# Service difficulty reports: Boeing 737-242C

A list on [Boeing 737-242C](https://openairdocs.org/model/boeing-737-242c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 60 reports

- [SDR CA151027006](https://openairdocs.org/sdr/CA151027006.md): Bellcrank · sheared · Oct 9, 2015 · Boeing 737242C · Cargo/Baggage Doors
  > (CAN) DURING OFFLOADING/LOADING OF CARGO ON 08 OCTOBER 2015, CAPTAIN REPORTED THAT MAIN CARGO DOOR LIFT ACTUATOR BELLCRANK ASSY WAS BROKEN/SHEARED. CREW STATED THAT THE FAILURE WAS NOTICED WHEN THE DOOR WAS OPEN WHILE THERE WAS WIND PRESENT, THAT WAS 5 KNOTS
- [SDR CA140408002](https://openairdocs.org/sdr/CA140408002.md): Indicator · failed · Apr 6, 2014 · Boeing 737242C · Trailing Flap Position Indicating System
  > (CAN) T/E FLAP SYS STALLING AND LOCKOUT TROUBLESHOOTING CARRIED OUT. T/E FLAP ASSEMBLIES INCLUDING TRACKS AND ROLLERS INSPECTED FOR DAMAGE, NO FAULTS FOUND. FLAP POSITION INDICATOR REPLACED AND ACFT RELEASED PENDING SATISFACTORY TEST FLIGHT. TEST FLIGHT CAR
- [SDR CA140110009](https://openairdocs.org/sdr/CA140110009.md): Slat Track · damaged · Jan 8, 2014 · Boeing 737242C · Leading Edge Devices
  > (CAN) DURING A POST C-CHECK TEST FLIGHT THE CREW WAS FLYING THE ACFT AT 16,000FT, WHEN THEY PERFORMED AN ALTERNATE FLAP EXTENSION TEST. THE ACFT DID EXTEND THE FLAPS AND SLATS PROPERLY. THE CREW RETRACTED THE FLAPS IN A NORMAL CONFIGURATION. THEN THEY DEPLOYE
- [SDR CA130719005](https://openairdocs.org/sdr/CA130719005.md): Engine · shutdown · Jul 19, 2013 · Boeing 737242C · Engine (Turbine/Turboprop)
  > (CAN) AIRCRAFT HAD UN-COMMANDED SHUTDOWN OF ENGINE NR 1 ON ROTATION. EMERGENCY WAS DECLARED. ACFT LANDED SAFELY, BUT WAS OVERWEIGHT AT TIME OF LANDING.
- [SDR CA130325004](https://openairdocs.org/sdr/CA130325004.md): Pcu · separated · Mar 22, 2013 · Boeing 737242C · Aileron Control System
  > (CAN) DURING ROUTINE MAINTENANCE, WITH "B" PUMPS ON AND HYDRAULIC INTERCONNECT "OPEN" TO LOWER THE FLAPS, WHEN NORMAL OPERATING PRESSURE WAS REACHED IMMEDIATE LOSS OF HYDRAULIC PRESSURE WAS NOTICED ALONG WITH MASSIVE AMOUNTS OF HYDRAULIC FLUID GUSHING OUT OF T
- [SDR CA100713016](https://openairdocs.org/sdr/CA100713016.md): Window · cracked · Jul 9, 2010 · Boeing 737242C · Flight Compartment Windows
  > OUTER PANE CRACKED DURING FLIGHT, WINDOW REPLACED AND TEMP CONTROLLER SENT TO BE CHECKED, IF THERE WAS AN ISSUE WITH THE TEMP CONTROLLER SDR WILL BE UPDATED.
- [SDR CA090313006](https://openairdocs.org/sdr/CA090313006.md): Strut · low · Mar 12, 2009 · Boeing 737242C · Nose/Tail Landing Gear Strut/Axle
  > (CAN) FOLLOWING DEPARTURE, THE CREW OBSERVED A FAIL TO RETRACT INDICATION ON THE NOSE GEAR. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MX FOUND A LOW OLEO PRESSURE CONDITION. THE OLEO WAS SERVICED AND THE ACFT WAS RETURNED TO
- [SDR CA061011009](https://openairdocs.org/sdr/CA061011009.md): Actuator · bypassing · Oct 4, 2006 · Boeing 737242C · Wheel/Ski/Float
  > (CAN) DURING DEPARTURE THE NOSE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR GRAVEL DEFLECTOR ACTUATOR WAS BYPASSING. THE UNIT WAS REPLACED AND THE AIRCRAFT REURNE
- [SDR CA061004003](https://openairdocs.org/sdr/CA061004003.md): Actuator · bypassing · Oct 2, 2006 · Boeing 737242C · Landing Gear Actuator
  > (CAN) ON CLIMB OUT THE NOSE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THAT THE NOSE LANDING GEAR GRAVEL DEFLECTOR ACTUATOR HAD FAILED. THE ACTUATOR WAS REPLACED AND THE AIRCE
- [SDR CA060725002](https://openairdocs.org/sdr/CA060725002.md): Fuel Control · malfunctioned · Jul 21, 2006 · Boeing 737242C · Fuel Control/Turbine Engines
  > (CAN) ENROUTE THE CREW ELECTED TO RETURN TO POINT OF DEPARTURE DUE TO A SUSPECTED ENGINE VIBRATION. AFTER ARRIVING, THE MAINTENANCE PERSONNEL INITIALLY REPLACED THE FORWARD ENGINE MOUNT ISOLATORS WITH NO APPARENT REMEDY OF THE PROBLEM. THE FCU WAS REPLACED AND
- [SDR CA060220002](https://openairdocs.org/sdr/CA060220002.md): Skin · cracked · Feb 16, 2006 · Boeing 737242C · Fuselage Main, Plate/Skin
  > DURING THE PREFLIGHT INSPECTION 2 CRACKS WERE OBSERVED IN THE FUSELAGE SKIN. BOTH DEFECTS WERE APPROXIMATELY 2 INCHES IN LENGTH. THE LOCATION IS ESTIMATED TO BE BS 750 STR 19/20. THE AIRCRAFT IS CURRENTLY OUT OF SERVICE FOR REPAIR.
- [SDR CA050121003](https://openairdocs.org/sdr/CA050121003.md): Quick Disconnect · failed · Jan 14, 2005 · Boeing 737242C · Pitot/Static System
  > (CAN) AC ENCOUNTERED AUTOPILOT, STATIC AIR TEMP INDICATION ANOMALIES. AUTOPILOT PITCH, ROLL COMPUTERS ALONG WITH 3 AIR DATA COMPUTERS (ADC). FOUND PITOT LINE QUICK DISCONNECT TO ADC HAD FAILED. INTERNAL BARREL THAT OPENS PITOT LINE TO ADC HAD FAILED. LINE SE
- [SDR CA030923009](https://openairdocs.org/sdr/CA030923009.md): Skin · cracked · Sep 19, 2003 · Boeing 737242C · Fuselage Main, Plate/Skin
  > (CAN) WHILE LOOKING AT FUSELAGE ON THE LT SIDE,THE TECHNICIAN WAS QUESTIONNING WHAT SEEM TO BE A SCRATCH MARK. AFTER FURTHER INVESTIGATION AND INTERIOR LINING REMOVAL,IT WAS DISCOVERED THAT THE SCRATCH WASINDEED A CRACK IN THE FUSELAGE LOCATED AT FUSELAGE STA
- [SDR CA030923008](https://openairdocs.org/sdr/CA030923008.md): Beam · cracked · Sep 19, 2003 · Boeing 737242C · Fuselage Main, Bulkhead
  > (CAN) WHILE PERFORMING SB 737-53A1173 (INSPECTION OF THE VERTICAL BEAMS AT STATION 178 PRESSURE BULKHEAD) THE FOLLOWING DEFECTS WERE FOUND, VERTICAL BEAM WEB CRACKED AT BS178 RBL 5.7 WL 1832-VERTICAL BEAM WEB CRACKED AT BS 178 RBL 17.1 WL 230 BOTH CRACKS WERE
- [SDR CA030923007](https://openairdocs.org/sdr/CA030923007.md): Flap Track · cracked · Sep 19, 2003 · Boeing 737242C · Trailing Edge Flaps
  > (CAN) WHILE PERFORMING AD 2002-05-07 (BOEING SB737-57A1249), THE RT SIDE FLAP TRACK POSITION NR 7 WAS FOUND CRACKED. TRACK WAS REPLACED.
- [SDR CA030620006](https://openairdocs.org/sdr/CA030620006.md): Line · misinstalled · Jun 19, 2003 · Boeing 737242C · Hydraulic System, Main
  > (CAN) FLT CREW REPORTED THAT NLG UNLOCKED BUT FAILED TO RETRACT. SUBSEQUENT GEAR SELECTS WERE UNSUCCESSFUL UNTIL SPEED REDUCED. GEAR DID RETRACT AT 160 KNOTS IAS, VERY SLOW, RETURN TO YEG. THIS ANOMALY DATES BACK TO 06/4/03, WHEN SKI ACTUATOR ROBBED TO SERV
- [SDR CA010403010](https://openairdocs.org/sdr/CA010403010.md): Bearing · broken · Feb 19, 2001 · Boeing 737242C · Trailing Edge Flaps
  > (CAN) DURING TAXI, FLAPS SELECTED WITH INDICATION PROBLEM. AIRCRAFT RETURNED TO GATE. FURTHER INVESTIGATION FOUND RT FLAP CARRIAGE BEARINGS WAS BROKEN IN 2 PIECES AND A SECOND BEARING SPLIT. NEW PARTS INSTALLED AND FLAP RIGGING CARRIED OUT I.A.W. MM. NO FURTHE
- [SDR CA010320019](https://openairdocs.org/sdr/CA010320019.md): Filter · clogged · Feb 6, 2001 · Boeing 737242C · Engine Oil Distribution (Airframe Furnished)
  > (CAN) DURING TAKEOFF NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED. REJECTED TAKEOFF CARRIED AND AIRCRAFT RETURNED TO GATE. NR 2 ENGINE BYPASS REMOVED AND FOUND CLOGGED. NEW FILTER INSTALLED AND LEAK CHECK CARRIED OUT. SERVICEABLE. NO FURTHER INCIDENT DURING SUB
- [SDR CA010320020](https://openairdocs.org/sdr/CA010320020.md): Pump · failed · Feb 2, 2001 · Boeing 737242C · Engine Fuel Pump
  > (CAN) DURING TAKEOFF, NR 1 ENGINE FAILED. REJECTED TAKEOFF ACCOMPLISHED. A/CSECURED AND AIRCRAFT RETURNED TO GATE. H.P. PUMP AND FCU CHANGED I.A.W. 73-11-1, TRIM RUNS AND LEAK CHECK CARRIED OUT I.A.W. 71-09-00. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.
- [SDR CA010117007](https://openairdocs.org/sdr/CA010117007.md): Pin · backed out · Nov 30, 2000 · Boeing 737242C · Landing Gear Position and Warning
  > (CAN) LANDING GEAR WOULD NOT RETRACT & CONFIGURATION HORN SOUNDED AT TAKEOFF. A/C RETURNED AS PER QRH PROCEDURE. MAIN R/H LANDING GEAR OLEO SERVICED. ON SUBSEQUENT FLIGHT, L/R GEAR SHOWED RED. GEAR SELECTED DOWN 3 GREEN. L/G ACCESSORY UNIT CHANGED. A/C TEST FL
- [SDR CA000830040](https://openairdocs.org/sdr/CA000830040.md): Connector · contaminated · Aug 9, 2000 · Boeing 737242C · Alternator-Generator Drive
  > (CAN) NR1 CSD IN TEMP ROSE TOWARDS 160 DEGREES WITH POWERED UP TO 80% TAKEOFF. FOUND MAIN CONNECTOR AT RIGHT SIDE OF CSD CONTAMINATED WITH OIL. THE CONNECTOR WAS CLEANED AND ENGINE GROUND RUN CARRIED OUT. SYSTEM CHECK SERVICEABLE. NO FUTHER ABNORMALITIES REPO
- [SDR CA000830036](https://openairdocs.org/sdr/CA000830036.md): Hydraulic Line · ruptured · Jul 27, 2000 · Boeing 737242C · Hydraulic System, Main
  > (CAN) LOSS OF HYDRAULIC FLUID DURING DESCENT AND LANDING. NR2 ENGINE THRUST REVERSER PRESSURE LINE WAS FOUND RUPTURED IN PYLON UNDER A SUPPORT CLAMP.HYDRAULIC PUMP AND FILTER WERE CHECKED FOR CONTAMINATION AND FOUND SERVICEABLE. HYDRAULIC LINE REPLACED AS PER
- [SDR CA000808017](https://openairdocs.org/sdr/CA000808017.md): Coupling · broken · Jul 6, 2000 · Boeing 737242C · APU Core Engine
  > (CAN) AFTER LANDING AND TAXIING AIRCRAFT, APU WAS STARTED & FIRE HANDLE ILLUMINATED & AUDIBLE WAS HEARD. CREW PULLED APU FIRE HANDLE & EMPTY THE APU FIRE BOTTLE. ON FURTHER INVESTIGATION, THE COUPLING FOR THE COMBUSTION LINER BROKE. COUPLING WAS REPLACED. FIRE
- [SDR CA000802021](https://openairdocs.org/sdr/CA000802021.md): Control Panel · missing · Jul 4, 2000 · Boeing 737242C · Fluid Service Doors
  > (CAN) DURING WALK AROUND IT WAS OBSERVED THAT THE RT INBOARD FUEL BOOST PUMP PANEL WAS MISSING. PANEL AREA TAPED. PANEL FASTENERS CAME LOOSE DUE TO VIBRATION AND AIRSPEED. PANEL WAS POSSIBLY LOST IN FLIGHT. PART REPLACED.
- [SDR CA000706004](https://openairdocs.org/sdr/CA000706004.md): Tire · missing · Jun 25, 2000 · Boeing 737242C · Tire
  > (CAN) AIRCRAFT ON TAKEOFF, REPORTED TIRE DEBRIS ON RUNWAY. MAINTENANCE ADVISED, UNABLE TO DETERMINE FLT, LANDING, CREW REQUESTED CFR, DUE POTENTIAL TIRE PROBLEMS. FLIGHT LANDED WITHOUT INCIDENT. INSPECTION FOUND TIRE CAP MISSING FROM LEFT INBOARD WHEEL. DAMAG
- [SDR CA000516034](https://openairdocs.org/sdr/CA000516034.md): Wheel · cracked · May 1, 2000 · Boeing 737242C · Wheel/Ski/Float
  > (CAN) WHILE TAXING MAINT NOTED NR 2 MAIN WHEEL ASSY WAS FLAT. FURTHER INVESTIGATION REVEALED 1/3 OF THE OUTBOARD WHEEL HALF HAD BROKEN OFF AND THE TIRE WAS CUT AT THE WALL EDGE. DAMAGE WAS FOUND ON THE WING BODY FAIRING, LT IB FORE FLAP AND THE LT UPPER WING T
- [SDR CA000501018](https://openairdocs.org/sdr/CA000501018.md): Wire · overheated · Apr 15, 2000 · Boeing 737242C · Electrical Power System Wiring
  > (CAN) PRIOR TO PASS BOARDING WHILE FLIGHT ATTENDANTS PREPARED THE CABIN FOR FLIGHT SMOKE AND ARCING WAS NOTICED COMING FROM THE REAR OF THE AIRCRAFT GALLEY COFFEE MAKER CB PANEL. ELECTRICAL POWER WAS REMOVER FROM THE AIRCRAFT GALLEY AND THE FIRE EXTINGUISHER F
- [SDR CA000501020](https://openairdocs.org/sdr/CA000501020.md): Sensor · intermittent · Apr 11, 2000 · Boeing 737242C · Leading Edge Slat Position Indicating System
  > (CAN) ON TAXI CREW OBSERVED LE SLAT IN TRANSIT LIGHT STILL ON. NR 4 LE SLAT PROXIMITY SENSOR REPLACED. SYS SERVICEABLE.
- [SDR CA000501019](https://openairdocs.org/sdr/CA000501019.md): Fire Loop · chafed · Apr 11, 2000 · Boeing 737242C · Fire Detection
  > (CAN) ON CLIMB CREW OBSERVED ON INTERMITTENT NR 2 ENG FIRE WARNING ILLUMINATION. A/C RETURNED. WIRE UNDER RT ENGINE ANTI SLAVE FOUND CHAFED. WIRE REPAIRED. CRUSH WASHERS UNDER FIRE LOOP CONNECTORS MISSING, REPLACED. FIRE LOOP TOUCHING LOWER COWL, REPOSITIONED.
- [SDR CA000331006](https://openairdocs.org/sdr/CA000331006.md): Fuel Control · out of rig · Mar 26, 2000 · Boeing 737242C · Fuel Controlling System
  > (CAN) ENGINE RIGGING DIFFICULTY.
- [SDR CA000313001](https://openairdocs.org/sdr/CA000313001.md): Proximity Switch · dirty · Mar 10, 2000 · Boeing 737242C · Landing Gear Retraction/Extension System
  > (CAN) NLG WOULD NOT RETRACT AFTER TAKEOFF. NLG RECYCLED NO FIX A/C LANDED. SLUSH IN GEAR GRAVEL DEFLECTOR, PROXIMITY SWITCH DIRTY, CLEANED AND SERVICEABLE.
- [SDR CA000308004](https://openairdocs.org/sdr/CA000308004.md): Unknown · odor · Feb 21, 2000 · Boeing 737242C · Air Distribution System
  > (CAN) BURNING SMELL IN COCKPIT ON ARRIVAL. FOUND LOOSE AND OVERHEATED ELECTRICAL TERMINAL STUD IN THE P18-3 PANEL. NEW TERMINALS INSTALLED A/C SERVICEABLE.
- [SDR CA000215032](https://openairdocs.org/sdr/CA000215032.md): Skin · cracked · Feb 3, 2000 · Boeing 737242C · Fuselage Main, Plate/Skin
  > (CAN) CRACK FOUND AT WL 234 RT 4TH AND 7TH RIVET STARTING OUTBOARD. REPAIRED.
- [SDR CA991116011](https://openairdocs.org/sdr/CA991116011.md): Plate · missing · Nov 4, 1999 · Boeing 737242C · Engine Oil Cooler
  > (CAN) PLATE SEPARATED FROM CSD OIL COOLER AT START UP.THIS WAS AN ACESS PANEL WE RE THE HINGED PORTION HAD BROKEN ALLOWING SEPARATION.
- [SDR CA991116023](https://openairdocs.org/sdr/CA991116023.md): Line · leaking · Nov 3, 1999 · Boeing 737242C · Hydraulic System, Main
  > (CAN) LOSS OF ALL NR 2 HYDRAULIC FLUID IN-FLIGHT. PIN HOLE IN LINE AT PYLON UNDER CLAMP. REPLACED NR 2 HYDRAULIC PUMP AND CASE DRAIN FILTER REPLACED.
- [SDR CA990916016](https://openairdocs.org/sdr/CA990916016.md): Interphone · short · Aug 27, 1999 · Boeing 737242C · Interphone/Passenger Announcement (PA) System
  > (CAN) DURING CLIMB, CREW HEARD RINGING CHIME AND THE CALL LIGHT WAS FLASHING INTERMITTENTLY. SMELL OF SMOKE WAS NOTICED FROM THE 3R COMMUNICATION PANEL AT R2 DOOR. WHEN DOOR OPENED, A SMALL FLAME WAS PRESENT ON THE ELECTRICAL PLUG OF THE PASSENGER ADDRESS IN
- [SDR CA990818013](https://openairdocs.org/sdr/CA990818013.md): Fitting · leaking · Aug 7, 1999 · Boeing 737242C · Engine Oil Indicating System
  > (CAN) O-RING FAILURE AT OIL PRESSURE TRANSMITTER TO MAIN OIL FILTER.
- [SDR CA990219030](https://openairdocs.org/sdr/CA990219030.md): Wire · broken · Feb 3, 1999 · Boeing 737242C · Engine Fuel System Wiring
  > (CAN) FUEL HEAT VALVE OPEN LIGHT ON NR 2 ENGINE REMAINED BRIGHT BLUE AFTER ENGINE START. AFTER CONSULTING MAINTENANCE, IT WAS DECIDED THAT THE VALVE HAD FAILED IN THE CLOSED POSITION. A/C OPERATED ON MEL FOR CLOSED VALVE. AFTER TAKEOFF, THE OIL TEMPERATURE
- [SDR CA990219028](https://openairdocs.org/sdr/CA990219028.md): O-Ring · worn · Feb 1, 1999 · Boeing 737242C · Trailing Edge Flap Control System
  > (CAN) LOSS OF A-SYSTEM HYDRAULIC QUANTITY. LEAK IN FLAP SELECTOR FLOW REGULATOR, SEAL REPLACED.
- [SDR CA990310046](https://openairdocs.org/sdr/CA990310046.md): Indicator · faulty · Jan 4, 1999 · Boeing 737242C · Engine Pressure Ratio (EPR)
  > (CAN) AIRCRAFT ABORTED TAKEOFF DUE TO NR 1 ENGINE EPR INDICATOR STUCK AT 1.6. THE EPR INDICATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR CA981230039](https://openairdocs.org/sdr/CA981230039.md): Accessory Unit · failed · Dec 12, 1998 · Boeing 737242C · Landing Gear Position and Warning
  > (CAN) THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED STEADY. AIRCRAFT RETURNED. LANDING GEAR ACCESSORY UNIT REPLACED PER M.M. NLG FLIGHT TO GROUND SWITCH ADJUSTED. AIRCRFAFT RETURNED TO SERVICE.
- [SDR CA980623023](https://openairdocs.org/sdr/CA980623023.md): Computer · contaminated · Jun 15, 1998 · Boeing 737242C · Autopilot Computer
  > (CAN) FLT INSTRUMENT ACCY, YAW DAMPER COUPLER, A/P ACCESSORY UNIT, A/P SWITCHING UNIT, INSTRUMENT AMPLIFIER, COMPASS RACK, STEERING COMPUTER WERE REPLACED DUE TO INGRESS OF WATER IN AVIONIC BAY. DURING CRUISE, AUTOPILOT ALTITUDE HOLD TRIPPED OFF FOLLOWED BY R
- [SDR CA971216028](https://openairdocs.org/sdr/CA971216028.md): Plate · cracked · Mar 17, 1998 · Boeing 737242C · Horizontal Stabilizer, Plate/Skin
  > (CAN) TRAILING EDGE OF HORIZONTAL STABILIZER BEAM ASSY CRACKED ON FORWARD EDGE OF THE COVER PLATE ALONG THE RADIUS IN 4 LOCATIONS. THE LONGEST CRACK WAS APPROX 2 INCHES LONG. BEAM LENGTH IS 12 FEET. THE RADIUS SHOULD BE.25 INCH RADII AND WAS ONLY.10 INCH R
- [SDR CA971231021](https://openairdocs.org/sdr/CA971231021.md): Skin · delaminated · Dec 12, 1997 · Boeing 737242C · Ailerons
  > (CAN) RIGHT AILERON UPPER SURFACE OUTER END APPROXIMATELY ONE SQUARE FOOT DELAMINATED. REPLACED. AIRCRAFT TT: 70,002 HOURS.
- [SDR CA970902019](https://openairdocs.org/sdr/CA970902019.md): Transmission · failed · Aug 14, 1997 · Boeing 737242C · Trailing Edge Flap Control System
  > (CAN) NR7 FLAP WOULD NOT FULLY RETRACT, HELD UP AT 10 DEGREES, BINDING INTERNALLY. TRANSMISSION REPLACED.
- [SDR CA970815004](https://openairdocs.org/sdr/CA970815004.md): Line · leaking · Aug 11, 1997 · Boeing 737242C · Hydraulic System, Main
  > (CAN) ON TAXI 'B' HYDRAULIC SYSTEM LOW PRESSURE LIGHT ON AND FLUID QUANTITY DROPPED TO 1.5 GALLONS. 'B' PUMPS TURNED OFF. EXTERNAL OBSERVER REPORTED MASSIVE LEAK. NR1 BRAKE LINE LEAKING. REPLACED.
- [SDR CA970807004](https://openairdocs.org/sdr/CA970807004.md): Gyro · inoperative · Aug 5, 1997 · Boeing 737242C · Directional Gyro and Indicating System
  > (CAN) NR1 COMPASS FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO BLOCKS. GYRO REPLACED.
- [SDR CA970618005](https://openairdocs.org/sdr/CA970618005.md): Terminal Strip · shorted · Jun 11, 1997 · Boeing 737242C · Landing Gear Position and Warning
  > (CAN) AIRCRAFT RETURNED TO BLOCKS DUE TO NOSE GEAR GREEN LIGHT INDICATED ON WITH NOSE GEAR UP AND LOCKED. TERMINAL STRIP T252 SHORTED TO GROUND. REPAIRED.
- [SDR CA970529006](https://openairdocs.org/sdr/CA970529006.md): Wheel Assembly · broken flange · May 16, 1997 · Boeing 737242C · Wheel/Ski/Float
  > (CAN) AFTER ARRIVAL #3 MAIN WHEEL FOUND MISSING A PIECE OF THE OUTBOARD FLANGE. REPLACED.
- [SDR CA970528005](https://openairdocs.org/sdr/CA970528005.md): Sensor · intermittent · May 15, 1997 · Boeing 737242C · Landing Gear Position and Warning
  > (CAN) ON TAKEOFF NO NOSE GEAR GREEN LIGHT. AIRCRAFT LANDED THEN FERRIED FOR REPAIR. NOSE GEAR DOWN LOCK SENSOR REPLACED.

Next page: https://openairdocs.org/model/boeing-737-242c/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 = '737242C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-242c/reports

---
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