Boeing 737-217

Service difficulty reports · 308

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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 = '737217'
  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 CALA9600693Angle · corrodedINSPECTION FOUND FRAME UPPER L-ANGLE AND WEB CORRODED AT BS 259, RT SIDE. THE L-ANGLE AND WEB WERE REMOVED AND REPLACED IAW SRM 51-40-2, 51-40-4, 51-30-2, 51-10-6 AND 51-10-2.May 6, 1996 · N12230 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600723Frame · crackedINSPECTION FOUND TWO, .75 INCH CRACKS IN FRAME AT BS 500B BETWEEN STRINGERS 22R AND 24R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING 65C25113.May 5, 1996 · N12230 · Boeing 737217 · Fuselage Main, FrameSDR CALA9600715Skin · delaminatedINSPECTION FOUND THE LT WING AILERON TAB SKIN DELAMINATING. THE DELAMINATED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9.May 5, 1996 · N12230 · Boeing 737217 · AileronsSDR CALA9600714Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR OUTER SKIN. THE DAMAGED AREA WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3.May 5, 1996 · N12230 · Boeing 737217 · Cargo/Baggage DoorsSDR CALA9600811Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, RBL 40 TO 55. THE CORRODED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND L-ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 52-20-1 AND 52-10-2.May 4, 1996 · N16232 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9600717Stringer · corrodedINSPECTION FOUND CHORD CORRODED AT STA 294 TO 335, STRINGER 26R. THE CHORD SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-0.May 4, 1996 · N12230 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9600810Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND MM 51-20.May 3, 1996 · N16232 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9600705Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK EXTENDING FROM RIVET OF FLOORBEAM AT STA 707, BBL 0. A REPAIR WAS INSTALLED IAW EA 5710-01322.May 2, 1996 · N12230 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9600812Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO FRAME AT STA 480, S21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND 51-10-2.May 1, 1996 · N16232 · Boeing 737217 · Fuselage Main, FrameSDR CALA9600803Bracket · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-0, 51-40-3, 51-10-2 AND 51-30-2.May 1, 1996 · N16232 · Boeing 737217 · Vertical StabilizerSDR CALA9600802Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2.May 1, 1996 · N16232 · Boeing 737217 · Vertical StabilizerSDR CALA9600797Channel · crackedTHE STRINGER TO FLOOR BEAM ATTACHMENT U-CHANNEL HAD TWO 1 INCH CRACKS AT STA 500A, STRINGER 28R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7 AND 51-30-2.May 1, 1996 · N16232 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600796Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 500, STRINGER 27L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2.May 1, 1996 · N16232 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600795Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 480, BL 0. THE CRACK WAS REMOVED AND A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.May 1, 1996 · N16232 · Boeing 737217 · Fuselage Main, FrameSDR CALA9600799Blkhd Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-21.Apr 30, 1996 · N16232 · Boeing 737217 · Fuselage Main, BulkheadSDR CALA9600809Skin · dentedINSPECTION FOUND SEVERAL DENTS IN FORWARD CARGO DOOR SKIN. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2 AND 51-10-2.Apr 29, 1996 · N16232 · Boeing 737217 · Cargo/Baggage DoorsSDR CALA9600808Skin · creasedINSPECTION FOUND A 3 INCH CREASE IN FUSELAGE SKIN AT STA 1120, BL 0. THE CREASED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Apr 29, 1996 · N16232 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600800Aux Track · crackedINSPECTION FOUND A .5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-30-2.Apr 29, 1996 · N16232 · Boeing 737217 · Wing Miscellaneous StructureSDR CALA9600709Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887, STRINGER 25R. THE DENTED AREA OF SKIN WAS CUT OUT, A SKIN SECTION AND SPLICE DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.Apr 29, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600708Skin · puncturedINSPECTION FOUND A HOLE IN FUSELAGE SKIN AFT OF AFT CARGO DOOR. A FILLER AND DOUBLER SMALL FLUSH REPAIR WAS INSTALLED IAW SRM 53-30-3.Apr 29, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600707Skin · dentedINSPECTION FOUND A DENT IN RT WING LEADING EDGE SKIN JUST OUTBOARD OF LANDING LIGHT. THE DENTED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1 AND 51-30-2.Apr 29, 1996 · N12230 · Boeing 737217 · Wing, Plate/SkinSDR CALA9600701Frame · crackedINSPECTION FOUND A .75 CRACK IN FRAME AT RT SIDE OF E AND E DOOR CUTOUT. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 57-40-3.Apr 29, 1996 · N12230 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600697Beam · crackedINSPECTION FOUND VERTICAL BEAM CRACKED IN HALF AT BS 540, RBL 24.8. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-2.Apr 29, 1996 · N12230 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600804Slide · inoperativeTHE L-1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. THE COVER LANYARD WOULD NOT RELEASE AND THE SLIDE ONLY PARTIALLY INFLATED. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-30.Apr 27, 1996 · N16232 · Boeing 737217 · Escape SlideSDR CALA9600807Sign · inoperativeTHE SELF ILLUMINATING EXIT SIGN IN AFT CABIN FAILED ILLUMINOSITY CHECK. THE EXIT SIGN WAS REMOVED AND REPLACED.Apr 26, 1996 · N16232 · Boeing 737217 · Emergency LightingSDR CALA9600805Wire · damagedA SECTION OF FORWARD CABIN EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. THE WIRING AT FORWARD TRACK SECTION WAS REPAIRED IAW MM 33-50-0.Apr 26, 1996 · N16232 · Boeing 737217 · Light System WiringSDR CALA9600722Bulkhead Web · crackedINSPECTION FOUND A 7 INCH CRACK IN BULKHEAD PRESSURE WEB AT STA 664, RBL 30. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, BulkheadSDR CALA9600713Stringer · corrodedINSPECTION FOUND STRINGER 23R CORRODED AT STA 355. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53-10-3.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9600712Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, FrameSDR CALA9600711Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED AT STA 360 TO 420. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-5.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9600710Stringer · corrodedINSPECTION FOUND STRINGER 20R CORRODED AT STA 383. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9600702Skin · crackedINSPECTION FOUND A 1.33 CRACK AT FASTENER HOLE IN AFT CARGO DOOR FRAME AFT SKIN. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600699Frame · crackedINSPECTION FOUND A 3 INCH CRACK AT NUTPLATE HOLE OF FRAME AT BS 500, LT SIDE. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW FRAME SEGMENT WAS SPLICED IN IAW BOEING DRAWING 65C25113.Apr 26, 1996 · N12230 · Boeing 737217 · Fuselage Main, FrameSDR CALA9600696Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN STA 500 AND 500A, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-41473.Apr 24, 1996 · N12230 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9600691Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500A BELOW WINDOW BELT ON BOTH LEFT AND RIGHT HAND SIDE OF FUSELAGE. BOTH AREAS WERE REPAIRED IAW SRM 53-30-3.Apr 24, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600690Skin · corrodedINSPECTION FOUND FUSELAGE SKIN AND FRAME SHEAR TIES CORRODED AT STA 328, STRINGER 18R. THE CORRODED AREAS OF SKIN AND SHEAR TIES WERE CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, SHEAR TIES WERE FABRICATED AND INSTALLED IAW SRM Apr 23, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600716Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1040. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.Apr 22, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600703Skin · dentedINSPECTION FOUND A DENT IN RT FUSELAGE AT STA 1040. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.Apr 22, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600692Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF L-1 DOOR LOWER SKIN. THE CRACKED SKIN WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3 AND 51-30-2.Apr 22, 1996 · N12230 · Boeing 737217 · Passenger/Crew DoorsSDR CALA9600687Skin · dentedINSPECTION FOUND SKIN DENTED FROM STA 360 TO 447 RT SIDE, STRINGER 19R TO 25R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 18, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9600686Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 259 TO 360, STRINGER 19R TO 24R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 18, 1996 · N12230 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CAL960453Connector · shortedCAE - FLT 1598 - THE NR 1 ENGINE FIRE LIGHT FLICKERED OFF AND ON AND THEN THE FIRE LIGHT AND BELL CAME ON STEADY WHILE EN ROUTE FROM TPA TO GSO. THE NR 1 ENGINE WAS SHUT DOWN. ONE FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. THE SECOND FIRE BOTTLEApr 10, 1996 · N12230 · Boeing 737217 · Fire DetectionSDR CAL960447Floorbeam · crackedGSO - INSPECTION FOUND A .50 INCH CRACK AND CORROSION ON COCKPIT AFT FLOORBEAM AT STA 459. THE CORRODED AREAS WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)Apr 5, 1996 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CAL960449Frame · crackedGSO - INSPECTION FOUND A 3 INCH CRACK IN LOWER FORWARD FRAME OF C-1 DOOR. THE FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Mar 30, 1996 · N14233 · Boeing 737217 · Cargo/Baggage DoorsSDR CAL960448Skin · corrodedGSO - INSPECTION FOUND THE NR 2 ENGINE FORWARD OUTBOARD COWL OUTER SKIN CORRODED AROUND ENGINE RADIUS WARNING PLACARD. THE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-2. (X)Mar 28, 1996 · N14233 · Boeing 737217 · Nacelle/Pylon, Plate/SkinSDR CA960402101Plug · dirty(CAN)APU FIRE WARNING ON ON GROUND JUST PRIOR TO TAKEOFF. APU HAD BEEN SHUT DOWN FOR 5 MINUTES. APU FIRE HANDLE PULLED STILL INDICATING FIRE FOR SOME MINUTES. VISUAL CHECK INDICATED NO EVIDENCE OF FIRE. FO UND EXHAUST FIRE DETECTOR PLUG CONTAMINATED BY CARBON Mar 22, 1996 · Boeing 737217 · Fire DetectionSDR CAL960309Wire · shortedFLT NR 1087 - EWR - THE CREW NOTICED APPROXIMATELY ONE THIRD OF THE EMERGENCY PATH LIGHTING SYSTEM WAS INOPERATIVE AFTER LOSING GROUND POWER. MAINTENANCE FOUND SHORTED WIRING BY ROW 4 WITH ASSOCIATED FUSES BLOWN. THE WIRING WAS REPAIRED AND THE FUSES WERE REMar 13, 1996 · N12230 · Boeing 737217 · Light System WiringSDR CAL960282Hyd Pump · leakingFLT NR 1160 - EWR - THE AIRCRAFT LOST ALL PRESSURE AND FLUID FROM THE 'A' HYDRAULIC SYSTEM DURING FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVE HYDRAULIC PUMP AT FAULT. THE NR 2 HYDRAULIC PUMP WAS REMOVMar 6, 1996 · N13234 · Boeing 737217 · Hydraulic Pump (Electric/Engine), MainSDR CAL960280Hyd Line · leakingFLT NR 512 - EWR - THE 'B' HYD SYSTEM WAS LOST AFTER TAKEOFF FROM EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF SYSTEM 'B' LOW PRESSURE LIGHTS. THE 'B' SYSTEM PUMPS WERE TURNED OFF AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAMar 5, 1996 · N12230 · Boeing 737217 · Hydraulic System, MainSDR CA960215103Csd · low oil pressure(CAN) AFTER TAKEOFF, #2 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED AND #2 GENERATOR DISCONNECTED. LANDED AIRCRAFT SAFELY AND REPLACED #2 CONSTANT SPEED DRIVE AND #2 OIL COOLER. #2 GENERATOR ALSO REPLACED DUE TO DAMAGE INCURRED WHILE CHANGINFeb 12, 1996 · Boeing 737217 · Alternator-Generator Drive
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