N941WN
Service difficulty reports · 219
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 = 'N941WN' 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 = 'N941WN' 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 SWAA2023061358611Battery Pack · inoperativeROW 1 AND 4 EMERGENCY LIGHTS INTERMITTENTLY INOP<[01] REPLACED EMERGENCY LIGHT; BATTERY PACK PER REF. AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED BATTERY PACK REPLACEMENT; OPS CHECK NORMAL.SDR SWAA2023061356215Light · inoperativePAX CABIN ROW 13 R/S EMERGENCY LIGHT ON OVERHEAD BIN IS INOP.<[01] REPLACED AREA LIGHT ROW 13 RH SIDE PER REF. AMM 33-51-03-960-801. TEST FOUND NORMAL.;[02] VERIFIED LIGHT REPLACEMENT.SDR SWAA2023061354591Barrier · crackedFOUND BRACKET AT R/H VAPOR BARRIER STA 663 RBL 25 LOWER AREA CRACKED.<[01] REMOVED AND REPLACED BRACKET (STIFFENER)AT R/H VAPOR BARRIER STA 663 RBL 25 LOWER AREA PER REF SRM 51-40-02-0G-0 AND DWG 111A1000;[02] VERIFIED REPLACEMENT OF BRACKET (STIFFENER) AT R/HSDR SWAA2023061351416Panel · corrodedCORROSION NOSE W/W L/H FWD ACCESS PANEL # 113AW MATING SURFACE MKD DOT<[01] VERIFIED WORK STEPS ACCOMPLISHED.SDR SWAA2023061350980Shield · crackedFWD E&E COMPT. HORIZONTAL STAB. TRIM DRIP SHIELD IS CRACKED.<[01] REMOVED FWD E&E COMPT. HORIZONTAL STAB. TRIM DRIP SHIELD REF B737-700 27-41-00-820-801;[02] VERIFIED STEP 1;[03] APPLIED REPAIR IN DAMAGED AREA AT TRIM DRIP SHIELD AS PER B737 AMM 25-00-00-340-8SDR SWAA2023061350666Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 17' FROM FRONT SPAR ; I/B ROW. CRACK LENGTH : 0.656' CRACK FOUND AT LEFT HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 17" FROM FRONT SPAR I/B ROW. CRACK LENGTH : 0.656"<[01] SDR SWAA2023061350651Panel · corrodedCORROSION AFT LOWER FUSELAGE LAV SERVICE ACCESS PANEL 145AL @ BONDING WIRE ATTACHING POINT AND EDGE MKD DOT<[01] REMOVED AND REPLACED LAV SERVICE ACCESS PANEL 145AL REF B737 SRM 51-40-02-0G-0;[02] VERIFIED LAV SERVICE ACCESS PANEL 145AL REPLACEMENT.;[03] CORRESDR SWAA2023061350650Panel · crackedL/W SPOILER PANEL NO- 6 LOWER SURFACE NEW DENT APPEARS CRACK BETWEEN DOUBLER REPAIRS @ CENTER SECTION MKD DOT<[01] PARTS TRANSACTION ACCOMPLISHED.;[02] REMOVED AND REPLACED L/W SPOILER PANEL #6 IN REFERENCE AMM 27-62-12-000-801 AND AMM 27-62-12-400-801.;[03] VSDR SWAA2023061350652Panel · corrodedCORROSION AFT LOWER FUSELAGE LAVATORY SERVICE ACCESS DOOR AFT HINGE MKD DOT<[01] CORROSION FOUND TO BE OUT OF LIMITS; PASSED THROUGH MATERIAL. REF B737 SRM 52-40-01-1A-4; REF TASK CARD TTG8Q00L6540 FOR HINGE REPLACEMENT;[02] VERIFIED CORROSION OUT OF LIMITS. PSDR SWAA2023061450649Bracket · crackedR/W T/E DEFLECTION CONTROL RIB O/B BRACKET CRACK.<[01] REMOVED AND REPLACED R/W T/E DEFLECTION CONTROL RIB O/B BRACKET PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1SDR SWAA2023061450640Cowling · corrodedLEFT INLET COWL LIP UPPER SURFACE EVIDENCE OF CORROSION AND DISCOLORED ALL AROUND<[01] REMOVED AND REPLACE #1 ENGINE INLET COWL IN REF AMM 71-11-01-000-802 AND 71-11-01-400-802;[02] VERIFIED #1 ENGINE INLET COWL REPLACEMENT.SDR SWAA2023061351534Barrier · crackedL/H MLG WHEEL WELL VAPOR BARRIER HAS A CRACK AT STA 663.75 LBL 34 AND WL150.<[01] APPLIED REPAIRED AT VAPOR BARRIER PER B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7)MATERIAL USED RESIN EY3804 PO#1800550 FIBERGLASS PO#1738579;[02] VERIFIED STEP 1SDR SWAA2023061351998Barrier · crackedR/H MLG WHEEL WELL VAPOR BARRIER HAS A CRACK AT STA 663.75 RBL 34 AND WL150.<[01] APPLIED REPAIRED AT VAPOR BARRIER PER B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7) MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1SDR SWAA2023040322828Girt Bar · brokenLOTO RESTRAINT BAR IS BROKEN<[01] REPLACED SLIDES AS PER SIPSDR SWAA2023032319199Light · inoperativeFWD ENTRY DOOR EXTERIOR EMER LIGHT INOP<[01] RELAMPED FWD ENTRY DOOR EXTERIOR EMER LIGHT REF AMM 33-51-04. NO FIX. REPLACED POWER SUPPLY FUSE REF AMM 33-51-06. OPS CHK GOOD.SDR SWAA2023032320222Fuse · inoperativeFWD ENTRY DOOR EXTERIOR EMER LIGHT INOP<[01] RELAMPED FWD ENTRY DOOR EXTERIOR EMER LIGHT REF AMM 33-51-04. NO FIX. REPLACED POWER SUPPLY FUSE REF AMM 33-51-06. OPS CHK GOOD.SDR SWAA2023012795920Lens · looseROW 17 BULLNOSE EMERGENCY LIGHT LENS LOOSE<[01] SECURED LENS IAW AMM 33-51-03SDR SWAA2023011791293Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INOP IN AFT CABIN<[01] R+R BATTERY PACK FOR AFFECTED EMERGENCY LIGHTS PER AMM 33-51-06. RELAMPED AFT SERVICE DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04; OPS CHECK GOOD.SDR SWAA2022040590093Flap · delaminatedLH OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED / [01] REMOVED AND REPLACED LH OUTBOARD AFT FLAP REF AMM 27-51-22-400-801. ALL CHECKS GOOD.;[02] INSPECTION C/W REMOVED AND REPLACED LH OUTBOARD AFT FLAP REF AMM 27-51-22-400-801. ALL CHECKS GOOD.;[03] INSPECTION SDR SWAA2022030177962Flashlight · lowUPPER FLASHLIGHT IN FWD L/H WINDSCREEN LOW BATTEERY / [01] REPLACED BATTERY IN FLASHLIGHT PER SIPSDR SWAA2022012864121Skin · delaminatedRIGHT WING I/B MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN IS DELAMINATED. THE DELAMINATED AREA MEASURES 20 1/4 INCHES LONG AND 8 INCHES WIDE. LOCATED AT THE TRAILING EDGE EXTENDING 8 INCHES ; FORWARD FROM THE TRAILING EDGE AND 18 12 INCHES OTOARD OF INOARDSDR SWAA2022011360660Panel · delaminatedWING TO BODY PANEL 193D HAS 7(EA) DISCREPANT FASTENER HOLES: SIX DELAMINATED AND ONE DELAMINATED AND ELONGATED (MARKED). ; / [01] INSTALLED NEW 193D PANEL IAW AMM 53-51-21. ORDERED PANEL UNDER REFERENCE TTG8Q001XKXNSDR SWAA2021120148487Light · inoperativeFWD ENTRY DOOR EMER EXIT LIGHT INOP ; FOND FWD L-1 DOOR EMERGENCY EXIT LIGHT SIGN NEAR FLOOR MONTED TO FWD LAV INOP AND DISCONNECTED / [01] RECONNECTED LIGHT ASSEMBLY IAW AMM 33-51-01 SEE TASK 725-41-01 FOR OTHER WORK PERFORMEDSDR SWAA2021102031223Circuit Breaker · poppedSUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHTS ILLUMINATED W/SWITCH IN ARMED POSITION. FOUND CB POPPED ; / [01] RESET EMERGENCY FWD CIRCUIT BREAKER PER AMM 20-60-01. OPS CK OK PER AMM 35-51-00.SDR SWAA2021081907429Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY EMERGENCY BATTERY PACK M1673 ARE INOP ; / [01] C/W IAW AMM 33-51-06-960-805 TEST GOOD<BR>ATAG BF3688; [02] VERIFIED ITEM 1<BR>FINAL AUDIT C/WSDR SWAA2021081903982Isolator · brokenPASSENGER CABIN RIGHT HAND SIDE STATION 578 3RD ISOLATOR FROM THE TOP IS BROKEN. ; STARTING AT THE PSU RAIL AND COUNTING DOWN . MARKED WITH A STREAMER. / [01] REPLACED RIGHT HAND SIDEWALL ISOLATOR AT STATION 578 3RD FROM THE TOP I/A/W SRM 51-40-02-01-0G; [02] SDR SWAA2021081903563Rib · crackedR/H HORIZ STAB L/E RIB AT STA 281.91 EVIDENCE OF CRACK IN RADIUS. REMOVED AND REPLACED RIGHT HAND HORIZONTLA STAB LEADINGEDGE RIB AT STA 281.91 IAW SRM 51-40-02 AND DRAWING 186A1001 P/N 186A1401-30 ATAG A52426. APPLIED CIC TO AREA IAW AMM 51-21-91.SDR SWAA2021081903564Rib · crackedL/H HORIZ STAB L/E RIB AT STA 272.62 FOUND CRACKED. ; / [01] STARTED REMOVING L/H HORIZ STAB LEADING EDGE RIB AT STA 272.62 IAW SRM 51-40-02; [02] REMOVED LH STAB LE RIB AT STA 272-62 IAW SRM 51-40-02-0G-0; [03] VERIFY NEW RIB AS P/N 186A1401-27 ATAG A70571 IASDR SWAA2021081999021Scuff Plate · crackedFORWARD CARGO DOOR FORWARD CORNER SCUFF PLATE CRACKED ; / [01] UPDATED MEASUREMENTS; [02] FWD CARGO DOOR; FWD CORNER SCUFF PLATE; REPAIRED ON WO 42430-1400-0002; [03] CW <BR>AUDIT CWSDR SWAA2021081997307Splice · corrodedAFT CARGO PIT; FLOOR SPLICE IS CORRODED AT STA 772.6. REMOVED AND REPLACED ON SHELF, AFT PIT FLOOR SPLICE. PN 136A901-4 IAW AIPC 53-42-11-30. ITEM 30. A-TAG # WN6565.SDR SWAA2021081997308Splice · corrodedAFT CARGO PIT; FLOOR BOARD SPLICE IS CORRODED AT STA 727D ; / [01] REMOVED FROM RACK; BAD AFT CARGO PIT FLOOR SPLICE FROM STATION 727D. REPLACED ON RACK; NEW SPLICE P/N 146A9401-8. IAW AIPC 53-42-11-30; ITEM # 5. A-TAG # A67475.; [02] C/W STEP 1<BR>AUDIT C/WSDR SWAA2021081996928Rub Strip · brokenHZ STAB CABLE STB RUBSTRIP IS BROKEN AT STA 1040. ; / [01] REMOVED AND REPLACED RUBSTRIP P/N 69-52800-6 TAG #A65728 IAW SRM 51-40-02 AND DWG251A4920 REV C; [02] VERIFIED ACTION 1 IS COMPLETE; [03] VERIFIED<BR>AUDIT C/WSDR SWAA2021081995616Seat Track · crackedSEAT TRACK WEB UPPER ATTACH ANGLE AT BS 520-500D LBL 24 IS CRACKED. ; / [01] VERIFIED ATTACH ANGLE TO SEAT TRACK TO BE 143A5410U9 A-TAG A58040 IAW DWG 143A5034; [02] VERIFIED STEP 1 SEAT TRACK ATTACH ANGLE C/W; [03] DRILLED UP NEW ATTACH ANGLE P/N 143A5410-9 ISDR SWAA2021081994580Angle · crackedWHILE REMOVING STA 663 R/H VAPOR BARRIER FOUND UPPER ANGLE COMMON TO VAPOR BARRIER WEB AND CENTER TANK LOWER REAR SPAR CRACKED AT RBL 7 ; / [01] RECIEVED -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP WORK ORDER 42430-0000-0001 SERIAL NO. 8199408 AND -2 SPLICE ASDR SWAA2021081993191Floorboard · damagedA22-88; CABIN FLOOR BOARD 231KF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED AND FOUND FLOOR BOARD 231KF TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 1(A)(NOTE) AND SAMPLE.<BR><BR>REPLACED BY FABRICATION SDR SWAA2021081993187Slide · out of positionAFT ENTRY DOOR SLIDE DRAGING ALONG SCUFF PLATE MAKING DOOR HARD TO CLOSE ; / [01] REMOVED AFT ENTRY DOOR LINER IAW AMM 52-13-31-000-802.<BR>REMOVED AFT ENTRY DOOR IAW AMM 52-13-00-000-802.; [02] REMOVED FUSELAGE TORQUE TUBE ACCESS PANEL IAW SRM 51-40-02-0G-0.<SDR SWAA2021081893192Floorboard · pulledA22-89; CABIN FLOOR BOARD 231UF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD.<BR><BR>CLEANED AND PRSDR SWAA2021081893193Floor Panel · pulledA22-92; CABIN FLOOR BOARD 241BF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED DAMAGE TO UPPER SURFACE; DAMAGE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B73SDR SWAA2021081893194Floorboard · pulledA22-93; CABIN FLOOR BOARD 242AF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED PANEL 242AF AND FOUND PULLED FIBER'S ON UPPER FACE SHEET. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP AREA'S. IAW B737-700 SSDR SWAA2021081893202Floorboard · pulledA22-90; CABIN FLOOR BOARD 232RF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED PANEL 232RF AND FOUND DAMAGED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A REV 73. CLEAN AND PREP AREA'S FOR REPAIR SDR SWAA2021081893203Floorboard · pulledA22-91; CABIN FLOOR BOARD 232SF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED PANEL 232SF AND FOUND DAMAGED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A REV 73. CLEAN AND PREP AREA'S. IAW B737-7SDR SWAA2021081893204Floorboard · pulledA22-94; CABIN FLOOR BOARD 242BF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-0SDR SWAA2021081893189Floorboard · pulledA22-86; CABIN FLOOR BOARD 231DF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED FLOOR BOARD AND FOUND MULTIPLE AREAS ACROSS ENTIRE UPPER SURFACE WITH DAMAGE. BOARD IS BER. FABRICATE NEW BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REV. 73 REPAISDR SWAA2021081893190Floorboard · pulledA22-87; CABIN FLOOR BOARD 231GF; UPPER SURFACE; AREAS OF PULLED FACE SHEET; MRK'D. ; / [01] EVALUATED FLOOR BOARD AND FOUND MULTIPLE AREAS ACROSS ENTIRE UPPER SURFACE WITH DAMAGE. BOARD IS BER. FABRICATE NEW BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REV. 73 REPAISDR SWAA2021081992458Splice Plate · crackedA22-81; CABIN FLOOR STRUCTURE; STA 540; LBL3; FLOOR SUPPORT SPLICE PLATE CRACKED ; / [01] REMOVED CRACKED SUPPORT SPLICE PLATE IAW SRM 51-40-02-0G-0 . VERIFIED NEW SUPPORT SPLICE PLATE AS P/N 143A5240-35 A-TAG WN3739 IAW BOEING DWG 143A0060 REV-; [02] CW STEP SDR SWAA2021081992459Splice Plate · crackedA22-80; CABIN FLOOR STRUCTURE STA 540; RBL3 & RBL25; FLOOR SUPPORT SPLICE PLATE CRACKED @ BOTH ENDS; MRK'D. ; / [01] REMOVED CRACKED SUPPORT SPLICE PLATA AT SET 540 RBL3 IAW SRM 51-40-02-0G-0. VERIFIED NEW SUPPORT SPLICE PLATE AS P/N 143A5240-36 A-TAG WN6712 ISDR SWAA2021081992456Seal · crackedA22-78; VERTICAL STAB STA 1018; LBL & RBL10'; JUST ABOVE FWD SPAR ATTACH LUGS; WEB STIFFNER CRACKED @ LEFT & RIGHT SIDES @ STRAIN RELIEF CUTOUTS; MRK'D. ; / [01] REMOVED EXPANSION JOINT ASSY. IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW SPRING SEAL AS P/N 176A3101SDR SWAA2021081991924Crease Beam · corrodedPASSENGER CABIN FLOOR;R1 CREASE BEAM ANGLE CORROSION AROUND SCUFF PLATE FASTNER HOLES ; / [01] REWORKED R1 CREASE BEAM ON FAULT TTG8Q005PK0X; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991432Angle · corrodedAFT CARGO COMPARTMENT; RH Z-ANGLE HAS CORROSION AT STA 767; RBL 21; WL 156; DOT#A-193-42 ; / [01] BEGAN REMOVING CORROSION FROM RH ZEE ANGLE BS 767 ORIGINAL T= .040' LOSS OF .015' REMAINING T= .025' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 TOOLING # 363SDR SWAA2021081991930Isolator · crackedR1 DOOR AFT SLIDE MOUNT ISOLATOR IS CRACKED ; / [01] REMOVED SLIDE MOUNT PLATE ASSY; REMOVED AND REPLACED SLIDE MOUNT ISOLATOR IAW SRM 51-40-02-0G-0.; [02] OK TO REINSTALL SLIDE MOUNT PLATE ASSY; [03] INSTALLED SLIDE PLATE ASSY IAW SRM 51-40-02-0G-0.; [04] REM
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