Boeing 737-244

Service difficulty reports · 176

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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 = '737244'
  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.

SDR P2EA98250Fitting · crackedSJO - BS 685 RT FRAME FITTING CRACKED. REPLACED FUSELAGE FRAME FITTING AT BS 685 RT FROM WL 186 TO WL 255 PER BOEING FAX COO-SJO-98-0632RR DATED SEPT 16, 1998. (M)Oct 1, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98214Skin · corrodedSJO - FUSELAGE SKIN CORRODED FROM BS 259.5 TO BS 360, BETWEEN STRINGER 19 RT AND STRINGER 24 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 259.5 AND BS 360, BETWEEN STRINGER 19 RT AND STRINGER 24 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Sep 30, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98150Skin · corrodedSJO - EXTERNAL FUSELAGE SKIN WITH MATERIAL LOSS MORE THAN 10 PERCENT IN SEVERAL PLACES DUE TO CORROSION AT STRINGER 20L FROM BS 767 TO BS 887. REMOVED CORROSION FROM FUSELAGE SKIN FROM BS 747 TO BS 832 AND BS 854 TO BS 881 AT STRINGER 20L IN REFERENCE TO SRM Aug 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98154Skin · crackedSJO - UPPER FUSELAGE BS 188, DOUBLER BELOW LEFT WINDSHIELD CENTER POST CRACKED. REPAIRED IAW BOEING S/B 737-53-1059. (M)Aug 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98153Angle · corrodedSJO - PASSENGER CABIN FORWARD NR 2 GALLEY FLOOR ANGLE WITH CORROSION. REPLACED ANGLE IN REFERENCE TO SRM 51-10-1 PAGE 5. (M)Aug 5, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98152Skin · crackedSJO - REPAIR INTERNAL DOUBLER AT BS 727A STRINGER 16R. REPAIRED FUSELAGE SKIN DUE TO CRACK FROM BS 727 PLUS 11 INCHES TO BS 727 PLUS 4 INCHES, BETWEEN STRINGERS 15R AND 19R IN REFERENCE TO SRM 53-30-3 FIG 17 DETAIL 5. (M)Aug 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98151Skin · crackedSJO - CRACKED SKIN AROUND FASTENER, EXTERNAL FUSELAGE BS 727A BETWEEN STRINGER 14R AND 15R. REPAIRED FUSELAGE SKIN CRACK AT BS 727A BETWEEN STRINGER 14R AND 15R IN REFERENCE TO SRM 53-30-3 FIGURE 17. (M)Aug 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98149Skin · crackedSJO - REPAIR L1 LOWER DOUBLER, FORWARD LOWER CORNER. REPAIRED FORWARD ENTRY DOOR EXTERNAL SKIN CRACK AT FORWARD LOWER CORNER BETWEEN BS 312 AND BS 318 FROM WL 212 TO WL 218 IN REFERENCE TO SRM 52-00-3 FIG 6. (M)Aug 4, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98127Wire · brokenMCI - FLT 303 - EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARM POSITION. REPAIRED BROKEN WIRE ON EMERGENCY EXIT SWITCH IN AFT GALLEY, OPS CHECK NORMAL. (M)Jul 19, 1998 · N620PC · Boeing 737244 · Light System WiringSDR P2EA98106Mechanism · out of adjustMCI - FLT 703 - NR 1 LEADING EDGE SLAT NOT EXTENDED WITH FLAPS AT 1 DEGREE. ADJUSTED NR 1 SLAT MID EXTEND DETENT ARMS PER MM 27-81-21. LEADING EDGE SLATS CHECK NORMAL PER MM 27-81-0. (M)May 11, 1998 · N620PC · Boeing 737244 · Leading Edge Slat Control SystemSDR P2EA98104Cover · crackedFLT 804 - MDW - NO EMERGENCY DECLARED LANDING NORMAL. GOT HAZY VAPOR IN CABIN DURING FLIGHT. FOUND NR 1 BEARING ACCESSORY COVER CRACKED ON NR 1 ENGINE, REPLACED COVER PER PWA M/M 72-23. PERFORMED ENGINE RUN NO LEAKS OR HAZE NOTED. (M)May 7, 1998 · N620PC · Boeing 737244 · Turbine Engine Compressor SectionSDR P2EA98101Check Valve · failedFLT 119 - MCI - NO EMERGENCY DECLARED LANDING NORMAL. WITH CENTER FUEL TANK BOOST PUMPS ON, RIGHT MAIN TANK CONTINUES TO FEED ON CLIMB-OUT DURING CRUISE, CENTER TANK TAKES ON FUEL WITH CENTER TANK BOOST PUMPS OFF. REPLACED RIGHT CENTER TANK BOOST PUMP CHECK May 1, 1998 · N620PC · Boeing 737244 · Aircraft Fuel Distribution SystemSDR P2EA98041Light · inoperativeATL - DISCREPANCY FOUND DURING SCHEDULED MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING INOP, SEAT ROW 11 AND AFT. REPAIRED WIRING AT ROW 18 AND AFT BULKHEAD. REPLACED FUSES IN FWD AND AFT BATTERY PACKS. (M)Mar 24, 1998 · N620PC · Boeing 737244 · Emergency LightingSDR P2EA98029Skin · dentedSJO - DURING C-CHECK, UPPER FUSELAGE DENTED SKIN SECTION OUT OF LIMITS AT STATION 397, BETWEEN STRINGERS 2 AND 3 LEFT. REPAIRED DAMAGED SECTION PER SRM 53-30-3, FIG 7. (M)Feb 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98027Frame · crackedSJO - DURING C-CHECK, FOUND TAIL COMPARTMENT STATION 1040, STRINGER 8R, FRAME HAS CRACKS. REPAIRED FRAME AT STATION 1040, BETWEEN STRINGE 8 AND 10 RT, PER SRM 53-10-4, FIG 4. (M)Feb 4, 1998 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA98032Skin · delaminatedSJO - DURING C-CHECK, FOUND RUDDER UPPER AFT TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-6, FIG 2, BALANCE OK PER SRM 51-80-1, POINT 2, FIG 8. (M)Feb 3, 1998 · N620PC · Boeing 737244 · Rudder, Plate/SkinSDR P2EA98031Skin · delaminatedSJO - DURING C-CHECK, RT AILERON UPPER AND LOWER SURFACES DELAMINATED AT SEVERAL PLACES. REPAIRED PER SRM 51-40-6, FIG 11. AILERON BALANCED PER SRM 51-80-1. AILERON REMOVED AND INSTALLED PER MM 27-11-11. (M)Feb 3, 1998 · N620PC · Boeing 737244 · AileronsSDR P2EA98030Skin · dentedSJO - DURING C-CHECK ITEM, UPPER FUSELAGE, DENTED SKIN SECTION OUT OF LIMITS AT BS 434 BETWEEN STRINGERS 1 AND 2L. REPAIRED DAMAGED SECTION IAW SRM 53-30-3 FIG 5. (M)Feb 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98028Rib · crackedSJO - DURING C-CHECK, FOUND RT W/W AT STATION 695, W/L 196, RIB WITH OUTBOARD CHORD CRACKED. REPAIRED OUTBOARD CHORD PER SRM 51-40-3. FIG1. (M)Feb 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, BulkheadSDR P2EA98025Skin · dentedSJO - DURING C-CHECK, FOUND UPPER FUSELAGE DENTED SKIN SECTION OUT OF LIMITS AT BS 890 BELOW STRINGER 21R. REPAIRED DAMAGED SECTION IAW SRM 53-30-3 FIG 5. (M)Feb 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98001Panels · missingPIT - FLT 424 - DURING POST FLIGHT WALKAROUND INSPECTION, 2 AFT COWLING PANELS WERE NOTED MISSING ON NR 2 ENGINE. REPLACED MISSING COWLING PANELS. SECURED LATCHES. NO OTHER DEFECTS NOTED. A/C OK FOR SERVICE. COWL PANELS DEPARTED A/C DURING T/O ROLL AT MDWJan 1, 1998 · N620PC · Boeing 737244 · Engine Cowling SystemSDR 98ZZZM85Panels · missingPIT - FLT 424 - DURING POST FLIGHT WALKAROUND INSPECTION, 2 AFT COWLING PANELS WERE NOTED MISSING ON NR 2 ENGINE. REPLACED MISSING COWLING PANELS. SECURED LATCHES. NO OTHER DEFECTS NOTED. A/C OK FOR SERVICE. COWL PANELS DEPARTED A/C DURING T/O ROLL AT MDWJan 1, 1998 · N620PC · Boeing 737244 · Engine Cowling SystemSDR P2EA97076Pack · failedMSP - FLT 707 - RETURNED TO GATE, NO EMERGENCY DECLARED. AFTER STARTING NR 1 ENGINE AND TURNING THE RIGHT PACK ON, THE MAIN CABIN FILLED UP WITH AN ODORLESS HAZE. DEFERRED RIGHT A/C PACK PER MEL 21-1. DISCONNECTED RT PACK CANNON PLUG, D492, AND SLOWED. RIGNov 17, 1997 · N620PC · Boeing 737244 · Cabin Cooling SystemSDR P2EA97070Bushing · leakingDEN - FLT 327 - AIR RETURN, NR 2 ENGINE INFLIGHT SHUT DOWN. EMERGENCY DECLARED, RETURNED TO DENVER. LANDING UNEVENTFUL. NR 2 ENGINE LOW PRESSURE LIGHT CAME ON AND OIL PRESSURE GAUGE DROPPED TO 20 PSI. OIL QUANTITY DROPPED TO ZERO. WINDMILLING INSPECTION REOct 10, 1997 · N620PC · Boeing 737244 · Turbine Engine Accessory DriveSDR P2EA97065Actuator · malfunctionedMCI - FLT 343 - NO EMERGENCY DECLARED, NORMAL LANDING ACCOMPLISHED. ACFT ROLLS TO RIGHT (10 DEGREES) WITH FLAPS 5. SAME AT FLAPS 10, AT FLAPS 15, INCREASES TO 15 DEGREES. REMAINS THE SAME AT FLAPS 25 AND 30. TEST FLT RESULTS, INSPECTED OTBD SEQ CARRIAGES PAug 8, 1997 · N236TA · Boeing 737244 · Drag Control ActuatorSDR P2EA97062Egt Indicator · malfunctionedFLT 302 - MCI - ABORTED TAKEOFF, RETURNED TO GATE, NO EMERGENCY DECLARE. REJECTED T/O AT 100 KTS DUE TO NR 1 EGT AND 620 CELSIUS AND RISING WITH N1 REDUCTION TO 93 PERCENT. PERFORMED MX ENG RUN AT T/O POWER 2.04 EPR NR 1 EGT 590 CELSIUS, NR 2 EGT 560 CELSIUSJul 25, 1997 · N236TA · Boeing 737244 · Engine EGT/TIT Indicating System
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