29, 1998 · N10251 · Boeing 737291 · Fire Detection
  > THE APU FIRE WARNING LIGHT AND BELL ACTIVATED, WITH APU OFF, WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT AND BELL CONTINUED TO ACTIVATE INTERMITTENTLY. THE AIRCRAFT WAS DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUN
- [SDR CALA9800876](https://openairdocs.org/sdr/CALA9800876.md): Skin · dented · May 17, 1998 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 294.5, STRINGER 14. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9800888](https://openairdocs.org/sdr/CALA9800888.md): Beam · cracked · May 16, 1998 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TRANSVERSE BEAM CRACKED IN RADIUS FORWARD AND AFT IN THREE EACH PLACES AT STA 675, RBL 24, WBL 208. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. THE CRACKS WERE STOP DRILLED. A REPAIR WAS INSTALLED IAW SA001-5710-01638.
- [SDR CALA9800887](https://openairdocs.org/sdr/CALA9800887.md): Frame · cracked · May 16, 1998 · N10251 · Boeing 737291 · Fuselage Main, Frame
  > INSPECTION FOUND A 1.5 CRACK IN RADIUS OF FRAME AT STA 675, RBL 24, WBL 208 AND A 1.5 CRACK IN FRAME AT STA 675, LBL 24, WBL 208. REPAIRS WERE PERFORMED IAW SA001-5710-01638.
- [SDR CALA9800875](https://openairdocs.org/sdr/CALA9800875.md): Tear Strap · corroded · May 16, 1998 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FRAME TO SKIN TEAR STRAP CORRODED AT BS 360, STRINGER 29R. REPAIRED IAW SRM 53-30-3.
- [SDR CALA9800874](https://openairdocs.org/sdr/CALA9800874.md): Web · cracked · May 16, 1998 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.25 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT FRAME AFT FACE OF WEB AT BS 492.4, STRINGER 25R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.
- [SDR CALA9800873](https://openairdocs.org/sdr/CALA9800873.md): Splice · cracked · May 16, 1998 · N10251 · Boeing 737291 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1 CRACK IN LT WING LANDING GEAR BEAM AFT SPLICE PLATE AT FS 727. THE SPLICE PLATE WAS REPAIRED IAW DRAWING NR 65C292288.
- [SDR CALA9800855](https://openairdocs.org/sdr/CALA9800855.md): Threshold · cracked · May 14, 1998 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > AFT PIT THRESHOLD AFT CORNER CRACKED (3.5). REMOVED AFT PIT THRESHOLD CORNER AND INSTALLED A NEW CORNER PER SRM 51-30-2.
- [SDR CALA9800826](https://openairdocs.org/sdr/CALA9800826.md): Skin · dented · May 11, 1998 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED STA 259 BETWEEN STR 23R AND 24R. FABRICATED, PRIMED, SEALED, AND INSTALLED DOUBLER PER SRM 53-30-3, 51-10-2 AND 51-20-4.
- [SDR CALA9800827](https://openairdocs.org/sdr/CALA9800827.md): Floor Panel · cracked · May 10, 1998 · N10251 · Boeing 737291 · Fuselage Floor Panel
  > FLOOR PANEL FWD PIT FS 380 TO 420 HAS TEARS. FABRICATED FWD PIT PANEL PER ECRA 2550-01046.
- [SDR CALA9800817](https://openairdocs.org/sdr/CALA9800817.md): Skin · dented · May 7, 1998 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT STA 905 STR 22R. REMOVED DAMAGED AREA, FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED PER SRM 53-30-1, 53-30-3, 51-20-2, AND MM 51-21-11.
- [SDR CALA980800](https://openairdocs.org/sdr/CALA980800.md): Doubler · chafed · May 6, 1998 · N10251 · Boeing 737291 · Engine Cowling System
  > NUMBER ONE ENGINE O/B COWLING NUMBER SIX RIB CHAFED AT DOUBLER REPAIR. REMOVED DOUBLER AND FILLER MATERIAL. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER PER SRM 51-40-3, 51-10-2, AND MM 51-20-11.
- [SDR CALA9800801](https://openairdocs.org/sdr/CALA9800801.md): Angle · cracked · May 6, 1998 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM ATTACH ANGLE CRACKED STA 520 BL 0.0. REMOVED CRACKED ATTACH ANGLE. FABRICATED, TREATED, PRIMED AND INSTALLED NEW ANGLE PER SRM 51-40-3, 51-10-2 AND MM 51-20-0.
- [SDR CALA9800799](https://openairdocs.org/sdr/CALA9800799.md): Skin · cracked · May 6, 1998 · N10251 · Boeing 737291 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR INNER SKIN CRACKED (1/2). FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-2, 51-10-2, 51-30-2 AND MM 51-20-0.
- [SDR CALA9800790](https://openairdocs.org/sdr/CALA9800790.md): Skin · dented · May 6, 1998 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > LOWER RIGHT SIDE AFT FUSELAGE AT BS 787 STR R26 DENTED FORWARD OF AFT CARGO DOOR CUTOUT. REMOVED DAMAGED AREA. INSTALLED REPAIR PER SRM 53-30-1, 51-00-00, 53-30-1, 51-10-2, 53-30-3 AND MM 25-52-1.
- [SDR CALA9700384](https://openairdocs.org/sdr/CALA9700384.md): Bulkhead · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A SIX INCH CRACK IN BULKHEAD AT STA 178, WL 208, RBL 18. ALSO, A SIX INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, WL 208, LBL 16. THE CRACKED AREAS WERE REMOVED IAW SRM 53-10-11. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-1
- [SDR CALA9700383](https://openairdocs.org/sdr/CALA9700383.md): Skin · punctured · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS PUNCTURED APPROXIMATELY FIVE FEET AFT OF L-1 DOOR SILL. THE PUNCTURED AREA OF SKIN AND DOUBLER WERE CUT OUT IAW SRM 53-30-3. A REPAIR DOUBLER, FILLER, AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, AND 51-30-2.
- [SDR CALA9700382](https://openairdocs.org/sdr/CALA9700382.md): Angle · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR ATTACH ANGLE CORRODED FROM BS 290 TO 360, LBL 65. REMOVED CHORD AND INSTALLED NEW CHORD IAW SRM 51-30-2. A DOUBLER AND FILLER FLOOR WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.
- [SDR CALA9700381](https://openairdocs.org/sdr/CALA9700381.md): Splice · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN STRINGER 27R SPLICE AT STA 420. THE CRACKED SPLICE WAS REMOVED, A NEW SPLICE WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65-45769 AND SRM 51-30-2.
- [SDR CALA9700380](https://openairdocs.org/sdr/CALA9700380.md): Web · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LT WEB CORRODED IN AN AREA APPROXIMATELY 20 BY 8.5 AT STA 1016. THE CORRODED WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA9700379](https://openairdocs.org/sdr/CALA9700379.md): Floorbeam · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Floor Beam
  > INSPECTION FOUND RT FLOORBEAM CORRODED AT STA 1016. THE CORRODED AREA OF FLOORBEAM CAP WAS CUT OUT, A NEW CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.
- [SDR CALA9700378](https://openairdocs.org/sdr/CALA9700378.md): Web · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT OUTBOARD WEB AT STA 996 TO 1016 CORRODED AND DELAMINATED APPROXIMATELY 10 BY 1.5 IN AREA. THE WEB AND TWO FLOOR SUPPORTS WERE REMOVED, A NEW WEB AND FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65-46812 AND SRM 51-30-2.
- [SDR CALA9700377](https://openairdocs.org/sdr/CALA9700377.md): Channel · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT COAT CLOSET FORWARD BULKHEAD FLOOR CHANNEL CORRODED ON TOP AND BOTTOM. THE CHANNEL WAS REMOVED AND A REPLACEMENT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-7 AND 51-30-2.
- [SDR CALA9700376](https://openairdocs.org/sdr/CALA9700376.md): Skin · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND.125 INCH CRACKS AT EIGHT FASTENER HOLES IN RT SECTION 41 SKIN PANEL. THE SKIN PANEL WAS REMOVED AND THE AREA WAS CLEANED IAW SRM 51-30-2 AND 51-10-2. FASTENER HOLES WERE DRILLED IN NEW SKIN AND SKIN WAS INSTALLED IAW SRM 51-10-2, 51-10-7 AN
- [SDR CALA9700375](https://openairdocs.org/sdr/CALA9700375.md): Skin · dented · Mar 7, 1997 · N10251 · Boeing 737291 · Cargo/Baggage Doors
  > INSPECTION FOUND SKIN DENTED AND BUCKLED AT FORWARD CARGO DOOR. THE SKIN WAS REMOVED AND NEW SKIN WAS FABRICATED IAW BOEING DRAWING 65-46921. THE SKIN WAS INSTALLED IAW SRM 51-30-2. THE FORWARD LOWER CORNER FRAME WAS REMOVED, NEW HOLES WERE LOCATED AND THE
- [SDR CALA9700374](https://openairdocs.org/sdr/CALA9700374.md): Intercostal · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN INTERCOSTAL AT BS 420 TO 440, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9700373](https://openairdocs.org/sdr/CALA9700373.md): Support Beam · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON TOP CAP OF LT DIAGONAL SUPPORT BEAM AT STA 996 TO 1006. THE SUPPORT BEAM WAS REMOVED AND A NEW SUPPORT BEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.
- [SDR CALA9700372](https://openairdocs.org/sdr/CALA9700372.md): Stringer · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 26L AT STA 420. THE CRACKED AREA OF STRINGER WAS CUT OUT IAW SRM 53-10-3. A NEW STRINGER SECTION, SPLICES, AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.
- [SDR CALA9700371](https://openairdocs.org/sdr/CALA9700371.md): Angle · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER ATTACH ANGLE AT STA 142 CENTER SPAR LEADING EDGE. THE CRACK WAS STOP DRILLED IAW SRM 55-10-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 55-10-4 AND 51-30-2.
- [SDR CALA9700370](https://openairdocs.org/sdr/CALA9700370.md): Angle · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > A 1 INCH CRACK WAS FOUND BETWEEN FASTENER HOLES IN RT MLG WHEEL WELL UPPER FORWARD ATTACH ANGLE AT STA 664, STATION 18A SHEAR BEAM. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 65C29228.
- [SDR CALA9700369](https://openairdocs.org/sdr/CALA9700369.md): Pan · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LAV SERVICE CENTER PAN STRUCTURE CORRODED AT STA 1006. CHANNELS WERE FABRICATED IAW BOEING DRAWING 69-36677 AND A NEW LAV PAN STRUCTURE WAS FABRICATED IAW SRM 51-30-5. INSTALLATION WAS PERFORMED IAW SRM 51-30-2.
- [SDR CALA9700368](https://openairdocs.org/sdr/CALA9700368.md): Floorbeam · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED FROM STA 1006 TO 1016, BBL 0. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65-46812 AND SRM 51-30-2.
- [SDR CALA9700367](https://openairdocs.org/sdr/CALA9700367.md): Web · corroded · Mar 7, 1997 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION IN AFT RT WEB AT STA 1016 TO 1022. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA9700366](https://openairdocs.org/sdr/CALA9700366.md): Support · cracked · Mar 7, 1997 · N10251 · Boeing 737291 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN RT WING FLAP WELL UPPER TRAILING EDGE PANEL SUPPORT JUST AFT OF AFT SPAR AT STA RSS 446.94. THE T-CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-7.
- [SDR CALA9700295](https://openairdocs.org/sdr/CALA9700295.md): Skin · cracked · Feb 25, 1997 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CRACKS AT EIGHT FASTENERS IN RT SECTION 41 SKIN PANEL. THE CRACKS WERE APPROXIMATELY.5 INCH LONG. THE SKIN PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-7, AND 51-20-4.
- [SDR CALA9601922](https://openairdocs.org/sdr/CALA9601922.md): Seal · leaking · Dec 31, 1996 · N10251 · Boeing 737291 · Turbine Section
  > THE NR 1 ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL WHILE EN ROUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM NR 1 ENGINE NR 6 BEARING GIT SEAL. THE NR 6 BEARING GIT SEAL WAS REMOVED AND REPLACED. THE ENGINE WAS SERVICED W
- [SDR CALA9600649](https://openairdocs.org/sdr/CALA9600649.md): Sensor · out of adjust · May 28, 1996 · N10251 · Boeing 737291 · Landing Gear Position and Warning
  > THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF. THE LANDING GEAR REMAINED DOWN WITH THREE GREEN LIGHTS AT ALL TIMES. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING THE LEVER LOCK SYSTEM IAW MM
- [SDR CAL960602](https://openairdocs.org/sdr/CAL960602.md): Battery Pack · discharged · May 2, 1996 · N10251 · Boeing 737291 · Emergency Lighting
  > GSO - THE AFT RT SERVICE DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X)
- [SDR CAL960601](https://openairdocs.org/sdr/CAL960601.md): Battery Pack · discharged · May 2, 1996 · N10251 · Boeing 737291 · Emergency Lighting
  > GSO - THE FORWARD RT SERVICE DOOR SLIDE LIGHT HAD NO VOTLAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X)
- [SDR CAL960600](https://openairdocs.org/sdr/CAL960600.md): Battery Pack · discharged · May 2, 1996 · N10251 · Boeing 737291 · Emergency Lighting
  > GSO - THE AFT LT ENTRY DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED AND LIGHTS ON. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X)
- [SDR CAL960597](https://openairdocs.org/sdr/CAL960597.md): Skin · corroded · Apr 30, 1996 · N10251 · Boeing 737291 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND LT AFT CORNER OF NOSE WHEELWELL CUT-OUT EXTERNAL SKIN CORRODED AT STA 294.5. THE CORRODED AREA OF SKIN AND BEAR STRAP WERE CUT OUT. STRAP FILLER, SKIN FILLER, AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 53-30-2
- [SDR CAL960596](https://openairdocs.org/sdr/CAL960596.md): Panel · cracked · Apr 30, 1996 · N10251 · Boeing 737291 · Wing, Plate/Skin
  > GSO - INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD OUTBOARD CORNER OF LT WING UPPER TRAILING EDGE PANEL FORWARD OF NR 4 SPOILER. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2. (X)
- [SDR CAL960599](https://openairdocs.org/sdr/CAL960599.md): Door Frame · cracked · Apr 29, 1996 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A 3 INCH CRACK IN AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME. THE FRAME SECTION WAS REMOVED AND REPLACED IAW EA 5310-02555. (M)
- [SDR CAL960598](https://openairdocs.org/sdr/CAL960598.md): Angles · cracked · Apr 28, 1996 · N10251 · Boeing 737291 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND FOUR EACH ATTACH ANGLES CRACKED AT LT MLG STR 18A SHEAR BEAM. THE CRACKS MEASURED FROM 2 TO 5 INCHES IN LENGTH. THE ANGLES WERE REMOVED AND NEW ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-03254. (X)
- [SDR CAL950212](https://openairdocs.org/sdr/CAL950212.md): Door · cracked · Mar 15, 1995 · N10251 · Boeing 737291 · Cargo/Baggage Doors
  > GSO - INSPECTION FOUND A 1.2 INCH CRACK IN AFT CARGO DOOR ON THE INSIDE RIGHT CORNER UNDER DOUBLER. THE CRACK WAS REPAIRED BY FABRICATING AND INSTALLING DOUBLER AND FILLER IAW SRM 51-40-3. (X)
- [SDR CAL950211](https://openairdocs.org/sdr/CAL950211.md): Slat · cracked · Mar 15, 1995 · N10251 · Boeing 737291 · Leading Edge Devices
  > GSO - INSPECTION FOUND A 1.1 INCH CRACK IN THE NR 2 SLAT INBOARD AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS REMOVED IAW SRM 57-30-4 AND REPAIR FILLER AND DOUBLER WITH SOLID FASTENERS WERE INSTALLED IAW SRM 51-30-2. (X)
- [SDR CAL950210](https://openairdocs.org/sdr/CAL950210.md): Le Rib · cracked · Mar 15, 1995 · N10251 · Boeing 737291 · Wing, Rib/Bulkhead
  > GSO - INSPECTION FOUND A 1.2 INCH CRACK IN RT WING LEADING EDGE RIB, JUST OUTBOARD OF NR 5 SLAT ACTUATOR. THE CRACKED SECTION WAS REMOVED IAW SRM 51-30-2 AND A REPAIR WAS INSTALLED IAW SRM 51-20-4 AND SRM 51-30-2. (X)
- [SDR CAL950209](https://openairdocs.org/sdr/CAL950209.md): Frame · cracked · Mar 15, 1995 · N10251 · Boeing 737291 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN FRAME AT BS 500B, STR 22L. THE CRACKED FRAME WAS REMOVED AND REPLACED WITH REPAIR KIT IAW BOEING DRAWING 65C25113. (X)

Next page: https://openairdocs.org/deregistered/N10251-1999-04-17/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 = 'N10251' AND deregistration_id = 'N10251-1999-04-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10251-1999-04-17/reports

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