N438US

Service difficulty reports · 235

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 = 'N438US' 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 USAA050357Skin · delaminatedPIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K)Feb 22, 2005 · N438US · Boeing 7374B7 · Elevator, Tab StructureSDR USAA050329Angle · crackedPIT - FOUND ANGLE CRACKED .25 INCH, S14R TO S15R AT BS 360 ANGLE BETWEEN STRINGERS. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050324Floorbeam · corrodedPIT - FOUND BEAM WITH CORROSION 48 INCH LONG SEVERAL AREAS, FS 312, UPPER CAP FLOORBEAM. CORROSION LEVEL 1, TASK C53-107-01. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-51, FIG 205. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050332Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, STATION 616 FRAME JUST BELOW FLOOR. DOUBLER INSTALLED PER TYPICAL REPAIR 53-62-01. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050334Channel · corrodedPIT - FOUND ZEE CHANNEL CORRODED 1 INCH BY 12 INCH AREA, RIGHT SIDE ZEE CHANNEL STATION 294-362. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01, 51-40-00. (M)Feb 19, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050359Support Bracket · corrodedPIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K)Feb 18, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050356Attach Angle · wornPIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K)Feb 18, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050294Beam · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .5 INCH, STOP CUTOUT AFT END NR 6 BEAM AFT LIP ON PAN. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)Feb 17, 2005 · N438US · Boeing 7374B7 · Passenger/Crew DoorsSDR USAA050293Skin · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED FOUR PLACES, .5 INCH EACH, INNER SKIN AFT EDGE AT BEAM 3, 4, 5, 6 STOP CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)Feb 17, 2005 · N438US · Boeing 7374B7 · Passenger/Crew DoorsSDR USAA050331Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .25 INCH, STRINGER 1 STATION 578. REMOVED AND REPLACED WITH NEW PART PR SRM 51-40-02. (M)Feb 16, 2005 · N438US · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA050330Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .5 INCH, STRINGER 2R STATION 578. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02. (M)Feb 16, 2005 · N438US · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA050292Skin · crackedPIT - FOUND AFT CARGO DOOR CRACKED .5 INCH, UPPER AFT CORNER OF HANDLE/FLAPPER CUTOUT TO RIVET. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M)Feb 16, 2005 · N438US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA050291Skin · crackedPIT - NR 1 SLAT WITH FIVE CRACKS .1875 INCH CRACKS, LOWER SKIN UNDER OUTBOARD SLAT FITTING, AFT RIVET ROW. INSTALLED DOUBLER PER SRM 57-43-01. (M)Feb 15, 2005 · N438US · Boeing 7374B7 · Leading Edge DevicesSDR USAA050290Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, RT WING LEADING EDGE WBL 204 AT LOWER WING SURFACE. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER T/R 57-41-02. (M)Feb 14, 2005 · N438US · Boeing 7374B7 · Wing, Plate/SkinSDR USAA050289Structure · crackedPIT - FOUND AFT CARGO DOOR WITH TWO .25 INCH CRACKS, LOCK FASTENER BOTTOM OUTBOARD T-CHORD AFT END. REMOVED AND REPLACED T-CHORD PER RM 51-40-02. (M)Feb 14, 2005 · N438US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAASB03178Socket · corrodedMAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT, JUST AFT OF AFT ENTRY DOOR, INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM THE LIGHT ASSEMBLY SOCKET AND RELAMPED, P/N 1618. OPERATIONAL CHECK GOOD. (M)Oct 12, 2003 · N438US · Boeing 7374B7 · Emergency LightingSDR USAASB01337Circuit Board · faultyPBI - FLT 714 - AFTER TAKEOFF FROM PBI, EN ROUTE TO CLT, THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION TO RAISE THE GEAR. FOLLOWED QRH PROCEDURES AND DID NOT ATTEMPT TO USE OVERRIDE BECAUSE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED WITH THE FLDec 6, 2001 · N438US · Boeing 7374B7 · Landing Gear Position and WarningSDR USAASB01274Sensor · out of adjALB - FLT 977 - ON CLIMB-OUT FROM ALB, EN ROUTE TO PHL, CREW COULD NOT GET THE LANDING GEAR LEVER TO THE UP POSITION. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND PULLING OVERRIDE TRIGGER BROUGHT THE GEAR UP. HOWEVER, WHEN THRUST LEVERS MOVED FOSep 30, 2001 · N438US · Boeing 7374B7 · Landing Gear Position and WarningSDR USAASB01117Light · inoperativeTPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD LEFT OVERWING LIGHT STATION 607L AND THE LEFT EXIT INDICATOR STATION 612L INOPERATIVE. (M)Apr 28, 2001 · N438US · Boeing 7374B7 · Emergency LightingSDR USAA010416Bear Strap · corrodedPIT - FOUND CORROSION 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING BEAR STRAP LOWER THRESHOLD. CORROSION LEVEL 1, TASK NR C53-202-1. DAMAGED AREA CUT OUT, REPAIR DOUBLER INSTALLED PER EA 70387. (M)Mar 27, 2001 · N438US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA010415Channel · corrodedPIT - FOUND CHANNEL CORRODED 1 INCH BY 12 INCHES, AFT CARGO DOOR OPENING C-CHANNEL LOWER THRESHOLD. REPLACED CHANNEL WITH NEW PART. CORROSION LEVEL 1, TASK NR C53-202-1. (M)Mar 27, 2001 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010414Doubler · corrodedPIT - FOUND CORROSION .035 INCH DEEP, INTERCOSTAL CAP STRAP DOUBLER STATION 787-847 STRINGER 25-26R. CORROSION LEVEL 1, TASK NR C53-202-01. REPLACED STRAP PER SRM 51-40-02. (M)Mar 27, 2001 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010409Angle · corrodedPIT - FOUND FLOOR SUPPORT ANGLE CORRODED 1.5 INCH DIAMETER - .020 INCH DEEP, STATION 947 ABOVE STRINGER 24L-25L FLOOR SUPPORT ANGLE. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED CORROSION, FABRICATED DOUBLER, INSTALLED REPAIR PER 53-60-53 FIG 101, SRM 51-7Mar 20, 2001 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAASB00343Light · defectiveLGA - FLT 798 - ON APPROACH TO LGA, AFTER LANDING GEAR EXTENSION, CREW DID NOT RECEIVE A GREEN LIGHT FOR THE LEFT MAIN LANDING GEAR. CREW RECYCLED THE GEAR AND RECEIVED SAME INDICATION. A GO-AROUND WAS EXECUTED AND THE LANDING GEAR WAS RECYCLED AGAIN. THIS Dec 6, 2000 · N438US · Boeing 7374B7 · Landing Gear Position and WarningSDR USAASB00213Panel · failedFLL - FLT 1167 - EN ROUTE FROM PHL-FLL, AT FL 350, THE LEADING EDGE FLAPS TRNSIT LIGHT ILLUMINATED ALONG WITH THE NR 4 FLAP TRANSIT LIGHT ON OVERHEAD PANEL. LIGHTS REMAINED ON FOR APPROX 5-8 MINUTES, THEN EXTINGUISHED. NO ROLL OR ABNORMAL CONTROL RESPONSE WAAug 8, 2000 · N438US · Boeing 7374B7 · Trailing Edge Flap Control SystemSDR USAASB99304Indicator · failedPHL - FLT 1424 - FLIGHT WAS ON APPROACH TO PHL AND AS THE CAPTAIN EXTENDED THE FLAPS/SLATS, THE SLATS OPERATED NORMALLY BUT THE FLAPS WOULD NOT EXTEND. CAPTAIN PUT THE FIGHT IN A HOLD PATTERN AND WENT THROUGH PROCEDURES. FLAPS STILL WOULD NOT EXTEND. CAPTAIDec 27, 1999 · N438US · Boeing 7374B7 · Trailing Flap Position Indicating SystemSDR USAASB99288Fire Detector · failedMIA - FLT 1040 - DURING CLIMB-OUT FROM MIA, AT FL200, THE NR 2 ENGNE OVERHEAT LIGHT ILLUMINATED. SINCE THE 'A' LOOP OVERHEAT SYSTEM WAS ALREADY ON MEL, CREW DECIDED TO RETURN TO FIELD AT MIA AND DECLARE AN EMERGENCY. LIGHT EVENTUALLY WENT OUT ON APPROACH TO Dec 5, 1999 · N438US · Boeing 7374B7 · Fire DetectionSDR USAASB98226Battery · dischargedGSO - FOUND EMERGENCY EXIT LIGHT AT ROW 11 LEFT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (M1479). (M)Aug 2, 1998 · N438US · Boeing 7374B7 · Emergency LightingSDR USAASB98116Regulator · failedPIT - FLT 158 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RIGHT PACK SHOWED ZERO PSI. MANUAL AND AUTO SYSTEM DID NOT OPERATE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT EMay 18, 1998 · N438US · Boeing 7374B7 · Pneumatic Distribution SystemSDR USAASB98067Light · failedPHL - PILOT REPORTED THE EMERGENCY PATH LIGHTING WAS INOP AT SEAT ROWS 24 AND 25ABC. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT ESCAPE SLIDE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)Mar 17, 1998 · N438US · Boeing 7374B7 · Emergency LightingSDR USAASB98050Battery Pack · dischargedLGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Feb 26, 1998 · N438US · Boeing 7374B7 · Emergency LightingSDR 98ZZZM335Charger · failedLGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Feb 26, 1998 · N438US · Boeing 7374B7 · Emergency LightingSDR USAA960692Stringer · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH AND 4 INCH CRACK AT STATION 747 TO STATION 767, ABOVE STRINGER 26R. INSTALLED SPLICE AND REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-11, CORROSION LEVEL 2. (M)Oct 27, 1996 · N438US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAASB96159Light · failedROC - MAINTENANCE FOUND THE MID CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE FOUND THE RIGHT FORWARD EMERGENCY HATCH EXIT LIGHT SOCKET AT FAULTY. REPLACED LIGHT ASSEMBLY. ALSO, REPLACED THE MID CABIN OVERHEAD BATTERY PACK, P/N AD2013-1A. OPS CHECK GOOD. Aug 17, 1996 · N438US · Boeing 7374B7 · Emergency LightingSDR USAASB96103Sensor Tube · failedLAS - FL 9 - AFT AUXILLIARY TANK FUEL INDICATION WAS ERRACTIC FROM 0 TO 3,300 POUNDS DURING FLIGHT. CREW WAS UNALE TO TRANSFER FUEL DURING FLIGHT. FLIGHT DIVERTED TO LAS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LENGTH OF COAX AND SENSOR TUBJun 10, 1996 · N438US · Boeing 7374B7 · Fuel Indicating System
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