Boeing 737-247
Service difficulty reports · 1,009
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 = '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 DL73E960188Trans Relay · failedAT CRUISE 33,000 FT, ALT LOST ALL ELECT POWER AND CAPT INSTRUMENTS WERE COMPLETELY OUT FOR APPROX 20 MIN. RECOVERED F/O INSTR AND EVENTUALLY CAPT INSTRUMENTS RETURNED. REPLACED NR 1 TXFR RLY R-3 CPN 243201020. FOUND NR 2 ALT TXFR BUS C/B POPPED AND WOULD NOSDR DL73E960381Skin · crackedDURING INSPECTION, A 1 INCH CRACK WAS FOUND JUST LEFT OF BL 0 AT STA 379 IN THE SKIN AFT OF THE E/E AIR DUCT CUTOUT. THE CRACK IS TYPICAL OF THOSE COVERED BY BOEING S/B 737-53-1117, REV 1. DURING REMOVAL OF THE EXHAUST DUCT, THE INTERNAL SURROUND DOUBLER WASSDR DL73E960145Socket · brokenEMERGENCY FLOOR LIGHT AT ROW 2 IS INOP. REPLACED SOCKET, DL (P/N 337201959), (MFG 08169-1), OPS GOOD.SDR DL73E960159Dn Switch · failedWHEN LANDING GEAR WAS PLACED DOWN, ALL 3 GREEN AND ALL 3 RED LIGHTS ILLUMINATED. REPLACED GEAR HANDLE DOWN SWITCH (S-78), OPERATION NORMAL.SDR DL73E960156Floor Panel · corrodedDURING HMV, LT FIXED FLOOR PANEL AT FS 777 FOUND CORRODED BEYOND LIMITS. REPAIRED PER MM 53-21-04 PG 801.SDR VSTA9601011Chord · crackedCRACKED FAIL-SAFE CHORD FS 727 LEFT HAND SIDE. REPAIRED IAW BOEING SB 737-53-1088. REPLACED REPAIRED CHORD IAW EO 53-10-3 R1 11/13/95. COMPLETION TERMINATES INSPECTION PER WORK CARD 5364 FOR SIDE REPLACED. MAINTENANCE PERFORMED BY SOUTHWEST AERO TECH NR S5SDR 96ZZZX969Chord · crackedBS 727 CHORD CRACKED STR 29L - STR 21L. REPAIRED IAW VISCOUNT AIR SERV. E.O. 53-10-03. REF SB 737-53-1088.SDR DL73E960094Skin · crackedDURING OVERHAUL INSPECTION, MAINTENANCE FOUND A 2.5 CRACK UNDER AN EXISTING REPAIR DOUBLER AT APPROXIMATELY FS 1027, BETWEEN S-7L AND S-8L. THE CRACK PROPAGATED IN THE SKIN FROM THE LOWER FORWARD CORNER OF THE DOUBLER. IN ACCORDANCE WITH B737-200 SRM 53-30-3SDR VSTA9601012Tab · crackedINTERMITTENT AIRFRAME VIBRATION. LOOSE FASTENERS AT LT ELEVATOR INBOARD HINGE LUG. REPLACED LT ELEVATOR TAB.SDR VSTA9601001Retract Mech · malfunctionedDURING RETRACT OF MLG PER B737 MM 32-32-0 FOR COMPLIANCE WITH VASI EO NR 32-30-1 RT GEAR OPERATION AND FAIRING WAS SATISFACTORY. ON DOWN SELECTION THE UPPER FLYING DOOR RUBBED HARD ON THE LOWER DOOR JAMMING BOTH DOORS TOGETHER AND CAUSING DOOR RODS AND FITTISDR DL73E954784Socket · shortedDURING SVC CK, FOUND LAST SECTION OF CABIN EMERGENCY FLOOR TRACK ESCAPE LIGHTS INOP. PROBLEM CAUSED BY FARTHEST AFT LIGHT SOCKET WAS SHORTED AND FUSE BLOWN IN POWER SUPPLY. REPLACED SHORTED LIGHT SOCKET AND POWER SUPPLY.SDR DL73E954677Floor Panel · corrodedAT HMV INSPECTION, FOUND THE FORWARD B/B LT FIXED FLOOR PANEL CORRODED AT STA 500-520. CORRECTION: REMOVED FIXED FLOOR. REPLACED FIXED FLOOR. INSTALLED FIXED FLOOR PANEL.SDR DL73E954574Fairing · came looseLEFT INBD FLAP FAIRING CANOE BROKE LOOSE IN FLT AND WAS FOUND PARTLY DETACHED FROM WING DURING POST FLT. REMOVED LEFT WING MIDFLAP CANOE, REPLACED BELL CRANK ASSY, INBD AND OTBD STRUTS AND REINSTALLED FAIRING PER MM 27-51-21.SDR CAL951075Hyd Line · chafedFLT 1616 - MCO - THE NR 1 ENGINE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WITH THE HYDRAULIC QUANTITY GAUGE READING NEAR ZERO WHILE EN ROUTE FROM MIA TO GSO. THE AIRCRAFT WAS DIVERTED TO MCO AND WHILE ON SHORT FINAL THE 'B LOW QUANTITY' LIGHT CAME ONSDR DL73E954358Eel Power Supply · inoperativeR1 DOOR EMERGENCY SLIDE LIGHT IS OUT. REPLACED EMERGENCY LIGHT POWER SUPPLY.SDR DL73E954357Eel Power Supply · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT IS DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, CHECKS OK.SDR USVA109512Stringer · crackedMODERATE CORROSION AND CRACK AT STRINGER 26L, FS 500A. REPAIRED STRINGER PER SRM 53-10-3, FIG 1. (M)SDR DL73E954094Eel Wire · damagedFOUND EMERGENCY FLOOR TRACK LIGHT MISSING AT ROW 10, AND TRACK WIRING IN POOR CONDITION. REPLACED LIGHT AND REPAIRED WIRING AS NECESSARY, OPERATION NORMAL.SDR DL73E960114Bulb · failedON APPROACH TO ATL, LANDING GEAR EXTENDED, NOSE GEAR DID NOT HAVE GREEN LIGHT. CYCLED GEAR, NO CHANGE. ACCOMPLISHED MISSED APPROACH. REPLACED BOTH INDICATOR BULBS, LOWERED GEAR GOT GREEN LIGHT AND LANDED NORMALLY.SDR DL73E954054Valve · wornON DESCENT, NR 1 ENG OIL TEMP RUNNING AT 140 DEG FOR A STEADY 15 MIN, TEMP LEVELED AT 130 DEG. DID NOT SHUT ENG DOWN, FUEL HEAT RECYCLED OK AND DIVERTED DFW. FOUND FUEL HEAT VALVE LEAKING. REPLACED VALVE, RAN ENG LEAK AND OPERATION OK.SDR USVA10958Eel Track · splitAFT PIECE OF EMERGENCY PATH LIGHTING SYSTEM TRACK SPLIT. REPLACED AFT SECTION PER MM 33-20-00. (M)SDR USVA109513Eel Assy · inoperativeAFT EMERGENCY EXIT LIGHTS AFT OF CABIN CEILING INOP. REPLACED LIGHT ASSY PER MM 33-20-00. (M)SDR USVA109511Skin · crackedLEFT WING UPPER SURFACE LEADING EDGE SKIN AFT OF NR 1 SLAT GUIDE CUTOUT HAS A 1 INCH WING CRACK. REPLACED SKIN PER SRM 57-30-4. (M)SDR USVA109510Stringer · crackedSTRINGER 26R IS CRACKED ON FORWARD SIDE OF FS 500B. REPLACED STRINGER PER SRM 52-10-3, FIG 2. (M)SDR 96ZZZX214Floor Beam · corrodedMAINTENANCE REPORT OF CORROSION AT FLOOR BEAM STA 947.5 LT UPPER T-CHORD. CORROSION RUNS APPROXIMATELY 23 INCHES INBOARD OF THE FRAME. CORROSION FOUND DURING INSPECTION OF AREA FOR 24-MONTH CPCP CARD C53-107-02 (BOEING). REPAIR OF AREA TO BE ACCOMPLISHED IASDR USVA109519Floor Beam · corrosionHEAVY CORROSION ON FLOOR BEAM UPPER SURFACE FS 947 BETWEEN 2BL 0 TO RBL 60. REPAIRED PER DALFORT AVIATION XEA NR X2-53-161 REVISION 1. (M)SDR USVA109518Stringer · corrosionHEAVY CORROSION ON STRINGER 22L, FS 925. REPAIRED STRINGER PER SRM 53-10-3, FIG 1. (M)SDR USVA109517Beam · corrosionHEAVY CORROSION ON TRANSVERSE BEAM FS 887 RBL 60.750. REPAIRED PER DALFORT AVIATION XEA NR X2-53-163. (M)SDR USVA109516Spar · crackedRIGHT WING MID INBOARD FLAP REAR SPAR UPPER ANGLE CRACKED 1 INCH LONG AT STATION WLB 73. REPAIRED PER DALFORT AVIATION XEA NR X8-57-82. (M)SDR USVA109515Frame · crackedBELT FRAME AT FS 460 IS CRACKED BETWEEN STRINGERS 20L-21L. REPAIRED FRAME PER SRM 51-40-3. (M)SDR USVA109514Floor Beam · crackedFLOOR BEAM HAS HEAVY CORROSION AND CRACK FS 1016, BETWEEN RBL 5 T0 20. REPAIRED BEAM PER SRM 53-10-9. (M)SDR DL73E953899Aoa Sensor · brokenON LIFT-OFF, THE STICK SHAKER ACTIVATED AND DID NOT STOP UNTIL TOUCHDOWN. FOUND LEFT AOA SENSOR BROKEN OFF FROM A/C. REPLACED LEFT AOA, OPS CKS GOOD.SDR USVA10957Spoiler · crackedNR 2 SPOILER HAS A 2 INCH CRACK ON TOP OF TRAILING EDGE. REPAIRED SPOILER PER SRM 51-40-6. (M)SDR USVA10956Chord · crackedVERTICAL CHORD ANGLE HAS A 1.75 INCH LONG CRACK AT FS 178, LBL 7, WL 184. REPAIRED PER DALFORT AVIATION XEA NR X2-53-162. (M)SDR USVA10955Floor Beam · corrosionHEAVY CORROSION ON ENTIRE LENGTH OF UPPER SURFACE OF FLOOR BEAM FS 987. REPAIRED FRAME PER SRM 53-10-9, FIGURE 1. (M)SDR USVA10954Frame · crackedBELT FRAME UPPER SURFACE AT FS 500, STRINGER 26L HAS A .75 INCH CRACK. REPAIRED FRAME PER SRM 51-40-3. (M)SDR USVA10953Web · corrosionHEAVY CORROSION ON RIGHT CUSP LINE WEB FS 967-1006. REPLACED WEB ASSEMBLY PER SRM 51-40-2. (M)SDR USVA109520Spoiler · delaminationNR 6 SPOILER DELAMINATED ON TOP OUTBOARD END. REPAIRED SPOILER PER SRM 57-50-5. (M)SDR USVA10952Floor Beam · corrosionHEAVY CORROSION ON UPPER SURFACE OF FLOOR BEAM, FS 360, JUST AFT OF GALLEY. REPAIRED BEAM PER SRM 53-10-9, FIGURE 9. (M)SDR USVA10951Flap · crackLEFT INBOARD AFT FLAP LOWER SURFACE HAS A 2 INCH LONG CRACK. REPAIRED CRACK PER SRM 51-40-6. (M)SDR 96ZZZX3286Skin · corrodedTUS - MAINTENANCE REPORT OF CORROSION AT FORWARD LAVATORY SERVICE PANEL SKIN AND REINFORCING DOUBLER, STA 257 TO STA 277, BETWEEN STR 23R AND STR 24R. AFTER CORROSION REMOVAL, FOUND REMAINING SKIN TO BE WITHIN LIMITS, IAW 737 SRM 53-30-1. FABBED SKIN AND REISDR 96ZZZX3277Cowling · wornTUS - MAINTENANCE REPORT NR 2 ENGINE NOSE COWL WORN 50 PERCENT OF DEPTH IN .040 INCH, 2024T3 SKIN UNDER MATING SURFACE OF FORWARD WING TO NACELLE FAIRING. FABRICATED DOUBLER .040 INCH, 2024T3, 2 FASTENER ROWS WIDER THAN EXISTING DAMAGE AND REPAIRED PER SHIVA SDR 95ZZZX6271Skin · corrodedMAINTENANCE REPORT OF CORROSION AT FORWARD LAV SERVICE PANEL SKIN AND REINFORCING DOUBLER, STA 257 TO STA 277, BETWEEN STR 23R AND STR 24R. AFTER CORROSION REMOVAL, FOUND REMAINING SKIN TO BE WITHIN LIMITS IAW 737 SRM 53-30-1. FABBED SKIN AND REINFORCING DOUSDR 95ZZZX6270Fairing · wornMAINTENANCE REPORT, NR 2 ENGINE NOSE COWL WORN 50 PERCENT OF DEPTH IN .040 INCH 2024T3 SKIN UNDER MATING SURFACE OF FORWARD WING TO NACELLE FAIRING. FABRICATED DOUBLER .040 INCH 2024T3, 2 FASTENER ROWS WIDER THAN EXISTING DAMAGE AND REPAIRED PER SHIVA ENT., ISDR 96ZZZX3288C-1 Blade · damagedIFP - FLT 3225 - EN ROUTE IFP - NR 2 ENGINE ENCOUNTERED A BIRD STRIKE. UPON INSPECTION, FOUND BIRD STRIKE DAMAGED, 3 EACH N1 FAN BLADES. REPLACED NOTED BLADES. BORESCOPE LP COMPRESSOR. NO DAMAGE FOUND. ENGINE RUN AND ENGINE PARAMETERS NORMAL. AIRCRAFT RESDR CAL950777Flow Contl Vlv · inoperativeCLE - FLT 1244 - THE AIRCRAFT LOST PRESSURIZATION AT 31,000 FEET AND ALL OXYGEN MASKS DEPLOYED WHILE EN ROUTE FROM DAY TO EWR. 'ABNORMAL' PROCEDURES WERE FOLLOWED, BUT THE CABIN PRESSURE WAS UNCONTROLLABLE. THE AIRCRAFT WAS DIVERTED TO CLE AND WHILE ON APPROSDR 96ZZZX3296Oil System · leakingLAS - FLT 432 - UPON ARRIVAL LAS, POST-FLIGHT INSPECTION, MAINTENANCE FOUND OIL ACCUMULATION IN TAILPIPE AREA BELOW TURBINE EXHAUST CONE. INSPECTED CSD OIL COOLER, NO LEAKS FOUND. INSPECTED NR 4, NR 5, AND NR 6 PRESSURE TUBES, AND NR 6 BEARING COMPARTMENT FOSDR DL73E953561Eel · inopON PRE-FLIGHT, FOUND EMERGENCY TRACK LIGHTS INOP AT SEAT ROWS 10 TO 15, FOUND SHORTED WIRES IN TRACK. REPAIRED WIRES, OPERATION NORMAL. ALSO, HAD FWD GALLEY AND BOTH AFT GALLEY DOORS EMERGENCY LIGHTS INOP. REPLACED FWD GALLEY LIGHT ASSEMBLY AND LENS. FOUNDSDR USVA8954Evac Slide · low pressureL-1 DOOR SLIDE READS ZERO PRESSURE. REMOVED AND REPLACED DOOR SLIDE IAW BMM 25-61-311. (X)SDR USVA8958Strap · corrosionGENERATED BY CPCP C53-202-02. CORROSION BULGE AT SKIN LAP STRAP, FS 351, BETWEEN STR 28L-STR 28R. REPAIRED. (X)
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