Boeing 737-297
Service difficulty reports · 454
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 = '737297' 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 = '737297' 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 P2EA00378Slat Track · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK. (X)SDR P2EA00405Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 WITH CORROSION OUT OF LIMITS, LENGTH 22 INCHES, WIDTH 2 INCHES, DEPTH .030 INCH. REPAIRED THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 IAW BOEINSDR P2EA00404Stringer · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING NR 2 FUEL TANK UPPER SURFACE STR 13 WBL 135.5 WITH CRACK INDICATION. CONFIRMED CRACK AT THE RIGHT WING NR 2 FUEL TANK UPPER SURFACE STR 13 WBL 135.5 BY HFEC INSPECTION ON 11-18-00. L = 1.250 INCHES. W = 0.001 INCH.SDR P2EA00381Floorbeam · corrodedSJO - DUIRNG Q-CHECK, FOUND THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 WITH CORROSION OUT OF LIMITS. (M)SDR P2EA00399Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD UPPER FUSELAGE WEB AT BS 178 RBL 14 WL 218 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD UPPER FUSELAGE WEB AT BS 178 RBL 14 WL 218 ON 11/19/00. (M)SDR P2EA00400Frame · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 ON 11/19/2000. (M)SDR P2EA00444Frame · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 ON 11/19/00, LENGTH .50 INCH, WIDTH .005. REPLACED THE BULKHEAD LOWER FUSDR P2EA00439Bulkhead · crackedDURING Q CHECK, FOUND BULKHEAD UPPER FUSELAGE WEB AT BS178 RBL14 WL218 WITH CONFIRMED CRACK ON 11/19/00 L/0.750 W/0.005.REPAIRED BULKHEAD UPPER FULELAGE WEB.SDR P2EA00423Skin · crackedDURING Q CHECK, FOUND THE L1 DOOR UPPER HINGE CUT OUT WITH CRACK. L/0.50 W/0.002. REPAIRED THE L1 DOOR UPPER HINGE CUT OUT.SDR P2EA00356Bulkhead · crackedDURNIG Q-CHECK, FUOND THE BULKHEAD WEB AT FS 178 WL 195 BETWEEN LBL 11-14 WITH CRACK. AFTER NDT INSPECTION, CONFIRMED NO CRACK. (M)SDR P2EA00357Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD WEB AT BS 178 WL 226 RBL 5.7 WITH CRACK. AFTER NDT INSPECTION, CONFIRMED NO CRACK. (M)SDR P2EA00365Skin · crackedSJO - DURING Q-CHECK, FOUND THE L-1 DOOR UPPER HINGE CUT OUT WITH CRACK. (M)SDR P2EA00377Support Bracket · crackedSJO - DURING Q-CHECK, FOUND THE L-1 DOOR LOWER AFT SUPPORT WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE L-1 DOOR LOWER AFT SUPPORT IAW BOEING SRM 51-10-1 PAGE 8. (X)SDR P2EA00406Spar · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE CRACKED LENGTH .250 INCH WIDTH .005 INCH. REPLACED THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE IAW BOEING SRM 51-10-1 PAGE 8. (M)SDR P2EA00403Stiffener · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE STIFFENER AT BS 178 RBL 5.5 WL 185 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE STIFFENER AT BS 178 RBL 5.5 WL 185 ON 11/20/00. (M)SDR P2EA00437Stiffener · crackedDURING Q CHECK , FOUND BULKHEAD LOWER FUSELAGE STIFFENER AT BS 178 RBL 5.5 WL 185 WITH CONFIRMED CRACK ON 11/20/00 L/0.750 W/0.005. REPAIRED BULKHEAD LOWER FUSELAGE STIFFENER.SDR P2EA00452Spoiler · delaminatedDURING Q CHECK, FOUND THE LT INBOARD GROUND SPOILER WITH DELAMINATION.L/10.00 W/12.00. REPLACED LT INBOARD GROUND SPOILER.SDR P2EA00419Clip · crackedDURING Q CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 639 STR 2R CRACKED L/0.50 W/0.002. REPLACED CABIN FRAME SUPPORT CLIP AT BS 639 STR 2R.SDR P2EA00436Door Frame · crackedDURING Q CHECK, FOUND L1 DOOR LOWER FORWARD CORNER OF FRAME, CRACKED. L/0.250W/0.005. REPLACED THE L1 DOOR LOWER FORWARD CORNER OF FRAME.SDR P2EA00420Clip · crackedDURING Q CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 616 STR 2L CRACKED L/0.25 W/0.003. REPLACED THE CABIN FRAME SUPPORT CLIP AT BS 616 STR 2L.SDR P2EA00434Skin · crackedDURING Q CHECK FOUND THE LT WING LEADING EDGE SKIN AT FSS 282 WITH CRACK L/0.125 W/0.005.REPAIRED THE LEFT WING LEADING EDGE SKIN AT FSS 282.SDR P2EA00438Stiffener · crackedDURING Q CHECK, FOUND THE BULKHEAD STIFFENER AT BS178 LBL5.5 WL182 CRACKED. REPAIRED BULKHEAD STIFFENER AT BS178 LWL5.5WL182.SDR P2EA00411Angle · crackedDURING Q CHECK, FOUND THE PASSENGER CABIN AT BS 328 LBL 46 WL 202 WITH CRACKED ANGLE. REPLACED PASSENGER CABIN ANGLE AT BS 328 LBL 46 WL 202.SDR P2EA00447Window · crackedDURING Q CHECK, FOUND NR1 WINDOW, LEFT HAND UPPER SIDE CORNER WITH CRACK. L/0.50 W/0.005 REPAIRED THE NR1 WINDOW, LEFT HAND UPPER SIDE CORNER.SDR P2EA00446Window · crackedDURING Q CHECK, FOUND THE NR1 WINDOW, RIGHT HAND UPPER SIDE CORNER WITH CRACK. L/0.50 W/0.005 REPAIRED THE NR1 WINDOW, RIGHT HAND UPPER SIDE CORNER.SDR P2EA00340Window · crackedSJO - DURING Q-CHECK, FOUND THE NR 1 WINDOW RIGHT UPPER SIDE CORNER WITH CRACK. (M)SDR P2EA00341Window · crackedSJO - DURING Q-CHECK, FOUND THE NR 1 WINDOW LEFT UPPER SIDE CORNER WITH CRACK. (M)SDR P2EA00342Angle · crackedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 328 LBL 46 WL 202 WITH CRACKED ANGLE. (M)SDR P2EA00354Stiffener · crackedSJO - DURING Q-CHECK, FOUND THE BULKHEAD STIFFENER AT BS 178 LBL 5.5 WL 182 CRACKED. (M)SDR P2EA00355Spar · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION RSS 205 TRAILING EDGE ANGLE CRACKED. (M)SDR P2EA00358Clip · crackedSJO - DURING Q-CHECK, FOUND THE FRAME SUPPORT CHIP AT BS 663.75 STRINGER 10L WITH CRACK. (M)SDR P2EA00359Skin · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING LEADING EDGE SKIN AT FSS 282 WITH CRACK. (M)SDR P2EA00362Clip · crackedSJO - DURING Q-CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 616 STRINGER 2L CRACKED. (M)SDR P2EA00363Door Frame · crackedSJO - DURING Q-CHECK, FOUND THE L-1 DOOR LOWER FORWARD CORNER OF FRAME CRACKED. (M)SDR P2EA00364Clip · crackedSJO - DURING Q-CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 639 STRIGNER 2R CRACKED. (M)SDR P2EA00366Skin · delaminatedSJO - DURING Q-CHECK, FOUND THE LEFT INBOARD GROUND SPOILER WITH DELAMINATION. (M)SDR P2EA00376Channel · corrodedSJO - DURING Q-CHECK, FOUND THE CABIN FLOOR CHANNEL BETWEEN BS 1006 - BS 1030 BL ZERO HAD CORROSION OUT OF LIMITS. L = 7.00 INCHES. W = 2.00 INCHES. D = 0.040 INCH. REPLACED THE CABIN FLOOR CHANNEL BETWEEN BS 1006 - BS 1030 BL ZERO IAW BOEING SRM 51-10-1 PSDR P2EA00395Frame · crackedSJO - DURING Q-CHECK, FOUND PASSENGER CABIN FRAME INTERNAL FLANGE AT BS 460 BETWEEN STRINGER 13-14R CRACKED, LENGTH 1 INCH, WIDTH .002 INCH. REPAIRED PASSENGER CABIN FRAME INTERNAL FLANGE AT BS 460 BETWEEN STRINGER 13-14R IAW BOEING SRM 53-10-4 FIG 10. (M)SDR P2EA00401Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND THE CABIN FLOORBEAM UPPER FLANGE AT BS 294.5 BETWEEN RBL 10-12 WL 208.5 WITH CORROSION. CONFIRMED CORROSION OUT OF LIMITS AT BS 294.5 BETWEEN RBL 10-12 WL 208.5 ON 11/20/00. (M)SDR P2EA00402Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND THE CABIN FLOORBEAM UPPER FLANGE AT BS 328 BETWEEN RBL 10.75-49 WL 208.5 WITH CORROSION. CONFIRMED CORROSION OUT OF LIMITS AT BS 328 BETWEEN RBL 10.75-49 ON 11/20/00. (M)SDR P2EA00456Channel · crackedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 807 RBL 18 WL 203 WITH CRACKED CHANNEL, LENGTH .500 INCH, WIDTH .005 INCH. REPLACED THE PASSENGER CABIN CHANNEL AT BS 867 RBL 18 WL 203 IAW BOEING SRM 51-10-1 PAGE 8 AND 51-30-2. REF P2EA00344. (M)SDR P2EA00428Floorbeam · corrodedDURING Q CHECK, FORND CABIN FLOOR BEAM UPPER FLANGE AT BS 328 BETWEEN RBL 10.75-49WL 208.5 WITH CORROSION OUT O LIMITS L/40.00W/2.00 D/0.040. REPAIRED CABIN FLOOR BEAM UPPER FLANGE.SDR P2EA00430Floorbeam · corrodedDURING Q CHECK, FOUND CABIN FLOOR BEAM UPPER FLANGE AT BS 294.5 BETWEEN RBL 10,12 WL 208.5 CONFIRMED CORROSION OUT OF LIMITS ON 11/20/00 L/40.00 W/2.00 D/0.074. REPAIRED CABIN FLOOR BEAM UPPER FLANGE.SDR P2EA00429Floorbeam · corrodedDURING Q CHECK, FOUND PASSENGER CABIN FLOOR BEAM, UPPER FLANGE AT BS 334 RBL 11 TO LBL 56 WL 208.5 WITH CORROSION. OUT OF LIMITS11/15/00 L/67.00 W/2.00 D/0.025. REPAIRED PASSENGER CABIN FLOOR BEAM UPPER FLANGE.SDR P2EA00421Web · crackedDURING Q CHECK, FOUND THE CABIN FLOOR BEEM WEB AT BS 312 RBL 1 WL 207 WITH CRACK L/0.50 W/0.005. REPAIRED THE CABIN FLOOR BEEM WEB AT BS 312 RBL 1 WL207.SDR P2EA00432Frame · dentedDURING Q CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME BETWEEN STR 24, 25L BS 807 WITH DENT. L/1.250 W/1.00 D/0.125.REPAIREDAFT CARGO COMPARTMENT FRAME BETWEEN STR 24, 25L BS 807.SDR P2EA00433Frame · dentedDURING Q CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME BETWEEN STR 24,25L BS827 WITH DENT. L/1.OO W/1.00 D/0.125 REPAIRED AFT CARGO COMPARTMENT FRAME BETWEEN STR 24, 25L BS 827.SDR P2EA00417Support Bracket · crackedDURING Q CHECK FOUND THE RT WING AUXILIARY SPAR AREA , UPPER FIXED PANEL SUPPORT ANGLE AT RSS 159 CRACKED L/2.00 W/0.005. REPAIRED RT WING AUXILIARY SPAR AREA UPPER FIXED PANEL SUPPORT ANGLE.SDR P2EA00415Intercostal · crackedDURING Q CHECK, FOUND THE AFT CARGO COMPARTMENT INTERCOSTAL AT BS 727 WL 176.1 LBL 14 CRACKED L/1.00 W/0.004.SDR P2EA00388Channel · crackedDURING Q CHECK FOUND IN AFT CARGO COMPARTMENT AT BS 727, 787 RBL 22 WITH CRACKED CHANNEL L/0.250 W/0.005. REPAIRED AFT CARGO COMPARTMENT AT BS 727,787 RBL22 CHANNEL.
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