Boeing 737-247
Service difficulty reports · 1,009
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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 = '737247' 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 = '737247' 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 DL73K010581Skin · crackedA 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 18 RT JUST AFT OF FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380422-14.SDR DL73K010539Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18 RT AT APPROXIMATELY FS 760. THE CRACK LOCATION WAS FWD OF AN EXISTING REPAIR FOR SIMILAR CRACKING. THE NEW CRACK WAS REMOVED WITH A 3 INCHES X 1.5 INCHES CUTOUT AND THE EXISTINGREPAIR REMSDR DL73K010512Skin · crackedA TYPICAL CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FWD GALLEY DOOR OPENING. THE CRACK WAS 1.4 INCHES LONG IN THE SKIN AND BONDED DOUBLER ONLY (BEAR STRAP NOT CRACKED). THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLERSDR P2EA01007Doubler · leakingSJO - REPAIR LEAKING ON FUSELAGE AT BS 727 TO BS 907 BETWEEN STRINGER 3R AND 5R. SENT TO BOEING ENGINEERING ON 3/26/01. IT WAS DETERMINED THAT NO MINOR REPAIR EXISTED. (M)SDR DL73E010457Stringer · crackedFUSELAGE STRINGER 18A SHEAR WEB CRACKED ON RH SIDE OF AIRCRAFT AT STA. 727. CRACK IS 1.0 INCH AND EXTENDS FORWARD FROM THE INBOARD/ AFT FASTENER LOCATION. CRACK IS TYPICAL OF S/B 737-53-1066.SDR DL73K010456Bulkhead · crackedDURING REPETITIVE INSPECTIONS, BS 178 BULKHEAD WEB FOUND WITH ADDTIONAL CRACKS. EXISTING REPAIR REMOVED, AND NEW REPAIR INSTALLED TO INCORPORATE EXISTING AND NEW DAMAGE LOCATIONS. EXISTING REPAIR DOCUMENT HAS BEEN SUPERCEDED BY ER/A 379924-14AD.SDR DL73K010417Skin · crackedFOUND ON O1 LETTER CK 1/4 MIN CRACK IN L-1 WINDOW CUTOUT AT UPPER OUTBD CORNER. REPAIRED PER SRM 53-30-3.SDR DL73E010420Frame · crackedTHE FS 178 BULKHEAD LT AND RT SIDE CHORDS WERE FOUND CRACKEDWHILE ACCOMPLISHING INSPECTIONS PER S/B 737-53A1173. THE CHORDS WERE REPLACED PER ERA 397346-14AD AT CV.SDR DL73K010381Battery Pack · dischargedPASSENGER SEAT 17C AND ALL SEAT EPATH LITES AFT OF IT ARE INOP. FOUND BATTERY PACK INOP. DAL P/N 337101963SDR DL73K010361Smoke Detector · malfunctionedLAV SMOKE LIGHT ILLUMINATED ON CLIMBOUT OF FLL. LAV SMOKE ALARM, POM PROCEDURE COMPLETED. DIVERTED TO MCO. LAV SMOKE LIGHT WENT OUT AFTER 13 MIN. CHECKED BOTH LAV TEMP PLATE INDICATORS. NO OVERHEAT INDICATED BOTH LAV EXT BOTTLES SEALED. FOUND 2 WIRES ON SDR DL73E010315Loop · intermittentAFTER T/O LEFT BODY OVERHEAT LIGHT ILLUMINATED AND REMAINED ON THEN FLICKERD AFTER POM. DROPPED ECS BAY LEADING EDGE FLAPS, SHOOK DOWN WIRES TO THERMOCOUPLES (FOUND NO INTERMITTENT LIGHT) REP COMPONENT OVERHEAT UNIT AND TESTED GOOD.SDR DL73K010272Skin · crackedA CRACK WAS FOUND IN THE SKIN AND UNDERLYING BEARSTRAP AT THE LOWER FWD CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1.25 INCH DEEP CUTOUT. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER ER/A 380029-14.SDR DL73K010244Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH TWO 1 INCH CRACKS AT RBL 5.7 AND WL 213. THE WEB HAD A PREVIOUS REPAIR DOUBLER FOR CRACKS AT RBL 5.7, WL 200 & BL 0, WL 190. THE EXISTING REPAIR WAS REMOVED AND A NEW ALUMINUM DOUBLER FABRICATED AND INSTALLED TO ENCOMPSDR DL73K010220Controller · failedDUE TO F/OS WINDSHIELD CRACKED IN FLT. REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK.SDR DL73K010215Window · crackedFIRST OFFICERS FRONT WINDOW CRACKED AT FL 310. REMOVED AND REPLACED F/OS R-1 WINDOW AND WINDOW HEAT CONTROLLER.SDR DL73K010198Bulkhead · crackedDURING ACCOMPLISHMENT OF THE FS 178 BULKHEAD INSPECTIONS PER AD 2000-05-29, CRACKS WERE FOUND IN THE ADJACENT FLOOR WEB AT WL 207 & LBL 25. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKED WEB WAS REMOVED AND A NEW WEB INSTALLED PER THE BAC S/BSDR DL73E010186Engine · fodON T/O ROLL, LOUD BANG W/ FULL PWR FELT VIBRATIONS. ABORTED T/O AT 10 KTS. PASSENGER REPORTED FLASH FROM AFT OF NR 1 ENG. PASSENGERS REPORTED BURNING SMELL IN CABIN AFTER BANG. FOUND NR 1 ENGINE INGESTED PLASTIC BAG. PERFORMED BORESCOPE OF NR 1 ENGINE PERSDR DL73K010181Skin · crackedFOUND AT N-1 LTR CK, CAPTS WINDSHIELD POST OUTER SKIN CRACKED AT UPPER FWD CORNER. REPAIRED PER SRM 53-30-3.SDR DL73K010106Battery · inoperativeEN ROUTE TO TPA 1L EMERGENCY FLASHLIGHT BATTERY FAILED. REPLACED SAME.SDR DL73E010082Frame · crackedDURING INSPECTIONS OF THE FS 178 BLKHD CRACKS WERE FOUND IN THE LT AND RT SIDE CHORDS AND IN THE BULKHEAD WEB AT RBL 10 WL 233.5. THE CHORDS WERE REPLACED AND THE WEB REPAIRED PER ERA 396656-14AD AT MV.SDR DL73E010081Skin · wornTHE INNER SURFACE OF THE LOWER WING SKIN WAS FOUND WORN AT THE BOOST PUMP ACCESS HOLE AT WBL 148. THE DAMAGE CLEAN UP WAS APPROXIMATELY 1.5 X 1.5 X .061 INCH. THE DAMAGE WAS REPAIRED PER ERA 396660-14 AT MV.SDR P2EA01001Adc · malfunctionedMCI - FLT 301 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT, STANDBY PRESSURIZATION COULD NOT MAINTAIN PRESSURIZATION SCHEDULE. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW MM 21-30-0, OPERATIONAL CHECK NORMAL. (M)SDR DL73E002480Tire · failedNR 1 MAIN TIRE BLEW ON TAKEOFF AT 150 KNOTS. LANDING WEIGHTWAS 105.5K. RATE OF DESCENT AT LANDING WAS 100FT/MIN. C/A R/R NBR 1 MAIN TIRE PER MM. PERFORMED OVER WEIGHT LNDG INSP PER MM 05-51-51. N.T.F.SDR P2EA00454Indicator · malfunctionedMCI - FLT 360 - ON LANDING, DURING L/E SLAT EXTENSION, NR 2 SLAT SHOWED NO INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. REPAIRED BROKEN WIRE PER MM CHAPTER 20. SYSTEM CHECKED NORMAL PER 27-88-0. (M)SDR P2EA00453Indicator · malfunctionedMSY - FLT 355 - ON LANDING, DURING L/E SLAT EXTENSION, (AT FLAPS 5) NR 2 SLAT SHOWED NO INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. DISCREPANCY COULD NOT BE DUPLICATE ON THE GROUND. (M)SDR DL73K002310Gasper Fan · failedELECTRICAL BURNING SMELL ASSOCIATED WITH POPPED C/B FOR GASPER FAN_C/A REPLACED GASPER AIR FAN PER M/M.SDR DL73E002263Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND CRACKED AT WL 195 AND LBL AND RBL 5.7. THE DAMAGE WAS REPAIRED AT MV PER ERA 396422-14AD SIMILIAR TO THAT OF S/B 737-53A1173.SDR DL73E002262Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND CRACKED AT WL 207 AND LBL AND RBL 25. ERA 396437-14AD REPAIRS THE AREA PER S/B 737-53A1173 AT MV.SDR DL73E002261Frame · crackedTHE LT OUTER CHORD ON THE FS 178 BULKHEAD WAS FOUND CRACKED AND WAS REPLACED PER ERA 396424-14AD AT MV.SDR DL73K002217Fitting · corrodedTHE LT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE MAIN LUG BORE. THE BORE WAS OVERSIZED TO REMOVE ALL CORROSION AND AN OVERSIZE REPAIR BUSHING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 379223-14.SDR DL73K002216Fitting · corrodedTHE RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE MAIN LUG BORE. THE BORE WAS OVERSIZED TO REMOVE ALL CORROSION AND AN OVERSIZE REPAIR BUSHING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 379224-14.SDR DL73E002186Floorbeam · corrodedFLOORBEAM CORRODED FS 344, RBL 14 TO LBL 48. REMOVED CORROSION PER SRM 51-10-6 AREA OUT OF LIMITS PER SRM 53-10-1. BEGAN REMOVING T-CAP. DRILLED UP REPLACMENT T-CAP PER M/M 53-21-0 FIG 803. OK TO INSTALL. STARTED INSTALLATION OF T-CAP PER M/M 53-21-0 FIG SDR DL73K002185Skin · crackedA CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE L2 DOOR OPENING. THE CRACK WAS REMOVED WITH A .75 INCH CUTOUT. THE DAMAGED AREA WAS REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 36 AND ER/A 379182-14, REV A.SDR DL73K002183Skin · crackedTHE UPPER HINGE CUTOUT OF THE L2 DOOR OPENING WAS FOUND CRACKED IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT TO REMOVE THE DAMAGE. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 21A AND ER/A 379178-14, REV A.SDR DL73E002177Floorbeam · corrodedFLOORBEAM CORRODED, FS 312, LBL 14 TO RBL 24. REMOVED CORROSION SRM 51-10-6. AREA OUT OF LIMITS PER SRM 53-10-1. BEGAN REMOVING FASTENERS. CHEMICAL TREATED PER 900-4-06. DRILLED REPLACEMENT CAP PER M/M 53-21-0 FIG 803. OK TO INSTALL. REPAIRED PER M/M 53SDR DL73K002156Fan · wornAT GATE READY FOR PUSHBACK, AN ELECTRICAL ODOR WAS SMELLED IN COCKPIT AND CABIN, NO SMOKE. FOUND GASPER FAN BADLY WORN. REPLACED SAME, OP CK NORMAL.SDR DL73E002145Terminal · burnedELECTRICAL ODOR STILL NOTICED NEAR F/O''S FRONT WINDOW AREA BETWEEN R-1 WINDOW AND EYEBROW WINDOW. ODOR DISAPPEARS WHEN R FWD WINDOW HEAT SWITCH TURNED OFF. FOUND BOTTOM RIGHT CONNECTOR LOOSE ON R1 WINDOW. REPLACED SAME AND RETORQUED. REPLACED P-59 WINDOW SDR P2EA00331Stiffener · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENE AT BS 540, LBL 25, WL 204 WITH CRACK 2 INCHES BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11.07-00. REPAIRED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 25, WL 204 IAW BOSDR P2EA00334Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 14 WL 178 WITH CRACK. L = 1.50 INCHES. W = 0.002 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPLACED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, LBL 14, WSDR P2EA00329Door Frame · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR FRAME LOWER FORWARD CORNER WITH CRACK .75 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11-07-00. REPAIRED THE FORWARD CARGO DOOR FRAME LOWER FORWARD CORNER WITH CRACK IAW BOEING SB 737-52-1090 REV 1 DATED SDR P2EA00333Door Frame · crackedSJO - DURING Q-CHECK, FO UND THE L-1 DOOR JAMB AFT LOWER CORNER SKIN WITH CRACK 2.5 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11-07-2000. REPAIRED THE L-1 DOOR JAMB AFT LOWER CORNER SKIN IAW BOEING SB 737-53-1083 SECT III PART IV REV 3 DATED DECEMBER 7,SDR P2EA00328Skin · corrodedSJO - DURING Q-CHECK, FOUND THE EXTERIOR FUSELAGE SKIN AT BS 306 - BS 311 STR 24R WITH CORROSION. L = 5.00 INCHES. W = 2.500 INCHES. D = 0.065 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE EXTERIOR FUSELAGE SKIN AT BS 306 - BS 311 STR 24R IAW BOSDR P2EA00330Stiffener · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, RBL 25 WL 204 WITH CRACK 1.5 INCH BY .002 INCH. IDENTIFIED AS REPORTABLE ON 11-07-2000. REPAIRED THE FORWARD CARGO BULKHEAD VERTICAL STIFFENER AT BS 540, RBL 25 WL 204 IAW BSDR P2EA00332Skin · damagedSJO - DURING Q-CHECK, FOUND THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN WITH WEAR 10 INCHES BY 1 INCH. IDENTIFIED AS REPORTABLE ON 11-07-00. REPAIRED THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN IAW BOEING FAX COO-SSDR P2EA00337Lap Joint · crackedSJO - DURING Q-CHECK, FOUND THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INDICATION AT BS 948 STR 25R. L = 1.00 INCH. W = 0.001 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INDSDR P2EA00336Lap Joint · crackedSJO - DURING Q-CHECK, FOUND THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INDICATION AT BS 500B STR 19R. L = 1.00 INCH. W = 0.001 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE LOWER EXTERIOR FUSELAGE LAP JOINT UPPER ROW WITH CRACK INSDR COOSDR000001Skin · crackedEXTERIOR FUSELAGE SECTION 41, RT FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATION, STA 227.8, BS 211.8, WL 215, WL 217, WL 221.5, AND WL 222. POSSIBLE CAUSE OF THE CRACK WAS SKIN FATIGUE. (X)SDR P2EA00335Skin · dentedSJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLIPPER FLAP, TRAILING EDGE WITH DENT. L = 9.875 INCHES. W = 7.625 INCHES. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE RIGHT WING OUTBOARD FLIPPER FLAP, TRAILING EDGE IAW COOPESA EOS COO-CMP-3-37-62SDR P2EA00327Skin · crackedSJO - DURING Q-CHECK, FOUND THE EXTERIOR FUSELAGE SKIN AT BS 227.8 WL 225 WITH CRACK. L = 1.200 INCH. W = 0.001 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE EXTERIOR FUSELAGE SKIN AT BS 227.8 WL 225 IAW BOEING FAX COO-SJO-00-1180H DATED OCT 17, SDR P2EA00326Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE LOWER NOSE COMPARTMENT VERTICAL CHORD AT BS 178 LBL 5.7 WL 184 WITH CRACK. L = 1.50 INCHES. W = 0.003 INCH. IDENTIFIED AS REPORTABLE ON 11-7-00. REPAIRED THE LOWER NOSE COMPARTMENT VERTICAL CHORD AT BS 178 LBL 5.7 WL 184 IAW
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