Boeing 737-247
Service difficulty reports · 1,009
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 = '737247' 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 = '737247' 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 P2EA00154Beam · crackedSJO - DURING C-CHECK, FOUND CABIN STUB BEAM WEB AT BS 616 FROM RBL 45 TO RBL 56 BETWEEN WL 208 AND WL 200 HAS CRACK. L = 0.373 INCH. W = 0.0005 INCH. REPAIRED STUB BEAM AT BS 616 FROM RBL 45 TO RBL 56 BEWEEN WL 208 AND WL 200 IAW BOEING SB 737-53-1061 REV 4SDR P2EA00155Beam · crackedSJO - DURING C CHECK, FOUND CABIN STUB BEAM WEB AT BS 639 FROM RBL 45 TO RBL 56 BETWEEN WL 208 AND WL 200 HAS CRACK. L = 0.373 INCH, W = O.0005 INCH. REPAIRED CABIN STUB BEAM WEB AT BS 639 FROM RBL 45 TO RBL 56 BETWEEN WL 208 AND WL 200 IAW BOEING SB 737-53-SDR P2EA00144Floorbeam · corrodedSJO - DURING C-CHECK, CORROSION ON FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 12 AND LBL 19. REPAIRED FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 41 AND RBL 21 IAW SRM 53-10-9 FIG 5. SEE COOPESA W/O N10316-1-241, VAM100 NR 780 AND 912SDA123. (X)SDR P2EA00158Skin · crackedSJO - DURING C-CHECK, FOUND EXT FUSELAGE SKIN AT BS 727A BETWEEN STR 20R AND STR 21R WITH CRACK. L= 0.250 INCH. W = 0.005 INCH. REPAIRED EXT FUSELAGE SKIN AT BS 727A BETWEEN STR 20R AND STR 21R IAW COOPESA EO NR COO-3-53-278-00 DATED APRIL 29, 2000, AND BOSDR P2EA00143Frame · misdrilledSJO - DURING C-CHECK, FRAME LOWER FLANGE WITH DOUBLE DRILLED HOLE AT BS 907 BETWEEN STRINGERS 26L AND 27L. REPAIRED FRAME LOWER FLANGE AT BS 907 BETWEEN STRINGERS 26L AND 27L IAW SRM 53-10-4 FIG 6 SHEET 3. SEE COOPESA W/O N10316-1-240, VAM100 NR 744 AND 912SDR P2EA00171Channel · corrodedSJO - DURING C-CHECK, FOUND FUSELAGE FLOOR SUPPORT CHANNEL FROM BS 1006 BS 1016 BETWEEN BL ZERO AND LBL 10 WITH CORROSION. REPAIRED FUSELAGE FLOOR SUPPORT CHANNEL FORM BS 1006 - BS 1016 BETWEEN BL ZERO AND LBL 10 IAW COOPESA EO NR COO-3-53-246-00 DATED APRILSDR P2EA00142Skin · canningSJO - DURING C-CHECK, APU DOOR SKIN OIL CANNED AT BS 1116, WL 223. REPAIRED APU DOOR SKIN FROM BS 1112 TO BS 1120 AND FROM BS 1135 TO BS 1145 IAW SRM 52-00-3 FIG 6. SEE COOPESA W/O N10316-3-59, VA100 NR 747 AND 912SDA122. (X)SDR P2EA00148Skin · delaminatedSJO - DURING C-CHECK, FOUND THE RIGHT AIR CONDITION BAY DOOR INNER SKIN WITH DELAMINATION. L = 120.0 INCHES, W = 12.0 INCH. REPAIRED RIGHT HAND AIR CONDITION BAY DOOR INNER SKIN IAW COOPESAE E.O. NR COO-IMP-3-53-272-00 DATED 4-29-00. DOCUMENTED ON FAA FORMSDR P2EA00156Frame · crackedSJO - DURING C-CHECK, FOUND FUSELAGE FRAME AT FORWARD CARGO BS 500 STR 26R WITH CRACK L = 1.125 INCHES, W= 0.005 INCH. REPAIRED FUSELAGE FRAME AT FORWARD CARGO BS 500 STR 25-278R IAW SRM 51-40-3 FIG 1. SEE COOPESA WO NR N10316-1-231 AND VAM 100-0745. (X)SDR DL73K000747Controller · noisyAUDIBLE RUMBLE WHEN ADDING POWER AS A/C POSITIONED RUNWAY. CYCLED ENGINE BLEEDS AND RUMBLE STOPPED. ON CLIMBOUT RUMBLE RETURNED AT CLIMB POWER. RUMBLE DIDN''T RETURN DURING DESCENT APPROACH AND LANDING. NO FLIGHT CONTROL PROBLEMS. INSPECTED A/C VISUALLY, SDR P2EA00172Structure · crackedSJO - DURING C-CHECK, FOUND FORWARD CARGO DOOR, AFT LOWER CORNER WITH CRACK. L = 0.437 INCH. REPAIRED FORWARD CARGO DOOR, AFT LOWER CORNER IAW COOPESA EO NR COO-3-52-286-00 DATED MAY 2, 2000, AND BOEING FAX NR COO-SJO-00-00463H DATED MAY 2, 2000, DOCUMENTED SDR P2EA00121Skin · crackedSJO - DURING C-CHECK, SKIN DOUBLER CRACKED AT BS 727 PLUS 19 BETWEEN 15R AND 16R. REPAIRED FUSELAGE SKIN FROM BS 727 PLUS 13 BS 727A PLUS 7, BETWEEN 15R AND 17R IAW SRM 53-30-3, FIG 6. (M)SDR P2EA00122Skin · delaminatedSJO - DURING C-CHECK, FOUND CORROSION AT BS 350, BETWEEN 25L AND 26L AND SKIN DELAMINATED. REPAIRED SKIN FROM BS 350 TO BS 352 AND BETWEEN 25L AND 26L IAW SRM 53-30-3, FIG 17 SHEET 6. CORROSION WITHIN LIMITS IAW SRM 51-10-6 PAGE 12. (M)SDR P2EA00125Skin · misrepairedSJO - DURING C-CHECK, REPAIR NOT IAW SRM BETWEEN BS 500B AND BS 520 ON STR 21L. REPAIRED STR 21L BETWEEN BS 500+3 AND BS 500+15 INCHES IAW SRM 53-10-3, FIG 1. SEE COOPESA W/O N10316-1-211 VAM100 NR 696 AND 912SDA112. (X)SDR P2EA00160Floorbeam · crackedSJO - DURING C-CHECK, FOUND FLOORBEAM LOWER CHORD BS 677, RBL 45.5 WL 202, WITH CRACK. L = 2.50 INCHES. W = 0.005 INCH. REPAIRED FLOORBEAM LOWER CHORD BS 677, RBL 45.5 WL 202, IAW BOEING FAX NR COO-SJO-00-00404H, DATED APRIL 21, 2000, DOCUMENTED ON FAA FORMSDR P2EA00123Frame · crackedSJO - DURING C-CHECK, FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME AT BS 787 BETWEEN STRINGERS 11L AND 14L IAW SRM 53-10-4, FIG 1. SEE COOPESA W/O N10316-2-194, VAM100 NR 613 AND 912SDA116. (X)SDR P2EA00124Floorbeam · corrodedSJO - DURING C-CHECK, CORROSION ON TOP OF FLOORBEAM AT BS 312 BETWEEN LBL 1 AND RBL 8. REPAIRED FLOORBEAM UPPER CHORD AT BS 312 FROM LBL 26 TO RBL 45 IAW SRM 53-10-9, FIG 5. SEE COOPESA W/O N10316-2-224, VAM100 NR 642 AND 912SDA111. (X)SDR P2EA00138Keelbeam · crackedSJO - DURING C-CHECK, KEEL BEAM CORRODED AND CRACKED AT BS 720, WL 148 AND LBL 5. REPAIRED KEEL BEAM LOWER CHORD BETWEEN BS 704 AND BS 727+4 IAW COOPESA E.O. COO-3-53-249-00, DATED 4-25-00. SEE COOPESA W/O N10316-1-178, VAM100 NR 538, 912SDA144, COOPESA E.O. SDR P2EA00139Bulkhead · crackedSHO - DURING C-CHECK, NOSE WHEELWELL AFT BULKHEAD WEB CRACKED AT BS 294.5, RBL 7.5 AND WL 165. REPAIRED WEB AT BS 294.5 FROM RBL 7.5 TO LBL 6.12, BETWEEN WL 173 AND WL 150 IAW SB 737-53-1079 REV 3, SECTION III FIG 3. SEE COOPESA W/O N10316-1-194, VAM100 NR 5SDR P2EA00140Frame · crackedSJO - DURING C-CHECK, FRAME CRACKED AT BS 597, STR 17L. REPAIRED STR 17L AT BS 597 BETWEEN STR 15L AND WING CHORD IAW SB 737-53-1061 REV 4 SECTION III PART III. SEE COOPESA W/O N10316-2-199, VAM100 NR 618, 912SDA140 AND BOEING SB 737-53-1061 DATED 7-16-92. SDR P2EA00141Frame · crackedSJO - DURING C-CHECK, FRAME CRACKED AT BS 597 STR 17R. REPAIRED FRAME FROM STR 15R TO WING CHORD IAW SB 737-53-1061 REV 4 SECTION III PARA II. SEE COOPESA W/O N10316-2-201, VAM100 NR 620, 912SDA125 AND BOEING SB 737-53-1061 DATED 7-16-92. (X)SDR P2EA00149Stringer · crackedSJO - DURING C-CHECK, FOUND STR 16R BETWEEN BS 500A AND BS 500B WITH CRACK L = 0.375 INCH. REPAIRED STR 16R BETWEEN BS 500A AND BS 500B IAW BOEING SB-737-53-1142 SECT III. (X)SDR 20000727AP001Valve · openFLT 67 - MIA-MGA - ON CLIMB, FUEL HEAT VALVE OPENED, UNABLE TO CLOSE. AC RETURNED TO MIA 30 MIN AFTER TAKEOFF. CONFIRMED DEFECT, VALVE PLACE DON MEL 73-2, FUEL HEAT VALVE ORDERED. (M)SDR P2EA00120Skin · dentedSJO - DURING C-CHECK, FOUND L1 DOOR SKIN DENTED BETWEEN NR 8 BEAM AND BOTTOM. REPAIRED L1 DOOR BETWEEN NR 8 BEAM AND BOTTOM AND FROM BS 339 TO BS 348 IAW SRM 52-00-3 FIG 6. (M)SDR P2EA00167Doubler · crackedSJO - DURING C-CHECK, FOUND RIGHT HAND NR 3 WINDOW LOWER FORWARD CORNER CUT-OUT DOUBLER WITH CRACK. REPAIRED RIGHT HAND NR 3 WINDOW LOWER FORWARD CORNER CUT-OUT DOUBLER IAW BOEING SB 737-53-1023 REV 11 DATED MAY 16, 1991 SECTION III PART II. SEE COOPESA WO NSDR P2EA00113Skin · canningSJO - DURING C-CHECK, R1 DOOR SKIN OIL-CANNED BETWEEN BEAM 47 AND BEAM NR 8. REPAIRED DOOR SKIN FROM BS 323 TO BS 337 AND BETWEEN BEAM NR 6 AND BEAM NR 9 IAW 52-00-03, FIG 6. (X)SDR P2EA00135Skin · dentedSJO - DURING C-CHECK, R2 DOOR SKIN DENTED BETWEEN BEAM NR 5 AND LOWER BEAM. REPAIRED DOOR SKIN FROM BS 968 TO BS 978 BETWEEN BEAM NR 5 AND LOWER BEAM IAW SRM 52-00-3, FIG 6. SEE COOPESA W/O N10316-2-149, VAM100 NR 426 AND 912SDA145. (X)SDR P2EA00136Frame · dentedSJO - DURING C-CHECK, FRAME DENTED AT BS 420 BETWEEN STRINGERS 22L AND 25L. REPAIRED FRAME AT BS 420 BETWEEN STRINGERS 20L AND 25L IAW SRM 51-40-3, FIG 1. SEE COOPESA W/O N10316-1-123, VAM100 NR 450, AND 912SDA146. (X)SDR P2EA00137Shear Tie · crackedSJO - DURING C-CHECK, FRAME SHEAR TIES CRACKED AT BS 294.5 BETWEEN STRINGERS 10L AND 12L. REPAIRED FRAME AT BS 294.5 BETWEEN STRINGERS 10L AND 12L IAW SRM 53-10-4, FIG 10. SEE COOPESA W/O N10316-2-171, VAM100 NR 531 AND 912SDA121. (X)SDR P2EA00153Frame · dentedSJO - DURING C-CHECK, FOUND THE FORWARD CARGO FRAME AT BS 400 BETWEEN STR 20 AND STR 25L WITH DENT. L = 2.0 INCHES. W = 0.100 INCH. REPAIRED DENT AT FORWARD CARGO FRAME AT BS 400 BETWEEN STR 20 AND STR 25L IAW SRM 51-40-3 FIG 1. REPLACED CLIPS BETWEEN STR SDR P2EA00117Skin · crackedSJO - DURING C-CHECK, L2 DOOR LOWER HINGE SKIN CRACKED. REPAIRED L2 DOOR FROM BS 995 O BS 963, BETWEEN NR 6 BEAM AND NR 8 BEAM IAW SRM 52-00-3, FIG 6. (X)SDR P2EA00173Skin · delaminatedSJO - DURING C-CHECK, FOUND THE LEFT AILERON FORWARD OUTBOARD LOWER SURFACE WITH DELAMINATED. REPAIRED THE LEFT AILERON FORWARD OUTBOARD LOWER SURFACE IAW BOEING SRM 51-40-6 PAR 11. (M)SDR P2EA00165Skin · damagedSJO- DURING C-CHECK, FOUND FUSELAGE SKIN FROM BS 260.5 - BS 269.5, STR 23 - STR 26L, WITH TEMP REPAIR. REPAIRED FUSELAGE SKIN FROM BS 260.5 - BS 269.5, STR 24 - STR 25L IAW COOPESA EO NR COO-3-53-266-00 DATED APRIL 27, 2000, AND BOEING FAX NR COO-SJO-00-00424SDR P2EA00127Skin · damagedSJO - DURING C-CHECK, TEMPORARY SKIN REPAIR INSTALLED AT BS 205 TO BS 213, BETWEEN WL 173 AND WL 183. REPAIRED FUSELAGE SKIN FROM BS 205 TO BS 216, BETWEEN WL 173 AND WL 186 IAW COOPESA E.O. COO-3-53-226-00 DATED 4-18-00. SEE COOPESA W/O N10316-1-6, VAM100 SDR P2EA00128Bulkhead · dentedSJO- DURING C-CHECK, DENT ON BULKHEAD WEB AT BS 294, WL 184 AND RBL 3.5. REPAIRED DENT AT BS 924 BETWEEN RBL 2 AND RBL 5 AND FROM WL 187.1 TO WL 182.1 IAW SRM 51-40-2, FIG 1. SEE COOPESA W/O N10316-1-22, VAM100 NR 109 AND 912SDA132. (X)SDR P2EA00129Skin · crackedSJO - DURING C-CHECK, LEFT WING L/E SKIN CRACKED AT WS 295.1 AND WS 299.1. REPAIRED L/E SKIN FROM WS 293.407 TO WS 338.407 IAW SRM 57-30-4, FIG 5. SEE COOPESA W/O N10316-5-17, VAM100 NR 138 AND 912SDA143. (X)SDR P2EA00130Frame · dentedSJO - DURING C-CHECK, FRAME DENTED AND CORRODED AT BS 500 BETWEEN STRINGERS 24R AND 26R. REPAIRED FRAME AT BS 500 BETWEEN STRINGERS 23R AND 25R IAW SRM 51-40-3, FIG 1. SEE COOPESA W/O N10316-1-47 VAM 100 NR 210 AND 912SDA120. (X)SDR P2EA00131Frame · corrodedSJO - DURING C-CHECK, CORROSION ON FRAME AT BS 500B BETWEEN STRINGERS 25R AND 26R. REPAIRED FRAME AT BS 500B BETWEEN STRINGERS 25R AND 27R IAW SRM 51-40-3, FIG 1. COOPESA W/O N10316-1-50, VAM100 NR 213 AND 912SDA142. (X)SDR P2EA00132Frame · dentedSJO - DURING C-CHECK, FRAME DENTED AT BS 500B BETWEEN STRINGERS 22R AND 25R. REPAIRED FRAME AT BS 500B BETWEEN 22R AND 25R IAW SRM 51-40-3, FIG 1. SEE COOPESA W/O N10316-1-52, VAM100 NR 215 AND 912SDA141. (X)SDR P2EA00152Frame · dentedSJO - DURING C-CHECK, FOUND THE FORWARD CARGO FRAME AT BS 500A BETWEEN STR 21 AND STR 25L WITH DENT. L = 2.0 INCHES. W = 0.750 INCH. REPAIRED DENT AT FORWARD CARGO FRAME AT BS 500A BETWEEN STR 21 AND STR 25L IAW SRM 51-40-3 FIG 1. SEE COOPESA WO NR N10316-SDR DL73E000711Skin · crackedTHE LOWER FWD CORNER OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN ASSY AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN ALL MEMBERS AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER B737 SRM 53-30SDR DL73E000710Skin · crackedTHE LOWER AFT CORNER OF THE FWD GALLEY DOOR CUTOUT (R1) WAS FOUND WITH A TYPICAL CRACK IN THE SKIN ASSY. THE UNDERLYING BEARSTRAP WAS NOT CRACKED. THE CRACK WAS ROUTED OUT WITH A 1 INCH CUTOUT AND REPAIRED WITH TWO INCH EXTERNAL ALUMINUM DOUBLERS PER B737 SRSDR P2EA00174Skin · wornSJO - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SKIN WBL 191-205 HAS WEAR BEYOND LIMITS. REPAIRED THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SIN WBL 191-205 IAW BOEING FAX NR COO-SJO-00-00439H DATED APR 27, 2000. (M)SDR P2EA00175Skin · wornSJO - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SKIN WBL 409-394 HAS WEAR BEYOND LIMITS. REPAIRED THE RIGHT OUTBOARD FOREFLAP INBOARD LEADING EDGE SKIN WBL 409-394 IAW BOEING FAX NR COO-SJO-00-00439H DATED APR 27, 2000. (M)SDR P2EA00176Rib · crackedSJO - DURING C-CHECK, FOUND THE NR 6 SLAT OUTBOARD SLIDING RAIL BEARINGS SUPPORT RIB WBL 523.5 CRACKED. REPAIRED THE NR 6 SLAT OUTBOARD SLIDING RAIL BEARINGS SUPPORT RIB WBL 523.5 CRACKED IAW COOPESA EO NR COO-3-57-287. (M)SDR P2EA00114Skin · dentedSJO - DURING C-CHECK, SKIN DENTED AT BS 402, STR 23R. REPAIRED FUSELAGE SKIN FROM BS 396 TO BS 408.5 BETWEEN STR 22R AND STR 24R IAW SRM 53-30-03 FIG 6. (X)SDR P2EA00133Stringer · crackedSJO - DURING C-CHECK, STR 26L CRACKED BETWEEN BS 727A, AND BS 727B. REPAIRED STR 26L BETWEEN BS 727+16 AND BS 717A+17 IAW SRM 53-10-3, FIG 1 DETAIL V. SEE COOPESA W/O N10316-1-69, VAM100 NR 292 AND 912SDA115. (X)SDR P2EA00134Stringer · corrodedSJO - DURING C-CHECK, CORROSION ON STR 27L SPLICE BETWEEN BS 907 AND BS 927. REPAIRED STR 27L BETWEEN BS 870 AND BS 993 AND SPLICE BETWEEN BS 900 AND BS 914 IAW SRM 53-10-3, FIG 1 AND SRM 51-10-1 PAGE 5. SEE COOPESA W/O N10316-1-72, VAM100 NR 295 AND 912SDA1SDR P2EA00150Structure · damagedSJO - DURING C-CHECK, FOUND THE CARGO DOOR FORWARD LOWER CORNER WITH CRACK. L = 3.00 INCHES. W= 0.005 INCH. REPLACED THE AFT CARGO DOOR FORWARD LOWER FRAME AND PERFORMED PREVENTIVE MODIFICATION ON LOWER AND UPPER CROSS BEAM IAW BOEING SB 737-52A1079 REV 6 DSDR P2EA00151Fitting · damagedSJO - DURING C-CHECK, FOUND THE RIGHT OUTBOARD MID-FLAP INBOARD CARRIAGE SUPPORT FITTING BEARING RETENTION HOLES ELONGATED. W = 0.382 INCH/0.322 INCH. REPAIRED THE RIGHT OUTBOARD MID-FLAP INBOARD CARRIAGE SUPPORT FITTING IAW COOPESA EO NR COO-3-57-270-00 DAT
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