Boeing 737-282
Service difficulty reports · 303
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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 = '737282' 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 = '737282' 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 BJNA040806Power Supply · inoperativeAFT EMERGENCY ESCAPE SLIDE LIGHTS INOPERATIVE. REMOVED AND REPLACD THE AFT EMERGENCY LIGHT BATTERIES IAW AMM 31-51-71. (M)SDR BJNA040807Door Frame · crackedDURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER FORWARD CORNER FRAME CRACKED. INSTALLED NEW LOWER FORWARD CORNER AT C1 DOOR IAW SRM 51-20-1 AND SERVICE BULLETIN 737-52A1100 REV 4. (M) BJNASDR BJNA040808Door Frame · crackedDURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER AFT CORNER FRAME CRACKED. INSTALLED NEW LOWER AFT CORNER AT C1 DOOR IAW SRM 51-20-1 AND SB 737-52A1100 REV 4. (M) BJNASDR BJNA040804Floor Support · corrodedDURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-19222 IAW THE BOEING 737 STRUCTRUAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M)BJNASDR BJNA040805Floor Support · corrodedDURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 LBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW THE SRM 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M)SDR BJNA040803Intercostal · corrodedDURING C-CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 306 LBL 12. REMOVED AND REPLACED FLOORBEAM INTERCOSTAL AT BS 306 LBL 12 IAW THE STRUCTURAL REPAIR MANUAL 53-30-2. (M)SDR BJNA040901Crossbeam · crackedDURING C-CHECK INSPECTION FOUND C-1 DOOR LOWER CROSS BEAM HAS WEB CRACK NEAR AFT CORNER. FABRICATED FILLER, .875 INCH BY 5 INCH AND 5 INCH BY 4 INCH MATERIAL USED 2024T3.050. INSTALLED REPAIR IAW SB 737-52A1100, REV 4 AND SRM 51-30-2 AND 51-10-2. (M)SDR BJNA040902Skin · crackedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BOTTOM OF L1 DOOR CUT OUT BS 336. INSTALLED DOUBLER AND STRAP AT L1 DOOR LOWER CUTOUT IAW SB 737-53-1083 REV 3. (M)SDR BJNA040802Skin · crackedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT LOWER AFT CORNER OF R1 DOOR CUTOUT AT BS 344. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIG 26. (M)SDR BJNA040801Skin · crackedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT L1 DOOR LOWER HINGE CUTOUT AT BS 304. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 31. (M)SDR BJNA040704Battery · inoperativeDURNG A MAINTENANCE WALK AROUND CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY P/N 6104789 FOR THE LEFT OVERWING EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE LSDR BJNA040702Battery · inoperativeDURING A MAINTENANCE WALK AROUND CHECK, THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE IAW BOEING MM 33-51-31. THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATED NORMALLY. (M)SDR BJNA040701Battery Pack · inoperativeDURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD CABIN DOOR R1 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FWD R1 CABIN DOOR IAW BOEING MM 33-51-81. THE FWD R1 CABIN DOOR EMERGENCY EXIT LIGHT NOW OPSDR BJNA040703Battery · inoperativeDURING A MAINTENANCE WALK AROUND CHECK, THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE FOR THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE AFT CABIN OVERHEAD EMSDR BJNA040601ABattery · dischargedDURING A MAINTENANCE WALK AROUND CHECK, THE RT SIDE OVER-WING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT HAND OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OSDR BJNA040601Power Supply · dischargedMAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY.SDR BJNA040503Light · burned outDURING A MAINTENANCE WALK AROUND CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP OF THE AFT SECTION OF EMERGENCY FLOOR TRACK IAW EEL COMPONENT MAINTENANCE MANUAL 33-50-01. SYSTEM NOW CSDR BJNA040502Actuator · leakingAFTER TAKEOFF, FLT CREW NOTICED HYD SYSTEM-A QUANTITY LOSS. A/C RETURNED TO MFE & MADE UNEVENTFUL OVERWEIGHT LANDING. B AND STANDBY HYD SYS NOT AFFECTED. MX DISCOVERED FLUID LEAKING FROM SHAFT SEALS ON NR 4 SPOILER ACTUATOR. SPOILER ACTUATORS ARE UNDER A-SSDR BJNA040501Battery Pack · dischargedDURING A MAINTENANCE WALK AROUND CHECK, AN AISLE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE PER BOEING MM 33-51-81, SYSTEM NOW CHECKS NORMAL. (M)SDR BJNA040202Wire · looseFORWARD FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED THE EMERGENCY LIGHT POWER SUPPLY FOUND WIRE PULLED FROM THE CONNECTOR, REPLACED THE POWER SUPPLY, OPS CHECK OK. (M)SDR BJNA040203Power Supply · inoperativeDURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND THE EMERGENCY BATTERY PACK IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMAL.SDR BJNA040102Connector · inoperativeDURING A MAINTENANCE WALKAROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE FORWARD BATTERY CHARGER AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKED NORMAL. WORK IAW MANUFACTURESSDR BJNA040101Battery Pack · will not testRIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERY PACK PER AMM 33-51-31. (M)SDR BJNA031201Engine · failedON TAKEOFF AT 80 KNOTS, NR 1 ENGINE FAILED. THE TOWER REPORTED THE ENGINE WAS ON FIRE, NO FIRE WARNING INDICATION. DISCHARGED THE FIRE BOTTLE. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. FAILURSDR BJNA031102Switch · inoperativeDURING A PREFLIGHT CHECK, EXTERIOR EMERGENCY EXIT LIGHTS DID NTO ILLUMINATE. MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT SWITCH WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT SWITCH IAW BOEING MM 33-51-01. EXTERIOR EMERGENCY SDR BJNA031101Battery Pack · inoperativeDURING A SCHEDULED MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT DOOR R-2, AND L2 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE R-2, AND L2 EMERGENCY BATTERY PACK IAW BOEING MM 33-51-01, LIGHTS NOW ILLUMINATE. (M)SDR TSAA0353219Skin · corrodedFOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB 228, NR 5 AT WBL 254, NR 6 AT WBL 264, NR 7 AT WBL 268, NR 8 AT WBL 234, NR 9 AT WBL 236, NR 10 AT SDR TSAA0353218Skin · corrodedFOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT WBL 92.5, NR 2, 3, 4, 5 AND 6 BETWEEN WBL 198.6 AND WBL 227.0, NR 7 AND 8 AT WBL 157, NR 9 AND 10 BESDR TSAA0253267Skin · crackedCLEANED OUTER SKIN AT EACH MOUNTING HOLE. OVER-DRILLED ELONGATED HOLES TO RESTORE HOLES TO CIRCULAR SHAPE. TRIMMED OUT CRACK DAMAGED HOLE LARGE ENOUGH TO REMOVE CRACK TO RECTANGULAR SHAPE. HFEC VERIFIED HOLES CRACK FREE. FABRICATED CIRCULAR AND RECTANGULARSDR TSAA0253249Floorbeam · crackedREMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COLD WORKED THE HOLES IN THE CHORD. INSTALLED SPLICE ANGLE AND STIFFENERS WITH FASTENERS SHOWN IN SESDR TSAA0253268Lap Joint · damagedTRIMMED BONDED DOUBLER ABOVE EXISTING FASTENER PATTERN LEAVING ED FOR FINAL FASTENER INSTALL. OPENED DISCREPANT COUNTERSINK HOLE TO .75 INCH DIAMETER. VERIFIED CRACK FREE USING HFEC. HOLE OPENED UP TO 1 INCH INSURANCE CUT. FABBED .032/.036 INCH THICK CIRCULSDR TSAA0255264Skin · gougedCUT AND REMOVED GOUGE AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0255266Skin · gougedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0255265Skin · dentedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR BJNA030801Bearing · failedAT FL 310, NR 1 ENGINE OIL PRESSURE NOTICED DROPPING, OIL QUANTITY WENT TO HALF GALLON, AND OIL TEMPERATURE ROSE TO THE YELLOW BAND. ENGINE WAS SHUTDOWN, LOW OIL PRESSURE LIGHT CAME ON AND THE ENGINE WIND-MILLED ABOUT 23 MINUTES AT 5-8 PSI OIL PRESSURE. DISASDR BJNA030701Tire · separatedON TAKEOFF ROLL HEARD LOUD BANG JUST BEFORE ROTATION. INSPECTION FOUND NR 2 NOSE TIRE HAD THROWN TREAD. (M)SDR BJNA030700Light · inoperativeDURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT LOCATED BY THE LEFT AFT ENTRY DOOR EXTERIOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BULB IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMALLY. (M)SDR BJNA030601Odor · detectedBURNING ODOR IN COCKPIT AND CABIN ON TAKEOFF. INSPECTED AIRCRAFT, RAN ENGINES, CHECKED AIR CONDITIONING PACKS AND VENTILATION SYSTEM. UNABLE TO DUPLICATE, NO FAULTS FOUND. (M)SDR BJNA030501Gearbox · leakingNR 2 ENGINE DEVELOPED OIL LEAK IN FLIGHT, ENGINE SHUT DOWN, AIRCRAFT LANDED WITHOUT INCIDENT. FOND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED, OIL LEAKING AROUND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH'S OIL LINE. INSTALLED A HELICAL COIL IAW PSDR BJNA03042Light · inoperativeDURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT OVER THE R-2 DOOR WOULD NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, SYSTEM CHECKS NORMALLY. (M)SDR BJNA03041Light · disconnectedEMERGENCY FLOOR PROXIMITY LIGHTING (FROM PASSENGER ROWS 14 THROUGH 17) NOT LIGHTING DURING OPERATIONAL CHECK. MAINTENANCE DISCOVERED THAT THE LIGHTING STRIP FOR THIS SECTION HAD BECOME DISCONNECTED FROM ITS POWER SOCKET. LIGHT STRIP WAS REATTACHED AND OPERATSDR BJNA030302Light · brokenEMERGENCY FLOOR LIGHTING STRIP BROKEN AT SEAT 15D. INSTALLED LIGHT STRIP AS REQUIRED, OPS CHECK GOOD, IAW AMM 33-51-07. (M)SDR BJNA03031Web · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT OVERHEAD WEB LOCATED AT FS 994 LBL 50. REMOVED THE L2 DOOR THRESHOLD DRAIN PAN FOR ACCESS TO CORRODED SECTION OF WEB, CORROSION ALSO EXTENDED TO THE INBOARD CHORD. REMOVED THE CSDR BJNA030220Skin · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE LT WING OUTBOARD BOOST PUMP CUTOUT AREA. BLENDED OUT THE CORROSION, HOWEVER THE REMAINING MATERIAL THICKNESS WAS BELOW MINIMUM REQUIRED, AND THE CUT OUT OF MATERIAL WAS BEYOND SRM LSDR BJNA303217Frame · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON A FRAME MEMBER LOCATED AT BS787 BETWEEN STRINGERS 22 AND 24 LEFT.SDR BJNA030218Stringer · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON STRINGER 26 RIGHT, LOCATED AT BS 980. REMOVED THE CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND STRINGER SPLICE IAW WITH SRM.SDR BJNA030219Skin · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED ON NR 2 ENGINE INBOARD COWLING. CORROSION WAS LOCATED UNDERNEATH THE FIRE SEAL AREA THROUGHOUT THE FORWARD AND AFT SECTION. REMOVED FIRE SEAL FOR ACCESS TO THE CORRODED SECTION OF SKIN. REMOVESDR BJNA030216Fitting · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND IN THE BORES OF THE HORIZONTAL STABILIZER CENTER SECTION FORWARD TERMINAL FITTINGS UPPER AND LOWER AFT LUGS. THE BORES WERE REAMED TO THE MAXIMUM DIAMETER (1.125 INCH) SHOWN IAW SB. AFTER REAMING INSPECTION SSDR BJNA030214Floor Support · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT CARGO BAY AT FS 772 LBL 5. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED NEW REPAIR SECTION IAW BOEING 737 SRM 53-10-5 FIGURSDR BJNA030213Splice · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A STRINGER SPLICE LOCATED ON STRINGER 22 LEFT AT STATION 727-727A. REMOVED THE CORRODED STRINGER SPLICE, FABRICATE AND INSTALLED REPLACEMENT PARTS IAW BOEING SRM 51-20-1 FIGURE 7, PATE
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