N445WN
Service difficulty reports · 289
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 = 'N445WN' 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 = 'N445WN' 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 SWAA2026081787426Light · inoperativeLEFT FWD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHKD GOOD.SDR SWAA2026022573053Compressor · stalled10-15 COMPRESSOR STALLS RIGHT ENGINE = 89% N1 @ 31;000 FT. RETARDED ENGINE TO 40% N1 & ENGINE STABILIZED. WAS ABLE TO GET ENGINE BACK TO NORMAL OPS PER QRH.<SDR SWAA2026022372611Check Valve · faultedRIGHT ENGINE COMPRESSOR STALLED AT FL 290. ACCOMPLISHED BORESCOPE INSPECTIONS IAW AMM 71-00-00-210-801-F00, NO FINDINGS TIME LIMITING OR BEYOND AMM LIMITS. REMOVED AND REPLACED 5TH STAGE BLEED AIR CHECKED VALVE IAW AMM 36-11-02-401. POWER ASSURANCE CHECKEDSDR SWAA2026011259836Check Valve · faultedSUSPECTED COMPRESSOR STALLS (X3) ON NR 1 ENG UPON LEVEL OFF. ACCOMP BY FLUCTUATING EGT MOMENTARILY. STABILIZED WITHOUT REPEAT FOR DURATION OF FLT. CREW NOTED EVENT HAPPENED WITH AUTOTHROTTLES ENGAGED. REMOVED ENG 1 HAND CRANK PAD IAW AMM 72-63-01-000-801-FSDR SWAA2026010555813Pressure Blkhd · crackedCRACK INDICATION AT BS 1016 APB DOME APEX UPPER LEFT FASTENER ON THE GORE WEB LAP SPLICE AT S-23R MEASURING 0.0625 INCH IN LENGTH FROM FASTENER HEAD. REPAIRED BS 1016 APB IAW EA 25-153-03516.SDR SWAA2025122955665Sign · detachedEXIT/SALIDA SIGN FELL FROM FORWARD CABIN ON TAKEOFF. R & R FWD EXIT SIGN LIGHT ASSY IAW AMM 33-51-01.SDR SWAA2025102721975Web · corrodedCORROSION UPPER MAIN SILL WEB LOCATED BETWEEN BS440 TO BS492 AT LEVEL STR 18R AND WL 198.5. REPLACED WEB AND FASTENERS LOCATED BTW BS440 TO BS492 AT LEVEL STR18R RBL70 WL 198.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, DWG 143A8111, SHEET 12, REV A, & DWGSDR SWAA2025102721977Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.SDR SWAA2025102721832Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV. -.SDR SWAA2025102721978Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.SDR SWAA2025102721833Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A.SDR SWAA2025102721831Support Angle · crackedCRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 24, REV A. MEASUREMENT OF CRACK IS L= 0.813".SDR SWAA2025102721976Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 376 INTERNAL CAVITY TRAILING EDGE AT RT WING.SDR SWAA2025102721683Strap · corrodedCORROSION STRAP LOCATED BETWEEN BS 794.5 TO 807, S26R, WL 153 IN AFT CARGO BAY. REPLACED STRAP & FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A8340, SHEET 21, REV -.SDR SWAA2025102721684Web · corrodedCORROSION LOWER SILL LOCATED BETWEEN BS 794.5 TO 847, STR 25R, WL156 IN AFT CARGO BAY. REPLACED LOWER SILL AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A8340 SHEET 21 REV.-.SDR SWAA2025102721477Floorbeam · crackedCRACKED BRAKE PANEL FLOORBEAM LOCATED BS 540, BL 0 TO RBL 24.75 AT PASSENGER CABIN REPLACED FLOORBEAM AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 36, REV A.SDR SWAA2025102721110Support Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND RBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE AT STA695 AND RBL24.75 PASSENGER CABIN IAW SRM 51-40-02-0G-0, DWG 273A9111, SHEET 6, REV A, AND DWG 111A6000, SHEET 178, RSDR SWAA2025102721479Tail Cone · delaminatedDELAMINATED TAIL CONE ON EXTERNAL SKIN. REPAIRED TAIL CONE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1 REPAIR 1.SDR SWAA2025102721109Support Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE IAW SRM 51-40-02-0G-0, & DWG 273A9111, SHEET 6, REV A, AND DWG 111A6000, SHEET 178, REV-.SDR SWAA2025102721106Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 571FB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 571FB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2025102720583Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2025102720580Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A6200, SHEET 10, REV-. MEASURESDR SWAA2025102720581Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 RESDR SWAA2025102720741Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SPAR AT RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5. REPAIR 5.SDR SWAA2025102719923Light · brokenBROKEN PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN 2025-611549<[01] REPLACED PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN IASDR SWAA2025102719924Light · brokenBROKEN PHOTOLUMINESCENT STRIP RH SIDE (7EA) AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802SDR SWAA2025092918571Slide · dislodgedFWD PAX DOOR DISLODGED AIR SLIDE FROM GIRT BAR, DID NOT INFLATE. RE-INSTALLED SLIDE PER MT 725-61-06SDR SWAA2025063085795Handle · unsecureINSIDE ASSIST HANDLE NEXT TO AFT SERVICE DOOR NOT SECURE.<[01] SECURED IAW SIP.SDR SWAA2025060377046Seat Back · out of adjustSEAT 12F WILL NOT STAY UP. SECURED UPRIGHT. <[01] SECURED SEAT UPRIGHT. REFER LP# 2258629 FOR NEW MEL.; [02] SIGNED OFF AS FACT IN MAINTENIX IN ERROR. CREATED NEW FAULT ON LP# 2258630.SDR SWAA2025040721623Transmitter · lockedFLAPS LOCK OUT AT 9 DEGREES; TRAILING EDGE DISAGREE LIGHT; WE DROVE THE FLAPS TO 15 DEGREES PER THE QRH. ALL INDICATIONS NORMAL.<[01] R&R R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01.SDR SWAA2025021796397Windshield · crackedR1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER MT 734-00-03. VERIFICATION # 46207SDR SWAA2025021796899Control Unit · faultedR1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER MT 734-00-03. VERIFICATION # 46207SDR SWAA2024091636149Web · crackedLMLG CENTER DOOR CRACKED AT WEB- MARKED<[01] REMOVED L/H MLG CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11. OK FOR CONTINUED SERVICE PER CDL 32-10-3XCSDR SWAA2024082629290Starter · overheatedON #1 ENGINE START HAD ENGINE 1 OVERHEAT FOLLOWED BY #1 ENGINE FIRE INDICATION; COMPLIED WITH QRC AND QRH PROCEDURES.<[01] REF BAR CODE TTG8Q00VE9LA FOR STARTER R+R AMM 80-11-01<BR>REF BAR CODE TTG8Q00VE8C7 FOR BOTH #1 + #2 FIRE BOTTLE CHANGE; AMM 26-21-01<BR>SDR SWAA2024070106898Lens · dislodgedEMERGENCY EXIT LENS DISLODGED FROM ABOVE FWD SERVICE DOOR LOCKING PIN MISSING FROM LIGHT ASSY FWD SIDE<[01] C/W EA M21-133-00720SDR SWAA2024060597715Light · inoperativeEXTERIOR AFT MOST LEFT EMERGENCY LIGHT INOP<[01] RELAMPED EXTERIOR AFT MOST EMERGENCY LIGHT REF AMM 33-51-00 OPS CHECK GOODSDR SWAA2024020246984Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF AFT ENTRY DOOR INOP<[01] RE-LAMPED THE EXTERIOR EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR IAW AMM 33-51-04. OPS CHECK GOODSDR SWAA2024012243019Girt Bar · out of adjustDOOR 1R FLOOR CLIPS FPR SLIDE GIRT BAR MIGHT BE FACING WRONG DIRECTION; AS NOTICED BY FLIGHT ATTENDANTS.<[01] REMOVED AND REINSTALLED FORWARD SERVICE DOOR FLOOR MOUNTED BRACKETS TO CORRECT POSITIONS PER AMM 25-66-02.SDR SWAA2024010432957Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACKS FOR POWER SUPPLY'S M1672; M1673; M1674 FAILED CAPACITY CHECK EMERGENCY LIGHTS INOP AND DID STAY ON.<[01] REMOVED AND REPLACED BATTERY PACKS FOR POWER SUPPLY M1672 ;M1673 ;M1674 PER B737 AMM 33-51-06-960-805. PERFORMED OPERATIONAL SDR SWAA2024010426504Scuff Plate · crackedR1 DOOR ; SCUFF PLATE FOUND CRACK AT FWD CORNER<[01] ACCOMPLISHED WELD REPAIR OF CRACK FOUND AT R1 DOOR SCUFF PLATE FWD CORNER PER REF B737 SRM 53-70-15-2R-1;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024010425465Rib · crackedLEFT HORIZONTAL STABILIZER LE (PANEL 331B)HAS CRAKED RIB # 19 DOT# 223<[01] REMOVED AND REPLACED RIB# 19 AT LEFT HORIZONTAL STABILIZER LE PANEL 331 B AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG# 186A1001;[02] VERIFIED; STEP # 1. REMOVED AND REPLACED RIB# 19 AT SDR SWAA2024010425462Intercostal · crackedAFT OF FWD CARGO COMPARTMENT; RIGHT SIDE STG 25 BS 500D TO BS 520 INTERCOSTAL CRACK NOTED (P/N: 143A9803-58).<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CARGO BETWEEN STA 500D AND STA 520 S-25R REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A7902.;[02] VERIFIED;SDR SWAA2023122924006Panel · crackedR2 DOOR LOWER PANEL 844DZ FOUND CRACKED AND BENT IN SEVERAL PLACES.<[01] RECEIVED NEW R2 DOOR LOWER PANEL 844DZ FROM STOCK. ITEM TO BE INSTALLED ON TTG8Q00PRE1S.;[02] VERIFIED STEP 1.SDR SWAA2024010527539Thrust Reverser · corrodedCORROSION AT NO-2 ENGINE INB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG I/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF LIMITS PER REF B737 SRM 54-30-01-1A-4. T/R WILL BE REPLACED ON FAULT TTG8Q00PYAGH.;[02] VERIFIED STEPSDR SWAA2024010527540Thrust Reverser · corrodedCORROSION AT NO-2 ENGINE OUB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG O/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF LIMITS PER REF B737 SRM 54-30-01-1A-4. T/R WILL BE REPLACED ON FAULT TTG8Q00PYA4B;[02] FINAL INSPECTISDR SWAA2024010323500Panel · crackedAFT CARGO COMPARTMENT PANEL #142YAC; WAVY SURFACE AND CRACKED EDGES.<[01] FABRICATED NEW AFT CARGO PANEL #142YAC PER REF AMM 25-52-01-201-801;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024010523222Panel · corrodedCORROSION SPOT AT R/W FRONT SPAR L/E FUEL QTY INDICATORS SUPPORT PANEL MKD DOT<[01] REMOVED REFUEL PANEL (P15) PER TASK 28-21-00-000-801; INSTALLED EWIS PROTECTION FOR MAINTENACE PER TASK 20-60-07-913-801;REMOVED AND REPLACED P15 INDICATOR FACEPLATE/BRACKET ASSDR SWAA2024010422609Support Bracket · corrodedCORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CENTER WING BOX LBL 64 STA 706 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] (RII) FINAL INSPECTIOSDR SWAA2024010422610Support Bracket · corrodedCORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706+10' MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CENTER WING BOX LBL 64 STA 706+10' REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] (RII) FINAL ISDR SWAA2024010422612Support Bracket · corrodedCORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-65 STA 727 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN LBL 65 STA 727 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] VERIFIED; STEP # 1.REMOVED AND REPLAC
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