Boeing 737-317
Service difficulty reports · 1,542
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 = '737317' 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 = '737317' 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 F3LA200200214Floorbeam · corrodedDURING C-7 CHECK, INSPECTION NOTED CORROSION ON STA 328 FLOORBEAM, NEAR PREVIOUS REPAIR NEAR L1 DOOR SILL. MAINTENANCE FOUND THE BEAM TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 53-10-51. MAINTENANCE REMOVED AND REPLACED THE UPPER CHORD OF STA 328 FLOORBEAM, SDR F3LA200200213Floorbeam · corrodedDURING C-7 CHECK, INSPECTION NOTED LIGHT SURFACE CORROSION IN FORWARD ENTRY AT STA 344. MAINTENANCE FOUND THE STA 344 FLOORBEAM TO BE OUT OF LIMITS IAW SRM 53-10-51. MAINTENANCE REMOVED AND REPLACED THE UPPER CHORD OF STA 344 FLOORBEAM, WL 208, RBL 17 THROUGSDR F3LA200200212Floor PanelDURING C-7 CHECK, INSPECTION NOTED LIGHT CORROSION IN THE AFT CARGO PIT AT FRAME STA 727 C, UNDER LEFT FLOOR TRANSITION PANEL. MAINTENANCE REMOVED THE SURFACE CORROSION IN ACCORDANCE WITH SRM 51-10-02, TREATED, PRIMED AND PAINTED THIS AREA IN ACCORDANCE WITH SDR F3LA200200211Tie Clip · corrodedDURING C-7 CHECK, INSPECTION NOTED CORROSION IN STRINGER CLIP AT STA 787, STR 26 R. MAINTENANCE FABRICATED STRINGER CLIP IN ACCORDANCE WITH BOEING DRAWING 69.35352. THE PART WAS THEN TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS SDR F3LA200200210Skin · crackedDURING C-7 CHECK, INSPECTION NOTED A CRACK IN THE FUSELAGE SKIN AT STA 727E STR 21 R. MAINTENANCE REMOVED THE DAMAGE. A DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01 FIGURE 201 AND SRM 53-60-01.SDR F3LA200200209Tie Clip · crackedDURING C-7 CHECK, INSPECTION NOTED STRINGER TIE CLIP AT STA 727E, STR 7 L WAS CRACKED. MAINTENANCE REMOVED THE CLIP, FABRICATED AND INSTALLED A NEW CLIP IN ACCORDANCE WITH THR ERQUIREMENTS OF BOEING DRAWING 69-35352 AND SRM 51-30-02 AND SRM 51-40-02.SDR F3LA200200208Skin · crackedDURING C-7 CHECK, INSPECTION NOTED A CRACK IN THE RIGHT HAND FUSELAGE SKIN AT STA 727E, BETWEEN STR 22 R AND 23 R. MAINTENANCE REMOVED THE DAMAGE, FABRICATED A DOUBLER AND INSTALLED THE DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01, FIGURE 201 ASDR F3LA200200207Skin · crackedDURING C-7 CHECK, INSPECTION FOUND A CRACK IN FUSELAGE SKIN AT STA 727E, STR 22 R. MAINTENANCE REMOVED THE DAMAGE, BLENDED THE AREA. A DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01 FIGURE 201 AND SRM 53-60-01.SDR F3LA200200206Tie Clip · crackedDURING C-7 CHECK, INSPECTION FOUNG A BROKEN TIE CLIP TO STRINGER AT STA 639 STR 4L. mAINTENANCE INSTALLED NEW STRINGER TIE CLIP AT STA 639 STR 4L IN ACCORDANCE WITH SRM 51-10-02 AND 51-40-03.SDR F3LA200200205Tie Clip · crackedDURING C-7 CHECK, INSPECTION NOTED CRASKS IN TIE CLIP TO STRINGER AT TOP RIVET AT STA 663 STR 10 LH. MAINTENANCE REPAIRED THE CONDITION BY INSTALLING A NEW CLIP AT STA 663 STR 10 L IN ACCORDANCE WITH SRM 51-10-02.SDR F3LA200200204Crossbeam · crackedDURING C-7 CHECK, INSPECTION NOTED CABIN FLOOR EXPANSION JOINT CROSS MEMBERS CRACKED AT FASTENER STATION 540 RBL 44, UNDER THE FLOOR. MAINTENANCE REPAIRED THE EXPANSION IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-2 AND 51-10-2.SDR F3LA200200203Skin · canningDURING C-7 CHECK, INSPECTION FOUND THE FUSELAGE SKIN AT BS 928, STR 21 LT, OIL CANNED (BUCKLED). MAINTENANCE REMOVED SECTION OF SKIN, FABRICATED REPAIR DOUBLER AND TRIPLER. PARTS WERE INSTALLED IN ACCORDANCE WITH SRM 51-40-02SDR F3LA200200200Stringer · crackedDURING C-7 CHECK, INSPECTION REPORTED A CRACK IN TIE CLIP TO STRINGER AT STA 616, STR 4R. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER WITH NEW PART IN ACCORDANCE WITH SRM 51-10-02.SDR F3LA200200199Stringer Clip · crackedDURING C-7 CHECK, INSPECTION REPORTED A CRACK IN TIE CLIP TO STRINGER AT STATION 540, STRINGER 5R. MAINTENANCE REMOVED AND REPLACED STRINGER CLIP, IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-01 AND SOPM 20-41-02.SDR 375PA0024Lens · looseFWD EMERGENCY FLOOR TRACK LIGHT LENS LOOSE AND INOP. INSTALLED NEW EMERGENCY LIGHT FLOOR ASSY. IAW 737-300 MM 33-51-81.SDR SWAA021493Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM.SDR SWAA021492Lens · brokenDURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.SDR SWAA021471Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 20L. REPAIRED SKIN PER SRM.SDR SWAA021368Slide · out of positionFWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.SDR SWAA021314Slide · looseSVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.SDR SWAA021062Slide · out of adjustDURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.SDR SWAA021058Slide · out of positionAFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.SDR SWAA021011Slide · out of positionAFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.SDR SWAA020867Bushing · wornDURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE AXIAL PLAY. REMOVED AND REPLACED TAB HINGE BUSHING PER MM.SDR SWAA020764Valve · damagedAIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND INNER STRUT SUPPORT VALVE DAMAGED, WOULD NOT LET STRUT FULLY EXTEND AND ACTUATE AIR SENSOR. REPACKED INNER STRUT AND REMOVED AND REPLACED SUPPORT VALVE PER MM.SDR SWAA020728Slide · out of positionFWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.SDR SWAA020720Flashlight · inoperativeEMERGENCY FLASHLIGHT INOP IN AFT CABIN TOP POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM.SDR SWAA020717Slide · out of adjustDURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.SDR SWAA020606Slide · out of positionAFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.SDR SWAA020609Slide · out of positionFWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.SDR AWXA200200246Wire · brokenMCN - EEL - "C" - DURING C-13 CHECK THE AFT CEILING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND A BROKEN WIRE AT STA 960 EMERGENCY POWER BATTERY PACK CONNECTOR, WIRE WAS REPAIRED IAW BOEING SWPM 20-92-00 PG. 1 & 2, FUNCTIONAL TSDR AWXA200200220Panel · out of adjustMCN - DURING C-13 CHECK RT OVERWING HATCH FAILED CLOSING REQUIREMENT FORCE CHECK. MAINTENANCE ADJUSTED SIDEWALL PANEL IAW BMM 52-21-00 PG 506. RT EMERGENCY EXIT CLOSING FORCE NOW WITHIN LIMITS PER BMM 52-21-00 PG 506.SDR AWXA200200219Panel · out of adjustMCN - DURING C-13 CHECK LT OVERWING HATCH FAILED CLOSING REQUIREMENT FORCE CHECK. MAINTENANCE ADJUSTED SIDEWALL PANEL IAW BMM 52-21-00 PG 506. EMERGENCY EXIT CLOSING FORCE NOW WITHIN LIMITS PER BMM 52-21-00 PG 506.SDR SWAA020497Tab · wornDURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.SDR SWAA020496Tab · wornDURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.SDR AWXA200200247Skin Panel · buckledMCN - MAJOR REPAIR - C - DURING C-13 CHECK LOOSE CHERRY MAX RIVETS WERE FOUND ON ALL 4 SIDES OF CENTER KEEL PANEL, PANEL WAS ALSO BUCKLED AND DISTORTED. MAINTENANCE DRILLED OUT RIVETS, REMOVED PANEL, FABRICATED A NEW PANEL, AND INSTALLED REPAIR IAW AWA ER 03-SDR SWAA020190Pump · failedNR 2 FUEL TANK FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 FUEL TANK FWD BOOST PUMP AND LOW PRESS SWITCH PER MM.SDR SWAA020170Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSE SKIN CRACKED (3 EA) AT BS 727E, STR 21R, BS 735, STR 18R AND BS 870, STR 24R. REPAIRED SKIN PER SRM.SDR AWXA200200067Cover · wrong partYVR - EEL - C - DURING C-13 CHECK EMERGENCY EXIT LIGHT LENS COVERS ON SEATS AT ROWS 10 & 11 WERE FOUND TO BE THE WRONG COLOR. MAINTENANCE REMOVED THE WHITE EMERGENCY LIGHT LENS COVERS AND REPLACED THEM WITH RED EMERGENCY LIGHT LENS COVERS AS PER AWA GENERAL MSDR AWXA200200066Charger · defectiveYVR - EEL - C - DURING C-13 CHECK THE AFT, AFT LT, AND AFT RT BATTERY CHARGERS DID NOT REACH 300 MILLI AMPS WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE AFT, AFT LT AND AFT RT BATTERY CHARGER IAW BMM 33-51-51 PG 206 AND 207. OPERATIONAL TEST WAS GOOD PESDR SWAA020137Slide · out of positionFWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM.SDR SWAA020128Slide · out of positionFWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.SDR AWXA200200034Charger · failedYVR - EEL - C - DURING C-13 CHECK, LT OVERWING EMERGENCY LIGHT DID NOT REACH TEST VALUE OF 300MA. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT BATTERY CHARGER M1134 IAW BMM 33-51-51, PG 206-207, STEP 4A-D. OPERATIONAL CHECK C/W IAW T/C A1C330SDR AWXA200200087Attach Fitting · chafedDURING C-13 CHECK DAMAGE WAS FOUND TO THE LT WING NR 2 L/E SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 2 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.SDR AWXA200200069Support · corrodedYVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 992, LBL 24. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 992, LBL 24; FABRICATED NEW ATTACH ANGLE AND INSTALSDR AWXA200200070Support · corrodedYVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 986 TO BS 1006, LBL 38. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 986 TO 1006, LBL 38; FABRICATED NEW FLOOSDR AWXA200200086Attach Fitting · damagedDURING C-13 CHECK DAMAGE WAS FOUND TO THE RT WING NR 5 SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 5 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.SDR AWXA200200076Floorbeam · crackedDURING C-13 CHECK A 1/4 INCH CRACK WAS FOUND ON AFT CARGO DOORWAY FLOORBEAM AT BS 727E, STR 24R. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK BETWEEN BS 727 TO BS 877 IAW DWG 65-46592, AND SRM 51-40-2, PG. 1.SDR AWXA200200075Intercostal · corrodedYVR - MAJOR REPAIR - DURING C-13 CHECK A 8 INCH AREA OF CORROSION WAS FOUND ON WEB AT LOWER INTERCOASTAL AFT CARGO DOORWAY OPPOSITE OF FLOOR TRACK BS 727A TO BS 727B, STR 24L. MAINTENANCE REMOVED AND REPLACED LOWER INTERCOASTAL FLOOR TRACK AT BS 727A TO BS 727SDR AWXA200200073Support · corrodedYVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 1006, RBL 6. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 1006, RBL 6; FABRICATED NEW ATTACH ANGLE AND INSTAL
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