Boeing 737-228

Service difficulty reports · 371

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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 = '737228'
  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 234TR0010Skin · crackedFUSELAGE SKIN CRACKED AFT OF COOLING AIR EXHAUST VENT. REPAIRED PER BOEING SB 737-53-1117.Jul 25, 2003 · N234TR · Boeing 737228 · Fuselage Main, Plate/SkinSDR 234TR0009Pcu · malfunctionedYAW DAMPER REPORTED WILL NOT STAY ENGAGED. SHOWS FAULT HISTORY MESSAGE 22-21003. REPLACED RUDDER POWER CONTROL UNIT PER MM 27-21-91 AND PERFORMED ADJUSTMENT AND TEST PER MM 27-21-91. YAW DAMPER CHECKS NORMAL PER MM 22-12.Jul 25, 2003 · N234TR · Boeing 737228 · Rudder Control SystemSDR 234TR0008Wire · brokenB-AUTO PILOT FAILED LRU INTERFACE -MCP TEST 73.6 (HDG SYNC). REPAIRED BROKEN WIRE AT CONNECTOR D994 ON E1-2 SHELF. OPERATES NORMAL.Jul 25, 2003 · N234TR · Boeing 737228 · Auto Flight System WiringSDR 234TR0007Indicator · malfunctionedFIRST OFFICER'S HSI - VOR FROM, ILS VALID, VOR VALID, FLAG ERRONEOUS. REPLACED HSI. ALL FUNCTIONS OPERATE NORMAL.Jul 25, 2003 · N234TR · Boeing 737228 · Dependent Position Determining SystemSDR 234TR0006Wire · malfunctionedFLIGHT CONTROL COMPUTER FAILS LRU INTERFACE TEST 25.21 SUBTEST 1 AND 2. REMOVED E1-1 SHELF AND CORRECTED WIRING. OPS NORMAL.Jul 25, 2003 · N234TR · Boeing 737228 · Auto Flight System WiringSDR 234TR0005Gyro · malfunctionedNR 1 VERTICAL GYRO SHOWS 3.5-4 DEGREES PITCH UP. REPLACED VERTICAL GYRO PER MM 34-21-21.Jul 19, 2003 · N234TR · Boeing 737228 · Attitude Gyro and Indicating SystemSDR 243TR0005Gyro · inaccurateNR 1 VERTICAL GYRO SHOWS 3.5-4 DEGREES PITCH UP. REPLACED VERTICAL GYRO PER MM 34-21-21.Jul 19, 2003 · N234TR · Boeing 737228 · Attitude Gyro and Indicating SystemSDR 234TR0004Fuel Control · malfunctionedNR 1 ENGINE ROLLED BACK ON SHORT FINAL APPROACH. REPLACED IGNITION EXCITER BOX PER MM 74-11-11 AND REPLACED FUEL CONTROL UNIT PER MM 73-09-255. OPS CHECKS OK.Jul 19, 2003 · N234TR · Boeing 737228 · Fuel Control/Turbine EnginesSDR 234TR0003Sensor · malfunctionedAUTO-PILOT A&B NEUTRAL SHIFT SENSOR OUT OF TOLERANCE PER ELEVATOR RIGGING BITE TEST. REMOVED, REPLACED, AND ADJUSTED NEUTRAL SHIFT SENSOR. OPS. CHECKS GOOD PER MM 22-11-122.Jul 15, 2003 · N234TR · Boeing 737228 · Autopilot SystemSDR 234TR0002Receiver · unreliableBOTH VOR RECEIVERS ARE ERRATIC AND UNRELIABLE. REMOVED AND REPLACED BOTH RECEIVERS. OPS CHECKS GOOD PER MM 34-31-41.Jul 15, 2003 · N234TR · Boeing 737228 · Landing and Taxi AidsSDR 234TR0001Gps · malfunctionedGPS WILL NOT ACQUIRE ANY SATELLITES. REMOVED AND REPLACED GNLU. GPS NOW ACQUIRES SATELLITES ON GROUND.Jul 15, 2003 · N234TR · Boeing 737228 · Global Positioning SystemSDR 252TR0006Coupler · intermittentMACH TRIM IS INTERMITTENT. PLACED ON MEL 22-5. 7/15/2003; REMOVED AND REPLACED MACH TRIM COUPLER IAW MM 22-21-0 AND CLEARED MEL.Jul 5, 2003 · N252TR · Boeing 737228 · Speed-Attitude Correction SystemSDR 252TR0005Coupler · inoperativeAUTO PILOT AT 315 KTS TRIM ROLLS BACK AND FORTH 3 TURNS EACH DIRECTION. REPLACED MACH TRIM COUPLER IAW MM 22-21-0. OPS TEST NORMAL.Jun 23, 2003 · N252TR · Boeing 737228 · Autopilot SystemSDR 252TR0004Pressure Switch · leakingB-CHANNEL AUTO PILOT WILL NOT ENGAGE. PLACED B-CHANNEL AUTO PILOT ON MEL CONT 0423001. REMOVED AND REPLACED HYD PRESSURE SWITCH. OPS AND LEAK CHECKS GOOD IAW MM 22-11-391Apr 23, 2003 · N252TR · Boeing 737228 · Hydraulic System, MainSDR 252TR0003CouplerYaw damper inop. Removed and replaced yaw damper coupler IAW MM 22-11-141. Ops. check good IAW MM 22-12-01.Feb 11, 2003 · N252TR · Boeing 737228 · Auto Flight SystemSDR 252TR0002LightEmergency exit light over L1 door does not work. Replaced emergency exit light over L1 door.Jan 3, 2003 · N252TR · Boeing 737228 · Emergency LightingSDR 252TR0001PAPanelreturn to departure point due to high a/c vibration. insp complete exterior of a/c all panels & flight controls to include doors,found several loose & missing screws on panel # 6537. replaced & retorqued screws on panel # 6537,no other defects noted.Aug 5, 2002 · N252TR · Boeing 737228 · Wing, Plate/SkinSDR F3LA200200202Turbine · failedON APPROACH, THE FLIGHT CREW NOTED A VIBRATION AT 30 PERCENT POWER IN THE RIGHT (NUMBER 2) ENGINE. THE FLIGHT CREW REDUCED POWER AND MADE A NORMAL LANDING. THE ENGINE WAS SHUT DOWN AND TAKEN TO THE GATE. DURING THE WALK AROUND INSPECTION, MAINTENANCE NOTED Aug 3, 2002 · N234TR · Boeing 737228 · Turbine SectionSDR 251TR0003VaneReference DMI #0707002. Auto pilot V/S mode reverts to LVL change uncommanded. Alpha vane replaced. See item #1 log page 09871, test C/W I/A/W ch. 22-11-381, ops chk. good. This clears DMI 0707002. Placard removed.Jul 12, 2002 · N251TR · Boeing 737228 · Autopilot SystemSDR 251TR0002VaneReference DMIReference DMI #0702001, Auto throttle will not engage with Capt. F/D chosen and go to max EPR in cruise flt. T/S system. Found Alpha vane failed & #2 auto throttle servo intermittent. Removed #1 AOA sensor, installed serviceable #1 AOA sensor I/Jul 9, 2002 · N251TR · Boeing 737228 · Auto Throttle SystemSDR 251TR0001Autopilot SysAuto pilot V/S mode reverts to LVL change mode uncommanded. Deferred per MEL 22-15-8 CTL #0707002 CATCJul 7, 2002 · N251TR · Boeing 737228 · Autopilot SystemSDR F3LA200200142Attach Angle · crackedDURING C-1 CHECK, INSPECTION REPORTED CRACKED ATTACH ANGLE ON LT WING LOWER TRAILING EDGE PANEL ON MLG BEAM. FABRICATED AND INSTALLED REPLACEMENT L-ANGLE PER SOPM 20-41-02 AND SRM 51-40-02.May 15, 2002 · N234TR · Boeing 737228 · Wing Miscellaneous StructureSDR F3LA200200145Support · corrodedDURING C-1 CHECK, INSPECTION REPORTED CORROSION ON WEB SUPPORT, STR 21L, STA 967. REPLACED WEB SUPPORT PER 51-30-2 SOPM 20-41-02.May 10, 2002 · N234TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200144Doubler · crackedDURING C-1 CHECK, INSPECTION REPORTED DOUBLER CRACKED AT LOWER AFT CORNER OF EXT. POWER DOOR CUTOUT. REMOVED CRACK IN DOUBLER AND REPAIRED PER SRM 53-30-01.May 9, 2002 · N234TR · Boeing 737228 · Fuselage Main, Plate/SkinSDR F3LA200200143Panel · crackedDURING C-1 CHECK, INSPECTION REPORTED LT VERTICAL PANEL 9507L INNER BRACE WORN AND CRACKED. FABRICATED PANEL RETAINER AND INSTALLED PER SRM 51-40-2, 51-30-50 AND SOPM 20-41-02.May 9, 2002 · N234TR · Boeing 737228 · Vertical Stabilizer, Plate/SkinSDR F3LA200200059Wire · chafedDURING SERVICE CHECK, MAINTENANCE REPORTED L1 AND R1 DOOR EMERGENCY EXIT SIGNS AND FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPLACED POWER SUPPLY UNIT AND BATTERY PACK, WHICH DID NOT CORRECT PROBLEM. FERRIED AIRCRAFT TO DEN FOR REPAIR. FOUNFeb 24, 2002 · N237TR · Boeing 737228 · Light System WiringSDR F3LA200200042Solenoid · failedUPON TAKEOFF IN SLC, HAD TO PULL LANDING GEAR LEVER TRIGGER TO GET GEAR HANDLE UP. IN DEN, MADE LOW PASS BY DENVER TOWER TO CONFIRM GEAR DOWN. NO GEAR INDICATION LIGHTS. RECYCLED HANDLE, ALL INDICATIONS NORMAL AND LANDED WITHOUT INCIDENT. REPLACED LANDING Feb 19, 2002 · N234TR · Boeing 737228 · Landing Gear Retraction/Extension SystemSDR F3LA200200028Doubler · corrodedDURING C-7 CHECK, INSPECTION REPORTED WEB DOUBLER CORRODED BETWEEN STR 23R AND 24R AT STA 787. FABRICATED NEW WEB PER BAC DRAWING 65-47959 AND INSTALLED REPAIR PER SRM 51-30-02.Jan 28, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR 2002F00246Wire · brokenDAL - AUTO PILOT B-CHANNEL ABRUPTLY PUSHES NOSE DOWN WHEN ENGAGED. REPAIRED BROKEN WIRE AT STATION 1080 DISCONNECT BRACKET IAW WPM 20-10-13. OPERATION CHECKED NORMAL IAW MM 22-11-01. (M)Jan 27, 2002 · N251TR · Boeing 737228 · Auto Flight System WiringSDR F3LA200200032Stringer · corrodedDURING C-7 CHECK, BOLT MIGRATING OUT UNDER LT WING-TO-BODY FAIRING CHORD AT STA 685. REMOVED BROKEN BOLT AND FOUND CORROSION INSIDE BOLT HOLE. OVERSIZED HOLE TO SECOND OVERSIZE OF ORIGINAL BOLT SIZE AND STILL FOUND INDICATION OF CORROSION. COMPLIED WITH INTJan 27, 2002 · N237TR · Boeing 737228 · Fuselage Main, Longeron/StringerSDR F3LA200200027Mount · wornDURING C-7 CHECK, INSPECTION REPORTED EXCESSIVE PLAY IN NR 2 ENGINE YOKE TO WING MOUNT. REPLACED ENGINE MOUNT FITTINGS AND YOKE PER MM 54-51-41.Jan 26, 2002 · N237TR · Boeing 737228 · Engine Mount SectionSDR F3LA200200037Wedge · delaminatedDURING C-7 CHECK, INSPECTION REPORTED RT INBOARD HINGE FLAP DELAMINATED ON TRAILING EDGE. REPLACED RT INBOARD TRAILING EDGE OF HINGE FLAP PER SRM 51-30-02.Jan 25, 2002 · N237TR · Boeing 737228 · Trailing Edge FlapsSDR F3LA200200036Bracket · corrodedDURING C-7 CHECK, INSPECTION REPORTED L-1 DOOR AFT GIRT BAR ATTACH BRACKET CORRODED. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER BOWING DRAWING 65C16121.Jan 25, 2002 · N237TR · Boeing 737228 · Passenger/Crew DoorsSDR F3LA200200035Intercostal · crackedDURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STA 440, STR 26-L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-1.Jan 25, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200034Floor Support · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CORRODED AT COCKPIT ENTRY AT STA 277. REPLACED FLOOR SUPPORT ANGLE PER EO 52-50-737-004.Jan 25, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200033Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED BETWEEN STA 500A AND 500B, STR 26-R. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED PER SRM 51-30-2.Jan 25, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200026Mount · wornDURING C-7 CHECK, INSPECTION REPORTED SEVERE MOVEMENT IN NR 2 ENGINE AT YOKE IN PYLON, INBOARD SIDE. REPLACED NR 2 ENGINE MOUNT YOKE PER MM 54-41-11, 4C - J, PAGES 41 AND 402.Jan 25, 2002 · N237TR · Boeing 737228 · Engine Mount SectionSDR F3LA200200023Door Frame · crackedDURING C-7 CHECK, INSPECTION REPORTED CRACK IN FWD GALLEY DOOR FRAME, UPPER FWD SIDE, STA 294.5. REPLACED FWD GALLEY DOOR FRAME SEGMENT ABOVE DOOR STOP AT STA 294.5 PER SRM 51-10-1 AND EA 53-737-151.Jan 19, 2002 · N237TR · Boeing 737228 · Fuselage Main, StructureSDR F3LA200200024Hydraulic Line · leakingEN ROUTE FROM PHX TO DEN, FLIGHT CREW REPORTED A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO, WITH SUBSEQUENT SYSTEM FAILURE. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PRESSURE LINE FOUND TO BE LEAKING AND PJan 18, 2002 · N234TR · Boeing 737228 · Hydraulic System, MainSDR F3LA200200022Frame · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOOR FRAME AT STA 480, STR 27-L, IN FWD CARGO COMPARTMENT CORRODED. FABRICATED REPLACEMENT FLOOR FRAME AND INSTALLED REPAIR PER SRM 53-10-4.Jan 18, 2002 · N237TR · Boeing 737228 · Fuselage Main, FrameSDR F3LA200200021Stringer · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STR 18-L AT STA 380. REMOVED CORROSION, FABRICATED STRINGER SPLICE AND DOUBLER, AND PERFORMED REPAIR PER SRM 51-10-1, 51-20-1, 51-30-2, 53-10-1, 53-10-3 AND 53-30-3.Jan 13, 2002 · N237TR · Boeing 737228 · Fuselage Main, Longeron/StringerSDR F3LA200200016Support Bracket · gougedDURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 827 GOUGED. FABRICATED REPLACEMENT SUPPORT BRACKET AND INSTALLED PER SRM 20-41-02.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200018Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM IN CARGO COMPARTMENT CORRODED AT RBL 8 AND PANEL SPLICE AT STA 770 OUT OF LIMITS. FABRICATED REPAIR ANGLES AND INSTALLED PER SRM 53-10-5.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Main, Floor BeamSDR F3LA200200020Strap · corrodedDURING C-7 CHECK, INSPECTION REPORTED LOWER FRAME FLANGE STRAP AT STA 794 CORRODED. REPLACED LOWER FRAME FLANGE STRAP PER SRM 51-10-2 AND 51-30-2.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200019Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON CARGO COMPARTMENT FLOORBEAM, LBL 2.5, STA 770. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-10-5.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Main, Floor BeamSDR F3LA200200017Support Bracket · gougedDURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 807 GOUGED. FABRICATED REPLACEMENT SUPPORT BRACKET AND INSTALLED PER SRM 51-10-2.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200015Angle · corrodedDURING C-7 CHECK, INSPECTION REPORTED THRESHOLD SUPPORT ANGLE, STA 794, STR 25-R, IN AFT CARGO COMPARTMENT CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-10-2 AND 51-30-2.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200014Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 767-787, STR 25-R, CORRODED. INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-5.Jan 10, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous StructureSDR F3LA200200008Torque Tube · corrodedDURING C-7 CHECK, INSPECTION REPORTED TORQUE TUBE CORRODED, L-2 DOOR TORQUE BOX. REPLACED TORQUE TUBE PER OHM 52-16-03.Jan 9, 2002 · N237TR · Boeing 737228 · Passenger/Crew DoorsSDR F3LA200200007Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL, STR 25R, AFT OF STA 500. REPLACED INTERCOSTAL PER SRM 51-10-02 AND BAC DRAWING 65-20726.Jan 8, 2002 · N237TR · Boeing 737228 · Fuselage Miscellaneous Structure
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