Boeing 737-281
Service difficulty reports · 120
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 = '737281' 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 = '737281' 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 P2EA98306Skin · delaminatedSJO - NR 2 SPOILER DELAMINATED, DEFECT SIZE TOTAL 6 SQUARE INCH. REPAIRED NR 2 SPOILER PER COOPESA EO COO-3-57-710-98 DATED NOV 30, 1998. (M)SDR P2EA98303Skin · delaminatedSJO - NR 7 SPOILER DELAMINATED, DEFECT SIZE TOTAL 325 SQUARE INCH. REPAIRED NR 7 SPOILER PER COOPESA EO COO-3-57-711-98 DATED NOV 30, 1998. (M)SDR P2EA98298Spoiler · delaminatedSJO - NR 8 SPOILER DELAMINATED, DEFECT SIZE TOTAL 320 SQ IN. REPAIRED NR 8 SPOILER PER COOPESA EO C00-3-57-713-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98295Spoiler · delaminatedSJO - NR 6 SPOILER DELAMINATED, DEFECT SIZE TOTAL 160 SQ INCH. REPAIRED NR 6 SPOILER PER COOPESA EO COO-3-57-712-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98294Skin · damagedSJO - FUSELAGE SKIN DOUBLER MISSING MATERIAL AT BS 178, WL 243, BETWEEN LBL 2 INCH AND LBL 7 INCH. REPLACED WINDOW CENTER POST DOUBLER AT BS 178, SL 243, BETWEEN LBL 7 INCH AND RBL PER BOEING SERVICE BULLETIN 737-53-1059 REV 1, SECTION III, FIG 2 DATED MAY 17SDR P2EA98267Stringer · crackedSJO - STRINGER 15 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED STRINGER 15 LEFT SECTION FROM BS 348 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98266Stringer · crackedSJO - STRINGER 14 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED FUSELAGE STRINGER 14 LT SECTION FROM BS 367 TO BS 348 PR SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98265Frame · crackedSJO - FRAME WEB CRACKED AT BS 303.9, BETWEEN STRINGER 16L AND STRINGER 17L, DEFECT SIZE, LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION AT BS 303.9, BETWEEN STRINGER 15 LEFT AND B STRINGER 18 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98293Stringer · corrodedSJO - FOUND CORROSION AT BS 727A, STRINGER 22 LEFT, LOWER CHORD, DEFECT SIZE LENGTH 2.5 INCH WIDTH 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 PLUS 11 INCH AND BS 727A PLUS 8 INCH, BETWEEN STRINGER 21 LEFT AND STRINGER 23 LEFT PER SRM 53-30-3, FIG 6. SDR P2EA98273Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS 907 AND BS 967, BETWEEN STRINGER 4 RT AND STRINER 5 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 902.5 TO BS 914, BETWEEN STRINGER 4 RT AND STRINGER 5 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. REMOVED CORROSION FROM BS 907 TOSDR P2EA98268Beam · crackedSJO - FORWARD SERVICE DOOR NR 7 BEAM CRACKED, DEFECT SIZE LENGTH .5 INCH. REPAIRED FUSELAGE SKIN FORWARD ENTRY DOOR BEAM NR 7 BETWEEN BS 302 AND BS 309 PER SRM 51-40-3 FIG 1. (M)SDR P2EA98264Frame · crackedSJO - FRAME CRACKED AT BS 344, BETWEEN STRINGER 23 RT AND STRINGER 24 RT, DEFECT SIZE LENGTH 6.75 INCH. REPLACED FRAME SECTION AT BS 344, BETWEEN STRINGER 21 RT AND STRINGER 27 RT PER 51-10-1 PAGE 5 AND SRM 51-30-2. REPAIRED FUSELAGE FRAME ANGLE SECTION AT BSDR P2EA98301Seat Track · crackedSJO - SEAT TRACK CRACKED AT BS 709, RBL 25 INCHES, WL 203.1, DEFECT SIZE LENGTH .625 INCH. REPAIRED FLOORBEAM SECTION FROM BS 698 AND BS 717, RBL 25 INCHES PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991 SECTION III FIG 5 AND BOEING FAX COO-SJO-98SDR P2EA98299Seat Track · crackedSJO - SEAT TRACK LOWER CHORD CRACKED AT FROM BS 663.75 TO BS 690 AT RBL 24.5, DEFECT SIZE LENGTH .563. REPAIRED FLOORBEAM UPPER CHORD BETWEEN BS 660 AND BS 682, LBL 24.82 PER BOEING INSTRUCTION LIST OF DATE INCLUDED ON FAA FOR 8110-3 AND COOPESA EO COO-3-57-6SDR P2EA98291Angle · crackedSJO - ANGLE CRACKED AT BS 559, RBL 46, WL 205 DEFECT SIZE LENGTH .4375. REPLACED FUSELAGE LOWER CHORD AT BS 559, WL 204, BETWEEN RBL 46 INCHES AND RBL 70 INCHES PER BOEING SERVICE BULLETIN 737-53-1061, REV 4, SECTION 111 FIG 2 DATED JULY 16, 1992. (M)SDR P2EA98290Floorbeam · crackedSJO - FLOORBEAM CRACKED AT BS 578, RBL 50, WL 206, DEFECT SIZE .5 INCH. REPAIRED FLOORBEAM WEB AT BS 578, BETWEEN RBL 45 INCHES TO RBL 70 INCHES, FROM WL 208 TO WL 204 PER SRM 51-30-2 AND 51-10-1 PAGE 5. (M)SDR P2EA98280Web · crackedSJO - WEB CRACKED AT BS 663.75, RBL 0, WL 206. DEFECT SIZE LENGTH 1.5 INCH. REPAIRED CENTER WING BOX, FLOORBEAM UPPER CHORD BETWEEN BS 650 AND BS 675, BL 0 PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991, SECTION III FIG 4. (M)SDR P2EA98274Rib · crackedSJO - RIB CRACKED AT RIGHT WING FUEL TANK WBL 135.5, DEFECT SIZE LENGTH 1.125 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATED 4-13-98, SECTION III, PART 3 FIG 3. (M)SDR P2EA98270Seat Track · crackedSJO - SEAT TRACK WEB CRACKED AT BS 639, RBL 45.5, WL 201, DEFECT SIZE LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION FROM BS 636 TO BS 642, FROM WL 204 TO WL 199.5, RBL 45.5 PER 51-40-2 FIG 1 PAGE 3. (M)SDR P2EA98269Stringer · crackedSJO - STRINGER 5 LEFT SPLICE CRACKED AT BS 360, DEFECT SIZE LENGTH .75 INCH. REPLACED FUSELAGE STRINGER 5 LEFT SPLICE FROM 348.2 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98260Angle · crackedSJO - RIGHT EMERGENCY EXIT DOOR FRAME ANGLE CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .375 INCH. REPLACED RIGHT EMERGENCY EXIT DOOR FORWARD FRAME ANGLE AT BS 622 PER SRM 51-10-01 PAGE 1 AND SRM 51-30-2. (M)SDR P2EA98258Skin · damagedSJO - LEFT WING OUTBOARD FOREFLAP LEADING EDGE SKIN REPAIR DOUBLER WORN. REPAIRED FOREFLAP LEADING EDGE SKIN BETWEEN WSL 493 AND WSL 488 PER SRM 57-50-4 FIG 1. (M)SDR SIMA98257Skin · crackedSJO - FORWARD RIGHT UPPER HINGE CUTOUT CRACKED AT BS 310, DEFECT SIZE LENGTH .50 INCH. REPAIRED FORWARD RIGHT SERVICE DOOR SKIN SECTION BETWEEN BS 308 AND BS 316, BETWEEN BEAM NR 3 AND BEAM NR 4 PER SRM 52-00-03 FIG 3. (M)SDR P2EA98308Skin · crackedSJO - INTERNAL DOUBLER CRACKED FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT, DEFECT SIZE LENGTH 1.937 INCH. REPAIRED FUSELAGE SKIN FROM BS 297 TO BS 305 BETWEEN STRINGER 9 LEFT AND STRINGER 11 LT PER COOPESA EO C00-3-53-723-98 DATED DEC 4, 1998 AND BOEING FAX COOSDR P2EA98302Web · crackedSJO - WEB CRACKED AT BS 253, LBL 8 INCHES DEFECT SIZE, LENGTH .375 INCH. REPAIRED FUSELAGE WEB SECTION BETWEEN BS 232 AND BS 257, WL 190 FROM BL 0 TO LBL 18 INCHES PER COOPESA EO COO-3-53-717-98 DATED DEC 2, 1998 AND BOEING FAX COO-SJO 98-1021RR DATED DEC 1, SDR P2EA98300Frame · crackedSJO - AFT ENTRY DOOR LOWER PAN SECTION CRACKED. DEFECT SIZE LENGTH 1.125 INCH. REPLACED AFT ENTRY DOOR FRAME AT BS 949 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98297Skin · canningSJO - AFT CARGO DOOR DENTED AND OL CANNED, DEFECT SIZE WIDTH 2.125 INCH DEPTH .060. REPLACED AFT CARGO DOOR OUTER SKIN BETWEEN BS 839 AND BS 887 PER SRM 51-10-1 PAGE 5 AND 51-20-2. (M)SDR P2EA98292Stringer · corrodedSJO - STRINGER 22 LEFT CORRODED BETWEEN BS 727 AND BS 727A, DEFECT SIZE LENGTH 3 INCH WIDTH .75 INCH. REPAIRED STRINGER 22 LEFT BETWEEN BS 727 AND BS 727A PLUS 13 INCHS PER SRM 53-10-3 FIG 1, SHEET 7. (M)SDR P2EA98288Skin · crackedSJO - INTERNAL DOUBLER CRACKED AT THE AFT SERVICE DOORWAY LOWER HINGE CUTOUT, DEFECT SIZE LENGTH .75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 939 TO BS 953, BETWEEN STRINGER 13 RT AND STRINGER 14 RT PER COOPESA EO COO-3-53-715-98 DATED DEC 2, 1998 AND BOESDR P2EA98281Frame · crackedSJO - FRAME CRACKED AT BS 578, WL 207, LBL 65, DEFECT SIZE LENGTH 5 INCH. REPLACED FUSELAGE FRAME SECTION AT BS 578, BETWEEN STRINGER 12 LEFT AND STRINGER 18 LEFT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98275Web · crackedSJO - NOSE LANDING GEAR WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 277 RBL 9 INCH, DEFECT SIZE LENGTH 5.25 INCH. REPAIRED NOSE WHEEL WELL UPPER WEB SECTION FROM BS 274.125 TO BS 280.300, BETWEEN RBL 4 INCH AND RBL 14 INCH PER BOEING FAX COO-SJO-98-1024RR DATSDR P2EA98271Skin · crackedSJO - MAIN ENTRY DOOR LOWER HINGE CUTOUT EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH .75 INCH. REPAIRED SKIN SECTION FROM BETWEEN BS 316.5 AND BS 324 AT LOWER HINGE CUT OUT PER SRM 52-00-3 FIG 6. (M)SDR P2EA98261Frame · crackedSJO - RIGHT FRAME CRACKED, AT E/E COMPARTMENT INTERNAL STRUCTURE AT BS 360, STRINGER 20 RT DEFECT SIZE LENGTH 3 INCHES. REPAIRED FUSELAGE FRAME SECTION AT BS 360, BETWEEN STRINGER 19 RT AND STRINGER 21 RT PER 51-40-3, FIG 1, DETAIL I. (M)SDR P2EA98259Angle · crackSJO - FORWARD ENTRY DOOR NR 7 BEAM ANGLE CRACKED, DEFECT SIZE LENGTH 1.625 INCH. REPAIRED FORWARD ENTRY DOOR NR 7 BEAM ANGLES BETWEEN BS 336 AND BS 346 PER SRM 51-40-3 FIG 1. (M)SDR P2EA98310Keel Beam · crackedSJO - KEEL BEAM CRACKED BETWEEN BS 727 AND 727A LEFT SIDE, DEFECT SIZE 4 INCH. REPAIRED KEEL BEAM LOWER CHORD BETWEEN BS 727 PLUS 4 AND BS 727A PLUS 6 PER COOPESA EO COOP-3-53-722-98 DATED DEC 3, 1998 AND BOEING FAX COO-SJO-98-1019RR DATED DEC, 1998. (M)SDR P2EA98309Rib · crackedSJO - NR 5 SLAT OUTBOARD RIB CRACKED AT FSS 480, DEFECT SIZE LENGTH 1.125 INCH. REPLACED LEADING EDGE CAVITY MAIN TRACK OUTBOARD RIB AT FSS 480 PER 51-10-1 PAGE 1 AND SRM 51-30-2. (M)SDR P2EA98289Stringer · crackedSJO - STRINGER 10 LEFT CRACKED AT BS 294.5 DEFECT SIZE LENGTH .625 INCH. REPAIRED FUSELAGE STRINGER 10 LEFT, FROM BS 275 TO BS 301 PER SRM 53-10-3, FIG 3. (M)SDR P2EA98287Fitting · crackedSJO - VERTICAL BEAM CRACKED AT BS 727, BETWEEN WL 208.5 AND WL 198.5 IN BL 0 INCH. DEFECT SIZE LENGTH 4 INCH. REPLACED FUSELAGE BULKHEAD PRESS UPPER FITTING AT BS 727, BL 0, BETWEEN WL 207 AND WL 198 PER BOEING SERVICE BULLETIN 737-53-1101, REV 2, SECTION IISDR P2EA98286Stiffener · crackedSJO - RIGHT HORIZONTAL STAB, STAB STATION 101.9, NR 4 STIFFENER LOWER CHORD CRACKED. DEFECT SIZE LENGTH 1.75 INCH. REPLACED STAB CHORD AT STAB STATION 101.9, BETWEEN FRONT AND REAR SPAR PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98285Web · crackedSJO - FUSELAGE BULKHEAD SKIN CRACKED AT BS 178, WL 219, RBL 15 INCH, DEFECT SIZE LENGTH 7 INCH. REPAIRED FUSELAGE WEB SECTION AT BS 178, FROM WL 210 TO WL 234, BETWEEN RBL 1.5 AND RBL 18 INCH PER SRM 53-10-11, FIG 1 SHEET 6, DETAIL III. (M)SDR P2EA98278Frame · crackedSJO - HORIZONTAL CHORD CRACKED AT BS 727, WL 202.5, LBL 26, DEFECT SIZE LENGTH 2.750 INCH. REPAIRED FUSELAGE BULKHEAD COMPRESSION CHORD AT BS 727, WL 202.5, BETWEEN LBL 18 INCH AND LBL 36 INCH PER BOEING SERVICE BULLETIN 737-53-1053, REV 5, DATED OCT 26, 1995SDR P2EA98277Support · crackedSJO - VERTICAL BEAM CRACKED AT BS 727, WL 197.5, RBL 26, DEFECT SIZE LENGTH 1 INCH. REPLACED BULKHEAD VERTICAL BEAM AT BS 727, RBL 26, BETWEEN WL 202, WL 151 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98276Beam · crackedSJO - VERICAL BEAM CRACKED AT BS 540, RBL 27, WL 203, DEFECT SIZE LENGTH 3.5 INCH. REPLACED FUSELAGE BULKHEAD VERTICAL BEAM AT BS 540, FROM WL 206 TO WL 151 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)SDR P2EA98272Frame · crackedSJO - BS 727 HORIZONTAL CHORD CRACKED AT WL 202.5, RBL 26, DEFECT SIZE LENGTH 2 INCHES. REPAIRED FUSELAGE BULKHEAD COMPRESSION CHORD AT BS 727, WL 202.5, BETWEEN RBL 18 INCH AND RBL 34 INCH PER BOEING SERVICE BULLETIN 737-53-1053 REV 5 DATED OCT 26, 1995 SECTSDR P2EA98233Pump · failedMCI - FLT 270 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. ON DESCENT INTO MCI, NR 2 OIL QTY STARTED TO DECREASE. ON APPROACH QTY WENT TO ZERO, OIL PRESSURE AND TEMPERATURE WERE WITHIN LIMITS. REPLACED NR 6 BEARING OIL SCAVENGE PUMPED PER PWA MM 72-50, DRAINSDR P2EA98304Skin · delaminatedSJO - RIGHT AILERON DELAMINATED, DEFECT SIZE TOTAL 20 SQUARE INCH. REPAIRED RIGHT AILERON PER COOPESA EO COO-3-57-703-98 DATED NOV 27, 1998. (M)SDR P2EA98177Bolt · mismanufacturedMCI - DURING ACCOMPLISHMENT OF AD 98-14-09, (S/B 737-54-1004), A DEFECT (POSSIBLE FRACTURE) WAS FOUND DURING ULTRASONIC INSPECTION OF THE NR 2 ENGINE FORWRD MOUNT, INBOARD ATTACH BOLT. REPLACED NR 2 ENGINE FORWARD MOUNT INBOARD ATTACH BOLT PER BOEING S/B 737-SDR P2EA98107Engine · overtempFLT 823 - ON TAKEOFF FROM MCI, THE NR 2 ENGINE EGT RAN HOT. PERFORMED WATER WASH ON NR 2 ENGINE PER AMM 71-00-PG 703D, VISUALLY INSPECTED WIRING REF 77-21-0, OPERATED NR 2 ENGINE AT TAKEOFF POWER MAX EGT NOTED WAS 570 DEGREES, MAX ALLOWABLE EGT IS 590 DEGREE SDR P2EA97094Sensor · failedFLT 215 - ATL-MCI - AFTER TAKEOFF THE RIGHT MAIN GEAR WOULD NOT RETRACT, ON 2ND TRY NOSE AND LEFT MAIN RETRACTED AND AFTER 30 SECONDS THE RIGHT MAIN RETRACTED. REMOVED AND REPLACED RT GEAR DOWNLOCK SENSOR OPS CHECK GOOD MM 32. GEAR OPS VERIFIED BY JACKING ANSDR P2EA97093Doubler · damagedSJO - REPLACEMENT OF FUSELAGE SKIN DOUBLER STRINGER 20 LEFT BETWEEN BS 938 AND BS 1000, LENGTH 62 INCHES, WIDTH 14 INCHES, DIAMETER .071 INCHES. SKIN BENEATH REPAIR WAS REPLACED REQUIRING DOUBLER REMOVAL AND REINSTALLATION. ACCOMPLISHED OVERLAPPING SKIN REPA
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