Boeing 737-3L9
Service difficulty reports · 1,188
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 = '7373L9' 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 = '7373L9' 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 F3LA200500008Sill · corrodedDURING C-4 CHECK INSPECTION, REPORTED L2 DOOR MOP SILL CORRODED. REPLACED L2 DOOR MOP SILL PER SRM 51-40-02.SDR F3LA200500010Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT GALLEY PAN STRAP AT BS 1016, BETWEEN RBL 30 AND LBL 30. FOUND TO BE OUT OF LIMITS PER SRM 53-60-61, FIG 101, DETAIL VII. REMOVED PAN STRAP PER SRM 51-40-02. FABRICATED NEW STRAP AND INSTALLED PER EA 53-SDR F3LA200500009Intercostal · corrodedDURING C-4 CHECK INSPECTION, REPORTED INTERCOSTAL AT BS 950, RBL 20 TO RBL 40, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REPLACED INTERCOSTAL PER SRM 51-40-05, 51-40-02, AND 53-60-51.SDR F3LA200500007Sill · corrodedDURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02.SDR SWAA050596Shear Tie · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 344, LBL 8-12, WL 148. REPAIRED SHEAR TIE PER SRM.SDR SWAA050595Shear Tie · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 380, LBL 5 TO RBL 5, WL 148. REPAIRED SHEAR TIE PER SRM.SDR SWAA050594Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE BETWEEN BS 350 & BS 370, STR 28R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.SDR SWAA050593Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE AT BS 358, STR 27R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.SDR SWAA050458Shear Tie · corrodedDURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.SDR F3LA200400117Proximity Sensor · faultyFLIGHT CREW REPORTED LANDING GEAR WARNING HORN STUCK ON WHEN FULLY CONFIGURED ON FINAL AND WOULD NOT SILENCE UNTIL FLAPS RETURNED TO UP POSITION AFTER LANDING. REPLACED PROXIMITY SENSOR 5853. OPS CHECKED GOOD.SDR DL73G041085Bolt · shearedUPON LANDING TOWER REPORTED PUFF OF SMOKE FROM GEAR AND UPON PARKING AT GATE FOUND NUMBER 1 TIRE FLAT AND 5 RIM BOLTS SHEARED. REPLACED BOTH NUMBER 1 AND NUMBER 2 WHEELS ASSY'S. INSPECTED A/C, NO EVIDENCE OF ANY OTHER DAMAGE.SDR SWAA042945Floorbeam · corrodedDURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, LBL 12, CORRODED. REPAIRED FLOORBEAM PER EA.SDR F3LA200400110Floorbeam · corrodedDURING A-4 CHECK, INSPECTION REPORTED PARTITION SUPPORT CORRODED AT FLOORBEAM, STA 986.5 - 1006, RBL 16. REPLACED PARTITION SUPPORT AT FLOORBEAM PER SRM 51-40-06 AND DRAWING 65C32675.SDR F3LA200400109Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT CORRODED AT STA 1010, RBL 10. REPLACED FLOORBEAM SUPPORT PER SRM 51-40-02, 51-40-05 AND BAC DRAWING 65C33375.SDR F3LA200400107Web · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR WEBS AFT OF STA 1016 FLOORBEAM, CENTER OF FUSELAGE, CORRODED. REPLACED FLOOR WEB HAT CHANNEL, STA 1016, BL 0, PER DRAWING 69-77731, AND SRM 51-40-02 AND 53-60-51.SDR F3LA200400108Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL SUPPORT CORRODED AT STA 986.5 - 1006, RBL 20. REPLACED FLOOR SUPPORT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.SDR F3LA200400106Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED L2 MOP SILL CORRODED. REPLACED L2 MOP SILL PER SRM 51-10-2 AND 51-40-02.SDR F3LA200400105Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED R2 MOP SILL CORRODED. REPLACED R2 MOP SILL PER SRM 51-10-2 AND 51-40-02.SDR F3LA200400103Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL FROM STA 947 - 986 LEFT OF CENTER CORRODED AT FLOOR PANEL NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375.SDR F3LA200400104Floorbeam · corrodedDURING C-4 CHECK, FLOORBEAM GOUGED AND CORRODED AT STA 947.5 - 967, RBL 16. REPLACED DAMAGED INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.SDR F3LA200400102Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT AT STA 947.5 - 967, LBL 14, CORRODED. REPLACED INTERCOSTAL AT STA 947.5 - 967, LBL 14, PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375.SDR F3LA200400100Floor Support · crackedDURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CRACKED AT STA 927 - 947.5, RBL 16. REMOVED FLOOR SUPPORT TO REPLACE CRACKED FLANGE. REPAIRED CRACKED FLANGE AND REINSTALLED FLOOR SUPPORT PER BOEING DRAWING 65-36656, 737-300 SRM 51-40-02 AND 51-10-02, ANDSDR F3LA200400099Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 947.5 CORRODED AT FLOOR PANEL NUT PLATES. REPAIRED FLOORBEAM UPPER CHORD PER SRM 53-00-51, 51-40-02, 51-20-01 AND MM 51-21-01.SDR F3LA200400098Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986.5 CORRODED AT FLOOR PANEL NUT PLATES. REPLACED FLOORBEAM UPPER CHORD AT STA 986.5 PER SRM 53-60-51, 53-00-51, FIG 202, AND MM 51-20-01.SDR F3LA200400097Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN STA 294.5 AND 312, 10.5 INCHES FROM CENTER LT, CORRODED AT STA 312 END. REMOVED UPPER T-CHORD ON FLOOR SUPPORT AT LBL 10.5, STA 294.5 THRU 312, AND INSTALLED NEW UPPER T-CHORD IAW SRM 51-40-02.SDR F3LA200400096Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 328 CRACKED 20 INCHES IN FROM FUSELAGE OUTER SKIN. VERTICAL ANGLE CRACKED ON LOWER END LT. REPLACED SHEAR TIE AT LBL 45 ON FWD SIDE OF STA 328 FLOORBEAM PER SRM 51-40-02, 51-40-05 AND SOPM 20-41-02.SDR F3LA200400095Floorbeam · corrodedDURING C-4 CHECK, INSPECTED REPORTED FLOORBEAM AT STA 967, LBL 42, CORRODED AT FLOOR PANEL SCREW NUT PLATE. FOUND FLOORBEAM TO BE CORRODED BEYOND LIMITS PER SRM 53-60-51. REMOVED DAMAGED AREA, FABRICATED REPAIR SECTION AND REPAIR PARTS AND INSTALLED PER SRM SDR F3LA200400094Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967, RBL 27.16, CORRODED AT FLOOR PANEL SCREW NUT PLATE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-51, FIG 202.SDR F3LA200400093Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL SPOTS FROM 10 INCHES LEFT OF CENTER TO 40 INCHES RT OF CENTER. ALL SCREW HOLES IN THIS AREA CORRODED. SCRATCH ON TOP OF BEAM RT SIDE, 12 INCHES FROM CENTER TO WALL. REPASDR F3LA200400092Skin · dentedDURING C-4 CHECK, COMPLIED WITH RW0000198, DENT IN FUSELAGE, AFT OF CARGO DOOR AT STA 500-500A. REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED REPAIR IAW BAC 737-300 SRM 53-00-01, PROCEDURE V, DETAIL VII-IX AND SOPM 40-20-01.SDR F3LA200400089Structure · crackedON WALK AROUND, MAINTENANCE REPORTED A 4-INCH CRACK IN RT FWD TOP WHEEL WELL. REPAIRED IAW SRM 53-10-51, PAGE 213, FIGURE 203.SDR F3LA200400091Pressure Panel · crackedFLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 203, DETAIL IV AND EA SDR SWAA042160Tee Fitting · crackedDURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER TEE CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER MM.SDR SWAA042159Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM.SDR SWAA042158Slide · out of adjustDURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.SDR SWAA042046Keelbeam · corrodedDURING SCHEDULED C2 CHECK, FOUND LT AND RT KEEL BEAM AT RT BS 540, GROUND A/C DUCT CENTERLINE, CORRODED. REPAIRED RT & LT KEEL BEAM CHORDS PER EA.SDR SWAA041994Cable · misroutedDURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM.SDR F3LA200400066Fire Loop · faultyAIR RETURN, NR 2 ENG OVERHEAT CAUTION LIGHT ILLUM TWICE. DECLARED EMERGENCY, LANDED W/O INCIDENT. ON DESCENT, MASTER CAUTION SYS ILLUM 4 TIMES, NO SIX PACK INDICATION. MX TESTED CAUTION SYS THRU SIMULATION OF CONDITIONS CAUSING ILLUMIN ANNUNCIATORS, ALL SYSSDR F3LA200400067Control Module · inoperativeABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTRANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLACED FLAP/SLAT MODULE PER MM 27-88-41. CHECKED TARGET TO EXTEND SENSORS ON NR 2, 3 AND 5 SLATS PESDR F3LA200400064Panel · damagedDURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51-40-02, SRM 51-40-08 AND MM 28-11-00. PERFORMED LEAK CHECK. NO LEAKS NOTED.SDR F3LA200400063Panel · crackedDURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51-40-02 AND 51-40-65.SDR SWAA041242Bulkhead · crackedDURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 7 TO LBL 8, CRACKED. REPAIRED BULKHEAD WEB PER SRM.SDR SWAA041157Skin · crackedDURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN BELOW L1 DOOR BS 335, LT LOWER SIDE, CRACKED. REPAIRED SKIN PER EA.SDR SWAA041161Skin · corrodedDURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 28R, CORRODED. REPAIRED SKIN PER EA.SDR SWAA041082Slide · out of adjustDURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.SDR SWAA041046Pressure Panel · crackedDURING SCHEDULED C1 CHECK, FOUND FORWARD TEE STIFFENER WEB AT NLG W/W CEILING CRACKED. REPAIRED WEB PER SRM.SDR SWAA041041Slide · out of adjustDURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.SDR SWAA040718Slide · out of adjustR2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.SDR SWAA040566Cover · crackedDURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW 14 DEF. REMOVED AND REPLACED EEPLS COVER PER MM.SDR SWAA040239Strip · crackedDURING SCHEDULED SPV, FOUND EEPLS PHOTO LUMINESCENT STRIP CRACKED AT RT, BS 833.45 TO BS 847.45. REMOVED AND REPLACED STRIP PER MM.
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