Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA960127Floor Beam · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB CUT OUT FOR LEFT AILERON BELLCRANK (1 INCH CRACK), BS 680 LBL 24 AND RBL 24 WEB OF FLOOR BEAM AT AILERON CUTOUT. INSTALLED REINFORCEMENT. REPAIRED PER EA 40739 AND SB 737-53-1130, R 4 FIG 5. (M)SDR USAA960126Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION FLOOR BEAM STATION 312, LBL 11 TO RBL 11. REPLACED T-CAP. REPAIRED PER TR 53-10-13. (M)SDR USAA960125Frame · damagedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BLEND OUT AFT CARGO FORWARD FRAME BS 794 STRINGER 19R THROUGH STRINGER 20R. INSTALLED DOUBLER. REPAIRED PER SRM 51-40-3. (M)SDR USAA960124Floor Beam · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB 4 INCHES AT FLOOR BEAM, BL O, STATION 706-710. CUTOUT CRACKED WEB AND INSTALLED FILLER AND DOUBLER. REPAIRED PER BOEING REPAIR DRAWING NR 65C34537. (M)SDR USAA960123Channel · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 307 LBL 11 TO LBL 42 AT CHANNEL. REPLACED CHANNEL. REPAIRED PER SRM 51-10-01. (M)SDR USAA960122Chord · chaffedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 17 INCHES BY 2 INCHES CHAFFED AND FRETTING LEFT CHORD BS 710 TO BS 727. FABRICATED WASHERS AND STRAP AND INSTALLED. REPAIRED PER EA 40745. (M)SDR USAA960121Frame · crackedINT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 616, 5 INCHES FLOOR LEVEL RIGHT SIDE FRAME. CUT OUT DAMAGE INSTALLED ANGLE AND FILLER. REPAIRED PER EA 40740. (M)SDR USAA960120Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION STATION 308 LBL 24 TO LBL 30 ANGLE AT BULKHEAD. REPLACED ANGLE, REPAIRED PER SRM 51-10-01. (M)SDR USAA960119Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION FLOOR BEAM FS 328 RBL 20 1/2. REMOVED DAMAGED 'T' CHORD FROM LBL 29 TO RBL 65. REPAIRED PER TYPICAL REPAIR NR 53-10-13 AND SRM CHAPTER 51-40-2 FIG 1. CORROSION TASK NR C53-107-02, CORSDR USAA960118Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT FRAME BS 616, 5 INCHES BELOW FLOOR LEVEL LEFT SIDE. CUT OUT DAMAGE, INSTALLED ANGLE AND FILLER. REPAIRED PER EA 40740. (M)SDR USAA960117Tie Clip · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP, STATION 1064 STR 9 L. REPLACED CRACKED TIE CLIP WITH ONE FABRICATED PER ORIG DRAWING. REPAIRED PER BOEING DRAWING 69-40276. (M)SDR USAA960115Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION PIT, TOP CAP FLOOR BEAM, STATION 328 AT RBL 20. REMOVED TOP 'T' OF FLOOR BEAM AND INSTALLED NEW T-CAP. REPAIRED PER TYPICAL REPAIR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LESDR USAA960114Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1875 INCH BY 3 INCH AND .1875 INCH BY 2 INCH CORROSION AT CABIN FLOOR SUPPORT ANGLE, BS 292 THROUGH BS 300. REPLACED SUPPORT ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (SDR USAA960113Floor Beam · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 520 LBL 25 WL 207.75 UPPER CHORD FLOOR BEAM. STOP DRILLED CRACK .25 INCH. INSTALLED REPAIR DOUBLER AND FLOOR BEAM MOD. REPAIRED PER EA 40741. (M)SDR USAA960112Tie Clip · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 47. REPLACED TIE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35353-14. (M)SDR USAA960111Tie Clip · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 6R. REPLACED TIE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M)SDR USAA960110Intercostal · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION INTERCOSTAL STATION 927 TO STATION 947 RBL 8 INCH. INSTALLED NEW INTERCOSTAL. REPAIRED PER DRAWING 65-67316. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960109Tie Clip · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER TIE CLIP, STATION 1064 STRINGER 17L. INSTALLED NEW TIE CLIP MFG PER BOEING DRAWING 69-40276. REPAIRED PER BOEING ASSEMBLY DRAWING 69-40276. (M)SDR USAA960108Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CORROSION ON BEAM AT BS 277-294.5 LBBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960107Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION AT CABIN FLOOR SUPPORT ANGLE, STATION 292 TO STATION 300 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAASB96009Windshield · crackedFLT NR 1080 - PIT - DIVERTED TO PIT, FLIGHT OFFICERS WINDSHIELD CRACKED IN FLIGHT. MAINTENANCE REPLACED FLIGHT OFFICERS COCKPIT WINDSHIELD. (M)SDR USAASB96006Wire · brokenFLT NR 1635 - PHL - UNSCHEDULED MAINTENANCE FOR CEILING EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED WIRE ON CENTER OVERHEAD CEILING LIGHT. EMERGENCY LIGHTS OPS CHECK NORMAL. (M)SDR USAASB96003Outflow Valve · stuckCLT - FLT 521 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. STOPPED AT 8,000 FEET ABOVE AGL, THEN RETURNED TO CLT. ON DESCENT AT 2,000 FEET, AIRCRAFT STARTED TO PRESSURIZE. MAINTENANCE REPLACED OUTFLOW VALVE DUE TO STICKING. OPS CHECKED OK. (X)SDR USAA960054Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREA ON INTERCOSTAL .5 INCH BY .25 INCH AT BS 986 TO BS 1006 APPROXIMATELY LBL 18 INCHES. REPLACED WITH IDENTICAL PART NR 1121963. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSSDR USAA960053Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 21 INCHES CORRODED AREA AT FLOOR BEAM BS 947 RBL 10 TO LBL 11. REPAIRED T-CAP. REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M)SDR USAA960052Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 38 INCHES IN LENGTH UPPER FLANGE CABIN FLOOR BEAM BS 967 LBL 10-RBL 28. INSTALLED T-CAP REPAIR. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)SDR USAA960051Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SPOTS OF CORROSION AT FLOOR BOARD BEAM ATTACH HOLES BS 986.5 LBL 18 TO RIGHT END. INSTALLED REPLACEMENT T-CAP. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M)SDR USAA960050Tie Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 616, STRINGER 2L TIE CLIP. INSTALLED NEW TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA960049Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, AT BS 639 STRINGER 6R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960048Frame · crackedINT - DURING Q-5 CHECK, EDDY CURRENT FOUND .5 INCH CRACK AT BS 400 STRINGER 25L TO STRINGER 26L. INSTALLED DOUBLER, REPAIRED PER EA 40544. (M)SDR USAA960047Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 597 RIGHT FRAME OUTBOARD FLANGE RADIUS JUST ABOVE CENTER WING. REMOVED AND REPLACED FRAME PER DRAWING 65-46538. NO WEIGHT CHANGE. (M)SDR USAA960046Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 RIGHT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING. INSTALLED FILLER AND REPAIR ANGLE. REPAIRED PER EA 40570. (M)SDR USAA960045Floor Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS RBL 25 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707-708, WL 203 AT FASTENER HOLES. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960044Floor Beam · crackedINT -DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BL 0 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707 WL 203 AT FASTENER HOLE. INSTALLED DOUBLER, REPAIRED PER BOEING REF DRAWING 65C34537. (M)SDR USAA960043Inner Chord · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 LEFT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING. INSTALLED FILLER AND ANGLE. REPAIRED PER EA 40570. (M)SDR USAA960042Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5R TIE CLIP, BS 727 B. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960041Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 10R TIE CLIP AT BS 747. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960040Clip · crackedDURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 3L, BS 747 AT STRINGER TIE CLIP. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960039Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 7R TIE CLIP, BS 727B. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960038Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 6L TIE CLIP, BS 727B. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960037Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CLIP AT BS 727A. REPLACED CLIP, REPAIRED PER EO NR 5394G227. (M)SDR USAA960036Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3R TIE CLIP AT BS 706. REPLACED CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960035Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP, BS 727 B. REPLACED TIE CLIP, REPAIRED PER EO NR 5393G227. (M)SDR USAA960034Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP BS 685. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960033Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER 3R TIE CLIP, AT BS 685. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960032Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, .1250 INCH CRACK IN STRINGER 2R TIE CLIP, AT BS 685. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960031Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CIP, BS 685. REPLACED TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA960030Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3L TIE CLIP, AT BS 685. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960029Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 827 STRINGER 10R. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960028Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 807, STRINGER 10R. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)
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