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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA970114Shear Beam Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 STRINGER 18 A LEFT SHEAR BEAM WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING 65C29228. (M)SDR USAA970113Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK STATION 748 TO STATION 751, STRINGER 18 RIGHT SKIN FUSELAGE. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. INSTALLED DOUBLER, REPAIR SRM 53-30-3. (M)SDR USAA970112Shear Beam Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK SHEAR BEAM WEB STRINGER 18A LEFT, JUST FORWARD OF STATION 727. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING 65C29228. (M)SDR USAA970111Stub Beam Web · crackINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK STATION 695 LBL 61 INCH STUB BEAM WEB. CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER, REPAIRED PER SRM. (M)SDR USAA970110Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 378 BBL 0 AFT OF EQUIPMENT COOLING EXHAUST SKIN. INSTALLED DOUBLERS, REPAIRED PER TR 53-30-04. (M)SDR USAA970109Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 33 INCH FLOORBEAM, BS 344 AT RBL 17 INCH TO LBL 50 INCH. INSTALLED DOUBLER, REPAIRED PER TR 53-10-13. (M)SDR USAA970108Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK T-CAP SEVERED ON LONGITUDINAL FLOORBEAM UPPER CHORD T-CAP, STATION 663 BL 0 WL 208. INSTALLED REPAIR DOUBLERS, REPAIRED PER BOEING DRAWING 65C34537. (M)SDR USAA970107Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION BEAM CABIN FLOOR BS 328, LBBL 50 INCH. INSTALLED REPAIR STRAPS, REPAIRED PER TR 53-10-01A. (M)SDR USAA970106Doublers · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK 2.5 INCHES LONG, BS 1138, SKIN DOUBLERS. FABRICATED NEW DOUBLERS AND INSTALLED, REPAIRED PER BOEING DRAWING 65-46585. (M)SDR USAA970105Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 727 BETWEEN STRINGER 14L AND 15L SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 9 AND 17. (M)SDR USAA970104Panel · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK AFT OF REAR SPAR, 18 INCH BELOW NR 4 RUDDER HINGE VERTICAL STABILIZER PANEL. INSTALLED DOUBLER, REPAIRED PER EA 42154. (M)SDR USAA970103Panel · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK RIGHT SIDE VERTICAL STABILIZER 18 INCH BELOW NR 4 HINGE STRUCTURAL PANEL. INSTALLED REPAIR DOUBLER, REPAIRED PER EA 42154. (M)SDR USAA970102Skin · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA BL 0 BS 628 STRINGER 1 SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)SDR USAA970101Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1.5 INCH CRACKS IN AFT SIDE OF BULKHEAD SKIN BS 178 LBL 5, WL 203 AND 195. INSTALLED BULKHEAD REPAIR AND REPAIRED PER TR NR 53-10-11. (M)SDR USAA970100T-Cap · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLES ON T-CAP CAP BS 344 LBL 21. REPLACED EXISTING BEAM REPAIR SECTION, REPAIRED PER TR 53-10-13. CORROSION TASK NR 53-107-02, CORROSION LVL 1. (M)SDR USAA970099Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AND .5 INCH CRACK SKIN AT BS 380 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)SDR USAA970098Floorbeam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 1 INCH CORRODED AREA FLOORBEAM BS 312, RBL 50. REPLACED T-CAP SPLICE, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA970097Skin · gougedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH GOUGE SKIN BS 668 JUST ABOVE STRINGER 14L. CUTOUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)SDR USAASB97083Fuel Heat Mnfld · failedRSW - FL 1115, ON TAKEOFF ROTATION, CREW RECEIVED ON OVERHEAT DETECTION LIGHT FROM THE NR 2 ENGINE. CREW CONTINUED TAKEOFF, WENT THROUGH PROCEDURES AND RETURNED TO FIELD AT RSW. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE NSDR USAASB97082O-Ring · leakingPHL - FL 1243, DURING CLIMB AT 10,000 FEET, THE NR 1 ENGINE OIL QTY DROPPED RAPIDLY TO ZERO, FOLLOWED BY A DROP IN OIL PRESSURE AND A RISE IN OIL TEMPERATURE. CAPTAIN DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLIGHT. FLIGHT RETURNED TO FIELD AT SDR F3LA97098Bulb · failedDEN - UPON ARRIVAL, FLIGHT CREW REPORTED L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LAMP AND CHECKED OK. (M)SDR USAASB97075Connector · looseALB - MAINTENANCE FOUND THE FIRST SIX ROWS OF INSEAT EMERGENCY EVACUATION LIGHTS INOP. MAINTENANCE FOUND WIRE CONNECTOR TO BATTERY PACK UNDER SEAT ROW FIVE, LEFT HAND SIDE, DISCONNECTED. RECONNECTED AND SECURED PLUG. OPERATIONAL CHECK GOOD. (M)SDR F3LA97097Skin · dentedFUSELAGE DENTS BETWEEN BS 360 AND 409. REMOVED SKIN FROM BS 360 TO 440, STRINGER 19R TO 24R. FABRICATED AND INSTALLED REPLACEMENT SKIN AND REPAIR IAW EWO 97-0080. REF WORK ORDER 214932 FUSELAGE 153/7-133 AND SRM. (M)SDR F3LA97096Skin · crackedPAE - A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT SKIN. WHILE ACCOMPLISHING EA 53-737-023 INADVERTENTLY OVERSIZED 34 HOLES ABOVE ALLOWABLE LIMITS IN BOEING SB 737-53-1163. REPAIRED DAMAGED HOLES IAW TRAMCO EWO 97-0140 BY OVERSDR USAASB97071Fan · failedEWR - FL 634 - WHILE DESCENDING TO FINAL APPROACH, CABIN AND COCKPIT CREW NOTICED A STRONG INTENSE ELECTRICAL BURNING SMELL THROUGHOUT THE ENTIRE AIRCRAFT. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMSDR USAASB97070Oil Line · leakingPHL - FL 1593 - CAPTAIN REPORTED HE SHUT DOWN THE NR 1 ENGINE IN FLIGHT, AS A PRECAUTION, DUE TO LOW OIL QUANTITY, LOW OIL PRESSURE INDICATION OF 20 PSI AND LOW OIL PRESSURE LIGHT. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED AT PHL WITHOUT INCIDENT. AIRCSDR USAASB97068Battery Pack · dischargedPIT - MAINTENANCE FOUND THE LEFT INTERIOR OVERWING EMERGENCY EXIT LIGHT ON SIDEWALL PANEL INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97063Wire · brokenCLE - MAINTENANCE FOUND THE EMERGENCY FLOOR LIGHT AT ROW 16ABC INOP. MAINTENANCE REPAIRED BROKEN WIRE. OPS CHECK GOOD. (M)SDR F3LA97093Skate Angle · crackedRIGHT VERTICAL STAB AFT MOUNT LUG INBOARD SKATE ANGLE CRACKED. REMOVED RIGHT VERTICAL STAB AFT MOUNTING LUG INBOARD SKATE ANGLE. FABRICATED REPAIR ANGLE FROM MATERIAL OF 7075-0 .071 AND HEAT TREATED BY GIDDENS INDUSTRIES, INC TO 7075-T6, PO NR 1ML212756. INSDR USAASB97060Battery Pack · dischargedROC - MAINTENANCE FOUND THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN FOR THE OVERWING EXITS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97061Power Supply · failedPHL - MAINTENANCE FOUND THE LEFT INTERIOR AND EXTERIOR OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE M192 POWER SUPPLY. OPS CHECK GOOD. (M)SDR USAA970074Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR .25 INCH CRACKS AT FASTENERS IN WEB SKIN OF LONGT FLOORBEAM BS 707, BL '0', WL 203. INSTALLED WEB REPAIR, REPAIRED PER BOEING DRAWING NR 65C34537. (M)SDR USAA970073Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 178 WL 201.5 LBL 5 BULKHEAD WEB. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)SDR USAA970072Skin · tornINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH TEAR IN EXTERIOR DOOR SKIN AT UPPER HINGE CUTOUT FORWARD SERVICE DOOR. INSTALLED EXTERIOR SKIN REPAIR, REPAIRED PER SRM 52-00-3, FIG 5. (M)SDR USAA970071Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK BS 765 STRINGER 19R FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAA970070Skin · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND PITTING CORROSION 2 INCH BY 8 INCH UNDER ANT MOUNT HAT CHANNEL AT BS 767 PLUS 12 BBL 0. INSTALLED EXTERIOR SKIN DOUBLER REPAIRED PER SRM 53-30-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA970069Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 INCH CRACK IN WEB SKIN AT BS 695 STUB BEAM LBL 61, WL 205. INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2. (M)SDR USAA970068T-Chord · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY .25 INCH CORRODED AREA (ALSO CRACKED) T-CHORD BS 500A PLUS 15 INCH S 26R. INSTALLED REPAIR ANGLE, REPAIRED PER EA NR 42093. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA970067Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BULKHEAD WEB BS 178 WL 198.5 LBL 5. INSTALLED DOUBLER, REPAIRED PER TR NR 53-10-11. (M)SDR USAA970066Bonded Doubler · crackedINT - DURING Q-6 CHECK HFEC INSPECTION, FOUND 2 CRACKS BONDED DOUBLER BS 663.75, S 18 A. SPOT FACED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER. REPAIRED PER EA 42114. (M)SDR USAA970065Angle · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SUPPORT ANGLE BS 178, RBL 5 WL 185. INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-17. (M)SDR F3LA97095Rib · crackedCLT - ONE INCH CRACK IN RIB AROUND RIVET HOLES BS 800, S19R TO S27R. INSTALLED NEW FRAME AND WEBS PER BOEING DRAWINGS 65-C35243 AND 69-42945, AND EA 59494. (M)SDR USAASB97057Wire · looseORD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 7 WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED WIRE BENEATHE SEAT AND RESECURED. OPERATIONAL CHECK GOOD. (M)SDR USAA970061Skin · crackedROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .5 INCH CRACK FORWARD GALLEY DOOR CUTOUT AFT LOWER CORNER STRINGER 17R BS 32 FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER TR 53-30-11/53-10-19 REV A. (M)SDR USAA970060Skin · crackedROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 INCH CRACK AFT ENTRY DOOR SKIN AT LOWER HINGE CUTOUT. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER TR 52-10-01. (M)SDR USAA970059Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BS 963.5. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. (M)SDR USAA970058Bracket · crackedCLT - I NSPECTION VISUALLY FOUND A 3 INCH CRACK LOCATED AT RADIUS OF SUPPORT BRACKET, FOR NLG ACTUATOR SUPPORT BEAM AFT END. FABRICATED REPAIR BRACKET AS PER SRM 51-40-03. (M)SDR F3LA97052Bracket · corrodedPAE - FOUND CORROSION (C53-107-01) ON AFT AIRSTAIR HINGE SUPPORT BRACKET AT BS 982, LBL 40, WL 208. REMOVED CORROSION FROM AFT AIRSTAIR HINGE SUPPORT BRACKET IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT PLATE AND FILLSDR F3LA97051Skin · crackedPAE - FORWARD SERVICE DOOR LOWER HINGE CUTOUT UPPER CORNER IS CRACKED .125 INCH IN LENGTH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING EXTERNAL DOUBLER IAW TRAMCO EWO 97-0094. (M)SDR F3LA97048Floor Beam · corrodedPAE - FLOOR BEAM UPPER CHORD AT BS 277 HAS TWO .625 INCH DIAMETER HOLES AT LBL 17 AND LBL 24, WL 208. CORROSION WAS DISCOVERED AT BS 277 LBL 17, LBL 20, AND LBL 25 WL 208. REMOVED CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS, IAW 53-10-1, REPAIRED FLOOR
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