Boeing 737-301

Service difficulty reports · 4,797

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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 = '737301'
  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.

SDR USAA040097Frame · corrodedPIT - FOUND CHORD CORRODED 4 SQUARE INCHES, FORWARD SIDE AT Y-CHORD. CLEANED CORROSION PER SRM 51-10-02. (M)Mar 30, 2004 · N574US · Boeing 737301 · Fuselage Main, FrameSDR AWXA200400311Flashlight · inoperativePHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Mar 29, 2004 · N325AW · Boeing 737301 · Emergency EquipmentSDR USA2004F00024Circuit Card · faultyON CLIMBOUT, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE M987 PRINTED CIRCUIT CARD. ALSO, ADMar 28, 2004 · N576US · Boeing 737301 · Electronic Shelf SectionSDR USAA040348Stringer · corrodedFOUND STRINGER CORRODED TWO AREAS, 1 INCH BY 6 INCHES AND 1 INCH BY 4 INCHES, FS 1016-1022 FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED STIFFENERS AND INSTALLED DOUBLERS AND SPLICES PER SRM 53-80-08 AND BOEING DWG PL 65C28106. (M)Mar 27, 2004 · N355US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040065Floor Support · crackedFOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PART EPN 1138864 PER SRM 51-40-00. (M)Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040064Shear Web · corrodedFOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-2. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040063Floor Panel · gougedFOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M)Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Floor PanelSDR USAASB04037Sensor · failedCLT - FLT 401 - DURING CRUISE, EN ROUTE FROM CLT-IND, THE AIRCRAFT EXPERIENCED MULTIPLE AVIONICS AND SYSTEM FAILURES. AIRCRAFT LOST THE FLIGHT DIRECTOR, L NAV, TRANSPONDER, CABIN PRESSURIZATION AND LOW IDLE ON ENGINE. CREW DECLARED AN EMERGENCY AND RETURNED Mar 26, 2004 · N352US · Boeing 737301 · Landing Gear Position and WarningSDR USAA040120Keelbeam · corrodedFOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED REPAIR STRAP PER EA 78097. LEVEL 1 TASK NR C53-212-01. (M)Mar 24, 2004 · N354US · Boeing 737301 · Fuselage Main, KeelSDR USAA040044Skin · crackedFOUND SKIN CRACKED 1.5 INCH, EXTERNAL FUSELAGE SKIN STATION 765 STRINGER 23R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M)Mar 24, 2004 · N334US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040045Skin · crackedFOUND SKIN CRACKED 1 INCH, EXTERNAL FUSELAGE SKIN STATION 727D PLUS 2 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Mar 24, 2004 · N334US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB04035Coalescer Bag · contaminatedPHL - FLT 1483 - EN ROUTE FROM BTV TO PHL, CREW REPORTED STRONG FUMES THROUGH OUT THE CABIN. MAINTENANCE CHECKED FOR LEAKS AT BOTH THE APU AND THE PACK AREA. NO LEAKS WERE NOTED. RAN ENGINES WITH BOTH PACKS ON FROM IDLE TO TAKEOFF POWER. NO FUMES NOTED. RAMar 23, 2004 · N584US · Boeing 737301 · Humidity Control SystemSDR AWXA200400324Tab · delaminatedMCN - MAJOR REPAIR - LOWER SURFACE OF RIGHT WING AILERON CONTROL TAB DELAMINATED AT WBL 456. MAINTENANCE PERFORMED BOND REPAIR ON RT WING AILERON CONTROL TAB AT WBL 456 IAW B737-300 SRM 51-70-16.Mar 21, 2004 · N325AW · Boeing 737301 · Aileron TabsSDR SWAA040853Cable · misroutedDURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.Mar 21, 2004 · N660SW · Boeing 737301 · Escape SlideSDR SWAA040852Light · looseDURING SCHEDULED C1 CHECK, FOUND RT FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM.Mar 21, 2004 · N660SW · Boeing 737301 · Emergency LightingSDR USAASB04033Warning Light · illuminatedON CLIMB-OUT FROM PHL, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M)Mar 18, 2004 · N576US · Boeing 737301 · Landing Gear Position and WarningSDR USAASB04032Door · openAFTER TAKEOFF, CREW COULD NOT GET THE A/C TO PRESSURIZE. FLT ATTENDANT REPORTED AN AIR LEAK COMING FROM FWD ENTRY DOOR. ALL OTHER INDICATIONS NORMAL. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX FOUND FORWARD ENTRY Mar 17, 2004 · N356US · Boeing 737301 · Passenger/Crew DoorsSDR USAASB04031Uplock Sensor · failedORD - FLT 1082 - ON CLIMB-OUT FROM ORD, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AFTER FOLLOWING ABNORMAL PROCEDURE CHECKLIST, DECISION WAS MADE TO RETURN TO FIELD AT ORD. FLIGHT LANDED WITHOUT FURTHER INCIDMar 16, 2004 · N576US · Boeing 737301 · Landing Gear Position and WarningSDR SWAA040771Slide · dislodgedL1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR EVAC SLIDE PER MM.Mar 13, 2004 · N659SW · Boeing 737301 · Escape SlideSDR USAASB04028Wire · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ON BULLNOSE AT SEAT ROW 6, RIGHT SIDE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT D2912 AND REPLACED BLOWN FUSE, P/N 21031-0005, IN POWER SUPPLY M1135. OPERATIONAL CHECK GOOD. (M)Mar 11, 2004 · N573US · Boeing 737301 · Light System WiringSDR USAA040055Stringer · crackedCLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVAL PER SRM 53-00-01 DETAIL XI FIG 229. (M)Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040054Stringer · crackedFOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVED PER SRM 53-00-01 FIG 229 DETAIL XI. (M)Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAASB04024Arm · fracturedCLT - FLT 240 - UPON GEAR RETRACTION, CREW HEARD A LOUD THUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BOTH LUGS OF THE LEFT MAIN GEAR ACTUATOR BEAM ARMMar 2, 2004 · N355US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USA2004F00019Arm · crackedUPON GEAR RETRACTION, CREW HEARD A LOUD THRUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. LT MAIN LANDING GEAR ACTUATOR BEAM ARM FOUND CRACKED. REAR Mar 2, 2004 · N355US · Boeing 737301 · Landing Gear ActuatorSDR USA2004F00002Charger · failedMAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK (PN 20131A). OPERATIONAL CHECK GOOD.Feb 29, 2004 · N356US · Boeing 737301 · Emergency LightingSDR USAA040031Stiffener · corrodedPIT - FOUND STIFFENER CORRODED, BS 1016 APBH CHANNEL STIFFENER RIGHT SIDE BOTTOM. CORRODED SECTIONS REPLACED PER EO 5302V112. (M)Feb 28, 2004 · N356US · Boeing 737301 · Fuselage Main, BulkheadSDR USA2004F00013Adc · failedSHORTLY AFTER TAKEOFF, ENROUTE, ALL THE CAPTAINS AIR AND FLIGHT INSTRUMENTS FAILED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AIR DATA COMPUTER. PERFORMED SATISFACFeb 28, 2004 · N356US · Boeing 737301 · Air Data ComputerSDR USAA040030Bulkhead · corrodedPIT - FOUND REAR PRESS BULKHEAD CORRODED 2 INCHES BY 4 INCHES, STATION 1016 BL 0 REAR PRESSURE BULKHEAD. CORRODED SECTIONS REPLACED PER EO 5302V112. (M)Feb 27, 2004 · N356US · Boeing 737301 · Fuselage Main, BulkheadSDR SWAA040644Slide · out of adjustL2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.Feb 27, 2004 · N660SW · Boeing 737301 · Escape SlideSDR SWAA040569Slide · dislodgedL1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE L1 DOOR EVAC SLIDE INTO CONTAINER PER MM.Feb 24, 2004 · N659SW · Boeing 737301 · Escape SlideSDR USAA040050Skin · crackedFOUND SKIN CRACKED 2.5 INCHES, BS 520 S12R. INSTALLED DOUBLER PER EA 95192. (M)Feb 20, 2004 · N353US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200400188Light · inoperativeDURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.Feb 19, 2004 · N325AW · Boeing 737301 · Emergency LightingSDR AWXA200400187Light · inoperativeEEL, DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD.Feb 19, 2004 · N325AW · Boeing 737301 · Emergency LightingSDR SWAA040498Slide · looseL1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.Feb 17, 2004 · N659SW · Boeing 737301 · Escape SlideSDR USAA040049Skin · crackedFOUND SKIN CRACKED 2 INCHES, 727D AND S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)Feb 12, 2004 · N355US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA040421Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM.Feb 9, 2004 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA040360Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STRINGER 24L. REPAIRED SKIN PER SRM.Feb 4, 2004 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA040327Module · faultyAIRTURN BACK, POWER STANDBY LIGHT ILLUMNINATED IN FLIGHT. QRH PROCEDURES FOLLOWED. LIGHT WOULD NOT RESET. REMOVED AND REPLACED STANDBY POWER MODULE PER MM.Feb 1, 2004 · N659SW · Boeing 737301 · DC Power Distribution SystemSDR USAA040009Stringer · corrodedPIT - FOUND STRINGER WITH 5 INCH CORROSION, S25L AT STATION 356 VERTICLE LEG OF STRINGER. CORROSION LEVEL 2, TASK NR C53-201-01. REMOVED STRINGER DAMAGE, INSTALLED SPLICE SECTION PER EA 77521. (M)Jan 25, 2004 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAASB04010Charger · inoperativePHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jan 21, 2004 · N560AU · Boeing 737301 · Emergency LightingSDR USAA040008Stiffener · corrodedPIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, BS 1016 APBH BL-0. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER BOEING DWG 65C28106 REF EO 5302V112A. (M)Jan 20, 2004 · N587US · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400176Clevis · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD CLEVIS, AT FORWARD LOWER FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD CLEVIS; OVERSIZED CENTER SECTION CLEVIS FORWARD LOWJan 20, 2004 · N324AW · Boeing 737301 · Horizontal Stabilizer Miscellaneous StructureSDR USAA040100Skin · damagedPIT - FOUND SKIN WITH SCRIBE MARKS 260 INCHES IN LENGTH, STRINGER 10 LEFT BS 360-540. ACCOMPLISHED CUT-OUT AND INSTALLATION OF REPAIR DOUBLER PER EA 77471. (M)Jan 19, 2004 · N573US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200400128Strap · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0156 INCH CRACK WAS FOUND ON FUSELAGE SPLICE STRAP AT BS 358, STR 28 RT, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF STRAP BETWEEN STR 27 RT AND STR 28 RT AT BS 358; FABRICATED A NEW SECTION OF REPLACEMEJan 17, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400166Stringer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT AT BS 344, AFT EDGE OF E&E BAY DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED STRINGER 28 RT FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT STRINGER CHANNEL PER DWG 69-489Jan 16, 2004 · N324AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200400047Light · brokenDFW - EEL - DURING THRU FLIGHT INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT SEAT ROW 8 LT BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD.Jan 14, 2004 · N325AW · Boeing 737301 · Emergency LightingSDR USAA040095Skin · crackedFOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M)Jan 13, 2004 · N354US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA040098Slide · out of adjustR2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDES PER MM.Jan 10, 2004 · N659SW · Boeing 737301 · Escape SlideSDR AWXA200400119Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1.1875 INCH CRACK WAS FOUND ON R-2 DOOR FORWARD FRAME SURROUND WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948, RBL 62, WL 251. MAINTENANCE REMOVED CRACKED SECTION OF R-2 DOOR WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948,Jan 9, 2004 · N324AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200400100Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727A, STR 2 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B7Jan 9, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach Fittings
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