Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 W8PA970097Intercostal · corrodedDURING C-CHECK, FOUND CORROSION BS 996-1006, LBL 10 - 13, WL 208 (INTERCOSTAL). REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL. (M)SDR W8PA970096Fitting · corrodedDURING C-CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR GIRT BAR FITTING MOUNTS. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, INSTALLED NEW FITTING MOUNTS IAW SRM 51-40-02. (M)SDR W8PA970095Stiffener · corrodedDURING C-CHECK, FOUND CORROSION ON STIFFENER AT LBL 16.5, BS 314, 320, 325, WL 208. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, REMOVED CORRODED PARTS AND INSTALLED NEW PARTS IAW SRM 51-10-02. (M)SDR W8PA970094Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 947, RBL 6, WL 208. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICATED INSTALLED PARTS PER SRM 53-30-51. (M)SDR W8PA970093Angle · crackedDURING C-CHECK, INTERCOSTAL TO SKIN TIE ANGLE IS CRACKED AT STATION 290, WL 241, BETWEEN STRINGER 13 AND 14 RIGHT. REMOVED AND REPLACED ANGLE. (M)SDR W8PA970092Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION BS 1006, LBL 36-RBL 36, WL 208, AROUND FLOOR BOARD ATTACH HOLES. REMOVED OUT OF LIMITS AREA AT BS 1006, LBL 29, WL 208. REPAIRED IAW SRM 51-70-11. (M)SDR W8PA970091Channel · corrodedDURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 11.5, BS 347, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL. (M)SDR W8PA970090Floor Support · corrodedDURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 45, BS 953, AND BS 957.5, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL (FLOOR SUPPORT).SDR W8PA970089Hat Channel · corrodedDURING C-CHECK, FOUND CORROSION ON CORNER OF HAT CHANNEL AND SUPPORT BRACKET BS 307, LBL 11, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)SDR W8PA970088Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION BS 967, FOUND ON UPPER CHORD OF THE FLOORBEAM AT BS 344, RBL 8.5, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)SDR W8PA970087Support · corrodedDURING C-CHECK, FOUND CORROSION BS 967, LBL 53 - RBL 53, WL 208, (AROUND FLOOR BOARD ATTACH HOLES). CORROSION FOUND TO BE OUT LIMITS. REPAIRED UPPER CHORD. (M)SDR W8PA970086Former · crackedDURING C-CHECK, FORMED SECTION CRACKED AT BS 295, RBL 54, WL 209. REMOVED AND REPAIRED CRACKED AREA. (M)SDR W8PA970085Intercostal · corrodedDURING C-CHECK, INTERCOSTAL CRACKED AT AFT CARGO DOOR UPLATCH ATTACH BS 787-807, RBL 16.5, WL 203. REPLACED INTERCOSTAL WITH NEW PART. (M)SDR W8PA970084Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 328, LBL 28.5, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS. (M)SDR W8PA970083Hat Channel · corrodedDURING C-CHECK, FOUND CORROSION BS 996, LBL 22-34, WL 208, (HAT CHANNEL FORWARD FLANGE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW HAT CHANNEL. (M)SDR W8PA970082Hat Channel · corrodedDURING C-CHECK, FOUND CORROSION BS 996, RBL 5-49, WL 208-209. (HAT CHANNEL AND GALLEY ATTACH ANGLE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW ATTACH ANGLE AND HAT CHANNEL. (M)SDR W8PA970081Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)SDR W8PA970080Angle · corrodedDURING C-CHECK, CORROSION BS 1012-1030, LBL 6 - 1030, LBL 6 - RBL 15, WL 208-209, (FLOOR WEB ATTACH STRAPS AND GALLEY ATTACH ANGLES). REMOVED CORROSION, FROM GALLEY ATTACH ANGLES AND FOUND TO BE OUT OF LIMITS, AFTER CORROSION REMOVAL FOUND OTHER AREAS TO BE ISDR W8PA970079Intercostal · corrodedDURING C-CHECK, FOUND CORROSION BS 108, LBL 8, WL 208 (INTERCOSTAL). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL. (M)SDR W8PA970078Intercostal · corrodedDURING C-CHECK, FOUND CORROSION BS 988, RBL 17, WL 208, INTERCOSTAL FLOOR ATTACH HOLE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW AND INSTALLED NEW INTERCOSTAL. (M)SDR W8PA970076Skin · corrodedDURING C-CHECK, FORWARD CARGO DOOR, INNER SKIN CRACKED AND/OR GOUGED AT LIGHTENING HOLE 17 INCH AFT OF FORWARD, EDGE 33 INCH ABOVE LOWER EDGE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER. (M)SDR W8PA970075Support · corrodedDURING C-CHECK, FOUND CORROSION ON BOTTOM SIDE OF FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATES BS 847-867, RBL 19-24, WL 161. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW SUPPORT. (M)SDR W8PA970074Channel · corrodedDURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500, LBL 24, WL 155. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE. (M)SDR W8PA970072Clip · corrodedDURING C-CHECK, FOUND CORROSION ON STRINGER CLIP BS 867, RBL 21, WL 164. REMOVED CORROSION FROM STRINGER CLIP FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STRINGER CLIP. (M)SDR AWXA9700156Wire · disconnectedDURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 2L EMERGENCY LIGHT INOP. RECONNECTED WIRES STC - SA1889SO.SDR USAASB97047Wire · shortedTPA - MAINTENANCE FOUND THE INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED A SHORTED WIRE IN THE FLOOR. OPERATIONAL CHECK GOOD. (X)SDR W8PA970071Extrusion · corrosionDURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON BOTTOM SIDE OF CARGO TRACK BS 753.5, LBL 8, WL 141, (IN AFT CARGO BAY). REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED. (M)SDR USAASB97038Packing · failedCLT - FL 2109 - FLIGHT DIVERTED TO CLT DUE TO 'A' SYSTEM HYDRAULIC LOSS. QUANTITY WENT TO EMPTY. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND A FITTING LEAKING AT THE 'A' SYSTEM HYDRAULISDR AWXA9700078Battery Charger · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 - 4. REPLACED EMERGENCY LIGHT CHARGER AND BATTERY ASSEMBLY AT LT FORWARD POSITION. EMERGENCY OPS CHECK GOOD. STC - SA1889SO. BATTERY ASSEMBLY 849029 DISCHARGED LT FORWARD CABIN.SDR AWXA9700077Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND FIRST CLASS EMERGENCY LIGHT INOPERATIVE. REPLACED LT FORWARD BATTERY PACK. OPS CHECK GOOD. STC - SA1889SO.SDR USAA970048Floor Beam · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 56 INCHES LOCATED AT FLOOR BEAM STATION 312. CORROSION TASK NR C53-107-03, CORROSION LEVEL 2. INSTALLED REPAIR ANGLES AS PER TYPICAL REPAIR 53-10-03. (M)SDR USAASB97030Rod End · failedPIT - FL 96 - FLIGHT RETURNED TO FIELD AT PIT DUE TO THE NR 6 LEADING EDGE SLAT WOULD NOT RETRACT. CAPTAIN ADVISED THAT THE NR 6 SLAT INDICATED THAT IT WAS ST ILL EXTENDED AND THAT CONTROL FEEL WAS ABNORMAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUTSDR USAASB97021Power Supply · dischargedTPA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOP AT ROWS 6, 7, 8 AND 10 ON THE LEFT SIDE OF CABIN. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE CABIN AT STAITON 629L. OPS CHECK GOOD. (M)SDR USAA970001Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES IN LENGTH AT BS 178 LBL 6 INCHES WL 200 BULKHEAD. REPAIRED PER T/R 53-10-07 REV A. (M)SDR USAA970000Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES AT BS 178 BULKHEAD RBL 6 INCHES WL 200. REPAIRED PER T/R 53-10-07 REV A SRM 51-10-02 PAGE 19. (M)SDR USAASB97005Oil Line · leakingINT - FL 7901 - FLIGHT WAS IN THE PROCESS OF COMPLYING WITH TEST HOP PROCEDURES, AFTER A HEAVY MAINTENANCE VISIT, WHEN THE CREW NOTICED A RAPID OIL QTY LOSS IN THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE AND RETURNED TO FIELD AT INT. NO EMERGENCY WAS DECLSDR AWXA9600777Wire · disconnectedDURING ROUTINE MAINTENANCE CHECK, FOUND ROW 19 FLOOR PROXIMITY LIGHTS INOP. RESPLICED WIRE, OPS NORMAL, STC - SA3140NM.SDR USAASB96253Battery Pack · dischargedALB MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATION LIGHTS INOPERATIVE AT ROWS 12, 16, 18, AND 20. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (X)SDR USAASB96249Oil Bypass Sw · failedPIT - FLT 1594 - AFTER LEVEL OFF AT FL 250, CREW RECEIVED THE LEFT OIL FILTER BYPASS INDICATION. LIGHT REMAINED ON WHEN THRUST WAS REDUCED. CREW SHUT DOWN LEFT ENGINE. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED THE OIL SDR USAA960768Bulkhead Skin · crackedINT - DURING Q-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND CRACK .25 INCH LONG AT STATION 178 BULKHEAD SKIN LBL 4 WL 199. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED. REPAIRED PER TR 53-10-07 STEP 2 AND 3. (M)SDR USAA960767Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK INTERIOR NR 1 CARGO DOOR SKIN STATION 450. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED. REPAIRED PER SRM 51-40-2, FIG 1. (M)SDR USAA960766Web · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORROSION STATION 986 TO 1006 LBL 38 WEB. FABRICATED WEB AND INSTALLED, REPAIRED PER BOEING DRAWING 65-C32677. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M)SDR USAA960765Angle · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 3 INCH BY .040 INCH, STATION 960 RBL 9 FLOOR SUPPORT ANGLE. REPLACED FLOOR ANGLE, REPAIRED PER MODIFIED PART NR 65-C10592-153. REPAIRED PER SRM 51-10-2 AND BOEING DRAWING NR 65-46812. (M)SDR USAA960764Skin · holeINT - DURING Q-3 CHECK CARRY OVER INSPECTION, FOUND 2 INCH BY 3 INCH HOLE BS 328, BETWEEN STRINGER 20R TO STRINGER 21R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-00-01 FIG 202. (M)SDR USAA960763Angle · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND 1.5 INCH CRACK BS 540 ABOVE STRINGER 22R ATTACH ANGLE. INSTALLED DOUBLER, REPAIRED PER TR 53-50-03. (M)SDR USAA960762Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH CORRODED AREA BS 500 D PLUS 2 INCHES STRINGER 28R. REMOVED CORRODED AREA INSTALLED REPAIR PARTS COMPLETED REPAIR, REPAIRED PER SRM 53-30-12 FIG 202. (M)SDR USAA960761Skin · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND GOUGED 4 INCH BY .75 INCH BY .037 INCH RIGHT WING INBOARD LEADING EDGE OF OUTBOARD MID FLAP SKIN OF FLAP. REMOVED EXISTING REPAIR, FABRICATED FILLER AND DOUBLER AND INSTALLED. REPAIRED PER EA 41754, SB 737-57-1SDR USAA960760Skin · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND GOUGED 3 INCH BY .5 INCH BY .027 INCH LEFT WING INBOARD LEADING EDGE OF OUTBOARD MIDFLAP SKIN. REMOVED EXISTING REPAIR, FABRICATED FILLER AND DOUBLER AND INSTALLED. REPAIRED PER EA 41753 AND SB 57-1236. (M)SDR USAASB96237Tire Tread · separationBWI - FL 209 - AFTER T/O, INFORMED TIRE DEBRIS WAS ON RUNWAY AFTER T/O. DURING PREP FOR LANDING, THE LT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. AFTER TWO FLYBYS, TOWER DETERMINED GEAR DOWN WITH SOME DEBRIS BETWEEN LEFT MAIN TIRES. F/O MADE VISUAL INSPECTIONSDR AWXA9600683Wire · shortedDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS OUT AT ROW 17. REMOVED AND REPLACED BATTERY ASSEMBLY. REMOVED AND REPLACED OPEN FUSE IN EMERGENCY BATTERY CHARGER ASSEMBLY. REPAIRED SHORTED WIRES UNDER SEAT AT ROW 21, LIGHTS CHECK GOOD.
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