N7715E
Service difficulty reports · 200
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N7715E' AND registry_match = 'registration' 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 n_number = 'N7715E' AND registry_match = 'registration' 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 SWAA2024072918199Battery Pack · inoperativeFOUND RH OVERWING ESCAPE EMERGENCY BATTERY PACK INOP.<[01] REMOVED AND REPLACED RH OVERWING ESCAPE BATTERY PACK ASSY. OPS CHECK GOOD. IN REF TO AMM 33-51-06.SDR SWAA2023082893490Access Door · deformedEGPR DOOR IS DEFORMED.<[01] R AND R EXTERNAL POWER RECEPTACLE ACCESS DOOR IAW M/M REF. 52-49-02.SDR SWAA2023082893489Idg · deformedELECTRICAL GROUND POWER (EGPR) DOUBLER LOWER FORWARD FLANGE DEFORMATION<[01] C/W 23-153-02612-WIP1SDR SWAA2022122082898Lamp · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022122080836Scuff Plate · crackedAFT CARGO DOOR CORNER SCUFF PLATE FWD POSITION CRACKED AT ATF CORNER<[01] ACCOMPLISHED WELDING REPAIR AT AFT CARGO COMP. FWD CORNER SCUFF PLATE BY OUTSIDE VENDOR WITH PO.#413972 PER B737-700 SRM 53-60-15-2R-1 STEP B-4 AND BAC 5975. THIS SCUFF PLATE WILL BE INSSDR SWAA2022122078395Floor Panel · delaminatedCABIN FLOOR PANEL 232SF TOP SKIN AFT AREA DELAMINATED<[01] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FIBER REPAIR PLIES; NO CORE DAMAGED; NO WATER NOTE AT FLOOR PANEL 232SF. REF B737 SRM 53-00-50-2R-1 PARAGRAPH 3 AND FIGURE 202.;[0SDR SWAA2022122077924Door Frame · crackedCRACK FOUND AT OPEN FASTENER HOLE AT EXTERNAL R1 DOOR CUT OUT STRUCTURE STA 291.5 + 7', BELOW STR 8R + 5'. REMOVED R1 DOOR CUTOUT FWD UPPER FRAME SECTION (PAN) IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW FRAME SECTION IAW SRM 51-10-02-0G-0. INSTALLED NSDR SWAA2022122077490Floor Panel · crackedMAIN CABIN AFT WET AREA FLOOR PANEL #241ADF CRACKED<[01] REPLACED MAIN CABIN AFT WET AREA FLOOR PANEL #241ADF REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALLED ON FAULT TTG8Q00F29X2;[02] VERIFIED STEP 1SDR SWAA2022122074306Structure · crackedFOUND CRACK AT L-1 DOOR INNER CHORD UPPER FLANGE BS 303.9. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.842'. START TO REMOVE INNER CHORD AT L1 DOOR LOWER SILL IAW SRM 51-40-02-0G-0. COMPLETED REMOVAL OF L1 LOWER SILL INNER CHOSDR SWAA2022122074301Floor Support · crackedMAIN CABIN FWD WET AREA BETWEEN STATION 344-360 BL-0 INTERCOSTAL CRACKED AT FASTENER HOLE<[01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 344-360 BL-0 PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED INTERCOSTAL AT MAIN CABIN PER B737-70SDR SWAA2022122074302Floor Support · crackedMAIN CABIN FWD WET AREA BETWEEN STATION 344-360 LBL 11 INTERCOSTAL CRACKED AT FASTENER HOLE<[01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 344-360 LBL-11 PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED INTERCOSTAL AT MAIN CABIN PER B73SDR SWAA2022122074305Angle · crackedMAIN CABIN FWD WET AREA BETWEEN STATION 380-400 BL-0 UPPER CORD ANGLE CRACKED AT FASTENER HOLE<[01] REMOVED MAIN CABIN UPPER CHORD ANGLE BETWEEN STA 380-400 BL-0 PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED MAIN CABIN UPPER CHORD ANGLE BETWEEN STA 3SDR SWAA2022122074303Angle · crackedMAIN CABIN FWD WET AREA BETWEEN STATION 380-400 RBL-9 UPPER CORD ANGLE CRACKED AT FASTENER HOLE. REMOVED UPPER CORD ANGLE AT MAIN CABIN FWD WET AREA IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED UPPER CORD ANGLE AT MAIN CABIN IAW SRM 51-10-02-0G-0. TREATED ASDR SWAA2022122074300Floor Support · crackedMAIN CABIN FWD WET AREA BETWEEN BS 279-294.5 BL-0 INTERCOSTAL CRACKED. REMOVED THE INTERCOSTAL IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-10-02-0G-0. INSTALLED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR SWAA2022122074304Floor Support · crackedMAIN CABIN FWD WET AREA BETWEEN BS 312-328, LBL 46 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-10-02-0G-0. INSTALLED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR SWAA2022122073289Strap · corrodedCORROSION FOUND ON AFT CARGO FLOOR STRAP AT BS 887, LBL9 RBL 21, WL 155.5. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. FOUND OUT OF LIMITS IAW SRM 53-0053-1A-2 INSTALLED A NEW STRAP SDR SWAA2022122073271Structure · corrodedCORROSION FOUND AT STA 940 LBL-57 ON INNER CORD.<[01] EVALUATED CORROED AREA; FOUND EXFOLIATING CORROSION; PASS THRU.FOUND TO BE OUT OF LIMITS PER REF 53-70-15-1A-1.;[02] CORRECTION STEP#1; WRONG CARD;;[03] CLEANED AREA; NO CORROSION NOTED PER SOPM 20-30-03. WSDR SWAA2022122073270Structure · corrodedL1 DOOR INNER CORD CORRODED AT BS 334. DURING REMOVAL OF CORROSION IAW SRM 51-10-02-0G-0; FOUND A CRACK AT BS 303.9 L-1 DOOR INNER CHORD WAS REPLACED ON TTG8Q00G61KM.SDR SWAA2022122073273Floorbeam · corrodedCORRODED FLOORBEAM FASTENER HOLE BS 986.5, LBL 45. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP IAW NDT P4 51-00-00, PROC 3. ACCOMPLISHED EA-M-21-153-00612.SDR SWAA2022122073274Door Sill · corrodedR2 DOOR SILL CORROED, BS 951 - 992.8. FOUND OUT 0F LIMITS IAW SRM 53-70-15-1A-1. REMOVED DAMAGE ON DOOR SILL IAW SRM 51-40-02-0G-0. REMOVED THE DOOR SILL IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW DOOR SILL IAW SRM 51-40-05-0G-0. INSTALLED THE DOOSDR SWAA2022122073275Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM BS 986.5, RBL40-45.5. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FABRICATED A FILLER & REPAIR IAW SRM 53-70-51-R2R-6 TABLE 204, ALTERNATIVE 4. TREATED AND PRIMED FILLER IAW AMM 51-21-41-370-801 AND 51-21-72-370-804, & INSTALLED SDR SWAA2022122073276Strap · corrodedGALLEY FLOOR STRAP HAS CORROSION STA 1016+5 LBL 4. REMOVED FASTENERS IAW SRM 51-40-02-0G-0. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1. RSDR SWAA2022122072222Rib · crackedSUSPECT CRACK ON LH HORIZONTAL STAB RIB 5 STIFFENER 4. PERFORMED HFEC AT SUSPECTED CRACK ON LH HORIZONTAL STAB. STIFFENER 4 IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED AT LOWER SECTION OF STIFFENER. REMOVED DAMAGE AT LH HORIZONTAL STAB. RIB #5 SDR SWAA2022122072223Floor Panel · damagedMAIN CABIN AFTE WET AREA FLOOR PANEL #241AAF TOP SKIN PEELING OFF SEVERAL AREAS<[01] REPLACED MAIN CABIN AFT WET AREA FLOOR PANEL #241AAF REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00F29X8;[02] VERIFIED STEP 1.SDR SWAA2022122072224Floor Panel · damagedMAIN CABIN CENTER AREA FLOOR PANEL #241AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] REPLACED FLOOR PANEL #241AF AT MAIN CABIN CENTER AREA IAW B737-700 AMM 53-21-00-400-801-NG.;[02] VERIFIED STEP 1.SDR SWAA2022122072865Bracket · crackedDURING REMOVAL OF R/H VAPOR BARRIER FOUND BRACKET AT STA 663.75 BETWEEN RBL45 AND RBL55 CRACKED.<[01] REPLACED RT VAPOR BARRIER BRACKET AT STA 663.75 BETWEEN RBL 45 THRU RBL 55 REF. B737-700 SRM 51-40-02-0G-0. THIS BRACKET WILL BE INSTALL ON FAULT #TTG8Q00G379SDR SWAA2022122072217Bear Strap · crackedR1 DOOR UPPER FWD CUTOUT CORNER BEAR STRAP; CRACK AT STA 291.5+4 RBL52 BETWEEN S8R AND S9R.<[01] PERFORMED HFEC INSP. AT R1 DOOR UPPER FWD CUTOUT CORNER BEAR STRAP AT STA 291.5+4 RBL52 BETWEEN S8R AND S9R. IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK LENSDR SWAA2022122072220Floor Panel · damagedMAIN CABIN FWD WET AREA L/H SIDE FLOOR PANEL #221BF TOP SKIN PEELING OFF SEVERAL AREAS<[01] REPLACED MAIN CABIN FWD WET AREA FLOOR PANEL #221BF. PANEL ASSY WILL BE INSTALLED ON FAULT #TTG8Q00F2A6D;[02] VERIFIED.SDR SWAA2022122072209Support · crackedL/W T/E ACCESS PANEL 561AB SUPPORT STRUCTURE CRACK.<[01] REMOVED AND REPLACED L/W T/E PANEL 561AB SUPPORT STRUCTURE PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED TABLE;[03] VERIFIED STEP 1;2SDR SWAA2022122072212Support · corrodedL/W T/E ACCESS PANEL 561AB SUPPORT STRUCTURE HAS CORROSION AROUND FASTENER HOLES.<[01] THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00G3L8S - FOUND CRACKED WILL BE REPLACE.;[02] VERIFIED STEP #1SDR SWAA2022122072193Vapor Barrier · crackedBS 663.75 VAPOR WEB HAS A VERTICAL CRACK 16 IN LONG AT RBL 31.83 BETWEEN WL 155 AND WL 170. STOP DRILLED SIZE 0.25 AT THE END OF THE CRACK ON VAPOR BARRIER IAW SRM 57-10-10-2R-2 PARA 6.A. PERFORMED VISUAL AND TAP TEST INSPECTION ON DAMAGED VAPOR BARRIER AND SDR SWAA2022092939016None · failedR/H AFT EMERGENCY LIGHS BATTERY PACK FAILED CAPACITY CHECK / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2022092939011None · failedL/H FWD EMERGENCY LIGHS BATTERY PACK FAILED CAPACITY CHECK / [01] REMOVED AND REPLACED BATTERY PACK POWER M/M 33-51-06.;[02] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2022071126850Light · out of positionPHOTO ILLUMINESCENT STRIP BETWEEN ROWS 7 TO 5 IS PEELING. / [01] SECURED STRIP PER SIP.SDR SWAA2022030278610Slide · out of adjustFORWARD SERVICE DOOR GRIT BAR IS STICKING. SLIDE IS NOT ALIGNED CORRECTLY / [01] READJUSTED SLIDE IAW AMM 25-66-00SDR SWAA2022012462770Bracket · cracked193D STATION 727 CRACKED BRACKET. ; 193D STATION 727 LEFT VERTICAL WE RACKET AND T-CLIP CRACKED. / [01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SDR SWAA2021090814902Slide · out of adjustAFT ENTRY DOOR ESCAPE SLIDE PRESSURE GAUGE DIFFICULT TO SEE. ; / [01] ADJUSTED ESCAPE SLIDE @ AFT ENTRY DOOR I.A.W. AMM 25-66-00. PRESSURE GAUGE IS IN VIEW WINDOW.SDR SWAA2021071493016Escape Rope · detachedESCAPE ROPE NOT ATTACHED CAPTAINS SIDE ; / [01] REATTACHED CAPT'S EMERGENCY ESCAPE ROPE IAW AMM 25-61-10. A/C OK FOR SERVICE.SDR SWAA2021062988115Glowstrip · looseEMERGENCY ESCAPE GLOW STRIP AT ROW 8 LOOSE / [01] VERIFIED SECURITY OF EMERGENCY PROXIMITY FLOOR STRIP @ 8A IAW AMM 33-51-15SDR SWAA2021061180733Lamp · inoperativeAFT MOST EMERGENCY LIGHT ON R/H SIDE OF FUSELAGE INOP ; / RELAMPED AFT MOST EMERGENCY LIGHT ON RIGHT SIDE OF FUSELAGE. OPS CK GOOD. PER AMM 33-51-04SDR SWAA2021060178144Light · looseESCAPE LIGHTING ON FLOOR NEXT TO ROW8 LEFT SIDE IS LOOSE. ; / SECURED FLOOR PATH ESCAPE LIGHTING STRIP NEAR ROW 8 PER S.I.P.SDR SWAA2021042665587Light · displacedFLIGHT ATTENDANTS REPORTED LUMINESCENT STRIPS ON CABIN FLOOR BOWED UP AT ROW EIGHT. REPORTED BOTH STRIPS WERE A TRIP HAZARD. AFTER FLIGHT; BOTH STRIPS CARPETING WERE FLAT ON THE FLOOR. RESECURED LUMINESCENT STRIPS ON CABIN FLOOR ROW EIGHT PER SIPSDR SWAA2021041564199Light · loosePHOTO ILLUMINCENT FLOOR LIGHTING FIRST OFFICERS SIDE; LOOSE AT ROW 9 / REMOVED DEBRI FROM UNDER PHOTO ILLUMINCENT FLOOR STRIP @ ROW 9 ON F/O SIDE; RESECURED PHOTO ILLUMINCENT STRIP @ 9D PER SIPSDR SWAA2021011441418Bulb · inoperativeCUSTOMER WALK, R-2 EMERGENCY EXIT SIGN 1 BULB OUT. RE-LAMPED R2 EMERGENCY EXIT SIGN (1) BULB, PER B737 AMM 33-51-01-960-8001. PERFORMED OPERATIONS CHECK OF NEW LAMP AT R2 EMERGENCY EXIT SIGN. TEST FOUND NORMAL.SDR SWAA2021011440708Slide · out of positionQC WALK- R2 DOOR ESCAPE SLIDE SKIRT TOUCHING SCUFF PLATE WHEN CLOSING. TUCKED EXCESS GIRT MATERIAL UPIN THE SLIDE COMPARTMENT ON THE R-2 DOOR SLIDE, IAW CUSTOMER CARD 8725-61-06/W193377 STEP 3. (1) SLIDE SKIRT DOES NOT TOUCH SCUFF PLATE.SDR SWAA2021011440709Skirt · out of positionL2 DOOR ESCAPE SLIDE SKIRT TOUCHING SCUFF PLATE WHEN CLOSING. RE-PADED L2 DOOR ESCAPE SLIDE SKIRT, IAW SOUTHWEST AIRLINES WORK INSTRUCTION NO 8725-61-06 STEP 3 I AND J.SDR SWAA2021011440713Light · unsecureQC WALK- EMERGENCY LIGHT LOCATED OVER ROW 8FED INOPERABLE. RESECURED EMERGENCY LIGHT AT ROW 8FED, AS PER REF B737 AMM 33-51-03-960-801. OPERATES NORMAL.SDR SWAA2021011440214Battery Pack · inoperativeCABIN LT SEATROW 6 ABC; 9 ABC; 12 ABC AND RT 8 DEF OVERHEAD BIN EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 6 ABC; 9ABC; 12ABC AND PERFORMED OPERATIONS CHECK, AS PER B737 AMM 33-51-06-960-805. TEST FOUND NORMAL.SDR SWAA2021042339266Scuff Plate · crackedAFT CARGO COMP. DOOR CUT OUT; AFT SCUFF PLATE CORNER CRACK; P/N 146A8341-9 / RECEIVED WELDED AFT CARGO SCUFF PLATE P/N 146A8341-9 (AFT SIDE) AND INSTALLATION TO BE ACCOMPLISH ON CUSTOMER CARD J753-140-00-02Y.SDR SWAA2021011437758Frame · puncturedEXTERNAL POWER RECEPTICLE AT FRAME STA 235.8, HOLE FROM PREVIOUS REPAIR ON FRAME OUTER CHORD, BETWEEN STRINGER 21 AND STRINGER 22 R. INSTALLED REPAIR FUSELAGE FRAME AT STA 235.8 BETWEEN WL 170 AND 190 AND STRINGER 21 AND 22R, PER RES WI NO 2016562-2 AND SWA E
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