N441US
Service difficulty reports · 189
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 = 'N441US' 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 = 'N441US' 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 USAA060759Skin · crackedSTRINGER 24R BETWEEN STA 727E AND 727F CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01, DEFECT SIZE: .25 INCH.SDR SB06033Cable · faultyDURING CRUISE AT FL340, CREW REPORTED ENGINES WERE FLUCTUATING 0.4% N1 FUEL FLOW FROM 2,600 TO 2,630 LBS. ALL GAUGES FLUCTUATING. ENGINES WOULD NOT STAY IN SYNC. PMC ON OR OFF MADE NO DIFFERENCE. AUTOTHROTTLES OFF FLUCTUATED AT 0.6%. DURING A TURN, FLUCTUSDR USAA060279Skin · gougedBELOW RUDDER STA 17.25 COMPOSITE LEADING EDGE. REPAIRED PER EA 82094 FIG 1 PG 2 & 3. DEFECT SIZE: 6 EA. GOUGESSDR USAA200510001Skin · crackedFOUND 2.25" CRACK FOUND AT BS 727F S-25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201.SDR USAA050901Support Fitting · crackedCLT - Q5 - AFT SUPPORT FITTING, 1 INCH, CRACKED, FASTENER HOLE AT MLG BEAM ATTACH PT TO AFT SPAR ON AFT SUPPORT FITTING UP CHRD. REPAIR OF FITTING INCLUDED REAMING OF DISCREP HOLE, SHIMMING IAW EA. (K)SDR USAA050899Skin · wornCLT - Q - SKIN, 12 INCHES X .250 INCH X .015 INCH, SKIN WEAR, BS870, WL306.5, LBL3. INSTALLED REPAIR DOUBLER AND INSTALLED NEW RUB STRIPS IAW EA, WEIGHT CHANGE OF 1.5 LBS. (K)SDR USAA050882Angle · crackedCLT - Q5 - ANGLE, .375 INCH, CRACKED AT STA 601LT SIDE BODY WING TERMINAL FORGING ANGLE CRACKED ON AFT SIDE. REMOVED DAMAGED AND INSTALLED REPAIR ANGLE IAW SRM. (K)SDR USAA050881Balance Arm · wornCLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)SDR USAA050853Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED .750 INCH, STATION 664 LBL 32.5. REMOVED DAMAGED DAMAGED AREA, INSTALLED REPAIR IAW SRM 53-60-04. (M)SDR USAA050850Splice · corrodedCLT - FOUND SPLICE STRAP CORRODED .5 INCH, AFT CARGO FLOOR PANEL SPLICE STRAP. FABRICATED NEW STRAP AND INSTALLED IAW SRM 51-10-02. (M)SDR USAA050851Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, CENTER AISLE FRAME BETWEEN STATION 380 AND 400. FABRICATED AND INSTALLED NEW PART IAW SRM 51-10-02. (M)SDR USAA050826Angle · crackedCLT - FOUND ANGLE CRACKED .750 INCH, STATION 616 LT SIDE BODY WING TERMINAL FORGING ANGLE, CRACKED ON FORWARD SIDE. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW RT 53-62-01. (M)SDR USAA050828Skin · lightning strikeCLT - FOUND SKIN WITH LIGHTNING STRIKE .125 INCH BY .125 INCH, STATION 500B, 2 INCHES BELOW STRINGER 18L AND 12 AFT. FASTENER INSTALLED IN SKIN IAW 53-00-01 FIG 219. (M)SDR USAA050829Skin · lightning strikeCLT - FOUND SKIN WITH LIGHTNING STRIKE, STATION 469, 4 INCHES ABOVE STRINGER 21L. FASTENER INSTALLED IN SKIN IAW 737 SRM 53-00-01 FIG 219. (M)SDR USAA050830Splice · crackedFOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4R. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)SDR USAA050831Splice · crackedCLT - FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4L. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)SDR USAA050836Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, FORWARD CABIN FLOOR STRUCTURE STATION 310 RBL 13 TOP OF SUPPORT INBOARD SCREW HOLE. REMOVED DAMAGED STIFFENER, FRILLED UP AND INSTALLED PART IAW SRM 53-10-51 FIG 101, PAGE 105. (M)SDR USAA050837Fitting · corrodedFOUND FITTING CORRODED .25 BY .25, HORIZONTAL STAB CTR SECTION, RT SIDE, FORWARD SPAR. SPOT FACED FORWARD FACE OF FORWARD LUG IAW 55-10-10. (M)SDR USAA050824Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1.5 INCH, STATION 312 RBL 10. NEW TEE CAP INSTALLED IAW SRM 53-10-01, AND SRM 53-00-51. (M)SDR USAA050825Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, BS 306 LBL 11 FORWARD CABIN FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL IAW SRM 53-10-51, 51-10-02, 51-40-02. (M)SDR USAA050816Floor Support · corrodedCLT - Q5 - FLOOR SUPPORT, 2 INCH X 2 INCH CORROSION, STA 312-328, RBL 13. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER SUPPORT IAW SRM. (K)SDR USAA050815Stiffener · corrodedCLT - Q5 - FLOOR STIFFENER, 2 INCH X 16 INCH CORROSION, STA 312-328, LBL12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)SDR USAA050814Floor Support · corrodedCLT - Q5 - STA 328-344, LBL9, 2 INCH X 2 INCH, CORROSION, FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)SDR USAA050801Skin · gougedCLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K)SDR USAA050800Skin · wornMID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K)SDR USAASB03091Circuit Card · faultyCLT - FLT 255 - ON APPROACH TO CLT, AT APPROX 5,000 FEET, THE CREW DID NOT RECEIVE A GREEN LIGHT FOR THE RIGHT MAIN LANDING GEAR UPON GEAR EXTENSION. CAPTAIN ABORTED APPROACH AND HAD A DEAD HEAD FIRST OFFICER VISUALLY CHECK FOR GEAR EXTENSION. IT WAS DETERMISDR USAA030040Skin · crackedFOUND SKIN CRACKED 3 INCHES, RIGHT FUSELAGE SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACKED SECTION OF SKIN AND INSTALLED .063 INCH EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M)SDR USAA030036Skin · crackedFOUND SKIN CRACKED 3 INCHES, RIGHT SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACK SECTION OF SKIN AND INSTALLED .63 INCHES EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M)SDR USAASB01238Light · inoperativeTPA - MAINTENANCE FOUND A SEGMENT OF SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY ON SEAT ROW 9ABC. OPS CHECK GOOD. (M)SDR USAASB01235Charger · inoperativeBDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6, 7, 8 AND 9ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK NORMAL. (M)SDR USAA011069Frame · corrodedPIT - FOUND FRAME CORRODED 4 INCHES BY .500 INCHES CORRODED, FORWARD FUSELAGE DOOR FRAME BS 794 ABOVE S25R. CORROSION LEVEL 1, TASK NR C53-100-01. INSTALLED DOUBLER PER SRM 53-60-15 AND EA 71737. (M)SDR USAA010950SkinPIT - FOUND SKIN WITH OVAL WEAR MARK, .071 INCH .375 INCH DIAMETER, RIGHT A/C BAY ABOVE ACM VALVE CENTER TANK LOWER SKIN. REAMED DAMAGE TO .25 INCH DIAMETER, INSTALLED FASTENER SAME SIZE AS HOLE PER EA 71719. (M)SDR USAA010949ElevatorPIT - FOUND ELEVATOR HAS CARBON DELAMINATION, .040 INCH DEEP BY .25 INCH DIAMETER, BOTTOM SIDE OF ELEVATOR 52 INCHES FROM BOTTOM END. REPAIR PER SRM 55-20-1 AND 51-70-17 PER EA 71791. (M)SDR USAASB00248Regulator · failedDCA - FLT 1893 - EN ROUTE FROM CLT-DCA, AT FL270, THE RIGHT ENGINE BLEED TRIPPED OFF FOLLOWED BY THE LEFT ENGINE BLEED TRIPPING OFF. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DESCENDED TO FL100. PERFORMED AUTO FAIL AND UNSCHEDULED PRESSURE CHANGE CSDR USAASB97348Battery Pack · dischargedCLT - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHT INOP. MAINTENANCE CLEANED THE LIGHT SOCKET, RELAMPED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M)SDR USAA970038Strap · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION. CORRODED STRAP MEASURING 1 INCH AT STATION 798 R, FRAME REINFORCING STRAP LOCATED AT 798 R FRAME. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. FABRICATED NEW DOUBLER AND TRIPLER AS PER EA 59179. (M)SDR USAASB96243Battery Pack · dischargedCLE - MAINTENANCE FOUND THE AFT RIGHT FUSELAGE, EXTERNAL EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (X)SDR USAASB96140Battery Pack · dischargedTPA - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE, 10R, 12L AND 20L OVERHEADS, RIGHT OVERWING AND LEFT LOWER FUSELAGE LIGHTS. MAINTENANCE REPLACED THE BATTERY PACK IN OVERHEAD AT STATION 753L. OPS CHECK GOOD. (M)SDR USAA950091Fairing · looseCLT - FLT 2442 - ON CLIMB, AIRFRAME VIBRATION AT HGH POWER SETTNGS. NO VIBRATION AT IDLE POWER DESCENT OR LOW POWER SETTING. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE RUN AT ALL POWER SETTINGS. VIBRATION INDICA
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