Boeing 737-4B7

Service difficulty reports · 5,757

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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 aircraft_model_key = '7374B7'
  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 USAASB01082Wire · damagedLGA - MAINTENANCE FOUND THE TWO ESCAPE PATH EMERGENCY LIGHTS MOUNTED ON THE FORWARD COAT CLOSET INOPERATIVE. MAINTENANCE REPAIRED WIRES IN THE FORWARD COAT CLOSET. OPERATIONAL CHECK GOOD. (M)Mar 16, 2001 · N434US · Boeing 7374B7 · Light System WiringSDR USAASB01073Relief Valve · failedPHL - FLT 2178 - EN ROUTE FROM PHL-NAS, CLIMBING THROUGH FL140, THE PRESSURIZATION SYSTEM WENT TO STANDBY MODE. CABIN ALTITUDE CLIMBED TO 14,000 FEET AND THE OXYGEN MASKS DEPLOYED. PRESSURIZATION WAS CONTROLLABLE. CREW ACCOMPLISHED CHECKLIST AND CLOSED OUTFMar 4, 2001 · N775AU · Boeing 7374B7 · Cabin Pressure Control SystemSDR USAASB01070Power Supply · failedTPA - MAINTENANCE FOUND THE AFT RIGHT INTERIOR OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY ASSEMBLY FOR THE AFT RIGHT INTERIOR OVERWING EXIT SIGN. OPS CHECK GOOD. (M)Mar 1, 2001 · N432US · Boeing 7374B7 · Emergency LightingSDR USAA010195Floorbeam · corrodedCLT - FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, STATION 967, LBL 16. CORROSION LEVEL 1. REPLACED T-CAP PER TR 53-10-05A. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010194Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 380, LBL 12, 28 RBL 12, 18 33. CORROSION LEVEL 1. REPLACED T-CAP, FILLER, SHIMS, ANGLES PER SRM 53-10-51. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010193Floorbeam · corrodedCLT - FOUND FLOORBEAM FLANGE CORRODED 1 INCH BY 2 INCHES, 6 PLACES, BS 344, BL 0, RBL 12, 18, 33, 40, 54, LBL 12, 28. INSTALLED REPAIR ANGLE AND T-CAP PER SRM 53-10-51 FIG 205. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010192Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 5 INCHES, BETWEEN STATION 294 AND 344, LBL 60. REPLACED Z-ANGLE PER SRM 51-10-2. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010197Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178 WL 188, RLB .5. INSTALLED DOUBLER PER EA 69140. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010191Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 907 RIGHT SIDE BETWEEN STRINGER 8R/9R. TRIMMED OUT DAMAGE PER TR 53-10-14. (M)Feb 28, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010219Frame · crackedCLT - FOUND FRAME CRACKED .80 INCH, BS 480 BETWEEN STRINGER 8/9 LEFT AT INBOARD RIVET. INSTALLED DOUBLER PER TYP REP 53-10-14. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010218Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480 BETWEEN STRINGER 8/9 LT. FRAME REPAIRED PER SRM 53-10-14. INSTALLED DOUBLER. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010217Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .375 INCH, BS 178, WL 213, RBL 6 STRAP. INSTALLED DOUBLER PER EO 5300V153 AND SRM 53-10-08 FIG 211. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010216Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .375 INCH, BS 178, WL 213, LBL 6. INSTALLED DOUBLER PER EO 5300V153/SRM 53-10-08 FIG 211. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010215Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .125 INCH, STATION 178, WL 206, RBL .5 AFT SIDE. INSTALLED DOUBLER PER EO 5300V153/SRM 53-10-08 FIG 211. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010214Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 201, RBL 6 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MK 90-93852). (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010213Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178, WL 201, LBL 5 AFT SIDE. INSTALLED DOUBLER PER EA 69140. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010212Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .375 INCH, BS 178, LBL 4, WL 200. INSTALLED DOUBLER PER EO 5300V153/SRM 53-10-08 FIG 211. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010211Bulkhead · crackedCLT - FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 198.5, RBL 6 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MK 90-93852). (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010210Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .125 INCH, STATION 178, WL 198.5, LBL 5 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MK 90-938-52). (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010209Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .5 INCH, STATION 178, WL 198, RBL 4.5 AFT SIDE. INSTALLED DOUBLER PER EA 69140 (MC 90-93852). (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010208Bulkhead · crackedCLT - FOUND FORWARD PRESSURE BULKHEAD CRACKED .25 INCH, STATION 178, WL 188, LBL .5, RBL .5 AFT SIDE. INSTALLED DOUBLER PER EA 69140. (M)Feb 27, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAASB01064Engine · overheatedCLT - FLT 1883 - ON CLIMB-OUT FROM CLT, EN ROUTE TO GCM, THE NR 1 ENGINE EGT REACHED 931 DEGREES WITH N1 CLIMB LIMIT. POWER WAS REDUCED TO MAINTAIN WITHIN LIMITS, BUT NR 1 ENGINE RAN APPROX 100 DEGREES GREATER THAN NR 2 ENGINE. FLIGHT RETURNED TO CLT AND LANFeb 27, 2001 · N446US · Boeing 7374B7 · Engine (Turbine/Turboprop)SDR USAA010280Strap · crackedCLT - FOUND STRAP CRACKED .875 INCH, BS 300 STRINGER 10L. REPLACED CRACKED STRAP PER SRM 51-40-00, 51-40-02. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010181Frame · crackedCLT - FOUND INNER CHORD OF FRAME CRACKED .5 INCH, BS 601 BELOW STRINGER 17L CREASEBEAM BOTTOM RIVET. REPLACED REPAIR ANGLE AND FILLER PER TR 53-62-01 AND EA 69176. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010180Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, STATION 328 LOWER AFT DOOR CUTOUT RADIUS. INSTALLED REPAIR DOUBLER PER SRM 53-10-01. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA010179Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 380 BETWEEN STRINGER 8-9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010178Angle · crackedCLT - FOUND ANGLE CRACKED .25 INCH, APPROX STATION 289 FORWARD SERVICE DOOR STRUCTURE. REPLACED ANGLE PER SRM 51-10-02. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010177Intercostal · crackedCLT - FOUND WEB INTERCOSTAL CRACKED .25 INCH, STATION 277.5 AT FORWARD SERVICE DOOR. REPLACED INTERCOSTAL PER SRM 51-10-02. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010173Pressure Panel · crackedCLT - FOUND PRESSURE DECK 1 INCH, BS 664, LBL 32, WL 202. INSTALLED DOUBLER PER TR 53-60-04. (M)Feb 26, 2001 · N432US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010185Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 907, BETWEEN STRINGER 8/9L. DOUBLER REPAIR PER SRM 53-10-14. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010184Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727F RT SIDE BETWEEN STRINGER 8/9R. REPAIRED DOUBLER PER TR 53-10-14. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010183Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED .25 INCH, BS 727B BETWEEN STRINGER 8 AND 9L. REPAIRED DOUBLER PER TR 53-10-14. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010182Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED 1 INCH, BS 664, LBL 32. INSTALLED DOUBLER AND STIFFENER PER TR 53-60-04 FIG 1. (M)Feb 26, 2001 · N435US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAASB01057Regulator · failedORD - FLT 916 - ON CLIMB-OUT FROM ORD, EN ROUTE TO CLT, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CAPTAIN TRIED TO RESET THE NR 2 ENGINE BLEED TRIP WITH NO HELP, AS LIGHT REMAINED ILLUMINATED. CABIN PRESSURE STARTED TO CLIMB WITH THE AIRCRAFT, SO THE CAPFeb 24, 2001 · N427US · Boeing 7374B7 · Pneumatic Distribution SystemSDR USAASB01058Fan · failedORF - FLT 888 - EN ROUTE FROM PBI TO PHL, CRUISING AT FL290, FUMES WERE NOTICED FOLLOWED BY SMOKE ORIGINATING AT ROW 23 NEAR THE OVERHEAD. CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT AS SMOKE AND HAZE CLEARED. AIRCFeb 24, 2001 · N783AU · Boeing 7374B7 · Air Distribution FanSDR USAASB01053Switch · faultyCLT - FLT 540 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A FORWARD LEADING EDGE SLAT INDICATION ALONG WITH A NR 3 SLAT OVERHEAD INTRANSIT LIGHT. CREW RECYCLED FLAPS TO FLAPS 1 PER CHECKLIST WITH NO HELP. FLIGHT RETURNED TO FIELD AT CLT AND LNDED WITH FLAP SETTINFeb 21, 2001 · N775AU · Boeing 7374B7 · Leading Edge Slat Position Indicating SystemSDR USAA010227Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, BS 178, RBL 5.7, WL 180 AFT SIDE. INSTALLED DOUBLER PER SRM 51-40-02. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010226Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, STATION 178 AT WL 207 LEFT SIDE CHORD. INSTALLED DOUBLERS PER EO 5300V157. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010225Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, RIGHT SIDE CHORD STATION 178 WL 207. INSTALLED DOUBLERS PER EA 68929/EO 5300V157. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010239Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 4 INCHES BY 27 INCHES, STATION 967-944 FLOOR LEVEL AFT ENTRY DOORWAY. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)Feb 21, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010233Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1.5 INCH, STATION 294.5, 12 INCHES LEFT OF CENTER. FILLED VOID WITH SEALANT PER EA 69083. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010232Angle · corrodedCLT - FOUND CHORD CORRODED 13 INCHES, LEFT Z-ANGLE. REPLACED ANGLE CHORD PER SRM 51-10-02. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010231Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 907 BETWEEN STATION 9L AND 8L. INSTALLED DOUBLER PER T/R 53-10-14. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010230Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 867 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER T/R 53-10-14. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010229Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER TR 53-10-14. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010228Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 747 BETWEEN STATION 9R AND 8R. INSTALLED DOUBLER PER T/R 53-10-14. (M)Feb 21, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010241Floorbeam · corrodedCLT - FOUND CORROSION 3 INCHES BY 108 INCHES, STATION 986.5 LBL 54 TO RBL 54. SPLICED IN NEW T-CAP PER TYP REP 53-50-01. CORROSION LEVEL 1. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010245Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 827 BETWEEN STATION 8/9 LEFT. INSTALLED DOUBLER PER TYP REP 53-10-14. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010244Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 787 FRAME RT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TYP REP 53-10-14. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010243Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FRAME 747 RIGHT BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TYP REPAIR 53-10-14. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Frame
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