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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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.SDR 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 CUSDR DL73S040382Transceiver · failedWX RADAR FAILED ON T/O. REPLACED R/T UNIT.SDR DL73S040246Proximity Sensor · failedDISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR.SDR 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 3860SDR 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.SDR 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.SDR 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.SDR DL73S040083Beam · crackedA CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 386098-14.SDR 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.SDR 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/SDR 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.SDR 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.SDR 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 OSDR 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 RESDR 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 BSDR 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.SDR 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 SDR 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 ALSDR 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 SDR 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 SDR 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 REPAISDR 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 SEVERALSDR 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.SDR 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.SDR 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.SDR 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 BAGSSDR 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 SEPSDR 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.SDR 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.SDR 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 SDR 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.SDR 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 EXTERSDR 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.SDR DL73K001264Panel · missingUPON ARRIVAL FOUND 01 O/B PYLON PANEL 5126L MISSING. REPLACED SAME.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 ANSDR 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 OUSDR 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 EXTSDR 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.SDR 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.
Back to N242WA, cancelled Jun 20, 2007