Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA002004Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .5 INCH, BS 178, LBL 5, WL 187. INSTALLED DOUBLER PER EA 68549. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002005Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, RBL 5 WL 187. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002006Stringer · crackedCLT - FOUND STRINGER CRACKED, BS 908, STRINGER 4R. INSTALLED STRINGER SPLICE PER SRM 51-40-00. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA002007Intercostal · crackedCLT - FOUND INTERCOSTAL WEB CRACKED 1 INCH, BS 278, STRINGER 14R. INSTALLED NEW INTERCOSTAL WEB PER DWG 65-45807-8. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002010Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 807, ABOVE STRINGER 9L. INSTALLED DOUBLER PER EA 68493. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002011Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 ABOVE STRINGER 9R. INSTALLED DOUBLER PER EA 68493. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002008Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 3 INCHES BY 108 INCHES, STATION 312. INSTALLED T-CAP PER SRM 53-00-51. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002009Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 3 INCHES BY 108 INCHES, STATION 328. INSTALLED T-CAP PER SRM 53-10-05. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAASB00331Windshield · leakingPIT - FLT 338 - DURING CLIMB-OUT FROM PIT, THE FIRST OFFICERS WINDSHIELD SEAL AND SEALANT HAD RUPTURED ON THE UPPER RIGHT CORNER. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. THE FIRST OFFICERS WINDSHIELD HNov 26, 2000 · N506AU · Boeing 7373B7 · Flight Compartment WindowsSDR USAASB00330Windshield · crackedPIT - FLT 1195 - EN ROUTE FROM DCA TO IND, AT FL350, THE FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED AND CONTINUED TO CRACK INTERMITTENTLY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPNov 25, 2000 · N506AU · Boeing 7373B7 · Flight Compartment WindowsSDR USAASB00329Acm · failedPIT - FLT 1217 - ON CLIMB-OUT FROM PIT, EN ROUTE TO IAH, A STRONG SMELL OF BURNING OIL WAS NOTICED IN THE COCKPIT AND CABIN. FLIGHT ATTENDANT REPORTED PASSENGERS WERE COMPLAINING OF EYES BURNING. CREW ISOLATED THE RIGHT PACK AND THE SMELL WENT AWAY. CAPTAINNov 25, 2000 · N508AU · Boeing 7373B7 · Cabin Cooling SystemSDR USAA002113Frame · corrodedPIT - FOUND FRAME CORRODED .010 INCH, FRAME 312 TOP AND BOTTOM. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED TOP CHORD SECTION PER SRM 53-10-51. (M)Nov 25, 2000 · N518AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAASB00325Acm · overservicedPIT - FLT 9550 - AIRCRAFT WAS ON A TEST HOP AFTER A MAINTENANCE CHECK, WHEN JUST AFTER TAKEOFF, A SMALL AMOUNT OF SMOKE WAS NOTED IN THE COCKPIT. FLIGHT RETURNED TO FIELD AT PIT WITHIN MINUTES OF TAKEOFF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYNov 22, 2000 · N376US · Boeing 7373B7 · Cabin Cooling SystemSDR USAA001979Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, FS 663.75 AT CUTOUT FOR NR 1 STRINGER. INSTALLED REPAIR PER SRM 53-00-07 FIG 207 SHT 6. (M)Nov 22, 2000 · N376US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002119Angle · crackedPIT - FOUND CHORD ANGLE CRACKED 2 INCHES, RIGHT CHORD ANGLE AT RWL 207 ON 178 BULKHEAD. CUT OUT CRACKS AND INSTALLED DOUBLER PER SRM 53-10-07 204. (M)Nov 22, 2000 · N391US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002121Angle · crackedPIT - FOUND CHORD ANGLE CRACKED 2 INCHES, LEFT CHORD ANGLE AT LWL 207 ON 178 BULKHEAD. CUT OUT DAMAGED AND INSTALLED DOUBLER PER SRM 53-10-08 FIG 204. (M)Nov 22, 2000 · N391US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002120Angle · crackedPIT - FOUND CHORD ANGLE CRACKED 2 INCHES, WL 184 BL 0 AFT SIDE. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-10-08. (M)Nov 22, 2000 · N391US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001975Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 664 RBL 40 WL 203 UPPER PRESS DECK OF MLG WW. INSTALLED DOUBLER PER T/R 53-60-04. (M)Nov 19, 2000 · N387US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001977Skin · crackedCLT - FOUND CARGO SKIN 2.5 INCH CRACKED, BS 664 LBL 32 WL 203 UPPER PRESS DECK OF MLG W/W. INSTALLED DOUBLER PER TR 53-60-04. (M)Nov 19, 2000 · N387US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001973Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .75 INCH, BS 178 WL 207 LBL 24. INSTALLED AND SPLICED IN NEW SECTION OF CHORD ANGLE PER EA 68503/EO 5300V157. (M)Nov 19, 2000 · N387US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001974Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, STATION 178 WL 234 LBL 10. INSTALLED DOUBLER AND FILLER PER SRM 53-10-08, PAGE 269 DETAIL 11 PAGE 266A. (M)Nov 19, 2000 · N387US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001976Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .75 INCH, BS 178 WL 207 RBL 24. INSTALLED NEW CHORD ANGLE AND SPLICED AT CUT PER EO 5300V157 AND EA 68503. (M)Nov 19, 2000 · N387US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001947Skin · delaminatedPIT - FOUND RUDDER DELAMINATED IN 7 AREAS, LEFT AND RIGHT RUDDER SKIN DELAMINATE 1ST LAYER. 200-230 DEGREE CURE. WET LAY UP REPAIR USING 51-70-17 THEN BALANCED PER 51-60-00 AND EA 56867. (M)Nov 18, 2000 · N376US · Boeing 7373B7 · Rudder, Plate/SkinSDR DL733002247Seal · obstructedMASTER CAUTION (DOORS) LIGHT ILLUMINATED ON TAKEOFF. REMOVED BAG FROM C-2 CARGO DOOR. DOOR INDICATION SYSTEM CKS NORMAL.Nov 18, 2000 · N947WP · Boeing 7373B7 · Door Warning SystemSDR USAASB00315Adc · failedCLT - FLT 230 - AT ROTATION, THE FIRST OFFICERS ALTIMETER AND AIRSPEED INDICATOR FAILED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR DATA COMPUTER. FUNCTIONALNov 15, 2000 · N514AU · Boeing 7373B7 · Air Data ComputerSDR AWXA0000874Floorboard · corrodedCORROSION AROUND AND BENEATH FASTENERS IN CREASE BEAM STA 727D STR 17R. REMOVED FLOORBOARD AND WEB, FABRICATED WEB AND INSTALLED IAW SRM 51-40-02 & 53-60-13 FIG 1.Nov 15, 2000 · N328AW · Boeing 7373B7 · Fuselage Floor PanelSDR USAA001926Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, LBL 24. REPAIRED SRM 53-10-08 FIG 207. (M)Nov 13, 2000 · N387US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001927Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 179, RBL 28, WL 207. INSTALLED NEW WEB PER EA 68503. (M)Nov 13, 2000 · N387US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001939Mount · corrodedCLT - FOUND LEFT STAB MOUNT CORRODED 1 INCHES, FORWARD FACE OF LOWER BOLT HOLE FORWARD FORK STAB CENTER SECTION. INSTALLED BUSHING PER SRM 55-10-10. (M)Nov 13, 2000 · N521AU · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA001938Angle · corrodedCLT - FOUND Z-ANGLE CORRODED, STATION 312-344. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)Nov 13, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001920Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, ABOVE STRINGER 9L, STATION 767. REMOVED DAMAGED AND INSTALLED WITH DOUBLER PER TR 53-10-14. (M)Nov 9, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001880Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 178, WL 207, RBL 26. INSTALLED NEW CHORD SECTION PER EA 68397. (M)Nov 7, 2000 · N389US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001881Bulkhead · crackedCLT - FOUND WEB CRACKED .25 INCH, BS 178, WL 234, RBL 10.3. INSTALLED DOUBLER PER SRM 53-10-11. (M)Nov 7, 2000 · N389US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAASB00308Actuator · leakingCLT - FLT 1975 - ON DESCENT INTO CLT, FROM ROC, SYSTEM A HYDRAULIC QUANTITY DROPPED TO ONE-THIRD. FLUID WAS NOTICED ON TOP OF THE LEFT WING. CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED NORMALLY TO THE GATE. MAINTENANCE JACNov 4, 2000 · N371US · Boeing 7373B7 · Drag Control ActuatorSDR USAA002107Bracket · crackedPIT - FOUND ANGLE BRACKET CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 8 AND 9 RT OVERHEAD PIN ATT PT. INSTALLED .045 INCH ANGLE COUPLER PER US AIRWAYS TYPICAL REPAIR 53-10-14. (M)Nov 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001878Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, BS 291 BETWEEN STRINGER 11R AND 12R. INSTALLED NEW ANGLE PER SRM 51-40-02. (M)Nov 3, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR DL733002158Oven · inoperativeA/C DIVERTED INTO DENVER FOR ODOR IN AFT CABIN. REPLACED AFT GALLEY LEFT OVEN.Nov 3, 2000 · N947WP · Boeing 7373B7 · Buffet/GalleysSDR USAA001860Stiffener · crackedCLT - FOUND STIFFENER CRACKED .5 INCH, BS 178, WL 184, LBL 5.7. SPLICED IN NEW CHORD PER SRM 53-10-08. (M)Nov 2, 2000 · N389US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001863Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED, STRINGER 8L, BS 727B. REPAIRED PER DWG 65 46596. (M)Nov 2, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001852Bulkhead · crackedCLT - FOUND SKIN CRACKED .25 INCH, STATIN 178, BULKHEAD, WL 234, RBL 10.3. REMOVED DAMAGE AND FABRICATED REPAIR PER SRM 53-10-11. (M)Nov 1, 2000 · N389US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001838Web · crackedCLT - FOUND WEB CRACKED .25 INCH, HORIZONTAL WEB JUST FORWARD STATION 639, STRINGER 17L CREASEBEAM. INSTALLED DOBLER PER SRM 51-70-13. (M)Nov 1, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001836Frame · crackedCLT - FOUND L-CHORD CRACKED 1 INCH, STATION 178, LBL 26, WL 207 AND WL 195. SPLICED IN NEW CHORD SECTION EA 68321. (M)Oct 31, 2000 · N389US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001834Frame · crackedTPA - FOUND FORWARD CARGO DOOR CRACKED .50 INCH, FORWARD CARGO DOOR FRAME JUST BELOW LOWER LATCH ROLLER. INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. (M)Oct 31, 2000 · N390US · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA001828Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED 3 INCHES, STATION 540, STRINGER 22L RAM AIR INLET SUPPORT ANGLE. INSTALLED DOUBLER PER TR 53-50-03. (M)Oct 26, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA001949Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, FORWARD S/E DOOR SKIN LOWER HINGE RADIUS INTO DRAIN TABLE. INSTALLED DOUBLER REPAIR AND ROUTED OUT DAMAGE PER SB 737-52-1096 AND EA 56696. (M)Oct 25, 2000 · N518AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA001948Angle · corrodedPIT - FOUND Z AND L ANGLES CORRODED 1 INCH BY 12 INCHES, UNDER FORWARD SERVICE DOOR SIL TOP ALL Z-ANGLE/INBOARD L ANGLE. CORROSION LEVEL 1, TASK NR C53-107-01. Z-ANGLE CLEANED, TREATED AND PAINTED; L ANGLE REPLACED PER SRM 51-10-02, REMOVED AND REPLACED ON LOct 25, 2000 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002108Fitting · corrodedPIT - FOUND FITTINGS CORRODED .75 INCH BY 1 INCH, STRINGER FITTINGS STATION 1016 STRINGER 23L, 24L, 25L. CORROSION LEVEL 1 TASK NR C53-701-01. CLEANED CORROSION, TREATED AND PRIMED. (M)Oct 25, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA002110Ring · corrodedPIT - FOUND DOME SUPPORT RING CORRODED .5 INCH BY 1.5 INCH, STATION 1016 DOME SUPPORT RING 23R-21R AND 18R-8R. CLEANED CORROSION, TREATED AND PRIMED PER 51-20-02. (M)Oct 25, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002112Beam · corrodedPIT - FOUND BEAM CORRODED .008 INCH DEEP, BETWEEN BEAM 328-344 UNDER PANEL 8. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED INTERCOSTAL PER BOEING DWG 65-45834. (M)Oct 25, 2000 · N518AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAASB00301Charger · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE COCKPIT, RIGHT INTERIOR LIGHT OVER SERVICE DOOR AND PASSENGER DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIOOct 25, 2000 · N395US · Boeing 7373B7 · Emergency Lighting
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