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 SWAA2022112973122Floor Panel · damagedDOT A24-10 MID CABIN FLOOR BOARD 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED DAMAGED AREAS IAW BSDR SWAA2022112973123Floor Panel · damagedDOT A24-11 MID CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED DAMAGED AREAS IAW BSDR SWAA2022112973125Floor Panel · damagedDOT A24-12 MID CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [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.<BR><BR>CLEANED AND PREPPED IAW SRM 5SDR SWAA2022112973303Attach Angle · crackedA-240 DOT 001 #2 ENGINE OUTBD FAN COWL ATTACH ANGLE AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED. / [01] REMOVED #2 ENG OUTBD FAN COWL ATTACH ANGLE IAW SRM 51-40-02;[02] VERIFIED ACTION 1;[03] OK TO INSTALL NEW #2 ENGINE OTBD FAN COWL ATTACH ANGLE;[04] INSTALLSDR SWAA2022112972974Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 LBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 5;[02] VERIFIED ITEM 2 OF STEP 8;[03] VERIFIED STEP 9;[04] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[05] NO LEAKS NOTED<BR>AUDIT C/WSDR SWAA2022112972975Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 RBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 8;[02] VERIFIED STEP 9;[03] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[04] LEAK CHECK GOOD<BR>AUDIT C/WSDR SWAA2022111671444Slide · looseSLIDE LOOSE ON R-2 DOOR. R-2 DOOR SLIDE CHECKED FOR SECURITY IAW MMMM 25-66-01. OK FOR SERVICE.SDR SWAA2022092716658None · crackedFOUND #2 SLAT UPPER SKIN CRACKED @ SLAT STATION 327 DURING BIRD STRIKE INSPECTION DENT IS L= 10.0 W= 2.5CRACK IS 2.25 / [01] REMOVED #2 LE SLAT IAW AMM 27-81-21. NEEDS INSTALL AND RIG CHECK.;[02] INSPECTED CAN HOUSING AND FOUND NO DEBRIS OR FOD. INSPECTED HARDSDR SWAA2022081741980Fairing · damagedLOWER PYLON FAIRING BELOW ACCESS PANEL 434BL SHOWS FRETTING WEAR FROM PYLON DRAIN TUBE / [01] REMOVED AND REPLACED LOWER PYLON FAIRING AT PYLON DRAIN TUBE PER SRM 51-40-02 AND SRM 51-40-05.SDR SWAA2022030779023Bracket · crackedLH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET IS CRACKED BEHIND #1 PYLON / [01] REMOVED AND REPLACED LH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET PER SRM 51-40-02 AND AMM 20-50-11SDR SWAA2022030379014Bracket · crackedLH MLG CENTER DOOR FWD LOWER ATTACH POINT BRACKET IS CRACKED /SDR SWAA2022030379020Web · crackedRH MLG CENTER DOOR FWD LOWER MOUNTING ATTACH WEB HAS A 1.0' CRACK /SDR SWAA2021120649281None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80SDR SWAA2021120650021None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80SDR SWAA2021120650020None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80SDR SWAA2021060477927Rib · crackedRH HORIZONTAL LE PANEL 331B; 3RD RIB LE STA 95.96 FROM INBD EDGE; HAS A CRACK AT UPPER MOST AFT FASTENER ; PANEL 341B NOT 331B / APPLIED CIC TO RIB IAW AMM 51-21-91; REMOVED AND REPLACED RH STAB LE RIB CHORD AT LE STA 95.96 IAW DWG 186A1303 REV 1; SRM 51-40-02SDR SWAA2021060477926Lamp · inoperativeR/H OVERWING EXIT EMERGENCY EXIT LOCATOR LIGHT L1358 IS INOP ; / REPLACED LAMPS IN R/H OVERWING EXIT EMERGENCY EXIT LOCATOR LIGHT L1358; OPS CHECK GOOD IAW AMM 33-51-01-960-801.<BR>ATAG A69819; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021060476890Battery Pack · inoperativeLEFT OVERWING ESCAPE LIGHT (L6) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1668 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. LEFT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021060479805Charger · inoperativeLEFT OVERWING ESCAPE LIGHT (L6) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1668 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. LEFT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021060476887Battery Pack · inoperativeLEFT OVERWING ESCAPE LIGHT (L7) INOP ; RIGHT OVERWING ESCAPE LIGHT (L7) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1669 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. RIGHT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; REPLACED BATTERY PACK AND SDR SWAA2021060479806Charger · inoperativeLEFT OVERWING ESCAPE LIGHT (L7) INOP ; RIGHT OVERWING ESCAPE LIGHT (L7) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1669 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. RIGHT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; REPLACED BATTERY PACK AND SDR SWAA2021060476458Rib · crackedLH HORZ STAB RIB 120.30; CRACKED O/B LOWER FLANGE AT FWD END IN RADIUS ; / APPLIED CIC TO REPAIR AREA & OEM RIB IAW AMM 51-21-91; REMOVED DAMAGE ON L/H HORIZ STAB RIB 120.3 FWD LOWER O/B END IAW B737 SRM 55-10-09-2R-5. ACCOMPLISHED REPAIR PER EA 21-155-01399-WSDR SWAA2021060477924Rib · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / COMPLETED EA 21-155-01399 FINAL; FINAL AUDIT C/WSDR SWAA2021060473219Skin · debondedRIGHT WING INBOARD MAIN FLAP TRAILING EDGE SKIN DISBONDED AT OUTBOARD END / REPAIRED AREA OF DELAMINATION ON I/B R/W MAIN FLAP LOWER SKIN. IAW B737-700 SRM 57-53-01-2R-7;SRM 51-70-10-2R-4; SRM 51-70-10-2R-0; AMM 51-21-99-300-801.; STEP 12 OK; SUMMARY STATEMENTSDR SWAA2021060475326Skin · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / ACCOMPLISHED EA 21-155-01399-WIP1; VERIFIED EA 21-155-01399-WIP1 ALL STEPS COMPLETE; FINAL AUDIT C/WSDR SWAA2021060473220Rib · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / REMOVED DAMAGED AREA FROM LH HORIZ STAB RIB AT STA 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE PER B737 SRM 51-10-02-0G-0. REPAIRED SDR SWAA2021060477923Skin · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / AUDIT C/WSDR SWAA2021060472685Stub Frame · crackedR1 DOOR CUTOUT STA 291+9; FWD UPPER STUB FRAME ABOVE UPPER HINGE HAS CRACK IN FASTENER HOLE COMMON TO UPPER HOLE IN SEAL DEPRESSOR. MARKED ; / REMOVED AND REPLACED R1 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV C DOOR UPPER STUB FRAME; VERIFIED STEP 9; ASDR SWAA2021060473158Rib · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / REMOVED DAMAGE; FABRICATED REPAIR PARTS AND INSTALLED REPAIR TO RH HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE IAW EA 21-155-01361; VERIFIED ITEM 29 AND 30; AUDIT C/WSDR SWAA2021060474863Skin · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / VERIFIED TRIMMED DAMAGED AREA I.A.W EA21-155-01361 STEP1 COMPLETE; EA C/W; AUDIT C/WSDR SWAA2021060473159Floor Support · crackedSTA 927-947 RBL 25 INTERCOSTAL FOUND CRACKED ; / REMOVED AND REPLACED INTERCOSTAL BS 927-947 RBL 20 IAW DWG 147A7500 REV C; SRM 51-40-02-0G-0. RESTORED CIC IAW AMM 51-21-91-620-802; ALL WORK C/W; AUDIT C/WSDR SWAA2021060472687Angle · crackedFWD CARGO COMPT STA 500B - 500C LBL25 BAFFLE IS BENT AND AFT ANGLE IS CRACKED. DOT A-21-071 ; / VERIFIED ITEM 4.<BR>OK TO INSTALL.; INSTALLED BAFFLE STA 500B-C FWD PIT IAW SRM 51-40-02 & BOEING DWG 143A7510 REV B; INSPECTION CW CORROSION PROTECTION CW REF SWA SDR SWAA2021060472686Strap · corrodedAFT CARGO COMP. AFT BULKHEAD LOWER BULKHEAD STRAP CORRODED STA.947 APPROX STR 21R TO STR 25R WL 158 ; / FOUND MATERIAL LSS TO BE 100%; REMOVED AND REPLACED AFT CARGO AFT BULKHEAD RH SUPPORT RAIL BS 947 IAW SRM 51-40-02-0G-0; DWG 149A8117 REV -; RESTORED CIC IASDR SWAA2021051772683Stiffener · crackedRIGHT HORIZONTAL STABILIZER; RIB STA 92.7; RIB STIFFENER #1 CRACKED ABOVE LOWER FLANGE. CUT OUT DAMAGE AREA ON #1 STIFFENER STA.92.70 HORIZONTAL STAB RIB IAW SRM 55-10-09-2R-4 REPAIR4 VERIFIED MATERIAL ID FOR REPAIR PARTS 55100003-01 TAG #WN 4752 IAW DWG 5510SDR SWAA2021051772682Rib · crackedDOT-125-01 RIGHT HORIZONTAL STABILIZER RIB STA 129.5; FWD LOWER FLANGE CRACKED.SDR SWAA2021060477922Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / VERIFIED STEPS ALL STEPS COMPLETE. IAW EA 21-155-01364-P1 AND FINAL<BR>FINAL AUDIT C/WSDR SWAA2021060472106Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / ADDING P1 AND FINAL TO ITEM 12. EA 21-155-01364-WIP 1 REV P1 AND FINAL COMPLETE; VERIFIED COMPLETION OF EA 21-155-01364-WIP1 REV P1 AND FINAL; VERIFIED STEPS 12;SDR SWAA2021060474864Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / SUMMARY EA 21-155-01364 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK OF THE FAULT.<BR><BR>NOTE: THE TYPICAL WORK STEP ENG SIGN OFF WAS OMITTED FROM THE WSDR SWAA2021060470136Door · gougedAPU COWL DOOR; 38' AFT OF FWD EDGE; RIGHT SIDE FRAME; DEEP GOUGE. ; / N/A'D REQUIRED STEPS; VERIFIED ITEMS 9 AND 10<BR>AUDIT C/W; VERIFIED ITEMS 9 AND 10<BR>AUDIT C/WSDR SWAA2021052470141Angle · corrodedCORROSION ON LOWER SURFACE OF Z ANGLE WL 156 RBL 20 STA 727C TO 767 AROUND NUT PLATES ; / VERIFIED LIMITE ON R/H Z-ANGLE; STA 727C TO STA 767. ORIG 'T' .040. REM 'T' .031; LOSS .009. FOUND TO BE OUT OF LIMITS IAW. SRM 51-10-02-0G-0; VERIFIED MATERIAL LOSS IS OSDR SWAA2021081370121Strap · corrodedDOT# A45-014; AFT CARGO PIT DOOR CUTOUT; INTERCOSTAL LOWER ATTACH STRAP HAS CORROSION; WL: 156; RBL: 19; STA: 787+12. ; / [01] REMOVED STRAP FROM STATION 787+12 TO REMOVE CORROSION IAW B737 SRM 51-40-02; [02] REMOVED CORROSION ON STRAP AT STATION 787+12 ORIGINSDR SWAA2021081370126Attach Angle · corrodedDOT# A45-027; AFT CARGO PIT; RH INTERCOSTAL UNDER Z-ANGLE HAS CORROSION; WL:156; RBL:22; STA: 747-767. ; / [01] REMOVED CORROSION ON R/H INTERCOSTAL AT STATION 747-767 ORIGINAL THICKNESS .032 REMOVED .007 REMAINING .025 INTERCOSTAL WAS FOUND TO BE OUT OF LIMITSDR SWAA2021060470128Splice Plate · crackedDOT-42-A22; CABIN STA 538; RBL1; FLOOR BBOARD SPLICE PLATE CRACKED @ INBD/AFT CORNER. ; / AUDIT CW; AUDIT CW; FOUND COMPLETESDR SWAA2021060470125Attach Angle · corrodedAFT CARGO PIT; RH ATTACH ANGLE ON LOWER SURFACE OF FLOOR SHIELD HAS CORROSION; WL:156; RBL:22; STA: 767+4. ; / REMOVED CORROSION ON ATTACH ANGLE AT STATION 767+4 ORIGINAL THICKNESS .050 VERIFIED BY TOOL 36649 DUE 8-4-21MATERIAL REMOVED .012 REMAINING .038 ANGLSDR SWAA2021060470124Cargo Track · corrodedDOT# A45-021; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 2.5; STA: 767+6. ; / REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-53-2R-2 APPLIED CIC TO AREA IAW AMM 51-21-91-620-802; SDR SWAA2021060470122Attach Angle · crackedDOT# A45-015; AFT CARGO PIT; RH Z-ANGLE; LOWER SIDE ATTACH CLIP IS CRACKED IN RADIUS; WL: 155; RBL: 21; STA: 727+5. ; / CLIP REMOVAL & INSTALLATION ACCOMPLISHED ON FAULT TTG8Q004YWGX; FABRICATED NEW CLIP P/N 146A7505-4; ON SHOP W/O 42136-1600-0004. LOCATED ANDSDR SWAA2021060470117Cargo Track · corrodedDOT# A45-019; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 13; STA: 767+6. ; / REMOVED AND REPLACED TRACK SECTION RBL 13.8 BS 747+10-887 IN FAULT TTG8Q004YWLS; C/W; AUDIT C/WSDR SWAA2021060470116Cargo Track · corrodedDOT# A45-018; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; LBL: 2.5; STA: 767+6. ; / REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-53-2R-2 APPLIED CIC TO AREA IAW AMM 51-21-91-620-802; SDR SWAA2021060470114Support Angle · corroded185-019 AFT CARGO COMP.AFT BULKHEAD BOTTOM ANGLE CORRODED AROUND FASTNER HOLES STA.947 LBL 16-RBL 16 WL 158 ; / REMOVED CORROSION FROM AFT BULKHEAD LOWER SUPPORT RAIL. ORIGINAL T.080' REMAINING .062' LOSS OF .018' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 VISDR SWAA2021060470112Shield · corroded185-015 AFT CARGO;RH FLOOR SHIELD CORRODED AROUND FASTNER HOLES STA 847-867 RBL 16 WL 158 ; / INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV A; VERIFIED INSTALLATION ON STEP 8; VERIFIED ITEMS 8 & 9.<BR>AUDIT COMPLETE.
Back to N220WN