Boeing 737-222
Service difficulty reports · 657
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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 = '737222' 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 = '737222' 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 P2EA99122Skin · corrodedSJO - DURING Q-CHECK, THE RIGHT WING OUTBOARD MID-FLAP SKIN AT WS 497 WAS BULGED. REPAIRED SKIN AS PER BOEING FAX COO-SJO-99-0330RR. (M)SDR P2EA99116Mechanism · corrodedSJO - DURING Q-CHECK, THE L2 DOOR HANDLE MECHANISM HOUSING HAD CORROSION AT LOWER TORQUE TUBE BEARING HOLE. THE HOLE AND BUSHING WERE REWORKED IAW OHM 52-16-03. (M)SDR P2EA99115Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, INBOARD MID FLAP LE SKIN AT INBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX COO-SJO-99-0279RR. (M)SDR P2EA99114Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, OUTBOARD MIDFLAP LE SKIN AT OUTBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX NR COO-SJO-99-0279RR. (M)SDR P2EA99105Skin · wornSJO - DURING Q-CHECK, THE SKIN ON THE LEADING EDGE OF THE RIGHT WING OUTBOARD FOREFLAP WAS FOUND WITH WEAR. THE SKIN WAS REPAIRED FROM WSL 498 TO 505 AS PER SRM 57-50-40- FIG 1. (M)SDR P2EA99104Rib · crackedSJO - DURING Q-CHECK, LEFT WING OUTBOARD MID FLAP INTERNAL LE RIB AT WBL 298 WAS FOUND CRACKED. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99103Rib · crackedSJO - DURING Q-CHECK, THE LEFT INBOARD MID FLAP STRUCTURE, FOREFLAP CENTER TRACK SUPPORT FITTING RIB (INBOARD) WAS CRACKED AT TWO PLACES. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99093Stringer · corrodedSJO - DURING Q-CHECK, A REPAIR LOCATED AT BS 767, STRINGER 9L WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 6. (M)SDR P2EA99080Skin · damagedSJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 727A, STRINGER 8R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND A PERMANENT REPAIR WAS INSTALLED AS PER SRM 53-30-3 FIGURE 6. (M)SDR P2EA99895Cargo Track · corrodedSJO - DURING Q-CHECK, THE FORWARD CARGO COMPARTMENT CARGO TRACK AT BS 468, RBL 14, WAS FOUND WITH CORROSION. THE TRACK WAS REPAIRED AS PER SRM 53-10-5 FIG 5. (M)SDR P2EA99121Splice · crackedSJO - DURING Q-CHECK, THE STRINGER SPLICE AT BS 359, STRINGER 14L WAS FOUND CRACKED. THE STRINGER SPLICE WAS REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99112Stringer · corrodedSJO - DURING Q-CHECK, TO VERIFY SRM COMPLIANCE, A REPAIR AT BS 1016 STRINGER 18L WAS REMOVED FOR INVESTIGATION. THE AREA WAS CLEANED, INSPECTED, AND REPAIRED AS PER COOPESA EO NR COO-3-53-152-99. (M)SDR P2EA99110Web · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE NLG WHEEL WELL UPPER WEB AT BS 278, RBL 10. THE UPPER WEB WAS REPAIRED IAW COOPESA EO NR COO-SJO-99-0267. (M)SDR P2EA99109Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE RIGHT WING INBOARD MIDFLAP, LE SKIN AT WBL 87.75. CRACK REPAIRED IAW BOEING FAX COO-SJO-99-0280. (M)SDR P2EA99102Rib · crackedSJO - DURING Q-CHECK, RIGHT WING, UPPER CHANNEL OF THE LE RIB AT WS 213 WAS FOUND CRACKED. THE CHANNEL WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M)SDR P2EA99096Support · corrodedSJO - DURING Q-CHECK, THE PASSENGER CABIN FLOOR SUPPORT LOCATED AT BS 996, LBL 12, WAS FOUND WITH CORROSION. THE SUPPORT WAS REPLACED FROM BS 996 TO BS 1009 IAW SRM 51-30-2. (M)SDR P2EA99087Floorbeam · corrodedSJO - DURING Q-CHECK, CABIN FLOORBEAM AT BS 312, RBL 45 FOUND WITH CORROSION. THE FLOORBEAM UPPER SECTION AT STATION 312 FROM RBL 19 TO RBL 61 WAS REPLACED IAW SRM 51-30-2. (M)SDR P2EA99086Skin · corrodedSJO - DURING Q-CHECK, THE SKIN AT BS 1016, STRINGER 26R HAD BULGED SKIN. CORROSION WAS FOUND. AREA WAS REPAIRED IAW SRM 53-10-3 FIG 3, SHEET 7. (M)SDR P2EA990088Splice · crackedSJO - DURING Q-CHECK, AT BS 360, STRINGER 15L, A CRACK WAS FOUND ON THE STRINGER SPLICE. THE SPLICE WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M)SDR P2EA99108Rib · crackedSJO - DURING Q-CHECK, THE RIGHT WING LE RIB LOCATED AT WS 524 WAS FOUND CRACKED. THE RIB WAS REPAIRED AS PER COOPESA EO NR COO-3-57-129-99. (M)SDR P2EA99094Rib · corrodedSJO - DURING Q-CHECK, THE RIGHT WING, LEADING EDGE RIB AT WBL 279.25 HAD WEAR ON THE LOWER FLANGE. THE AREA WAS REPAIRED BY APPLYING PRIMER AND ALODINE AS PER BOEING FAX NR COO-SJO-0261-RR. (M)SDR P2EA99120Web · crackedSJO - DURING Q-CHECK, A CRACK WAS FUOND AT THE NLG WHEEL WELL, UPPER WEB AT BS 286, RBL 9. AREA WAS REPAIRED AS PER COOPESA EO NR COO-3-53-137-99 AND BOEING FAX NR COO-SJO-99-0267. (M)SDR P2EA99075Handle · out of positionFLT - 612 - MYR - TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, FLAPS 1, TRIM 5.4. CREW REPORTS, ABORTED AT 40 KNOTS. FOUND SPEED BRAKE HANDLE OUT OF DETENT. CYCLED SEVERAL TIMES, OPS CHECKED OK PER MM 31-26-0. (M)SDR P2EA99073Skin · damagedSJO - PROVISIONAL REPAIR AT BS 1006, STRINGER 16 RT. REPAIRED FUSELAGE SKIN BETWEEN BS 995 AND BS 1008 FROM STRINGER 14 RT AND STRINGER 16 RT PER SRM SRM 53-30-3 FIG 6. (M)SDR P2EA99072Skin · delaminatedSJO - RIGHT WING OUTBOARD AFT FLAP DELAMINATED. DEFECT SIZE LENGTH 1 INCH. REPAIRED FLAP PER SRM 51-40-6, PAR 5 FIG 4. (M)SDR P2EA99069Skin · wornSJO - NR 2 ENGINE NOSE COWL UPPER SKIN SECTION WITH WEAR, DEFECT SIZE LENGTH 10 INCH WIDTH .5 INCH. REPAIRED NR 2 ENGINE COWLING PER SRM 54-30-3, FIG 2. (M)SDR P2EA99005Seal · tornMSP - FLT 701 - DURING CRUISE FLIGHT, FELT NOSE AND VIBRATION. CABIN PRESSURE BEGAN TO RISE. SWITCHED TO STANDBY PRESSURE AND BEGAN DESCENT. CABIN PRESSURE STABILIZED AT FL 180. FOUND FORWARD CARGO DOOR SEAL TORN. REPLACED FORWARD CARGO DOOR SEAL PER MM 5SDR P2EA99004Structure · vibrationMDW - FLT 701 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CRUISE, FELT VIBRATION. CABIN PRESSURE BEGAN TO CLIMB 1500 FPM. BEGAN DESCENT AND SWAPPED TO STANDBY PRESS AT FL 180, CABIN PRESSURE STABILIZED. COMPLETED CABIN PRESS CHECK. CHECKED AUTO PRSDR P2EA99034Doubler · disbondedSJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, STRINGER 8 LT TO STRINGER 9 LT. DEFECT SIZE, LENGTH 23 INCH WIDTH 20 INCH. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 TO BS 639, BETWEEN STRINGER 8 LEFT AND STRINGER 9 LEFT PER SRM 53-30-3, FIG 17. (M)SDR P2EA99033Doubler · disbondedSJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT, DEFECT SIZE, LENGTH 23 INCHES, WIDTH 20 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 AND BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT PER SRM 53-30-3, FIG SDR P2EA99022Doubler · disbondedSJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 951 TO BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT. DEFECT SIZE, LENGTH 34 INCHES, WIDTH 12 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 951 AND BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT PESDR P2EA99020Doubler · disbondedSJO - INTERNAL DOUBLER DISBONDED FROM BS 951-986.5, BETWEEN STRINGER 6 LEFT AND STRINGER 8 LEFT. DEFECT SIZE, LENGTH 34 INCH, WIDTH 12 INCH. REPAIRED INTERNAL DOUBLER FROM 951 TO BS 986.5, BETWEEN STRINGER LEFT AND STRINGER 8 LEFT PER SRM 53-30-3 FIG 17. (MSDR P2EA99070Fitting · crackedSJO - LEFT EMERGENCY EXIT DOOR FORWARD CENTRAL STOP CRACKED, LENGTH .187 INCH. REPLACED STOP FITTING PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA99053Frame · crackedSJO - Q-CHECK ITEM. FRAME WEB CRACKED AT BS 351.2 BETWEEN STR 19L AND STR 20L. DEFECT SIZE: LENGTH 0.375 INCH. REPLACED WEB AT BS 351.2 BETWEEN STR 18L AND STR 21L PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-1-133, VAM 100 NR 662. (XSDR P2EA99032Housing · damagedSJO - LEFT WING FUEL TANK, FORWARD CENTER TANK AFT BOOST PUMP HOUSING WITH TEMPORARY REPAIR. REPAIRED LEFT FUEL TANK BOOST PUMP HOUSING PER SRM 57-20-6, FIG 2. (M)SDR AT9900011Bulb · failedEMERGENCY PATH LIGHTING INOPERATIVE AT ROW 16. REPLACED LIGHT BULB AND LENS CAP IAW MM 33-50. OPS CHECKED GOOD. (X)SDR P2EA99050Support · wornSJO - Q-CHECK ITEM. RIGHT WING NR 7 CARRIAGE TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 2.0 INCHES. DEPTH 0.110 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0074RR DATED JAN 22, 1999. DOCUMENTED ON FAASDR P2EA99049Support · wornSJO - Q-CHECK ITEM. RIGHT WING NR 8 FLAP CARRIAGE FLAP TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 1.400 INCHES DEPTH 0.750 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0079RR JAN 22, 1999. DOCUMENTED ONSDR P2EA99045Rib · crackedSJO - Q-CHECK ITEM. RIB CRACKED IN LEFT FUEL TANK BETWEEN STIFFENERS 2 AND 3 AT STA 735.5. DEFECT SIZE: LENGTH 2.0 INCHES. REPAIRED RIB LOWER CHORD AT WBL 135.5 AND STR 2 AND STR 3 PER SB 737-57-1166, SEC III, PART III, FIG 3 DATED APRIL 13, 1989. SEE COOSDR P2EA99044Rib · crackedSJO - Q-CHECK ITEM. RIGHT WING, INBOARD MID-FLAP CENTER TRACK RIB CRACKED AT WBL 121. DEFECT SIZE: LENGTH 4.5 INCHES. REPLACED RIB AT WBL 121 RIGHT WING PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-003-6-43, VAM 100 NR 627. (X)SDR P2EA99071Rib · crackedSJO - LEFT WING INBOARD MID FLAP CENTE RTRACK INBOARD/OUTBOARD SUPPORT RIBS CRACKED AT LOWR FLANGE AREA, DEFECT SIZE WL 116.5 94 INCH) RWL 119.5 (2 INCH). REPLACED CENTER TRACK ROLLER SUPPORT RIBS AT WL 116.5 AND WL 119.5 PER SRM 51-10-1, PAGE 5 AND SRM 51-30SDR P2EA99041Skin · dentedSJO - Q-CHECK ITEM. RIGHT WING LOWER SURACE DENTED AT WBL 260 BETWEEN STIFFENER 6 AND STIFFENER 8. DEFECT SIZE: LENGTH 4.0 INCHES WIDTH 3.0 INCHES DEPTH 0.140 INCH. DENT FOUND STRUCTURALLY SATISFACTORY PER BOEING FAX COO-SJO-99-0043RR DATED JAN 18, 1998. SDR P2EA99026Angle · crackedSJO - ANGLE CRACKED AT BS 727, RBL 67, WL 208. DEFECT SIZE, LENGTH .375 INCH. FLOOR SUPPORT ANGLE REPAIRED FROM BS 716 TO BS 733, RBL 67, WL 208 PER SRM 51-40-1, FIG 1 DETAIL II. (M)SDR P2EA99010Skin · crackedSJO - AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. DEFECT SIZE, LENGTH .375 INCH. REPAIRED HINGE CUTOUT AREA BETWEEN BS 945.5 TO BS 956, BETWEEN STRINGER 10 RT AND STRINGER 12 RT PER SRM 53-30-3 FIG 21A. (M)SDR P2EA99046Frame · crackedSJO - Q-CHECK ITEM. RIGHT BS 727 CHORD CRACKED AT STR 18A. DEFECT SIZE: LENGTH - 2.125 INCHES. REPLACED RIGHT BS 727 CHORD FITTING BETWEEN STR 18R TO STR 24R PER SB 737-53-1088, SEC III, FIG 2 AND 3, DRAWING NR 65C35722, DATED 12-14-89. SEE COOPESA W.O. MSDR P2EA99042Frame · crackedSJO - Q-CHECK ITEM. BS 727 FUSELAGE OUTBOARD CHORD OF FRAME CRACKED AT STR 18L. DEFECT SIZE: LENGTH: 2.375 INCHES. REPLACED FUSELAGE BS 727 LT CHORD BETWEEN STR 18L TO STR 24L PER SB 737-53-1088, SECTION III, FIG 2 AND FIG 3, AND DRAWING NR 65C33722 DATE 1SDR P2EA99006Stringer · crackedSJO - STRINGER 9RT CRACKED AT BS 1064, WL 270.5, RBL 45. DEFECT SIZE, LENGTH .25 INCH. REPAIRED STRINGER 9RT BETWEEN BS 1056 AND BS 1067 PER SRM 10-3 FIG 2. (M)SDR P2EA99074Bulkhead Skin · crackedSJO - FORWARD PRESSURE BULKHEAD SKIN CRACKED AT BS 178. REPAIRED FORWARD PRESSURE BULKHEAD WEB AT BS 178 BETWEEN LBL 5.7 TO LBL 15.5 WL 231 TO 238.5, BETWEEN RBL 5.7 TO RBL 16 WL 231 TO WL 238.5, BETWEEN RBL 4.5 TO RBL 18.25, WL 216.3 TO WL 224.5 AND BETWEEN SDR P2EA99059Fitting · crackedSJO - Q-CHECK ITEM. MAIN ENTRY DOOR TORQUE TUBE LOWER SUPPORT FITTING CRACKED. DEFECT SIZE: LENGTH 0.500 INCH. REPLACED MAIN ENTRY DOOR STOP FITTING AT BS 294.5, STR 13L PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-2-123, VAM 100 NR 218. SDR P2EA99047Rib · crackedSJO - Q-CHECK ITEM. RIB CRACKED IN FRONT SPAR CAVITY FSS 390 (SLAT STATION 144.96). DEFECT SIZE: LENGTH 0.500 INCH. REPLACED LEADING EDGE RIB AT SS 144.96 PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-5-69, VAM 100 NR 313 FOR TECHNICAL
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