Boeing 737-48E
Service difficulty reports · 189
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 = '73748E' 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 = '73748E' 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 I5EA2023101400001Unknown · unknownCRACK ON FUSELAGE STA 727+6 STR 10R. REPAIRED FUSELAGE SKIN AT STA 727+6 STR 10R IAW BOEING MESSAGE SFW-SFW 23-0162-07B.SDR I5EA2023091600007Battery Pack · no testMODULE M1673 POWER SUPPLY BAD. REMOVED AND REPLACED M1673 POWER SUPPLY AT STA 973 IAW B737-400 AMM 33-51-51. TEST OK.SDR I5EA2023091600006Battery Pack · no testAFT ENTRY DOOR EXIT IDENTIFIER FOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1673 AT STA 973 WITH SERVICEABLE UNIT AND TEST IAW B737-400 AMM 33-51-51. TEST OK.SDR I5EA2023033000001Battery Pack · inoperativeFWD RIGHT EMERGENCY ESCAPE SLIDE LIGHT INOP - REMOVED AND REPLACED BATTERY PACK M1674 STA 324 WL 293 BL R7 IAW B737-400 AMM 33-51-51SDR I5EA2022111100005Battery Pack · inoperativeLEFT EMERGENCY EXIT LIGHT A/C LATCH INOP (LP 101907). REMOVED AND REPALCED BATTERY PACK LH MID IAW B737 AMM 33-51-51, OPAS CHECK GOODSDR I5EA2021081200010Battery Pack · dischargedCABIN BATTERT PACK LIGHT IS INOP CONNECTOR ( MO1672 ). REMOVED AND REPLACED THE BATTERY PACK EMERGENCY LIGHT CONNECTOR M01672. OPS CHECK TEST OK. IAW B737 AMM 33-51-51.SDR I5EA2020011402Light · inoperativeEMERGENCY LIGHT INOP AT M1695, STA565, WL213, RBL68SDR I5EA2019121707Gcu · malfunctioned#1 ENGINE GENERATOR WENT OFF LINE. APU ALREADY ON MEL. SYSTEM "B" HYD PRESS LOW LIGHT, YAW DAMP OFF, EQUIPMENT COOLING FAN OFF, ANTI-SKID INOP, MULTIPLE LOW PRESSURE LIGHTS.SDR I5EA2019012202Oxygen Gen · unwanted deployDISCREPANCY: 1/21/2019, LP 29887 - ROW 24DEF OXYGEN GENERATOR INADVERTENTLY DEPLOYED DURING MAINTENANCE INSPECTION. CORRECTIVE ACTION: 1/25/2019, LP 29888 - REMOVED AND REPLACED OXYGEN GENERATOR IAW AMM 35-22-11.SDR I5EA201812030001Fan · inoperativeDISCREPANCY: L/P 27388 - ITEM 1 - 30 MINUTES OUTSIDE OF MEM, THE LEAD FA INFORMED THE FLT DECK OF FUMES IN THE CABIN, DESCRIBED AS AN ELECTRICAL BURN SMELL, WITH THE FLIGHT DECK DOOR OPENED, IT COULD BE SMELLED ON THE FLIGHT DECK. RAN THE "SMOKE, FIRE, FUMES"SDR I5EA201811300004Unknown · odorDISCREPANCY: L/P 27385 - AT 34,000' THE CABIN CREW CALLED THE FLIGHT DECK TO INFORM THE PILOTS THEY SMELLED SMOKE IN THE CABIN. WHEN THEY OPENED THE FLIGHT DECK DOOR THE PILOTS COULD SMELL A STRONG ODOR OF SMOKE. THEY DONNED THEIR OXYGEN MASKS AND REQUESTEDSDR I5EA2018102209Indicator · malfunctionedDISCREPANCY: FLAPS EXTENDED TO 10 UNITS WITH FLAP HANDLE, GREATER THAN 1 UNITS, FLAP DISAGREEMENT CONDITION. CORRECTIVE ACTION: PERFORMED GENERAL VISUAL INSPECTION OF FLAP DRIVE SYS. AND ASSOCIATED COMPONENTS. NO FAULTS NOTED IAW AMM 27-58-41. REMOVED ANDSDR I5EA2018101004Slide · unwanted deployDISCREPANCY: R1 DOOR SLIDE DEPLOYED DURING REPACK. CORRECTIVE ACTION: REMOVED AND INSTALLED EMERGENCY DOOR SLIDE IAW AMM 25-61-35 AT R1 DOOR.SDR FOTR20180814007Bushing · corrodedRT STAB FORWARD LOWER SPAR JOINT LUG HAS CORROSION ON FWD. FACESDR FOTR20180814006Bushing · corrodedRH STAB. FWD. SPAR FITTING LOWER CLEVIS AFT FACE HAS CORROSION (AIRCRAFT SIDE)SDR FOTR20180814005Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING LOWER, FWD, CLEVIS, FWD FACE HAD CORROSION (AIRCRAFT SIDE)SDR FOTR20180814004Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING AFT, UPPER CLEVIS-AFT FACE HAS CORROSION (AIRCRAFT SIDE).SDR FOTR20180814003Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING UPPER FWD. CLEVIS FACE HAS CORROSION (AIRCRAFT SIDE)SDR FOTR20180814002Bushing · corrodedRH STABILIZER, FORWARD UPPER SPAR JOINT LUG HAS CORROSION ON FWD. FACE OF BUSHINGSDR FOTR20180814001Bushing · corrodedLEFT HORIZONTAL STABILIZER FWD ATTACH LUG, UPPER BUSHING, HAD CORROSION.SDR 2019F00051Bushing · corrodedLEFT STABILIZER, CENTER SECTION FRONT SPAR UPPER AFT CLEVIS, HAS CORROSION (AIRCRAFT SIDE)SDR 2019F00050Bushing · corrodedLEFT STAB. CENTER SECTION FRONT SPAR UPPER FWD CLEVIS HAS CORROSION (AIRCRAFT SIDE)SDR 2019F00049Bushing · corrodedLEFT HORIZONTAL STABILIZER, FWD. ATTACH LUG, LOWER BUSHING HAS CORROSION (STABILIZER SIDE)SDR 2019F00048Bushing · corrodedLH STAB. FORWARD SPAR FITTING, FWD FACE OF LOWER CLEVIS, HAS CORROSION (AIRCRAFT SIDE)SDR 2019F00047Bushing · corrodedLEFT LOWER AFT, FWD. STAB CLEVIS HAS CORROSION AROUND BUSHINGSDR 2019F00046Skin · cracked.5 INCH CRACK LOCATED THROUGH FASTENER UPPER LT WING SKIN AT WS 259, INBD. OF PYLON, 4 INCHES AWAY FROM TRIPLER.SDR FOTR2018080700334Skin · damagedRIGHT HORIZONTAL STAB, REMOVABLE L/E OTBD. END HAS ELONGATED HOLE.SDR 2018FA0000312Lug · corrodedRT STAB AFT UPPER SPAR JOINT LUG HAS CORROSION ON FWD FACE.SDR 2018FA0000311Clevis · corrodedRT STAB AFT SPAR FITTING AFT UPPER CLEVIS AFT FACE HAS CORROSION ( AIRCRAFT SIDE).SDR 2018FA0000310Clevis · corrodedRT STAB AFT SPAR FITTING FWD UPPER CLEVIS FWD FACE HAS CORROSION (AIRCRAFT SIDE).SDR 2018FA0000309Clevis · corrodedLT STAB REAR SPAR FWD FAIL SAFE CLEVIS HAS CORROSION.SDR 2018FA0000308Clevis · corrodedLT STABILIZER REAR SPAR AFT FAILSAFE CLEVIS HAS CORROSION (AFT SPAR) AT 7591.SDR 2018FA0000307Lug · corrodedLT HORIZONTAL STABILIZER AFT ATTACH LUG CENTER BUSHING AFT FACE HAS CORROSION (STABILIZER SIDE).SDR FOTR201806220001Floorbeam · corrodedMAIN CABIN BS 340, STRINGERS 17L - 17R, FLOORBEAM CORRODED, TOP SIDE.SDR FOTR201806190001Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM BS 947.5, THE ENTIRE LENGTHSDR FOTR201805310001Floor Support · crackedFLOOR SUPPORT, BS 344 - 360, LBL 26 HAD A 3/8 INCH CRACK IN THE LOWER FLANGE.SDR FOTR20180515004Floorbeam · corrodedCORROSION ON THE PASSENGER CABIN FLOORBEAM BS 986.5, ENTIRE LENGTHSDR FOTR20180515003Frame · crackedRIGHT BS 360 FRAME IS CRACKED AT THE INBD FASTENER HOLE OF THE AIR CONDITIONING ATTACH BRACKET FOR STRINGER 8R.SDR FOTR20180515002Threshold · corrodedR2 SERVICE DOOR BOTTOM INNER THRESHOLD CUTOUT ON FUSELAGE UPPER SURFACE FOUND CORRODED 30 SQUARE INCHES FROM BS 947 TO 1011.5.SDR FOTR20180515001Threshold · corrodedL2 DOOR THRESHOLD CUTOUT ON FUSELAGE, UPPER SURFACE CORRODED 15 SQUARE INCHES.SDR FOTR20180501001Web · corrodedMAIN CABIN BETWEEN BS 332 - 348, STRINGER 12R CORROSION ON WEB.SDR FOTR20180425004Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 967 UPPER FLANGE, UPPER SURFACE FOUND CORRODED 5 SQUARE INHCES, LBL 18, 30, 42, AND 48.SDR FOTR20180425003Door Frame · gougedAFT CARGO DOOR FWD FRAME HAS A .50 INCH GOUGE AT STRINGER 24 AND .50 INCH GOUGE 4 INCHES BELOW.SDR FOTR20180425002Floor Support · corrodedCORROSION ON THE AFT CARGO COMPARTMENT FLOOR SUPPORT, INBD SURFACE AND AROUND FASTENER HOLE.SDR FOTR20180425001Web · corrodedCORROSION ON THE AFT CARGO COMPARTMENT WEB BETWEEN BS 787 AND 794, RBL. 19.5.SDR FOTR20180421003Web · corrodedCORROSION IN THE AFT CARGO BAY WEB BETWEEN BS 795 AND 820, RBL 19.5.SDR FOTR20180421002Angle · corrodedAFT CARGO BAY FLOOR SUPPORT BS 787 TO 794, RBL 20 IN FILLER STRIP CORRODED 10 SQ. INCHES.SDR FOTR20180421001Floorbeam · corrodedCORROSION AROUND FASTENER HOLES ON THE AFT CARGO BAY FLOORBEAM, FWD ATTACH ANGLE BS 795 BETWEEN STRINGERS 25R AND 26R.SDR FOTR20180413001Attach Bracket · corrodedCABIN L-2 ENTRANCE DOOR INNER LWR CUTOUT AT STA 993.5 VERT ATTACH BRKT AT FLOOR LEVEL CORRODED 5 SQ IN.SDR FOTR20180411004Floor Support · crackedFLOOR SUPPORT AT BS 344 - 360, RBL 32 HAS 1/2 INCH CRACK.
Back to Boeing 737-48E