Boeing 737-3B7
Service difficulty reports · 4,722
Newest first. General aviation reporting is voluntary.
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.
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
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 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 INSTSDR 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; FABRICATESDR 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 CRACKSDR 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 CHESDR 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 RSDR 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 INSDR USAA020475Skin · crackedSKIN CRACKED, .500 INCH. FORWARD SERVICE DOOR, LOWER AFT CORNER STA 328 SILL PLATE. CUT OUT DAMAGE AND INSTALLED EXTERNAL DOUBLERS IAW SRM.SDR 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 EMSDR 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 EMERGENCYSDR 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 ODSDR 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.SDR USAA020472Frame · crackedHORIZONTAL STABILIZER, LOWER CHORD, 1.5 INCH CRACKED. TRIM OUT AFT SECTION LOWER CHORD AND SPLICE IN NEW SECTION.SDR 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 CAPTASDR USAA020467Skin · damagedRUDDER SKIN DAMAGE. LEFT SIDE TRIM DAMAGE SRM IAW EA.SDR USAA020469Floorbeam · corrodedFLOORBEAM TOP FLANGE LOWER FORWARD SIDE CORRODED.SDR USAA020470Skin · corrodedCORRODED SKIN, LEVEL 1 STA 986 BETWEEN STR S17L-S17R. FILLER AND EXTERNAL DOUBLER INSTALLED IAW SRM.SDR 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)SDR 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)SDR 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)SDR USAA020448Frame · crackedPIT - FOUND FRAME CRACKED .500 INCH LONG, STATION 639 STRINGER 9L. MANUFACTURED AND INSTALLED NEW SECTION PER EA 75051. (M)SDR 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)SDR USAA020450Frame · crackedPIT - FOUND FRAME CRACKED .100 INCH, STATION 639 STRINGER 9R. REMOVED DAMAGED SECTION OF FRAME PER SRM 53-00-01 FIG 101. (M)SDR 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)SDR 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 DSDR 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)SDR 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)SDR 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 FURTHERSDR USAA020443Stringer Clip · damagedPIT - FOUND STRINGER WITH MANGLED CLIP, BS 360 S-11R. INSTALLED REMANUFACTURED BELT FRAME CLIP PER SRM 51-40-02. (M)SDR 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)SDR 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. OPERSDR 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. MAINTENSDR 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. SDR 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)SDR USAA020411Skin · crackedCLT - FOUND SKIN WITH TWO CRACKS 2 INCHES AND .125 INCH, STATION 727E S24R. INSTALLED DOUBLER AND TRIPLER PER EA 86717. (M)SDR USAA020412Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767 S19R. INSTALLED DOUBLER AND TRIPLER PER EA 86718. (M)SDR USAASB02196Charger · inoperativePIT - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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 SDR 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)SDR 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 ASDR 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)SDR USAA020408Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, STATION 807-S9L. DAMAGE CUT OUT AND INSTALLED DOUBLERS PER TYPICAL REPAIR 53-10-20. (M)SDR USAA020395Frame · crackedFRAME CRACKED AT STA 827 BETWEEN STR 8R AND 9R. INSTALLED ANGLE DOUBLERS IAW SRM.SDR 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 A
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