Boeing 737-244

Service difficulty reports · 176

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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"

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SDR P2EA98195Seat Track · corrodedSJO - PAX CABIN SEAT TRACK CORRODED FROM BS 847 TO BS 947, RBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 847 TO BS 947 RBL 45 INCHES PER SRM 51-10-1 PAGE 5, 51-30-2, AND 53-10-5 FIG 2. (M)Oct 15, 1998 · N620PC · Boeing 737244 · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZM858Seat Track · corrodedSJO - PAX SEAT TRACK SECTION CORRODED FROM BS 727B TO BS 767, LBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 727B TO BS 767, LBL 45 INCHES, WL 208.1 PER SRM 51-10-1 PAGE 5, 51-30-2 AND 53-10-5 FIG 2. (M)Oct 15, 1998 · N620PC · Boeing 737244 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98199Skin · damagedSJO - PROVISIONAL FUSELAGE SKIN REPAIR FROM BS 1020 TO BS 1035, BETWEEN STRINGER 22 LT AND STRINGER 24 RT NOT COMPLIANT WITH THE SRM. REPAIRED FUSELAGE SKIN SECTION FROM BS 1020 TO BS 1035, BETWEEN STRINGER 2 LT AND STRINGER 24 LT PER SRM 53-30-3 FIG 16. (MOct 13, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98198Skin · damagedSJO - PROVISIONAL FUSELAGE SKIN REPAIR FROM BS 1036 TO BS 1051, BETWEEN STRINGERS 20 RT AND 23 RT NOT IN COMPLIANCE WITH SRM. REPAIRED FUSELAGE SKIN SECTION FROM BS 1035 TO BS 1054, BETWEEN STRINGER 19 RT AND 23 RT PER SRM 53-30-3 FIG 7. (M)Oct 13, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98251Skin · dentedSJO - LEFT WING OUTBOARD FOREFLAP WORN AND DENTED. DEFECT SIZE, VARIOUS. REPAIRED LEFT WING OUTBOARD FOREFLAP PER COOPESA EO COO-3-57-583-98 DATED OCT 21, 1998. REPAIRED LEADING EDGE PER SRM 57-50-4 FIG 1. (M)Oct 11, 1998 · N620PC · Boeing 737244 · Trailing Edge FlapsSDR P2EA98249Skin · damagedSJO - NR 5 SLAT DELAMINATED UPPER AND LOWER SKIN. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-573-98 DATED OCT 17, 1998. (M)Oct 11, 1998 · N620PC · Boeing 737244 · Leading Edge DevicesSDR P2EA98248Skin · damagedSJO - LEFT AILERON DELAMINATED AND WITH HAIL DAMAGE, DEFECT SIZE VARIOUS. REPAIRED LEFT AILERON PER COOPESA EO COO-3-57-565-98 DATED OCT 15, 1998. (M)Oct 11, 1998 · N620PC · Boeing 737244 · AileronsSDR P2EA98232Skin · damagedSJO - PROVISIONAL FUSELAGE SKIN REPAIR AT BS 901, BETWEEN STRINGER 24 LT AND STRINGER 26 LT PER COOPESA EO C00-3-53-591-98 DATED OCT 27, 1998 AND BOEING FAX C00-SJO-98-0830RR DATED OCT 26, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Oct 11, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98231Skin · damagedSJO - PROVISIONAL FUSELAGE SKIN REPAIR AT BS 1016, BETWEEN STRINGER 12 LEFT AND STRINGER 15 LEFT. REPLACED FUSELAGE SKIN SECTION FROM BS 989 TO BS 1016, BETWEEN STRINGER 10 LEFT AND STRINGER 14 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. REPAIRED FUSELAGE SKIOct 11, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98228Skin · delaminatedSJO - UPPER SKIN DELAMINATED INBOARD MID FLAP TRAILING EDGE. REPLACED LEFT WING, INBOARD MID FLAP TRAILING EDGE UPPER SKIN. (M)Oct 11, 1998 · N620PC · Boeing 737244 · Trailing Edge FlapsSDR P2EA98191Skin · disbondedSJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 286 TO BS 303, BETWEEN STRINGER 4RT AND STRINGER 5 RT. REPAIRED FUSELAGE INTERNAL DOUBLER FROM BS 286 TO BS 303 PER SRM 53-30-3, FIG 17, DETAIL 1. (M)Oct 9, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98190Skin · disbondedSJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 344 TO BS 360, BETWEEN STRINGER 6 RT AND STRINGER 7 RT. REPAIRED FUSELAGE SKIN INTERNAL DOUBLER FROM BS 344 TO BS 360, BETWEEN STRINGER 6 RT AND STRINGER 7 RT PER SRM 53-30-3, FIG 17, DETAIL 1. (M)Oct 9, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98189Skin · disbondedSJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 328 TO BS 338, BETWEEN STRINGER 4 LT AND STRINGER 6 LT. REPAIRED INTERNAL DOUBLER FROM BS 328 TO BS 338, BETWEEN STRINGER 4 LT AND STRINGER 6 LT PER SRM 53-30-03, FIG 17 DETAIL 1. (M)Oct 9, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98242Floorbeam · corrodedSJO - FLOORBEAM UPPER AND LOWER CHORD CORRODED AT BS 360, RBL 53. REPAIRED FLOORBEAM UPPER CHORD AT BS 360, BETWEEN RBL 47 INCH AND RBL 60 INCH PER SRM 53-10-9 FIG 7. REMOVED CORROSION AT LOWER CHORD AT BS 360, RBL 53 INCH AND FOUND WITHIN LIMITS PER SRM 51-Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA98230Skin · crackedSJO - FORWARD SERVICE DOOR (R1) UPPER HINGE CUTOUT CRACKED, DEFECT SIZE, CANNOT DETERMINE. REPAIRED FUSELAGE SKIN FROM BS 286.5 TO BS 292.5, BETWEEN STRINGER 9 RT AND STRINGER 13 RT. (M)Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98221Floorbeam · corrodedSJO - FLOORBEAM UPPER CHORD CORRODED AT BS 947, FROM RBL 45 INCHES TO RBL 53 INCHES. REPAIRED FLOORBEAM UPPER CHORD AT BS 947, FROM LBL 60 INCH TO RBL 60 INCH PER BOEING FAX COO-SJO-98-0764RR DATED OCT 12, 1998 AND COOPESA EO COO-3-53-569-78 DATED OCT 15, 199Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA98208Skin · crackedSJO - AFT SERVICE DOORWAY, LOWER HINGE CUTOUT CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .625 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 946 TO BS 956, BETWEEN STRINGER 13 RT AND STRINGER 16 RT PER SRM 53-30-3 FIG 33. (M)Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98203Floorbeam · corrodedSJO - PAX CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 55. REPLACED FLOORBEAM UPPER FLANGE AT BS 344 BETWEEN LBL 67 INCH TO RBL 41 INCH PER SRM 53-10-9 FIG 5, AND SRM 51-10-1 PAGE 5. (M)Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA98186Frame · crackedSJO - FUSELAGE FRAME CRACKED AT BS 927, STRINGER 2 RT, DEFECT SIZE, LENGTH=.500 INCH. REPAIRED FRAME SECTION BS 927, BETWEEN STRINGER 2RT AND STRINGER 3 RT PER SRM 53-10-04 FIG 10. (M)Oct 6, 1998 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA98229Floorbeam · crackedSJO - FLOORBEAM CRACKED IN MULTIPLE PLACES FROM BS 663 AND BS 673, LBL 24 INCHES, AVERAGE DEFECT SIZE, LENGTH .312 INCH. REPAIRED FLOORBEAM UPPER CHORD FROM BS 660 AND BS 681, LBL 24.82. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA98219Rib · crackedSJO - RIGHT WING NR 3 FUEL TANK RIB CRACKED IN AFT SECTION BETWEEN REAR SPAR AND STRINGER 2, WBL 135.5 DEFECT SIZE, LENGTH 1 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5 BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATEDOct 5, 1998 · N620PC · Boeing 737244 · Wing, Rib/BulkheadSDR P2EA98218Skin · corrodedSJO - FUSELAGE SKIN CORRODED AND DISBONDED FROM BS 244 TO BS 259, STRINGER 25LT, WL 154, LBL 19. REPAIRED FUSELAGE SKIN FROM BS 235.8 TO BS 259.5, BETWEEN STRINGER 24 LT AND STRINGER 26LT PER COOPESA EO COO-3-53-577-98 DATED OCT 19, 1998 AND BOEING FAX COO-SJOct 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98210Splice · crackedSJO - INTERIOR FUSELAGE SPLICE CRACKED AT BS 663.75, STRINGER 6 LT, DEFECT SIZE LENGTH .25O INCH. REPLACED FUSELAGE SPLICE FROM BS 657 TO BS 669, STRINGER 6 LEFT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98209Splice · crackedSJO - INTERIOR FUSELAGE SPLICE 5-7R CRACKED AT BS 663.75, DEFECT SIZE LENGTH .25 INCH. REPLACED FUSELAGE SPLICES FROM BS 657 AND BS 669, BETWEEN STRINGER 6 LT AND STRINGER 7 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98206Skin · disbondedSJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 462 TO BS 464, BETWEEN STRINGER 13 LT AND STRINGER 14 LT. REPAIRED FUSELAGE SKIN INTERNAL DOUBLER FROM BS 400 TO BS 500, BETWEEN STRINGER 10 LT AND STRINGER 14 LT PER BOEING SERVICE BULLETIN 737-53-1048, Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98204Seat Track · corrodedSJO - PAX CABIN SEAT TRACK AND ANGLE CORRODED FROM BS 344 TO BS 380, LBL 46 INCHES AND LBL 63 INCHES. REPLACED SEAT TRACK SECTION BETWEEN BS 344 AND BS 380, LBL 46 INCHES PER SRM 53-10-5 FIG 2, 51-10-1 PAGE 5, AND 51-30-2. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98200Rib · crackedSJO - LEFT WING NR 1 FUEL TANK RIB CRACKED AT WBL 135.5 IN AFT SECTION, BETWEEN REAR SPAR AND STRINGER 16. REPAIRED LEFT WING LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SB 737-57-1186 DATED APRIL 13, 1989 SECTION 3, PART 3, FIG 3. Oct 5, 1998 · N620PC · Boeing 737244 · Wing, Rib/BulkheadSDR P2EA98194Seat Track · corrodedSJO - PASSENGER CABIN SEAT TRACK CORRODED FROM BS 344 TO BS 420, LBL 25, WL 208.1. REPLACED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 51-10-1 PAGE 5, 51-10-2, 53-10-5 FIG 2. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA98178Stringer · crackedSJO - STRINGER 5 RT CRACKED AT BS 685, DEFECT SIZE .375 INCH LENGTH. FUSELAGE STRINGER 5 RT REPAIRED BETWEEN BS 679 TO BS 691 PER SRM 53-10-3, FIG 4. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Main, Longeron/StringerSDR 98ZZZM836Angle · corrodedSJO - PAX CABIN SEAT TRACK AND ANGLE CORRODED FROM BS 344 TO BS 380, LBL 46 INCHES AND LBL 63 INCHES. REPLACED SEAT TRACK SECTION BETWEEN BS 344 AND BS 380, LBL 46 INCHES PER SRM 53-10-5 FIG 2, 51-10-1 PAGE 5, AND 51-30-2. (M)Oct 5, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98241Skin · wornSJO - RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTION WORN. REPAIRED RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTION FROM WS 493 TO WS 505 PER SRM 57-50-4 FIG 1. (M)Oct 4, 1998 · N620PC · Boeing 737244 · Leading Edge DevicesSDR P2EA98234Skin · wornSJO - RIGHT WING OUTBOARD FORE FLAP LEADING EDGE SKIN WORN. REPAIRED RIGHT WING FORE FLAP LEADING EDGE SKIN FROM WSL 490 TO WSL 505, PER SRM 57-50-4 FIG 1. (M)Oct 4, 1998 · N620PC · Boeing 737244 · Trailing Edge FlapsSDR P2EA98188Beam · crackedSJO - C1 DOOR BEAM NR 5 CRACKED, DEFECT SIZE=.500 INCH. REPAIRED C1 DOOR NR 5 BEAM, PER SRM 51-40-3, FIG 1. (M)Oct 4, 1998 · N620PC · Boeing 737244 · Cargo/Baggage DoorsSDR P2EA98182Skin · lightning strikeSJO - LIGHTING STRIKE DETECTED IN FUSELAGE SKIN SECTION AT BS 312, STRINGER 3 LEFT, DEFECT SIZE .125 INCH LENGTH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 310 AND BS 314 AT STRINGER 3 LEFT PER SRM 53-30-03, FIG 5. (M)Oct 4, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98226Skin · disbondedSJO - FUSELAGE SKIN DISBONDED FROM BS 259 TO BS 360, STRINGER 24 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 259 TO BS 360, BETWEEN STRINGER 24 RT AND BL 0 PER SRM 51-10-1 PAGE 5, SRM 51-30-2 PAGE 1. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98225Fitting · wornSJO - FORWARD ENTRY DOOR AFT LOWER STOP FITTING WORN. FORWARD ENTRY DOOR LOWER AFT STOP FITTING REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Passenger/Crew DoorsSDR P2EA98223Skin · damagedSJO - FUSELAGE SKIN MISSING MATERIAL AT BS 178, BETWEEN BL 0 TO RBL 6 INCH, WL 231. REPLACED FUSELAGE SKIN DOUBLER FROM BS 178 AND BS 188, FROM RBL 9 INCH TO LBL 9 INCH PER BOEING SERVICE BULLETIN 737-53-1059 REV 1 DATED MAY 17, 1990, SECTION 3. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98217Skin · damagedSJO - HOLE FOUND IN FUSELAGE OUTER SKIN SECTION AT BS 203, RBL 7 INCH AND WL 153 INCH, DEFECT SIZE LENGTH .75 INCH WIDTH .437 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 192.5 TO BS 203, BETWEEN BL 0 AND RBL 17 INCH, WL 153 PER SRM 53-30-3 FIG 6. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98213Frame · dentedSJO - FORWARD CARGO COMPARTMENT FRAME DENTED AT BS 500A, BETWEEN STRINGER 23 RT AND STRINGER 24 RT. REPAIRED FORWARD CARGO COMPARTMENT FRAME, UPPER FLANGE AT BS 500A, BETWEEN STRINGER 23 RT AND STRINGER 24 RT PER SRM 51-40-3, FIG 1, PAGE 5. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA98187Skin · damagedSJO - FUSELAGE SKIN WITH MISSING MATERIAL AT BS 1104, WL 223, RBL 23, DEFECT SIZE = .75 INCH. REPAIRED FUSELAGE SKIN BETWEEN BS 1095 AND BS 1108, WL 217 TO WL 223, RBL 23 INCH PER SRM 53-30-03 FIG 3. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98184Fitting · wornSJO - L1 ENTRY DOOR LOWER STOP FITTING WORN. REPLACED STOP FITTING PER SRM 51-10-01 PAGE 5 AND SRM 51-30-2. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98181Stringer · corrodedSJO - STRINGER 23RT CORRODED BETWEEN BS 259.5 TO BS 294.5, DEFECT SIZE 35 INCHES IN LENGTH. REPAIRED FUSELAGE STRINGER SECTION BETWEEN BS 259 AND BS 313 PER SRM 53-10-03 FIG 1 SHEET 7. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Longeron/StringerSDR P2EA98180Stringer · crackedSJO - STRINGER 25 LT CRACKED AT BS 927, DEFECT SIZE .375 INCH. REPAIRED FUSELAGE STRINGER SECTION BETWEEN BS 920 AND BS 933 PER SRM 53-10-03 FIG 1 SHEET 6. (M)Oct 3, 1998 · N620PC · Boeing 737244 · Fuselage Main, Longeron/StringerSDR P2EA98220Beam · crackedSJO - VERTICAL BEAM CRACKED IN AFT CARGO COMPARTMENT AT BS 727, LBL 18 INCHES, WL 150. DEFECT SIZE LENGTH 1 INCH. REPAIRED FUSELAGE BULKHEAD VERTICAL BEAM SECTION AT BS 727, LBL 18, WL 150 PER SRM 51-40-4 FIG 2. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98216Beam · wornSJO - RIGHT WING TRUNNION SUPPORT BEAM WORN AT RSS 222. REPAIRED RIGHT WING MAIN LANDING GEAR BEAM UPPER FORWARD FLANGE SECTION PER BOEING FAX COO-SJO-98-0761RR DATED OCT 12, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Wing Miscellaneous StructureSDR P2EA98215Skin · cannedSJO - FUSELAGE SKIN OIL CANNED FROM BS 345 TO BS 360, BETWEEN STRINGER 16 RT AND STRINGER 19 RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 311 TO BS 360, BETWEEN STRINGER 15 RT AND STRINGER 19 RT PER COOPESA EO COO-3-53-570-98 DATED OCT 16, 1998 AND BOEING FAX COct 2, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98212Skin · dentedSJO - C1 DOOR SKIN DENTED, SCRATCHES AND PROVISIONAL REPAIRS, DEFECT SIZE AVERAGE .200 INCH. REPLACED C1 DOOR SKIN PER SRM 52-30-2 FIG 3. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Cargo/Baggage DoorsSDR P2EA98211Stiffener · wornSJO - RIGHT WING REAR STIFFENER WORN AT RSS 155. REPLACED RIGHT WING REAR SPAR STIFFENER AT RSS 155 PER SRM 51-10-1 PAGE 5, AND SRM 51-30-2. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Wing Miscellaneous StructureSDR P2EA98205Door Frame · dentedSJO - C1 DOOR FRAME DENTED AT BS 500B, STRINGER 25 RT, DEFECT SIZE LENGTH 1 INCH WIDTH .135 INCH. REPAIRED C1 DOOR FRAME AT BS 500B, BETWEEN STRINGER 22 RT AND STRINGER 25 RT PER SRM 51-40-3 FIG 1 PAGE 5. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA98179Skin · corrodedSJO - FUSELAGE SKIN SECTION CORRODED AT BS 815, STRINGER 20 LT. REPAIRED FUSELAGE LAP JOINT SKIN SECTION BETWEEN BS 809 AND BS 854, BETWEEN STRINGERS 19 LT AND 21 LT DUE TO CORROSION PER SRM 53-30-3 FIG 15. (M)Oct 2, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/Skin
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