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 AWXA200201261Angle · crackedLCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE UNDERSIDE RADIUS OF FLOOR BEAM SUPPORT ANGLE BS 540, BL "O". MAINTENANCE REMOVED CRACKED FLOOR BEAM SUPPORT ANGLE AT BS 540, BL "0"; FABRICATED A NEW REPLACEMENT FLOOR BEAM SUPPORT ANGLE; AND INSTDec 14, 2002 · N328AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200201260Skin · crackedLCQ - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND ON LOWER AFT INNER SKIN OF L-1 DOOR ON INBOARD SIDE. MAINTENANCE REMOVED CRACKED ANGLE AND STOP DRILLED CRACK ON INNER SKIN; HFEC INSPECTION WAS ACCOMPLISHED TO VERIFY CRACK WAS CONTAINED; FABRICATEDec 13, 2002 · N328AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA200201252Skin · crackedLCQ - MAJOR REPAIR - DURING C-11 CHECK 2 CRACKS WERE FOUND ON THE R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 300. MAINTENANCE STOP DRILLED CRACKS ON R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 300; PERFORMED HFEC INSPECTION TO VERIFY THE CRACKDec 13, 2002 · N328AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02221Indicator · failedCAE - FLT 489 - ON DESCENT INTO CLT FROM ATL, THE ATTITUDE FLAG IN THE CAPTAIN'S ADI CAME IN TO VIEW. FLIGHT DIVERTED TO CAE AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S ADI. OPERATIONAL CHEDec 12, 2002 · N523AU · Boeing 7373B7 · Integrated Flight SystemSDR AWXA200201259Angle · crackedLCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND AROUND FASTENER HOLE OF CABIN FLOOR SUPPORT ANGLE BETWEEN BS 500D AND BS 500E AT BL "0". MAINTENANCE REMOVED DAMAGE ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 500D AND BS 500E AT BL "0"; FABRICATED 3 EACH RDec 12, 2002 · N328AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200201251Floor Support · corrodedLCQ - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND AROUND 3 FASTENER HOLES ON FLOOR SUPPORT AT BS 995 - 1006, LBL 13. MAINTENANCE REMOVED THE DAMAGED FLOOR SUPPORT AT BS 995 - 1006, LBL 13; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INDec 12, 2002 · N328AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA020475Skin · crackedSKIN CRACKED, .500 INCH. FORWARD SERVICE DOOR, LOWER AFT CORNER STA 328 SILL PLATE. CUT OUT DAMAGE AND INSTALLED EXTERNAL DOUBLERS IAW SRM.Dec 10, 2002 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02218Transceiver · malfunctionedCLT - FLT 502 - ON CLIMB-OUT FROM CLT, CREW LOST ALL COMMUNICATIONS. UNABLE TO COMMUNICATE WITH ATC ON ANY RADIO. MIC'S WERE UNPLUGGED AND CHECKED. COMM 2 STARTED TO WORK ON 121.5. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMDec 8, 2002 · N532AU · Boeing 7373B7 · Audio Integrating SystemSDR USAASB02219Jackscrew · lack of lubeAFTER TAKEOFF, THE LEADING EDGE FLAPS WOULD NOT RETRACT. CREW WENT THROUGH SEVERAL PROCEDURES BUT THE FLAPS STILL WOULD NOT RETRACT FROM THE 2 DEGREE POSITION. FLIGHT RETURNED TO THE FIELD WITH A 15 DEGREE FLAP LANDING WITHOUT FURTHER INCIDENT. NO EMERGENCYDec 8, 2002 · N389US · Boeing 7373B7 · Leading Edge Slat Control SystemSDR USAASB02217Valve · stuckAFTER LIFTOFF, THE FORWARD LAVATORY SMOKE DETECTOR BEGAN SOUNDING. AN ELECTRICAL ODOR WAS ALSO NOTED COMING FROM THE FORWARD LAVATORY. CREW PULLED THE CIRCUIT BREAKERS FOR THE WATER HEATER IN THE FORWARD LAVATORY AND THE SMOKE ALARM STOPPED SOUNDING. THE ODDec 7, 2002 · N512AU · Boeing 7373B7 · Cabin Temperature Control SystemSDR USAA020474Skin · crackedSKIN, 2 INCH CRACK, 3 INCHES BELOW PREVIOUS PATCH AT WING EMERGENCY LIGHT. CUT OUT DAMAGE, INCORP ENTIRE AREA INTO ONE EXTERIOR DOUBLER/TRIPLER REPAIRED IAW EA.Dec 1, 2002 · N395US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020472Frame · crackedHORIZONTAL STABILIZER, LOWER CHORD, 1.5 INCH CRACKED. TRIM OUT AFT SECTION LOWER CHORD AND SPLICE IN NEW SECTION.Nov 30, 2002 · N504AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAASB02213Computer · malfunctionedDTW - FLT 503 - ON TAKEOFF ROLL, THE AUTO THROTTLE DISCONNECTED AND WOULD NOT REENGAGE UNTIL AFTER TAKEOFF. THEN ON CLIMB OUT, AFTER GEAR RETRACTION, THE FIRST OFFICERS AIRSPEED INDICATION BECAME ERRONEOUS INDICATING APPROXIMATELY 60 KNOTS LESS THAN THE CAPTANov 28, 2002 · N523AU · Boeing 7373B7 · Airspeed/Mach IndicatorSDR USAA020467Skin · damagedRUDDER SKIN DAMAGE. LEFT SIDE TRIM DAMAGE SRM IAW EA.Nov 27, 2002 · N504AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA020469Floorbeam · corrodedFLOORBEAM TOP FLANGE LOWER FORWARD SIDE CORRODED.Nov 27, 2002 · N504AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA020470Skin · corrodedCORRODED SKIN, LEVEL 1 STA 986 BETWEEN STR S17L-S17R. FILLER AND EXTERNAL DOUBLER INSTALLED IAW SRM.Nov 27, 2002 · N504AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020464Skin · crackedPIT - FOUND SKIN CRACKED 2 INCHES, RIGHT SIDE STATION 727E STRINGER 24 RT. CUTOUT DAMAGE, INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 225. (M)Nov 21, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020446Frame · crackedPIT - FOUND FRAME CRACKED .250 INCH, STATION 663 AND STRINGER 2L. REMOVED DAMAGED FRAME SECTION, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS PER SRM 53-00-07, EA 75. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020447Frame · crackedPIT - FOUND FRAME CRACKED .100 INCH LONG, STATION 663 STRINGER 3L. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-00-07, EA 75015. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020448Frame · crackedPIT - FOUND FRAME CRACKED .500 INCH LONG, STATION 639 STRINGER 9L. MANUFACTURED AND INSTALLED NEW SECTION PER EA 75051. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020449Angle · crackedPIT - FOUND ANGLE CRACKED .250 INCH LONG, FRAME TO SKIN ANGLE, STATION 616 BETWEEN STRINGER 8L AND 7L. FABRICATED NEW ANGLE PER BOEING DWG, HEAT TREATED AND INSTALLED PER DWG NR 66-24124. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA020450Frame · crackedPIT - FOUND FRAME CRACKED .100 INCH, STATION 639 STRINGER 9R. REMOVED DAMAGED SECTION OF FRAME PER SRM 53-00-01 FIG 101. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020451Angle · crackedPIT - FOUND ANGLE CRACKED 26 INCHES, RBBL 57 STATION 580-608 LOWER FUSELAGE SKIN. REMOVED AND REPLACED DAMAGED ANGLE PER SRM 51-40-02. (M)Nov 10, 2002 · N384US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB02204Controller · failedCLT - FLT 1279 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MKE, CREW REPORTED THE CABIN ALTITUDE WARNING HORN SOUNDED PASSING THROUGH FL030. FLIGHT RETURNED TO FIELD AT CLT. SHORTLY AFTER BEGINNING DESCENT, CABIN ALTITUDE RETURNED TO NORMAL. NO OXYGEN MASKS WERE DNov 9, 2002 · N395US · Boeing 7373B7 · Cabin Pressure ControllerSDR USAA020444Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH CRACK, STATION 727D, STRINGER S23L. CRACKED REMOVED AND SKIN DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-03. (M)Nov 5, 2002 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020445Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH, STATION 727D, STRINGER S23R. CRACK REMOVED AND SKIN DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-03. (M)Nov 5, 2002 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02200Hydraulic Line · leakingCLT - FLT 794 - AFTER TAKEOFF AND GEAR RETRACTION FROM CLT, EN ROUTE TO SYR, CREW REPORTED THE LOSS OF SYSTEM 'A' HYDRAULICS DURING FLAP RETRACTION FROM 5 UNITS TO 1 UNIT. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHERNov 3, 2002 · N389US · Boeing 7373B7 · Hydraulic System, MainSDR USAA020443Stringer Clip · damagedPIT - FOUND STRINGER WITH MANGLED CLIP, BS 360 S-11R. INSTALLED REMANUFACTURED BELT FRAME CLIP PER SRM 51-40-02. (M)Nov 2, 2002 · N532AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA020452Floor Support · damagedPIT - FOUND BEAM WITH ELONGATED HOLES, STATION 980 LBBL 18-30. REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH LIKE P/N PER SRM 51-40-02. (M)Nov 2, 2002 · N384US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB02198Battery Pack · dischargedPIT - DURING WEEKLY CHECK, WHILE ACCOMPLISHING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN/AFT SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERNov 2, 2002 · N391US · Boeing 7373B7 · Emergency LightingSDR USAASB02197Odor · detectedLGA - FLT 370 - ON TAKEOFF FROM PIT, EN ROUTE TO LGA, CREW REPORTED A STRONG BURNED OIL SMELL AT THE FORWARD LEFT ENTRY DOOR AND AT THE AFT LEFT ENTRY DOOR. SMELL DISSIPATED DURING FLIGHT. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT LGA. MAINTENNov 1, 2002 · N517AU · Boeing 7373B7 · Air Distribution SystemSDR DL733021289Seal · tornAFTER LEVELING AT FL350 MASTER CAUTION W/OVERHEAD ON THE MASTER CAUTION PANEL ILL. PASS. O2 LIGHT ON THEOVERHEAD WASILL. CABIN ALT. WAS AT 15,000FEET. FA CONFIRMED MASKS HAD DROPPED. AUTO FAIL LIGHT WAS ILL. BUT NO ALT. ALERT HORN HADSOUNDED. ALT. CONT. Nov 1, 2002 · N947WP · Boeing 7373B7 · Pneumatic SystemSDR USAA020413Skin · crackedPIT - FOUND SKIN CRACKED 1.25 INCH LONG, STATION 380 B/L 0. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 75219C. (M)Oct 31, 2002 · N511AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020411Skin · crackedCLT - FOUND SKIN WITH TWO CRACKS 2 INCHES AND .125 INCH, STATION 727E S24R. INSTALLED DOUBLER AND TRIPLER PER EA 86717. (M)Oct 30, 2002 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020412Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767 S19R. INSTALLED DOUBLER AND TRIPLER PER EA 86718. (M)Oct 30, 2002 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02196Charger · inoperativePIT - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Oct 28, 2002 · N528AU · Boeing 7373B7 · Emergency LightingSDR USAASB02195Battery Pack · dischargedIND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 17 LEFT THROUGH 22 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND RELAMPED THE LIGHTS. OPERATIONAL CHECK GOOD. (M)Oct 28, 2002 · N506AU · Boeing 7373B7 · Emergency LightingSDR USAA020406Stringer · crackedCLT - FOUND STRINGER CRACKED .375 INCH, STATION 663.75 STRINGER 2 RIGHT. CUT OUT DAMAGE, INSTALLED DOUBLERS PER EA 75013, SRM 53-00-07. (M)Oct 28, 2002 · N384US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020409Skin · crackedPIT - FOUND SKIN CRACKED 2.4375 INCH, RIGHT SIDE STATION 727E AT STRINGER 18 RIGHT. SKIN DOUBLER INSTALLED PER SRM 53-00-01, FIG 201. (M)Oct 28, 2002 · N389US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020433Keelbeam · crackedPIT - FOUND KEEL BEAM CRACKED 2 INCHES LONG AND PROGRESSIVE FORWARD, LEFT KEEL BEAM, AFT STRINGER 540. REPAIRED PER TYPICAL REPAIR 53-60-09. (M)Oct 28, 2002 · N384US · Boeing 7373B7 · Fuselage Main, KeelSDR USAASB02193Charger · failedPIT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Oct 25, 2002 · N514AU · Boeing 7373B7 · Emergency LightingSDR USAA020402Skin · delaminatedPIT - FOUND RUDDER WITH DELAMINATION, STATION 0.00 RT, 1.5 LEFT, 121.0 LEFT, 174.9 RT, 200.0 RT. REPAIRED WITH WET LAYUP USING SRM 51-70-17, 51-60-00 PER EA 75136. (M)Oct 25, 2002 · N395US · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA020407Clip · crackedPIT - FOUND CLIPS CRACKED .375 INCH, IN TIE CLIPS 360 AND 380, 8 LEFT. SPLICED IN STRINGER AND REPLACED TIE CLIPS PER SRM 53-00-03 FIG 203. (M)Oct 25, 2002 · N384US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR DL733021238Bulkhead · crackedFUSELAGE / BULKHEAD / FS 178 / SIDE CHORDS, FLOOR WEBS, & VERTICAL BEAM CHORDS : CRACK REPAIRS INSPECTION OF THE FS 178 BULKHEAD REVEALED CRACKS IN THE LBL & RBL VERTICAL BEAM CHORDS AT WL 184 AND CRACKS IN THE LH & RH SIDE CHORDS Oct 25, 2002 · N947WP · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA020403Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH LONG, STATION 380 B/L 0. INSTALLED REPAIR DOUBLER PER EA 75166 AND TYPICAL REPAIR 53-30-07. (M)Oct 24, 2002 · N514AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR DL733021237Floorbeam · corrodedTHE FS 967 & 986.5 PASSENGER FLOORBEAMS WERE FOUND WITH SEVERAL AREAS OF CORROSION ON THE UPPER CAPS OF THE BEAMS. THE UPPER CAPS WERE TRIMMED OFF TO REMOVE THE CORROSION. NEW EXTRUDED CAP SECTIONS WERE INSTALLED TO REPAIR THE AREAS PER ER/A 383998-14, REV AOct 23, 2002 · N947WP · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA020410Skin · crackedPIT - FOUND SKIN CRACKED 1.24 INCH, RIGHT SIDE STATION 747 AT STRINGER 18 RIGHT. SKIN DOUBLER INSTALLED PER SRM 53-00-01, FIG 201. (M)Oct 21, 2002 · N389US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020408Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, STATION 807-S9L. DAMAGE CUT OUT AND INSTALLED DOUBLERS PER TYPICAL REPAIR 53-10-20. (M)Oct 20, 2002 · N384US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020395Frame · crackedFRAME CRACKED AT STA 827 BETWEEN STR 8R AND 9R. INSTALLED ANGLE DOUBLERS IAW SRM.Oct 14, 2002 · N532AU · Boeing 7373B7 · Fuselage Main, FrameSDR DL733021199Spar · crackedINSPECTION OF THE MLG BEAM ATTACH FITTINGS AND REAR SPAR ON THE LT WING REVEALED 6 HOLES COMMON TO THE FITTINGS AND SPAR WITH CRACK INDICATIONS. ADDITIONAL HOLES WERE DAMAGED OR ELONGATED DURING REWORK OF AREA. THE HOLES WERE OVERSIZED TO REMOVE ALL CRACKS AOct 14, 2002 · N951WP · Boeing 7373B7 · Wing Spar
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