N449WN
Service difficulty reports · 298
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 = 'N449WN' 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 = 'N449WN' 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 SWAA2023090585509Angle · crackedCRACK ANGLE LOCATED BS807 AND S-25R AFT CARGO COMPARTMENT 2023-477646<[01] REPLACED ANGLE LOCATED BS807 AND S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8120 SHEET 31 REV -.;[02] REPLACED ANGLE LOCATED BS807 AND S-25R AFT CARGO COMPSDR SWAA2023090585510Angle · crackedCRACK ANGLE LOCATED BS907 TO BS 927 FWD POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2023-477644<[01] REPLACED ANGLE AND FASTENERS LOCATED BS907 TO BS 927 FWD POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; B737-700 SDR SWAA2023090585511Angle · crackedCRACK ANGLE LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2023-477643<[01] REPLACED ANGLE LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. AND DWG 147A7221 REV:D SDR SWAA2023090585512Cargo Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS727E AND S-26R AFT CARGO COMPARTMENT 2023-477647<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BTW BS 727D AND BS 787 IAW B737-700 SRM 53-00-SDR SWAA2023090585513Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS 927 TO BS 947.5 AND S-25R AFT CARGO COMPARTMENT 2023-477642<[01] REPLACED WEB - INTERCOSTAL LOCATED BS 927 TO BS 947.5 AND S-25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEESDR SWAA2023090585514Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2023-477641<[01] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 AND DWG #149A8103 SHEET: 6 REV: -.;[02] CORRECTED STEP 1.<BR>REPLACED ANSDR SWAA2023090585515Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND LBL 6.01 KEEL BEAM 2023-477651<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL 6.01 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02.;[02] REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL 6SDR SWAA2023090585516Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND RBL 6.01 KEEL BEAM 2023-477650<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND RBL 6.01 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02.;[02] COMPLETEDSDR SWAA2023091184932Panel · crackedCRACK ACCESS PANEL 194FL BODY FAIRING APU SHROUD DRAIN MAST FUSELAGE EXTERIOR 2023-477631<[01] REMOVED AND REPLACED APU SHROUD DRAIN MAST ON ACCESS PANEL 194FL BODY FAIRING I.A.W. B737-700 AMM 28-25-07-020-801 AND 28-25-07-420-801 SEE INDIVIDUAL SING-OFF BELOWSDR SWAA2023090584933Panel · crackedCRACK ACCESS PANEL 192F BODY STATION 616 MARKER BEACON ANTENNA KEEL BEAM 2023-477632<[01] REPLACED MARKER BEACON ANTENNA KEEL BEAM IAW AMM 34-32-11-000-802 AND 34-32-11-400-802.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED MARKER BEACON ANTENNA KEEL BEAM IASDR SWAA2023090584931Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCHES FROM FRONT EDGE LT HORIZONTAL STAB 2023-477627<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC SDR SWAA2023090784733Retainer · crackedCRACK FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING 2023-477583<[01] REPLACED FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 113A9130 SHEET 1 REV B;[02] REPLACED FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING IAW BSDR SWAA2023090684736Angle · crackedCRACK ANGLE LOCATED BS 695 AND LBL 24.75 WL 203 AT CENTER WING BOX 2023-477588<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 22-DEC-23.;[02] REPLSDR SWAA2023090584574Fairing · corrodedCORROSION ACCESS PANEL 192HL BODY FAIRING ON PLATE FUSELAGE EXTERIOR 2023-477570<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 192HL BODY FAIRING IAW B737-700 SRM 51-10-02 AND DRAWING 149A7263 SHEET 2 REV A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED PLATE LSDR SWAA2023090584575Fairing · corrodedCORROSION ACCESS PANEL 192HR BODY FAIRING ON PLATE FUSELAGE EXTERIOR 2023-477572<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 192HR BODY FAIRING IAW B737-700 SRM 51-10-02 AND DRAWING 149A7263 SHEET 2 REV A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED PLATE LSDR SWAA2023090584408Handle · deterioratedDETERIORATED ENTRY AND SERVICE DOORWAY NUT PLASTIC ASSISTLE HANDLE AT AFT GALLEY AREA (4 EA) 2023-477564<[01] REPLACED ENTRY AND SERVICE DOORWAY NUT PLASTIC ASSISTLE HANDLE AT AFT GALLEY AREA (4 EA) I.A.W 25-21-25-420-801 STEP 3.B.(5);[02] CORRECTED STEP 1<BR>SDR SWAA2023090584406Slide · deterioratedDETERIORATED GIRT BAR FITTING LOWER HARDWARE AFT ENTRY AFT SERVICE DOOR AT AFT GALLEY AREA 2023-477559<[01] REPLACED GIRT BAR FITTING LOWER HARDWARE AFT ENTRY AFT SERVICE DOOR AT AFT GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 AND THE INSTALLATION IS DOCUMENSDR SWAA2023090584735Stringer · corrodedCORROSION STRINGER 26L LOCATED BS540 AND WL151 FWD CARGO COMPARTMENT 2023-477581<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 38DLPLUS; S/N: 120398603; CAL DUE DATE: 07-NOV23;[02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022237 DUE DASDR SWAA2023090584734Stringer · corrodedCORROSION STRINGER 22R LOCATED BS540 AND WL168 FWD CARGO COMPARTMENT 2023-477579. REPAIRED STRINGER S-22R BETWEEN BSTA 500C TO BSTA 540 IAW EA 23-153-02581-WIP1 AND EA 23-153-02581. REPAIRED STRINGER S-22R BETWEEN BSTA 500C TO BSTA 540 IAW EA 23-153-02581-WSDR SWAA2023090584073Lens · brokenBROKEN SIDEWALL PANEL 231YHW EMERGENCY EXIT LENS AT PASSENGER CABIN 2023-477530<[01] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LENS AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-801 STEP C (4);[02] CORRECTED STEP 1<BR>REPLACED SIDEWALL PANEL 231YHW EMERSDR SWAA2023090683795Angle · crackedCRACK ANGLE LOCATED STA 695 AND BL0; WL207 RH SIDE AT PASSENGER CABIN 2023-477506<[01] REPLACED ANGLE AND FASTENERS LOCATED STA 695 AND BL0; WL207 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 273A9112; SHEET: 27; REV.: ?.<BR>SEE INDIVIDUSDR SWAA2023090683794Angle · crackedCRACK ANGLE LOCATED STA 695 AND BL0; WL207 LH SIDE AT PASSENGER CABIN 2023-477504<[01] REPLACED ANGLE AND FASTENERS LOCATED STA 695 AND BL0; WL207 LH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 273A9110; SHEET: 6; REV.: A.<BR>SEE INDIVIDUSDR SWAA2023090683796Angle · crackedCRACK ANGLE LOCATED STA 695 AND RBL24.75; WL203 AT PASSENGER CABIN 2023-477512<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 22-DEC-23;[02] REPLASDR SWAA2023090583797Floor Panel · crackedCRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2023-477507<[01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 AND DWG# 453A1610 REV C. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED<BR>SEE INDIVIDUAL SIGN OFF BELOWSDR SWAA2023090583793Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-477502<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18229508;DUE DATE:30-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[03] REPAIRED FWD CORNESDR SWAA2023090584072Panel · crackedCRACK ACCESS PANEL 194BR BODY FAIRING AT LOWER FUSELAGE 2023-477520<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED SCALE P/N:CR5200 S/N:8342514510 DUE DATE: 13-FEB-24;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 151023SDR SWAA2023050443631Cover · brokenLOWER EMERG EXIT LIGHT LENS AT R/H OVERWING EXIT BROKEN<[01] R & R EXIT LIGHT LENS COVER; REF AMM 33-51-01SDR SWAA2023031012965Flap · delaminatedLEFT WING O/B AFT FLAP I/B CORNER IS DELAMINATED 4.3 X 3.1<[01] REMOVED DAMAGED L/W O/B AFT FLAP AND INSTALLED SERVICEABLE L/W O/B AFT FLAP IAW BOEING 737 AMM 27-51-22 UP TO AND INCLUDING STEPS 3.F(5)G).<BR><BR>CONTINUE FROM STEPS 3.G.;[02] COMPLETED INSTALLATSDR SWAA2023020800068Panel · crackedFWD BIN C AND B HAVE CRACK IN FLOOR STA 190 AND STA 205<[01] REPAIRED IAW 25-52-01 AMM OK FOR SVCSDR SWAA2022091352662None · out of adjustL2 SLIDE SKIRT STIFF AND HARD TO CLOSE / [01] R/R L-2 SLIDE AS PER AMM 25-66-01SDR SWAA2022072430612Battery Pack · failedALL SEVEN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST / [01] REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1668;M1669;M1670;M1672;M1673;M1674; AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005SDR SWAA2022072433311Battery Pack · failedALL SEVEN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST / [01] REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1668;M1669;M1670;M1672;M1673;M1674; AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005SDR SWAA2022072433312Battery Pack · failedALL SEVEN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST / [01] REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1668;M1669;M1670;M1672;M1673;M1674; AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005SDR SWAA2022072530795Bracket · crackedFUSELAGE PANEL 192E FORWARD 2 ATTACH BRACKETS CRACKED / [01] REMOVED AND REPLACED 2 BRACKETS AT FUSELAGE PANEL 192E. BRACKET SECURED REF SRM 51-40-02 .SDR SWAA2022063023394Bracket · looseR1 SLIDE HOUSING BRACKET LOOSE / [01] TIGHTENED BRACKET PER S.I.P.SDR SWAA2021121351555Panel · elongatedSUPPLEMENTAL INFORMATION: PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02 AND SRM 51-40-05; [02] C/WSDR SWAA2021112947500Fairing · cracked194E PNL HAS 1 DIMPLED AND CRACKED HOLE; AND 3 ELONGATED HOLES ON THE TRAILING EDGE ; / [01] REMOVED AN REPLACED WING TO BODY FAIRING PER AMM 53-51-21-401SDR SWAA2021112947501Fairing · elongated193D PANEL HAS 7 OVERSIZED AND ELONGATED HOLES ON THE TRAILING EDGE ; / [01] REMOVED AN REPLACED WING TO BODY FAIRINGS PER AMM 53-51-21-401SDR SWAA2021102230802Strip · looseSUPPLEMENTAL INFORMATION: CREW REPORTS PHOTOLUMINESCENT STRIP AT 9DEF NEEDS SECURED ; / [01] RESECURED PHOTOLUMINESCENT EGRESS STRIP AT 9DEF PER SIP.SDR SWAA2021092722416None · looseSUPPLEMENTAL INFORMATION: CENTER ISLE MID CABIN CEILING EMERGENCY EXIT SIGN HANGING. ; / [01] REINSTALLED & SECURED OVERHEAD ISL EXIT LIGHT ASSY.SDR SWAA2021090713202Fuse · failedR/H SIDE OVER WING EMERGENCY EXIT LIGHT (EXIT / SALIDA) INOP. ; / [01] REPLACED BAD FUSE AT R/H SIDE OVER WING EMERGENCY EXIT LIGHT M1669; AS PER B737 AMM 33-51-06-960-804; TEST FOUND NORMAL.; [02] VERIFIED STEP 1SDR SWAA2021090706245Track · crackedFOUND LEFT HORIZONTAL UPPER FWD TRACK ASSY CRACKED. ; / [01] REMOVED LEFT HORIZONTAL UPPER FWD TRACK ASSY PER B737-700 SRM 51-40-02-0G-0.; [02] OK TO INSTALL NEW FWD TRACK.; [03] INSTALLED LEFT HORIZONTAL UPPER FWD NEW TRACK ASSY PER B737-700 SRM 51-40-02-0G-0SDR SWAA2021090706244Track · crackedFOUND RIGHT HORIZONTAL UPPER FWD TRACK ASSY CRACKED ; / [01] REMOVED RIGHT HORIZONTAL UPPER FWD. TRACK I.A.W. B 737-700 SRM 51-40-02-0G-0; [02] OK TO INSTALL NEW FWD TRACK.; [03] CLOSED RIGHT HORIZONTAL UPPER FWD TRACK I.A.W. B 737-700 SRM 51-40-02-OG-O; [04] SDR SWAA2021090705751Skin · delaminatedL/WING INBOARD MAIN FLAP HAS A DELAMINATED SPOT AT LOWER SURFACE 7' FROM O/B EDGE AND 6' FROM T/E ; / [01] PERFORMED CUT OUT OF 2' AND REMOVED DAMAGED SKIN AT L/W INBOARD MAIN FLAP TRAILING EDGE WEDGE LWR SURFACE AS PER B737-700 SRM 51-70-10-2R-0 PARAGRAPH 7.<SDR SWAA2021090705381Angle · corrodedFLIGHT COMPARTMENT; COCKPIT ENTRANCE STA270 BL'0' ANGLE SUPPORT; CORRORED ; / [01] REMOVED CORROSION FROM ANGLE SUPPORT AT FLIGHT COMPARTMENT COCKPIT ENTRANCE STA 270; BL-0 PER B737-700 SRM 51-10-02-0G-0; [02] CORROSION IS THRU ON BL 0; ANGLE SUPPORT; STA 270;SDR SWAA2021090705380Channel · corrodedFLIGHT COMPARTMENT; COCKPIT ENTRANCE STA270 BL'0' CHANNEL; CORRORED ; / [01] REMOVED ANGLE SUPPORT CORRORED FROM FLIGHT COMPARTMENT COCKPIT ENTRANCE STA 270 BL-0 PER B737-700 SRM 51-40-02-0G-0; [02] EVALUATED CORROSION PER B737-700 SRM 51-10-02-0G-0 AND FOUND SDR SWAA2021090704428Web · corrodedFWD CARGO COMPARTMENT DOOR CUTOUT; SCUFF PLATE WEB CORRORED AROUND HOLES ; / [01] LOCATED AND DRILLED NEW FWD CARGO COMP.DOOR CUT-OUT SCUFF PLATE WEB REF B737-7 SRM 51-40-05-0G-0; [02] PERFORMED COUNTERSINK HOLES AT NEW WEB REF B737-7 SRM 51-40-08-0G-0; [03] VSDR SWAA2021090704421Door Frame · crackedR1 DOOR UPPER CORNER INTERNAL FRAME ASSY CRACKED ; / [01] REMOVED INTERNAL FRAME ASSY FROM R1 DOOR UPPER CORNER PER B737-700 SRM 51-40-02-0G-0; [02] LATE ENTRY : REMOVED STOP FITTING AND SEAL DEPRESSOR FROM R1 DOOR INTERNAL FRAME ASSY FOR ACCESS TO INTERNAL FRSDR SWAA2021090703716Floorbeam · crackedMAIN CABIN FLOOR BEAM STA 328 RBL-20' FASTENER HOLE CRACKED ; / [01] INSTALLED EWIS PROTECTION AT CABIN FROM STA 312 TO STA 344 BETWEEN RBL-60 TO LBL 20 REF B737-7 AMM 20-60-07-913-801; [02] VERIFIED WORK PERFORMED; [03] REMOVED INTERCOSTAL AT CABIN BETWEEN STSDR SWAA2021090703341Angle · corrodedR2 DOOR LOWER SILL ANGLE;BETWEEN STA967 AND STA.986.5 CORRORED/ ; / [01] REMOVED CORROSION AT R2 DOOR SILL ANGLE BETWEEN STA967 AND STA986.5AS PER REF B737 SRM 51-10-02-; [02] VERIFIED STEP 1.; [03] PERFORMED UT THICKNESS INSP ON REWORKED AREA AT R2 DOOR LOWER
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