# Service difficulty reports: N236WA, cancelled Nov 21, 2007 A list on [N236WA, cancelled Nov 21, 2007](https://openairdocs.org/deregistered/N236WA-2007-11-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL73S040046](https://openairdocs.org/sdr/DL73S040046.md): Floorbeam · cracked · Jan 16, 2004 · N236WA · Boeing 737247 · Fuselage Main, Floor Beam > DURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 665, BS 669 AND BS 673. DAMAGE WAS REPAIRED AS PER ERA 385959-14AD. - [SDR DL73S040043](https://openairdocs.org/sdr/DL73S040043.md): Skin · cracked · Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/Skin > DURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 559 & 579. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOU - [SDR DL73S040040](https://openairdocs.org/sdr/DL73S040040.md): Skin · damaged · Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/Skin > DENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14. - [SDR DL73S040039](https://openairdocs.org/sdr/DL73S040039.md): Frame · damaged · Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Frame > A DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REPAIRED PER ERA 386004-14. - [SDR DL73S040038](https://openairdocs.org/sdr/DL73S040038.md): Floorbeam · cracked · Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Floor Beam > DURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH. UPPER CHORD WAS CUT OFF AND A NEW SECTION SPLICED IN PER ERA 385945-14. - [SDR DL73S040022](https://openairdocs.org/sdr/DL73S040022.md): Frame · cracked · Jan 9, 2004 · N236WA · Boeing 737247 · Fuselage Main, Frame > CRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRACKS INDICATIONS WERE REMOVED AND REPAIR INSTALLED PER ERA 385971-14. - [SDR DL73S040021](https://openairdocs.org/sdr/DL73S040021.md): Skin · dented · Jan 9, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14. - [SDR DL73K001960](https://openairdocs.org/sdr/DL73K001960.md): Support Fitting · corroded · Oct 6, 2000 · N236WA · Boeing 737247 · Fuselage, Landing Gear Attach Fittings > THE LOWER MAIN LUGS ON THE LT AND RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTINGS AT FS 685 WERE FOUND CORRODED. THE EXISTING BUSHINGS WERE REMOVED AND LUG BORES OVERSIZED TO REMOVE THE CORROSION. LARGER DIAMETER REPAIR BUSHINGS WERE INSTALLED TO REPAIR THE - [SDR DL73K001405](https://openairdocs.org/sdr/DL73K001405.md): Bulkhead · cracked · Jul 23, 2000 · N236WA · Boeing 737247 · Fuselage Main, Bulkhead > WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, A TYPICAL CRACK WAS FOUND IN THE BULKHEAD WEB AT WL 234 AND RBL 7. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER BAC S/B 737-53A1173 AND DOCUMENTED PE - [SDR DL73K001404](https://openairdocs.org/sdr/DL73K001404.md): Bulkhead · cracked · Jul 23, 2000 · N236WA · Boeing 737247 · Fuselage Main, Bulkhead > WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, TYPICAL CRACKS WERE FOUND IN THE ADJACENT FLOOR WEBS AT WL 207 AND RBL & LBL 25. THE CRACKED WEBS WERE REMOVED AND NEW WEBS INSTALLED PER BAC S/B 737-53A1173 AND ER/A 377928-14AD. - [SDR DL73K000682](https://openairdocs.org/sdr/DL73K000682.md): Bullet · dented · Apr 9, 2000 · N236WA · Boeing 737247 · Turbine Engine Compressor Section > EN ROUTE FROM BDL TO FLL, NR 1 ENGINE HAD COMPRESSOR STALLS. CREW PULLED THROTTLE TO IDLE. DIVERTED TO BOS. BOS MTC FOUND NR 1 ENGINE NOSE BULLET DETACHED AND FAN DAMAGE. - [SDR DL73E992274](https://openairdocs.org/sdr/DL73E992274.md): Duct · failed · Oct 15, 1999 · N236WA · Boeing 737247 · Cabin Cooling System > AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O CONFIGURED FOR RIGHT BLEED AND RIGHT PACK OPERATION. AUTO/STBY/AND MANUAL MODES ATTEMPED. OUTFLOW VALVE FULL CLOSED FWD OUTFLOW VALVE CLOSED. FOUND APU BLEED AIR DUCT RUPTURED. REPLACED SAME. - [SDR DL73E982039](https://openairdocs.org/sdr/DL73E982039.md): Fan · failed · Oct 3, 1998 · N236WA · Boeing 737247 · Air Distribution Fan > GASPER FAN C/B FOUND OPEN, WHEN CLOSED IT RETRIPPED ACCOMPANIED BY A LOUD POP HEARD UNDER FLOOR IN MID CABIN AND STRONG ELECTRICAL SMELL. INSP GASPER FAN NO PROBLEMS. REPLACED FAN. - [SDR DL73E981375](https://openairdocs.org/sdr/DL73E981375.md): Line · chaffed · Jun 30, 1998 · N236WA · Boeing 737247 · Hydraulic System, Main > A/C RETURN ATL, DUE TO RT HYD PUMP LOW PRESS LIGHT AND HYD QTY ZERO ON CLIMB-OUT. FOUND HYD RTN LINE CHAFFED. REPLACED LINE AND FILTER AND EDP PER M/M. LEAK CK GOOD AND SYS OPS NML PER M/M. - [SDR DL73E981270](https://openairdocs.org/sdr/DL73E981270.md): Duct · cracked · Jun 16, 1998 · N236WA · Boeing 737247 · Pneumatic Distribution System > WITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMELL IN MID CABIN AREA. FOUND APU BLEED LINE CRACKED JUST AFT OF APU BLEED VALVE. REPLACED BLEED DUCT - [SDR DL73E980933](https://openairdocs.org/sdr/DL73E980933.md): Skin · cracked · Apr 28, 1998 · N236WA · Boeing 737247 · Fuselage Main, Plate/Skin > THE R2 DOOR OPENING SURROUND SKIN WAS FOUND WITH A.75 INCH LONG CRACK AT THE CUTOUT FOR THE LOWER HINGE. THE SKIN AND BONDED DOUBLERS WERE CUTOUT TO REMOVE THE CRACK. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 36464 - [SDR DL73E971675](https://openairdocs.org/sdr/DL73E971675.md): Skin · corrosion · Aug 9, 1997 · N236WA · Boeing 737247 · Fuselage Main, Plate/Skin > A BULGE WAS FOUND IN THE FUSELAGE SKIN AT STA 927 BETWEEN STR 14R AND 15R. MX REMOVED THE AFFECTED AREA OF THE CHEM-MILLED LOWER SKIN (65-45778-82), JUST BELOW THE STR 14R LAP JOINT. THE CUTOUT MEASURED 2.5 BY 8. A TIME LIMITED REPAIR USING BLIND FASTENERS - [SDR DL73E961724](https://openairdocs.org/sdr/DL73E961724.md): Bulkhead Web · cracked · Jul 9, 1996 · N236WA · Boeing 737247 · Fuselage Main, Bulkhead > THREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 198. THE SECOND IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT WL 200. THE THIRD IS LOCATED NEAR LBL 5.7 AT APPRO - [SDR DL73E954574](https://openairdocs.org/sdr/DL73E954574.md): Fairing · came loose · Nov 29, 1995 · N236WA · Boeing 737247 · Trailing Edge Flaps > LEFT INBD FLAP FAIRING CANOE BROKE LOOSE IN FLT AND WAS FOUND PARTLY DETACHED FROM WING DURING POST FLT. REMOVED LEFT WING MIDFLAP CANOE, REPLACED BELL CRANK ASSY, INBD AND OTBD STRUTS AND REINSTALLED FAIRING PER MM 27-51-21. - [SDR DL73E960091](https://openairdocs.org/sdr/DL73E960091.md): Bulb · failed · Jan 15, 1995 · N236WA · Boeing 737247 · Emergency Lighting > AFT LOWER BODY EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD. ## 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 = 'N236WA' AND deregistration_id = 'N236WA-2007-11-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N236WA-2007-11-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.