Boeing 737-201

Service difficulty reports · 2,471

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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 = '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 USAASB00351Engine · failedFLL - FLT 2828 - ON CLIMB-OUT FROM FLL, EN ROUTE TO BOS, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND HIGH EGT. CAPTAIN SHUTDOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND ADVISED THE FLIGHT ATTENDANTS THEY WERE RETURNING TO FIELD AT FLL. CAPTAIN FIRED Dec 18, 2000 · N243US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA200101173Seal · leakingON CLIMB OUT FROM TPA, A VERY LOUD SQUEAL WAS COMING FROM THE FORWARD ENTRY DOOR. AC WAS PRESSURIZING, NOISE BECAME LOUDER AS AC CLIMBED HIGHER. FLIGHT RETRUNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.MAINTENANCE REMOVED AND REPDec 18, 2000 · N242US · Boeing 737201 · Passenger/Crew DoorsSDR CA010205021Skin · corroded(CAN) AIRCRAFT WAS ON D CHECK AND ON IMPORTATION PROCESS. ON FUSELAGE AT FS 727 BETWEEN STRINGER 27 LT AND 27 RT AN EXTERNAL REPAIR WAS EVALUATED FOR COMPLIANCE WE FOUND BULGING AT RIVETS. THE REPAIR WAS REMOVED AND WE FOUND HEAVY CORROSION IN BETWEEN SKIN. BODec 15, 2000 · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002147Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 787, STRINGER 13L. INSTALLED DOUBLER PER SRM 51-40-3 AND TR 53-10-27. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Main, FrameSDR USAA002146Skin · crackedCLT -FOUND FUSELAGE SKIN CRACKED 1.625 INCH, BS 767 PLUS 8 INCHES AND STRINGER 18L. CUTOUT DAMAGED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002145Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 727 BETWEEN STRINGER 14L AND 15L. INSTALLED FILLER AND DOUBLER PER EA 68651. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Main, FrameSDR USAA002144Structure · crackedCLT - FOUND T-CAP AND WEB CRACKED 6 INCHES, STATION 663, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M)Dec 14, 2000 · N245US · Boeing 737201 · Wing, Center BoxSDR USAA002143Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 326, WL 207 STRINGER 17R. REPAIRED PER SRM 53-30-3. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002142Web · crackedCLT - FOUND WEB CRACKED THREE PLACES .875 INCH, BS 178 WL 218, LBL 12 - LBL 14. NEW WEB AND DOUBLER INSTALLED PER EA 68663 AND SRM 53-10-11. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002141Web · crackedCLT - FOUND WEB SIDE CHORD CRACKED .875 INCH, BS 178, LBL 26, WL 207. NEW CHORD SPLICED IN PER EA 68631 AND EO 5300V157. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002140Web · crackedCLT - FOUND WEB SIDE CHORD CRACKED .875 INCH, BS 178 RBL 26, WL 207. NEW CHORD SPLICED IN PER EA 68631 AND EO 5300V157. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002139Structure · crackedCLT - FOUND VERTICAL CHORD CRACKED .250 INCH, BS 178 AFT SIDE BULKHEAD. NEW CHORD AND DOUBLER INSTALLED PER SRM 53-10-11. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002138Web · crackedCLT - FOUND WEB CRACKED 4 PLACES 1 INCH EACH, BS 178, LBL 5.7 FROM WL 195 TO 215. REMOVED DAMAGE PER EA 68663. (M)Dec 14, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002131Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, STATION 663, RBL 25, WL 203. SPLICED ANGLES PER EA 68620. (M)Dec 13, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002130Strap · corrodedCLT - FOUND INNER PLATE/STRAP CORRODED TWO AREAS .75 INCH, INSIDE FORWARD CARGO DOOR CUTOUT. REPLACED STRAP PER SRM 51-10-1. (M)Dec 13, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002091Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER, LBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M)Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002090Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER, RBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M)Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002089Stringer · crackedCLT - FOUND 5 CRACKS IN STRINGER .5 INCH TO .25 INCH, STRINGER 15L, BETWEEN BS 520 AND 540. REPAIRED PER SRM 53-10-3. (M)Dec 11, 2000 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA002088Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, FLOORBEAM UPPER CHORD STATION 578, LBL 62. INSTALLED UPPER CHORD FLOORBEAM PER SRM 51-10-01. (M)Dec 11, 2000 · N245US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA002087Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, UPPER CHORD ANGLE STATION 663, LBL 25, WL 203. INSTALLED ANGLE PER EA 68620. (M)Dec 11, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002086Attach Angle · crackedCLT - FOUND FRAME ATTACH ANGLE CRACKED 2 INCHES, STATION 348, STRINGER 15L. REPAIRED PER SRM 51-40-02. (M)Dec 11, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002085Bulkhead · crackedCLT - FOUND WEB CRACKED .125 INCH, BS 178, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002084Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .5 INCH EACH, BS 178, WL 218, RBL 11 AND RBL 13. INSTALLED DOUBLER PER EA 68609A. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002083Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, FORWARD FASTENER RBL 28, WL 207, STATION 179. INSTALLED NEW WEB SECTION PER SRM 51-10-01 AND 51-30-0. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002082Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER LBL 28, WL 207, STATION 179. INSTALLED NEW WEB SECTION PER SRM 51-30-0 AND 51-10-01. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002081Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .5 INCH, BS 178, WL 207, LBL 1 AND RBL 1. INSTALLED DOUBLER PER EA 68609A. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002080Structure · crackedCLT - FOUND SIDE CHORD .75 INCH, BS 178, WL 207, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002079Structure · crackedCLT - FOUND SIDE CHORD CRACKED .75 INCH, BS 178, WL 195, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002076Stringer · corrodedTPA - FOUND STRINGER CORRODED 2 INCHES BY 3 INCHES, STATION 965, STRINGER 27R. CORROSION LEVEL 2. SPLICED IN SECTION PER SRM 53-10-3 PAGE 4 FIG 1. (M)Dec 6, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA002065Skin · crackedCLT - FOUND SKIN CRACKED 3.5 INCH, STATION 952 LOWER FORWARD CORNER AFT ENTRY DOOR. REPAIRED FILLER, DOUBLER, TRIPLER PER SRM 53-30-03. (M)Dec 6, 2000 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002064Skin · crackedCLT - FOUND SKIN PLATE CRACKED 2.25 INCH, FORWARD STATION 947 STRINGER 22L. REMOVED DAMAGED AND FABRICATED FILLER AND DOUBLER PER SRM 53-30-3. (M)Dec 6, 2000 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002056Bulkhead · crackedCRACK BS178 WL234 LBL 13.25. CORRECTIVE ACTION: REMOVED DAMAGE & INSTALLED DOUBLER PER SRM 53-10-11 FIG 1Dec 4, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002055Window Post · crackedCRACK STA 231.8. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3Dec 4, 2000 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA002054Frame · crackedCRACK STA 767 STR 13R FUSE. FRAME SPLICE RIVET. CORRECTIVE ACTION: FABRICATED REPAIR ANGLE & FILLER INSTALLED PER SRM 53-10-7 & 51-40-3Dec 4, 2000 · N245US · Boeing 737201 · Fuselage Main, FrameSDR USAA002053Gusset · crackedCRACK NOSE GEAR ACTUATOR ATTACH GUSSET. CORRECTIVE ACTION: REPLACED PART PER SRM 51-30-3 & 51-10-1Dec 4, 2000 · N245US · Boeing 737201 · Fuselage, Landing Gear Attach FittingsSDR USAA002052Floorbeam · crackedCRACK LBL 25 FLOORBEAM AT LWR FAST.S707-712, W1202.5. CORRECTIVE ACTION: FABRICATED DOUBLER PER EA 68629Dec 4, 2000 · N245US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA002051Crease Beam · corrodedCORROSION LEVEL 1 1 CREASE BEAM S935 TO S990 WL 208CORRECTIVE ACTION: REPLACED CREASE BEAM PER SRM 51-10-1Dec 4, 2000 · N245US · Boeing 737201 · Fuselage Main, StructureSDR USAA002045Angle · corrodedCORROSION LEVEL 1 BS 298-BS360, RBL 64. CORRECTIVE ACTION: REMOVED SURFACE CORROSION PER SRM 51-10-02Nov 30, 2000 · N245US · Boeing 737201 · Fuselage Main, StructureSDR USAA002044Floorbeam · corrodedCORROSION LEVEL 1 LOWER SURFACE UPPER FLOORBEAM BS 324, LBL 12CORRECTIVE ACTION: REPLACED FLOORBEAM SUPPORT PER SRM 51-10-2Nov 30, 2000 · N245US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA002043Frame · crackedFRAME CRACKED BS767, STR 13 & 14L. CORRECTIVE ACTION: FILLER & DOUBLER INSTALLED PER TR 53-10-27Nov 29, 2000 · N245US · Boeing 737201 · Fuselage Main, FrameSDR USAA002042Stiffener · crackedCRACKED LBL 15 LONGITUDINAL STIFFENER STA 726 WL 202. CORRECTIVE ACTION: REPLACED ANGLE PER SRM 51-30-3Nov 29, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002019Tie Clip · crackedTIE CLIP CRACKED BS 578 STR 3. CORRECTIVE ACTION: REPLACED TIE CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002027Tie Clip · crackedTIE CLIP CRACKED STA 787 STR 10L. CORRECTIVE ACTION: INSTALLED NEW CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002026Tie Clip · crackedTIE CLIP CRACKED STA 767 STR 11. CORRECTIVE ACTION: REPLACED TIE CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002025Tie Clip · crackedTIE CLIP CRACKED STA 747 STR 3R. CORRECTIVE ACTION: REPLACED TIE CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002024Tie Clip · crackedTIE CLIP CRACKED STA 685 STR 4L. CORRECTIVE ACTION: REPLACED TIE CLIP PER EO5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002023Tie Clip · crackedCRACK STA 663 STR 10LCORRECTIVE ACTION: INSTALLED NEW CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002022Tie Clip · crackedTIE CLIP CRACKED BS 639 STR 5. CORRECTIVE ACTION: INSTALLED NEW CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002021Tie Clip · crackedTIE CLIP CRACKED BS 639 STR 3. CORRECTIVE ACTION: INSTALLED NEW CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002020Tie Clip · crackedTIE CLIP CRACKED BS 616 STR3. CORRECTIVE ACTION: REPLACED TIE CLIP PER EO 5393G227Nov 27, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous Structure
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