Boeing 737-347
Service difficulty reports · 359
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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 = '737347' 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 = '737347' 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 DL733060250Stiffener · crackedDURING ACCOMPLISHMENT OF 05-086589-12AD, THE WING CENTER SECTION REAR SPAR STIFFENER AT LBL 6.15 WAS FOUND CRACKED. REPLACED REAR SPAR STIFFENER.SDR DL733060111Duct · unknownUNABLE TO MAINTAIN PRESSURIZATION WITH LT PACK AT FL 240. RT PACK CURRENTLY ON MCO. REPAIRING RT PACK. REPLACED DUCT ON RT PACK CLEARED MCO ON RT PACK A/C PRESSURIZATION CHECK NORMAL.SDR DL733060098Actuator · brokenNR 4 O/B SPOILER ACTUATOR BROKE OFF AT REAR HINGE POINT, CAUSING HINGE POINT TO BREAK AT SPOILER PANEL. REPLACED BOTH UNITS. ACTUATOR P/N 273001083.SDR DL733050836Packing · splitDECLARED EMERGENCY HYD QTY A DROPPED TO 1/2. REPLACED LOWER PACKING ON A HYD SYS EMDP ACCOUSTIC FILTER, LEAK CK OK HYD SERVICED.SDR DL733050659Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS APPROX 2 INCHES LONG AFT OF BS 727D, JUST BELOW STR 23L. REPAIRED WITH DOUBLER PER ER/A 451209-14AD, REF AD 2004-18-06.SDR DL733050637Skin · crackedFUSELAGE SKIN CRACK WAS FOUND AT CHEM MILL LINE AT BS 727E, STR 24R. CRACK IS 3 INCHES LONG. DOULBER INSTALLED PER ER/A 451199-14AD, AD 2004-18-06, AND SRM 53-00-01.SDR DL733050524Skin · crackedCRACK FOUND IN FUSELAGE SKIN AT CHEM-MIL WHILE ACCOMP OPN 57546. CRACK REPORTED TO BE 1.5 INCH LONG, LOCATED AT FS 727E, S-24L. REPAIRED PER SRM 53-00-01, FIGURE 201. RELATED TO AD 2004-18-06, S/B 737-53A1210, & S/B 737-53-1065.SDR DL733050523Skin · crackedCRACK WAS FOUND IN THE FUSELAGE SKIN WHILE DOING OPN 57546 INSPECTIONS. REPAIRED PER SRM 53-00-01, FIGURE 201. REF AD 2004-18-06 / S/B 737-53A1210 / 737-53-1065.SDR DL733050497Indicator · unserviceableDURING T/O ROLL AFTER 80 KTS NR 2 OIL PRESS ROLLED BACK TO BELOW THE RED DIAL. ALL OTHER IND NORMAL. CONTINUED T/O AND PERFORMED LOP CK LIST PROCEDURE PER QRH. ENG SHUTDOWN AND RETURNED TO DTW. SWAP INDICATORS. PROBLEM FOLLOWED. REPLACED NR 2 OIL PRESS ISDR DL733050323Outflow Valve · unserviceableAIRCRAFT WOULD NOT PRESSURIZE. FOUND AUTO FLOW CONTROL VALVE NOT CLOSING PER CABIN PRESS LEAK TEST 05-51-91-702. REPLACED VALVE PER MM 21-58-31. OP CK OK. AIRCRAFT PRESSURIZED ON GROUND PER MM.SDR DL733050214Circuit Breaker · trippedON CLIMBOUT, BATTERY ON DC- IRS LIGHTS ILLUMINATED. BATTERY VOLTS ZERO. RETURNED TO SLC. MTC IN WORK. FOUND HOT BATTERY BUS C/B POPPED P18 PNL. RESET C/B. PERFORMING DC POWER CHECK.SDR DL733050197Fire Loop · faultyAPU FIRE WARNING LIGHT/ALARM BELL IN FLIGHT APPROX 1 TO 2 MINS AFTER APU SHUTDOWN IN FLIGHT AT 10 TO 12,000 FT ALT FIRE BOTTLE USED. REMOVED APU SHROUD, APU INSPECTED FOUND NO EVIDENCE OF FIRE. REPLACED AFT DETECTOR LOOP.SDR DL733050181Apu · defectiveSMOKE SMELL IN CABIN WITH APU AIR. REPLACED APU.SDR DL733050148Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 SSDR DL733050137Apu · fusesCREW REPORTS FUMES IN CABIN WHILE AT THE GATE. DEPLANED PASSENGERS AND TURNED OVER TO MAINTENANCE. REPLACED APU PER MM.SDR DL733050107Connector · damagedEMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F.SDR DL733050050Apu · fireAFTER LANDING STARTED APU. TAXIED TO GATE, DURING ENGINE SHUTDOWN HAD APU FIRE LIGHT. ACCOMPLISHED QRH PROCEDURE. MAINTENANCE INSPECTED, FIRE BOTTLE FOUND DISCHARGED. REMOVED BATHTUB AND INSPECTED APU FOR DAMAGE. FIRE WAS LIMITED TO TAILPIPE AREA. REAR FSDR DL733050035Outflow Valve · contaminatedAIRCRAFT FAILED TO PRESSURIZE. FOUND PRESSURE RELIEF VALVE STUCK OPEN.SDR DL733041124Skin · crackedINSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVEALED A 3 INCH CRACK ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 15R AT FS 500D+7. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER ESDR DL733041086Switch · intermittentAFTER TAKEOFF AND FLAPS WERE RAISED PILOT HAD NR 4 SLAT INDICATION PROBLEM ON THE FWD PANEL AND ON THE OVERHEAD. REPLACED SWITCH ON NR 4 SLAT ROD END.SDR DL733041069Wire Harness · burnedJUST PRIOR TO T/O WHEN LANDING LIGHTS TURNED ON, SPARKS CAME FROM OVERHEAD PANEL. TURNED OFF LIGHTS SPARKS STOPPED. REPAIRED WIRE BUNDLE IN OVERHEAD.SDR DL733040960Skin · dentedFUSELAGE SKIN DENTED AT STA 827 BETWEEN STR 26R - 28R. REPAIRED IAW ERA 093986-14.SDR DL733040805Skin · crackedTWO CRACKS WERE FOUND RUNNING ALONG THE BONDED SKIN DOUBLER LINE OF STRINGER 24L. ONE CRACK WAS JUST FWD AND THE OTHER JUST AFT OF A PREVIOUSLY INSTALLED SKIN REPAIR FOR REPAIR OF SIMILAR MILL LINE CRACKING. THE SKIN PANEL WAS CUT FROM THE STRINGER 20L LAP JSDR DL733040802Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT FOUR LOCATIONS. THE CRACKS WERE ALL LOCATED ALONG THE EDGE OF THE UNDERLYING BONDED DOUBLER. A 1 INCH VERTICAL CRACK WAS FOUND AT FS 767 ABOVE STR 23R. A 3.5 INCH HORIZONTAL CRACK WAS JUST BELOW S-22R AT FS 760, A .25 SDR DL733040796Wedge · debondedNR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14.SDR DL733040776Skin · crackedCRACK REPAIR, THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 757 JUST BELOW STRINGER 19R RUNNING ALONG THE UNDERLYING BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 092756-14.SDR DL733040746Skin · crackedA SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 23L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092528-1SDR DL733040617Skin · crackedFUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14.SDR DL733040616Skin · crackedFUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14.SDR DL733040604Odor · detectedFLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE.SDR DL733040311Psu · inoperativePAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU.SDR DL733040313Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH 2 CRACKS ALONG THE BONDED DOUBLER EDGES AT STRINGERS 22R & 23R. AN EXISTING REPAIR FOR A SIMILAR CRACK WAS LOCATED AT STRINGER 24R. THE EXISTING REPAIR WAS REMOVED, ALL CRACKS REMOVED WITH CUTOUTS, AND THE CUTOUTS REPAIRED WISDR DL733040216Wire · shortedAFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME.SDR DL733040188Cylinder · shearedWHILE TAKING THE RUNWAY IN A LEFT TURN, HEARD A BANG. THOUGH THE A/C FELT OK, ELECTED TO PULL OFF THE RUNWAY AND HAVE MAINT INSPECT THE AIRCRAFT. FOUND THE LEFT NOSE WHEEL AND AXLE BROKEN. REPLACED NOSE GEAR.SDR DL733040090Extinguisher · dischargedPORTABLE FIRE EXTINGUISHER PRESSURE LOW. REPLACED SAME.SDR DL733040060Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A.SDR DL733040007Tire · cutON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM.SDR DL733030968Engine · overtempON TAKEOFF ROLL, NR 1 ENGINE EGT WAS INCREASING TO 954 DEGREE CELSIUS. THROTTLES (AUTO THROTTLES) HAD TO BE DISCONNECTED TO KEEP ENGINE EGT FROM CLIMBING HIGHER. N1 WAS 91 PERCENT, N2 WAS 102 PERCENT AND INCREASING. FUEL FLOW NORMAL ON T/O ROLL. REPLACED ESDR DL733030948Fuse · blownEMERGENCY LIGHT AT SEAT 27DEF INOP. REPLACED 5 AMP FUSE ON BATTERY RACK.SDR DL733030877Skin · crackedFUSELAGE/SKIN/STA 500D - STA 520/STR 12R - REPAIR OF CRACK. THE CRACK IS CUT OUT OF THE FUSELAGE SKIN AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER ARE INSTALLED IN ACCORDANCE WITH ER/A 381822-14 REV C.SDR DL733030876Skin · dentedFUSELAGE/SKIN/FS430-460, S23R TO S27R - DENTS AND WEAR. THE SUBJECT DAMAGE IS CUT OUT FROM THE FUSELAGE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLER, TRIPLER AND STRUCTURAL FILLER IN ACCORDANCE WITH ER/A 385699-14. DAMAGE DUE TO CONTACT WITH GROUND EQUIPSDR DL733030855Beam · corrodedCORROSION WAS FOUND IN THE AFT LUG BORE OF THE NR 1 PYLON CROWN BEAM FITTING AT NAC STA 257.25. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION, HFEC INSPECTED, AND STEEL REPAIR BUSHINGS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385679-14.SDR DL733030852Wire Harness · inoperativeWHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M.SDR DL733030850Intercostal · crackedMODIFICATION OF THE FS 178 BULKHEAD REVEALED A CRACK IN THE LBL & RBL 28 COCKPIT FLOOR INTERCOSTAL WEB AND CHORD AT WL 107. THE CRACKED CHORD AND WEB WERE REMOVED AT BOTH LOCATIONS AND PARTS INSTALLED PER ER/A 385678-14AD.SDR DL733030784Sensor · out of toleranceAFTER TAKEOFF GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE OVERRIDE TO RAISE HANDLE. ONCE GEAR WAS UP AND FLAPS WERE RETRACTED TAKEOFF WARNING HORN SOUNDED UNTIL FLAPS WERE LOWERED AGAIN. AIRCRAFT RETURNED TO SFO. SFO LINE MTC T/S TAKEOFF WARNING SYSTEM, FOUSDR DL733030626Iru · faultyLOST LEFT IRU IN FLIGHT. UNABLE TO GET HEADING IN ATT. BOTH AUTOPILOTS INOP. REPLACED LEFT INERTIAL REFERENCE UNIT PER M/M.SDR DL733030611Light · inoperativeEMERGENCY LIGHTS INOP AT SEAT 2B OVERHEAD, AT 10D AND 14D. REPLACED OVERHEAD LIGHT ASSY AT 2B AND RELAMPED SEAT LIGHTS AT 10D & 14D CHECKS GOOD.SDR DL733030568Bulb · inoperativeON L/O FOUND EMERGENCY OVERHEAD PATH LIGHTING AT SEATS 23ABC AND 17D INOP. RELAMPED SAME, OPS CHECK NORMAL.SDR DL733030563Bulkhead · corrodedCORROSION WAS FOUND ON THE FWD SIDE OF THE AFT PRESSURE BULKHEAD. THE DAMAGE IS TO THE WEB AND STIFFENER AT THE BOTTOM OF THE BULKHEAD AT BL 0 AND STA 1016. DAL ER/A 385133-14AD PROVIDES INSTRUCTIONS TO REPAIR THE WEB AND STIFFENER PER BOEING SB 737-53A1075,SDR DL733030502Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST ABOVE STRINGER 24R AND A 2 INCH CRACK JUST BELOW STRINGER 24R. THE CRACKS RAN ALONG THE BONDED WAFFLE DOUBLER MILL LINE. THERE WAS AN EXISTING EXTERNAL DOUBLER REPAIR IN THE AREA FOR SIMILAR PREVIOUS CRACK
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