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.

SDR USAA060759Skin · crackedSTRINGER 24R BETWEEN STA 727E AND 727F CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01, DEFECT SIZE: .25 INCH.Jun 5, 2006 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR 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, FLUCTUApr 2, 2006 · N441US · Boeing 7374B7 · Compressor Bleed ControlSDR USAA060279Skin · gougedBELOW RUDDER STA 17.25 COMPOSITE LEADING EDGE. REPAIRED PER EA 82094 FIG 1 PG 2 & 3. DEFECT SIZE: 6 EA. GOUGESFeb 16, 2006 · N441US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA200510001Skin · crackedFOUND 2.25" CRACK FOUND AT BS 727F S-25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201.Oct 4, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR 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)Jul 21, 2005 · N441US · Boeing 7374B7 · Wing, Landing Gear Attach FittingsSDR 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)Jul 21, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR 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)Jul 18, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050881Balance Arm · wornCLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)Jul 18, 2005 · N441US · Boeing 7374B7 · Rudder StructureSDR 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)Jul 8, 2005 · N441US · Boeing 7374B7 · Fuselage Main, BulkheadSDR 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)Jul 7, 2005 · N441US · Boeing 7374B7 · Fuselage Floor PanelSDR 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)Jul 7, 2005 · N441US · Boeing 7374B7 · Fuselage Main, FrameSDR 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)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR 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)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050830Splice · crackedFOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4R. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050831Splice · crackedCLT - FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4L. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jul 5, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jul 5, 2005 · N441US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR 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)Jul 1, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR 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)Jul 1, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Jun 27, 2005 · N441US · Boeing 7374B7 · Trailing Edge FlapsSDR 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)Jun 27, 2005 · N441US · Boeing 7374B7 · Trailing Edge FlapsSDR 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 DETERMIJun 24, 2003 · N441US · Boeing 7374B7 · Landing Gear Position and WarningSDR 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)Apr 7, 2003 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR 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)Apr 7, 2003 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB01238Light · inoperativeTPA - MAINTENANCE FOUND A SEGMENT OF SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY ON SEAT ROW 9ABC. OPS CHECK GOOD. (M)Aug 20, 2001 · N441US · Boeing 7374B7 · Emergency LightingSDR 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)Aug 19, 2001 · N441US · Boeing 7374B7 · Emergency LightingSDR 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)Aug 1, 2001 · N441US · Boeing 7374B7 · Fuselage Structure (General)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)Jul 28, 2001 · N441US · Boeing 7374B7 · Fuselage Structure (General)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)Jul 25, 2001 · N441US · Boeing 7374B7 · Empennage StructureSDR 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 CSep 6, 2000 · N441US · Boeing 7374B7 · Pneumatic Distribution SystemSDR 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)Dec 26, 1997 · N441US · Boeing 7374B7 · Emergency LightingSDR 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)Jan 14, 1997 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 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)Oct 18, 1996 · N441US · Boeing 7374B7 · Emergency LightingSDR 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)Jul 26, 1996 · N441US · Boeing 7374B7 · Emergency LightingSDR 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 INDICAJan 31, 1995 · N441US · Boeing 7374B7 · Aerodynamic Fairings
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