N227WN
Service difficulty reports · 286
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 = 'N227WN' 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 = 'N227WN' 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 SWAA2023020294337Floor Panel · damagedA-204 DOT #27. FLOOR PANEL 241AF; FWD LH CORNER HAS MISSING FACE SHEET.<[01] EVALUATED AND FOUND PLY MISSING AT FWD L/H CORNER. NO DAMAGE TO CORE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BRSDR SWAA2023020294329Floor Panel · damagedA-204 DOT #29. FLOOR PANEL 241BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 241BF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 241BF FOR WET LAY-UP IAW B737-700SDR SWAA2023020294338Floor Panel · damagedA-204 DOT #30. FLOOR PANEL 241BF; UPPER FACE SHEET PREVIOUS REPAIR HAS LAYERS OF FIBERS TORN OFF.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 241BF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 241BF SDR SWAA2023020294330Floor Panel · damagedA-204 DOT #31. FLOOR PANEL 231YF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 231YF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 231YF FOR WET LAY-UP IAW B737-700SDR SWAA2022092283359None · looseEXIT/SALIDA SIGN NEAR FO SIDE OVERWING EXIT DOOR IS LOOSE AND WILL NOT REMAIN ATTACHED TO SIDEWALL. / [01] INSTALLED NEW EXIT COVER AT FO SIDE AFT OF OVERWING EXIT DOOR PER A.M.M. 33-51-01SDR SWAA2022090650088None · out of positionFLIGHT ATTENDANT REPORTED FWD SERVICE DOOR SLIDE GIRT BAR NEEDS ADJUSTMENT. HARD TO OPERATE / [01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT BAR PER AMM 25-66-01. A/C OK FOR SERVICE.SDR SWAA2022080237085Slide · looseL2 DOOR SLIDE APPEARS LOOSE / [01] SECURED SLIDE IN CONTAINER PER M/M 25-66-01SDR SWAA2022053111387Light · inoperativeBOTH L/H AND R/H EMERGENCY EXIT WINDOW LIGHTS INOP / [01] RELAMPED BOTH L/H AND R/H EMERGENCY EXIT WINDOW LIGHTS PER AMM 33-21-00SDR SWAA2021121350742Battery · failedSUPPLEMENTAL INFORMATION: EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATION M1669 AND M1675 ; / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATION M1669 AND M1675 PER AMM 33-51-06; [02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LSDR SWAA2021101924464None · crackedCRACKED REAR SPAR LT FWD DRAG BRACE FITTING INBOARD POSITION AT VERTICAL STABILIZER. REMOVED REAR SPAR DRAG BRACE FITTING IAW SRM 51-40-02, DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM AND MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGSDR SWAA2021101922861Floor Panel · missingSUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241BF AT PASSENGER CABIN ; 2021-437381 / ER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.N; TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 11/DEC/21.; [21] COMPLETED STEP 20. RII[23] RSDR SWAA2021100423328Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-437395 / [19] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REP 1.; [20] JOB COMPLETED RIISDR SWAA2021101922847None · corrodedSUPPLEMENTAL INFORMATION: CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL24 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437334 / [24] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ASDR SWAA2021101922835Stringer · crackedCRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT ; 2021-437310 / [24] REPAIRED STRINGER 25L LOCATED BTW BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206. AND DAWING # 143A3230 REV. J.; [25] CERTIFIED STEP 23.; [26] REPAIRED STRINGER 2SDR SWAA2021101922838Gusset · crackedCRACK GUSSET LOCATED BS 500D, S19R IN FWD CARGO COMPARTMENT. REMOVED GUSSET IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. CRACK LENGTH IS: 0.496 INCHES. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO SDR SWAA2021101922834Stringer · crackedCRACK STRINGER 23R LOCATED BS 540 AT FWD CARGO COMPARTMENT. ] INSTALLED REPAIR TO STRINGER SECTION, ANGLE (2EA) AND CHANNEL (1EA) AND TIE CLIP AND SHEAR TIE AND FASTENERS IAW SRM 51-40-02 AND 53-00-03-2R-1, REPAIR 1, FIG 206, AND DWG 143A1225, SHEET, NG, NRCSDR SWAA2021101922836Stringer · crackedCRACK STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT ; 2021-437311 / [19] INSTALLED REPAIR PARTS STRINGER SECTION (1EA); ANGLE (2EA) AND CHANNEL (1EA) LOCATED AT STR26L AND BTW BS500D + 10 TO BS540 AT FWD CARGO COMPARTMENT AND FASTENERS IAW SRM B737-700 SDR SWAA2021101922842None · crackedCRACK ANGLE SUPPORT LOCATED BS 867, S26L IN AFT CARGO. REMOVED ANGLE SUPPORT IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AREA AND NOT FOUND MORE DAMAGE. ANGLE MUST BE REPLACED DUE NOT FOUND ALLOWABLE DAMAGE LIMIT IN SRM. CRACK LENGTH IS: 0.500 INCHES. SDR SWAA2021101922845None · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 767 RBL25 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437333 / [19] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 767 RBL25 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG # 146A750SDR SWAA2021101922843None · corrodedCORROSION LOWER SILL LOCATED BS794 TO BS847 RBL24 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437329 / [13] REPLACED LOWER SILL LOCATED BS 794 TO BS 847 RBL 24 AND WL 156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 21 REV-;SDR SWAA2021101922846None · corrodedCORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794 RBL25 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437332 / [13] REPLACED WEB-INTERCOSTAL LOCATED BTW BS767 TO BS794 RBL25 AND WL156 AT AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 ANDSDR SWAA2021101922253None · corrodedCORROSION REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER ; 2021-437292 / [07] INSTALLED NEW REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 148A8200 SHEET 4 REV -; [SDR SWAA2021101922254None · corrodedCORROSION REAR SPAR LT DRAG BRACE FITTING AT AFT INBD POSITION OF VERTICAL STABILIZER, REMOVED REAR SPAR LH DRAG BRACE FITTING IAW SRM 51-40-02. PERFORMED A VISUAL INSPECTION OF AREA AND NO FOUND DAMAGE. DRILLED A NEW REAR SPAR LT DRAG BRACE FITTING IAW SRM SDR SWAA2021101922248Seat Track · corrodedCORROSION SEAT TRACK LOCATED BS520 LBL45.50 WL208.1 AT PASSENGER CABIN ; 2021-437284 / [21] OK TO INSTALL REPAIR PARTS: [1] SEAT TRACK SECTION; [2] REPAIR CHANNEL ON REPAIR AREA LOCATED BTW BS500C TO BS520 AND LBL45.50; WL208.1 AND FASTENERS.; [22] STEP 21 COMSDR SWAA2021101922250Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS695 AND BL0 AT PASSENGER CABIN ; 2021-437288 / [15] REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 AT PASSENGER IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DRAWING # 273A9111 REV -. MATERIAL: P/N: 7075-T0/0.050 INCH (BAC1490-2883) POSDR SWAA2021092721338Rib · crackedCRACK LEADING EDGE RIB LOC. LE STA 105.26. AT LT HORIZONTAL STABILIZER. REMOVED LEADING EDGE RIB LOC. LE STA 105.26. AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. STEP 1 COMPLETED DRILLED NEW CHORD SDR SWAA2021092721339Rib · crackedCRACK LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER. REMOVED LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STAB IAW SRM 51-40-02 & PERFORMED VISUAL INSP ON AREA & NOT FOUND DAMAGE. DRILLED NEW LEADING EDGE RIB IAW SRM 51-40-05 & APPLISDR SWAA2021092721340Rib · crackedCRACK LEADING EDGE RIB LOC. LE STA 161.04 AT LT HORIZONTAL STABILIZER. REMOVED L/E RIB IAW SRM 51-40-02 & PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. COMPLETED DRILLED NEW L/E RIB IAW SRM 51-40-05 & APPLIED PROTECTIVE TREATMENT ON OPENED HOLES SDR SWAA2021070991025Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1668 INOP ; / [01] R&R THE L/H CABIN EMERGENCY LIGHT BATTERY PACK M1668; OPS CK GOOD REF 33-51-06.SDR SWAA2021041462684Light · inoperativeLH AFT ENTRY EXTERIOR EMERGENCY LIGHT IS OUT / RELAMPED LH AFT ENTRY EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04SDR SWAA2021040159125Panel · elongated193D PANEL HAS 27 FASTENER HOLES COUNTER SINKS SEVERELY WORN AND ELONGATED. / DRILLED AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05SDR SWAA2021040159126Panel · delaminated193D PANEL HAS DELAM WITH PITTING; MEASURING 4'X 1 1/2' OF AFT SIDE; MIDDLE OF PANEL / DRILLED AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05SDR SWAA2021040159127Panel · chafedSEVERE WEAR/CHAFEING ON AFT SIDE OF 193D PANEL / DRILL AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05SDR SWAA2021033159124Floor Panel · damaged194E PANEL HAS 35 FASTENER HOLES COUNTER SINKS SEVERELY WORN 6 ELONGATED. R&R'D 194E PANEL REF 5351-I-14642-NG AND AMM 53-51-21.SDR SWAA2020040635592Slide · out of positionAFT SERVICEDOOR SLIDE HOUSING DRAGS ON FLOOR DURING DOOR OPERATION / REMOVED AND REPOSITIONED SLIDE IN CONTAINER PER MT 725-61-06SDR SWAA2019102538184Sign · detachedR/H SIDE OVER WING EXIT, EXIT SIGN FELL OFF. / SECURED EXIT SIGN IAW AMM.SDR SWAA2022040109225Scuff Plate · crackedAFT CARGO DOOR; AFT CORNER SCUFF PLATE IS CRACKED IN 2 LOCATIONS / AFT CARGO AFT CORNER SCUFF PLATE REPAIRED ON WO# 39996-8300-0001 AND EA 1-A53-2076 REV 11.SDR SWAA2019101657840Stub Frame · crackedR1 DOOR FORWARD UPPER STUB FRAME CRACKED IN THE RADIUS. R&R STUB FRAME IAW DWG AND SRM.SDR SWAA2019101657839Fitting · crackedR1 DOOR UPPER HINGE ARM FITTING OF FUSELAGE SIDE BENT AND CRACKED. R&R FITTING IAW DWG.SDR SWAA2022032909214Bracket · crackedLH STA 663 VAPOR BARRIER BULKHEAD BRACKET CRACKED AT LBL 45. / REMOVED AND REPLACED LH STA 663 VAPOR BARRIER BULKHEAD BRACKET P/N 276A9183-5 IAW DWG 111A1000 REV F AND B-737 SRM 51-40-02-0G-0 STEP 7.D. ATAG_A37649SDR SWAA2022032909211Panel · corrodedNOSE WHEEL WELL PANEL 113BW HAS CORROSION AROUND FASTNER HOLES ON INNER SURFACE / VERIFIED NEW NOSE WHEEL WELL PANEL PART NUMBERS 141A7900-4 IAW AIPC 32-22-11-02; RECEIVED. ATAG WN5738. EVALUATED CORROSION. NO ALLOWABLE DAMAGE LIMITS PUBLISHED. REMOVED AND REPSDR SWAA2022032909210Support · crackedEXTERNAL FUSELAGE; STA 1016; 8' ABOVE LH VERTICAL STAB ATTACH LUG. LONGITUDINAL SUPPORT IS CRACKED IN RADIUS / REMOVED AND REPLACED LONGITUDINAL SUPPORT ABOVE LH VERTICAL ATTACH LUG STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A3101 REV BSDR SWAA2022032909202Plate · crackedRH WING REAR SPAR; 9' I/B OF #6 FLAP TRACK; LOWER PANEL ATTACH PLATE IS CRACKED AT O/B FASTNER HOLE / RH WING REAR SPAR; 9' IB OF #6 FLAPTRACK LOWER PANEL ATTACH PLATE CRAKED AT OB FASTENER HOLE REMOVED CRACKED (PLATE) IAW SRM 51-40-02-0G-0 AND REPLACED WITH NSDR SWAA2022032909200Scuff Plate · crackedFWD CARGO DOOR CUT-OUT AFT CORNER SCUFF PLATE CRACKED. / FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REMOVED CRACKED SCUFF PLATE ON CUSTOMED CARD J753-646-62-01. SENT SCUFF PLATE TO BACK SHOP FOR WELDING. BACKSHOP REPAIRED BROKE SCUFF PLATE IAW SWA ESDR SWAA2019101437738Plate · crackedL/H WING LOWER SURFACE PANEL # 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.SDR SWAA2019100837685Floor Panel · delaminatedCABIN FLOOR PANEL 241BF, AFT INBOARD CORNER, DELAMINATED DAMAGE. R&R THE FLOOR PANEL IAW SRM & DWG.SDR SWAA2019100837661Stiffener · crackedINTERNAL L/H HORIZONTAL STABILIZER, RIB ASSEMBLY NR 6 STAB. STA. 138.70, 1ST STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.SDR SWAA2019100837660Stiffener · crackedINTERNAL L/H HORIZONTAL STABILIZER, RIB ASSEMBLY #5, STAB. STA. 129.50, 4TH STIFFENER FROM FORWARD END CRACKED AT LOWER END. / REPAIRED STIFFENER IAW SRM.SDR SWAA2019100837659Stiffener · crackedINTERNAL L/H HORIZONTAL STABILIZER RIB ASSEMBLY NR 5, STAB. STA. 129.50, 2ND STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.SDR SWAA2019100877657Stiffener · crackedINTERNAL R/H HORIZONTAL STABILIZER, RIB ASSEMBLY NR 5 STAB. STA. 129.50, 2ND STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.
Back to N227WN