N242WA, cancelled Jun 20, 2007

Service difficulty reports · 53

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 = 'N242WA' AND deregistration_id = 'N242WA-2007-06-20'
  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 DL73S060193Skin · puncturedPUNCTURE 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.Mar 14, 2006 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S060064Floorbeam · crackedTHE 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.Jan 15, 2006 · N242WA · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73S050736Skin · crackedCRACKS 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.Nov 21, 2005 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S041016Skin · crackedINSPECTION 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.Nov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S041015Skin · crackedINSPECTION 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 CUNov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040382Transceiver · failedWX RADAR FAILED ON T/O. REPLACED R/T UNIT.Apr 30, 2004 · N242WA · Boeing 737247 · Weather Radar SystemSDR DL73S040246Proximity Sensor · failedDISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR.Mar 18, 2004 · N242WA · Boeing 737247 · Leading Edge Slat Position Indicating SystemSDR DL73S040103Fitting · corrodedDURING 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 3860Jan 28, 2004 · N242WA · Boeing 737247 · Empennage Flight Control Surfaces, Attach FittingsSDR DL73S040100Skin · damagedSCRIBE 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.Jan 28, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040085Skin · damagedSCRIBE 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.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040084Skin · corrodedCORROSION WAS NOTED IN THE FUSELAGE SKIN AT S27L BETWEEN BS 947.50 TO 967. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386110-14.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040083Beam · crackedA CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 386098-14.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, StructureSDR DL73S040076Skin · damagedTHE 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.Jan 23, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040075Skin · damagedTHE 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/Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040070Bulkhead · corrodedCORROSION 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.Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, BulkheadSDR DL73S040069Skin · damagedSCRIBE 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.Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040068Skin · damagedSCRIBE 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 OJan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040067Skin · damagedSCRIBE 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 REJan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040073Skin · damagedTHE 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 BJan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040072Skin · damagedTHE 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.Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040071Skin · damagedTHE 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 Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040065Skin · damagedTHE 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 ALJan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040063Lap Joint · scratchedTHE 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 Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040062Skin · scratchedTHE 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 Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040054Lap Joint · scratchedINSPECTION 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 REPAIJan 16, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K021187Drain · failedON 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 SEVERALOct 11, 2002 · N242WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73K021165Skin · crackedTHE 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.Oct 1, 2002 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K021150Tire · separatedNR 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.Sep 29, 2002 · N242WA · Boeing 737247 · TireSDR DL73K020648Wire · chafedON 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.Jun 11, 2002 · N242WA · Boeing 737247 · Light System WiringSDR DL73K020029Coalescer Bag · dirtyWITH 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 BAGSJan 8, 2002 · N242WA · Boeing 737247 · Humidity Control SystemSDR DL73K020022Odor · detectedWITH 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 SEPJan 8, 2002 · N242WA · Boeing 737247 · Air Distribution SystemSDR DL73K011140Doubler · crackedINSPECTION 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.Jul 9, 2001 · N242WA · Boeing 737247 · Wing, Center BoxSDR DL73K011052Safety Switch · faultyA/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.Jun 24, 2001 · N242WA · Boeing 737247 · Landing Gear Position and WarningSDR DL73K010982Outflow Valve · failedAT 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 Jun 15, 2001 · N242WA · Boeing 737247 · Pressure Regulator/Outflow ValveSDR DL73K010272Skin · crackedA 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.Feb 13, 2001 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K001923Skin · gougedTHE 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 EXTERSep 30, 2000 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K001515Guide · damagedNR 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.Aug 9, 2000 · N242WA · Boeing 737247 · Leading Edge DevicesSDR DL73K001264Panel · missingUPON ARRIVAL FOUND 01 O/B PYLON PANEL 5126L MISSING. REPLACED SAME.Jul 5, 2000 · N242WA · Boeing 737247 · Nacelle/Pylon StructureSDR DL73K992781Angle · corrodedTHE 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.Dec 17, 1999 · N242WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73K992733Stringer · crackedTHE 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.Dec 14, 1999 · N242WA · Boeing 737247 · Fuselage Main, Longeron/StringerSDR DL73K992722Skin · gougedTHE 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.Dec 13, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K992719Skin · damagedFUSELAGE 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.Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K992702Skin · dentedTHE 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.Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K992701Bulkhead · crackedTWO CRACKS WERE FOUND IN THE FS 178 BULKHEAD WEB. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PER ERA 333854-14.Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, BulkheadSDR DL73K992697Stringer · crackedTHE 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.Dec 10, 1999 · N242WA · Boeing 737247 · Fuselage Main, Longeron/StringerSDR DL73K992292Retract Mech · malfunctionedDURING 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 ANOct 18, 1999 · N242WA · Boeing 737247 · Leading Edge Slat Control SystemSDR DL73K991625Skin · crackedFUSELAGE / 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 OUJul 16, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73K990373Skin · crackedTHE 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 EXTFeb 20, 1999 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E971259Bearing · failedSTAB 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.Jun 27, 1997 · N242WA · Boeing 737247 · Stabilizer Control SystemSDR DL73E960556Fan · failedSMOKE 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.Mar 12, 1996 · N242WA · Boeing 737247 · Air Distribution Fan
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