Boeing 737-201

Service difficulty reports · 2,471

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 = '737201'
  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 USAA001615Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 639 STRINGER 2R. MODIFIED PART INSTALLED PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001614Splice · crackedCLT - FOUND STRINGER END SPLICE CRACKED .5 INCH, STATION 360 STRINGER 14L. REPLACED SPLICE PER SRM 51-10-01. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001610Skin · crackedCLT - FOUND DOOR CUTOUT CRACKED 3 INCHES, LEFT AFT ENTRY DOOR LOWER FORWARD CORNER. INSTALLED DOUBLER PER SRM 53-30-03 AND EA 68158. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001609Bulkhead · crackedCLT - FOUND AFT NOSE W/W BULKHEAD CRACKED 1.5 INCHES, ACT SUPPORT BEAM WEB STATION 228, WL 185.5, BL 0. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001601Splice · corrodedCLT - FOUND KEELBEAM SPLICE CORRODED 1 INCH BY 5 INCHES, BS 727 PLUS 6, LBL 6 OUTBOARD SIDE OF KEEL CHORD. INSTALLED DOUBLER AND FILLER PER EA 67973 AND SRM 53-10-1 AND 53-10-6. CORROSION LEVEL 1. (M)Sep 28, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001600Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .75 INCH, STATION 663 BULKHEAD UPPER CHORD ANGLE LBL 24 WL 201.5. INSTALLED DOUBLER AND STIFFENER PER DWG 691A0032. (M)Sep 28, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001599Angle · crackedCLT - FOUND VERTICAL ANGLE CRACKED .25 INCH, AFT SIDE STATION 727, BULKHEAD RBL 6.5. REPLACED ANGLE PER SRM 51-10-01 AND EA 68132. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001570Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 339, STRINGER 17LT. REPAIRED PER DWG 65C27257 AND 65C27297. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001569Frame · crackedCLT - FOUND SIDE CHORD CRACKED 2 INCHES, BS 178, WL 207, LBL 25. INSTALLED REPAIR ANGLE PER SRM 53-10-11 AND EA 68032. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001598Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 6.75 WL 201. ENLARGED CUT OUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001590Structure · corrodedCLT - FOUND ZEE CHORD CORRODED 1 INCH BY 4 INCHES, STATION 270 LBL 5 TO RBL 5. SPLICED IN NEW ZEE CHORD PER TYPICAL REP 53-20-04. CORROSION LEVEL 1, TASK NR C53-101-01. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, StructureSDR USAA001589Web · corrodedCLT - FOUND WEB CORRODED 3 INCHES BY 2 INCHES, BS 268 RBL 10 BOTH VERTICAL AND HORIZONTAL SURFACES. CORROSION LEVEL 1, TASK NR C53-101-01. REPLACED WEB PER SRM 51-10-02. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001588Floorbeam · crackedCLT - FOUND 1 INCH CRACK, BS 520 LBL 45. COLLECTOR KIT INSTALLED PER EA 67976 SB 737-53-1120, BOEING DWG. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001587Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 520 RBL 24. COLLECTOR KIT INSTALLED PER EA 67976 SB 737-53-1120 BOEING DWG. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001586Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 520 LBL 24. COLLECTOR KIT INSTALLED PER SB 737-53-1120, EA 67976 BOEING DWG. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001585Skin · crackedCLT - FOUND SKIN CRACKED TWO PLACES, .300 INCH LONG, .400 INCH, RIGHT WING, LE AT CTR UPSTOP CUTOUT FOR NR 6 SLAT. INSTALLED DOUBLER PER EA 67989. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Wing, Plate/SkinSDR USAA001584Skin · crackedCLT - FOUND SKIN CRACKED .375 INCH, BS 336, STRINGER 17 LEFT. INSTALLED DOUBLER PER DWG 65C27257. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001583Splice · crackedCLT - FOUND SPLICE CRACKED .500 INCH, STATION 907 AT S4L. REMOVED OLD PORT AND INSTALLED NEW ONE PER BOEING SRM 737-200, 51-10-1. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001582Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 597 LEFT AFT OUTBOARD CHORD ANGLE AT LOWER END WING CENTER. REMOVED AND REPLACED CHORD ANGLE PER SRM 51-10-1, 51-30-0. (M)Sep 27, 2000 · N262AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001575Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 986, RBL 46, LBL 12. CORROSION LEVEL 1, C53-107-02. INSTALLED FABRICATED T-CAP AND SPLICE DOUBLER PER TR 53-60-01 REV A. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001574Web · crackedCLT - FOUND WEB CRACKED TWO PLACES .25 INCH EACH, 2 INCHES AND 3 INCHES AFT OF BS 706 AT BL 0. INSTALLED FILLER, DOUBLER AND TRIPLER PER TR 57-10-05. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Wing Miscellaneous StructureSDR USAA001573Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, RBL 25, WL 201.5 ON L/B SIDE. INSTALLED REPAIR ANGLE AND SPLICES PER EA 68031. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001572Torque Box · crackedCLT - FOUND TORQUE BOX CRACKED .5 INCH, FS 947 PLUS 1, STRINGER 10L. INSTALLED FILLER AND REPAIR STRAP PER TR 53-30-07A. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, StructureSDR USAA001571Web · crackedCLT - FOUND WEB CRACKED 3 INCHES, IN RADIUS OF NLG ACT BEAM WEB. REPLACED WEB PER SRM 51-10-02. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001567Angle · crackedCLT - FOUND ANGLE CRACKED .250 INCH, AFT SIDE 178 BULKHEAD, RBL 24.5, WL 195. FABRICATED AND INSTALLED ANGLE PER DWG 65-16300. (M)Sep 26, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001566Frame · crackedCLT - FOUND CHORD ANGLE CRACKED .75 INCH, STATION 663 BULKHEAD UPPER CHORD, RBL 25, WL 201.5. INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-0. (M)Sep 26, 2000 · N262AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001565Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 962, STRINGER 17 LEFT. INSTALLED DOUBLER PER SRM 53-30-3 FIG 24. (M)Sep 26, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001564Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STAITON 597 LEFT FORWARD OUTBOARD CHORD LOWER END ABOVE WING CENTER. REMOVED AND REPLACED CHORD ANGLE PER SRM 51-10-1, 51-30-0. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001563Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION RIGHT 597 FORWARD OUTBOARD CHORD ANGLE LOWER END ABOVE WING. REMOVED AND REPLACED WEB SECTION PER SRM 51-40-00. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001562Stringer · crackedCLT - FOUND SHELF CRACKED, .375 INCH, BS 727 18A LEFT. REPLACED SHELF PER SRM 51-10-01. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001561Clip · crackedCLT - FOUND CLIP CRACKED 1 INCH, S5L STATION 685. MODIFIED PART NR INSTALLED PER EO 5393G227. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001560Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 1 INCH, 4 PLACES, BL 0 LONG FLOORBEAM WEB STATION 707-714, WL 202.5. WEB REPAIR INSTALLED PER TR 57-10-05. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001549Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 PLUS 1.5, RBL 29, WL 207. INSTALLED FABRICATED WEB PER SRM 51-30-01. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001548Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 PLUS 1.5, LBL 29, WL 207. INSTALLED FABRICATED WEB PER SRM 51-10-01. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001547Angle · crackedCLT - FOUND WEB ANGLE CRACKED .250 INCH, BS 178 AFT SIDE, RBL 24.5, WL 195. INSTALLED REPAIR ANGLE PER DWG 65-16300. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001546Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED 4 PLACES 1 INCH, RBL 25 FLOORBEAM WEB STATION 707-714, WL 202.5. INSTALLED DOUBLER PER EA 67997A. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001545Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED TWO PLACES, LBL 25, FLOORBEAM WEB STATION 707 TO 710, WL 202.5. INSTALLED DOUBLER PER EA 67997A. (M)Sep 25, 2000 · N262AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001544Floorbeam · corrodedCLT - FOUND FLOORBEAM 2 INCHES BY 10 INCHES, BS 1016, LBL 5 - LBL 15. CORROSION LEVEL 1. REPAIRED T-CAP PER TR 53-60-02. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR SAA001543Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 827, STRINGER 9RT. REPAIRED PER EO 5393G227. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001539Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 3 INCHES, STATION 178, LBL 5.7, WL 211-214. INSTALLED DOUBLER PER SRM 53-10-11. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001538Frame · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, LBL 25, WL 201.5 ON L/B SIDE. INSTALLED DOUBLER PER EA 68031. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001558Skin · crackedCLT - FOUND CRACK IN SKIN 2 INCHES, S16L BETWEEN STATION 727A AND 727B. INSTALLED REPAIR DOUBLER PER RM 53-30-3 FIG 17. (M)Sep 25, 2000 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00267Battery Pack · faultyCLE - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK TO BE INTERMITTENTLY OPEN. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Sep 22, 2000 · N259AU · Boeing 737201 · Emergency LightingSDR USAASB00270Gyro · faultyBWI - FLT 2821 - ON CLIMB-OUT FROM BWI, THE HEADING COMPARATOR LIGHT ILLUMINATED. CAPTAINS AND FIRST OFFICERS COMPASS SYSTEM SPLIT 30 DEGREES APART AND REMAINED THAT WAY FOR 10 MINUTES. CAPTAINS ADVISED BWI THAT HE WAS RETURNING TO FIELD. JUST PRIOR TO LANDSep 22, 2000 · N243US · Boeing 737201 · Directional Gyro and Indicating SystemSDR USAASB00264Light · failedATL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHT ABOVE THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Sep 20, 2000 · N263AU · Boeing 737201 · Emergency LightingSDR USAASB00260Control Unit · failedFLL - FLT 2995 - EN ROUTE FROM LGA-FLL, AT FL310, THE PASSENGERS OXYGEN DROPPED TO ZERO PSI. CREW ACCOMPLISHED PROCEDURES AND DESCENDED TO FL100. BEFORE LANDING, THE PASSENGER OXYGEN PRESSURE RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE PASSENGESep 17, 2000 · N246US · Boeing 737201 · Passenger Oxygen SystemSDR USAASB00258Transformer · failedEWR - FLT 2663 - ON CLIMB-OUT FROM LGA, AT APPROX 10,000 FT, F/A REPORTED A STRONG ELECT ODOR AND PLASTIC BURNING SMELL IN THE CABIN. CREW NOTICED THE NR 2 TRANSFORMER RECTIFIER C/B HAD POPPED. CAPT DECIDED TO DIVERT TO EWR. FLT LANDED WITHOUT FURTHER INCIDSep 16, 2000 · N251AU · Boeing 737201 · DC Rectifier/ConverterSDR USAASB00257Shaft · dirtyMCO - FLT 2753 - ON APPROACH TO MCO FROM IAD, AT APPROX 200 FEET, THE GROUND PROXIMITY WARNING WENT OFF. ON GLIDESCOPE AND NORMAL APPROACH, GEAR RED WARNING LIGHTS ILLUMINATED CAUSING GPWS WARNING. CREW INITIATED GO-AROUND, CYCLED LANDING GEAR AND RECEIVED TSep 16, 2000 · N257AU · Boeing 737201 · Landing Gear SelectorSDR USAASB00255Unknown · odorLGA - FLT 2667 - DURING CLIMB-OUT FROM LGA, EN ROUTE TO MCO, PASSENGERS IN SEAT ROW 4 COMPLAINED OF AN UNUSUAL ODOR. FLIGHT ATTENDANTS AND FIRST OFFICER CONFIRMED THAT THERE WAS INDEED AN UNRECOGNIZABLE ODOR IN THE CABIN. CAPTAIN DECLARED AN EMERGENCY AND RESep 14, 2000 · N251AU · Boeing 737201 · Air Distribution SystemSDR CA001024051Bolt · missing(CAN) DURING ROUTINE MAINTENANCE WAS UNABLE TO DEPLOY LOWER THRUST REVERSER DOOR NR 2 ENGINE. SUSPECT BOLT (NAS1633-10D) AND NUT (AN 320-3) WERE NOT FOUND. ALL OTHER AIRCRAFT IN FLEET HAS BEEN INSPECTED. NO FURTHER DEFECTS FOUND. ALL OTHER AIRCRAFT ARRIVING INSep 13, 2000 · Boeing 737201 · Engine Thrust Reverser
Back to Boeing 737-201