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 TSAA0626063Control Panel · failedNON-ETOPS FLT 72 LIH-HNL: AFTER ENGINE START, ( OVHT/DET) ANNUNCIATOR LIGHT ILLUMINATED WITH NO CORRELATED SYSTEM OVERHEAT INDICATION DURING RECALL CHECK. CREW ELECTED TO SHUTDOWN ENGINES AND RETURN TO BLOCK. AS THE ENGINES WERE SPOOLING DOWN, (SMOKE) ANNUNCIASDR TSAA0626064Warning Light · false indicationNON-ETOPS FLT 34 HNL-ITO: AFTER ENGINE START, OVHT/DET ANNUNCIATOR LIGHT ILLUMINATED WITH NO CORRELATED SYSTEM OVERHEAT INDICATION DURING RECALL CHECK. CREW WAS UNABLE TO RESET LIGHT AND ELECTED TO SHUTDOWN ENGINES AND RETURN TO BLOCK. AS THE ENGINES WERE SPOOSDR TSAA0621058Fan · odorNON-ETOPS FLT 269 KOA-HNL: SHORTLY AFTER LANDING, THE CREW AND FLIGHT MECHANIC NOTICED A BURNING SMELL COMING FROM THE GASPERS. THE CREW SWITCHED OFF THE GASPER FAN AND THE BURNING SMELL DISSIPATED SHORTLY AFTER. THE CREW CONTINUED TAXIING TO THE GATE WITHOUT SDR PIDA06047Panel · corrodedDURING B-CHECK, INSPECTION NOTED FORWARD LAVATORY SERVICE PANEL CORRODED ON INBOARD SIDE. REMOVED MINOR SURFACE CORROSION FROM LAVATORY PAN PER SRM 51-10-6 AND REPLACED INTERNAL DOUBLER 65-55757-2 PER DWG 65-45802.SDR PIDA06046Autopilot Sys · malfunctionedLEFT AUTO PILOT TURNED HEADING FROM 050 TO 080. AUTO PILOT ROLLED INTO A 30 DEGREE RIGHT TURN (AS IT SHOULD) THEN PITCHED DOWN 5 DEGREES FOR NO REASON. DISCONNECTED AUTO PILOT. PLACED AUTO PILOT -A- CHANNEL ON MEL 22-1. PERFORMED AUTO-PILOT BITE CHECK PER SDR PIDA06044Computer · malfunctionedWHEN AUTO PILOT -B- SYSTEM IS ENGAGED, PITCH MODE FLUCTUATES. REPLACED FCC -B- COMPUTER. OPS NORMAL PER MM 22-11-331.SDR PIDA06041Control Unit · malfunctionedTAKEOFF ABORTED DUE TO NR 1 GENERATOR TRIPPED OFF LINE. CHECKED NR 1 CSD OIL LEVEL, DP INDICATOR, FOUND NORMAL. CHECKED APU OIL QUANTITY. DISCONNECTED NR 1 CSD AND PLACED NR 1 GENERATOR ON MEL 24-1. REPLACED NR 1 ENGINE GENERATOR CONTROL UNIT PER MM 24-20 SDR PIDA06034Flap · lack of lubeDURING RETURN TO FIELD FOR STAB TRIM PROBLEM, AT 225 KIAS AT 6000 FT MSL WHEN FLAPS EXTENDED TO 5, FELT SHUDDER IN RUDDER PEDALS WHICH CONTINUED TO LANDING. MADE OVERWEIGHT LANDING AT 112000 LBS. INSPECTED AIRCRAFT PER MM 5-51 FOR OVERWEIGHT LANDING, NO DAMASDR PIDA06033Relay · failedAFTER TAKEOFF, STABILIZER TRIM BECAME INOPERATIVE. STAB TRIM LIGHT ILLUMINATED BUT TRIM WOULD NOT MOVE. RETURNED TO FIELD; INSPECTED AIRCRAFT. FERRIED AIRCRAFT FOR MAINTENANCE. 03/17/2006: FOUND HIGH RESISTANCE BETWEEN C1 AND C2 OF R64 STAB TRIM CONTROL RSDR PIDA06028Power Supply · inoperativeFORWARD AND AFT SECTIONS OF SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED FWD AND AFT POWER SUPPLIES PER MM 33-50.SDR PIDA06029Control Unit · out of adjustAUTO THROTTLE ADVANCES THRUST LEVERS UNCOMMANDED. ADJUSTED RIGHT ENGINE LVDT PER MM 22-31-81.SDR PIDA06026Connector · corrodedRIGHT WING EGRESS LIGHTS OUT. CLEANED SLIGHT CORROSION FROM BULB CONNECTOR. OPS CHECKS GOOD.SDR PIDA06006Control Unit · malfunctionedYAW DAMPER WILL NOT ENGAGE. PLACED ON MEL 22-3-B. 01/16/2006: REPLACED YAW DAMPER CONTROL UNIT. SYSTEM TESTS OK PER MM 22-12-01.SDR PIDA20050202Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT ROW 2. REPLACED BATTERY PACK. OPS CHECKS GOOD PER MM 25-60-10.SDR PIDA2005O187Actuator · intermittentMACH TRIM INTERMITTENT. PLACED ON MEL 22-5. 11/07/2005: REPLACED MACH TRIM ACTUATOR PER MM 22-21-11. OPS CHECKS GOOD.SDR PIDA2005O186Switch · malfunctionedAUTO PILOT A & B DISENGAGES AT FLAP 1 POSITION. REPLACED FLAP UP SWITCH 25EN55-6 PER MM 27-51-291. SYSTEM OPS CHECKS GOOD.SDR PIDA20050183Control Panel · malfunctionedMODE CONTROL PANEL INOP. REPLACED MODE CONTROL PANEL PER MM 22-11-01.SDR PIDA20050185Computer · malfunctionedAUTO PILOT "A" CHANNEL DISENGAGES. REPLACED "A" SYSTEM FCC. OPERATION NORMAL PER MM 22-11-00.SDR PIDA20050184Recorder · malfunctionedAERO INSTRUMENTS & AVIONICS READOUT OF THE FDR INDICATE THAT THE LEADING EDGE SLAT DISCRETES NEVER CHANGE STATE DURING FLIGHT. ACCOMPLISHED EMTEQ ENGINEERING MOD PAA1-001M-1 DATED 9-6-05.SDR PIDA20050179Yaw Damper · malfunctionedYAW DAMPER TRIPS OFF ON GROUND ONLY WHEN WIDE TURNS ARE MADE WITH TILLER OR RUDDER. PLACED ON MEL 22-3-1B.SDR PIDA20050173Yaw Damper · failedYAW DAMPER WILL NOT ENGAGE. PLACED YAW DAMPER ON MEL 22-3-18.SDR PIDA20050172Transformer · failedAUTO THROTTLES WON'T ENGAGE. LOSS OF VALID AIR DATA SPEED SIGNAL PREVENTED AUTO THROTTLE ENGAGEMENT. REPLACED T98 TRANSFORMER IN J4 BOX PER WDM SPM CHAPTER 20 DUE TO SHORT. AUTO THROTTLES OPS CHECK GOOD PER MM 22-31-01.SDR PIDA20050171Battery Pack · inoperativeRIGHT SIDE EMERGENCY LIGHT FOR OVERWING EXIT NOT ILLUMINATING. REPLACED RIGHT SIDE OVERWING EXIT LIGHT BATTERY PACK. LIGHT OPS CHECKS GOOD.SDR PIDA20050164Battery Pack · inoperativeEMERGENCY EXIT LIGHTS AT REAR EXIT DOORS AND AT FORWARD EXIT DOORS ARE NOT ILLUMINATING. REPLACED BATTERY PACK FOR REAR DOOR LIGHTS AND FORWARD DOOR LIGHTS AND OPS CHECKED PER MM 33-51-71.SDR PIDA200500016Compass · malfunctionedAFTER TAKEOFF, BOTH COMPASS HEADINGS ROLLED AWAY FROM RUNWAY HEADING. RETURNED TO FIELD. PERFORMED SYSTEM CHECKOUT PER MM 34-21-00. SYSTEM CHECKED NORMAL. PERFORMED VISUAL INSPECTION OF BOTH DIRECTIONAL GYROS, NO PROBLEMS NOTED.SDR 249TR0105Indicator · malfunctionedRIGHT ENGINE N1 GAUGE WENT TO 80 PERCENT AND STOPPED. ABORTED TAKEOFF PRIOR TO 60 KNOTS. MINIMUM BREAKING APPLIED. REPLACED N1 TACH AND OPS CHECKED PER MM 77-12-0 AND 31-00-11.SDR 250TR0060Wire · damagedIN PREPARATION TO TAXI, LEFT ENGINE UNCOMMANDED SHUT DOWN AFTER START. FOUND BROKEN WIRES W368-011 AND 010 UNDER CLAMP SIX INCHES BEFORE FUEL SHUTOFF VALVE CONNECTOR 0788. PRECAUTIONARY, CHECKED RIGHT ENGINE AND DISCOVERED WIRES DAMAGED IN SAME LOCATION. RESDR 249TR0103Gasper Fan · burned outGASPER FAN CREATES A SMELL OF SMOKE IN FORWARD SECTION OF CABIN. REPLACED GASPER FAN AND OPS CHECKED GOOD PER MM 21-24-21. NOTE: NO FURTHER WRITE UPS AS OF 01/17/2005. TEAR DOWN REPORT INDICATED IMPELLER DIFFICULT TO ROTATE BY HAND. INSPECTION REVEALED BESDR 249TR0104Circuit Breaker · trippedAUTO PILOT WILL NOT FOLLOW COMMANDED INPUTS FROM PILOT AND FLIGHT DIRECTOR. RESET STABILIZER TRIM CIRCUIT BREAKER. SYSTEM TESTS GOOD PER MM 22-11-01.SDR 249TR0102Switch · inoperativeRIGHT TO/GA SWITCH IS INOP. REPLACED SWITCH S787B IN RIGHT THROTTLE PER MM 34-22-0 AND MM 22-31-01.SDR 249TR0088Intercostal · corrodedINTERCOSTAL AT RBL 8, BETWEEN BS 947.5 AND BS 927 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-0 AND 53-10-2.SDR 249TR0101Computer · faultyAUTO THROTTLE FAILS STEP A; SHOWS AF6 FAULT CODE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101.SDR 249TR0100Actuator · leakingEVIDENCE OF FLUID LEAK FROM -A- SYSTEM AUTO PILOT ELEVATOR SERVO ACTUATOR. FOUND -B- SYSTEM AUTO PILOT ACTUATOR LEAKING DOWN ONTO -A- SYSTEM ACTUATOR. REPLACED -B- SYSTEM ACTUATOR PER MM 22-11-261.SDR 249TR0099Stringer · misrepairedSTRINGER REPAIRS NOT PER THE SRM AT STR 15LT. REPAIRED PER SRM 53-10-3.SDR 249TR0098Support Angle · crackedLEFT INBOARD SUPPORT ANGLE CRACKED UNDER FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-341.SDR 249TR0097Galley Track · corrodedRIGHT OUTBOARD GALLEY TRACK CORRODED FOR G-2 GALLEY. REPLACED SECTION OF TRACK PER BOEING DRAWING 65-45834 AND SRM 53-10-2 AND 51-10-2.SDR 249TR0096Intercostal · corrodedEDGE OF INTERCOSTAL BETWEEN BS 328 AND BS 340 AT LBL 12 DAMAGED. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR 249TR0095Intercostal · corrodedCORROSION ON TWO INTERCOSTALS AT BS 320 RBL 12 AND RBL 56. REPLACED INTERCOSTALS PER SRM 51-10-1.SDR 249TR0094Intercostal · corrodedCORROSION ON INTERCOSTAL BETWEEN BS 312 AND BS 328 AT RBL 12. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR 249TR0093Intercostal · corrodedCORROSION ON INTERCOSTAL AT LAV DOOR FROM BS 294 TO BS 312. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-2.SDR 249TR0092Attach Angle · corrodedCORROSION ON ATTACH ANGLE FOR AFT WALL OF FORWARD LAV. REPLACED HAT CHANNEL PER SRM 51-10-1.SDR 249TR0091Seat Track · corrodedSEAT TRACK AT RBL 38 HAS CORROSION AT BS 986 + 4. REPLACED SECTION OF TRACK PER SRM 51-10-1 AND 53-10-2.SDR 249TR0090Intercostal · corrodedINTERCOSTAL AT BS 947+14 FROM RBL 8 TO RBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR 249TR0089Intercostal · corrodedINTERCOSTAL FROM BS 947 TO BS 967 AT RBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592 AND SRM 51-40-0.SDR 249TR0087Intercostal · corrodedINTERCOSTAL AT BS 947+14 FROM RBL 17 TO RBL 44 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR 249TR0086Intercostal · corrodedINTERCOSTAL FROM BS 967 TO BS 986 AT LBL 18 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0.SDR 249TR0085Intercostal · corrodedINTERCOSTAL FROM BS 947 TO BS 967 AT LBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR 249TR0084Intercostal · corrodedINTERCOSTAL AT BS 947+9 FROM LBL 17 TO LBL 41 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592.SDR 249TR0083Intercostal · corrodedDIAGONAL INTERCOSTAL FROM BS 986 TO BS 1006 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0.SDR 249TR0082Intercostal · corrodedDIAGONAL INTERCOSTAL FROM BS 1006 TO BS 1016 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1.
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