Boeing 737-2K5
Service difficulty reports · 261
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 = '7372K5' 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 = '7372K5' 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 250TR0057Skin · crackedCRACK AT FORWARD END OF OXYGEN SERVICE PANEL CUTOUT. REPAIRED PER EA 53-288 AND SRM 53-30-3.SDR 250TR0056Stringer · corrodedCORROSION ON STR 27 RT JUST FORWARD OF BS 360. REPAIRED IAW EA NR 53-291 AND SRM 53-10-3.SDR 250TR0055Skin · corrodedCORROSION ON INSIDE OF FUSELAGE SKIN BETWEEN STR 24 RT AND STR 25 RT AT BS 1016+4. REPAIRED PER EA 53-294.SDR 250TR0054Web · crackedWEB FROM BS 490 TO BS 500 AT STR 26 RT IS CRACKED. REPLACED WEB IAW MFG DWG. 65-20726 AND SRM 51-30-2.SDR 250TR00531Attach Angle · crackedINTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-37261 AND SRM 51-30-2.SDR 250TR0052Intercostal · crackedINTERCOSTAL WEB FROM BS 500A TO BS 500B AT STR 26 LT IN FORWARD CARGO BIN IS CRACKED. REPLACED WEB AND ATTACH ANGLE PER BOEING DWG 69-41473 AND DWG 69-51411 AND SRM 51-30-0.SDR 250TR0051Attach Angle · crackedATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 480 AND STR26RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-16784 AND SRM 51-30-0.SDR 250TR0050Attach Angle · crackedATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 460 AND STR 26 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-16784 AND SRM 51-30-02.SDR 250TR0049Stringer · corrodedCORROSION AROUND NUT PLATE IN STR 28 LT AT BS 500 IN FORWARD CARGO BIN. REPAIRED PER SRM 53-10-3.SDR 250TR0047Attach Angle · crackedATTACH ANGLE AT BS 663 BELOW WALL TO FLOOR TRANSITION ANGLE CRACKED, RIGHT SIDE. REPLACED ATTACH ANGLE PER SRM 51-10-2 AND SRM 53-10-2.SDR 250TR0045Beam · damagedAFT LUG ON THE RIGHT MAIN GEAR BEAM ARM HAS AN INDICATION OF A DEFECT. REPLACED WALKING BEAM ARM PER 737 MM 32-11-00.SDR 250TR0044Angle · crackedDRAG ANGLE CRACKED UNDER LEFT FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-290.SDR 250TR0043Frame · corrodedCORROSION UNDER NUT PLATE ON FRAME AT BS 1006 AT RBL 5. REPLACED FRAME SECTION PER SRM 51-10-1 AND SRM 51-30-0.SDR 250TR0042Stringer · corrodedCORROSION OF STR 25 LT FROM BS 986 TO BS 1006. REPAIRED PER SRM 53-10-2.SDR 250TR0041Stringer · corrodedCORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1.SDR 250TR0040Support Channel · corrodedDRAIN MAST UPPER SUPPORT CHANNEL FROM BS 986 TO BS 1006 AT STR 25 LT HAS CORROSION. REPLACED SUPPORT CHANNEL IAW SRM 53-10-2.SDR 250TR0039Clip · corrodedFRAME TO SKIN ATTACH CLIP HAS CORROSION AT BS 967 BETWEEN STR 26 LT AND STR 25 LT. REPLACES ATTACH CLIP PER SRM 51-10-1.SDR 250TR0038Stringer Clip · corrodedAFT SIDE OF TIE CLIP AT BS 1006 AND STR 27 LT HAS CORROSION. REPLACED TIE CLIP PER SRM 51-10-1.SDR 250TR0037Support · crackedSUPPORT FOR RADAR TR RACK CRACKED. REPAIRED IAW SRM 51-40-3.SDR 250TR0036Skin · bulgedSKIN BULGING AROUND RIVETS AT SERVICE INTERPHONE JACK AT STR 23 LT AND BS 1040 AT THE AFT PRESSURE BULKHEAD DOOR. REPAIRED PER EA 53-287.SDR 249TR0037Switch · malfunctionedAUTO THROTTLES WOULD NOT ARM. PLACED AUTO THROTTLE ON MEL 22-4. REPLACED LEFT AUTO THROTTLE DISENGAGE SWITCH AND CHECKED NORMAL PER MM 22-31-0.SDR 249TR0036Light · inoperativeR-1 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R-1 EMERGENCY EXIT LIGHT. OPS CHECKS OK.SDR 249TR0035Computer · inoperativeAUTO THROTTLES BECAME INOP WHILE EN ROUTE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101 AND OPS CHECKED PER 22-31-01.SDR 249TR0034Force Limiter · malfunctionedAUTO PILOT -B- WILL NOT ENGAGE IN FLIGHT. REPLACED AILERON FORCE LIMITER AND OPS CHECKED PER MM 22-11-132.SDR 249TR0033Control Unit · inoperativeAUTO THROTTLE INOPERATIVE. REPLACED PDC CDU IAW MM 34-18-21 AND OPS CHECKED IAW MM 34-18-21 AND 22-31-01.SDR 249TR0032Computer · malfunctionedAUTO THROTTLES WILL ONLY ARM EVERY OTHER FLIGHT AND WHEN DISENGAGED TO DO TREND, AUTO THROTTLES WILL NOT RE-ARM. REPLACED AUTO THROTTLE COMPUTER AND OPS CHECKED PER MM 22-31-01.SDR 249TR0031ALight · inoperativeLEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD.SDR 249TR0031Transmitter · out of adjustAUTO THROTTLE SHUTS OFF ON TAKEOFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81.SDR 250TR0035Wire · damagedL-2 LOW LEVEL LIGHT DOOR IDENTIFIER INOP. REPAIRED WIRING AT LIGHT ASSY. OPS CHECKS NORMAL.SDR 250TR0034Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ON RIGHT EXTERIOR BELOW HATCH AND AFT OF WING INOP. REPLACED BATTERY PACK AND OPS CHECKED OK PER MM 33-51-81.SDR 249TR0030Wire · damagedBOTH TOGA SWITCHES INOP AND A-SYSTEM AUTO PILOT INOP. PLACED BOTH SYSTEMS ON MEL. REPAIRED GROUND WIRE ON T215. PERFORMED LAND VERIFY TEST AND OPERATIONAL TEST SATISFACTORY PER MM 22-11-01. CLEARED MEL.SDR 250TR0033Battery Pack · inoperativeAFT DOORS EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY BATTERY CHARGER FOR L2 AND R2 EXTERIOR EMERGENCY LIGHTS. OPS CHECKS GOOD PER MM 33-51-8P.SDR 249TR0029Computer · malfunctionedAUTO THROTTLES WILL NOT ENGAGE ON GROUND BEFORE TAKEOFF. PDC MUST BE RELOADED. RE-SEATED PDC AND AUTO THROTTLE COMPUTERS. PERFORMED BITE TEST. OPS NORMAL PER MM 22-31-01.SDR 249TR0028Battery Pack · inoperativeEMERGENCY EXIT LIGHT OVER L2 DOOR INOP. REPLACED BATTERY PACK PER MM 33-51-51. OPS NORMAL.SDR 249TR0027Computer · inoperativeAUTO THROTTLE COMPUTER INOPERATIVE. PLACED ON MEL 22-4. 04/27/2004: REPLACED AUTO THROTTLE COMPUTER AND OPS. CHECKED PER MM 22-31-01. CHECKS GOOD. CLEARED MEL.SDR 249TR0026Indicator · inoperativeNO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PERFORMED. ADI OPERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUBLE-SHOOTING PURPOSES AND SELF TEST PERFORMED SATISFACTORISDR 2419TR0026Indicator · malfunctionedNO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PREFORMED. ADI OPSERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUPBLE-SHOOTING PURPOSES AND SELF TEST PERFORMED SATISFACTOSDR 250TR0032Battery · inoperativeFWD CABIN AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED BATTERY. SYSTEM CHECKS NORMAL.SDR 250TR0031Battery Pack · inoperativeFORWARD CABIN CENTER AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED OK.SDR 250TR0029Lamp · inoperativeLOW LEVEL EMERGENCY LIGHTS INOP AT ROWS 5DEF, 11DEF, 20DEF. RELAMPED AND OPS CHECKS NORMAL.SDR 250TR0030Power Supply · inoperativeEMERGENCY PATH LIGHTING INOP. REPLACED POWER SUPPLY. OPS CHECKS NORMAL.SDR 250TR0028Skin · crackedCRACK IN THE FUSELAGE SKIN AT THE LEFT AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED DAMAGE PER SRM 53-30-3 FIG. 24.SDR 249TR0024Bottle · lowDURING A-CHECK FOUND L-1 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR SLIDE WITH SERVICEABLE UNIT PER MM 25-61-311.SDR 249TR0023Battery · inoperativeR1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. OPS CHECKS NORMAL PER MM 33-51-51.SDR 249TR0025Flap Track · damagedULTRASONIC INSPECTION OF LEFT I/B TRACK OF O/B FLAP SHOWS DEFECT IN UPPER PORTION OF AFT ATTACH BORE. REPLACED I/B TRACK OF O/B FLAP.SDR 249TR0021Battery · failedHEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED IAW MM 22-11-01. REPLACED BATTERY IAW MM 24-31-11. TEST OK.SDR 249TR0002AAComputer · malfunctionedHEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED PER MM 22-11-01. REPLACED BATTERY PER MM 24-31-11. TEST OK.SDR 250TR0027Battery Pack · inoperativeRIGHT HAND OVERWING & FLAP EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK M193 AND REFLECTOR. OPS CHECKS GOOD PER MM 33-51-1.SDR 250TRBattery Pack · inoperativeRIGHT HAND OVERWING & FLAP EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK M193 AND REFLECTOR. OPS CHECKS GOOD PER MM 33-51-1.SDR 250TR0026Computer · malfunctionedCAPTAIN'S FLIGHT DIRECTOR FLAG IN VIEW. REPLACED NR 1 FLIGHT CONTROL COMPUTER PER MM 22-11-331. OPS CHECKS GOOD.
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