Boeing 737-247
Service difficulty reports · 1,009
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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 = '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 DL73K002049Landing Gear · lack of lubeDURING AFTER T/O CHECKLIST GEAR HANDLE PLACED TO OFF, HEARD A THUMP AND GOT A LEFT GEAR GREEN AND RED LIGHT. LEFT GEAR DOWN AND DIVERTED TO BOSTON. JACKED A/C, SWUNG GEAR SEVERAL TIMES AND ALL INDICATIONS NORMAL. FOUND NOSE GEAR LOCKING ARM MAKING LOUD BANGSDR DL73K002035Hydraulic Line · rupturedSHIP 363 FLIGHT 2131 ARRIVED EWR AT 2353E. DURING TAXI TO TERMINAL CREW NOTICED A SYSTEM HYDRAULIC QUANTITY DEPLETED. FOUND BRAIDED HYDRAULIC LINE WITH PINHOLE LEAK. LINE IS LOCATED IN AFT SECTION OF NOSE WHEEL WELL. REPLACED HYDRAULIC LINE.SDR DL73K002014Tire · failedNR 1 TIRE BLEW ON LANDING. SPEED 142 KTS, AUTOBRAKES MEDIUM. AUTOBRAKE DISARM LIGHT W/OUT CREW INTERVENTION. REPLACED NR 1 AND NR 2 WHEEL ASSYS PER M/M. INSPECTED BRAKE, GEAR AND AIRCRAFT. NO DAMAGE FOUND. DEFERRED ANTI SKID SYSTEM.SDR P2EA00314Stringer · damagedDURING Q CHECK FOUND THE FUSELAGE STRINGER 24R BETWEEN BS 294.5 AND BS 328 WITH ELONGATED HOLES. REPLACED THE FUSELAGE STRINGER 24R BETWEEN BS 294.5 AND BS 328 IAW BOEING SRM 53-10-3 FIG 1SDR P2EA00305Floorbeam · crackedDURING Q CHECK FOUND THE PAX CABIN FLOORBEAM WEB AT BS 312 BETWEEN RBL 8 AND RBL 18 WITH CRACK L=0.50 W=0.002. REPAIRED THE PAX CABIN FLOORBEAM WEB AT BS 312 BETWEEN RBL 8 AND RBL 18 IAW BOEING FAX COO-SJO-OO-1175H DATED OCT 13, 2000 DOCUMENTED ON FAA FORM 8SDR P2EA00302Floorbeam · crackedDURING Q CHECK FOUND THE PAX CABIN FLOORBEAM WEB AT BS312 BETWEEN RBL 5 AND REL 14 WITH CRACK L=0.75 W=0.002. REPAIRED THE PAX CABIN FLOORBEAM WEB AT BS312 BETWEEN RBL 5 AND RBL 14 IAW BOEING FAX COO-SJO-OO-01182H DATED OCT 17, 2000 DOCUMENTED ON FAA FORM 81SDR P2EA00322Panel · delaminatedDURING Q CK FOUND LT WING AFT PYLON ACCESS PANEL AT WBL 191 WITH DELAMINATION L=12.0 IN, W=10.0 INREPLACED LEFT WING AFT PYLON PANEL AT WBL 9=191 IAW COOPESA EO#COO-CMP-3-57-633-00 DATED OCT 9, 2000 DOCUMENTED ON FAA FORM 8110-3 APPROVED AND SUBMITTED BY FAA DSDR P2EA00339Doubler · crackedSJO - DURING Q-CHECK, FOUND DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CONTROL QUADRANT AT BS 678 LBL 24.82 CRACKED. L = 1.00 INCH. W = 0.002 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPLACED DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CONSDR P2EA00300Lap Joint · crackedSJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE LAP JOINT UPPER ROW AT BS 749L STR 25L WITH CRACK INDICATION. REPAIRED THE LOWER FUSELAGE LAP JOINT UPPER ROW AT BS 749L STR 25L IAW BOEING SRM 53-30-3 FIG 13. (X)SDR P2EA00299Lap Joint · crackedSJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE LAP JOINT UPPER ROW BETWEEN BS 478 - BS 480L STR 19L WITH CRACK INDICATION. REPAIRED THE LOWER FUSELAGE LAP JOINT UPPER ROW BETWEEN BS 478 - BS 480L STR 19L IAW BOEING SRM 53-30-3 FIG 14. (X)SDR COOSDR000009Lap Joint · crackedFUSELAGE SKIN, STA 749, STR 25L, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR 20001129SH026Lap Joint · crackedFUSELAGE SKIN, STA 948, STR 25R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000007Lap Joint · crackedFUSELAGE SKIN, BETWEEN STA 478 TO STA 480, STR 19L, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000006Lap Joint · crackedFUSELAGE SKIN, STA 500B, STR 19R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000005Lap Joint · crackedFUSELAGE SKIN, BETWEEN STA 306 TO STA 311, STR 24R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR DL73E001979Actuator · failedDURING APP WHEN FLAPS 2 SELECTED L/E FLAP TRANS LIGHT STAYED ILLUM AND 4 SLAT SHOWED UNSAFE YELLOW ON OVHD PANEL FLAPS WERE SELECTED TO 5 AND ALL WENT GREEN AND SHOWED SAFE. ABOUT 5 SECS LATER L/E FLAP TRANS LIGHT REILLUM AND 4 SLAT SHOWED UNSAFE AGAIN. FLASDR P2EA00338Doubler · crackedSJO - DURING Q-CHECK, FOUND DOUBLER ON PREVIOUS REPAIR ON FLOORBEAM AT AILERON CONTROL QUADRANT AT BS 678 RBL 24.82 CRACKED. L = 1.00 INCH. W = 0.002 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPLACED DOUBLER ON PREVIOUS REPAIR FLOORBEAM AT AILERON CONTROSDR P2EA00309Frame · crackedDURING Q CHECK FOUND THE FUSELAGE FRAME WEB AT BS 260L, LBL 19 WL 276 WITH CRACK L=1.00 W=0.002. REPAIRED THE FUSELAGE FRAME WEB AT BS260L, LBL 19"WL276 WITH CRACK L=1.00" W+0.002" IAW 51-40-2 FIG 1SDR P2EA313Floorbeam · corrodedDURING Q CHECK FOUND THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS 947 LBL 45 WITH CORROSION LEVEL 2. REPAIRED THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS947 LBL45 IAW BOEING FAX COO-SJO-00-01194H DATED OCT 19, 2000 AND COOPESA EO COO-3-53-636-00 DATED OCT 20, SDR P2EA00313Floorbeam · corrodedDURING Q CHECK FOUND THE FAX CABIN FLOORBEAM UPPER SURFACE AT BS 947 LBL45 WITH CORROSION LEVEL 2. REPAIRED THE PAX CABIN FLOORBEAM UPPER SURFACE AT BS947 LBL 45 IAW BOEING FAX COO-SJO-00-01194H DATED OCT 19, 2000 AND COOPESA EA#COO-3-53-636-00 DATED OCT 20, SDR P2EA00308Frame · crackedDURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R WITH CRACK L=1.00 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R IAW BOEING SRM 53-10-4 FIG 1SDR P2EA00307Frame · crackedDURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R WITH CRACK L=1.00 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS 420R STR 26R IAW BOEING SRM 53-10-4 FIG 1SDR P2EA00304Angle · crackedDURING Q CHECK FOUND THE AFT CARGO COMPARTMENT LOWER DOOR JAMB ANGLE BETWEEN BS 817 AND 822 RBL 20 WITH CRACK L=1.00 W=0.001. REPAIRED THE AFT CARGO COMPARTMENT LOWER DOOR JAMB ANGLE BETWEEN BS817 AND 822 RBL20" IAW BOEING SRM 51-40-3 FIG 2SDR P2EA00303Frame · crackedDURING Q CHECK FOUND THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT BS500A BETWEEN STR 20-21L WITH CRACK L=1.50 W=0.002. REPAIRED THE LOWER FUSELAGE FWD CARGO COMPARTMENT FRAME AT VS500A BETWEEN STR 20-21L IAW BOEING SRM 53-10-6 FIG 1SDR P2EA00298Frame · dentedSJO - DURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT AT BS 727B BETWEEN STR 24 - STR 25L FRAME WITH DENT. L - 1.50 INCHES. W = 1.00 INCH. D = 0.125 INCH. REPAIRED THE AFT CARGO COMPARTMENT AT BS 727B BETWEEN STR 24 - STR 25L FRAME IAW BOEING SRM 51-40-3 FSDR P2EA00297Frame · crackedSJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 420 BETWEEN STR 20 - STR 21L FRAME WITH CRACK. L = 1.00 INCH. W = 0.002 INCH. REPAIRED THE LOWER FUSELAGE FORWARD CARGO COMPARMENT AT BS 420 BETWEEN STR 20 - STR 21L FRAME IAW BOSDR P2EA00296Frame · crackedSJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 500 BETWEEN STR 21 - STR 22R FRAME WITH CRACK. L = 1.250 INCHES. W = 0.001 INCH. REPAIRED THE LOWER FUSELAGE FORWARD CARGO COMPARTMENT AT BS 500 BETWEEN STR 21 - STR 22R FRAME IASDR P2EA00294Frame · dentedDURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT BS 747 BETWEEN STR 24 - STR 25R FRAME WITH DENT. L = 1.50 INCHES. W = 1.00 INCH. D = 0.160 INCH. REPAIRED THE AFT CARGO COMPARTMENT BS 747 BETWEEN STR 24 - STR 25R FRAME 6 IAW BOEING SRM 53-10-4. (X)SDR P2EA00293Door Frame · crackedSJO - DURING Q-CHECK, FOUND THE R-1 DOOR CUT OUT LOWER CORNER AT BS 315 WITH CRACK. L = 1.50 INCHES. W = 0.002 INCH. REPAIRED THE R-1 DOOR CUT OUT LOWER CORNER AT BS 315 IAW BOEING SRM 53-30-3 FIG 26. (X)SDR P2EA00292Splice · crackedSJO - DURING Q-CHECK FOUND THE AFT CARGO COMPARTMENT FROM BS 907 TO BS 927, STR 23L SPLICE WITH CRACK. L = 0.625 INCH. REPLACED THE AFT CARGO COMPARTMENT, STR 23L SPLICE AT BS 907 TO BS 927 IAW BOEING SRM 51-10-1. (X)SDR P2EA00291Flap · delaminatedSJO - DURING Q-CHECK, FOUND THE LEFT OUTBOARD AFT FLAP TRAILING EDGE AT WBL 289 WITH DELAMINATION. L = 4.0 INCHES. W = 2.0 INCHES. REPAIRED THE LEFT OUTBOARD AFT FLAP TRAILING EDGE AT WBL 289 IAW BOEING SRM 51-40-6 PARA 2.5 FIG 3. (X)SDR COOSDR000014Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500, BETWEEN STR 21R AND STR 22R, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000013Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 420, STR 26R, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000012Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500A, BETWEEN STR 20L AND STR 21L, FRAME CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000011Skin · crackedFUSELAGE SKIN, FORWARD ENTRY DOOR, AFT LOWER CORNER, CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000010Skin · crackedFUSELAGE SKIN, FORWARD SERVICE DOOR, AFT LOWER CORNER, CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR P2EA00311Skin · crackedDURING Q CHECK FOUND THE LT WING LEADING EDGE LOWER SKIN AT WBL 355 WITH CRACK L=1.00 W=0.002. REPAIRED THE LT WING LEADING EDGE LOWER SKIN AT WBL 355 IAW BOEING SRM 57-30-4 FIG 5SDR P2EA310Skin · crackedDURING Q CHECK FOUND THE FUSELAGE SKIN AT LT SECTION 41 BS219 WL214 WITCH CRACK L=0.750 W=0.001. REPAIRED THE FUSELAGE SKIN AT LT SECTION 41 BS219 WL214 IAW BOEING FAX COO-SJO-00-01172H DATED OCT 12, 2000 AND COOPESA EO COO-353-621-00 DATED OCT 13, 2000 DOCUMSDR P2EA00306Frame · crackedDURING Q CHECK FOUND THE FWD CARGO COMPMT FRAME AT BS 500 BETWEEN STR 20-21L WITH CRACK L=1.250 W=0.003. REPAIRED THE FWD CARGO COMPARTMENT FRAME AT BS 500 BETWEEN STR 20-21L IAW BOEING SRM 53-10-4 FIG 1SDR P2EA00290Skin · dentedSJO - DURING Q-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER AT SS 119.5, 5 INCHES FORWARD OF REAR SPAR WITH DENT. L = 2.25 INCHES. W = 1.50 INCHES. D = 0.10 INCH. REPAIRED THE LEFT HORIZONTAL STABILIZER AT SS 119.5, 5 INCHES FORWARD OF REAR SPAR IAW BOEING SDR P2EA00289Skin · dentedSJO - DURING Q-CHECK, FOUND THE LOWER FUSELAGE SKIN AFT CARGO COMPARTMENT FROM BS 944 - BS 948 BETWEEN STR 24 - STR 26L AT LOWER ROW OF FASTENERS OF FUSELAGE LAP JOINT WITH DENT. L = 1.00 INCH. W = 0.75 INCH. D = 0.125 INCH. REPAIRED THE LOWER FUSELAGE SKISDR PE2A00288Frame · dentedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO COMPARTMENT FUSELAGE FRAME AT BS 500B BETWEEN STA 22 - STA 24L WITH DENT. L= 1.25 INCHES. W - 1.0 INCH. D - 0.100 INCH. REPAIRED THE FORWARD CARGO COMPARTMENT FUSELAGE FRAME AT BS 5006 BETWEEN STA 22 - STA 24L SDR P2EA00287Frame · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD COMPARTMENT FUSELAGE FRAME AT BS 460 BETWEEN STA 21 - STA 23L WITH CRACK. L = 0.570 INCH. W = 0.050 INCH. REPAIRED THE FORWARD CARGO COMPARTMENT FUSELAGE FRAME AT BS 460 BETWEEN STA 21 - STA 23L IAW BOEING SRM 53-10-4SDR COOSDR000015Skin · crackedEXTERIOR FUSELAGE SECTION 41, LEFT FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATION, STA 227.8 AND WL 214. POSSIBLE CAUSE OF THE CRACK WAS SKIN FATIGUE. (X)SDR COOSDR000004Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500B, BETWEEN STR 22L AND STR 24L. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)SDR COOSDR000002Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 500, BETWEEN STR 21L AND STR 20L. POSSIBLE CAUSE OF CRACK WAS FATIGUE. (X)SDR COOSDR000003Frame · crackedLOWER FUSELAGE FORWARD CARGO COMPARTMENT, STA 460, BETWEEN STR 21L AND STR 23L. POSSIBLE CAUSE OF CRACK WAS FATIGUE. (X)SDR DL73K001960Support Fitting · corrodedTHE LOWER MAIN LUGS ON THE LT AND RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTINGS AT FS 685 WERE FOUND CORRODED. THE EXISTING BUSHINGS WERE REMOVED AND LUG BORES OVERSIZED TO REMOVE THE CORROSION. LARGER DIAMETER REPAIR BUSHINGS WERE INSTALLED TO REPAIR THESDR DL73E001942Door Frame · crackedTHE FWD FRAME OF THE C2 CARGO DOOR WAS FOUND WITH A 1 INCH CRACK IN THE UPPER AND LOWER FRAME WEBS AT THE FRAME LAP SPLICE ABOVE THE NR 3 STOP. THE CRACK WAS STOP DRILLED AND REPAIRED WITH TWO TITANIUM REPAIR ANGLES ON A TIME-LIMITED BASIS PER ER/A 378809-1SDR DL73E001936Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH LONG CRACK NEAR FS 520 AND STRINGER 16L. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 1 AND ER/A 378803-14.
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