N440US, cancelled Feb 24, 2025
Service difficulty reports · 220
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 = 'N440US' AND deregistration_id = 'N440US-2025-02-24' 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 = 'N440US' AND deregistration_id = 'N440US-2025-02-24' 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 I5EA2023110600006Battery Pack · no testMID CABIN OVERHEAD EMERGENCY LIGHT INOP. - REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY WITH SERVICEABLE UNITS IAW B737 AMM 33-51-51. OPS CHECK GOOD.SDR I5EA2021062900002Adapter · inoperativeLOSS OF BOTH ADI'S AND BOTH FLIGHT DIRECTORS, USED STANDBY ADI TO RETURN TO FIELD, EMERGENCY DECLARED. REMOVED AND REPLACED DIGITAL ANALOG ADAPTER IAW B737-400 AMM 34-28-11, OPS CHECKED GOOD. ALSO PERFORMED FLIGHT DIRECTOR CHECK INTHE DFCS BITE CHECK IAW B73SDR I5EA2021022600008Battery Pack · no testCENTER AISLE EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT CENTER AISLE STA 629 BATTERY PACK AND OPS CHECK GOOD IAW B-737-400 AMM 33-51-51.SDR I5EA2020040901Light · inoperativeEMERGENCY LIGHT INOP AT ROW 7 DEF.SDR I5EA201910310903Slide · unsecureL1 DOOR SLIDE LOOSESDR I5EA201910250003Slide · looseL1 DOOR SLIDE LOOSE.SDR I5EA2019050800001Power Supply · failedDISCREPANCY: EMERGANCY LIGHT POWER SUPPLY M1479 STA 598A INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGANCY LIGHT POWER SUPPLY M179 AT STA 597A IAW AMM 33-51-51.SDR I5EA2018102900013Battery Pack · dischargedDISCREPANCY: EMERGENCY LIGHT BATTERY PACK AT M1132 AT STA 338L. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1132 AT STA 338L, TEST GOOD IAW AMM33-51-51.SDR I5EA2017062200135Battery · dischargedSOME OF THE EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. FOUND THE BATTERY DISCHARGED.SDR I5EA2015051800032Landing Gear · malfunctionedAT 9000 FT, WITH THE GEAR HANGLE IN THE OFF POITION, GEAR EXTENDED. WHEN THE HANDLE WAS MOVED UP, WITH OVERIDE, 3 RED LIGHTS AND THE GEAR DID NOT COME UP. IN DOWN POSITION 3 GREEN LIGHTS FOLLOWED QRH. PERFORMED GEAR CONTROL SYS, NLG & MLG EXTENTION AND RETRSDR I5EA201502210001Aoa · malfunctionedRTO AT 100K 97.000LBS TEMP -12C BRAKE COOLING REQUIRED 48 MINUTES. REASON FOR RTO GOT STICK SHAKER. R & R LT AOA SENSOR OPS CHECK GOOD.SDR I5EA0201511300024Squat Switch · malfunctionedSTALL WARNING SHAKER ON JUST PAST 80K ON T/O ROLL. R & R CIRCOIL CARD M990 GROUND SENSING SQUAT SW. FUNCTIONAL CHECK OF CARD AND RELATED SYSTEM GOOD. STALL WARNING TEST GOOD.SDR USAA2014060300006Lens · brokenCREW REPORTED THE EXIT LIGHT LENS 12C BROKEN. REPLACED LIGHT ASSEMBLY AT ROW 12C IAW ESPM 20-45-01. OPERATIONS CHECKED SATISFACTORY.SDR USAA2014052000001Light · brokenTHE 2L DOOR EMERGENCY EXIT LIGHT BROKEN. REPLACED LIGHT ASSEMBLY, EMERGENCY LIGHT AT 2L DOOR CHECKED GOOD.SDR USAA2014050500018Cover · damagedREPORTED THE LT OVERWING EXIT SIGN COVER DAMAGED. R & R LT OVERWING EXIT SIGN COVER IAW AMM 33-51-11-002-004 402-007.SDR USAA2014050500025Skin · crackedA .437 INCH CRACK ON FUSELAGE SKIN AT BS 312, STRINGER 6L. REPAIRED SKIN IAW SRM 53-10-01, REPAIR 17, DETAIL IV & EA 105901.SDR USAA2014042300004Skin · crackedDROP IN VISIT 2 INCH CRACK ON FUSELAGE SKIN BELOW L2 DOOR AT BS 970, STRINGER 20L. REPAIRED FUSELAGE SKIN BELOW L2 DOOR AT BS 970, STRINGER 20L IAW EA 105839.SDR USAA2014030600004Seat Track · lack of lubeCREW REPORTS THE CAPTAIN`S SEAT IS DIFFICULT TO MOVE BACK & FWD. LUBED SEAT TRACK AS NEEDED, CHECKED OK.SDR USAA2014030300013Lens · brokenCREW REPORTS SEAT 4C COVER FOR AISLE LIGHT EMERGENCY LIGHT LENS CLIPPED OFF. REPLACED LIGHT LENS ASSEMBLY. OPERATIONS CHECKED OK, ACCOMPLISHED AT SEAT 4C.SDR USAA2013122400005Placard · unsecureCREW REPORTED THE EMERGENCY EXIT PLACARD, OVERWING EXIT RT SIDE, FELL OFF. REATTACHED PLACARD AS NEEDED, CHECKED OK.SDR USAA2013101400012Skin · delaminatedC2 CHECK, DELAMINATION ON RT AILERON UPPER SURFACE AT 0.5 INCH FROM OTBD END & 11 INCHES FROM TRAILING EDGE. REPAIRED RT AILERON UPPER SURFACE IAW SRM 51-70-04 & 51-70-30.SDR USAA2013101100001Skin · delaminatedC2 CHECK, DELAMINATION ON LT WING OTBD FOREFLAP T/E APPROXIMATELY 2" FROM INBD END. REPAIRED LT WING OTBD FOREFLAP T/E IAW SRM 57-53-02-01.SDR USAA2013092500001Unknown · unknownAFTER TAKEOFF, PASSENGER IN ROW 3 REPORTED AN ODOR THAT MADE THEM FEEL QUEASY. NO ODOR OR ABNORMAL COCKPIT INDICATIONS OBSERVED. MX ACCOMPLISHED TROUBLESHOOT CABIN ODOR IAW J/C 03L00021001. NO ODOR DETECTED.SDR USAA2013081600015Seat · lack of lubeCREW REPORTED THE CAPTAIN'S SEAT DIFFICULT TO ADJUST IN FWD & AFT MOVEMENT. MX LUBED CAPTAIN'S SEAT AS NEEDED. CHECKED OK.SDR USAA2013080800018Sensor · faultyON DESCENT OUT OF 23,000 FT, AUTO THROTTLES PULLED THROTTLES TO IDLE. UPON REACHING IDLE, ONE OF THE ENGINES COMPRESSOR STALLED. ALL ENGINE INDICATIONS WERE NORMAL AFTER EVENT. YAW WAS FELT ALONG WITH A BANG. MOC AND PILOT CONFERENCED THAT LT ENGINE STALLED.SDR USAA2013080600004Skin · delaminatedUPPER RT SIDE OF RUDDER HAS DELAMINATION AT T/E 22" FROM UPPER TIP. REPLACED RUDDER IAW 03L70827003 & 03C70827007.SDR USAA2013070900026Sign · missingCREW REPORTED THE EXIT SIGN AT 2R DOOR MISSING. MX REPLACED EXIT SIGN AT DOOR 2R.SDR USAA2013071000008Girt Bar · out of positionCREW REPORTED THE 1R DOOR GIRT BAR WILL NOT STOW PROPERLY. MX REPOSITIONED GIRT BAR AT 1R DOOR. OPS CHECK OK.SDR USAA2013052200003Seat Track · lack of lubeCREW REPORTED THE CAPTAIN'S SEAT IS DIFFICULT TO ADJUST FORE AND AFT. MX LUBRICATED SEAT TRACKS. OPS CHECK FINE.SDR USAA2013040800020Ballast · inoperativeMAINTENANCE REPORTED THE LIGHT ASSEMBLY BALLAST INOP (OVERWING EXIT). MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST PER AMM 33-51-11-002-004 AND 33-51-11-402-007.SDR USAA2013030400042Proximity Switch · out of toleranceAFTER TAKEOFF FROM MCO, CREW REPORTED THE AIRCRAFT THINKS IT'S ON THE GROUND - VNAV-LNAV-TCAS-A/T-ACARS WILL NOT WORK IN ANY FLIGHT MODES. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT MCO WITHOUT INCIDENT. MAINTENANCE CONFIRMED FAULT AND FOUND GROUND SDR USAA2013030100007Controller · faultyEN ROUTE FROM MIA TO CLT, CREW REPORTED THE CABIN ALTITUDE HORN SOUNDED AND CABIN ROSE TO 13,000 FEET. CAPTAIN INSTRUCTED FLIGHT ATTENDANT'S TO DEPLOY THEIR OXYGEN MASKS. (PASSENGER OXYGEN MASKS WERE NEVER DEPLOYED.) CREW INITIATED AN EMERGENCY DESCENT AND SDR USAA2013020400007Frame · crackedQ6 CHECK - CRACKS ON FUSELAGE FRAME AT BS 847 BETWEEN S19R & S21R. REPLACED FUSELAGE FRAME AT BS 847 BETWEEN S19R & S21R IAW B737 SRM 51-40-02-0G, PAR 4, FIGS 3, 8 & 12.SDR USAA2013020400006Frame · corrodedQ6 CHECK - CORROSION ON FUSELAGE FRAME AT BS 794.3, S25R BETWEEN RBL 20 TO RBL 25. REPLACED FUSELAGE FRAME AT BS 794.3, S25R BETWEEN RBL 20 TO RBL 25 IAW B737 SRM 51-40-02-0G, PAR 4 & 7D, FIGS 3, 8 & 12.SDR USAA2013013100003Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 727F, S26R, WL 145. REPLACED STRINGER TIE CLIP AT BS 727F, S26R, WL 145 IAW B737 SRM 51-40-02-0G, FIG 3.SDR USAA2013020400004Stringer Clip · crackedQ6 CHECK - CRACK ON STRINGER CLIP AT BS 947, S23L. REPLACED STRINGER CLIP AT BS 947, S23L IAW B737 SRM 51-40-02-0G, PAR 4, FIG 12.SDR USAA2013012800020Frame · crackedQ6 CHECK - CRACK ON FUSELAGE FRAME AT BS 500G BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500G BETWEEN S20L TO S21L IAW B737 SRM 53-00-07-2R-13.SDR USAA2013020400005Stringer Clip · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER CLIP AT BS 947.5, S27R. REPLACED STRINGER CLIP AT BS 947.5, S27R IAW B737 SRM 51-40-02-0G, PAR 4, FIG 12.SDR USAA2013020700001Stringer · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION ON STRINGER S26R AT BS 963.5. REPAIRED STRINGER S26R AT BS 963.5 IAW B737 SRM 53-00-03-2R-1, FIG 201.SDR USAA2013020400011Skin · corrodedQ6 CHECK - CORROSION ON FUSELAGE SKIN AT BS 947.5, S27R. REPAIRED FUSELAGE SKIN AT BS 947.5, S27R IAW EA 504630.SDR USAA2013020400003Intercostal · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS 947, S27R. REPLACED INTERCOSTAL AT BS 947, S27R IAW B737 SRM 51-40-02-0G, PAR 4B, FIG 3 & 8.SDR USAA2013013100004Stringer · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER 27R AT BS 947.5, WL 148. REPAIRED STRINGER 27R AT BS 947.5, WL 148 IAW B737 SRM 53-00-03-2R-1.SDR USAA2013012300023Tie Clip · crackedQ6 CHECK - CRACK IN STRINGER TIE CLIP AT BS 947, S26L. REPLACED STRINGER TIE CLIP AT BS 947, S26L IAW B737 SRM 51-40-02-0G, FIG 8 & 12.SDR USAA2013012800019Channel · corrodedQ6 CHECK - CORROSION ON CHANNEL BETWEEN BS 767 TO BS 794, S25R. REPLACED CHANNEL BETWEEN BS 767 TO BS 794, S25R IAW B737 SRM 51-40-02-0G, FIG 2.SDR USAA2013012800021Stringer Clip · crackedQ6 CHECK - CRACK ON STRINGER CLIP AT BS 727E, S25R. REPLACED STRINGER CLIP AT BS 727E, S25R IAW B737 SRM 51-40-02-0G.SDR USAA2013020600007Skin · crackedQ6 CHECK - CRACK ON FUSELAGE SKIN BETWEEN BS 344 TO BS 360 & BETWEEN S1L TO S2L. REPAIRED FUSELAGE SKIN BETWEEN BS 344 TO BS 360 & BETWEEN S1L TO S2L IAW B737 SRM 53-00-01-2R-31 FIG 201.SDR USAA2013012300015Tie Clip · crackedQ6 CHECK - CRACK IN STRINGER TIE CLIP AT BS 727F, S24L. REPLACED STRINGER TIE CLIP AT BS 727F, S24L IAW B737 SRM 51-40-02-0G, PAR 4 & 7, FIG 8.SDR USAA2013012300011Shear Web · corrodedQ6 CHECK - LEVEL 2 FILIFORM CORROSION ON AFT LEFT SHEAR WEB AT BS 986.5+8 INCHES, LBL 47. REPLACED AFT LEFT SHEAR WEB AT BS 986.5+8 INCHES, LBL 47 IAW B737 SRM 51-40-02-0G, FIG 12.SDR USAA2013012300007Angle · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR SILL ANGLE BETWEEN BS 967 TO BS 986.5, S17L, LBL 57. REPLACED L2 DOOR SILL ANGLE BETWEEN BS 967 TO BS 986.5, S17L, LBL 57 IAW B737 SRM 51-40-02-0G PAR 4 & 7D, FIG 8 & 12.SDR USAA2013012300019Stringer Clip · crackedQ6 CHECK - CRACK IN STRINGER CLIP AT BS 707, S4L. REPLACED STRINGER CLIP AT BS 707, S4L IAW B737 SRM 51-40-02-0G, PAR 4 & 7D, FIG 8 & 12.
Back to N440US, cancelled Feb 24, 2025