# Service difficulty reports: Boeing 737-376

A list on [Boeing 737-376](https://openairdocs.org/model/boeing-737-376.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 195 reports

- [SDR AU510001746](https://openairdocs.org/sdr/AU510001746.md): Girt Bar · faulty · Dec 12, 2005 · Boeing 737376 · Escape Slide
  > (AUS) DOOR R1 ESCAPE SLIDE GIRT BAR CONTACTING DOOR FRAME.
- [SDR AUS20040494](https://openairdocs.org/sdr/AUS20040494.md): Bolt · sheared · May 26, 2004 · Boeing 737376 · Fasteners
  > (AUS) RT MAIN LANDING GEAR OB STABILIZING FITTING OB LOWER ATTACHMENT BOLT SHEARED ALONG THE SHANK IN AN AREA COINCIDING WITH THE WING REAR SPAR.
- [SDR AUS20040426](https://openairdocs.org/sdr/AUS20040426.md): Windshield · failed · May 18, 2004 · Boeing 737376 · Flight Compartment Windows
  > (AUS) FIRST OFFICER'S NR 1 WINDOW OUTER PANE SHATTERED ALONG WITH ARCING FROM THE WINDSCREEN.
- [SDR AUS20040423](https://openairdocs.org/sdr/AUS20040423.md): Autopilot Sys · failed · May 17, 2004 · Boeing 737376 · Autopilot System
  > (AUS) DUAL AUTOPILOT MALFUNCTION. LIMITED INFORMATION PROVIDED.
- [SDR AUS20040422](https://openairdocs.org/sdr/AUS20040422.md): Tire · damaged · May 14, 2004 · Boeing 737376 · Tire
  > (AUS) RT NOSE LANDING GEAR TIRE DAMAGED BY DEBRIS ON RUNWAY. TIRE SHREDDED AND CAUSED DAMAGE TO FORWARD LOWER FUSELAGE SKIN. FOD WAS IDENTIFIED AS THRUST REVERSER BLOCKER DOOR PARTS.
- [SDR AUS20040415](https://openairdocs.org/sdr/AUS20040415.md): Drive Shaft · worn · May 13, 2004 · Boeing 737376 · Trailing Edge Flap Actuator
  > (AUS) NR 4 TRAILING EDGE FLAP TRANSMISSION UNIVERSAL DRIVESHAFT WORN AXIALLY BEYOND LIMITS. END FLOAT WAS APPROXIMATELY 0.406MM(0.016IN) AT OUTPUT END.
- [SDR AUS20040388](https://openairdocs.org/sdr/AUS20040388.md): Generator · failed · May 9, 2004 · Boeing 737376 · AC Generation System
  > (AUS) APU GENERATOR FAILED.
- [SDR AUS20040365](https://openairdocs.org/sdr/AUS20040365.md): Oven · faulty · May 6, 2004 · Boeing 737376 · Buffet/Galleys
  > (AUS) AFT GALLEY OVEN ELECTRICAL FAULT. INVESTIGATION FOUND FILTERBOARD CAUGHT FIRE DUE TO THE FORMATION OF DRY SOLDER JOINTS ON INDUCTOR CONTACTS.
- [SDR AUS20040330](https://openairdocs.org/sdr/AUS20040330.md): Force Limiter · faulty · May 2, 2004 · Boeing 737376 · Autopilot System
  > (AUS) AUTOPILOT WOULD NOT ENGAGE. SUSPECT FAULTY FORCE LIMITER.
- [SDR AUS20040312](https://openairdocs.org/sdr/AUS20040312.md): Bolt · separated · Apr 27, 2004 · Boeing 737376 · Fasteners
  > (AUS) PASSENGER SEAT SUPPORT BEAM TO AISLE SIDE LEG STRUCTURE BOLTS SEPARATED AND FOUND UNDER SEAT 12 DEF.
- [SDR AUS20040384](https://openairdocs.org/sdr/AUS20040384.md): Indicator · faulty · Apr 26, 2004 · Boeing 737376 · Trailing Flap Position Indicating System
  > (AUS) FLAP POSITION INDICATOR FAULTY.
- [SDR AUS20040260](https://openairdocs.org/sdr/AUS20040260.md): Stop · faulty · Apr 5, 2004 · Boeing 737376 · Passenger/Crew Doors
  > (AUS) FOLLOWING LOUD CRACKING NOISES IN FLIGHT AN INSPECTION OF THE DOOR AND DOOR CUTOUT AREA WAS CARRIED OUT. I NVESTIGATION FOUND THE DOOR STOPS HEAVILY WORN AND DRY.
- [SDR AUS20040457](https://openairdocs.org/sdr/AUS20040457.md): Limiter · faulty · Mar 30, 2004 · Boeing 737376 · Autopilot System
  > (AUS) AUTOPILOT TORQUE LIMITER FAULTY.
- [SDR AUS20040192](https://openairdocs.org/sdr/AUS20040192.md): Indicator · failed · Mar 11, 2004 · Boeing 737376 · Airspeed/Mach Indicator
  > (AUS) FIRST OFFICER'S AIRSPEED INDICATOR/MACHMETER FAILED.
- [SDR AUS20040182](https://openairdocs.org/sdr/AUS20040182.md): Pin · separated · Mar 9, 2004 · Boeing 737376 · Passenger/Crew Doors
  > (AUS) L2 OUTER DOOR HANDLE MOVED TO VERTICAL POSITION AFTER DEPARTURE. DURING INVESTIGATION, THE WHOLE HANDLE AND SHAFT ASSEMBLY CAME AWAY FROM THE DOOR. A LOOSE CASTELLATED NUT AND SHIMS WERE FOUND IN THE HOUSING ASSEMBLY. FURTHER INVESTIGATION FOUND A DEF
- [SDR AUS20040172](https://openairdocs.org/sdr/AUS20040172.md): Valve · failed · Mar 7, 2004 · Boeing 737376 · Fuel Selector/Shut-Off Valve
  > (AUS) NR 2 ENGINE FUEL SYSTEM SPAR VALVE FAILED.
- [SDR AUS20040141](https://openairdocs.org/sdr/AUS20040141.md): Actuator · failed · Feb 29, 2004 · Boeing 737376 · Fuel Transfer Valve
  > (AUS) FUEL CROSSFEED VALVE ACTUATOR FAILED.
- [SDR AUS20040123](https://openairdocs.org/sdr/AUS20040123.md): Hose · leaking · Feb 24, 2004 · Boeing 737376 · Landing Gear Retraction/Extension System
  > (AUS) RT MAIN LANDING GEAR ACTUATOR UP LINE LEAKING DUE TO CHAFING ON B SYSTEM LOW PRESSURE RETURN LINE. ENGINE DRIVEN PUMP FAILED AND RETURN FILTERS CONTAMINATED.
- [SDR AUS20040098](https://openairdocs.org/sdr/AUS20040098.md): Bearing · seized · Feb 10, 2004 · Boeing 737376 · Elevator Control System
  > (AUS) ELEVATOR CONTROL CENTERING UNIT MOUNT BEARING SEIZED.
- [SDR AUS20040097](https://openairdocs.org/sdr/AUS20040097.md): Actuator · cracked · Feb 9, 2004 · Boeing 737376 · Drag Control Actuator
  > (AUS) NR 4 GROUND SPOILER OB ACTUATOR BODY CRACKED AND LEAKING IN AREA NEXT TO RETRACT FITTING.
- [SDR AUS20040080](https://openairdocs.org/sdr/AUS20040080.md): Hydraulic System · leaking · Feb 6, 2004 · Boeing 737376 · Hydraulic System, Main
  > (AUS) HYDRAULIC SYSTEM LEAKING.
- [SDR AUS20040042](https://openairdocs.org/sdr/AUS20040042.md): Sensor · out of adjust · Jan 22, 2004 · Boeing 737376 · Leading Edge Slat Position Indicating System
  > (AUS) LEADING EDGE FLAP NR 2 EXTEND SENSOR OUT OF ADJUSTMENT.
- [SDR AUS20040198](https://openairdocs.org/sdr/AUS20040198.md): Hydraulic System · contaminated · Jan 21, 2004 · Boeing 737376 · Hydraulic System, Main
  > (AUS) HYDRAULIC SYSTEM A FAULTY. ENGINEERING INVESTIGATION SUSPECTS AIR IN HYDRAULIC SYSTEM. LT MAIN LANDING GEAR HYDRAULIC HOSE HAD BEEN REPLACED ON THE PREVIOUS DAY.
- [SDR AUS20040031](https://openairdocs.org/sdr/AUS20040031.md): Hose · burst · Jan 20, 2004 · Boeing 737376 · Hydraulic System, Main
  > (AUS) LT MAIN LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC HOSE BURST. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20040013](https://openairdocs.org/sdr/AUS20040013.md): Engine · overheated · Jan 5, 2004 · Boeing 737376 · Engine (Turbine/Turboprop)
  > (AUS) ENGINE EXCEEDED EGT LIMITS. EGT REACHED 938 DEGREES C.
- [SDR AUS20031125](https://openairdocs.org/sdr/AUS20031125.md): Pipe · chafed · Nov 3, 2003 · Boeing 737376 · Hydraulic System, Main
  > (AUS) NOSE LANDING GEAR UP HYDRAULIC PIPE CHAFED AND LEAKING. LOSS OF HYDRAULIC FLUID. SPRAY OF HYDRAULIC FLUID CONTAMINATED E1-3 AVIONICS RACK CONNECTORS D4115P AND D4067P.
- [SDR AUS20031095](https://openairdocs.org/sdr/AUS20031095.md): Brake Assy · faulty · Oct 27, 2003 · Boeing 737376 · Landing Gear Brake System
  > (AUS) AUTOBRAKE SYSTEM NOT ARMING. LIMITED INFORMATION PROVIDED.
- [SDR AUS20031076](https://openairdocs.org/sdr/AUS20031076.md): Fire Detector · inoperative · Oct 24, 2003 · Boeing 737376 · Fire Detection
  > (AUS) NR 1 ENGINE FIRE DETECTOR SYSTEM INOPERATIVE.
- [SDR AUS20030996](https://openairdocs.org/sdr/AUS20030996.md): Actuator · binding · Sep 18, 2003 · Boeing 737376 · Compressor Bleed Control
  > (AUS) NR 1 ENGINE VARIABLE BLADE VALVE ACTUATORS AT THE 4 O'CLOCK AND 5 O'CLOCK POSITIONS BINDING AND INTERNAL HEXAGONAL DRIVES WORN.
- [SDR AUS20030950](https://openairdocs.org/sdr/AUS20030950.md): Fire Loop · faulty · Sep 17, 2003 · Boeing 737376 · Fire Detection
  > (AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. INVESTIGATION FOUND A HIGH RESISTANCE (2000OHMS) SENSOR IN LOOP B'. MEL APPLIED BUT DEFECT OCCURRED DURING NEXT TAKEOFF AND ON SUBSEQUENT FAULT FINDING GROUND RUN. SEE MDR 03/0948 FOR RELATED INCIDENT.
- [SDR AUS20030948](https://openairdocs.org/sdr/AUS20030948.md): Fire Loop · faulty · Sep 17, 2003 · Boeing 737376 · Fire Detection
  > (AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. NR 1 ENGINE LOOP `B` FAULTY.
- [SDR AUS20030942](https://openairdocs.org/sdr/AUS20030942.md): Warning Light · intermittent · Sep 17, 2003 · Boeing 737376 · Engine Thrust Reverser
  > (AUS) NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATING INTERMITTENTLY.
- [SDR AUS20030858](https://openairdocs.org/sdr/AUS20030858.md): Engine · malfunctioned · Aug 21, 2003 · Boeing 737376 · Engine (Turbine/Turboprop)
  > (AUS) NR 1 ENGINE MOMENTARILY LOST POWER. POWER LOSS NOTED ON ENGINE GAUGES AND AIRCRAFT YAWED. NO REOCCURRENCE DURING FLIGHT. VIBRATION NOTICEABLE AT FLIGHT IDLE.
- [SDR AUS20030866](https://openairdocs.org/sdr/AUS20030866.md): Pump · failed · Aug 10, 2003 · Boeing 737376 · Hydraulic Pump (Electric/Engine), Main
  > (AUS) STANDBY HYDRAULIC PUMP FAILED. PUMP RUNS BUT FAILS TO PRODUCE PRESSURE. SUSPECT FAILED SHAFT.
- [SDR AUS20030829](https://openairdocs.org/sdr/AUS20030829.md): Spar · corroded · Jul 24, 2003 · Boeing 737376 · Wing Spar
  > (AUS) RT WING VENT BOX CORRODED. NR 10 STIFFENER AFT FACE CORRODED IN AN AREA LOCATED BETWEEN WS563 & WS 578 OVER AN AREA APPROX 381MM BY 63.5MM. RT WING UPPER SKIN INNER SURFACE CORRODED BETWEEN WS 557 & 583 IN AN AREA BETWEEN STIFFENER NR 11 & WING REAR SPAR
- [SDR AUS20030761](https://openairdocs.org/sdr/AUS20030761.md): Access Panel · leaking · Jul 20, 2003 · Boeing 737376 · Wing, Plate/Skin
  > (AUS) FUEL LEAKING FROM WING AND RUNNING OVER UPPER SURFACE OF INBOARD FLAPS. INVESTIGATION FOUND THE FUEL LEAKING FROM THE FUEL TANK PANEL ACCESS DOOR AT LOWER WING SKIN CUTOUT NR 7404R LOCATED BETWEEN WBL 157 AND WBL 183.4. THE FUEL TANK CUTOUT HAD BEEN RECE
- [SDR AUS20030714](https://openairdocs.org/sdr/AUS20030714.md): Odor · detected · Jul 15, 2003 · Boeing 737376 · Cabin Cooling System
  > (AUS) FUMES WITH SLIGHT SULPHUR ODOR REPORTED BY CABIN CREW AROUND REAR GALLEY AND REAR CABIN VENTS. DURING INVESTIGATION AND GROUND RUNNING THE EQUIPMENT COOLING EXHAUST FAN FAILED AND THE CIRCUIT BREAKER POPPED.
- [SDR AUS20030727](https://openairdocs.org/sdr/AUS20030727.md): Structure · cracked · Jul 4, 2003 · Boeing 737376 · Cargo/Baggage Doors
  > (AUS) AFT CARGO DOOR OUTER TEE STRUCTURE CRACKED IN AFT LOWER CORNER. CRACK WAS LOCATED BETWEEN TWO FASTENERS. CRACK LENGTH APPROXIMATELY 19.05MM (0.75IN).
- [SDR AUS20030674](https://openairdocs.org/sdr/AUS20030674.md): Pmc · faulty · Jul 3, 2003 · Boeing 737376 · Fuel Controlling System
  > (AUS) NR 2 ENGINE LOW POWER. SUSPECT CAUSED BY FAULTY POWER MANAGEMENT CONTROL (PMC).
- [SDR AUS20030707](https://openairdocs.org/sdr/AUS20030707.md): Door Frame · cracked · Jun 25, 2003 · Boeing 737376 · Fuselage Main, Structure
  > (AUS) DOOR FRAME CRACKED. FORWARD CORNER HAS CRACK INDICATIONS IN FIVEHOLES. AFT CORNER HAS CRACK INDICATION IN ONE HOLE. FOUND DURINGEDDY CURRENT INSPECTION IAW QANTAS ENGINEERING INSTRUCTION733-53-14R4, BOEING SB:737-53-1116 AND CASA AD/B737/24.
- [SDR AUS20030649](https://openairdocs.org/sdr/AUS20030649.md): Sensor · faulty · Jun 22, 2003 · Boeing 737376 · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR FAULTY.
- [SDR AUS20030640](https://openairdocs.org/sdr/AUS20030640.md): Connector · faulty · Jun 13, 2003 · Boeing 737376 · Fire Detection
  > (AUS) RT ENGINE FIRE DETECTION SYSTEM FAULTY. SUSPECT FAULTY CONNECTOR.
- [SDR AUS20030583](https://openairdocs.org/sdr/AUS20030583.md): Sensor · faulty · Jun 4, 2003 · Boeing 737376 · Landing Gear Position and Warning
  > (AUS) MAIN LANDING GEAR AIR SENSOR S106 FAULTY.
- [SDR AUS20030547](https://openairdocs.org/sdr/AUS20030547.md): Warning Light · illuminated · May 26, 2003 · Boeing 737376 · Trailing Flap Position Indicating System
  > (AUS) FLAP ASSYMETRY PROBLEMS. LIMITED INFORMATION PROVIDED.
- [SDR AUS20030545](https://openairdocs.org/sdr/AUS20030545.md): Attach Fitting · cracked · Apr 30, 2003 · Boeing 737376 · Fuselage Main, Attach Fittings
  > (AUS) FUSELAGE FRAME CLEATS CRACKED. SMALL CRACK IN CLEAT AT UPPER AFT FASTENER HOLE IN BS707 STRINGER 10L. FOUND DURING EDDY CURRENT INSPECTION.
- [SDR AUS20030652](https://openairdocs.org/sdr/AUS20030652.md): Bear Strap · cracked · Apr 28, 2003 · Boeing 737376 · Fuselage Main, Structure
  > (AUS) FORWARD GALLEY DOOR CRACKED. SEVEN CRACKS FOUND ON FORWARD UPPER CORNER (BEAR STRAP AND INTERNAL DOUBLER) AND ONE CRACK FOUND ON THE AFT UPPER CORNER (BEAR STRAP DOUBLER). FOUND DURING EDDY CURRENT INSPECTION IAW ENGINEERING INSTRUCTION 737-53-14R4.
- [SDR AUS20030468](https://openairdocs.org/sdr/AUS20030468.md): Indicator · false indication · Apr 20, 2003 · Boeing 737376 · Fuel Quantity Indicator
  > (AUS) NR 1 FUEL GAUGE INDICATING FUEL LEAK. INSPECTION COULD FIND NO EVIDENCE OF LEAKS.
- [SDR AUS20030559](https://openairdocs.org/sdr/AUS20030559.md): Frame · cracked · Apr 11, 2003 · Boeing 737376 · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME BS 400 CRACKED. CRACK LENGTH 10.16MM (0.4IN). FUSELAGE FRAME BS440 CRACKED. CRACK LENGTH 12.7MM (0.5IN). FRAMES CRACKED AT FLANGE BEND RADIUS BETWEEN S-13R AND S-14R. FOUNDDURING EDDY CURRENT INSPECTION IAW EI 733-53-11, BOEING NTM PART 6
- [SDR AUS20030415](https://openairdocs.org/sdr/AUS20030415.md): Connector · loose · Apr 11, 2003 · Boeing 737376 · APU Indicating System
  > (AUS) APU INOPERATIVE, LIGHT FAULTY. INVESTIGATION FOUND BACKSHELL ON CONNECTOR D4934J LOOSE.
- [SDR AUS20030544](https://openairdocs.org/sdr/AUS20030544.md): Frame · cracked · Apr 8, 2003 · Boeing 737376 · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAMES CRACKED AT PSU ATTACHMENT POINTS. A TOTAL OF ELEVEN FRAMES CRACKED ON LT SIDE AND SEVEN FRAMES ON THE RT SIDE. FOUND DURING EDDY CURRENT INSPECTION IAW EI 737-53-61R1.

Next page: https://openairdocs.org/model/boeing-737-376/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = '737376'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-376/reports

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