Boeing 737-2H4
Service difficulty reports · 4,801
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '7372H4' 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 aircraft_model_key = '7372H4' 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 SWAA950325Spar Web · puncturedDURING SCHEDULED C2 CHECK, FOUND SPAR WEB PUNCTURED AT BS 616, 4 INCHES FROM BOTTOM NEXT TO O/B SIDE OF O/B AUX TRACK OF NUMBER 1 SLAT. REPAIRED PER BOEING SRM.SDR SWAA950301Compressor · stalledEN ROUTE PHX TO AUS, CREW EXPERIENCED NR 1 ENGINE COMPRESSOR STALL. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. BORESCOPED INSPECTED AND DETERMINED ENGINE CHANGE REQUIRED. REPLACED ENGINE ASSEMBLY AND SDR SWAA95287Tr Module · malfunctionedAFTER DEPARTURE, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH ISOLATION PRESSURE SWITCHES AND T/R ISOLATION MODULE. LEAK AND OPS CHECKED NORMAL PER BOEING MM.SDR SWAA95288Connector · brokenDURING CLIMBOUT, NUMBER 1 ENGINE OIL TEMP INDICATOR ENTERED YELLOW RANGE FOR 14 MINUTES. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NR 1 ENGINE OIL TEMP SENSOR CANNON PLUG PIN B BROKEN. REPLACED PIN AND PERFORMED ENGINE POWSDR SWAA95295Skin · crackedDURING SCHEDULED QUARTER D-CHECK, FOUND FUSELAGE SKIN CRACKED 1.2 INCH AT AC GROUND SERVICING CUTOUT, RBL 5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95293Skin · crackedDURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .75 INCH AT BS 767 AND STRINGER 19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95286Hyd Pumps · malfunctionedIN FLIGHT, NUMBER 1 AND 2 ENGINE HYDRAULIC PUMPS INDICATED LOW PRESSURE, 'A' SYSTEM QUANTITY DISPLAYED ZERO. AIRCRAFT RETURNED TO SAT AND MADE AN UNEVENTFUL LANDING. AFTER LANDING, SYSTEM 'A' INDICATED 1.5 GAL AND BEFORE REACHING GATE, INDICATED 2.5 GAL. FOSDR SWAA95265Pwr Supply · inopDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER SUPPLY PER BOEING M/M.SDR SWAA95264Web · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 10.5 TO 12.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95263Web · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 7.7 TO 14.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95262Web · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 5.7, WL 184 TO 207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95261Web · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 5.7, WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95260Beam · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 7, WL 203. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95259Skin · crackDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND SKIN CRACK AT BS 987, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0241 AND BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95258Skin · damageDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LIGHTNING STRIKE DAMAGE AT BS 361, BETWEEN S2R AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95257Web · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 209, AND 218, RBL 11.7 TO 13.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA95256Web · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 184 TO 207, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR 95ZZZX1826Spring · damagedSPRING (56) IS COMPRESSED INSIDE STOP (57). GUIDE (55) RELEASED FROM SPRING (56) AND WAS CRUSHED INSIDE LOCK PISTON (47). GUIDE (55) IS TIGHTLY INSTALLED INSIDE SPRING (56). SUSPECT THAT GUIDE (55) WAS NOT TIGHT INSIDE SPRING (56), CAME LOOSE AND CAUSED COLSDR SWAA950254Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 767, 11 INCHES ABOVE SKIN LAP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950248Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LEFT OVERWING LIGHT BATTERY PER BOEING M/M.SDR SWAA950238Splice · corrodedDURING SCHEDULED MAINT CHECK, FOUND BS 312, FLOOR BEAM UPPER SPLICE CORRODED. REPAIRED PER SWA RA 1-253-420.SDR SWAA950237Floor Beam · corrodedDURING SCHEDULED MAINT CHECK, FOUND BS 328, RBL 22 TO RBL 48, FORWARD FLANGE, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1256.SDR SWAA950236Floor Beam · corrodedDURING SCHEDULED MAINT CHECK, FOUND BS 360, BL 0, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1258.SDR SWAA950235Floor Beam · corrodedDURING SCHEDULED MAINT CHECK, FOUND BS 308, LBL 20, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1257.SDR SWAA950234Chord · crackedDURING SCHEDULED MAINT CHECK, FOUND BS 178, LBL 5.7, FORWARD CHORD CRACKED. REPAIRED PER SWA RA 1-253-1255.SDR SWAA950233Frame · crackDURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STRINGER 3R. REPAIRED PER SWA RA 1-253-1260.SDR SWAA950231Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION, EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950230Web · crackedDURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED 1 INCH AT I/B RADIUS ABOVE RAM AIR DUCT AT FWD END ATTACH POINT, LEFT AC BAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950229Beltframe · crackedDURING SCHEDULED QUARTER D CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950228Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT AFT ENTRY DOOR UPPER AFT CORNER, BS 986.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950227Stiffener · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT VERTICAL STIFFENER, BS 178, RBL 6, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950226Bulkhead Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950225Stiffener · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, LBL 6, WL 184. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950224Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 391, STRINGER 14L. REPAIRED PER TRAMCO EWO 95-0203 AND 95-0205.SDR SWAA950223Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 727+11, 757, AND 758, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0203.SDR SWAA950222Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 470, 471, AND 490, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0203.SDR SWAA950221Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND FORWARD SECTION OF CABIN EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING MM.SDR BJNA53001Wire · brokenEMERGENCY LIGHTING INOP, ROWS 1-6. REPAIRED BROKEN WIRE WITH BUTT SPLICE PER BSWP 20-30-22. SYSTEM OP CHECKED GOOD PER BMM 33-51-0. (X)SDR SWAA950204Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950203Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950202Eel Battery · dischargedDURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950200Beltframe · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, S26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950198Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 768, AT STRINGER 4R. REPAIRED PER TRAMCO EWO 95-0200.SDR SWAA950197Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 767, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200.SDR SWAA950196Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 867, 860, 870, 887, 888, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200.SDR SWAA950195Skin · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 818 TO 828, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200.SDR SWAA950194Blkhd Web · crackedDURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD PRESSURE WEB FROM BL 0 TO RBL 17, WL 184 TO 230, UNDER STRAPS AND ANGLES. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950190Blkhd Angle · crackedDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT BS 178 PRESSURE BULKHEAD VERTICAL T-ANGLE AT LBL 5.7 AT WL 184, IN THE I/B AND O/B FLANGE RADIUS. REPAIRED PER SWA RA 1-253-1250.SDR SWAA950189Skin · crackedDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION NEAR SEVERAL FASTENERS IN PRESSURE WEB AT I/B SIDE OF STRAP, BS 178, LBL 5.7, FROM WL 205 TO 186. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950188Skin · crackDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT FUSELAGE SKIN LAP, BS 480, S10L, AT BS 500B+10, S14L AND AT BS 530, S10R. REPAIRED PER SWA RA 1-253-1251 AND SI 8615-53.
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