N944WN
Service difficulty reports · 204
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 = 'N944WN' 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 = 'N944WN' 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 SWAA2024101045747Hook And Loop · detachedFWD ENTRY DOOR ESCAPE SLIDE; HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] REPOSITIONED AND ATTACHED HOOK AND LOOP STRIPS TO GIRT BAR ON THE BACKING PAN SHELF PER 25-66-01 & MT 725-61-06SDR SWAA2024092541178Engine · failed#1 ENGINE FAILURE PASSING THROUGH 10;000 FT MILD VIBRATION AND OVER TEMP OIL QTY 16% ON LANDING<[01] REMOVED AND REPLACED #1 ENGINE PER MT 771-00-01. REFERENCE TTG8Q0064PQR.;[02] ADDED FAULT TTG8Q00W2JEX TO CAPTURE RII REQUIREMENT AS REQUESTED BY LARRY STALLCUSDR SWAA2024052990540Lens · missingINTERIOR EMG LIGHT LENS ON CA SIDE OVERWING EXIT MISSING<[01] INSTALLED NEW LENS COVER IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.SDR SWAA2024042376735Handle · looseFWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] TIGHTENED FWD SERVICE DOOR HANDLE CAM PLATE PER AMM 20-50-11;[02] C/W INSPECTIONSDR SWAA2023122028404Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241DF HAS DELAMINATION DAMAGE ON TOP.<[01] REFER TO FAULT TTG8Q00Q3BDA WHERE EA 23-153-03594 WAS ADDED AS A SUBTASK.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2023122028406Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231XF HAS DELAMINATION DAMAGE ON TOP.<[01] REFER TO FAULT TTG8Q00Q3BDA WHERE EA 23-153-03594 WAS ADDED AS A SUBTASK.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2023122028405Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231EF HAS DELAMINATION DAMAGE ON TOP.<[01] UPDATED STEP 1.;[02] COMPLETED STEP 1;[03] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 231EF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-81 ITEM 35 MAINTENANCE WAS ACCOMPLISHSDR SWAA2023122028407Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231GF HAS DELAMINATION DAMAGE ON TOP.<[01] UPDATED STEP 1.;[02] UPDATED STEP 1;[03] IDENTIFIED FLOOR PANEL 231GF IAW SRM 53-00-50-0I-1 FIG. 3 SHEET 1 TABLE 3 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FABRICATESDR SWAA2023122028409Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231KF HAS DELAMINATION DAMAGE ON TOP.<[01] UPDATED STEP 1.;[02] UPDATED STEP 1;[03] IDENTIFIED FLOOR PANEL 231KF IAW SRM 53-00-50-0I-1 FIG. 3 SHEET 1 TABLE 3 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FABRICATESDR SWAA2023122028408Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232CF HAS DELAMINATION DAMAGE ON TOP.<[01] PASSENGER CABIN FLOOR PANEL 232CF WITH DELAMINATION DAMAGE ON TOP WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] UPDATED STEPSDR SWAA2023122028410Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232DF HAS DELAMINATION DAMAGE ON TOP.<[01] UPDATED STEP 1.;[02] UPDATED STEP 1;[03] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 232DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-81 ITEM 75 MAINTENANCE WAS ACCOMPLISHEDSDR SWAA2023122028083Girt Bar · brokenFWD SERVICE DOOR SLIDE COVER; AFT GIRT BAR BRACKET HAS BROKEN RIVET<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE COVER; AFT GIRT BAR BRACKET IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2023122028082Rib · crackedHORIZONTAL STAB RIB #4 AFT STIFFENER IS CRACKED AT LOWER RADIUS. (STAB STA 120.3; MARKED)<[01] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-5 REPAIR 5.;[03] UPDATED STEP 3.;[04] VERIFIED STEP 2.;[05] REMOSDR SWAA2023122027951Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] CRACK WAS FOUND TO BE OUT OF LIMITS REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR AS PER SRM 57-10-10-2R-5.;[02] VERIFIED CORRRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2023122028068Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION DAMAGE ON TOP.<[01] UPDATED STEPS 4;5.;[02] UPDATED STEP 4 AND 5;[03] IDENTIFIED FLOOR PANEL 241AF IAW SRM 53-00-50-0I-1 FIG. SHEET 1 TABLE 4 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FASDR SWAA2023090196241Slide · out of adjustR2 SLIDE FALLING FROM BUSTLE<[01] REPACKED R2 SLIDE IAW MT 725-61-06.SDR SWAA2023070573641Lens · looseLENSE COVER MISSING AT 12F (EXIT LENSE LOOSE)<[01] REPLACED LOOSE LENSE COVER FOR EMER EXIT LIGHTS AT 12F PER AMM 33-51-00.SDR SWAA2022013162298Light · inoperativeINOP EMERGENCY LIGHT POWER SUPPLY ASSY ROW 11 RT SIDE AT PASSENGER CABIN ; 2021-567452 / [01] REPLACEMENT EMERGENCY LIGHT POWER SUPPLY ASSY ROW 11 RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.; [02] CORRECTED STEP 1: REPLACEMENT EMERGENCY LIGHTSDR SWAA2022013157828Rib · crackedSUPPLEMENTAL INFORMATION: CRACK FRONT SPAR INSPAR RIB 4 STA 111.10 AT 37 INCH RT HORIZONTAL STAB ; 2021-567428 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 2000053402 DUE DATE: 23-APR-22; [02] PERFORMED PERMANENT REPAIR ON INSPAR RIB LOSDR SWAA2022013157677None · crackedSUPPLEMENTAL INFORMATION: CRACK ANGLE - CLIP LOCATED BS440 AND STR 26L AT LEVEL FLOOR STRUCTURE LH SIDE AT FWD CARGO COMPARTMENT ; 2021-567427 / [01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS440 AND STR 26L AT LEVEL FLOOR STRUCTURE LH SIDE AT FWD CARGO COSDR SWAA2022013155267Service Door · corrodedCORROSION INTERNAL SKIN TOILET SERVICE DOOR 145AL BETWEEN BST 847 TO BST 867 LBL 31 AND WL 165.1 AT LOWER FUSELAGE ; 2021-567374 / [01] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130061901; CAL DUE DATE: 11-MAY-22; [02] REPLACED TOILET SERVICE DOOR #SDR SWAA2022013154926Plate · brokenBROKEN ACCESS PANEL 441AT LATERAL RETAINER PLATE AT RT PYLON (1 EA) ; 2021-567318. / [01] REPLACED RETAINER PLATE AND FASTENERS (1EA) ON ACCESS PANEL 441AT AT RT PYLON IAW B737-700 SRM 51-40-02; [02] CORRECTIVE STEP 1 REPLACED RETAINER PLATE AND FASTENERS (1EASDR SWAA2022013154922Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 RBL21 WL156 AFT CARGO. REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BS767 TO BS787 RBL21 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DWG# 146A0081 SHEET 43 REV -SDR SWAA2022013154923Support · corrodedCORROSION SUPPORT ZEE LOCATED BS727 TO BS847 LBL21 WL156 AFT CARGO COMPARTMENT ; 2021-567312 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 130066401 DUE DATE: 17-JUN-22; [02] REPLACED SUPPORT LOCATED BS727 TO BS847 LBL21 WL156 AFT CARGO COMPARTMENSDR SWAA2022013154924Strap · corrodedCORROSION STRAP LOCATED BTW BS767 TO BS787 AND BTW RBL21 TO LBL21 WL156 AFT CARGO. REPLACED STRAP LOCATED BTW BS767 TO BS787 AND BTW RBL21 TO LBL21 WL156 AFT CARGO IAW SRM 51-40-02 AND DWG #146A7500; SHEET 1; REV B;SDR SWAA2022013154921Support · corrodedCORROSION SUPPORT ZEE LOCATED BS727 TO BS767; RBL21 AND WL156 AFT CARGO MADE AND DRILLED NEW SUPPORT ZEE IAW SRM B737-700 51-40-05 AND DRAWING 146A7502 SHEET 2 REV: A. REPLACED SUPPORT ZEE LOCATED LOCATED BS727 TO BS767; RBL21 AND WL156 AFT CARGO IAW SRM SDR SWAA2022013154925Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.5 INCH APPROX ; 2021-567315 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600 D; S/N: 210136503; DUE DATE: 0SDR SWAA2022013154912Frame · crackedCRACK FRAME ON BS 312 AT LEVEL S-5L AT FWD GALLEY AREA ; 2021-567193 / [01] NO CRACK INDICATION FOUND. REPAIRED FRAME LOC. BS BS 312 AT LEVEL S-5L AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 FIGURE 203 REPAIR 1. THIS REPAIR IS CATEGORY B AND MUST BE INSDR SWAA2022013154911Web · crackedCRACK WEB LOCATED BS 294.5 TO BS BS 303.9 AND S-16L AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BS 294.5 TO BS BS 303.9 AND S-16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG:141A8180 SHEET:22 REV- PART USED P/N:141A8181SDR SWAA2022013154909Tie Clip · crackedCRACK TIE CLIP LOCATED BS 277 AND S- 10R AT PASSENGER CABIN ; 2021-567184 / [01] REPLACED TIE CLIP LOCATED BS277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG #141A1110; SHEET 18; REV -; [02] CORRECTIVE ACTION 1 CORRECTED<BR><BR>REPLACED TIE CSDR SWAA2022013154917Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344 AND LBL45 FWD GALLEY AND LAV ; 2021-567199 / [01] REPLACED WEB LOCATED BETWEEN BS328 TO BS344 AND LBL45 FWD GALLEY AND LAV IAW SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 141A5400 SHEET 44SDR SWAA2022013154915None · crackedCRACK INNER CHORD LOCATED BS303 AND LBL57 AT FWD GALLEY AREA ; 2021-567200 / [01] REPLACED INNER CHORD LOCATED BST 227+6 INCH TO BST 360 AND LBL57 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 142A0050 REV:- ; PART USED P/N: 654A0004-1073 SDR SWAA2022013154916Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL45 FWD GALLEY AND LAV ; 2021-567197 / [01] REPLACED NEW WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL45 FWD GALLEY AND LAV. IAW B737-700 SRM 51-40-02; B737-7SDR SWAA2022013154920Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS540 AND BL0 TO LBL24 AT PASSENGER CABIN ; 2021-567235 / [01] REPLACED SUPPORT ANGLE LOCATED BS540 AND BL0 TO LBL24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND 51-40-02; MATERIAL USED: PN# 143A5240-35; BATCH#2021002885. SEE INSDR SWAA2022013154390Grommet · brokenBROKEN FITTING GROMET LOCATED ON BS1016 AND BL0 UPPER STRUCTURE AT PASSENGER CABIN ; 2021-567194 / [01] REPLACED FITTING GROMET LOCATED ON BS1016 AND BL0 UPPER STRUCTURE AT PASSENGER CABIN IAW B737-700 SOPM 20-50-03.; [02] REPLACED FITTING GROMET LOCATED ON BSSDR SWAA2022013154389Bracket · crackedCRACK BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE (1 EA) ; 2021-567190. / [01] REPLACED BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-SDR SWAA2022013154276Fairing · brokenBROKEN ACCESS PANEL 194FL BODY FAIRING PIPELINE DRAIN FUSELAGE EXTERIOR ; 2021-567168 / [01] REPLACED DRAIN ASSY FUSELAGE EXTERIOR LOC. ACCESS PANEL 194FL BODY FAIRING IAW B737-700 SRM 51-10-02 ITEM 9 AND AMM 28-25-07-420 801 ITEM 3G (1) (A) TO (C) PART USED PSDR SWAA2022012854018Scuff Plate · crackedSUPPLEMENTAL INFORMATION: CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-567144 / [01] TOOL USED; DIGITAL CALIPER P/N:700-113-10 S/N:0023256 DUE DATE:06-OCT-22.; [02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRMSDR SWAA2022013153589Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED HFEC INSPECTION ON CUT OUT EDGE OF THE STIFFENER AND WEB AS PER NDT MANUAL D637239 PART 06 51-00-00 PROCEDURE 23 NO CRACKS FOUND. PERFORMED HFEC INSPECTION OF SDR SWAA2022013153590Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB ; 2021-567111 / [01] PERFORMED HFEC INSPECTION OF THE CUT EDGE OF THE STIFFENER AND WEB AS PER NDT MANUAL D637239 PART 06 51-00-00 PROCEDURE 23 NO CRACKS FOUND. PERFORMED PSDR SWAA2022013153587Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED IRSS 216 RT WING ; 2021-567112 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED IRSS 216 RT WING IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED PLATE ASSY TRSDR SWAA2022013153588Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE LOCATED IRSS 215 APROX. AT LT WING ; 2021-567109 / [01] REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE LOCATED IRSS 215 APROX. AT LT WING IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDSDR SWAA2022013153478Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AT LEVEL FLOOR STRUCTURE RH SIDE FWD CARGO COMPARTMENT ; 2021-567087 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AT LEVEL FLOOR STRUCTURE RH SIDE FWD CARGO COMPARTMENT IAW B737-7SDR SWAA2022013153165Angle · crackedCRACK ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT ; 2021-567086 / [01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 AND DWSDR SWAA2022013153479Bracket · brokenBROKEN REAR SPAR SUPPORT BRACKET LOCATED IRSS140 UPPER AREA AT RT WING ; 2021-567093 / [01] REPLACED REAR SPAR SUPPORT BRACKET LOCATED IRSS140 UPPER AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART NUMBER USED: 115A5582-2; P.O: 2021 24283SDR SWAA2022013156092Bracket · elongatedELONGATED HOLE SUPPORT BRACKET LOCATED INTERNAL CAVITY 511AT LEADING EDGE AT LT WING ; 2021-567078 / [01] REPLACED SUPPORT BRACKET LOCATED INTERNAL CAVITY 511AT LEADING EDGE AT LT WING IAW B737-700 SRM 51-10-02 AND 51-40-02; MATERIAL USED: PN#212A1214-1; PO#20SDR SWAA2022013156093Bracket · elongatedELONGATED HOLE SUPPORT BRACKET LOCATED INTERNAL CAVITY ACCESS PANEL 611AT LEADING EDGE AT RT WING ; 2021-567079 / [01] REPLACED SUPPORT BRACKET LOCATED INTERNAL CAVITY ACCESS PANEL 611AT LEADING EDGE AT RT WING IAW B737-700 SRM 51-10-02 AND 51-40-02; MATERIAL SDR SWAA2022013152692Gusset · crackedCRACK GUSSET LOCATED ON BS 500D STRINGER 19L FWD CARGO COMPARTMENT ; 2021-567052 / [01] REPLACED GUSSET AND FASTENERS LOCATED ON BS 500D STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 DWG 143A7902 SHEET 259 REV- SEE INDIVSDR SWAA2022013152802Gusset · crackedCRACK GUSSET LOCATED ON BS 500D STRINGER 19R FWD CARGO COMPARTMENT ; 2021-567053 / [01] REPLACED GUSSET AND FASTENERS LOCATED ON BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 DWG 143A7902 SHEET 259 REV-. SEE INDISDR SWAA2022013152688Light · crackedCRACK SIDEWALL PANEL 232YJW EMERGENCY LIGHT COVER LENS AT PASSENGER CABIN (1 EA) ; 2021-567041 / [01] REPLACED SIDEWALL PANEL 232YJW EMERGENCY LIGHT COVER LENS AT PASSENGER CABIN (1 EA) IAW AMM 33-51-01-960-801 ITEM 2C STEP (4); [02] TASK COMPLETED.
Back to N944WN