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 CA020730003Acm · failed(CAN) CREW REPORTED "BURNING SMELL IN FLIGHT DECK AND CABIN. MIX VALVES CYCLED FULL COLD SMELL DISSIATED". MAINT REPLACED PACK CONTROL VALVE INITIALIALY, THEN ON SUBSEQUENT FLIGHT THE PACK TRIPPED IN AUTO. ACM REPLACED SNAG CLEARED. ACM OUT FOR OVERHAUL.Jul 28, 2002 · Boeing 737201 · Cabin Cooling SystemSDR CA020726004Gusset · cracked(CAN) 2.5 INCH IN CRACK IN CENTRE OF GUSSET (GUSSET TOTAL LENGTH 10.5 INCHES).VISIBLE ALONG INSIDE RADIUS.REF SDA AL-2002-03TAT: 54113.9 HR. LDG: 52167Jul 15, 2002 · Boeing 737201 · Fuselage Miscellaneous StructureSDR CA020726003Gusset · cracked(CAN) 2.5 INCH CRACK IN CENTER OF GUSSET (GUSSET TOTAL LENGTH 10.5 INCHES). VISIBLE ALONG INSIDE RADIUS. REF SDA AL-2002-03TAT 57540.8 HRLDG 55883Jul 15, 2002 · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB01328Charger · failedLGA - THE MID CABIN AISLE EMERGENCY EXIT SIGN FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN CHARGER. (M)Nov 28, 2001 · N249US · Boeing 737201 · Emergency LightingSDR USAASB01317Engine · failedMIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTNov 19, 2001 · N262AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR 2001F00706Engine · failedMIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTNov 19, 2001 · N262AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA011361Skin · crackedPIT - FOUND SKIN CRACKED .20, FUSELAGE SKIN BETWEEN FRAME 727A AND 727B STRINGER 16R. INSTALLED DOUBLER AND REPAIR ANGLE PER EA 72869 AND SRM 53-30-3. (M)Nov 7, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR CA011119007Bellcrank · wrong part(CAN) WHILE THE AIRCRAFT WAS ON A "C" CHECK, RT OUTBOARD FLAP INBOARD FAIRING COULD NOT BE RIGGED. AFTER INVESTIGATION FROM THE INSPECTOR, FOUND THE WRONG BELLCARANK INSTALLED. RT OUTBOARD WAS INSTALLED AT RT INBOARD. PROPER BELLCRANK INSTALLED, RIGGING CARRIENov 5, 2001 · Boeing 737201 · Trailing Edge Flap Control SystemSDR USAA011351Skin · dentedCLT - FOUND SKIN DENTED 4 INCHES BY 3 INCHES, BETWEEN BS 908 TO 951 S17R AND S20R. INSTALLED DOUBLER AND TRIPLER PER EA 85513. (M)Oct 23, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01301Battery · dischargedBSI - THE EMERGENCY LIGHT ABOVE THE 1R EXIT FLASHES ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Oct 21, 2001 · N254AU · Boeing 737201 · Emergency LightingSDR USAASB01294Battery Pack · dischargedBWI - THE RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)Oct 13, 2001 · N251AU · Boeing 737201 · Emergency LightingSDR USAA011350Angle · crackedCLT - FOUND DRAG ANGLE CRACKED, STATION 540, JUST ABOVE STRINGER 23L. FABRICATED PART PER T/R 53-50-03A. (M)Oct 12, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011299Beam · crackedCLT - FOUND BEAM CRACKED 1.5 INCH, LOWER INTERIOR FORWARD CORNER OF FORWARD ENTRY DOOR BEAM. INSTALLED A NEW BEAM ASSY PER SRM 51-10-1 AND 51-30-2. (M)Oct 10, 2001 · N265AU · Boeing 737201 · Passenger/Crew DoorsSDR USAASB01289Power Supply · dischargedLGA - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLY. (M)Oct 10, 2001 · N254AU · Boeing 737201 · Emergency LightingSDR USAA011304Stringer · corrodedCLT - FOUND STRINGER CRACKED 6 INCHES, STRINGER 20L STATION 777. INSTALLED STRINGER REPAIR PER SRM 53-10-3 DETAIL VII. (M)Oct 4, 2001 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA011300Skin · crackedCLT - FOUND SKIN CRACKS 1.5 INCH AND .250 INCH, BS 380 EQUIP COOLING EXHAUST. INSTALLED REPAIR DOUBLER PER T/R 53-30-04. (M)Oct 3, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011348Strap · damagedCLT - FOUND DAMAGED TEAR STRAP 8.9 INCHES, STATION 500 STRINGER 24L TO S25L. INSTALLED DOUBLER AND TRIPLER. (M)Oct 2, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB01278Wire · damagedLGA - THE FLOOR PATH EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 7. MAINTENANCE REPAIRED A WIRE UNDER THE SEAT ASSEMBLY. (M)Oct 2, 2001 · N263AU · Boeing 737201 · Light System WiringSDR USAA011283Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 10 INCHES, STATION 1006 TO STATION 1016 BBL 0. REPAIRED PER SRM 51-30-2. (M)Sep 30, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011281Structure · chafedCLT - FOUND WEAR CHAFING FROM APU BLEED DUCT .250 BY 3 INCH, STATION 1064. INSTALLED REPAIR DOUBLER PER EA 85490. (M)Sep 28, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011268Door Frame · crackedCLT - FOUND DOOR FRAME CRACKED .200 INCH, FORWARD SERVICE DOOR AFT FRAME NR 3 FITTING CUT OUT. INSTALLED DOUBLER PER EA 85464. (M)Sep 25, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR USAA011292Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, RBL 45 BS 1013 FLOOR LEVEL. FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 51-10-2. (M)Sep 25, 2001 · N265AU · Boeing 737201 · Fuselage Structure (General)SDR USAA011280Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES BY 1 INCH, STATION 968 STRINGER 25L. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)Sep 24, 2001 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA011263Shear Tie · damagedCLT - FOUND SHEAR TIE WITH WORKING FASTENERS, STATION 360 ATTACH LUG, BETWEEN STRINGER 28R AND 27R. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 9A. (M)Sep 22, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR USAASB01266Power Supply · dischargedBWI - THE EMERGENCY LIGHTS FOR THE LAST FIVE SEAT ROWS IN THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Sep 22, 2001 · N242US · Boeing 737201 · Emergency LightingSDR USAA011267Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH BS 300 S8R. REPLACED UPPER DOOR FRAME WITH LIKE PART. (M)Sep 20, 2001 · N265AU · Boeing 737201 · Fuselage Main, FrameSDR USAA011276Seat Track · corrodedCLT - FOUND SEAT TRACK SECTION CORRODED 1 INCH BY 3 INCHES, STATION 328 TO 360 RBL 55. SPLICE IN NEW SECTION OF TRACK PER 51-10-1. (M)Sep 20, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA011264Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 328 S17R. REPAIR PREVIOUSLY ACCOMPLISHED PER BOEING REPAIR DRAWING 65C2757. (M)Sep 19, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011286Skin · damagedCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER 10 INCHES BY 8 INCHES, STATION 380 BETWEEN S24 AND S23. INSTALLED NEW DOUBLER PER SRM 53-30-3 FIG 1. (M)Sep 19, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01261Powerpack · failedBWI - THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Sep 19, 2001 · N264AU · Boeing 737201 · Emergency LightingSDR USAA011309Skin · crackedCLT - FOUND SKIN CRACKED 15 INCHES BY 13 INCHES, STATION 947 S15R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 35. (M)Sep 18, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011241Bolt · corrodedPIT - FOUND FAIL SAFE BOLT SEVERELY CORRODED, VERTICAL STABILIZER BOTTOM LEFT ATTACH FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR DEFECTIVE BOLT FOUND IN YQB. (M)Sep 14, 2001 · N227AU · Boeing 737201 · Vertical Stabilizer, Attach FittingsSDR USAA011239Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 706 AT S10L. NEW CLIP INSTALLED PER EO 53936227. (M)Sep 14, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011238Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 663, S10L. NEW CLIP INSTALLED PER EO 53936227. (M)Sep 14, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011307Frame · dentedCLT - FOUND FRAME DENTED 1 INCH BY 1 INCH, AFT CARGO STATION 767 ABOVE STRINGER 24R. INSTALLED DOUBLER AT STATION 767 PER SRM 51-40-3. (M)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage Main, FrameSDR USAA011303Seat Track · corrodedCLT - FOUND FLOOR TRACK CORRODED 1 INCH BY 1 INCH, AFT CARGO STATION 806 S26R. INSTALLED REPAIR TIE DOWN FLOOR SUPPORT PER SRM 53-10-5 FIG 11. (M)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA011282Beam · corrodedCLT - FOUND BEAM CORRODED, AFT CARGO STATION 797 S26R. REPLACED STRAP 65-47957-11 SRM 51-10-01. (M)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011306Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 847 JUST ABOVE STRINGER 26R. INSTALLED DOUBLER. (M)Sep 12, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011302Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .5 INCH, AT STRINGER 25R TO FRAME AT STATION 947.5. REPLACE TIE CLIP. (M)Sep 12, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR USAA011301Stringer · corrodedCLT - FOUND STRINGER CORRODED 1.5 INCH BY 13 INCHES, STRINGER 27L BETWEEN STATION 900 AND 913. INSTALLED DOUBLER AND SECTION OF STRINGER. (M)Sep 12, 2001 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA011279Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 4 INCHES, STATION 663 BL 0. INSTALLED WEB, SPLICE ANGLE REPAIR. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011285Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED AT CLIP NUT HOLES 2 INCHES BY 60 INCHES, BS 986, LBL 6 TO RBL 54, WL 207. INSTALLED NEW T-CAP. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA011284Intercostal · corrodedCLT - FOUND BEAM INTERCOSTAL CORRODED 2 INCHES BY 26 INCHES, BS 990-1016 LBL 6 TO LBL 16. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-3. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011289Floorbeam · corrodedCLT - FOUND BEAM CORRODED 2 INCHES BY 33 INCHES, BS 1016 BBL 0 LBL 33. INSTALLED T-CAP PER T/R 53-60-02. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011290Floorbeam · corrodedCLT - FOUND BEAM/CHANNEL/WEB CORRODED 5 INCHES, BS 1014-1019 BBL 0 LBL 6. INSTALLED T-CAP. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAASB01255Ballast · failedBWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACSep 10, 2001 · N263AU · Boeing 737201 · Lighting SystemSDR USASB01255Light · faultyBWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACSep 10, 2001 · N263AU · Boeing 737201 · Passenger Compartment LightingSDR CA010921024Generator · failed(CAN) ON LANDING INTO YYZ, PILOT STARTED THE APU BUT COULD NOT GET APU GENERATOR ON LINE. MAINTENANCE NOTIFIED AND APU GENERATOR AND WIRING INSPECTED. IT WAS THEN DETERMINED THE WIRING AT THE FIREWALL DISCONNECT WAS BURNED AND CONNECTOR DAMAGED. AIRCRAFT WAS RSep 10, 2001 · Boeing 737201 · APU System WiringSDR USAA011261Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 4 FEET BY 2 INCHES, STATION 328, BL 0 RIGHT TO SERVICE DOOR. FABRICATED AND INSTALLED T-CAP. (M)Sep 8, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011291Skin · dentedCLT - FOUND SKIN DENTED 1 INCH, BS 280 STRINGER 24R. REMOVED DAMAGE, INSTALLED REPAIR PER SRM 53-30-3. (M)Sep 6, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/Skin
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