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 USAA960794Keel Beam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .25 INCH DIAMETER SEVERAL AREAS BS 670 TO 727 LEFT SIDE KEEL BEAM W/W LEFT OUTBOARD FLANGE. INSTALLED REPAIR STRAP AND CHAFING STRIP, REPAIRED PER EA 41879. CORROSION TASK NR C53-212-01, CORROSION LEVSDR USAA960793Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 BULKHEAD LBL 5.7 WL 184 BEAM CHORD. STOP DRILLED AND INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-17. (M)SDR F3LA96066Skin · crackedFLT 93 - DEN - DURING WALK AROUND, MAINTENANCE REPORTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STATION 784 TO 786, .5 INCH ABOVE STRINGER 24L. MAINTENANCE STOP DRILLED CRACK AND INSTALLED TYPICAL REPAIR PER BOEING SRM 53-30-3. (M)SDR F3LA97005Skin · crackedPAE - FOUND CRACK IN EXTERNAL SKIN AT BS 797, STRINGER 24 LEFT, CRACK WAS APPROXIMATELY 4 INCHES LONG. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-30-3. WORK WAS DOCUMENTED ON TRAMCO CARD NR FUSELAGE 240, CUST ID NR 0732. (M)SDR USAASB96261Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB96260Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS AT THE AFT GALLEY SERVICE DOORS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT RIGHT SIDE OF THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M)SDR F3LA96065Clip · crackedPAE - FOUND CRACKED STRINGER CLIP BS 727A STRINGER 21R. REMOVED STRINGER CLIP BS 727A STRINGER 21R. FABRICATED STRINGER CLIP, ALODINED AND PRIMED. INSTALLED STRINGER CLIP IAW SRM 51-20-1 AND SRM 51-30-02. (M)SDR F3LA96064Sill · corrodedFOUND CORROSION 9C53-107-02) THROUGH R/T MOP SILL, BS 920-960, RBL 60, WL 208. FOUND R/T MOP SILL (CREASE BEAM) CORRODED OUT OF LIMITS PER SRM 53-10-3. REMOVED AND REPLACED MOP SILL AT BS 920-960, RBL 60, WL 208 PER SRM 51-30-02. (M)SDR USAA960786Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION STRINGER 27L BS 957 TO 962. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAA960787Skin · corrosionGSO - DURING TRANSIT CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH SQUARE AT 6 INCH AFT OF 500 A, 2 INCH SQUARE AT STATION 500 AT STRINGER 28 R STATION 500 A 6 INCH AFT BELLY AND 500 STATION SKIN, STRINGER. INSTALLED DOUBLER, REPAIRED PER EA 41878. (M)SDR USAA960783Skin · crackedROA - DURING A-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK LOCATED AT STA 767 AT S20R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGES 11 THROUGH 12B. (X)SDR USAASB96255Light · failedBWI - FLT 404 - CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE SEAT 9C IS INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAA960775Frame · crackedINT - DURING Q-4 CHECK, EDDY CURRENT INSPECTION FOUND .1250 INCH LONG CRACK FRAME CHORD STA 727 STR 18A LEFT SIDE. REPLACED FRAME CHORD, REPAIRED PER EO 5394G068. (X)SDR USAA960774Strap · tornINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND .50 INCH GOUGE AND TORN AT REINFORCEMENT STRAP STA 907, STR 20R. REPAIRED DOUBLER, REPAIRED PER SRM 53-10-4 AND EA 41803. (X)SDR USAA960773Skin · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION STA 767 TO STA 787, BL ZERO 'O' BRACKET AND SKIN. INSTALLED SKIN DOUBLER AND REPLACED BRACKET. REPAIRED PER SRM 53-30-3. (X)SDR USAA960772Bulkhead Web · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION REAR PRESSURE BULKHEAD WEB LOWER EDGE BS 1016, S23R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (X)SDR USAA960771Angle · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 40 INCH Z-ANGLE LEFT SIDE STA 947 TO STA 986. INSTALLED REPAIR AT FORWARD SECTION OF UPPER FLANGE. REMAINDER OF CORROSION WAS MINOR, REPAIRED PER SRM 53-40-3. CORROSION TASK NR: C53-107-02SDR USAA960770Stringer · corrodedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 4 INCH BY 2 INCH CORRODED STRINGER AT S28L BS 525. INSTALLED DOUBLER, REPAIRED PER EA 41784. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X)SDR USAA960769Angle · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION .50 INCH BY .24 INCH CHORD ANGLE, STA 767 TO STA 795, STR 25R. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-40-4 AND EA 41801. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)SDR USAASB96250Air Cycle Mach · failedORF - FLT 916 - AFTER TAKEOFF, CREW NOTED ACRID SMELL IN COCKPIT FOLLOWED BY BOTH SMOKE DETECTORS ACTIVATING. FLIGHT RETURNED TO ORF AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RT AIR CYCLE MACHINE. (X)SDR USAASB96247Wire · failedPHL - CABIN EMERGENCY LIGHTS ILLUMINATED AND WOULD ONLY EXTINGUISH WHEN TURNED OFF FROM THE COCKPIT. MAINTENANCE REPAIRED WIRING AT ROW 13 LEFT. (X)SDR F3LA96063Frame · corrodedPAE - FOUND CORROSION ON FORWARD SIDE OF FUSELAGE FRAME VERTICAL FLANGE, STATION 227.8 RBL 19, WL 168. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM. FLAP PEENED REWORKED AREA AND TREATED. FABRICATED STRAP, ALODINED AND PRIMED REPAIR PARTS AND INSTALLEDSDR F3LA96061Skin · dentedFOUND DENT ON AFT AIRSTAIR DOOR APPROXIMATELY 16 INCHES FROM TOP OF DOOR. REMOVED DAMAGE ON AFT ENTRY DOOR OUTER SKIN 1.75 INCH BY 1.75 INCH APPROX 16 INCHES FROM TOP OF DOOR AND 16 INCHES FROM FORWARD SIDE. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3, 52-10-1,SDR USAA960753Doubler · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SKIN DOUBLER BS 377.5 TO BS 379 LBL 3 WL 148.5. FABRICATED AND INSTALLED NEW DOUBLER, REPAIRED PER SRM 53-30-2 AND SRM 51-10-1. (M)SDR USAA960752Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK WL 148.5 LBL 4, BS 279 SKIN. INSTALLED EXT DOUBELR WT ADDED 9.4 LBS AT BS 279, REPAIRED PER TR 53-30-4. (M)SDR USAA960751Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK BS 708 STRINGER 18R, SHEAR BEAM WEB. INSTALLED REPAIR KIT, REPAIRED PER EO NR 5393G256 AND BOEING DRAWING NR 65C29228. (M)SDR USAA960750Chord · crackedINT - DURING Q-3 CHECK NDT INSPECTION, FOUND .25 INCH CRACK INBOARD AT FORWARD OUTBOARD HOE AT INTERSECTION OF STRINGER 18 A OUTBOARD STRAP AND BS 727 CHORD (RIGHT SIDE). INSTALLED REPAIR/MOD, REPAIRED PER EO 5394G068. (M)SDR USAA960749Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN SKIN STATION 1156, LBL 12. INSTALLED DOUBLER (REPLACED DOUBLER), REPAIRED PER SRM 53-30-3, FIG 6. (M)SDR USAA960748Skin · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 967 BETWEEN STRINGER 27L AND STRINGER 27R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. CORROSION TASK NR C53--202-01, CORROSION LEVEL 1. (M)SDR USAA960747Bulkhead · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA AT BULKHEAD BS 1023 RBL 1 INCH WL 195. INSTALLED EXT REPAIR, REPAIRED PER SRM 53-10-4/53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA960746Splice · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA STRINGER SPLICE BS 362 TO 363, STRINGER 27L. INSTALLED NEW SPLICE WITH 2 ADDITIONAL FASTENER ROWS, REPAIRED PER EA NR 41756. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA960745Chord · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK INDICATION INSIDE FORWARD UPPER FASTENER HOLE OUTSIDE CHORD BS 727, STRINGER 18 A STRAP. INSTALLED REPAIR MOD, REPAIRED PER EO 5394G068. (M)SDR USAA960744Frame · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION AT FRAME, BS 967. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 53-10-4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA960743Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA STRINGER 27R, BS 373 TO BS 378 (STRINGER). INSTALLED STRINGER REPAIR AND REPAIRED PER SRM 53-10-3, FIG 1. CORROSION LEVEL 1, CORROSION TASK NR C53-202-01. (M)SDR F3LA96060Skin · crackedPAE - FOUND CRACK IN SKIN AT THE TOP EDGE OF LOWER DOOR CUTOUT AT BS 977 WL 208. CRACK IS APPROXIMATE 1.5 INCH LONG, TRAVELING FROM EDGE INTO HOLE AND BEYOND. CRACK IS IN QUADRUPLER. REMOVED CRACKED QUADRUPLER, AND TRIPLER AT BS 947-1016 WL 218-190 AND FABRSDR USAASB96241Connector · looseJAX - FL 1420 - EN ROUTE FROM MCO-IAD - AT FL 290, THE NR 1 ENGINE OIL TEMPERATURE ROSE TO 140 DEGREES CELSIUS. CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. CAPTAINDID DECLARE AN EMERGENCY. TOTAL SINGLE ENGINESDR F3LA96059Floorbeam · corrodedPAE - FOUND CORROSION ON FLOORBEAM AROUND NUTCLIP HOLE AT BS 947, RBL 50, WL 208. BLENDED DAMAGED AREA PER SRM 51-10-02, DAMAGED AREA WAS FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR STRAP AND TREATED PER SRM 51-20-01. INSTALLED STRAP, ALL WORK ACCOMPLISHSDR F3LA96058Chord · crackedPAE - CRACK INDICATIONS NOTED (3), RIGHT CHORD BS 178, BETWEEN WL 195 AND WL 204. REMOVED 178 RT WEB FOR ACCESS. REMOVED CRACKED CHORD, FABRICATED NEW CHORD AND INSTALLED CHORD AND RT WEB IAW SRM 53-10-11, SRM 51-30-2, CUS NR 0000899 FUSE NR 00292. (M)SDR USAASB96230Static Line · disconnectedMYR - FL 8033 - ON T/O AT INT, BOTH THE CAPTAINS AND F/O ALTIMETERS FROZE AT 1,200 FT ANT TRIPPED TO STANDBY. TRIED BOTH STANDBY STATIC SOURCES WITH NO RECOVERY OF EITHER ALTIMETER. ALTIMETERS APPEARED TO OPERATE NORMALLY UPON PASSING THROUGH 1,200 FT. FLIGSDR F3LA96057Chord · puncturedPAE - FOUND PUNCTURE IN FAIL/SAFE CHORD BS 440 BETWEEN STRINGER 27 AND 28 RT. PUNCTURE IS BELIEVED TO HAVE BEEN CAUSED BY CORROSION. REMOVED AND REPLACED ENTIRE CHORD, REF SRM 51-30-2, SRM 53-10-2. WORK ACCOMPLISHED ON TRAMCO MWO NR FUSELAGE 214. (M)SDR F3LA96056Chord · crackedPAE - FOUND CRACK INDICATION NOTED AT BS 727 OUTBOARD CHORD AT LEFT STRINGER 18A UPPER AFT FASTENER HOLE. ACCESSED AREA, INSTALLED TEMPORARY REPAIR PER SB 73753A1166. REINSTALLED ALL ITEMS REMOVED FOR ACCESS. ALL WORK DOCUMENTED ON TRAMCO MWO NR FUSELAGE 26SDR F3LA96055Chord · crackedPAE - FOUND CRACK INDICATIONS NOTED IN BS 727 OUTBOARD CHORD AT RT STRINGER 18A BETWEEN FORWARD AD AFT FASTENERS, UPPER AND LOWER. ACCESSED AREA. INSTALLED TEMPORARY REPAIR PER SB 737-53A1166. REINSTALLED ALL ITEMS REMOVED FOR ACCESS. WORK DOCUMENTED ON TRSDR USAA960742Skin · crackedROA - DURING CX-1 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .1.25 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17 R BS 328) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-19 REV A. (M)SDR USAA960741Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION AT STRINGER 26 RIGHT BS 996 TO 1016. REMOVED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M)SDR USAA960740Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 68 INCH CORROSION AT STRINGER 27 LEFT BS 948 TO 1016. REMOVED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M)SDR USAASB96228Oil Gauge · failedBWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRESSURE GAUGE AND TRANSDR 96ZZZM1563Oil Transmitter · failedBWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRESSURE GAUGE AND TRANSDR USAASB96234Battery Pack · dischargedALB, MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTING ON SEATS 1-3 AB AND 4-6 ABC INOP. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT 5 ABC. OPS CHECK GOOD. (M)SDR F3LA96052Stringer · corrodedPAE - FOUND CORROSION ON FORWARD END OF STRINGER BS 260-266 STRINGER 22L. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER AND REPAIRED PER SRM 53-10-03. WORK ACCOMPLISHED ON TRAMCO MWO FUSELAGE 289. (M)SDR F3LA96053Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM AT NUTCLIP HOLE BS 986.5 RBL 18 UNDER SIDE OF UPPER CHORD. REPAIRED FLOOR BEAM AT BS 986.5, RLB 18, WL 208 IAW EWO NR 96-0742, SRM 53-10-0 AND SRM 51-20-01 CUST NR 0000844 INT NR 224. (M)
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