N220WN
Service difficulty reports · 358
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 = 'N220WN' 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 = 'N220WN' 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 SWAA2021060470111Angle · corrodedDOT# A45-010; AFT CARGO PIT; RH Z-ANGLE HAS CORROSION; WL: 154; RBL: 20; STA: 727 TO 727C+10. ; / REMOVED CORROSION IAW RH STA 727-727C VERIFIED WITTH 10X MAGNIFY GLASS IAW SRM 53-00-53-1A-2. VERIFIED MATERIAL LOSS ORIGINAL THICKNESS .040' LOSS .008'; REMAININSDR SWAA2021060470107Splice Plate · corroded185-016 AFT CARGO;FLOOR PANEL SPLICE PLATE CORRODED AROUND FASTNER HOLES STA 887 LBL 16-RBL 16 WL 158 ; / REMOVED CORR0SION FROM AFT CARGO FLOOR SUPPORT PANEL SPLICE AT STA 887 LBL 16 RBL 16 VERIFIED OUT OF LIMITS DUE TO NO PUBLISHED LIMITS VERIFIED NEW PART PSDR SWAA2021060469795Stiffener · crackedRIGHT HORIZONTAL STAB RIB STA 92.70; RIB STIFFENER #3 IS CRACKED 1' ABOVE LOWER FLANGE. CRACK VERIFIED BY HFEC. DOT 177A-001 ; / CUT OUT DAMAGED AREA ON R/H HORZ STAB RIB ON #3STIFFENER I.A.W SRM55-10-09-2R-4.<BR>FABRICATED AND DRILLED REPAIR KIT I.A.W SRM55-1SDR SWAA2021052470119Cargo Track · corrodedDOT# A45-020; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 8; STA: 767+6. ; / REMOVED CORROSION FROM FLOOR SUPPORT RAIL AT STA 767+6' RBL 8 MEASURED MATERIAL LOSS USING TOOL #1714 CAL DUE 10/6/21 ORIGINAL MATERIAL THICKNESS .071 LOSS OF .031 SDR SWAA2021052470113Cargo Track · corrodedDOT# A45-013; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 14; STA: 767 TO 807. ; / REMOVED CORROSION IAW B737 SRM 51-10-02-0G-0. ORIGINAL T .071' REMAINING .058'; LOSS OF .013. OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2 FIG 103 VIEW A-A. AAR TSDR SWAA2021052470110Angle · corrodedDOT# A45-009; AFT CARGO PIT; RH Z-ANGLE HAS CORROSION; WL: 156; RBL: 20; STA: 727C+10 TO 767. ; / VERIFIED NEW Z-ANGLE MATERIAL AS PN BAC1496-377-7075 T6. A TAG A73414; IAW BOEING 737 SRM 53-60-53-01-2 FIGURE 2.; VERIFIED NEW PART EFFECTIVITY.; CONTINUED TO LOSDR SWAA2021052470108Angle · corrodedDOT# A45-012; AFT CARGO PIT; LH Z-ANGLE HAS CORROSION; WL: 156; LBL: 21; STA: 727C+10 TO 807+10. ; / VERIFIED NEW PART EFFECTIVITY.; CONTINUED LOCATING AND DRILLING NEW Z-ANGLE IAW SRM 53-00-53-2R-5.; VERIFIED IN PROCESS STEPSDR SWAA2021052470106Angle · corrodedDOT# A45-011; AFT CARGO PIT; LH Z-ANGLE HAS CORROSION; WL: 154; LBL: 20; STA: 727 TO 727C+10. REMOVE Z-ANGLE LH BS 727-727C + 10' IAW SRM 51-40-02-0G-0.; VERIFIED MATERIAL FOR Z-ANGLE AS PN BAC1496-377 7075 T6; 'A' TAG A81056 IAW SRM 53-60-53-01-2 FIG 2.; VESDR SWAA2021052470105Floor Support · corrodedDOT# A45-008; AFT CARGO PIT DOOR CUTOUT; RH INTERCOSTAL HAS CORROSION ON UPPER AND LOWER SURFACE; WL: 156; RBL: 19; 767 TO 767+8. ; / REMOVED CORROSION ON R/H INTERCOSTAL AT STATION 767 ORIGINAL THICKNESS .056 REMOVED .016 REMAINING .040 INTERCOSTAL WAS FOUND SDR SWAA2021052470104Shield · corrodedAFT CARGO PIT; RH FLOOR SHIELD HAS CORROSION; WL:156; RBL:22; STA: 767-787. REMOVED CORROSION ON AFT CARGO FORWARD FLOOR SHIELD ORIGINAL THICKNESS .050 REMAINING .030 REMOVED .020 SHIELD WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60--15-1A-1 TOOL 36649 DUE 8-4SDR SWAA2021052470102Web · corrodedDOT# A45-006; AFT CARGO PIT; DOOR CUTOUT THRESHOLD WEB; UPPER SURFACE HAS CORROSION. WL: 156; RBL: 26; STA: 787+11 TO 827+10. ; / REMOVED CORROSION IAW SRM 51-10-02-0G-0; ORIGINAL T .045' REMAINING .036' LOSS OF .009'. OUT OF LIMITS IAW B737 SRM 53-60-15-1A-1 SDR SWAA2021060469392Rib · crackedDOT 18_A22: LEFT HORIZONTAL STAB RIB STA 120.30; LOWER FLANGE CRACKED JUST FWD OF #4 STIFFENER ; / REMOVED AND REINSTALLED LEFT HORIZONTAL STAB RIB STA 120.30 IAW SRM 51-40-02-0G-0; DWG 002A0001. REPAIRED IAW EA 21-155-01399; VERIFIED STEP 30 RII; AUDIT COMPLESDR SWAA2021060469791Bracket · crackedVERTICAL STAB PANEL 324AL LOWER BRACKET IS CRACKED DOT A-21-13 ; / INSTALLED NEW RETAINER ON PANEL 324AL IAW B737 SRM 51-40-02-0G-0; DWG 172A6123 REV A; REMOVED AND REPLACED RETAINER ON PANEL 324AL IAW SRM 51-40-02-0G-0; DWG 172A6123 REV A; COMPLETED INSPECTIOSDR SWAA2021060469785Web · corrodedDOT# 31 A-186 FWD PIT SILL WEB CORRODED STA 440-480 RBL 28 WL156 ; / AUDIT CW; VERIFIED STEP C/W; VERIFIED ITEM #5<BR>AUDIT CWSDR SWAA2021060469784Floor Panel · corrodedDOT#30 A-186 FWD PIT FLOOR CORRODED STA 420+16 LBL18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WSDR SWAA2021060469783Shield · corrodedDOT#26 A-186 FWD PIT FWD SHILD CORRODED STA 420-440 RBL24 WL156 ; / VERIFIED STEPS 2; 3; 10; 11 AND 21 COMPLETE; REMOVED CORROSION LOSS OF .010 IS OUT OF LIMITS DUE TO NO DOCUMENTED LIMITS REMOVED AND REPLACED SHIELD IAW SRM 51-40-02 AND DWG 143A0080; VERIFIEDSDR SWAA2021060469782Cargo Track · corrodedDOT#25 A-186 FWD PIT FLOOR RAIL CORRODED STA 40[+2 LBL 18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WSDR SWAA2021060469778Seat Track · corrodedDOT 23-A22; CABIN SEAT TRACK STA 463-466; LBL25; WL208; LIGHT CORROSION IN BASE OF SEAT TRACK ; / CORRECTIVE ACTION SHOULD READ: FAULT RAISED IN ERROR DUPLICATE WRITE UP TO TTG8Q004YCAQ; VERIFIED CORRECTIVE ACTION SHOULD READ: FAULT RAISED IN ERROR DUPLICATE WSDR SWAA2021060469777Seat Track · corrodedDOT 22-A22; CABIN SEAT TRACK STA 400-404; LBL22.5; WL208; LIGHT CORROSION IN BASE OF SEAT TRACK ; / UPDATED MEASUREMENTS; CERTIFIED STEP C/W; VERIFIED <BR>AUDIT C/WSDR SWAA2021060469772Cargo Track · corrodedDOT#32 A-186 FWD PIT FLOOR RAIL CORRODED STA 480+16 LBL 18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021060469770Cargo Track · corrodedDOT# 27 A-186 FWD PIT FLOOR RAIL CORRODED STA 400+ 18 RBL 14 WL156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WSDR SWAA2021060469764Stiffener · crackedDOT 21-A-22; RIGHT HORIZONTAL STAB RIB STA 129.50; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED AREA I.A.W MM51-21-91-620-802; REMOVED RIB TO REPAIR CRICKET # 3 STIFFENER AT R /H HORZ STAB STA129.5 I.A.W ARM 51-40-02-0G-0<BR>REMOVED DAMAGED AREA SDR SWAA2021060469763Stiffener · crackedDOT 20-A-22; RIGHT HORIZONTAL STAB RIB STA 92.70; RIB STIFFENER #2 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED RIBI.A.W MM51-21-91-620-802; REINED RIB AT R/H HORZ STAB STA92.70 TO REPAIR #2 RIB STIFFENER I.A.W SRM51-40-02-0G-0.<BR>REMOVED DAMGE AT #2 RIB STIFFENSDR SWAA2021060469393Stiffener · crackedDOT 19_A22: LEFT HORIZONTAL STAB; RIB STA 120.30; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE. ; / REMOVED DAMAGE FROM L/H HORIZ STAB RIB STA 120.3; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE IAW B737 SRM 55-10-09-2R-4. REPAIRED PER 55-10-09-2R-4 CIC APSDR SWAA2021060469389Seat Track · corrodedDOT0 21-A061 SEAT TRACK BASE HAS CORROSION FROM STA 727E+18' TO STA 747+1' RBL 45 WL ; / UPDATE MEASUREMENTS; I.A.W SRM 53-00-52-1A-1<BR>UPDATED STEP 7; VERIFIED STEPS 7; 8; AND 9<BR>AUDIT C/WSDR SWAA2021060469781Door Frame · crackedR1 DOOR SURROUND;FWD TOP CORNER INSIDE THE FRAME BEHIND THE T/T LATCH RECEIVER EVIDENCE OF A CRACK AT FASTNER (MARKED) ; / TASK COMPLETE; FINAL AUDIT C/W; FINAL AUDIT C/WSDR SWAA2021051473157Panel · damagedDOT#48 A-186 FWD PIT PNL 120CF DAMAGE AT FASTENER HOLES ; / FOUND FWD CARGO PANEL 120 CF TO BE OUT OF LIMTS IAW SRM 53-00-53-1A-1 STEP 5 B 1; VERIFIED ITEM 1SDR SWAA2021060469371Skin · damagedSKIN DAMAGE AT STA 1008 1.5' ABOVE STR 15L ; / N/A MEASUREMENT TABLE DUE TO NO DENT IN AREA; VERIFIED DENT TABLE MEASUREMENTS ARE N/A'D DUE TO DENT BEING PREVIOUSLY REPAIRED; VERIFIED AND AUDITED.SDR SWAA2021060469370Floor Panel · damagedCABIN FLOOR PANEL 241CF EDGE HAS DAMAGE. DOT A-21-09 ; / VERIFIED STEPS 1;2;3 TAP TESTED GOOD; REPAIRED EDGE DAMAGE ON CABIN FLOOR PANEL 241CF I/A/W SRM 53-00-50-2R-10 TAP TEST GOOD; VERIFIED ITEM 5. TAP TEST GOOD<BR>AUDIT C/WSDR SWAA2021060469369Floor Panel · damagedCABIN FLOOR PANEL 231ZF EDGE HAS DAMAGE. DOT A-21-08 ; / RII STEPS; BONDED REPAIR AT EDGE DAMAGE ON FLOORBOARD PANEL 231ZF I/A/W SRM 53-00-50-2R-1 3A-N &REV 73); RII C/W FINAL INSPECTION; AUDIT C/WSDR SWAA2021060469368Floor Panel · damagedCABIN FLOOR PANEL 231WF EDGE HAS DAMAGE. DOT A-21-07 ; / APPLIED POTTING COMPOUND TO INBOARD FWD AND AFT CORNERS CORE ONLY. CURED FOR 5 HOURS AT 125 DEGREES WITH HEAT LAMP I/A/W 53-00-50-2R-10 (3) A-G REV73; REPAIRED INBOARD FWD AND AFT EDGE DAMAGE ON CABIN FLSDR SWAA2021060469367Floor Panel · damagedCABIN FLOOR PANEL 241FF HAS EDGE DAMAGE. DOT A-21-11 ; / REPAIRED EDGE DAMAGE ON FLOOR PANEL 241FF WITH POTTING COMPOUND I/A/W SRM 53-00-50-2R-10 STEP 3A-G (REV 73); VERIFIED STEPS 1-4; AUDIT CWSDR SWAA2021060469366Floor Panel · peelingCABIN FLOOR PANEL 241CF HAS PEELED FIBERS. DOT A-21-10 ; / REPAIRED PEELED FIBERS ON CABIN FLOOR PANEL 241CF I/A/W SRM 53-00-50-50-2R-1 (3) A-M (REV73) TAP TEST GOOD; VERIFIED ITEMS 1;2;3;4; AND 7<BR>AUDIT C/W; CLOSING INDEPENDENT INSPECTION THAT WAS SELECTED SDR SWAA2021060469386Floor Panel · pulledDOT 005-A061 CABIN FLOOR BOARD 232SF UPPER SURFACE PULLED FIBERS ; / REPAIRED CABIN FLOOR BOARD 232SF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1; OK; STEP 4 & 5 OK AUDIT COMPLETESDR SWAA2021060469385Floorboard · damagedDOT 001-A061 CABIN FLOOR BOARD 232SF AFT INBD CORNER DAMAGED ; / EVALUATED AND FOUND DAMAGE TO CORE AT AFT I/B CORNER AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-10 REV 73.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-10 STEP 3 A-D. <BR><BR>APPLIEDSDR SWAA2021060469384Floorboard · damagedDOT 003 A061 CABIN FLOOR BOARD 241EF HAS DAMAGE TO THE LEADING EDGE ; / BONDED REPAIR ON LEADING EDGE AREA ON FLOORBOARD PANEL 241EF I/A/W SRM 53-00-50-2R-1 STEP 3A-N (REV 73); REPAIRED LEADING EDGE DAMAGE ON FLOORBOARD 241EF I/A/W SRM 53-00-50-2R-1 STEP 3A-N SDR SWAA2021060469383Floorboard · pulledDOT 006-A061 CABIN FLOOR BOARD 242AF UPPER SURFACE PULLED FIBERS ; / BONDED REPAIR PLIES; CURED 3 HOURS AT 150 DEGREES IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3J;K;L;M AND SRM 53-00-50-2R-0 REPAIR GENERAL REV. 73. TOOLING--OVEN B0-06 DUE 5-26-21. TAP TEST GOOD.; RSDR SWAA2021060469382Floorboard · damagedDOT002-A061 CABIN FLOOR BOARD 242AF AFT INBD CORNER DAMAGED ; / INSTALLED INSERTS IAW BOEING DRAWING 144A5810-189 REV. A AND BAC5085 STEP 8.4.2.2 CURED 1 HOUR AT 150 DEGREES. TOOLING--AAR 30347 DUE 4-29-22; REPAIRED DAMAGE TO AFT EDGE OF FLOORBOARD 242AF IAW SSDR SWAA2021060469381Floorboard · pulledDOT 008-A061 CABIN FLOOR BOARD 242DF UPPER SURFACE PULLED FIBERS ; / REPAIRED CABIN FLOOR BOARD 242DF UPPER SURFACE PULLED FIBERS IAW SRM 53-00-50-2R-1 AND 53-00-50-2R-0 REPAIR GENERAL.; OK; VERIFIED STEP 3 AND 4 COMPLETE AND AUDIT COMPLETESDR SWAA2021060469380Floorboard · pulledDOT 009_A061 CABIN FLOOR BOARD 241AF UPPER SURFACE HAS PULLED FIBERS ; / REPAIRED DAMAGE TO UPPER SURFACE OF PANEL 241AF. IAW B 737-700SRM 53-00-50-2R-1;SRM 53-00-50-2R-0; OK; STEP 4 & 5 OK. AUDIT COMPLETESDR SWAA2021060469374Seat Track · corrodedDOT 020-A061 SEAT TRACK BASE HAS CORROSION FROM STA 727C+16' TO STA 727D+10 RBL 45 WL 208 ; / UPDATE MEASUREMENTS; VERIFIED STEP 7 AND 8 COMPLETE AND AUDIT COMPLETE; OKSDR SWAA2021060468449Bulkhead Web · crackedAFT CARGO; FWD BULKHEAD PNL 141LW CRACKED; DOT A-193-11 / VERIFIED PART AS 453A2510-20; SI#7254212; ITEM# 45; IAW AIPC 25-52-19-01A. PANEL TO BE INSTALLED ON W/O 42133-1000-0233.; A TAG # FOR PART IS WN1222; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021052469360Floor Panel · corrodedAFT PIT PANEL 140CF HAS CORROSION AROUND FASTENER HOLES LEFT AND RIGHT SIDES A172-0003 ; / VERIFIED STARTING FABRICATION OF PANEL; STARTED FABING FLOOR PANEL. 140CF IAW AMM 25-52-01-201-801; EVALUATED CORROSION ON AFT CARGO FLOOR PANEL 140CF FLOOR PANEL WAS FOSDR SWAA2020060387851Battery Pack · dischargedEMERGENCY LIGHTS IN FWD GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FWD GALLEY OVERHEAD LT SIDE IAW AMM 33-51-06.SDR SWAA2020051175668Seat Track · wornF/OS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11SDR SWAA2020051175667Seat Track · wornCAPTS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11SDR SWAA2020051175656Glowstrip · wornPASSENGER CABIN FWD GALLEY TO ROW 2DEF PHOTO ILLUMINES STRIPS WORN AND HAVE MOISTURE UNDER COVER BOTH SIDES / R&R PHOTO ILLUMINES STRIPS PER AMM 25-27-31SDR SWAA2021081706096Skin · cracked193B PANEL HAS SEVERAL DAMAGE ON OUTER SURFACE- SKIN (DENTS;CRACKS & HOLES) / REPLACED 193B PANEL PER AMM 53-51-21SDR SWAA2019121639602Cover · detachedR/H OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. / INSTALLED COVER PER AMM.SDR SWAA2019110138447Light · inoperativeR/H OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
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