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 USAA980218Chord · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 BULKHEAD LBL 25 COMPRESSION CHORD. STOP DRILLED AND INSTALLED DOUBLER. REPAIRED PER TR 53-10-03A. (M)SDR USAA980217Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FORWARD SERVICE DOOR CUTOUT FORWARD FRAME STATION 296, WL 208.5 LOW INBOARD RADIUS. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-40-3. (M)SDR USAA980216Doubler · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 952 STRINGER 12 LEFT DOUBLER. REPLACED DOUBLER AND REPAIRED PER TR53-30-07. (M)SDR USAA980215Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 360 STRINGER 20 R FRAME. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-40-3. (M)SDR USAA980214Skin · crackINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT ENTRY DOOR LOWER HINGE CUTOUT, LOWER FORWARD EDGE OF FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER SRM 53-30-3 FIG 34. (M)SDR USAA980213Floorbeam · crackINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 676.5, WL 206 PLUS WL 204, RBL 25 FLOORBEAM DOUBLER AND TRIPLER ON LONG FLOORBEAM UPPER AND LOWER CHORD. INSTALLED NEW DOUBLER AND CHANNEL, REPAIRED PER EO 5791G632 AND 65C34537-26. (M)SDR USAA980212Floorbeam · crackedDURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 676.5 WL 206 LBL 25 FLOORBEAM UPPER TEE DOUBLER AND TRIPLER OF LONGITUDINAL FLOOR SUPPORT. INSTALLED DOUBLER AND CHANNEL, REPAIRED PER EO 5791G632, 65C3453726. (M)SDR USAA980211Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 706 TO 714 BL '0' LONGITUDINAL FLOORBEAM. INSTALLED DOUBLER REPAIRED PER SB 737-57-1210 AND EA 43855. (M)SDR USAA980210Bulkhead Web · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS BS 178 LBL 4.75 WL 201 AND WL 198 BULKHEAD WEB. INSTALLED DOUBLER AND REPAIRED PER TR 53-10-11. (M)SDR USAA980209Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 360 AT STRINGER 20R FRAME. INSTALLED REPAIR DOUBLER AND REPAIRED PER SRM 51-40-3. (M)SDR USAA980208Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKED .5 INCH LONG STATION 460, STRINGER 20L TO 22L FRAME. REPLACED FRAME SECTION, REPAIRED PER SRM 51-40-3, BOEING DRW 69C36696, EO 5387G271. (M)SDR USAA980207Support · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 5.5 WL 184 SUPPORT. INSTALLED REPAIR ANGLE AND REPAIRED PER TR 53-10-17. (X)SDR USAA980206Stringer · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND TOOL DAMAGE .25 INCH STA 460 STR 19L STRINGER. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. (X)SDR USAA980205Stringer · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT ATTACH HOLE OF STR 16R (TIE CLIP) BS 747, STR 16R. FABRICATED REPAIR PARTS AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3. (X)SDR USAA980204Frame · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACKED FRAME AT LT BS 480 AT STR 22L. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (X)SDR USAA980203Frame · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STA 500 FRAME BETWEEN STR 28L AND STR 28R. DOUBLER INSTALLED PER SRM 51-40-3, REPAIRED PER SRM 51-40-3. (X)SDR USAA980202Frame · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 500 FRAME BETWEEN STR 28L AND STR 28R. CUT OUT DAMAGE, INSTALLED TWO DOUBLERS, REPAIRED PER SRM 51-40-3. (X)SDR USAA980201Frame · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 500 FRAME BETWEEN STR 28L AND STR 28R. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-3. (X)SDR USAA980200Support · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK NOSE GEAR ACTUATOR SUPPORT BEAM WEB AT RIVET HOLE, STA 227.8 + 4 INCHES. DOUBLER INSTALLED PER SRM 51-40-2, REPAIRED PER SRM 51-40-2. (X)SDR USAA980199Stringer · corrodedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND CORROSION ON STR 26L FROM STA 947+4 INCHES TO STA 1006. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)SDR USAA980198Stringer · corrodedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 FEET TO 6 FEET CORRODED AREA STR 25R BETWEEN STA 947.6 AND STA 967. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL; 2. (X)SDR USAASB98109Coalescer Bag · dirtyGSO - FLT 1704, EN ROUTE ATL-BWI, BOTH THE FORWARD AND AFT CABIN SMOKE DETECTOR ALARMS WENT OFF DURING FLIGHT. CREW NOTED A BURNING PLASTIC SMELL BUT COULD NOT LOCATE SOURCE. THERE WAS NO INDICATION OF SMOKE OF FIRE. FLIGHT DIVERTED TO GSO AND LANDED WITHOUSDR USAA980190Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 180 LBL 26 INCHES WL 195 SHEAR WEB. INSTALLED DOUBLER AND COVER PLATE ON 178 PRESSURE BULKHEAD, REPAIRED PER SRM 53-10-11 AND TR 53-10-18. (M)SDR USAA980189Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN DOOR FRAME CUTOUT JUST BELOW DOOR CENTERING FITTING (ON DOOR) FORWARD SERVICE DOOR. INSTALLED DOOR FRAME REPAIR, REPAIRED PER SRM 52-20-1, 51-40-3. (M)SDR USAA980188Floorbeam · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIPNUT HOLES ON FLOORBEAM UPPER 'T' CAP BS 947.5, RBL 8 TO RBL 50 (RT END). INSTALLED 'T' CAP REPAIR, REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)SDR USAA980187Floorbeam · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS OF 1 INCH BY 1 INCH EACH BS 986.5 LBL 42 INCHES TO RBL 40 FLOORBEAM. REMOVED UPPER CHORD, INSTALLED TEE CHORD WITH SPLICE ANGLES AND STRAPS. REPAIRED PER EA 43952. CORROSION TASK NR C53-SDR USAA980186Chord · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES STATION 718 LEFT KEEL BEAM CHORD. INSTALLED DOUBLER, REPAIRED PER EA 43946. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M)SDR USAA980185Floorbeam · chafedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CHAFE MARK ON MAIN FRAME 'I' BEAM BS 1016, RBL 34, 67 INCHES ABOVE FLOOR WL 275. FABRICATED AND INSTALLED DOUBLER, REPAIRED PER EA 43941. (M)SDR USAA980184Doubler · tornINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH TEAR IN BONDED DOUBLER BS 374, RBL 2 AT EQUIPMENT COOLING DUCT OUTLET. INSTALLED EXT SKIN DOUBLER, REPAIRED PER TR 53-30-4. (M)SDR USAA980183Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK IN FUSELAGE SKIN UPPER FORWARD END OF CUTOUT AFT SERVICE DOOR FUSELAGE SKIN. INSTALLED EXT DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M)SDR USAA980182Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK FUSELAGE SKIN AT LOWER HINGE CUTOUT AFT ENTRY DOOR. INSTALLED SKIN REPAIR/MOD, REPAIRED PER SRM 53-30-3 FIG 34. (M)SDR USAA980181Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 695 LBL 45 WL 202.5 LONGITUDINAL FLOORBEAM. INSTALLED REPAIR ANGLES, REPAIRED PER SRM 51-40-4 FIG 1. (M)SDR USAA980180Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 712-715 WL 203 BL '0' LONGITUDINAL FLOORBEAM WEB. CUTOUT DAMAGED AREA, INSTALLED WEB REPAIR PARTS AND REPAIRED PER EO 5394G176 AND DRAWING 165C34537. (M)SDR USAA980179Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 712-715 25 INCHES RBL WL 103 LONGITUDINAL FLOORBEAM WEB. INSTALLED WEB REPAIR PARTS, REPAIRED PER SRM 51-40-2. (M)SDR USAASB98107N2 Gearbox · failedBWI - FLT 2400 - CREW DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLT DUE TO LOSS OF OIL QTY AND PRESSURE AND TEMPERATURE INDICATIONS. FLT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE NORMALLY. TOTAL SSDR USAASB98104Light · inoperativePIT - PILOT REPORTED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ABOVE THE AFT SERVICE DOOR IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X)SDR F3LA98037Wire · failedELP - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT WAS 1 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)SDR USAA980173Skin · crackedCLT - DURING PILOTS REPORT A 2.75 INCH CRACK WAS FOUND IN THE SKIN BS 759-761.75 STRINGER 24L. INSTALLED FILLER AND DOUBLER PER REPAIR DOCUMENT SRM 53-30-3 FIG 17. (M)SDR USAA980168Skin · crackedROA - DUIRNG A-CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK BS 947, STR 24L, FUSELAGE SKIN. INSTALLED REPAIR WITH BLIND FASTENERS/SOLID FASTENERS TO BE INSTALLED NEXT Q-CHECK. REPAIRED PER SRM 53-30-3, PAGE 2C. (X)SDR USAA980148Angle · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA AND OTHER SMALLER AREAS AT BS 237 LBL 24 TO RBL 24 NOSE WHEEL WELL UPPER CHORD ANGLE. FABRICATED NEW ANGLE AND INSTALLED, REPAIRED PER DRW 65-45819 SRM 51-10-1. CORROSION TASK NR SDR USAASB98101Accessory Unit · failedBUF - FL475 - UPON LOWERING LANDING GEAR TO LAND AT BUF, CREW RECEIVED 3 GREEN LIGHTS AND 3 RED LIGHTS FOR THE GEAR. CREW RECYCLED GEAR 3 TIMES WHEREAS THE THIRD ATTEMPT, A NORMAL GEAR INDICATION WAS RECEIVED. THE CREW THEN ACCOMPLISHED A FLYBY AND THE TOWERSDR F3LA98032Skin · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED BULGING SKIN AT AFT CORNER OF CUTOUT AT BS 294.5 WL 148, RBL 24. MAINTENANCE REMOVED CORRODED AREAS. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-1, 51-30-2 AND ER 96-0315. (M)SDR F3LA98030Skin · crackedPAE - DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LOWER CORNER OF AFT CARGO DOOR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1, FIGURE 2, SRM 51-10-6, SRM 51-30-2 AND ER 98-0291. (M)SDR F3LA98029Skin · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED SKIN PILLOWING AT BS 415-430, STRINGER 18R TO 19R. MAINTENANCE REMOVED A 13 INCH BY 20 INCH CORRODED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, AND 53-30-3. (M)SDR USAASB98097Battery Pack · dischargedPIT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT AND THE WING-TO-BODY FAIRING EMERGENCY LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE M193 EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (X)SDR F3LA98031Lights · inoperativeDURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)SDR F3LA98028Skin · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED BULGE IN SKIN AT BS 1018 BETWEEN STRINGER 27-R AND 28-R. MAINTENANCE REMOVED DAMAGED AREA (7.1 INCH BY 2 INCH). FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3, PAGE 97, SRM 53-30-3, FIGURE 128, SRM 51-30-2, ANSDR F3LA98027Stringer · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-R, BS 360-540. MAINTENANCE REMOVED CORRODED AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3, FIGURE 16, AND SRM 51-30-2. (M)SDR USAA980160Skin · crackedROA - DURING C-5 CHECK, FOUND 2 INCH CRACK AT STA 740, S17R FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER EA 51596. (X)SDR USAA980159Skin · crackedROA - DURING C-5 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REMOVED CRACK AND INSTALLED DOUBLER PER EA 61580. (M)
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