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 USAASB96239Battery Pack · dischargedROA - MAINTENANCE FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE RIGHT OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (M)SDR F3LA96054Frame · corrodedPAE - WHILE WORKING FLOOR WEB AT BS 987, FOUND CORROSION AND MECHANICAL DAMAGE ON FRAME AT BS 993, RBL 49, WL 210-206. BLENDED OUT CORROSION ON FRAME. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA OF FRAME. MECHANICAL DAMAGE WAS LOCATED ON WEB AREA OF FRAME. CSDR USAASB96233Light · inoperativeROA - MAINTENANCE FOUND THE AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND INSTALLED NEW BATTERIES (P/N S106). OPS CHECK GOOD. (M)SDR USAASB96242Beam · fracturedCLT - FL 693 - CAPTAIN REPORTED THE RIGHT MAIN LANDING GEAR UPLOCK DOES NOT ENGAGE. WITH GEAR LEVER UP, RIGHT MAIN GEAR RED LIGHT IS ILLUMINATED. MOVE GEAR LEVER TO OFF, THE RIGHT MAIN GEAR COMES DOWN. FLIGHT LANDED AT CLT. MAINTENANCE FOUND THE RIGHT MAINSDR USAASB96226Windshield · crackedPIT - FL 820 - ON CLIMB-OUT, CAPTAINS FORWARD WINDSHIELD ARCED AND THEN CRACKED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. (M)SDR USAASB96225Connector · looseRSW - FL 1429 - ON APPROACH TO RSW, CREW RECEIVED THE FIRE WARNING FOR THE NR 2 ENGINE. CREW SHUT DOWN ENGINE AND FIRED BOTH BOTTLES. FLIGHT LANDED AT RSW WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF FIRE. THE D1096 CSDR USAA960734Skin · crackedROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17L, BS 950) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED REPAIR, REPAIRED PER SRM 53-30-3, FIG 24. (M)SDR USAA960721Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOND 2 INCH BY 12 INCH CORRODED AREA BS 947 TO 967 STRINGER 25R. REMOVED CORRODED STRINGER RADIUS FILLER AND SPLICED IN NEWE RADIUS FILLER (ACTUAL STRINGER NOT AFFECTED BY CORROSION) LESS THAN ONE POUND ADDED. CORROSSDR USAA960720Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 100 INCH CORROSION BS 328 LBBL 50 INCH THROUGH RBBL 50 INCH FLOOR BEAM T-CAP. FABRICATED NEW T-CAP AND SPLICE, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960719Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1. 5INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 202. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960718Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN RBBL 5 INCH WL 199. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960717Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.5 INCH CRACK 178 BULKHEAD SKIN RBBL 5 INCH WL 202. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960716Angle · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FORWARD CARGO DOOR AT LOWER AFT CORNER STOP FITTING, SKIN TO WEB ATTACH ANGLE. FABRICATED AND INSTALLED REPAIR ANGLES, REPAIRED PER SRM 51-40-4. (M)SDR USAA960715Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 199. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960693Skin · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3 FIG 6. CORROSION TASK NR C53-100-01, CORROSION LEVEL 2. (M)SDR USAASB96217Engine · failedBDL - FLT 268 - AT FL 285, CAPTAIN HEARD A LOUD BANG. THE NR 1 ENGINE THEN SHOWED INDICATIONS OF LOW POWER. AS A PRECAUTION, THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO BDL. CAPT DID DECLARE AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENTSDR USAA960688Skin · crackedROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 1.375 INCH CRACK AFT GALLEY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17 R BS 857) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 24, EA 58949. (M)SDR USAA960687Skin · crackedROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17R BS 328) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 26. (M)SDR F3LA96051Stringer · corrodedPAE - FOUND CORROSION AROUND FASTENERS IN STRINGER 27R, BS 947-967 WL 173. REMOVED DAMAGED SECTION OF STRINGER 27R, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-3. (M)SDR USAASB96212Tr Unit · failedITH - FLT 2075 - CLIMBING THROUGH 12,000 FT, THE CABIN PRESS WARNING HORN SOUNDED. DESCENDED TO 10,000 FT AND WENT TO STANDBY. CHECKED FOR C/B'S POPPED AND FOUND THE E/E COOLING FAN C/B POPPED. SWITCHED TO ALTERNATE FAN AT WHICH TIME FLT ATTENDANTS REPORTEDSDR USAA960689Skin · crackedINT - DURING B-CHECK, EDDY CURRENT INSPECTION, FOUND .120 INCH CRACK LOWER FORWARD CORNER OF FORWARD SERVICE DOOR LOWER CUT OUT IN RADIUS SKIN. INSTALLED DOUBLER AND REWORKED PER EA AND SRM. REPAIRED PER EA 41649, SRM 53-30-3 FIG 32. (M)SDR USAA960680Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 2 INCH BY 2 INCH STATION 947.5 STRINGER 27L. REPLACED STRINGER FROM STATION 940 TO 1016, REPAIRED PER SRM 53-10-3. CORROSION TASK NR 53-202-01, CORROSION LEVEL 1. (M)SDR USAA960679Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.24 INCH CRACK EXT SKIN LBL 3 BS 380. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)SDR USAA960678Frame · crackDURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FRAME STATION 767 AT STRINGER 21 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M)SDR USAA960677Web · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROX 1 INCH LONG EACH IN VERTICAL WEB STATION 706 LBL 24. INSTALLED DOUBLER AND ANGLES, REPAIRED PER SRM 51-40-2. (M)SDR USAA960676Web · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACKS APPROXIMATELY 1 INCH LONG IN VERTICAL WEB STATION 706 RBL 24. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960675Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.875 INCH CRACK IN SKIN BS 727B AT STRINGER 17R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. REPAIRED PER SRM 53-30-3. (M)SDR USAA960674Former · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 500 A STRINGER 26 R FORMER. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 51-40-3, CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)SDR USAA960673Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS .25 INCH AND .375 INCH FORWARD SERVICE DOOR AFT FRAME 1 AT NR 3 STOP, 1 AT NR 4 STOP. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)SDR USAA960672Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 754 ABOVE STRINGER 18R FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6 AND EA 58706. (M)SDR USAA960671Keel Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 SCREW HOLES CORRODED .25 INCH AROUND OPENINGS, BS 720-725 RIGHT FLANGE UPPER SIDE KEEL BEAM. INSTALLED DOUBLER AFTER SPOT FACING, REPAIRED PER EA NR 41637. CORROSION TASK NR C53-212-01, CORROSION LEVEL 1. (MSDR F3LA96050Bulkhead Web · crackedPAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS REPLACED IAW BOEING SRM AND BOEING DRAWING NR 65-16300. REPLACEMENT ACCOMPLISHED ON TRAMCO MWO FUSELAGE 212. (M)SDR F3LA96049Bulkhead Web · crackedPAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES BELOW PRESSURE DECK IAW EWO 96-0606. LEAK CHECKED ALL ITEMS. REMOVED FOR ACCESS, NO LEAKS FOUND.SDR F3LA96048Chord · crackedPAE - FOUND CRACK INDICATIONS IN LT BS 727, STRINGER 18A OUTBOARD CHORD FORWARD AND AFT OF BOTH FASTENER HOLES. ACCESSED REPAIR AREA. FOUND CRACKS CONTAINED IN FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PARTS FOR INTERIM REPAIR PER SB 737-53A1166. RE-SDR F3LA96046Floorbeam · crackedPAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS BS 520 WL 207.75, RBL 25 AND RBL 46. REPAIRED FLOORBEAM CRACK AT BS 520, WL 207.75, RBL 25 AND RBL 46 IAW EWO 396-0643. (M)SDR F3LA96045Floorbeam · crackedPAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS AT BS 520, WL 207.75, LBL 25 - LBL 47. REPAIRED CRACKS IN FLOORBEAM AT BS 520, WL 207.75, LBL 25, LBL 45 AND LBL 47 PER EWO NR 96-0643. (M)SDR F3LA96044Chord · crackedPAE - HFEC INSPECTION OF THE BS 178 LT SIDE CHORD AT WL 194-196 SHOWS A CRACK INDICATION. CUT OUT DAMAGED AREA OF CHORD. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER TRAMCO EWO NR 96-0619. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 276. (M)SDR F3LA96043Chord · crackedDURING SERVICE CHECK, INSPECTION REPORTD A .5 INCH CRACK IN OUTER CHORD AT STATION 727, STRINGER 25R. REPAIRED PER BOEING TELEX FRO-DEN-96-0090RR AND SRM 51-40-4, FIG 1. (M)SDR F3LA96040Keelbeam · crackedPAE - FOUND CRACK IN THE AFT END OF RT KEELBEAM BS 814-818, STRINGER 27 RT. REPAIRED CRACK IAW TRAMCO EWO 96-0613. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 255. (M)SDR F3LA96047Stiffener · crackedPAE - FOUND CRACK EMANATING FROM FASTENER HOLE AT BS 540, WL 203.5, LBL 26 ON VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER AND INSTALLED PER SRM 57-10-02, SRM 51-30-02. WORK DOCUMENTED ON TRAMCO MWO INTERIOR 174. (M)SDR F3LA96042Chord · crackedHFEC INSPECTION EXHIBITS CRACK APPROX 1.5 INCH LONG IN RADIUS OF BS 540 CHORD BETWEEN STRINGER 21R AND STRINGER 22R, CRACK IS ON SPLICE PLATE. ACCESSED AREA, REMOVED DAMAGED SPLICE PLATE. FABRICATED NEW SPLICE PLATE PER TRAMCO EO NR 96-0629. INSTALLED NEW SSDR F3LA96041Door Frame · crackedPAE - HFEC INSPECTION OF THE FORWARD CARGO DOOR FRAME, REVEALED A CRACK INDICATION AT STRINGER 23R ON THE FORWARD SIDE OF THE FRAME AT THE LOWEST OUTBOARD CORNER OF THE DOOR STOP FITTING. ACCESSED INDICATED AREA AND FOUND NUMEROUS GOUGES LOCATED BENEATH DOOR SDR F3LA96038Frame · corrodedPAE - FOUND CORROSION (C53-208-01) ON AFT SIDE OF FRAME BS 520 RBL 7, WL 150. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FRAME PER SRM 51-40-3. (M)SDR USAA960670Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKIN STRINGER 17L, BL 950. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M)SDR USAA960669Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.24 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN STRINGER 17 R, BS 328. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 26. (M)SDR F3LA96039Frame · crackedPAE - FOUND CRACK IN FRAME WEB AT UPPER CORNER OF STRINGER CUTOUT BS 294.5, STRINGER 18R. FOUND CRACK CONTAINED IN FASTENER HOLE. REPAIRED PER SRM 51-40-02 AND TRAMCO ER100396MW3. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 233. (M)SDR F3LA96037Shear Tie · corrodedPAE - FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-10-4, FIG 8. DURING REPAIR, FOUND DAMAGE TO BONDED DOUBLER BENEATH SHEAR TIE. CUT OUT DAMAGED DOUBLESDR F3LA96036Floorbeam · corrodedPAE - FOUND CORROSION ON UNDERSIDE OF CARGO FLOORBEAM BS 500, RBL 18, WL 156. REMOVED CORROSION ON UNDERSIDE OF FLOORBEAM AND REPAIRED IAW SRM 53-10-1, 51-40-3 REF WORK ORDER FUSELAGE 262. (M)SDR F3LA96035Stringer · crackedPAE - FOUND CRACK IN STRINGER 10 LEFT, BS 296, WL 256. REMOVED DAMAGED SECTION OF STRINGER 10L BS 296, WL 256. REPAIRED STRINGER IAW SRM 53-10-3 FIGURE 3 RED WORK ORDER INTERIOR 154. (M)SDR F3LA96034Intercostal · crackedPAE - FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS ARE CRACKED ON THE AFT OTBOARD FLANGE. REMOVED AND REPLACED FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS IAW SRM 51-10-1, 51-10-2, 51-30-2, REF WORK ORDER D
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