Boeing 737-2K5

Service difficulty reports · 261

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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.

SDR 249TR0020Coupler · failedYAW DAMPER SWITCH WILL NOT LOCK ON. TRIPS BREAKER. PLACED ON MEL 22-3-1. 11/20/2003: REPLACED YAW DAMPER COUPLER. OPS NORMAL PER MM 22-12-01. CLEARED MEL 22-3-1.Nov 13, 2003 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0025Skin · delaminatedNR 1 LEADING EDGE SLAT FOUND DELAMINATED. REPLACED NR 1 LEADING EDGE SLAT ASSY PER MM 27-81-21.Oct 1, 2003 · N250TR · Boeing 7372K5 · Leading Edge DevicesSDR 249TR0019Battery · dischargedFORWARD EMERGENCY LIGHT BATTERY WILL NOT HOLD A CHARGE. REPLACED EMERGENCY LIGHT BATTERY IAW MM 25-60. OPS. CHECKS OK.Sep 12, 2003 · N249TR · Boeing 7372K5 · Emergency LightingSDR 250TR0024Switch · damagedAUTO THROTTLE WILL NOT ENGAGE. REPLACED BOTH AUTO THROTTLE DISCONNECT SWITCHES. OPS CHECKS OK PER MM 22-31-01.Sep 10, 2003 · N250TR · Boeing 7372K5 · Auto Throttle SystemSDR 250TR0023Computer · inoperativeFIRST OFFICER'S FLIGHT DIRECTOR FLAG IN VIEW DURING FLIGHT. REPLACED NR 1 AND NR 2 FLIGHT CONTROL COMPUTER IAW MM 22-11-331.Sep 10, 2003 · N250TR · Boeing 7372K5 · Autopilot ComputerSDR 250TR0022Gyro · malfunctionedB CHANNEL AUTO PILOT JERKS EXCESSIVELY IN RIGHT AND LEFT TURNS. PLACED B CHANNEL AUTO PILOT ON MEL 22-1. 8/15/2003: REPLACED NR 1 AND 3 VERTICAL GYROS PER MM34-22-1. AUTO PILOT BITE TEST NORMAL PER MM22-11-01.Aug 3, 2003 · N250TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0021Indicator · faultyADI ATTITUDE FLAG STICKS WHEN TEST SWITCH ACTUATED ON FIRST OFFICER'S SIDE. REPLACED FIRST OFFICER'S INDICATOR AND OPS CHECKED OK PER MM 34-22-0.Jul 19, 2003 · N250TR · Boeing 7372K5 · Integrated Flight SystemSDR 250TR0020Coupler · failedYAW DAMPER INOPERATIVE. REPLACED YAW CAMPER COUPLER PER MM 22-12-01. OPS CHECKS NORMAL.Jun 27, 2003 · N250TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0019Bulb · burned outOVERWING EMERGENCY LIGHT INOP. RELAMPED OVERWING EMERGENCY LIGHT.Jun 10, 2003 · N250TR · Boeing 7372K5 · Emergency LightingSDR 250TR0018Indicator · malfunctionedF/O'S ADI JUMPS & TURNS. REPLACED F/O'S ADI. OPERATIONAL TEST NORMAL PER MM 34-22-0.Jun 6, 2003 · N250TR · Boeing 7372K5 · Attitude and Direction Data SystemSDR 250TR0017Floor Panel · damagedHOLE IN NR 2 FLOOR PANEL IN FORWARD CARGO BIN. REPAIRED PER SRM 51-40-2 FIG 1.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Floor PanelSDR 250TR0016Frame · crackedCRACK IN FRAME AT BS 480 AT LEFT TRANSITION ANGLE (FORWARD CARGO BIN). REPAIRED PER SRM 51-40-3.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Main, FrameSDR 250TR0015Stiffener · damagedHOLE IN STIFFENER AT STR 26RT BETWEEN BS420 AND BS440. FABRICATED NEW WEB PER DWG 65-20726 AND INSTALLED PER SRM 51-10-1.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Miscellaneous StructureSDR 250TR0014Web · crackedWEB PANEL CRACKED BELOW LEFT TRANSITION ANGLE BS440 (FORWARD CARGO BIN). FABRICATED AND INSTALLED NEW WEB PER DWG 69C41473.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Miscellaneous StructureSDR 250TR0013Angle · corrodedCORROSION ON LEFT TRANSITION ANGLE BS440 TO BS480 (FORWARD CARGO BIN). REPLACED CORRODED SECTION OF TRANSITION ANGLE PER EA53-114.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Miscellaneous StructureSDR 250TR0011Cargo Track · damagedRIGHT CARGO TIE DOWN TRACK CRACKED AT BS 460 (FORWARD CARGO BIN).REPAIRED PER SRM 51-40-4.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage, Seat/Cargo Attach FittingsSDR 250TR0012Panel · crackedWEB PANEL CRACKED LEFT SIDE UNDER TRANSITION ANGLE AT BS460 (FORWARD CARGO BIN). FABRICATED NEW WEB IAW DWG 69C41473 AND INSTALLED.Apr 29, 2003 · N250TR · Boeing 7372K5 · Fuselage Miscellaneous StructureSDR 249TR0018Circuit Breaker · trippedNO AUTO PILOT TRIM. FOUND AUTO PILOT TRIM CIRCUIT BREAKER POPPED. RESET BREAKER. OPS CHECKED OK PER MM 22-11-01.Apr 26, 2003 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 249TR0017Battery Pack · inoperativeDURING PRE-AMP CHECK, FOUND L1 & R1 EMERGENCY SLIDE LIGHTS INOP. RELAMPED L1 DOOR SLIDE LIGHT, REPLACED R1 DOOR SLIDE LIGHT ASSEMBLY AND REPLACED TWO BATTERY PACKS PER MM 33-51-81.Apr 22, 2003 · N249TR · Boeing 7372K5 · Emergency LightingSDR 250TR0010Computer · malfunctionedB-AUTO PILOT CREATES JERKING OF ELEVATORS WHILE AIRCRAFT BANKED; OK WITH -A- AUTO PILOT. SWAPPED FCC'S FOR FURTHER TROUBLESHOOTING.Apr 21, 2003 · N250TR · Boeing 7372K5 · Autopilot ComputerSDR 249TR0016Warning Light · illuminatedMACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. UNABLE TO DUPLICATE. PERFORMED BITE TEST VIA PDCS CDU, NO FAULTS NOTED.Mar 31, 2003 · N249TR · Boeing 7372K5 · Speed-Attitude Correction SystemSDR 249TR0015Warning Light · illuminatedMACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT, THEN WENT AWAY. COMPLETED MACH TRIM TEST PER MM 22-21-0. OPS CHK OK.Mar 30, 2003 · N249TR · Boeing 7372K5 · Speed-Attitude Correction SystemSDR 250TR0009Light · malfunctionedEMERGENCY EXIT LIGHT COMES ON WHEN POWER IS SWITCHED OFF AND EMERGENCY EXIT SWITCH IS IN OFF POSITION. REPLACED RT FWD EMERGENCY EXIT LIGHT ASSY AND OPS CHECK PER MM 33-51-11.Mar 26, 2003 · N250TR · Boeing 7372K5 · Emergency LightingSDR 250TR0008Transmitter · malfunctionedAUTO THROTTLE KEEPS DISCONNECTING DURING FLIGHT. REPLACED LT. ENGINE THRUST LEVER POSITION TRANSMITTER PER MM 22-31-81. OPS CHECKED OK.Mar 23, 2003 · N250TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0014ComputerPDC dumps data during take off, auto throttles retarding from climb power when EPR selected, (major power reduction). Unable to duplicate. Swapped PDC com. from A/C 251TR per MM 34-18-11. Ops chk good per MM 34-18-0Mar 3, 2003 · N249TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0013Limit SwitchBoth A & B auto pilots disengage after flaps reach #1 positon during approach. Will not re-engage until selected beyond flaps 5 positon. Replaced flaps up limit switch 5245(?) per MM 27-51-291 ops chk normal per MM 22-11-01.Mar 3, 2003 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0007Cowling#2 engine air inlet cowl has gouge at 1:30 position. Repaired damaged area per EA No. 54-045 dated 2/14/2003.Feb 2, 2003 · N250TR · Boeing 7372K5 · Engine Cowling SystemSDR 250TR0006ComputerAuto throttle would not engage. R&R auto throttle computer. Chks good per MM 22-31-01.Feb 2, 2003 · N250TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0012ComputerF/O's ADI & HSI will not self test in VOR or ILS. Removed & replaced FCCB computer. Ops checknormal per MM 34-31-0 and 22-11-01. Ops check good.Jan 13, 2003 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 249TR0011SwitchA/P & F/D mode indicates TO/GA prior to take-off without input from crew & IAS changes to 165 knots on its own. Cleaned #2 throttle TO/GA switch, performed AP/FD bite test per MM 22-11-01.System tests normal.Dec 24, 2002 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0005Wire · brokenA/T FAILS INTERFACE TEST 6.9 & 56.9 SUB.TEST 8 & 9. ITEM DEFERRED IAW 737-200 MEL 22-4 CONTROL NR 1221003. 01/10/2003. REPAIRED BROKEN WIRES AT SUMMING POINTS ON E1-3 SHELF PER WDM CHPT. 20 A/T OPS NORMAL PER BITE & A/P INTERFACE TESTS. CLEARED MEL 22-4, Dec 19, 2002 · N250TR · Boeing 7372K5 · Auto Flight System WiringSDR 249TR0008LightL2 emergency exit overhead light inop. Removed and replaced L2 overhead emergency exit light. Ops chk OK.Nov 11, 2002 · N249TR · Boeing 7372K5 · Emergency LightingSDR 249TR0010Light · inoperativeL2 OUTSIDE EMERGENCY LIGHT INOP. INSTALLED NEW EMERGENCY EXIT LIGHT ASSY.Nov 5, 2002 · N249TR · Boeing 7372K5 · Emergency LightingSDR 249TR0009LightL2 door emergency exit overhead light inop. Installed new emergency exit light assy.Nov 5, 2002 · N249TR · Boeing 7372K5 · Emergency LightingSDR 249TR0007ComputerA/T fails bite test and goes completely inop at times. R&R A/T computer Ops normal per Bite test MM 22-31-01Aug 7, 2002 · N249TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0002Computer · faultyA/T FAILS BITE TEST AND GOES COMPLETELY INOP AT TIMES. REMOVED AND REPLACED A/T COMPUTER, OPS NORMAL PER BITE TEST MM 22-31-01.Aug 7, 2002 · N249TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0022Indicator · malfunctionedBOTH ADI'S HAD SPEED FLAGS WHICH MADE AUTOTHROTTLES INOP. INSTALLED SERVICEABLE ADI IAW 34-22-0, ACCOMPLISHED PDC BITE OF AUTOTHROTTLES PER MM 22-31-01, OPS CHECK GOOD.Aug 2, 2002 · N249TR · Boeing 7372K5 · Attitude and Direction Data SystemSDR 249TR0006IndicatorBoth ADI's had "speed" flags which made auto throttles inop. Installed serviceable ADI IAW 34-22-0, accomplished PDC Bite of auto throttles per MM 22-31-01, ops check goodAug 2, 2002 · N249TR · Boeing 7372K5 · Attitude and Direction Data SystemSDR 250TR0004Potentiometer"A" Auto-pilot jerky in all modes. R&R stab trim potentiometer.May 31, 2002 · N250TR · Boeing 7372K5 · Autopilot ComputerSDR N250TR0003Autothrust SysAuto Throttles Inop.May 5, 2002 · N250TR · Boeing 7372K5 · Auto Throttle SystemSDR N249TR0005Autopilot SysCapt. Flt director during App. while on "B" channel turns itself off. Bite test OK.May 5, 2002 · N249TR · Boeing 7372K5 · Autopilot SystemSDR N249TR0004Autopilot SysCapt. Flt director during App. while on "B" channel turns itself off. Bite test OK.May 5, 2002 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 249TR0004Autopilot SysAuto pilot in B mode shakes aircraft while engaged. Bite ck OK.May 5, 2002 · N249TR · Boeing 7372K5 · Autopilot SystemSDR 250TR0002Switch · out of adjustAUTO THROTTLES WILL SET TAKEOFF AND CLIMB POWER BUT WILL NOT RETARD THROTTLES TO MAINTAIN SPEED. DURING CRUISE PDC SPEED IS THE ONLY MODE THAT WORKS. MCP SPEED MODE WILL NOT WORK IN ANY REGIME. ADJUSTED AUTO THROTTLE SWITCH. OP'S CHECKS OK.Apr 12, 2002 · N250TR · Boeing 7372K5 · Auto Throttle SystemSDR 250TR0001ReceiverMCP panel @ 7000`, engage PDC A/S bug goes to 310K. Speed mode would not engage. When flaps select to 5 auto pilots kick off, would not re-engage. R&R both radio altimeters.Apr 9, 2002 · N250TR · Boeing 7372K5 · Speed-Attitude Correction SystemSDR 249TR0003Autothrust SysAutothrottles inop.Apr 8, 2002 · N249TR · Boeing 7372K5 · Auto Throttle SystemSDR 249TR0001Battery PackAft service door, aft entry door and fwd entry door emergency lights are inop. R&R battery pack/light assy.Mar 18, 2002 · N249TR · Boeing 7372K5 · Emergency LightingSDR 2002F00250Switch · defectiveINT - WHEN FLAPS SELECT FROM 1-5 UNITS AUTO PILOT KICKS OFF. REMOVED AND REPLACED FLAPS UP SWITCH AND RIGGED PER MM 27-51-291. (M)Jan 22, 2002 · N249TR · Boeing 7372K5 · Trailing Edge Flap Control SystemSDR 2001F00216Sensor · out of adjGUA - FLT 970 - LANDING GEAR LEVER GOT STUCK IN THE OFF POSITION AFTER TAKEOFF, IT TOOK SEVERAL TRIES TO BRING LANDING GEAR UP, IT OCCURRED AFTER TAKEOFF IN FLIGHT FROM SJO TO GUA. ADJUSTED LANDING GEAR SAFETY SENSOR TO CORRECT GAP, AS PER AMM 32-09-200 AND PAug 8, 2001 · N231TA · Boeing 7372K5 · Landing Gear Position and WarningSDR 2001F00007Module · malfunctionedMIA - FLT 321 - AFTER TAKEOFF OF FLIGHT, THE LANDING GEAR DID NOT GO UP WHEN RAISED. THE AIRCRAFT RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE, LANDING WAS NORMAL. T/S WAS PERFORMED AS PER AMM 32-09-200 PAGE 501, ADJUSTED GROUND SAFETY SWITCH, AIRCRAFT JACKJun 5, 2001 · N231TA · Boeing 7372K5 · Hydraulic System, Main
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