Boeing 737-222
Service difficulty reports · 657
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 = '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 P2EA00022Frame · dentedSJO - DURING Q-CHECK, FOUND FRAME DENTED AT BS 500A, BETWEEN STRINGER 24L AND 22L. REPAIRED FRAME AT BS 500A BETWEEN STRINGER 26L AND 21L IAW SRM 51-40-3 FIG 1. (M)SDR P2EA00045Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 259.5, WL 208 AND BETWEEN RBL 5 AND RBL 10. REPAIRED FLOORBEAM UPPER CHORD, BETWEEN RBL 10 AND LBL 29 AIW SRM 51-40-4, FIG 1. (M)SDR P2EA00005Hinge · wornPIT - FLT 578 - F/A REPORTED VIBRATION IN THE BACK OF A/C. IT SEEMS MORE NOTICEABLE ON THE LEFT OF THE A/C. VIBRATION IS ALSO NOTICEABLE IN THE COCKPIT AND IN THE THROTTLES. PERFORMED EVALUATION FLIGHT. DURING EVALUATION FLIGHT, NOTED LOW FREQUENCY VIBRATISDR 2000ZZZM217Bearing · wornPIT - FLT 578 - F/A REPORTED VIBRATION IN THE BACK OF A/C. IT SEEMS MORE NOTICEABLE ON THE LEFT OF THE A/C. VIBRATION IS ALSO NOTICEABLE IN THE COCKPIT AND IN THE THROTTLES. PERFORMED EVALUATION FLIGHT. DURING EVALUATION FLIGHT, NOTED LOW FREQUENCY VIBRATISDR P2EA00001Fire Loop · malfunctionedBUF - FLT 938 - NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, AFTER THRUST LEVER IS RETARDED TO FLIGHT IDLE THE OVERHEAT LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO GROUND UNEVENTFUL. OVERHEAT SYSTEM CHECKED PER MM 26-10-01, NO DEFECTS NOTED. CHECKED CONDISDR P2EA99348Skin · delaminatedSJO - LEFT WING OUTBOARD FLIPPER FLAPPER DELAMINATED. DEFECT SIZE, LENGTH 9 INCH, WIDTH 7.25 INCH. REPAIRED FLIPPER FLAPPER PER COOPESA EO COO-CMP-3-57-711-99, DATED DECEMBER 7, 1999. (M)SDR P2EA99344Frame · crackedSJO - C-CHECK, FRAME CRACKED AT BS 967, BETWEEN STRINGER 20/21LT. DEFECT SIZE, LENGTH 3.5 INCH, WIDTH .16 INCH, DEPTH .63 INCH. REPAIRED FUSELAGE SECTION AT BS 967, BETWEEN STRINGER 19 AND 21 LEFT PER SRM 51-40-3. (M)SDR P2EA99337Seat Track · corrodedSJO - C-CHECK, SEAT TRACK CORRODED FROM BS 360 TO BS 380, LBL 35 INCHES. DEFECT SIZE, LENGTH 8 INCHES, WIDTH 2.25 INCHES, DEPTH .200 INCHES. REPAIRED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 53-10-5, FIG 2. (M)SDR P2EA99356Skin · disbondedSJO - DURING C-CHECK, RIGHT AILERON INBOARD TRAILING EDGE DISBONDED AT REAR SPAR AREA. REPAIRED RIGHT AILERON PER SRM 51-40-6, PAR 5. (M)SDR P2EA99347Frame · crackedSJO - FORWARD CARGO DOOR FRAME CRACKED AT AFT FRAME, DEFECT SIZE, LENGTH .750 INCH. REPAIRED FORWARD CARGO DOOR BETWEEN BEAM NR 1 AND BEAM NR 3 PER SRM 51-40-3 FIG 1. (M)SDR P2EA99346Rib · crackedSJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH .32 INCH. REPLACED RIB AT SS 356 OUTBOARD TRACK PER SRM 51-30-2. (M)SDR P2EA99338Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM UPPER CHORD CORRODED AT BS 344, WL 208, BETWEEN LBL 32 AND BL 0. DEFECT SIZE, LENGTH 15 INCHES, WIDTH 1.5 INCH, DEPTH .050 INCH. REPAIRED FLOORBEAM AT BS 344, BETWEEN RBL 9 INCHES AND LBL 40 INCHES PER SRM 53-10-2, FIG 7. (M)SDR P2EA99334Intercostal · crackedSJO - FORWARD SERVICE DOOR INTERCOSTAL CRACKED AT BEAM 3. ANGLE REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2 PAGE 8. (M)SDR P2EA99341Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACK FROM BS 764 TO BS 767 BETWEEN STRINGER 18 AND 19 LEFT. DEFECT SIZE, LENGTH 3 INCH, WIDTH .032 INCH, DEPTH .028 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 759.5 TO BS 771, BETWEEN STRINGER 18 LT AND 20 LT PER COOPESA EO COSDR P2EA99339Skin · scratchedSJO - C-CHECK, E/E DOOR WITH DEEP SCRATCHES AND MISSING MATERIAL. DEFECT SIZE, LENGTH 1.125 INCH, WIDTH .250 INCH, DEPTH .040 INCH. REPLACED DOOR SKIN PER SRM 51-10-1 PAGE 5 AND PER SRM 51-30-2. (M)SDR AT9900840Slide · looseFOUND L1 DOOR EMERGENCY SLIDE PACK LOOSE. SECURED L1 DOOR EMERGENCY SLIDE PACK IAW B737 MM 25-61.SDR P2EA99309Detent Arm · out of adjustMDW - FLT 277 - FLAPS 1 THROUGH 25 SELECTED, NR 6 LEADING EDGE SLAT EXTENDS CROOKED. FLAPS 30 THROUGH 40 SELECTED, NR 6 LEADING EDGE SLAT GOES TO FULL EXTEND. ADJUSTED DETENT ARMS ON NR 6 L/E SLAT PER MM 27-81-0A. OPS CHECKS NORMAL. (X)SDR 2000ZZZX481Wire · brokenUNCOMMANDED RT AND LT YAW AFTER TAKEOFF. SWITCHED YAW DAMPER TO THE 'OFF' POSITION AND YAWING STOPPED. MAINTENANCE FOUND A BROKEN WIRE IN THE D4117J ELECTRICAL CONNECTOR AT THE FORWARD END OF THE E1 EQUIPMENT RACK FOR THE AUTOPILOT ACCESSORY UNIT. THE WIRE SDR 2000ZZZX480Control Cable · jammedUNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. LATER INVESTIGATION REVEALED THE AIR/GROUND TELEFLEX CABLE ON THE RIGHT LANDING GEAR JAMMED. THE CABLE WAS REPLACED IAW BOEING MM AND LANDING GEAR RETRACT CHECK WAS PERFORMED. CHECKED OK.SDR P2EA99267Control Panel · failedFLT 416 - MDW - AIR RETURN, LANDING UNEVENTFUL. AT ABOUT 4000 FT AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED THAT A SMOKE DETECTOR WENT OFF. LIGHT FLASHING AND HORN GOING. DEFERRED PER MEL 26-16, CI M603392 AND M603393 ASSIGNED. REF MEL 26-16, M603392 ANDSDR 99ZZZX3931Mlg · corrodedDURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON RIGHT MAIN LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND WITH CORROSION, GROOVES, AND WORN OUT. IN ADDITION, THERE WERE SOME COMPONENTS WITH LOOSE BUSHINGS AND MISSING, LOOSE, AND BROKEN RIVET.SDR 99ZZZX3930Mlg · corrodedDURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON LEFT MAIN LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND WITH CORROSION AND GROOVES. IN ADDITION, THERE WERE SOME COMPONENTS WITH LOOSE BUSHINGS.SDR 99ZZZX3929Nlg · corrodedDURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON NOSE LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND WITH CORROSION, GROOVES, AND WORN OUT.SDR P2EA99222Engine · bird strikeMDW - FLT 938 - ABORTED TAKEOFF AT 110 KNOTS DUE A LOUD BANG FOLLOWED BY A BURNT SMELL IN CABIN AND COCKPIT. DISCOVERED BIRD STRIKE NR 1 ENGINE. PERFORMED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. (X)SDR P2EA99216Mechanism · out of adjustMDW - FLT 586 - NR 6 LEADING EDGE SLAT WOULD NOT EXTEND IN FLIGHT UNTIL FLAPS 30 POSITION WAS SELECTED. ADJUSTED TENSION ON NR 6 SLAT DETENT ARMS PER MM 27-81-0. SLATS OPERATE NORMALLY. (X)SDR P2EA99212Engine · failedMCI - FLT 819 - DURING A REDUCED THRUST TAKEOFF, NR 2 EGG WAS IN THE YELLOW BAND. AFTER LIFT-OFF, THE EGT ROSE ABOVE THE RED-LINE, ABOUT 625 FOR 10 TO 15 SECONDS. RETARDING THE THROTTLES TO BRING THE EGT INTO THE GREEN, RESULTED IN AN EPR READING OF 1.72. ASDR P2EA99199Connector · looseDEN - FLT 305 - EMERGENCY DECLARED (APU PREVIOUSLY DEFERRED) LANDING UNEVENTFUL AT SCHEDULED DESTINATION. LEFT ENGINE DRIVEN GENERATOR DROPPED OFF LINE IN FLIGHT AND WOULD NOT RESET. SWAPPED APU GCU WITH NR 1 ENGINE GCU. RAN NR 1 ENGINE. GENERATOR OPS CHECSDR AT9900379Batteries · dischargedLEFT HAND OVERWING HATCH EMERGENCY LIGHT ABOVE DOOR HAS DEAD BATTERIES. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW B737 MM 33-51-31. OPS CHECKED OK.SDR P2EA99184Tire · failedMDW - FLT 709 - ON LANDING, NR 2 MAIN TIRE BLEW. LANDING AND ALL OTHER INDICATIONS NORMAL. REPLACED NR 2 MAIN WHEEL ASSEMBLY PER MM 32-45-11. REPLACED NR 1 MAIN TIRE ASSEMBLY PER MM 32-45-11 DUE TO NR 2 MAIN TIRE DISCREPANCY. (M)SDR P2EA99178Skin · corrodedSJO - DURING C-CHECK, THE FUSELAGE SKIN BETWEEN BS 986.5 AND BS 1016, FROM STRINGER 10L, TO STRINGER 14L WAS FOUND WITH CORROSION. REPLACED FUSELAGE SKIN PANEL FROM BS 986.5 AND BS 1016 BETWEEN STRINGER 10L AND 14L DUE TO CORROSION PER COOPESA EO COO-3-53-243SDR P2EA99179Skin · misrepairedSJO - DURING C-CHECK A REPAIR WAS FOUND NOT PER SRM ON THE FUSELAGE BETWEEN BS 995 AND BS 1010, STRINGER 14 RIGHT. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 993 AND BS 1013 FROM STRINGER 13 TO STRINGER 15 RIGHT SIDE PER SRM 53-30-3 FIGURE 16. (M)SDR P2EA99180Skin · corrodedSJO - DURING C-CHECK AT THE FUSELAGE, BETWEEN BS 907 AND BS 1016, FROM STRINGER 14L TO 20L, SKIN PANEL WAS FOUND WITH CORROSION OUT OF LIMITS. REPLACED FUSELAGE SKIN PANEL FROM BS 908 TO BS 1016, BETWEEN STRINGER 14 TO STRINGER 20 LEFT SIDE DUE TO CORROSION PSDR P2EA99163Stringer · crackedSJO - DURING C-CHECK, ON THE FUSELAGE AT BS 1016, STRINGER 27L WAS FOUND WITH A CRACK. REPAIRED STRINGER 27L FROM BS 1016 TO BS 1024 PER SRM 53-10-3, FIGURE 1. (M)SDR P2EA99157Floorbeam · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN, BS 360, RBL 13, THE FLOORBEAM UPPER CHORD WAS FOUND WITH CORROSION. REPAIRED FLOORBEAM UPPER CHORD AT BS 360 BETWEEN RBL 5 AND RBL 21 DUE TO CORROSION PER SRM 53-10-9 FIGURE 1. (M)SDR P2EA99156Floorbeam · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN, BS 344, BETWEEN LBL 60 AND RBL 60 FLOORBEAM UPPER CHORD WAS FOUND WITH CORROSION. REPAIRED FLOORBEAM UPPER CHORD AT BS 344, BETWEEN LBL 65 AND RBL 65 DUE TO CORROSION PER SRM 53-10-9 FIGURE 5. (M)SDR P2EA99153Stringer · corrodedSJO - DURING C-CHECK, STRINGER 18 LEFT, AFT CARGO COMPARTMENT, BS 727B PLUS 12, WAS FOUND WITH CORROSION. REPAIRED FUSELAGE STRINGER 18 LEFT BETWEEN BS 727B PLUS 5 INCHES AND BS 752 DUE TO CORROSION PER SRM 53-10-3 FIGURE 1. FABRICATED ANGLES AND SPLICE PER SDR P2EA99177Floorbeam · corrodedSJO - DURING C-CHECK, IN PASSENGER CABIN AFT LAVATORY AREA, BS 947, BETWEEN RBL 54 INCH AND LBL 54 INCH, FLOORBEAM WAS FOUND WITH CORROSION. REPAIRED FLOORBEAM UPPER CHORD AT BS 947, BETWEEN LBL 59 AND RBL 59 PER COOPESA EO COO-3-53-222-99, DATED APR 8, 1999.SDR P2EA99171Floorbeam · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 987, BETWEEN RBL 47 INCH AND LBL 47 INCH, FLOORBEAM WAS FOUND CORRODED. REPAIRED UPPER CHORD OF FLOORBEAM, BS 987, BETWEEN LBL 51.250 AND RBL 51.250 PER COOPESA EO COO-3-53-223-99, DATED APR SDR P2EA99170Intercostal · corrodedSJO - DURING C-CHECK IN THE PASSENGER CABIN, AFT LAVATORY AREA, BETWEEN BS 987 AND BSL 1016, FROM BL 0 TO LBL 19 INCH, WL 208.1, FLOOR SUPPORTS (INTERCOSTALS) WERE FOUND WITH CORROSION. REPAIRED FLOOR SUPPORT CHANNEL BETWEEN BS 987 AND BS 1006, BL 0 PER COOPESDR P2EA99169Floorbeam · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 1016, BETWEEN RBL 38 INCH AND LBL 38 INCH, FLOORBEAM WAS FOUND CORRODED. REPAIRED FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN LBL 41 INCH AND RBL 41 INCH PER COOPESA EO COO-3-53-224-99, DATED ASDR P2EA99166Intercostal · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN AFT LAVATORY AREA, BETWEEN BS 967 AND BS 987, WL 208.1, RBL 17 INCH, FLOOR SUPPORT (INTERCOSTAL) WAS FOUND WITH CORROSION. REPAIRED FLOOR SUPPORT CHANNEL BETWEEN BS 967 AND BS 987, RBL 17 INCH PER COOPESA EO COO-3-SDR P2EA99162unknownSJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 967, BETWEEN RBL 54 AND LBL 54, FLOORBEAM WAS FOUND CORRODED. REPAIRED FLOORBEAM UPPER CHORD BS 967, BETWEEN LBL 12 AND RBL 12 PER SRM 53-10-9 FIGURE 7. CORROSION REMOVED, TREATED, AND WITHISDR P2EA99161Floor · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN AFT LAVATORY AREA, BETWEEN BS 1016 AND BS 1016 PLUS 11 INCHES, FROM BL 0 TO RBL 36, FLOOR WEB WAS FOUND WITH CORROSION INCLUDING THE SUPPORT ANGLE. REPLACED FLOOR WEB BETWEEN BS 1016 TO BS 1032.5 FROM BL 0 TO RBL 3SDR P2EA99147Stringer · corrodedSJO - DURING C-CHECK, ON THE EXTERNAL FUSELAGE FROM BS 957 TO BS 1016, STRINGER 22L WAS FOUND WITH CORROSION. REPAIRED FUSELAGE NR 22 LEFT STRINGER SECTION BETWEEN BS 952 AND BS 1016 DUE TO CORROSION PER SRM 53-10-03 FIGURE 1. (M)SDR P2EA99160Frame · crackedSJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR FORWARD AND AFT LOWER CORNERS FRAMES WERE FOUND WITH CRACKS. REPAIRED THE FORWARD CARGO COMPARTMENT DOOR FORWARD AND AFT LOWER CORNERS DUE TO CRACKS PER SB 737-52-1100, SECTION III, FIGURE 3 AND 4, REVISDR P2EA99151Stringer · corrodedSJO - DURING C-CHECK, STRINGER 25L WAS FOUND WITH CORROSION BETWEEN BS 967 AND BS 1016 AND A CRACK BETWEEN BS 1006 AND BS 1016. REPLACED FUSELAGE STRINGER 25 LEFT BETWEEN BS 967 AND BS 1016 PER SRM 51-10-1 PAGE 5 AND 51-30-2. (M)SDR P2EA99149Tee · crackedSJO - DURING C-CHECK, THE EXTERNAL FUSELAGE, BS 927, BETWEEN STRINGERS 24L AND 25L, 'T' WAS FOUND WITH A CRACK. REPLACED 'T' AT BS 927 BETWEEN STRINGERS 24 LEFT AND 25 LEFT PER SRM 51-10-1 PAGE 5. RIVETS REPLACED PER SRM 51-30-2. FABRICATED 'T' PER COOPESA SDR P2EA99143Doubler · corrodedSJO - DURING C-CHECK, THE FUSELAGE BETWEEN BS 947 AND BS 967, BETWEEN STRINGERS 24L AND 27L, DOUBLER WAS FOUND WITH CORROSION. REPLACED FUSELAGE SKIN INTERNAL DOUBLER BETWEEN BS 947 AND BS 967 FROM STRINGER 24 TO 27 LEFT SIDE DUE TO CORROSION PER SRM 51-10-1 SDR P2EA99168Stringer · corrodedSJO - DURING C-CHECK, AT THE FUSELAGE, BETWEEN BS 967 AND BS 1016, STRINGER 20L WAS FOUND WITH CORROSION. REPLACED STRINGER 20 LEFT, BETWEEN BS 907 AND BS 1016 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)SDR P2EA99150Tee · crackedSJO - DURING C-CHECK, THE EXTERNAL FUSELAGE BETWEEN STRINGERS 23L AND 24L, BS 947, 'T' WAS FOUND WITH A CRACK. REPLACED 'T' AT BS 947 BETWEEN STRINGERS 23 LEFT AND 24 LEFT PER SRM 51-10-1 PAGE 5, SRM 51-30-2. FABRICATED 'T' PER COOPESA EO COO-3-53-212-99, DA
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