# Service difficulty reports: N242WA, cancelled Jun 20, 2007

A list on [N242WA, cancelled Jun 20, 2007](https://openairdocs.org/deregistered/N242WA-2007-06-20.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 · 53 reports

- [SDR DL73S060193](https://openairdocs.org/sdr/DL73S060193.md): Skin · punctured · Mar 14, 2006 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > PUNCTURE DAMAGE TO DUE TO RUNNING A/C INTO TAILDOCK. PUNCTURE AT FS 940, BETWEEN S-19L & S-20L. TWO EXISTING REPAIRS NEAR BY. DAMAGE WAS CUT OUT AND A DOUBLER WAS INSTALLED.
- [SDR DL73S060064](https://openairdocs.org/sdr/DL73S060064.md): Floorbeam · cracked · Jan 15, 2006 · N242WA · Boeing 737247 · Fuselage Main, Floor Beam
  > THE LBL 24.8 OVERWING FLOORBEAM PREVIOUSLY MODIFIED PER 03-056673-03AD, BUT IT NO LONGER MEETS THE REQUIREMENT OF AD 2001-17-18. THE DISCREPANT CHANNEL WAS REPLACED WITH A NEW CHANNEL.
- [SDR DL73S050736](https://openairdocs.org/sdr/DL73S050736.md): Skin · cracked · Nov 21, 2005 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND IN THE FUSELAGE SKIN AT BS 727B-750, STR 18R AT THE CHEM MILL. CRACKS WERE REMOVED AND A DOUBLER INSTALLED PER ER/A 451748-14AD AND THE SRM. REF AD 2004-18-06, 2005-13-30.
- [SDR DL73S041016](https://openairdocs.org/sdr/DL73S041016.md): Skin · cracked · Nov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVELED A 4 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER EDGE AT STRINGER 18L AND FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094729-14AD.
- [SDR DL73S041015](https://openairdocs.org/sdr/DL73S041015.md): Skin · cracked · Nov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE SKIN PER AD 2004-18-06 REVEALED A 4.7 INCH CRACK ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 24L BETWEEN FS 937 & 947. THE CRACK WAS ADJACENT TO AN EXISTING REPAIR DOUBLER FOR ANOTHER SKIN CRACK CUTOUT. THE CRACK WAS REMOVED WITH A CU
- [SDR DL73S040382](https://openairdocs.org/sdr/DL73S040382.md): Transceiver · failed · Apr 30, 2004 · N242WA · Boeing 737247 · Weather Radar System
  > WX RADAR FAILED ON T/O. REPLACED R/T UNIT.
- [SDR DL73S040246](https://openairdocs.org/sdr/DL73S040246.md): Proximity Sensor · failed · Mar 18, 2004 · N242WA · Boeing 737247 · Leading Edge Slat Position Indicating System
  > DISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR.
- [SDR DL73S040103](https://openairdocs.org/sdr/DL73S040103.md): Fitting · corroded · Jan 28, 2004 · N242WA · Boeing 737247 · Empennage Flight Control Surfaces, Attach Fittings
  > DURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLEVIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES REWORKED PER ERA 3860
- [SDR DL73S040100](https://openairdocs.org/sdr/DL73S040100.md): Skin · damaged · Jan 28, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S10L LAP SPLICE BETWEEN BS 259 AND 291. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386027-14.
- [SDR DL73S040085](https://openairdocs.org/sdr/DL73S040085.md): Skin · damaged · Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LWR SKIN AT LAP SPLICE LOCATED AT S14L BETWEEN BS 345 TO BS 360. SCRIBE MARKS REMOVED AND AREA REPAIRED PER ERA 088065-14.
- [SDR DL73S040084](https://openairdocs.org/sdr/DL73S040084.md): Skin · corroded · Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > CORROSION WAS NOTED IN THE FUSELAGE SKIN AT S27L BETWEEN BS 947.50 TO 967. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386110-14.
- [SDR DL73S040083](https://openairdocs.org/sdr/DL73S040083.md): Beam · cracked · Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Structure
  > A CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 386098-14.
- [SDR DL73S040076](https://openairdocs.org/sdr/DL73S040076.md): Skin · damaged · Jan 23, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 10R LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 330-360. THE SCRIBED SECTION OF SKIN WAS CUT AND REMOVED. THE AREA WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386026-14.
- [SDR DL73S040075](https://openairdocs.org/sdr/DL73S040075.md): Skin · damaged · Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 14L LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360-540. THE LAP JOINT AND SCRIBE WERE COMPLETELY CUT OUT TO REMOVE ALL DAMAGE. THE AREA WAS RESTORED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/
- [SDR DL73S040070](https://openairdocs.org/sdr/DL73S040070.md): Bulkhead · corroded · Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Bulkhead
  > CORROSION WAS NOTED ON THE BS 1016 PRESSURE BULKHEAD, AT BL 0 AND AFFECTED BOTH THE WEB AND CHANNEL STIFFENERS. CORROSION WAS REMOVED AND DAMAGE REPAIRED PER ERA 385929-14.
- [SDR DL73S040069](https://openairdocs.org/sdr/DL73S040069.md): Skin · damaged · Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE FOUND AT THE LAP JOINT LOCATED AT S10R, BETWEEN BS 259 TO BS 290. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386028-14.
- [SDR DL73S040068](https://openairdocs.org/sdr/DL73S040068.md): Skin · damaged · Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS FOUND ON THE LOWER SKIN OF THE LAP SPLICE AT S10L, BETWEEN BS 908 TO 1016. A NEW SKIN PANEL IS TO BE INSTALLED. HOWEVER, THE NEW PANEL WAS NOTED TO HAVE DISCREPANCIES. THE SUBJECT SKIN PANEL WAS REWORKED AT BS 908, S-14L PER ERA 386020-14, IN O
- [SDR DL73S040067](https://openairdocs.org/sdr/DL73S040067.md): Skin · damaged · Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS FOUND IN THE LOWER SKIN OF THE LAP SPLICE AT S10L BETWEEN BS 908 AND 1016. THE SKIN PANEL WAS BEING REPLACED. THE NEW PANEL WAS NOTED AS HAVING SEVERAL DISCREPANCIES FROM THE MANUFACTURER. DISCREPANCIES WERE NOTED ALONG THE S20L LAP AND WERE RE
- [SDR DL73S040073](https://openairdocs.org/sdr/DL73S040073.md): Skin · damaged · Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER FUSELAGE SKIN OF THE STRINGER 14L SKIN LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE LINE WERE REMOVED WITH A CUTOUT. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER B
- [SDR DL73S040072](https://openairdocs.org/sdr/DL73S040072.md): Skin · damaged · Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 14R SKIN LAP JOINT WAS FOUND WITH A SCRIBE ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE WERE CUT OUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087866-14.
- [SDR DL73S040071](https://openairdocs.org/sdr/DL73S040071.md): Skin · damaged · Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360 TO FS 540. THE SKIN LAP JOINT WAS CUT OUT TO REMOVE THE LAP AND THE SCRIBE MARK. THE AREA WAS THEN REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS
- [SDR DL73S040065](https://openairdocs.org/sdr/DL73S040065.md): Skin · damaged · Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN PANEL AT THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 345 TO FS 360. THE LOWER SKIN WAS CUT BELOW THE SCRIBE AND THE DAMAGED SECTION REMOVED. THE CUT AND LAP JOINT WERE REPAIRED WITH 2 EXTERNAL AL
- [SDR DL73S040063](https://openairdocs.org/sdr/DL73S040063.md): Lap Joint · scratched · Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE PANEL LENGTH FROM FS 540 - FS 727. THE LAP JOINT WAS DISASSEMBLED, INSPECTED, ALL DAMAGE MACHINED AWAY, RE-INSPECTED AND RE-ASSEMBLED. THE REPAIR WAS ACCOMPLISHED
- [SDR DL73S040062](https://openairdocs.org/sdr/DL73S040062.md): Skin · scratched · Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE LAP JOINT WAS UNFASTENED, SEPARATED, ALL DAMAGE REMOVED THROUGH MACHINING, AND THOROUGHLY INSPECTED TO ENSURE NO CRACKS OR
- [SDR DL73S040054](https://openairdocs.org/sdr/DL73S040054.md): Lap Joint · scratched · Jan 16, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT BETWEEN FS 727 & 908 REVEALED A SCRIBE LINE ALONG THE LENGTH OF THE PANEL. THE ENTIRE LAP JOINT ALONG THE PANEL LENGTH WAS CUT AND REMOVED AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAI
- [SDR DL73K021187](https://openairdocs.org/sdr/DL73K021187.md): Drain · failed · Oct 11, 2002 · N242WA · Boeing 737247 · Fuselage Miscellaneous Structure
  > ON CLIMBOUT NOTICED EXCESSIVE CABIN CLIMB RATE. LEVELED OFF AT 10000 FT. CABIN CONTINUED TO CLIMB TO 10000 FT. OUTFLOW VALVE SHOWED FULL CLOSED. FORWARD OUTFLOW VALVE SHOWS FULL CLOSED. COULD NOT CONTROL CABIN ALTITUDE AT ALL IN DESCENT. REPLACED SEVERAL
- [SDR DL73K021165](https://openairdocs.org/sdr/DL73K021165.md): Skin · cracked · Oct 1, 2002 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE SKIN AT THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A.375 INCH TYPICAL CRACK. THE CRACK WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 383941-14, REV A.
- [SDR DL73K021150](https://openairdocs.org/sdr/DL73K021150.md): Tire · separated · Sep 29, 2002 · N242WA · Boeing 737247 · Tire
  > NR 4 TIRE TREAD SEPARATION ON T/O FROM FLL. OUTBOARD GEAR DOOR MISSING WITH DAMAGE TO NR 2 ENGINE NACELLE AND RIGHT FLAP ASSEMBLY ONLY MINOR BUMP FELT ON T/O ROLL PRIOR TO ROTATION. REPLACED BOTH RIGHT MAIN WHEEL ASSY, REPLACED DOOR, RPD NACELLE.
- [SDR DL73K020648](https://openairdocs.org/sdr/DL73K020648.md): Wire · chafed · Jun 11, 2002 · N242WA · Boeing 737247 · Light System Wiring
  > ON ARRIVAL FOUND RIGHT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED EXIT SIGN OVERHEAD BATTERY AND BATTERY POWER SUPPLY, REPAIRED CANNON PLUG WIRING AT POWER SUPPLY DUE TO CHAFED WIRING. ALL CHECK NORMAL.
- [SDR DL73K020029](https://openairdocs.org/sdr/DL73K020029.md): Coalescer Bag · dirty · Jan 8, 2002 · N242WA · Boeing 737247 · Humidity Control System
  > WITH POWER APPLIED THERE WAS A SMELL LIKE BURNING RUBBER. SMELL DISSIPATED WITH POWER BACK, NO INDICATIONS. RAN BOTH ENGS TO T/O POWER WITH PACKS ON, ANTI-ICE ON. CHECKED AIR MIX DISTRIBUTION PLENUM IN FWD B/B, NO CRACKS. REPLACED BOTH WATER SEPARATOR BAGS
- [SDR DL73K020022](https://openairdocs.org/sdr/DL73K020022.md): Odor · detected · Jan 8, 2002 · N242WA · Boeing 737247 · Air Distribution System
  > WITH POWER APPLIED HAD A SMELL LIKE BURNING RUBBER. DISSIPATED WITH POWER BACK, NO INDICATIONS. RAN BOTH ENGINES TO T/O POWER WITH PACKS ON, NO SMELL. CHECKED AIR MIX DISTRIBUTION PLENUM IN FWD BAG BIN, NO CRACKS OR LEAKS. REPLACED RIGHT AND LEFT WATER SEP
- [SDR DL73K011140](https://openairdocs.org/sdr/DL73K011140.md): Doubler · cracked · Jul 9, 2001 · N242WA · Boeing 737247 · Wing, Center Box
  > INSPECTION OF THE LONGITUDINAL FLOORBEAM AT RBL 24 ABOVE THE CENTER WING BOX REVEALED A CRACK IN THE REINFORCING DOUBLER OF THE BEAM WEB AT FS 678 ADJACENT TO A CABLE CUTOUT.
- [SDR DL73K011052](https://openairdocs.org/sdr/DL73K011052.md): Safety Switch · faulty · Jun 24, 2001 · N242WA · Boeing 737247 · Landing Gear Position and Warning
  > A/C DEPRESSURIZED, HAD TO DESCEND TO CONTROL CABIN. CABIN ALTITUDE REACHED 13,000 FEET WITH A/C DESCENDING BACK DOWN THROUGH 13,000 FEET AND THEN DESCENDED WITH AIRCRAFT TO TOUCHDOWN. REPLACED LDG SAFETY SWITCHES. OPS CHECKS GOOD.
- [SDR DL73K010982](https://openairdocs.org/sdr/DL73K010982.md): Outflow Valve · failed · Jun 15, 2001 · N242WA · Boeing 737247 · Pressure Regulator/Outflow Valve
  > AT 23,000 FEET STARTED TO FEEL CABIN RISING AND GOT THE ALT HORN. CABIN WAS AT 11,000 FEET AND CLIMBING 1000 FPM. STARTED DESCENT AUTO SYS FAILED TO STBY BUT CABIN KEPT CLIMBING UNTIL A/C PASSED THROUGH ACTUAL ALTITUDE. REPLACED PRESSURE CONTROLLER AND AFT
- [SDR DL73K010272](https://openairdocs.org/sdr/DL73K010272.md): Skin · cracked · Feb 13, 2001 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE SKIN AND UNDERLYING BEARSTRAP AT THE LOWER FWD CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1.25 INCH DEEP CUTOUT. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER ER/A 380029-14.
- [SDR DL73K001923](https://openairdocs.org/sdr/DL73K001923.md): Skin · gouged · Sep 30, 2000 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT WAS FOUND WITH A DEEP GOUGE. THE GOUGE WAS LOCATED 2 INCHES ABOVE THE TYPICAL CRACK LOCATION FOR THIS CORNER. THE GOUGE WAS TRIMMED OUT OF THE SKIN AND BONDED DOUBLER. THE CUTOUT WAS REPAIRED WITH AND EXTER
- [SDR DL73K001515](https://openairdocs.org/sdr/DL73K001515.md): Guide · damaged · Aug 9, 2000 · N242WA · Boeing 737247 · Leading Edge Devices
  > NR 2 SLAT INBOARD GUIDE BROKE ON TAKEOFF. PUNCTURED SLAT AND CAUSED SHEET METAL DAMAGE ON A/C AND SLAT ITSELF. REPLACED SLAT AND REPAIRED DAMAGE.
- [SDR DL73K001264](https://openairdocs.org/sdr/DL73K001264.md): Panel · missing · Jul 5, 2000 · N242WA · Boeing 737247 · Nacelle/Pylon Structure
  > UPON ARRIVAL FOUND 01 O/B PYLON PANEL 5126L MISSING. REPLACED SAME.
- [SDR DL73K992781](https://openairdocs.org/sdr/DL73K992781.md): Angle · corroded · Dec 17, 1999 · N242WA · Boeing 737247 · Fuselage Miscellaneous Structure
  > THE INNER CHORD ANGLE OF THE R1 DOOR SILL WAS FOUND CORRODED. A 1.5 X 1.0 CUTOUT WAS USED TO REMOVE THE DAMAGE. THIS WAS FOUND AT MV AND REPAIRED PER ERA 333863-14.
- [SDR DL73K992733](https://openairdocs.org/sdr/DL73K992733.md): Stringer · cracked · Dec 14, 1999 · N242WA · Boeing 737247 · Fuselage Main, Longeron/Stringer
  > THE LT STR 18A HAD A CRACK RUNNING FWD AND AFT SIMILIAR TO THOSE NOTED IN S/B 737-53-1170 AND 737-53-1066. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 333890-14.
- [SDR DL73K992722](https://openairdocs.org/sdr/DL73K992722.md): Skin · gouged · Dec 13, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS GOUGED AT THE C-1 DOOR, FS 492 AND STR 23R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333902-14.
- [SDR DL73K992719](https://openairdocs.org/sdr/DL73K992719.md): Skin · damaged · Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN JUST FWD OF C-1 DOOR CUTOUT AT BS 440 WAS FOUND CRACKED IN TWO PLACES BETWEEN S-22R AND 24R. REPAIR ENLARGED TO ENCOMPASS STATIC PORT, ER/A 333852-14 REV A.
- [SDR DL73K992702](https://openairdocs.org/sdr/DL73K992702.md): Skin · dented · Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED AT FS 425 BETWEEN STR 14L AND 15L. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PER ERA 333892-14.
- [SDR DL73K992701](https://openairdocs.org/sdr/DL73K992701.md): Bulkhead · cracked · Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Bulkhead
  > TWO CRACKS WERE FOUND IN THE FS 178 BULKHEAD WEB. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PER ERA 333854-14.
- [SDR DL73K992697](https://openairdocs.org/sdr/DL73K992697.md): Stringer · cracked · Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Longeron/Stringer
  > THE RIGHT STR 18A HAD A CRACK IN THE SHEAR WEB SIMILAR TO THAT OF S/B 737-53-1170. DAMAGE WAS FOUND AT AMV IN ATL. DAMAGE WAS REPAIRED PER ERA 333859-14.
- [SDR DL73K992292](https://openairdocs.org/sdr/DL73K992292.md): Retract Mech · malfunctioned · Oct 18, 1999 · N242WA · Boeing 737247 · Leading Edge Slat Control System
  > DURING FLIGHT, NR 2 SLAT WOULD NOT RETRACT FULLY. COCKPIT INDICATIONS SHOWED NR 2 RETRACTED. DURING EXTENSION FROM 1-5 DEGRESS IT DID NOT EXTEND, BUT FROM 5-10 DEGREES IT SLAMMED TO FULL EXTEND AND THEN RETRACTED TO EXT WITH ASSOCIATED L/E INTRANSIT LIGHT AN
- [SDR DL73K991625](https://openairdocs.org/sdr/DL73K991625.md): Skin · cracked · Jul 16, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN ASSY / R1 DOOR CUTOUT / LOWER AFT CORNER / FS 332: CRACK REPAIR. THE R1 DOOR CUTOUT WAS FOUND WITH A.375 INCH LONG TYPICAL CRACK IN THE LOWER AFT CORNER (FS 332). THE CRACK WAS THROUGH THE SKIN ASSY AND BEAR STRAP. THE CRACK WAS ROUTED OU
- [SDR DL73K990373](https://openairdocs.org/sdr/DL73K990373.md): Skin · cracked · Feb 20, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND BONDED DOUBLER AT THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A.25 INCH LONG TYPICAL CRACK IN THE LOWER HINGE CUTOUT. THE UNDERLYING BEAR STRAP WAS NOT CRACKED. THE CRACK WAS ROUTED OUT OF THE SKIN ASSY AND REPAIRED WITH AN EXT
- [SDR DL73E971259](https://openairdocs.org/sdr/DL73E971259.md): Bearing · failed · Jun 27, 1997 · N242WA · Boeing 737247 · Stabilizer Control System
  > STAB TRIM JAMMED IN FLT AT 2 DEGS NOSE DOWN TRIM. FOUND CROSSOVER SHAFT AND BEARINGS SEVERLY DAMAGED. REPLACED SHAFT, BEARINGS AND STAB TRIM SPROCKET PER M/M, CKS NML.
- [SDR DL73E960556](https://openairdocs.org/sdr/DL73E960556.md): Fan · failed · Mar 12, 1996 · N242WA · Boeing 737247 · Air Distribution Fan
  > SMOKE IN THE COCKPIT AFTER LDG IN ICT, ABOUT THE SAME TIME THE CONTROL CABIN AUG FAN C/B POPPED. CONTRACT MTC INSPECTED FAN AND TESTED A/C SYS, PLACED THE AUG FAN ON MCO. FAN WAS LATER REPLACED.

Next page: https://openairdocs.org/deregistered/N242WA-2007-06-20/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 = 'N242WA' AND deregistration_id = 'N242WA-2007-06-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N242WA-2007-06-20/reports

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