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 P2EA98111Angle · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-46-5223C, A CRACK WAS NOTED ON BEAM NR 7 ANGLE, OF THE L1 DOOR. THE CRACK WAS 1.25 INCHES LONG. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 FIG 1. (M)SDR P2EA98110Angle · crackedSJO - DURING C-CHECK ROUTINE INSPECTION PER WORK CARD NR J2C-46-5223C, A CRACK WAS NOTED ON BEAM NR 8 AFT ANGLE OF THE L1 DOOR. THE CRACK WAS 4 INCHES LONG. INSTALLED ANGLE REPAIR PER SRM 51-40-3 FIG 1. REF: COOPESA W.O. NR LI-0630, VAM100-240, 208SDA007. SDR P2EA98115Support · crackedDURING C-CHECK ROUTINE INSPECTION PER WORK CARD J2C-512525, CRACKS WERE FOUND AT THE FOLLOWING LOCATION: ANTENNA SUPPORT CHANNEL AT BS 500 AND BS 500A, BETWEEN STR 28L AND STR 28R. REPLACED ANTENNA SUPPORT CHANNEL IAW SRM 51-10-1 PG 5. FABRICATED PARTS IAW SDR P2EA98114Stringer · corrodedDURING C-CHECK WHILE PERFORMING ROUTINE INSPECTION PER WORK CARD J2C-512525, CORROSION WAS FOUND AT STR 26 LEFT BETWEEN BS 500 B + 16 INCHES AND BS 528. THE CORROSION WAS OUT OF LIMITS (10 PERCENT REMOVED) PER THE SRM. THE STRINGER WAS REPAIRED IAW SRM 53-10SDR P2EA98113Stringer · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-51-2525, A CRACK WAS FOUND AT BS 480 BETWEEN STRINGER NR 26 AND NR 27 RT. THE CRACK WAS REPAIRED AS PER SRM 53-10-4. (M)SDR P2EA98112Stringer · crackedSJO - DURING C-CHECK ROUTIN EINSPECTION AS PER WORK CARD J2C-51-2525, A CRACK WAS FOUND ON STRINGER NR 23 RT, BETWEEN BS 493 AND BS 514. THE CRACK WAS .25 INCH LONG. THE CRACK WAS REPAIRED AS PER SRM 53-10-03. (M)SDR P2EA98109Frame · crackedSJO - DURING C-CHECK, ROUTINE INSPECTION PER CARD NR J2C 51 2525, NOTED CRACK ON FUSELAGE FRAME AT BS 400 BETWEEN STR 25 AND 26 LT. CRACK WAS .250 INCH IN LENGTH. CRACK WS REPAIRED IAW SRM 53-10-4 FIG 6. COOPESA W.O. NR L1-0630, NR VAM 100-225, 208SDA006. SDR P2EA98108Torsion Link · brokenMDW - FLT 424 - ON INITIAL TAKEOFF ROLL, ENCOUNTERED NOSE WHEEL SHIMMY, ABORTED TAKEOFF. AIRCRAFT STOPPED AND WAS UNABLE TO TAXI BACK TO GATE DUE TO STEERING PROBLEM. AIRCRAFT TOWED BACK TO GATE. FOUND LOWER TORSION LINK BROKEN. REPLACED UPPER AND LOWER TOSDR 98ZZZX2392Torsion Link · brokenTAKEOFF ABORTED. NO EMERGENCY DECLARED. ON INITIAL TAKEOFF ROLL, ENCOUNTERED NOSE WHEEL SHIMMY, ABORTED TAKEOFF. AIRCRAFT STOPPED AND WAS UNABLE TO TAXI BACK TO GATE DUE TO STEERING PROBLEM. AIRCRAFT TOWED BACK TO GATE. FOUND LOWER TORSION LINK BROKEN.SDR 98ZZZX2415Connector · failedAFT SECTION OF TRACK FLOOR EMERGENCY LIGHTING FROM OVERWING EXIT TO BACK INOPERATIVE. FOUND BAD PIN IN CONNECTOR AT AFT END OF TRACK LIGHTING. REPLACED PIN. OPERATIONS CHECK OK IAW BOEING MM, CHAPTER 33-51-01.SDR 98ZZZX2414Battery · dischargedAFT OVER AISLE EMERGENCY EXIT LIGHT INOPERATIVE. FOUND BATTERY VOLTAGE LOW. REMOVED AND REPLACED BATTERIES. OPERATIONS CHECK OK IAW BOEING MM 33-51-81. (X)SDR P2EA98103Latch · brokenATL - FLT 264 - DURING REPOSITIONING OF JETWAY CAB ON THROUGH FLT, CONTACT WITH THE L-1 DOOR OCCURRED. FORWARD ENTRY DOOR LATCH BROKEN, GUIDE ARM, EYEBOLT, AND HINGE FAIRING BROKEN. REPLACED ROD END AND HINGE FAIRING, ADJUSTED PER MM 52-11-00. (M)SDR CALA9800690Line · leakingTHE B SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.8 GALLONS IN FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF THE B SYSTEM LOW QUANTITY LIGHT. THE ABNORMAL CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDSDR P2EA98079Light · inoperativeFLT 119 - ATL - FLT DECK EMERGENCY LIGHT INOP. DEFERRED PER MEL 33-15A, CI M208000 ASSIGNED. REF CI M208000, FLT DECK EMERGENCY LIGHT INOP. REPLACED FLT DECK EMERGENCY LIGHT ASSY, OPS OK CI M208000 CLEARED. (M)SDR P2EA98078Pitot Tube · failedFLT 264 - MCI - ON TAKEOFF POWER APPLICATION, CAPTAINS ALTIMETER DROPPED 20 FT TO 980. AN OFF FLAG CME ON. A CROSS CHECK OF THE F/O'S ALTIMETER SHOWED THE SAME. REPLACED UPPER RT PITOT PROBE PER MM 34-11-11, LEAK CHECKS OF CAPTAINS AND F/O'S SYSTEMS NORMAL SDR P2EA98042Light · missingFLT 435 - PIT - FOUND DURING PREFLIGHT WALK AROUND, TAXI LIGHT MISSING, BRACKET CRACKED. DEFERRED PER CDL 33-40-2. CI NR C603807 ASSIGNED. INSTALLED NOSE TAXI LIGHT ASSY AND WIRE HARNESS REF MM 33-42-51. OPS CHECK OK. PERFORMED NOSE GEAR SWING ALL CLEARANSDR CALA9800390Sign · shortedTHE CREW REPORTED SMOKE APPEARED MOMENTARILY IN CABIN AT PUSH TIME. MAINTENANCE FOUND THE NO SMOKING FASTEN SEAT BELT SYSTEM INOPERATIVE WITH THE ROW 6 ABC OVERHEAD PSU BASE ASSEMBLY SHORTED OUT. THE WIRES FOR PSU AT ROW 6 ABC WERE CUT AND STOWED AND THE SYSSDR P2EA99082Skin · damagedSJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 500A, STRINGER 26R WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 1. (M)SDR 98UAL900070Coffeemaker · dirtySMOKE IN AFT CABIN FROM AFT GALLEY AREA. IT APPEARS TO BE FROM COFFEEMAKER AREA. *S/D* FOUND COFFEE POT LID UNDER GALLEY INBOARD COFFEEMAKER. REMOVED DEBRIS. APPLIED POWER TO AFT GALLEY. NO SMOKE/ODORS DETECTED, OK TO CONTINUE.SDR P2EA98026Hydraulic Line · leakedTHE AIRCRAFT EXPERIENCED LOSS OF A-SYSTEM HYDRAULIC QUANTITY IN-FLIGHT FROM MCI TO DFW. AN UNEVENTFUL LANDING ACCOMPLISHED AT DFW. DELTA AIRLINES MAINTENANCE, A CONTRACT MAINTENANCE PROVIDER FOR VANGUARD AIRLINES, WAS DISPATCHED AND DISCOVERED A HYDRAULIC LISDR P2EA98022Clamp · looseDEN - FLT 604 - DEN-MCI - THE NR 2 ENGINE OVERHEAT LIGHT CAME ON INTERMITTENTLY WITH NO OTHER ABNORMAL INDICATIONS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEN WHERE THE LANDING WAS UNEVENTFUL AT 2217Z. FRONTIER AIRLINES AN APPROVED CONTRACT MAINTENANSDR 98ZZZX1045Skin · corrodedFOUR CRACKS WERE FOUND AT UPPER FUSELAGE BETWEEN BS 616 AND BS 639 BETWEEN STR 1 AND STR 2 RT IN THE BODY SKIN. IT APPEARS TO BE THE FIRST TIME FOR A CRACK IN THIS AREA PER BOEING FAX COO-SJO-98-0057RR DATED 1-22-98. THE SUSPECT CAUSE OF THIS DAMAGE IS STRESSDR P2EA98023Support · gougeDURING INSPECTION, FOUND A GOUGE AT THE RIGHT WING OUTBOARD FLAP OUTBOARD TRACK GIMBLE SUPPORT. BLENDED OUT GOUGED AREA ON SUPPORT FITTING IAW BOEING TELEX NR C00-SJO-98-0063RR. (M)SDR P2EA98021Frame · damagedSJO - DURING C-CHECK, AFT CARGO DOOR TEMPORARY REPAIR. INSTALLED PERMANENT REPAIR IAW SRM 51-40-3 AND EO 973752A043. (M)SDR P2EA98020Rib · crackedSJO - DURING C-CHECK, LEFT WING NR 1 SLAT AREA, INBOARD RAIL, OUTBOARD RIB CRACKED. REPAIRED IAW BOEING DRAWING 65C25658. (M)SDR P2EA98019Fitting · crackedSJO - DURING C-CHECK, LEFT WING NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPLACED LEFT WING NR 3 SLAT ACTUATOR SUPPORT FITTING IAW SRM 51-10-1. (M)SDR P2EA98024Support · crackedDURING MAINTENANCE FOUND A CRACK AT THE UPPER VHF ANTENNA SUPPORT BASE. REPAIRED IAW COOPESA EO-C00-3-53-047-98. (M)SDR P2EA98018Skin · crackedSJO - DURING C-CHECK, UPPER EXTERIOR FUSELAGE SKIN HAS 4 CRACKS AT VHF ANTENNA CUT OUT, BETWEEN BS 616 AND BS 639 AT STRINGER NR 1 AND NR 2 RIGHT. REPAIRED FUSELAGE SKIN SECTION IAW EO C00-3-53-039-98. (M)SDR P2EA98017Skin · damagedSJO - DURING C-CHECK, TEMPORARY SKIN REPAIR INSTALLED BETWEEN BS 223 AND BS 255 BETWEEN WL 204 AND WL 234R. INSTALLED PERMANENT REPAIR PER BOEING S/B 737-53-1111 REV 1. (M)SDR P2EA98016Skin · corrosionSJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORRODED) FROM BS 727 TO 780, STRINGER 20L. REPAIRED FUSELAGE FRAME SECTION IAW SRM 53-30-3 FIG 15. (M)SDR 98UAL900037Vhf Trans · failedLOST COMM ON FREQUENCY 127.8 MHZ ON NUMBER ONE VHF. COMM APPEARED WEEK ON OTHER FREQUENCIES AS WELL. *S/D* REPLACED NR 1 VHF COMM TRANSCEIVER, OP CHECKED GOOD.SDR P2EA98015Frame · corrosionSJO - DURING C-CHECK, FUSELAGE FRAME CORRODED AT BS 312 BETWEEN STRINGERS 26R AND 27R (ELECTRONIC EQUIPMENT COMPARTMENT). REPAIRED FUSELAGE FRAME SECTION IAW SRM 53-10-4 FIG 10. (M)SDR P2EA98014Skin · corrosionSJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) FROM BS 787 TO BS 800, STRINGER 23R AND 25R. REPAIRED FUSELAGE SKIN SECTION IAW SRM 53-30-3 FIG 1. (M)SDR P2EA98013Skin · corrosionSJO - DURING C-CHECK, UPPER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) AT BS 907, BETWEEN STRINGER 3L AND 3R. REPAIRED FUSELAGE SKIN SECTION IAW SRM 53-30-3 FIG 28. (M)SDR P2EA98012Stringer · corrodedSJO - DURING C-CHECK, STRINGER 20R CORRODED AT BS 767. REPAIRED STRINGER IAW 53-10-3 FIG 1. (M)SDR P2EA98011Skin · corrosionSJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) AT BS 907, BETWEEN STRINGER 18R AND 23R. REPAIRED FUSELAGE SKIN BUTT JOINT IAW 53-30-3 FIG 28. (M)SDR P2EA98010Frame · crackedSJO - DURNG C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPRTMENT AT BS 500A, AT STRINGER 20R AND 21R, CRACK SIZE 14 INCH BY 4 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M)SDR P2EA98009Frame · crackedSJO - DURING C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPARTMENT AT BS 420, BETWEEN STRINGER 22L AND 23L, CRACK SIZE 13.5 INCH BY 2.5 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M)SDR P2EA98008Frame · crackedSJO - DURING C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPARTMENT AT BS 460, STRINGER 20L AND 21L, CRACK SIZE 10.25 INCH BY 4 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M)SDR P2EA98007Skin · dentedSJO - DURING C-CHECK, DENT IN LOWER EXTERIOR FUSELAGE SKIN AT BS 318, STRINGER 22 RT, DENT SIZE LENGTH 8.5 INCH BY WIDTH 7.5 INCH. REPAIRED DENT IAW SRM 53-30-3 FIG 7. (M)SDR P2EA98006Frame · crackedSJO - FUSELAGE FRAME CRACKED, IN FORWARD CARGO COMPARTMENT AT BS 460, BETWEEN STRINGER 28L AND 27R, CRACK SIZE 11 INCH BY 4 INCH. REPAIRED FUSELAGE FRAME CRACK, PER SRM 53-10-4 FIG 10. (M)SDR P2EA98005Frame · crackedSJO - DURING C-CHECK, FUSELAGE FRAME, UPPER FLANGE CRACKED, IN FORWARD CARGO COMPARTMENT AT BS 500, BETWEEN STRINGER 19L AND 21L, CRACK SIZE 11 INCH BY 4 INCH. REPAIRED FUSELAGE FRAME CRACK, PER SRM 53-10-4 FIG 1. (M)SDR P2EA98315Plate · crackedSJO - IN C-CHECK OPERATION AT COOPESA, A CRACK WAS FOUND IN THE UPPER VHF ANTENNA BASE PLATE. A NEW BASE PLATE WAS FABRICATED AND REPLACED PER BOEING SPECIFICATIONS. (M)SDR P2EA98314Fitting · gougedSJO - IN C-CHECK OPERATION AT COOPESA, A GOUGE WAS FOUND AT RIGHT WING, OUTBOARD TRACK, WBL 355, ON THE OUTBOARD FLAP GIMBLE SUPPORT FITTING. THE GOUGE WAS BLENDED OUT AND FOUND WITHIN LIMITS AS PER BOEING AIRCRAFT CO. (M)SDR P2EA98003Valve · failedPIT - FLT 435 - EMERGENCY DECLARED, LANDING AT DESTINATION AIRPORT UNEVENTFUL, WITH CROSSFEED OPEN AND LEFT BOOST PUMPS OFF, FUEL CONTINUED TO BURN OUT OF THE LEFT WING TANK. REPLACED FUEL CROSSFEED VALVE PER MM 28-22-21. LEAK AND OPS CHECK OK. RAN ENGINES SDR 98ZZZM162Radar R/T · failedFURING FLT 642 FROM MCO AIRCRAFT 468, REPORTED WX RADAR WILL NOT PAINT WX OR GROUND. AIRCRAFT RETURNED TO MCO. REMOVED AND REPLACED THE WEATHER RADAR R/T. SYSTEM OPS CHECKED NORMAL PER MM 34-41-0. AIRCRAFT RETURNED TO SERVICE.SDR P2EA97097Skin · dentedSJO - C-CHECK - UPPER FUSELAGE BS 1088 WL 222 AND LBL 32 SKIN WITH DENT OUT OF LIMITS IAW SRM 53-30-1 FIG 1 BETWEEN STR 18L AND 20L. REPAIRED FUSELAGE SKIN BETWEEN BS 1088 AND BS 1094. STR 18L AND STR 20L DUE TO DENT, OUT OF LIMITS IAW COOPESA EO COO-3 53-55SDR P2EA97096Angle · corrodedSJO - DISCREPANCY FOUND DURING SCHEDULED C-CHECK MAINTENANCE, SKIN BULGED AT LOWER FUSELAGE STATION 947.5, BETWEEN STRINGER 24 LEFT AND STRINGER 26 LT. REPLACED T-ANGLE AT STATION 947.5 BETWEEN STRINGER 24 AND STRINGER 26 LEFT IAW SRM 51-10-01 AND SRM 51-30-0SDR P2EA97095Skin · crackedSJO - DURING C-CHEC, FOUND NR 5 L/E SLAT HAS A LOOSE RIVET AND A CRACK IN THE SLAT SKIN, LOWER SURFACE LEADING EGE AT OUTBOARD AUXILLARY TRACK. REPAIRED NR 5 SLAT LEADING EDGE LOWER SKIN CRACK AND LOOSE RIVET IAW COOPESA EO COO-3-57-557-97, DATED 12-10-97 ANDSDR P2EA97077Lock Actuator · brokenFLT 635 - MDW - DURING INITIAL GEAR EXTENSION ON APPROACH TO MDW FROM MCI, THE GREEN LIGHT FOR THE NOSE GEAR DID NOT ILLUMINATE AND THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. PERFORMED CHECKLIST AND CYCLED THE GEAR AND RECEIVED NORMAL INDICATIONS, NORMAL L
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