N244WN
Service difficulty reports · 297
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 = 'N244WN' 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 = 'N244WN' 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 SWAA2024052176838Floor Panel · delaminatedAFT FLOOR PANEL 242RF HAS TOP SURFACE DELAMINATION<[01] AFT FLOOR PANEL 242RF WITH TOP SURFACE DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024052176452Tip Cap · crackedRT HORIZ STAB TIP CAP 345A HAS CRACK<[01] CLOSED TIP CAP 345A IAW AMM 27-41-21-400-801;[02] UPDATED PART REMOVED INFO.;[03] CUSTOMER CARD COMPLETESDR SWAA2023112023223Panel · delaminatedWING-TO-BODY FAIRING PANEL 193B DELAMINATED.<[01] LOCATED AND DRILLED FASTENERS HOLES ON NEW 193B PANEL IAW SRM 51-40-06;[02] R/R PANEL 193B PER AMM 53-51-21SDR SWAA2023102715095Panel · debondedDISBONDING IN MULTIPLE LOCATIONS AROUND FASTENER HOLES ON 193B PANEL<[01] #1 FASTENER HOLE 3 LAYERS DISBONDED;[02] #33 FASTENER HOLE 2 LAYERS DISBONDED;[03] #34 FASTENER HOLE 1 LAYER DISBONDED;[04] DISREGARD ABOVE ENTRIES.<BR>#1 FASTENER HOLE 3 LAYERS DISBONDESDR SWAA2023080884686Hinge Pin · brokenA255 -025 PANEL 192G CENTER TANK SUMP PANEL HINGE PIN BROKEN.<[01] REPLACED HINGE PIN OF PANEL 192G CENTER TANK SUMP IAW AMM 53-51-21-000-802 STEP 4.E.5.A.7. AND 53-51-21-400-802 STEP 5.I.2.D.G . <BR><BR>ISSUE TAG A197417;[02] REPLACED HINGE BRAKET P/N MS20001SDR SWAA2023080984063Shield · crackedA225 008 #2 OTBD FAN COWL INNER AFT SHIELD CRACKED AT INNER OIL ACCESS DOOR.<[01] REMOVE #2 OTBD FAN COWL INNER AFT SHIELD AT INNER OIL ACCESS DOOR IAW SRM 51-40-02-0G-0<BR>INSTALLED NEW SHIELD ON #2 OTBD FAN COWL INNER AFT AT INNER OIL ACCESS DOOR IAW SRM 51-SDR SWAA2023080884061Angle · cracked#2 ENGINE AFT STRUT FAIRING; AFT CASTING P/N 313A2752-2; FWD ATTACH ANGLE HAS A 1.3' CRACK. VERIFIED WITH HFEC AND MARKED END IN BLACK.<[01] AUDIT C/WSDR SWAA2023080882928Floor Panel · pulledDOT A24-26 MID CABIN FLOOR PANEL 232SF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] CLEANED UPPER SURFACE OF FLOORBOARD 232SF IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 5A(1);[02] VERIFIED ITEM 1;[03] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0SDR SWAA2023080882932Floorboard · pulledDOT A24-23 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW. 144A5810 AND BAC5085 STEP 8.4.2.<BR>CURED ADHESIVE WITH HEAT LAMP AND DIGITSDR SWAA2023080882934Floorboard · pulledDOT A24-24 MID CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW. 144A5810 AND BAC5085 STEP 8.4.2.<BR>CURED ADHESIVE IN OVEN B0-06 DUE 10-27-SDR SWAA2023080882931Floorboard · pulledDOT A24-22 MID CABIN FLOOR PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] CLEANED PANEL 231YF FOR N.D.T. INSPECTION. IAW B737-700 SRM 53-00-50-2R-0 PAR 5 A(1).;[02] VERIFIED ITEM 1;[03] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0 REPSDR SWAA2023080882660Angle · crackedCRACK FOUND ON VAPOR BARRIER WEB UPPER ATTACH ANGLE AT STA 663 RBL 40 (WL 167)<[01] ACCOMPLISHED OPEN HOLE NDT IAW B737 NDT P6 51-00-00 P16 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] STARTED FABRICATION OF REPAIR ANGLES AND SPLICE IAW SRM 57-10-10-2R-5;[03] SSDR SWAA2023080882661Angle · crackedCRACK FOUND ON VAPOR BARRIER WEB UPPER ATTACH ANGLE AT STA 663 LBL 40 (WL 167)<[01] ACCOMPLISHED OPEN HOLE NDT IAW B737 NDT P6 51-00-00 P16 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] ACCOMPLISHED ATTACH ANGLE REPAIR AT STA 663; LBL 40; WL 167 IAW SRM 57-10-10SDR SWAA2023051147180Web · crackedRT WING TE WEB FITTING AT APPR WS 278.5 CRACKED<[01] REMOVED AND REPLACED RT WING TE WEB FITTING AT APPR WS 278.5 IAW SRM 51-40-02-0G-0-A00729.SDR SWAA2023010486913Lamp · inoperativeL2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMER LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2022112875403Battery · inoperativeFWD LEFT EMERGENCY LIGHT BATTERY DEAD / [01] R&R BATTERY REF AMM 33-51-06 OPS CHECK GOOD NO OTHER DEFECTS NOTED AT THIS TIME A/C OK TO CONTINUESDR SWAA2022112875295Light · out of positionEMERGENCY EXIT LIGHT DETACHED FROM CEILING / [01] INSTALLED LIGHT PER M/M 33-51-01SDR SWAA2022080538824Slide · out of positionSERVICE DOOR SLIDE PACK FELL OUT / [01] REMOVED FWD SERVICE DOOR SLIDE TO REPAIR GIRT BAR SUPPORT PER SRM-51-40-02. C/W MT 725-61-06 FOR SLIDE REPLACEMENTSDR SWAA2022072632082Light · out of positionAFT CEILING EMERGENCY EXIT LIGHT SIGN DETACHED FROM CEILING / [01] RE-SECURED AFT CEILING EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-01.SDR SWAA2022052610714Bracket · looseR2 DOOR FRWD. GIRT BAR FLOOR BRACKET IS LOOSE. / [01] SECURED R2 DOOR FWD GIRT BAR FLOOR BRACKET AS PER B737 AMM 25-66-02-400-801-NG;[02] VERIFIED AND INSPECTED STEP#1; SECURED R2 DOOR FWD GIRT BAR FLOOR BRACKET AS PER B737 AMM 25-66-02-400-801-NG.SDR SWAA2022052510469Light · inoperativeEMERGENCY EXTERIOR LIGHT AT R2 DOOR INOP. / [01] RELAMPED EMERGENCY EXTERIOR LIGHT AT R2 DOOR AS PER B737 AMM 33-51-04-960-801. TEST OK;[02] VERIFIED STEP 1.SDR SWAA2022052610216Panel · delaminatedWTB FAIRING 194E HAS EXTERIOR COMPOSITE DELAM. (MARKED RED DOT 237-1) / [01] CLEANED DAMAGE AREA; CUT OUT DAMAGE SIZE .500' DIA. NO CORE DAMAGE; PERFORMED DRY OUT ; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-1;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPSDR SWAA2022052606747Frame · corrodedFOUND WTB FAIRING SUPPORT FRAME WITH SEVERE WEAR & CORROSION DAMAGE AT LOWER MATTING SURFACE; BS 663-667.68; LBL 20 APPROX. REMOVED CORROSION AT WTB FAIRING SUPPORT FRAME; AS PER B737-7 SRM 51-10-02-0G-0.ORIG. MAT. OF FRAME: 0.100'; MAT. REMOVED: 0.030'; REMASDR SWAA2022053103470Support · corrodedCORROSION AFT CARGO COMPARTMENT. R/H SIDE WALL SUPPORT FRANE UPPER FLANGE DOUBLER REPAIR @ S-25R STA 787 MKD DOT. REMOVED CORROSION ON AFT CARGO COMPARMENT RH SIDEWALL SUPPORT FRAME UPPER FLANGE AS PER B737-700 SRM 51-10-02-0G-0;REMOVED CORROSION ON AFT CARGO SDR SWAA2022052603479Gusset · crackedFWD CARGO COMP STA 500D STR 19L GUSSET CRACKED / [01] REMOVED DAMAGE GUSSET AT FWD. CARGO COMPT. STA. 500D STR. 19L; AS PER B737-7 SRM 51-40-02-0G-0.;[02] LOCATED & DRILLED NEW GUSSET AS PER B737-7 SRM 51-40-05.;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW GSDR SWAA2022052603480Gusset · crackedFWD CARGO COMP STA 500D STR 19R GUSSET CRACKED / [01] REMOVED DAMAGE GUSSET AT FWD. CARGO COMPT. STA. 500D STR. 19R; AS PER B737-7 SRM 51-40-02-0G-0.;[02] LOCATED & DRILLED NEW GUSSET AS PER B737-7 SRM 51-40-05.;[03] VERIFIED STEPS 1 AND 2;[04] OK TO INSTALL GSDR SWAA2022052702262Scuff Plate · crackedAFT CARGO DOOR AFT SCUFF PLATE IS CRACKED / [01] RECEIVED SERVICEABLE REPAIRED (WELDED) AFT CARGO DOOR SCUFF PLATE AFT CORNER. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00297N3;[02] VERIFIED STEP#1. RECEIVED SERVICEABLE REPAIRED (WELDED) AFT CARGO DOSDR SWAA2022052702261Scuff Plate · crackedAFT CARGO DOOR SCUFF PLATE FWD CORNER IS CRACKED / [01] RECEIVED SERVICEABLE REPAIRED (WELDED) AFT CARGO DOOR SCUFF PLATE FWD CORNER. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00297N3;[02] VERIFIED STEP #1. RECEIVED SERVICEABLE REPAIRED (WELDED) AFT SDR SWAA2022053102263Bulkhead · crackedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL 142MW CRACKED. / [01] INSPECTED AFT CARGO COMPT FWD BULKHEAD PANEL 142MW AND NO DAMAGE FOUND. IDENTIFIED DAMAGED PANEL 142NWB AND RECEIVED REPLACEMENT PART;[02] INSPECTED AFT CARGO COMPT FWD BULKHEAD PANEL 142MW AND NO SDR SWAA2022052605743Vapor Barrier · crackedLH VAPOR HAS TEMP REPAIR; NEED PERMANENANT REPAIR.CLEANED AND PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL CRACK AS PER B737 SRM 51-70-04-2R-10; PERFORMED DRY OUT ON DAMAGE AREA ; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[04] VERIFIED MEASUREMENTS; CLEAN ASDR SWAA2022053101970Angle · crackedATTACH ANGLE CRACKED AT CENTER TANK LOWER SKIN EXTERIOR STA. 663 LBL 5-21 / [01] FORMED REPLACEMENT ANGLE MAT. USED 2024T3 CLAD.063 &REPAIR ANGLE;MATERIAL USED 2024T3 .071 AS PER SRM. B737-7 51-30-01-0G-0 &SRM 57-10-10-2R -5 REPAIR 5;[02] VERIFIED STEP 1;[03] SDR SWAA2022053101971Attach Angle · crackedATTACH ANGLE CRACKED AT CENTER TANK LOWER SKIN EXTERIOR STA. 663 RBL 5-21 / [01] FORMED REPLACEMENT ANGLE MAT. USED 2024T3 CLAD .063AND REPAIR ANGLE; MAT. USED 2024T3 .071 AS PER. SRM 51-30-01-0G-0 &SRM57-10-10-2R REPAIR 5 ;RBL5-21; FORMED REPLACEMENT ANGLE MASDR SWAA2022053101665Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABALIZER LOWER SKIN STAB STA 193.90 ; 10' FROM REAR SPAR ; I/B FASTENER ROW. CRACK LENGTH = 1' CRACK FOUND AT RIGHT HORIONTAL STABALIER LOWER SKIN STAB STA 193.90 10' FROM REAR SPAR I/B FASTENER ROW. CRACK LENGTH = 1' . REMOVESDR SWAA2022052601666Panel · elongatedFILLET FAIRING 193B HAS SEVERAL ELONGATED FASTENER HOLES / [01] PERFORMED VISUAL INSPECTION AND TAP TEST AT FAIRING PANEL #193B FOUND SEVEN ELONGATED FASTENER HOLES AS PER B737 NTM 51-05-01;[02] VERIFIED STEP 1;[03] PREPARED DAMAGED AREA TO APPLY REPAIR AT PANSDR SWAA2022052601317Spacer · missingEXTERNAL POWER DOOR CUTOUT AFT SPACER MISSING A SECTION / [01] REMOVED THE INITIAL RUBBING BLOCK & THE LAMINATE SHIM AT AFT MIDDLE CUTOUT OF EGPR; AS PER B737-7 SRM 51-40-02.;[15] INSTALLED REPAIR AT EXTERNAL POWER CUTOUT AFT. AREA PER REF. B-737-7 SRM 53-10-1SDR SWAA2022040489208Light · inoperativeFLOOR LIGHT STRIP IN AFT AIRCRAFT NOT ILLUMINATING. / [01] REPLACED EMERGENCY EXIT LIGHT STRIP AFT R/H SIDE ADJACENT TO R/H GALLEY. REF AMM 33-51-15.SDR SWAA2022021069485Slide · out of adjustR1 DOOR SLIDE FELL OUT OF BUSSEL ; / [01] REMOVED AND REPLACED SLIDE PER 25-66-01 OF THE AMMSDR SWAA2021090713613Battery Pack · inoperativeAFT GALLEY INBOARD EMERGENCY FLASHLIGHT RED DOT NOT FLASHING ; / [01] REPLACED AFT GALLEY INBOARD EMERGENCY FLASHLIGHT BATTERY PER AMM REF 25-64-00SDR SWAA2021062184586Bulkhead Web · crackedAS SEEN FROM LEFT A/C BAY LOOKING AFT; CRACK IN VAPOR BARRIER AT BS 663; LBL 41. ; / MEASURED AT 15.5' IN LENGTH. PERFORMED INTERM REPAIR WITH STOP DRILL AND SPEED TAPE. OK TO CONITUNE REF SRM 57-10-10-1A-2.; MEASURED AT 15.5' IN LENGTH. PERFORMED INTERM REPAISDR SWAA2021061884589Circuit Breaker · trippedR/H AFT EMERGENCY LIGHT BATTERY CHARGER POPS C/B ; / REMOVED AND REPLACED R/H AFT EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY/ CHARGER PER AMM 33-51-06. OPS CK GOOD.; C/WSDR SWAA2021061885490Charger · failedR/H AFT EMERGENCY LIGHT BATTERY CHARGER POPS C/B ; / REMOVED AND REPLACED R/H AFT EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY/ CHARGER PER AMM 33-51-06. OPS CK GOOD.; C/WSDR SWAA2020112431710Psu · smokeF/A REPORTED HEAVY ELECTRICAL BURNING SMELL FROM ROW NR 2-4 CAPTS SIDE AT APPROXIMATELY FL 290. RAN QRH FIRE/SMOKE/FUMES CHECK LIST. F/A REPORTED ELECTRICAL SMELL DIMINISHING, DECLARED EMERGENCY. HAD FIRE DEPT SCANNED INSIDE WITH THERMAL SCANNER AND HAD SMESDR SWAA2020060889307Battery Pack · dischargedLT OVERWING EXIT EMERGENCY SIGN LIGHTS ARE INOP. R&R BATTERY PACK PER AMM 35-51-06.SDR SWAA2021072989269Threshold · bentFWD ENTRY DOOR THRESHOLD AFT CORNER IS BENT UP IN RADIUS (HIGHLY VISIBLE TO PASSENGERS) / READJUSTED FWD ENTRY DOOR THRESHOLD AFT CORNER KICK PLATE AND SECURED FLUSH WITH THRESHOLD PER AMM 25-21-31SDR SWAA2020060889261Attach Angle · crackedRIGHT HORIZ STAB FWD SPAR STIFFENER AT STA 120.3 CRACKED NEAR LOWER RADIUS. REMOVED FWD STIFFENER AND INSTALLED NEW RIB FWD STIFFENER ATTACH ANGLE IAW SRM 51-40-02. SEE WIPS AND SUB TASK FOR INDIVIDUAL WORK AND SIGN OFFS.SDR SWAA2021081289256Skin · delaminatedR/H I/B MAIN FLAP O/B WEDGE LOWER SKIN HAS DELAMINATION / REMOVED AND REPLACED R/H I/B MAIN FLAP O/B WEDGE PER SOPM 20-50-01.SDR SWAA2020060589249Stiffener · crackedLT HORIZ STAB INSPAR RIB 4 STIFFENER 1 CRACKED NEAR LOWER RADIUS. REPAIRED PER SRM 55-10-09-2R-4SDR SWAA2020060589250Stiffener · crackedLT HORIZ STAB INSPAR RIB 4 STIFFENER 4 CRACKED NEAR LOWER RADIUS. REPAIRED PER SRM 55-10-09-2R-4.SDR SWAA2020060889183Floor Panel · damagedPASSENGER CABIN FLOORBOARD 241AF HAS FIBER DAMAGE ON UPPER SURFACE. REPLACED FLOOR PANEL 241AF IAW AMM 53-21-00.SDR SWAA2020060889184Floorboard · damagedPASSENGER CABIN FLOORBOARD 241BF HAS NUMEROUS HEEL STRIKES ON UPPER SURFACE. INSTALLED REPLACEMENT FLOOR PANEL IAW AMM 53-21-00.
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