N949WN
Service difficulty reports · 164
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 = 'N949WN' 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 = 'N949WN' 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 SWAA2025041524925Transmitter · out of limitsON APPROACH TRAILING EDGE STOPPED AT LESS THAN 5 DEGREES WITH A SLIGHT ASYMMETRY. PSEU LIGHT ILLUMINATED AFTER LANDING. <[01] SWAPPED LH & RH FLAP POSITION TRANSMITTERS FOR TROUBLESHOOTING IAW AMM 27-58-01. INITIAL RIG WAS GOOD. NO FIX. RE-CHECK OF RIG VALUESSDR SWAA2024100443816Girt Bar · looseAFT PASSENGER DOOR SLIDE GIRT BAR FLAP IS NOT VELCROWED UP AND SECURE. (DRAGS ACROSS THRESHOLD WHEN CLOSING DOOR).<[01] RESECURED AFT PASSENGER DOOR SLIDE GIRT BAR FLAP VELCRO IAW AMM 25-66-00-201-NGSDR SWAA2024072214617Cable · out of adjustDURING LANDING AT ABOUT 100 FEET AN UNCOMMANDED ROCKING OF THE WINGS FROM LEFT TO RIGHT HAPPENED ALL THE WAY DOWN TO TOUCHDOWN.<[01] INTERROGATED FSEU; FOUND F/C 27-51351; T/E FLAP UCM.<BR>PERFORMED FIM TASK FLAP LOAD RELIEF TEST 27-51-830. NO FAULTS;[02] SUSPSDR SWAA2024070207318Bulb · inoperativeL2 DOOR EMERGENCY EXIT LIGHT ON LAV B HAS BLOWN OUT LIGHT BULB<[01] REMOVED AND RELAMPED LWR L2 DOOR EMERGENCY EXIT LIGHT ON LAV B AND PERFORMED A GOOD IAW AMM 33-51-01-960-801 STEP 2.C(1)(A)4)(C)(2)(3)(4);[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024070206515Panel · delaminatedPANEL 193AR MATING SURFACE HAS DELAMINATION.<[01] REPAIRED DELAMINATION DAMAGE ON PANEL 193AR IAW SRM 51-70-05-2R-6.;[02] VERIFIED JOB COMPLETESDR SWAA2024070205703Shroud · out of adjustAFT ENTRY DOOR ESCAPE SLIDE SHROUD LOWER ATTACH POINT NOT PROPERLY ENGAGED ON BOTTOM SUPPORT BRACKET ON DOOR.<[01] REMOVED AND REINSTALLED AED ESCAPE SLIDE TO ELIMINATE NOTED CONDITION ON TC: TTG8Q00U7FJS;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024070202044Receptacle · corrodedG4 GALLEY HAS CORROSION UNDER THE COFFEE MAKER RAILS<[01] OK TO INSTALL;[02] OK TO INSTALL GIVEN.;[03] COMPLETED STEP 2. IAW AMM 38-10-00-790-801 PER ATS TOOL ID:IS000141 S/N:315583A CAL DUE 12/2024;[04] ALL STEPS COMPLETED;[05] COMPLETESDR SWAA2024070201770Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] STEPS 6 AND 8 COMPLETE;[02] REPAIRED UPPER ATTACH ANGLE BS663 RH PER SRM 57-10-10-2R-5- REPAIR 5 AND EA 24-157-01651 REV A;[03] VERIFIED.;[04] THE DAMAGE WAS REPAIRED PER 737-700 SSDR SWAA2024070201565Rib · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 2ND VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5;[02] VSDR SWAA2024070201106Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 160.<[01] REPAIRED UPPER ATTACH ANGLE BS663 LH PER SRM 57-10-10-2R-5- REPAIR 5 AND EA 24-157-01650 REV A;[02] VERIFIED.;[03] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 57-10-10-2R-5 (REPAIR 5)SDR SWAA2024070200888Vapor Barrier · crackedBS663 RH VAPOR BARRIER REQUIRES PERMANENT REPAIR<[01] UPDATED MEASUREMENTS;[02] REMOVED AND REINSTALLED BS663 VAPOR BARRIER IAW SRM 51-40-02-0G-0; DWG 111A1000; DWG 111A1001; DWG 111A1152 & DWG 149A1152;[03] VERIFIED.SDR SWAA2024070200890Vapor Barrier · crackedL/H B.S.663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] L/H VAPOR BARRIER CRACK AT MIDSPAN WAS REPAIRED IAW SRM 51-70-102R-10.;[02] VERIFIED COMPLETESDR SWAA2024070201098Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED.<[01] LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER REPAIRED IAW B-737-700 SRM 53-10-09-2R-4 REPAIR 4SDR SWAA2024070201100Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED.<[01] THIS TASK CARD WILL BE ACCOMPLISHED WITH COSTUMER CARD TTG8Q00U0Z7G.SDR SWAA2024070201099Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 4TH VERTICAL STIFFENER IS CRACKED.<[01] LEFT HAND HORIZONTAL STABILIZER; INSPAR RIB; AT STATION 120.30; 4TH VERTICAL STIFFENER; WAS REPAIRED IAW B-737-700 SRM 53-10-09-2R-4 REPAIR 4.FIG.SDR SWAA2024070201101Rib · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5;[02] SDR SWAA2024070201105Rib · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5;[02] SDR SWAA2024070201124Skin · crackedCRACK FOUND RH HORIZONTAL STABILIZER LOWER SKIN AT STATION 193.90 RIB 17.5' FROM FWD EDGE .06 LENGTH (MARKED) CORRECTION TO CRACK LENGTH: SHOULD SAY .60' IN LENGTH<[01] TRIMMED-OUT THE DAMAGE PART AT DISCREPANCY AREA AND INSTALLED REPAIR PARTS IAW SRM 55-10-01SDR SWAA2024040370072Transmitter · faultyFLAP POSITION INDICATION DISAGREE ON FINAL WITH FLAPS AT 15 & EAR DOWN FLAPS WERE SELECTED TO 30. THE FLAPS DID NOT GO TO 30. THEY INDICATED 15% 25. WE EXECUTED A GO AROUND. WHILE DIVERTING WE NOTICED THAT BOTH FLAPS WERE INDICATING 25 WITH THE SELECTOR IN 30.SDR SWAA2024010236775Floor Panel · crackedAFT CARGO BAY FLOOR HAS 2 FT CRACK<[01] R&R CARGO FLOOR PANEL 140BF IAW AMM TASK 25-52-10SDR SWAA2023062973201Slide · out of positionFORWARD ENTRY DOOR EMERGENCY SLIDE HAD EXCESS MATERIAL HANGING OVER GIRT BAR<[01] REPOSITIONED FWD ENTRY DOOR ESCAPE SLIDE MATERIAL PER SIPSDR SWAA2023040723459Slide · lowAFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BELOW RANGE<[01] R&R AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PER MT 725-61-06-AE.SDR SWAA2022092683318Light · inoperativeRH OVER WING EMERGENCY LIGHT INOP. / [01] RELAMPED RH OVER WING EMERGENCY LIGHT IAW AMM 33-51-04.SDR SWAA2022071322476Bracket · corrodedCORROSION -- WING TO BODY FAIRING SUPPORT BRACKET HAS FRETTIOG CORROSION; O/B OF ECS EXHAUST. / [01] REMOVED DAMAGE WING TO BODY FAIRING SUPPORT BRACKET O/B OF ECS EXHAUST IN REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW WING TO BODY FAIRING SUPPORT BRACKSDR SWAA2022071318494Floor Splice · elongatedAFT CARGO FLOOR SPLICE AT STA 767+5; O/B HOLES ELONGATED / [01] RECEIVED NEW AFT CARGO FLOOR SPLICE P/N 146A9401-4; NEW SPLICE TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004ABEG;[02] VERIFIED STEP 1.SDR SWAA2022071316537Gusset · crackedFWD CARGO COMPARTMENT AFT L/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19L STA 500D / [01] REMOVED DAMAGED GUSSET REF. SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET REF. 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATESDR SWAA2022071316538Gusset · crackedFWD CARGO COMPARTMENT AFT R/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19R STA 500D / [01] REMOVED DAMAGED GUSSET REF. SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET REF. 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATESDR SWAA2022071315384Access Panel · elongatedCENTER LWR AFT FAIRING ACCESS PANEL 194E FASTENER HOLE ELONGATED (25-162) / [01] PREPARED AREA FOR REPAIR FASTENER HOLE ELONGATED AT CENTER LWR AFT FAIRING ACCESS PANEL#194E AS PER B737-800 SRM 51-70-04-2R-9;[02] REPAIRED ELONGATED HOLE AT CENTER LWR AFT FAIRISDR SWAA2022071315372Channel · corroded** CORROSION ** AFT CARGO RH Z-CHANNEL BETWEEN: STA 767 STA 727; AT STR 25R AND AT WL 156.4; HAS MULTIPLE SPOTS OF CORROSION (DOT 25-13). / [01] REMOVED CORROSION AFT CARGO R/H Z CHANNEL BETWEEN STA. 767 TO STA.727 AND STRINGER 25 LOWER REF. SRM 51-10-02-0G-0;SDR SWAA2022071315083Web · corroded**CORROSION** FWD CARGO DOOR CUTOUT WEB; AT STA: 440 TO 492.4; STR: 25R; WL: 156.4; HAS MULTIPLE SPOTS OF CORROSION (DOT: 25-3). / [01] EVALUATED FWD CARGO DOOR CUTOUT WEB AND FOUND DOOR CUTOUT WEB EXFOLIATED REF B737-700 SRM 53-00-53-1A-2;[02] LOCATED AND DRISDR SWAA2022071315085Rail · corroded** CORROSION ** FWD CARGO; AFT BULKHEAD; CENTER PANEL; LWR FLOOR STRAP; AT STA: 500D HAS MULTIPLE SPOTS WITH CORROSION (DOT 25-4). / [01] REMOVED CORROSION AT FWD CARGO AFT BULKHEAD CENTER PANEL ;LOWER FLOOR STRAP STA 500D;FOUND EXFOLIATED CORROSION AND PASS TSDR SWAA2022071314605Floor Support · crackedMAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ STA 540 LBL-2 MKD DOT / [01] LOCATED AND DRILLED NEW FLOOR SUPPORT AT MAIN CABIN FS 540 LBL 2 IN REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] OK TO TREAT AND PRIME HOLES;[04] TREATED AND APPLIED SDR SWAA2022071314613Angle · crackedFWD CABIN ABOVE L-1 DOOR FUS. CUTOUT FWD FRAME FLANGE CRACKED @ CUTOUT STA 312 MKD DOT / [01] REMOVED FASTENERS AS REQUIRED FOR FREME REPAIR REF USED B737-7 SRM 53-10-07-2R-1 STEP 4.B;[06] FABRICATED ANGLE FRAME REPAIR MATERIAL USED 7075-0 0.063' PO#1416601 LOSDR SWAA2022071314596Web · corrodedCORROSION. ** AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB & STRAP AT STA 1016+11' ;LBL-3 MKD DOT / [01] REMOVED CORROSION IN AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB AND STRAP AT STA 1016+11 AND LBL -3 I.A.W. B737-700 SRM 51-10-02-0G-0.[14] INSTALLING NEW SSDR SWAA2022071314082Panel · crackedAFT CARGO FWD. BULKHEAD PANEL 142 NW CRACK / [01] RECEIVED NEW AFT CARGO FWD BULKHEAD SHROUD PANEL P/N 453A2510-1; NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00BRAM1;[02] VERIFIED STEP 1SDR SWAA2022071313041Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 140AF CRACKED. / [01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140 AF REF AMN 25-52-01-201-801;[02] VERIFIED STEP 1.SDR SWAA2022070713043Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 140DF CRACKED. / [01] AFT CARGO COMPARTMENT FLOOR PANEL 140DF CRACKED. [TTG8Q00CQVV5] <BR><BR> HELP \ LOG OUT \ OMAR MARENCO (SOUTHWEST AIRLINES) AFT CARGO COMPARTMENT FLOOR PANEL 140DF CRACKED. [TTG8Q00CQVV5] <BR><BR> HELP \ SDR SWAA2022070713042Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 140BF CRACKED. / [01] REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140 BF. REF AMMM 25-52-01-201 801;[02] VERIFIED STEP 1.SDR SWAA2022071312457Vapor Barrier · crackedRT STA 663 VAPOR BARRIER IS CRACKED / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT RT VAPOR BARRIER FOUND 3 CRACKS OF 14''; 2'' AND 1'' THE LENGTH. REF B737-700 NDT PART 1 51-05-01.;[02] REMOVED THE DAMAGED PLIES AND MADE STOP DRILL AT THE CRACKSDR SWAA2022071312456Skin · crackedCRACK FOUND ON LT HAND HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 16.5' FROM FRONT SPAR ; I/B ROW.CRACK LENGTH : 1.25' CRACK FOUND ON LT HAND HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW.CRACK LENGTH : 1.25' / [01]SDR SWAA2022030177679Handle · brokenFWD SERVICE DOOR - ASSIST HANDLE IS BROKEN / [01] R&R FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31;[02] ABOVE STEPS COMPLETESDR SWAA2022021470988Panel · delaminatedWING TO BODY FAIRING PANEL 193B DELAMINATED. PLANNED DAL 2/24 / [01] REMOVED AND REPLACED 193B WING TO BODY FAIRING PANEL PER TASK CARD# 5351-I-14108-NGSDR SWAA2022012462217Girt Bar · brokenFWD FO SIDE SERVICE DOOR. RT SIDE PLASTIC RING ON GIRT BAR BROKEN ; / [01] REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR STOP-RELEASE PER AMM 25-66-01. REF LP 1917636 FOR ROBBED PART INFO.SDR SWAA2021072697321Doubler · crackedTHE ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS A 2 CRACK IN ZONE 2 AND ADJACENT TO TWO FASTENERS. ; / [01] C/W 10X VISUAL INSPECTION OF THE TRIMMED OUT AREA.; [02] C/W HFEC INSPECTION OF TRIM OUT EDGE AND INTERIOR STRUCTURE PER NDT PART 6 51-00-00SDR SWAA2020120733738Lamp · inoperativeAFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT OUT. RELAMPED AND OPERATIONS CHECK NORMAL, PER AMM 33-51-00.SDR SWAA2021071431100Floor Support · crackedFORWARD CARGO AIR CONDITIONING DISTRIBUTION BAY CENTER RIGHT FLOOR SUPPORT IS CRACKED AT STA540 / REMOVED AND REPLACED FORWARD CARGO AIR CONDITIONING DISTRIBUTION BAY CENTER RIGHT FLOOR SUPPORT PER SRM 51-10-02 AND SRM 51-40-02.SDR SWAA2020111831105Battery · no testCABIN EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATIONS M01668; M01669; M01670; M01672 AND M01673. REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERIES AT LOCATIONS M01668; M01669; M01670; M01672 AND M01673, PER AMM 33-51-06.SDR SWAA2020081006704Slide · looseF/A REPORTS AFT ENTRY DOOR SLIDE IS CATCHING ON THE DOOR FRAME.SECURED AFT ENTRY DOOR SLIDE PER THE MM 25-66-01SDR SWAA2020062994706Glowstrip · missingAFT L/H AND R/H PHOTO LUMINESCENT STRIPS 'AM AND AK' ARE MISSING/DAMAGED. / REMOVED REPLACED AND INSTALLED AFT L/H AND R/H PHOTO LUMINESCENT STRIPS 'AM AND AK' PER AMM 33-51-15.SDR SWAA2020062994697Stringer · crackedLEFT FIXED LEADING EDGE STRINGER FOUND CRACKED. R & R THE STRINGER IAW SRM 51-40-02.
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