Boeing 737-347

Service difficulty reports · 359

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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 = '737347'
  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 DL733030498Spar · damagedNR 2 INBOARD MID FLAP FRONT SPAR ASSEMBLY WAS FOUND DAMAGED. A REPLACEMENT WEB SECTION AND SPLICE DOUBLER WAS INSTALLED PER ER/A 423065-14.May 29, 2003 · N312WA · Boeing 737347 · Trailing Edge FlapsSDR DL733030478Fitting · corrodedCORROSION WAS FOUND IN THE LUG BORE AND AFT LUG FACE OF THE LT MLG SIDE STRUT FITTING AT FS 685. THE BORE WAS OVERSIZED AND THE FACE SPOTFACED TO REMOVE ALL CORROSION. A REPAIR BUSHING WAS INSTALLED IN THE BORE AND A WASHER INSTALLED TO FILL THE SPOTFACE. May 19, 2003 · N2310 · Boeing 737347 · Fuselage, Landing Gear Attach FittingsSDR DL733030434Skin · dentedFUSELAGE / SKIN / DENTING AND CREASE AT STA 380 BETWEEN STRINGERS 17L AND 18L. DENTED AND CREASED SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 384851-14.May 7, 2003 · N2310 · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030417Heat Exchanger · crackedRIGHT WING BODY OVERHEAT LIGHT CAME ON DURING CLIMB RAN PROCEDURE BUT LEFT PACK WOULD NOT HOLD CABIN ALTITUDE CABIN UNDER CONTROL AT 18000 MAX CABIN ALT 9500. FOUND FIBERGLASS PLENUM AT HEAT EXCHANGER BLOWN OUT ON LOWER SEAM ALSO FOUND BOTH HEAT EXCHANGERS CMay 3, 2003 · N3301 · Boeing 737347 · Pneumatic Distribution SystemSDR DL733030408Frame · crackedFUSELAGE / COCKPIT FLOOR STRUCTURE / CRACKED WEB AND INTERCOSTAL / STA 178, WL 207, RBL 28, THE INTERCOSTAL OUTBOARD STRUCTURE AND HORIZONTAL WEB WERE FOUND CRACKED. BOTH ARE LOCATED IMMEDIATELY AFT OF THE STA 178 BULKHEAD. THE CRACK WAS TRIMMED OUT OF THE STMay 1, 2003 · N2310 · Boeing 737347 · Fuselage Main, FrameSDR DL733030363Wedge · delaminatedRT INBOARD AFT FLAP TE WEDGE DISBONDED. REPAIRED PER ER/A 422820-14Apr 17, 2003 · N3301 · Boeing 737347 · Trailing Edge FlapsSDR DL733030353Power Supply · inoperativeAFT CABIN EMERGENCY LIGHT INOPERATIVE, RELAMPED NO HELP R & R POWER SUPPLY LIGHT OPS NORMAL.Apr 11, 2003 · N308WA · Boeing 737347 · Emergency LightingSDR DL733030435Arm · brokenWHEN CATERING ATTEMPTED TO OPEN THE LEFT REAR SERVICE DOOR . IT WOULD NOT OPEN. REPLACED BROKEN ARM ASSEMBLYApr 6, 2003 · N303WA · Boeing 737347 · Service DoorsSDR DL733030331Skin · gougedDURING HMV INSPECTIONS, THREE (3) DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 20R AND 21R. ADDITIONALLY, FOUR (4) DENTS WERE FOUND BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 21R AND 22R. ALL DENTS WERE WApr 2, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030330Fitting · misalignedVERTICAL STABILIZER REAR TERMINAL FITTING LUGS WERE DETERMINED TO HAVE UNDERGONE PREVIOUS REWORK WHICH LEFT THE LUG THICKNESS LESS THAN BLUEPRINT SPECIFICATIONS AT EACH OF THE FOUR LUGS. AREA INSPECTED AND NEW BUSHINGS WERE FABRICATED PER DAL ER/A 384672-14 TApr 2, 2003 · N309WA · Boeing 737347 · Vertical Stabilizer, Attach FittingsSDR DL733030328Skin · crackedDURING ACCOMPLISHMENT OF PERMANENT REPAIR OF FUSELAGE SKIN/DOUBLER CRACKING, ADDITIONAL CRACK WAS FOUND IN BOTH. THE DAMAGE WAS TRIMMED OUT AND TWO EXTERNAL DOUBLERS WERE INSTALLED WITH SOLID FASTENERS PER ER/A 366481-14, REV C.Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030322Skin · dentedA DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 1000 AND 1016 AND BETWEEN STRINGERS 13L AND 14L THE DENT IS CUT OUT AND EXTERNAL DOUBLER AND FILLER ARE INSTALLED SIMILAR TO B737-200 SRM 53-30-3, FIG 48 BUT IN ACCORDANCE WITH ER/A 384711-14.Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030321Skin · dentedREPAIR OF DENTA DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STRINGER 17L AND 18L AT STA 360. THE DENTED MATERIAL WAS CUT OUT AND TWO EXTERNAL ALUMINUM DOUBLERS WERE INSTALLED PER ER/A 384678-14.Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030320Skin · wornTHE FUSELAGE SKIN WITH AN AREA OF WEAR BETWEEN FS 857 & 877 NEAR STRINGER 1. THE DAMAGE WAS BLENDED SMOOTH AND AN AREA CUTOUT. THE DAMAGE WAS REPAIRED WITH AN ALUMINUM EXTERNAL REPAIR DOUBLER PER ER/A 384701-14, REV A.Mar 31, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030303Structure · debondedINBOARD FORE FLAP DELAMINATED. REPAIRED PER ER/A 422922-14.Mar 31, 2003 · N3301 · Boeing 737347 · Trailing Edge FlapsSDR DL733030317Skin · crackedTHE FUSELAGE SKIN WAS FOUND DENTED AND CRACKED AT THE LOWER FWD CORNER OF THE C2 DOOR OPENING. THE DAMAGE WAS REMOVED WITH A 1.5 X 1 INCH CUTOUT TO THE CORNER THROUGH THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP. THE CORNER WAS REPAIRED WITH MULTIPLE ALUMMar 30, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030314Skin · dentedTHE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 470 BETWEEN STRINGERS 22L & 23L. THE DENT WAS REMOVED WITH A 7 INCHES CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384681-14, REV A.Mar 29, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030313Fitting · corrodedTHE AFT LUG OF THE CROWN BEAM FITTING ON THE NR 2 ENGINE PYLON WAS FOUND WITH CORROSION IN THE HOLE BORE. THE BORE WAS OVERSIZED TO 3.10 INCH TO REMOVE THE CORROSION. A STEEL REPAIR BUSHING WAS INSTALLED AND THEN A NEW BEARING. THE REPAIR WAS ACCOMPLISHED PMar 29, 2003 · N309WA · Boeing 737347 · Nacelle/Pylon, Attach FittingsSDR DL733030199Smoke Detector · malfunctionedRT AFT LAV SMOKE DETECTOR LIGHT AND CHIME CAME ON AND OFF IN FLT. REPLACED SMOKE DETECTOR UNITFeb 26, 2003 · N308WA · Boeing 737347 · Smoke DetectionSDR DL733030162Hose · leakingON ARRIVAL DEN FOUND FUEL LEAKING FROM RT ENGINE. INSP FOUND MAIN FUEL LINE FROM PYLON TO ENG FUEL PUMP LEAKING AT SWEDGED END / PYLON SIDE. REPLACED SAME.Feb 18, 2003 · N304WA · Boeing 737347 · Engine Fuel DistributionSDR DL733030151Fire Loop · unserviceableDURING PUSHBACK APU FIRE WARNING CAME ON APU SHUTDOWN AND INDICATION EXTINGUISHED APPROXIMATELY 2 MINUTES LATER. FIRE INDICATION RETURNED AND REMAINED ON. CREW FIRED APU EXTINGUISHER BOTTLE AND FIRE LIGHT DID NOT GO OUT. INSPECTED APU AND COMPARTMENT AREA NFeb 13, 2003 · N304WA · Boeing 737347 · Fire DetectionSDR DL733030147Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE LT AND RT PRIMARY FORWARD CLEVIS LUGS. THE LHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.440 INCH TO REMOVE THE CORROSION. THE RHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.408 Feb 12, 2003 · N308WA · Boeing 737347 · Fuselage, Stabilizer Attach FittingsSDR DL733030146Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE REAR SPAR LT AND RT PRIMARY AND FAIL-SAFE FIN LUGS. THE BORES WERE ENLARGED TO REMOVE CORROSION. ALSO, THE FORWARD FACE OF THE LHS PRIMARY FIN LUG WAS SPOTFACED TO REMOVE CORROSION. REPAIR BUSHINGS WERE INSTALLEDFeb 12, 2003 · N308WA · Boeing 737347 · Vertical Stabilizer, Attach FittingsSDR DL733030144Control Module · failedAT 8000 FT APU FIRE LIGHT AND BELL SOUNDED, C/W PROC LIGHT STILL ON. AIR TURNBACK TO OAK. REPLACED FIRE DETECTOR CONTROL MODULE.Feb 11, 2003 · N304WA · Boeing 737347 · Fire DetectionSDR DL733030142Light · inoperativeEMERGENCY EXIT LIGHTING INOP AT ROW 22 AND 25. REPLACED LIGHT SOCKET AT ROW 22 AND REATTACHED WIRES AT ROW 25. BOTH EMERGENCY EXIT LIGHTS NOW CHECK NORMAL.Feb 10, 2003 · N312WA · Boeing 737347 · Emergency LightingSDR DL733030129Wire · arcedCO-PILOTS FRONT WINDSHIELD POWER WIRE IN UPPER RT CORNER ARCED. C/BS PULLED TO REMOVE POWER. REPLACED TERMINAL END AND HARDWARE. REPAIRED SAME.Feb 5, 2003 · N303WA · Boeing 737347 · Flight Compartment WindowsSDR DL733030081Coffeemaker · odorFLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR.Jan 23, 2003 · N306WA · Boeing 737347 · Buffet/GalleysSDR DL733030082Skin · dentedFUSELAGE / SKIN / FS 277-290.5 / STRG. 20R-22R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY GROUND EQUIPMENT JUST AFT OF THE LAVATORY SERVICE DOOR BETWEEN FS 277 & 290.5 AND BETWEEN STJan 21, 2003 · N3301 · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030066Fitting · corrodedCORROSION WAS FOUND ON THE AFT FACE OF THE RT REAR SPAR PRIMARY FITTING LUG. THE AFT SIDE OF THE LUG WAS SPOT FACED .005 INCH TO REMOVE THE CORROSION. A REPAIR BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.Jan 16, 2003 · N307WA · Boeing 737347 · Vertical Stabilizer, Attach FittingsSDR DL733030053Skin · debondedLEFT INBOARD FORE FLAP DISBONDED. REPAIRED PER ER/A 418180-14.Jan 13, 2003 · N307WA · Boeing 737347 · Trailing Edge FlapsSDR DL733030032Fitting · corrodedTHE RHS MLG SIDE STRUT SUPPORT FITTING HAD CORROSION IN THE BORE AND FORWARD AND AFT FACES OF THE FITTING AT FS 685, WL 188.5. THE BORE WAS OVERSIZED AND REPAIR BUSHINGS INTALLED. CORROSION WAS BLENDED FROM THE FACES. THE DAMAGE WAS FOUND AT HMV.Jan 7, 2003 · N307WA · Boeing 737347 · Fuselage, Landing Gear Attach FittingsSDR DL733030028Skin · damagedTHREE AREAS OF PRE-EXISTING DAMAGES WERE REPORTED. THE FIRST TWO WERE PREVIOUS BLENDS AT FS 757 AT STR 15R AND JUSTBELOW STR 14R. THE FINAL DAMAGE WAS JUST AFT AT STR 15R. ALL OF THE DAMAGES WERE REMOVED WITH TWO CUTOUTS. THE DAMAGE AT FS 757 RESJan 6, 2003 · N307WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733030027Frame · corrodedCORROSION WAS FOUND ON THE INNER FLANGE OF THE R-1 DOORWAY AFT FRAME JUST ABOVE THE FLOORLINE. THE CORROSION WAS REMOVED TO A MAX DEPTH OF .017". ADDITIONALLY, A GOUGE WAS REMOVED 4" ABOVE THE CORROSION TO A MAX DEPTH OF .021". A REPAIR ANGLE WAS INSJan 6, 2003 · N307WA · Boeing 737347 · Fuselage Main, FrameSDR DL733021460Fitting · corrodedCORROSION WAS FOUND IN THE BORE OF THE #1 PYLON CROWN BEAM AFT FITTING. THE BORE WAS REAMED TO A DIAMETER OF 3.102" TO REMOVE THE CORROSION. THE DAMAGE WAS FOUND AT HMV.Dec 23, 2002 · N307WA · Boeing 737347 · Nacelle/Pylon, Main FrameSDR DL733021446Skin · crackedFUSELAGE / SKIN / FS 727D / STRG. 23R : CRACK REPAIR A 3" CRACK WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF FS 727D. THE CRACK RAN ALONG THE EDGE OF THE INTERNAL BONDED INTERNAL DOUBLER JUSDec 16, 2002 · N311WA · Boeing 737347 · Fuselage Main, Plate/SkinSDR DL733021369Attach Fitting · corrodedCORROSION WAS FOUND ON THE AFT FACE OF THE #3 LUG AND THE FORWARD FACE OF THE #6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUGS. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 25, 2002 · N306WA · Boeing 737347 · Vertical Stabilizer, Attach FittingsSDR DL733021368Skin Panel · crackedSEVERAL CRACKS WERE FOUND IN THE KEEL BEAM LOWER SKIN PANEL FROM FS 661 TO FS 727. THE SKIN PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV.Nov 25, 2002 · N306WA · Boeing 737347 · Fuselage Main, Floor BeamSDR DL733021367Fitting · corrodedCORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 25, 2002 · N306WA · Boeing 737347 · Fuselage, Stabilizer Attach FittingsSDR DL733021366Wedge · delaminatedRH INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED PER ER/A 418047-14.Nov 25, 2002 · N306WA · Boeing 737347 · Trailing Edge FlapsSDR DL733021365Wedge · delaminatedTE WEDGE DISBONDED. REPAIRED PER ER/A 418046-14.Nov 25, 2002 · N306WA · Boeing 737347 · Trailing Edge FlapsSDR DL733021354Engine · making metalCLIMBING THROUGH FL240, NR 1 ROLLED BACK TO 0 INDICATIONS AFTER LOUD BANG. ENG FAIL CK LIST WAS COMPLETED. METAL IN TAIL PIPE, ENG CHANGED.Nov 21, 2002 · N303WA · Boeing 737347 · Engine (Turbine/Turboprop)SDR DL733021347Beam · wornWORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 20, 2002 · N306WA · Boeing 737347 · Nacelle/Pylon, Main FrameSDR DL733021346Spar · damagedWHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED.Nov 20, 2002 · N306WA · Boeing 737347 · Wing SparSDR DL733021340Flap · delaminatedINBOARD MID FLAP WAS FOUND DAMAGED BEYOND ALLOWABLE LIMITS. REPAIR PER ER/A 417941-14.Nov 19, 2002 · N305WA · Boeing 737347 · Trailing Edge FlapsSDR DL733021304Power Supply · dischargedEMERGENCY SEAT LIGHTS NOT WORKING FROM ROWS 1-12. REPLACED POWER SUPPLY UNIT. LIGHTS OPS NORMAL.Nov 8, 2002 · N305WA · Boeing 737347 · Emergency LightingSDR DL733021266Battery Pack · dischargedFIRST 5 ROWS OF EMERGENCY EXIT LIGHTS NOT WORKING. REPLACED BATTERY PACK, OP CKS NORMAL.Oct 30, 2002 · N305WA · Boeing 737347 · Emergency LightingSDR DL733021260Spar · corrodedDURING OVERHAUL THE NR 1 MID-FLAP WAS FOUND WITH CORROSION IN THE REAR SPAR LOWER CHORD. REPAIR PER ER/A 417872-14.Oct 29, 2002 · N304WA · Boeing 737347 · Trailing Edge FlapsSDR DL733021191Window · defectiveHAD ARCING AT POWER WIRE FOR FO WINDSHIELD WINDOW HEAT. REPLACED WINDOW.Oct 13, 2002 · N305WA · Boeing 737347 · Windshield/Door Rain/Ice RemovalSDR DL733021132Light · inoperativeEMERGENCY EXIT LIGHT AT SEAT 10 DEF INOP. RELAMPED SAME OPS CK GOODSep 23, 2002 · N3301 · Boeing 737347 · Emergency LightingSDR DL733021125Fitting · corrodedCORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE VERTICAL STABILIZER ATTACH LUGS. THE BORE DIAMETERS WERE INCREASED AND THE FACES BLENDED. OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND HMV.Sep 23, 2002 · N305WA · Boeing 737347 · Vertical Stabilizer, Attach Fittings
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