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 USAA991028Stringer · corrodedCLT - DURING A RON VISUAL INSPECTION FOUND CORROSION 9 INCHES BY 2 INCHES BY .075 INCH AT BS 500B PLUS 14 INCHES, STR 28R STRINGER (KEEL BEAM). CORROSION LEVEL 2. REMOVED CORROSION, INSTALLED KEEL BEAM REPAIR ANGLES AND SHIMS PER EA 65660. (X)SDR USAA991027Skin · corrodedCLT - DURING A RON VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 2 INCH BY 8 INCH AT BS 500B PLUS 14 INCHES, STR 28R SKIN. DAMAGE CUT-OUT AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-03 FIG 6. (X)SDR USAASB99231Csd Oil Cooler · bird strikeBOS - FLT 2851 - DURING TAKEOFF, TWO SEA GULLS STRUCK THE NR 2 ENGINE. AFTER INGESTION, THERE WAS A SMELL IN THE CABIN. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED BIRD STRIKE CONSDR USAA990992Skin · crackedTPA - DURING A CX-CHECK VISUAL INSPECTION, FOUND A .250 INCH LONG CRACK AT AFT SERVICE DOOR BOTTOM HINGE AFT CORNER DOOR SKIN. INSTALLED REPAIR DOUBLER PER TR 52-40-03A AND EA 65097. (M)SDR USAA990953Skin · crackedCLT - DURING WALKAROUND CHECK, VISUAL INSPECTION, FOUND A .625 INCH CRACK IN SKIN AT STATION 380 2 INCHES LEFT OF CENTER LINE. INSTALLED REPAIR DOUBLERS PER TR 53-30-04, DRAWING 65C3390. (M)SDR USAA990931Skin · crackedTPA - DURING CX-4 CHECK VISUAL INSPECTION VERIFIED WITH EDDY CURRENT, FOUND A 3 INCH CRACK IN SKIN STATION 938, STRINGER 24L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)SDR USAASB99223Battery Pack · dischargedBWI - FLT 2639 - BEFORE DEPARTURE, THE CAPTAIN REPORTED THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA990927Stiffener · corrodedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION, LOWER END OF STIFFENER, STATION 540, RBL 14.90. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER SRM 51-40-4 FIG 1.. (M)SDR F3LA99119Axle · corrodedDEN - DURING C-4 CHECK, INSPECTION REPORTED DAMAGE FROM CORROSION PITTING ON NOSE LANDING GEAR RT AXLE. REPLACED INNER CYLINDER ASSY PER BOEING MM 32-21-11. (M)SDR USAA990947Skin · crackedBOS - DURING RON FOUND 1.125 INCH CRACK IN SKIN AT 767, 1.5 INCH ABOVE STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3, PAGE 2E, FIG 1 SHT 4. (M)SDR USAA990946Skin · crackedBOS - DURING RON, FOUND 1.5 INCH CRACK IN SKIN AT STATION 770, .5 INCH BELOW STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3, PAGE 2E, FIG 1 SHT 4. (M)SDR USAASB99212Line · failedMCO FLT 2692 - SHORTLY AFTER TAKEOFF FROM MCO, AFTER GEAR AND FLAP RETRACTION, THE 'A' HYDRAULIC SYSTEM LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT FLICKERED. HYDRAULIC QUANTITY RAPIDLY WENT TO ZERO. AIRCRAFT LEVELED OFF AT 5,000 FEET AS CREW ACCOMPLISHED CHSDR USAASB99211Module · failedSDF - FLT 1473 - AIRCRAFT WAS PREPARING TO LAND AT ADF, WHEN THE MASTER CAUTION FLIGHT CONTROL ANNUNCIATOR ILLUMINATED ALONG WITH THE 'A' HYDRAULIC SYSTEM LOW PRESSURE LIGHT. SYSTEM PRESSURE WAS AT 1,200 PSI WHILE QTY REMAINED CONSTANT AT 3.5 GALLONS. THE LASDR USAASB99209Wire · damagedCLT - FLT 8031 - AFTER TAKEOFF FROM CLT, THE AIRCRAFT YAWED LEFT AND RIGHT. AIRCRAFT CONTROL WAS MAINTAINED AND QUICK REF HANDBOOK PROCEDURES WERE ACCOMPLISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SDR F3LA99115Wire · failedDEN - DURING C-4 CHECK INSPECTION, REPORTED EMERGENCY EXIT SIGN INOPERATIVE AT ROW 9 LEFT SIDE. MAINTENANCE REPAIRED WIRING AT SEAT 9C FOR EMERGENCY EXIT SIGN. (M)SDR USAA990880Skin · crackedTPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK IN SKIN STATION 727B STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1 AND EA 64759. (M)SDR USAA990851Skin · crackedTPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 3.25 INCH CRACK IN SKIN LONGERON 17R, STATION 727A. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 65090. (M)SDR USAA990850Shear Tie · corrodedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND CORROSION ATTACH ANGLE SHEAR TIP STRINGER 26L STATION 967 FRAME. CORROSION LEVEL 1. REINSTALLED STRINGER SHEAR TIP PER SRM 53-10-3. (M)SDR USAA990849Skin · crackedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 1 INCH CRACK IN SKIN AT STATION 727A PLUS 7 AND STRINGER 19L. REPAIRED PER SRM 53-30-3 FIG 1. (M)SDR USAA990848Skin · crackedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 4 INCH CRACK IN SKIN AT STATION 727B PLUS 14 AND STRINGER 18L. REPAIRED PER SRM 53-30-3 FIG 25. (M)SDR F3LA99113Wire · brokenDEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN GROUND WIRE AFT OF BATTERY PACK CONNECTION. TC: 90,747. (X)SDR F3LA99112Wire · brokenDEN - FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE AT D9022P AND CHECKED OKAY. TC: 90,745. (X)SDR F3LA99111Battery Pack · dischargedDEN - FLT 317 - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS FLICKERED IN-FLIGHT. MAINTENANCE RECHARGED BATTERY PACKS AND OPERATIONAL CHECKED OKAY. PART TC: 90,740. (X)SDR F3LA99109Mask · did not deployDEN - DURING DEMONSTRATION, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM MANUAL ACTIVATION PER MM 35-21-00A AND CHECKED OKAY. TC: 88,247. (X)SDR F3LA99108Masks · did not deployDEN - DURING DEMO FLIGHT, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DROP IN MANUAL MODE. MAINTENANCE RESET T-HANDLE IN COCKPIT AND PERFORMED AN ANNUAL DROP TEST PER MM 35-21-00A. SYSTEM CHECKED OKAY. TC: 91,843. (X)SDR USAASB99196Connector · failedBWI - FLT 2620 - AFTER TAKEOFF, THE STANDBY HYDRAULIC QTY LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGNCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG FOR THE STANDBY HYDRAULIC LOW QUANTISDR F3LA99110Battery Charger · failedDEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING DID NOT EXTINGUISH WHEN TESTED. MAINTENANCE REPLACED AFT SEAT BATTERY CHARGING UNIT. TC: 9,073. (X)SDR USAASB99193Position Ind · failedBWI - FLT 2638 - ON PREPARATION FOR LANDING AT BWI, CREW ENCOUNTERED A SPLIT FLAP INDICATION OF 1 DEGREE. FLAPS WOULD NOT EXTEND BEYOND 2 DEGREES OR RETRACT. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. FLIGHT LANDED WITHSDR USAASB99192Fuel Control · unknownPIT - FLT 1279 - APPROXIMATELY 100 MILES EAST OF PIT, FLIGHT WAS CLEARED TO FL350 FROM FL290. CAPTAIN REPORTED A THROTTLE SPLIT WITH A 5 KNOT DIFFERENCE IN ENGINE THRUST DURING CLIMB. FLIGHT RETURNED TO FL290 AND THEN DIVERTED TO PIT WHERE THE FLIGHT LANDED SDR USAASB99184Batteries · dischargedROC - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE COCKPIT DOOR INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECKED GOOD. (X)SDR USAASB99182Hinge · failedBWI - FLT 2622 - DURING CLIMB-OUT FROM BWI, CREW REPORTED A LOUD UNBEARABLE SQUEAL COMING FROM THE MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTSDR USAA990744Skin · crackedPIT - DURING RON MAINTENANCE, FOUND 5 INCH LONG CRACK AT STATION 420, BODY LINE 0, CENTER LINE UNDERSIDE ON FUSELAGE SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1 (SHEET 4). (M)SDR USAA990743Floorbeam · corrodedTPA - DURING CX-1 CHECK, FOUND 2 INCH BY 10 INCH CORRODED AREA ON TOP SECTION OF 985.5 FLOORBEAM, RT SIDE AT PREVIOUS REPAIR. INSTALLED NEW REPAIR AT FLOORBEAM PER TYPICAL REPAIR MANUAL 53-60-01. (M)SDR USAA990742Fitting · crackedTPA - DURING CX-1 CHECK, FOUND TWO EACH 1 INCH LONG CRACKS IN FITTING AT BS 727 COMPRESSION CHORD, ONE AT RBL 25 AND ONE AT RBL 45. INSTALLED REPAIR PER TYPICAL REPAIR 53-10-03A. (M)SDR USAASB99180Adc · failedBWI - FLT 2612 - DURING TAKEOFF AND CLIMB-OUT FROM BWI, CAPTAIN REPORTED HE LOST NR 1 AIR DATA COMPUTER AND WINDSHEAR WARNING WAS GOING OFF. PRESSURIZATION WAS LOST IN AUTOMODE AND REGAINED BY SWITCHING OVER TO STANDBY MODE. CAPTAIN PLACED FLIGHT IN HOLDING SDR USAA990732Tie Clip · crackedCLT - DURING C-CHECK, FOUND .25 INCH CRACK IN TIE CLIP AT STATION 480 STRINGER 24L (TOP LEFT CORNER). REPLACED TIE CLIP PER SRM 51-40-02. (M)SDR USAA990736Skin · crackedPIT - DURING RON CHECK, FOUND .5 INCH LONG CRACK AT STATION 727A STRINGER 18 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M)SDR USAA990735Skin · crackedPIT - DURING RON CHECK, FOUND A .75 INCH CRACK AT STATION 747 STRINGER 18 RT AND A .75 INCH LONG CRACK AT STATION 767 STRINGER 19 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M)SDR USAA990734Web · crackedPIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED SHEETMETAL DOUBLERS AND FILLERS PER TYPICAL REPAIR 53-10-12 REV A AND EA 52440. (M)SDR USAASB99173Light · failedCLE - PILOT REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD GALLEY DOOR ILLUMINATED WITH THE EMERGENCY EXIT SWITCH OFF AND GROUND SERVICE POWER ON. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY OVER THE FORWARD GALLEY DOOR. OPERATIONAL CHECK GOOD. SDR USAA990673Skin · crackedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN SKIN AT STATION 727B AND STRINGER 18L, SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)SDR F3LA99102Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)SDR F3LA99101Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)SDR F3LA99100Wire Harness · damagedDURNG C-CHECK INSPECTION, REPORTED DAMAGED WIRING IN THE VERTICAL STABILIZER. CAUSE OF DAMAGE APPEARS TO BE SKYDROL HYDRAULIC FLUID. THE DAMAGE BEGAN APPROX 8 INCHES FROM RUDDER PCU ELECTRICAL CONNECTORS D-289 AND D-291 AND CONTINUED FOR APPROX 5 FEET, AFFECSDR USAASB99166Uplock Sensor · failedBOS - FLT 2673 - AFTER TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON. CAPT RECYCLED THE GEAR BUT THE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENSDR USAA990704Angle · crackedCLT - DURING A RON VISUAL INSPECTION, FOUND A 3 INCH CRACK AT NOSE GEAR GUSSET ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-6. (M)SDR USAA990663Seat Track · corrodedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND MINOR CORROSION AT FORWARD END OF LEFT SEAT TRACK INBOARD AND OUTBOARD, CORROSION LEVEL 1. SPLICED IN AND FABRICATED REPAIR PARTS PER SRM 53-10-5 FIG 2. (M)SDR USAASB99160Wire · brokenCLT - PILOT REPORTED THAT THE OVERHEAD EMERGENCY LIGHTS AND THE FLOOR LEVEL EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. MAINTENANCE FOUND A BARE WIRE AT THE CONNECTOR FOR THE BATTERY PACK AT SEAT ROW 5ABC AND A BROKEN WIRE AT THE WIRE PLUG AT SESDR USAA990664Skin · crackedCLT - DURING RON CHECK VISUAL INSPECTION, FOUND A 75 INCH CRACK AFT SIDE OF EQUIPMENT COOLING EXHAUST AT STATION 380 BETWEEN BL 0 AND STRINGER 28L FUSELAGE SKIN. REPAIRED PER TR 53-30-04. (M)SDR USAA990662Skin · crackedCLT - DURING A PILOTS REPORT VISUAL INSPECTION CHECK, FOUND A 2. 5 FT CRACK JUST BELOW STRINGER 21L FROM STATION 978 TO 980 IN FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 6 AND EA 65015. (M)
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