N374US, cancelled Mar 16, 2006
Service difficulty reports · 109
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 = 'N374US' AND deregistration_id = 'N374US-2006-03-16' 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 = 'N374US' AND deregistration_id = 'N374US-2006-03-16' 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 SB05079Indicator · failedCLT FLT 1417 AFTER TAKEOFF FROM CLT ENROUTE TO PBI, CREW REPORTED THE FLAPS LOCKED DURING RETRACTION DUE TO AN ASYMMETRY CONDITON. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPESDR USAA050553Support Beam · crackedBFM - FOUND AFT SUPPORT BEAM CRACKED, LT MLG BEAM AFT SUPPORT FITTING ON AFT SPAR, APPROX WBL 157.0 S1 WING. REMOVED FASTENERS, PERFORMED NDT INSPECTION, REINSTALLED FASTENERS PER TYPICAL REPAIR 57-40-13 REV A. (M)SDR USAA050540Seat Track · gougedBFM - FOUND SEAT TRACK WITH NICKS AND GOUGES, .90 INCH BY .2 INCH BY .022 INCH AND .40 INCH BY .10 INCH BY .025 INCH, MCD FROM STATION 480-520. FABRICATED NEW SEAT TRACK, REMOVED AND REPLACED PER SRM 53-00-52, SRM 51-40-02. (M)SDR USAA050554Stringer Splice · crackedBFM - FOUND STRINGER SPLICE CRACKED .750 INCH, FASTENERS MOUNTING HOLE, AFT CABIN LEFT CEILING, STRINGER 4L AT BS 908. FABRICATED PARTS, INSTALLED FABRICATED CHANNEL ON STRINGER SPLICE PER SRM 51-40-02. (M)SDR USAA050539Sleeve · chafedBFM - FOUND SUPPORT SLEEVE CHAFED MARK .086 WEAR, RT MLG FORWARD TRUNNION BEARING SUPPORT FITTING. REMOVED AND REPLACED FORWARD TRUNNION SUPPORT SLEEVE PER TYPICAL REPAIR 57-20-04. (M)SDR USAA050542Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 3 INCHES LONG BY 1 INCH WIDE BY .055 INCH DEEP AND 3 INCHES LONG BY 1 INCH WIDE BY .043 INCH DEEP, AFT CARGO FLOOR LBL 12.5 AND RBL 3. FABRICATED REPAIR ANGLES AND INSTALLED PER TYP REPAIR 53-10-06B. CORROSION LEVEL 1, TASK C53SDR USAA050541Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT/ANGLE CORRODED 1 INCH LONG BY 1 INCH WIDE BY .028 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 867 LBL 8.10 INCH. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B AND SRM 53-60-53. (M)SDR USAA050536Stiffener · corrodedBFM - FOUND STIFFENER EXFOLIATED AND CORRODED CHORD, BS 290-303, LBL 11.10 FLOOR SUPPORTS WL 208. INSTALLED FABRICATED PARTS PER SRM 53-10-51, 51-40-02. (M)SDR USAA050538Support Angle · crackedBFM - FOUND SUPPORT ANGLE CRACKED 4 INCHES, LT WING TE NR 3 (INBOARD TO OUTBOARD) HINGE WS 573.872 WBL, 415.93. REMOVED, FABRICATED NEW, INSTALLED NEW SUPPORT ANGLE PER SRM 57-51-02, 51-40-05, 51-40-02. (M)SDR USAA050537Floorbeam · corrodedBFM - FOUND SUPPORT, T-ANGLE, WEB CORRODED AND CRACKED 4 INCHES LONG, 1 INCH WIDE AND 1 INCH, BS 994 WL 208 AFT CABIN FLOOR. BLENDED SUPPORT, REMOVED AND REPLACED T-ANGLE AND WEB WITH NEW FABRICATED PARTS PER SRM 51-40-02, 53-60-51. (M)SDR USAA050524Channel · corrodedBFM - FOUND FLOOR SUPPORT CHANNEL CORRODED 2 INCHES LONG BY .90 INCHES WIDE BY .030 INCHES DEEP, AFT CARGO BS 704 RBL 8.10. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B. (M)SDR USAA050526Shear Web · corrodedFOUND SHEAR WEB CORRODED 10 INCHES BY 27 INCHES, BS 1016 FLOOR BL 0 - LBL 27. CORROSION LEVEL 1, TASK C53-202-01. FABRICATED NEW SHEAR WEB AND INSTALLED NEW PARTS PER SRM 53-60-51, 51-30-01, 51-24-00, 51-40-02. (M)SDR USAA050525Shear Tie · corrodedFOUND FRAME BOTTOM SHEAR TIE CORRODED, 2 INCHES LONG BY .80 INCH WIDE BY .032 INCH DEEP, BS 360 WL 148.5 RBL 4. REPLACED SHEAR TIE PER SRM 51-40-02. (M)SDR USAA050534Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 2.5 INCHES LONG BY 1 INCH WIDE BY .045 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 773 LBL 12.5 - RBL 8.10. FABRICATED DOUBLERS AND INSTALLED PER TYPICAL REPAIR 53-10-06B. (M)SDR USAA050528Channel · corrodedBFM - FOUND CHANNEL CORRODED 2 INCHES WIDE BY .056 INCHES DEEP BY 4.0 INCHES LONG, BETWEEN BS 986-1006, S-24L AND S-25L. INSTALLED REPAIR SUPPORT PLATE, CHANNEL, PER BOEING DWG 65-55843 AND SRM 51-40-02. (M)SDR USAA050527Access Panel · corrodedBFM - FOUND ACCESS PANEL CRACKED AND CORRODED 1.5 INCH CRACK, 3 INCH CORROSION .050 DEEP, RIGHT W/W LOWER PANEL. FABRICATED NEW PART PER 51-40-02. (M)SDR USAA050532Stringer · corrodedBFM - FOUND STRINGER CORRODED 8 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP AREA, BS 967, STRINGER 25L. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-00-03. (M)SDR USAA050530Plate · corrodedBFM - FOUND PANEL FLANGE PLATE CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCH DEEP, NR 1 PYLON MID FAIRING PANEL FLANGE PLATE. INSTALLED REPAIR SPLICE PLATE PER SRM 54-50-70 AND BOEING DWG 313A1380. (M)SDR USAA050529Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCHES DEEP, AFT CARGO COMPARTMENT FLOOR SUPPORT BS 727D PLUS LBL 12.5- RBL 8.10 INCH. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR ANGLE IAW TYPICAL REPAIR 53-10-06B AND 53-6SDR USAA050533Floor Support · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE BY 2 INCHES LONG BY .053 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 825 LBL 8.10 INCH AND RBL 3. INSTALLED REPAIR ANGLE PER TYP REPAIR 53-10-06B, 53-60-53, 51-10-02. (M)SDR USAA050535Floor Support · corrodedBFM - FOUND FLOOR SUPPORT ANGLE CORRODED 1.6 INCH BY .90 INCH BY .043 INCH, AFT CARGO COMPARTMENT 3 INCHES AFT OF BS 727B. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR IAW TR 53-10-06B, SRM 53-60-53. (M)SDR USAA050531Web · corrodedBFM - FOUND DOOR SILL WEB CORRODED 1 INCH BY 1 INCH BY .063 INCH AREA, FORWARD CARGO DOOR SILL BS 440-485. CORROSION LEVEL 1, TASK C53-208-01. FABRICATED SILL WEB TR 501886, SRM 53-30-15, 51-40-02. (M)SDR USAA050064Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 2.5 INCH AREA, NR 3 SLAT INBOARD TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, DOUBLERS PER SRM 51-70-10. (M)SDR USAA050046Rivet · loosePIT - FOUND LT WING FOREFLAP 42 LOOSE RIVETS, LT WING OUTBOARD FOREFLAP APPROX 42 INCHES. DEFECTIVE PART REPLACED WITH IDENT PART. (M)SDR USAA050045Skin · crackedPIT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-10 AND EA 79782. (M)SDR USAA040764Skin · crackedCLT, RON, SKIN-1 INCH CRACK, BS 727E AT STRINGER 22R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229.SDR USAA040560Skin · crackedCLT - FOUND SKIN CRACKED 4.3125, LT SIDE FUSELAGE STATION 18 AT STATION 75. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M)SDR USAASB04112Static Line · loosePHL - FLT 477 - EN ROUTE FROM PHL-RDU, CREW REPORTED THE FIRST OFFICER ALTIMETER, AIRSPEED AND VSI WENT INOPERATIVE. CREW ALSO REPORTED THAT ON TAKEOFF ROLL, THE AUTO THROTTLES DISENGAGED AND THE N1 BUGS SLOWED TO ZERO. FLIGHT RETURNED TO FIELD AT PHL AND LANSDR USAASB04034Seal · leakingON CLIMB-OUT FROM CLT, PASSING THROGH 7,000 FT, THE A-HYD SYSTEM EMDP LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED SHORTLY THEREAFTER BY THE 'A' HYDRAULIC SYSTEM EDP LOW PRESSURE LIGHT. QUANITY FOR 'A' HYDRAULIC SYSTEM READ ZERO. CREW DECLARED AN EMERGENCY AND RSDR USAASB04027Valve · crackedCREW REPORTED LOSING SYSTEM A-HYDRAULICS ON TAKEOFF AS LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY INDICATED ZERO. FLT LEVELED OFF AT 5,000 FEET TO COMPLETE QUICK REFERENCE HANDBOOK PROCEDURES, THEN THE FLIGHT RETURNED TO FIELD AT BNA. UPON LANDING, THE LANDSDR USAA040046Skin · crackedFOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN AND BEAR STRAP BS 957 S-14R SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER PER SRM 53-60-01 AND EA 78095. (M)SDR USAA040047Skin · crackedFOUND SKIN CRACKED .5 INCH, AFT SERVICE DOOR LOWER HINGE CUTOUT. CUT OUT DAMAGE AND INSTALLED DUOBLER PER SRM 53-60-01 FIG 208 AND EA 78095. (M)SDR USAASB03223Duct · rupturedFLT DEPARTED WITH LT PACK ON MEL 21-1A. EN ROUTE AT FL250, RT PACK UNABLE TO HOLD CABIN PRESSURE AS CABIN PRESSURE WENT TO 10,000 FT. CREW DESCENDED TO FL200 BUT CABIN PRESSURE WOULD NOT COME DOWN UNTIL 16,000 FT. FLT CONTINUED ON & LANDED WITHOUT FURTHER ISDR USAASB03187Engine · overtempON CLIMB-OUT FROM IAH, EN ROUTE TO PHL, CREW SHUTDOWN THE NR 2 ENGINE DUE TO HIGH OIL TEMPERATURE. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES.SDR USAA030148Skin · crackedCLT - FOUND SKIN CRACKED THREE PLACES, THREE INCH CRACK 1.5 INCHES FORWARD STATION 727E, 1 INCH CRACK AFT OF 727E, .75 INCH CRACK .375 INCH AFT OF 727E. INSTALLED DOUBLER AND TRIPLER AT STATION 727E AT S24R PER SRM 53-00-01 FIG 229. (M)SDR USAASB03086Actuator · leakingSAV - FLT 486 - DURING CLIMBOUT FROM SAV TO CLT, THE A HYD SYS LOW OIL PRESSURE LIGHT ILLUM. FLT CREW NOTED A LOSS OF A HYD SYS QUANTITY. ELEC HYD PUMPS AND NR 1 ENG DRIVEN HYD PUMP WERE SHUTOFF 40 SECONDS AFTER FIRST INDICATION OF SYS LOSS. CREW DECLARED ASDR USAASB03025Module · failedPIT - FLT 553 - EN ROUTE FROM CLT TO CLE, DURING CRUISE, THE 'B' HYDRAULIC SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYSDR USAASB03004Controller · failedPWM - FLT 1528 - EN ROUTE FROM PHL TO PWM, AT FL370, CREW REPORTED THE CABIN ALTITUDE GRADUALLY CLIMBED ABOVE 10,000 FEET. NO FAULT INDICATIONS WERE INDICATED ON PRESSURIZATION PANEL. CREW REGAINED CONTROL OF CABIN DURING DESCENT TO FL250 IN MANUAL AC MODE. SDR USAASB01264Door · not closedBUF - FLT 1105 - ON CLIMB-OUT FROM BUF, EN ROUTE TO PHL, THE CABIN WOULD NOT PRESSURIZE. THE FORWARD MAIN ENTRY DOOR WAS SQUEALING SO THE CREW ELECTED TO RETURN TO FIELD AT BUF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCESDR USAA010470Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH B.25 INCH, BS 1006, LBL 10. REPLACED T-CAP SECTION PER EA 69149A. (M)SDR USAA010459Angle · dentedCLT - FOUND ANGLE DENTED .75 INCH BY .75 INCH, BS 639, LBL 68 AT CREASE BEAM WEB. FABRICATED AND INSTALLED NEW ANGLE PER BOEING DRAWING 69-37422, SRM 51-30-01, 51-40-00 AND 51-40-03. (M)SDR USAA010460Frame · crackedCLT - FOUND FRAME/DOUBLER CRACKED .5 INCH, BS 1104 FRAME AFT SIDE, FORWARD LOWER LEFT HORIZONTAL STABILIZER FIT. INSTALLED REPAIR DOUBLER, FILLERS, SHIMS PER EA 69484 AND SRM 51-70-11. (M)SDR USAA010464Bulkhead · corrodedCLT - FOUND PRESSURE WEB CORRODED 5.5 INCHES BY 1.5 INCHES, BS 1016, BL 0. INSTALLED REPAIR DOUBLER. (M)SDR USAA010465Angle · corrodedCLT - FOUND FAIL/SAFE ANGLE CORRODED .5 INCH BY .5 INCH, BS 767, BETWEEN S27L AND S26L. INSTALLED REPAIR DOUBLER PER SRM 51-20-01, 51-70-11, AND 53-00-07. (M)SDR USAA010469Strap · corrodedCLT - FOUND INNERCHORD STRAP CORRODED 3 SQUARE INCH AREA, BS 794, S20R TO S25R. REMOVED AND REPLACED STRAP, SRM 51-10-2, SRM 51-40-00. (M)SDR USAA010462Frame · corrodedCLT - FOUND FORMER CORRODED 1.5 INCH BY 1 INCH AREA, BS 1016, FRAME BL 0, UNDER FLOOR. INSTALLED REPAIR PLATE, FILLER PER SRM 51-40-02. (M)SDR USAA010463Frame · corrodedCLT - FOUND FORMER CORRODED 1.5 INCH BY 1 INCH, BS 1016, L SIDE OF PRESSURE BULKHEAD BL-0. INSTALLED REPAIR PLATE AND FILLER PER SRM 51-40-02. (M)SDR USAA010468Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .5 INCH, BS 178, WL 234, RBL 8. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND SRM 53-10-08. (M)SDR USAA010467Gusset · crackedCLT - FOUND GUSSET/ANGLE CRACKED 6 INCHES, HORIZONTAL STABILIZER CENTER SECTION, INT SEC OF BEAMS INBOARD SIDE UP CHORD. INSTALLED REPAIR DOUBLER. (M)SDR USAA010466Gusset · crackedCLT - FOUND GUSSET/FITTING CRACKED .5 INCH, HORIZONTAL STABILIZER CENTER SECTION, AFT LEFT INT SECTION OF BEAMS. FABRICATED NEW ANGLE PER BOEING DRAWING 65-47598, INSTALLED PER SRM 51-40-02 AND 03. (M)
Back to N374US, cancelled Mar 16, 2006