# Service difficulty reports: Boeing 737-275

A list on [Boeing 737-275](https://openairdocs.org/model/boeing-737-275.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 290 reports

- [SDR CA101028005](https://openairdocs.org/sdr/CA101028005.md): Line · cracked · Oct 27, 2010 · Boeing 737275 · Engine Fuel Distribution
  > (CAN) ENGINE FOUND TO BE LEAKING FUEL BY MAINTENANCE, ENGINE REMOVED FUEL MANIFOLD LINE FOUND TO BE CRACKED UNDER THE SHROUDS, REPLACED THE LINE. ENGINE RE-INSTALLED SERVICEABLE.
- [SDR CA100104005](https://openairdocs.org/sdr/CA100104005.md): Spindle · cracked · Dec 28, 2009 · Boeing 737275 · Trailing Edge Flap Control System
  > (CAN) SPINDLE BROKE IN AREA OF AD 2003-24-08 PRIOR TO THE INSP THRESHOLD OF 3000C. UNIT HAD BEEN O/H, FAILED PART IS CURRENTLY WITH QA AND WILL BE SHIPPED TO MFG UNLESS OTHERWISE INSTRUCTED. FLAP SPINDLE CRACK OCCURRED AT CRITICAL "A" AREA SPECIFIED IN ASB 73
- [SDR CA091002004](https://openairdocs.org/sdr/CA091002004.md): Accumulator · out of tolerance · Jun 20, 2009 · Boeing 737275 · Hydraulic System, Main
  > (CAN) PART WAS INSTALLED WHEN NOT IN COMPLIANCE WITH AD 2003-11-03 THIS AD EFFECTIVE O3-JULY-03 STATES THAT PN 2660 472M2 MAY NOT BE INSTALLED ON ANY ACFT.
- [SDR CA090106006](https://openairdocs.org/sdr/CA090106006.md): Hydraulic System · malfunctioned · Jan 2, 2009 · Boeing 737275 · Hydraulic System, Main
  > (CAN) WHILE ON THE TAXI FROM MX HANGAR TO THE TERMINAL, THE TAXI CREW APPLIED THE BRAKES WITH NO EFFECT. THE ACFT WAS SHUT DOWN. THE AMM WAS CONSULTED, AND REMOVED A HYDRAULIC CASE DRAIN FILTER, AND FOUND THE FILTER TO BE COMPLETED BLOCKED WITH ICE. IT IS P
- [SDR CA080208006](https://openairdocs.org/sdr/CA080208006.md): Nose Bullet · separated · Dec 30, 2007 · Boeing 737275 · Engine Air Intake System
  > (CAN) FOLLOWING DEPARTURE, THE CREW REPORTED COMPRESSOR STALLING OF THE NR 1 ENG AT CLIMB PWR. THE ENGINE PWR WAS REDUCED AND COMPRESSOR STALLS STOPPED. THE AC RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT. INSP OF THE ENGINE IDENTIFIED THAT THE NR 1 ENGINE N
- [SDR CA050504006](https://openairdocs.org/sdr/CA050504006.md): Controller · inoperative · May 3, 2005 · Boeing 737275 · Cabin Pressure Controller
  > (CAN) ON DEPARTURE, A/C WAS CLIMBING THROUGH FL210 WHEN THE CREW NOTICED THE CABIN DIFFERENTIAL WAS AT MAXIMUM AND THE CABIN RATE OF CLIMB WAS EXCEEDING 3000 FPM (UP). THEY IMMEDIATELY INITIATED A RAPID DESCENT AND STABILIZED THE CABIN ALTITUDE AT AN A/C ALTI
- [SDR CA041013010](https://openairdocs.org/sdr/CA041013010.md): Actuator · cracked · Oct 13, 2004 · Boeing 737275 · Spoilers
  > (CAN) A SYSTEM HYDRAULIC LIGHTS ILLUMINATED, A SYSTEM QTY READ ZERO. NR 8 SPOILER ACTUATOR FOUND CRACKED. ACTUATOR REPLACED MM 27-62-91. CARRIED OUT RII INSPECTION.
- [SDR CA040819003](https://openairdocs.org/sdr/CA040819003.md): Fitting · cracked · Jul 29, 2004 · Boeing 737275 · Landing Gear Door Actuator
  > (CAN) CRACKED FITTING FOUND DURING CPCP INSPECTION. RT MAIN LANDING GEAR ACTUATORS WING LINK FORWARD ATTACH FITTING (TO WING REAR SPAR ATTACH).
- [SDR CA030704004](https://openairdocs.org/sdr/CA030704004.md): Light · failed · Jul 3, 2003 · Boeing 737275 · Exterior Lighting
  > (CAN) WHILE CLIMING THROUGH 23,000 FT. THEY EXPERIENCED A RAPID DEPRESSURIZATION, LOSS OF CABIN PRESSURE (O2 MASKS WERE DONNED BY FLT CREW). CREW MANUALLY CLOSED OUTFLOW VALVE HOWEVER AIRCRAFT WOULD NOT PRESSURIZE. CREW REQUESTED DESCENT AND RETURN TO BASE - N
- [SDR CA030527002](https://openairdocs.org/sdr/CA030527002.md): Bypass Valve · malfunctioned · May 23, 2003 · Boeing 737275 · Engine Oil Indicating System
  > (CAN) ON TOP OF CLIMB NR 1 ENGINE OIL FILTER BY-PASS CAME ON STEADY. CHECK LIST WAS PERFORMED AND LIGHT REMAINED ON. ENGINE SHUT DOWN HAD TO BE COMPLETED AS PER QRH, AIRCRAFT RETURNED TO TORONTO.
- [SDR CA030331004](https://openairdocs.org/sdr/CA030331004.md): Line · leaking · Mar 25, 2003 · Boeing 737275 · Turbine Engine Oil System
  > (CAN) ON DEPARTURE, OIL QUANTITY ON NR 2 ENGINE AT OR NEAR ZERO AS THEY PASSED THROUGH 300 FT. CREW ELECTED TO CONTINUE FLT & MONITOR. PASSING THROUGH 22,000 FT. OIL PRESSURE STARTED TO FLUCTUATE, CREW IMMEDIATELY CONDUCTED ENG SHUTDOWN CHECKLIST. A/C RET
- [SDR CA030204001](https://openairdocs.org/sdr/CA030204001.md): Control Panel · smoke · Feb 2, 2003 · Boeing 737275 · Instrument System Wiring
  > (CAN) AT 33000 FT, SMOKE WAS NOTICE COMING FROM THE OVERHEAD COCKPIT FUEL PANEL P5-2. PUMPS SELECTED OFF. DECLARED AN EMERGENCY LANDING. REPLACED PANEL.
- [SDR CA021213001](https://openairdocs.org/sdr/CA021213001.md): Static Inverter · Dec 5, 2002 · Boeing 737275 · AC Inverter
  > (CAN) DATE OF REMOVAL NOV 25/02 DATE OF ARRIVAL IN SHOP SNAG DESCRIPTIONWHEN CONDUCTING W/C 12010 ITEM 8 B737 DAILY CHECK,STNDBY PWR CHECK AC VOLT METER FULL DEFLECTING RIGHT 130 VOLTS. #1 AND 2 AUTO XFMR C/B POPPED AND CADC AC & 26VAC C/BS POPPED, UNABLE TO
- [SDR CA030103022](https://openairdocs.org/sdr/CA030103022.md): Static Inverter · malfunctioned · Nov 26, 2002 · Boeing 737275 · AC Inverter
  > (CAN) WHEN CONDUCTING AN EMERGENCY POWER CHECK THE AC VOLT METER WENT FULL DEFLECTION TO 130 VOLTS. NR 1 AND 2 AUTO TRANFORMER C/B POPPED AND CADC AC AND 26 VAC C/B'S POPPED. SHOP REPORT CONFIRMED THE FAULT THAT THE INVERTER WAS PUTTING OUT 155 VAC. THIS WAS
- [SDR CA021115011](https://openairdocs.org/sdr/CA021115011.md): Engine · failed · Nov 11, 2002 · Boeing 737275 · Turbine Engine Compressor Section
  > (CAN) DURING TAKEOFF AT HIGH SPEED, CREW EXPERIENCED TWO BANGS. TAKEOFF REJECTED AT 140 KNOTS. NR 2 ENGINE REPLACED AND HIGH ENERGY STOP INSPECTION CARRIED OUT AS PER MM 05-51-11 PARA D.
- [SDR CA020830022](https://openairdocs.org/sdr/CA020830022.md): Engine · vibration · Aug 23, 2002 · Boeing 737275 · Engine (Turbine/Turboprop)
  > (CAN) RT ENGINE VIBRATION FELT FROM TOP OF DESCENT TO LANDING. NR 2 FUEL LEVER VIBRATING AND DURING TAXI WHEN POWER ADDED. TURBINE VIBRATION GOES UP TO 2.5 TO 3.
- [SDR CA020826007](https://openairdocs.org/sdr/CA020826007.md): Fuel Control · failed · Aug 16, 2002 · Boeing 737275 · Fuel Control/Turbine Engines
  > (CAN) ON LANDING ENGINE 1 AND 2 ONLY GO INTO IDLE REVERSE. UNABLE TO PULL ANY REVERSE POWER. NR 1 ENGINE FCU REPLACED AND CHECKED SERVICEABLE AS PER AMM.
- [SDR CA020731009](https://openairdocs.org/sdr/CA020731009.md): Controller · malfunctioned · Jun 30, 2002 · Boeing 737275 · Windshield/Door Rain/Ice Removal
  > (CAN) OUTER PANE OF F/O,S NR 1 FORWARD WINDOW CRACKED AND DELAMINATED WHILE CRUSING AT 330. ALTITUDE REDUCED, DIFFERENTIAL REDUCED AS PRECAUTION. F/O,S WINDOW AND HEAT CONTROLLER REPLACED AS PER AMM.
- [SDR CA020610005](https://openairdocs.org/sdr/CA020610005.md): Gasper Fan · failed · Jun 9, 2002 · Boeing 737275 · Air Distribution Fan
  > (CAN) WHILE BOARDING PAX. SMOKE STARTED ENTERING CABIN IN MID-CABIN RIGHT SIDE AREA.(L1251724)PAX. DEPLANED VIA FWD ENTRY DOOR. FOUND GASPER FAN CONNECTOR & FUSILAGE INSULATION BLANKET BURNT. REPLACED AIR COND. MODULE & CIRCUIT BREAKER AS PER STANDARD PRACTICE
- [SDR CA020606002](https://openairdocs.org/sdr/CA020606002.md): Keelbeam · corroded · Jun 5, 2002 · Boeing 737275 · Fuselage Main, Keel
  > (CAN) FUSELAGE SKIN BULGED AND SUSPECT CORROSION RT KEELBEAM STA 520 STR 28 RT ALSO RIVETS HEADS SHEARED AND LOOSE STA 480 TO STA 520 (M1121878) SKIN CUT AND CORROSION REMOVED AS PER SRM 53-30-3 FIG 1.KEELBEAM STA 520 STR 28 RT WITHIN LIMITS AFTER CORROSION RE
- [SDR CA020725009](https://openairdocs.org/sdr/CA020725009.md): Engine · failed · Jun 2, 2002 · Boeing 737275 · Engine (Turbine/Turboprop)
  > (CAN) ON DEPARTURE FROM OTTAWA, CLIMBING THROUGH FL 270 TO 280, A LOUD BANG WAS HEARD AND A SHUDDER CAME FROM NR 1 ENGINE, POWER WAS REDUCED AND ENGINE WAS SHUT DOWN, OTHER THAN FLUCTUATING VIBRATION, OTHER PARAMETERS NORMAL.NUMBER ONE ENGINE REPLACED. MORE
- [SDR CA020531005](https://openairdocs.org/sdr/CA020531005.md): Engine · failed · May 31, 2002 · Boeing 737275 · Turbine Section
  > (CAN) PRELIMINARY REPORT, NR 1 ENGINE SHUT DOWN, ENGINE STARTED ROUGH WITH VIBRATION, ANTI-SELECTED OFF WITH NO CHANGE,AIRCRAFT LANDED WITHOUT ANY INCIDENT. FOUND ENGINE TURBINE DAMAGED
- [SDR CA020528011](https://openairdocs.org/sdr/CA020528011.md): Circuit Breaker · failed · May 22, 2002 · Boeing 737275 · AC Generation System
  > (CAN) ON DESCENT LOST THE NR 2 AND 3 TRANSFORMER RECTIFIERS, ONE FUEL PUMP ON THE NR 1 TANK AND BOTH FUEL PUMPS ON THE NR 2 TANK ALSO F/O'S INSTRUMENTS AND NR 2 RADIO. CREW NOTICED SLIGHT ELECTRICAL SMELL AND ON BASE LEG THE TRANSFER BUS LIGHT CAME ON. CAPTA
- [SDR CA020507001](https://openairdocs.org/sdr/CA020507001.md): Transformer · malfunctioned · May 1, 2002 · Boeing 737275 · AC Generation System
  > (CAN) DURING FLIGHT NUMEROUS MOMENTARY POWER INTERUPTION CAUSING AUTO PILOT TO DISENGAGE AND NUMEROUS INSTRUMENT WARNING FLAGS. FOUND TO BE THE NR 1 ENGINE CURRENT TRANSFORMER AT FAULT. TRANSFORMER REPLACED. AIRCRAFT TIME 53656HRS
- [SDR CA020502017](https://openairdocs.org/sdr/CA020502017.md): Fuel Control · failed · Apr 10, 2002 · Boeing 737275 · Fuel Control/Turbine Engines
  > (CAN) 1ST ATTEMPT AT TAKEOFF NR 1 ENGINE STALLED AT APPROXIMATELY 1,70 EPR.RETURNED TO RAMP FOR MAINTENANCE (MAINTENANCE CHECKED AIRCRAFT SERVICEABLE). 2ND ATTEMPT TAKOFF NR 1 ENGINE STALLED TWICE BETWEEN V1 AND GEAR UP. IN BOTH CASES WHILE NR 1 ENGINE ACCELER
- [SDR CA020502018](https://openairdocs.org/sdr/CA020502018.md): Window · failed · Apr 4, 2002 · Boeing 737275 · Flight Compartment Windows
  > (CAN) ON GROUND FOUND FIRST OFFICER NR 4 WINDOW SHATTERED. RELACED NR 4 WINDOW.
- [SDR CA020426004](https://openairdocs.org/sdr/CA020426004.md): Latch · failed · Apr 3, 2002 · Boeing 737275 · Passenger Oxygen System
  > (CAN) CABIN OXYGEN PSUS NR 9 RT AND NR 14 RT, NO FLOW FOUND DURING FUNCTIONAL TEST. BOTH UNITS ARE FROM THE SAME BATCH NR. BATCH NR 99795 REPLACED LATCH ASEMBLIES.
- [SDR CA020315006](https://openairdocs.org/sdr/CA020315006.md): Panel · sheared · Jan 29, 2002 · Boeing 737275 · Trailing Edge Flaps
  > (CAN) PRIOR TO DEPARTURE, FLAPS EXTENDED FOR SREVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS.FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01
- [SDR CA020308010](https://openairdocs.org/sdr/CA020308010.md): Panel · sheared · Jan 29, 2002 · Boeing 737275 · Vertical Stabilizer, Plate/Skin
  > (CAN) FLAPS EXTENDED FOR SERVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS.FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01. AIRCRAFT FERRIED F
- [SDR CA020104009](https://openairdocs.org/sdr/CA020104009.md): Engine · stalled · Dec 6, 2001 · Boeing 737275 · Fuel Control/Turbine Engines
  > (CAN) ON TAKE OFF OUT OF WHITEHORSE, FLIGHT CREW EXPERIENCED COMPRESSOR STALL. ENGINE THROTTLE BACK TO IDLE, ENGINE NORMAL, ADVANCED THROTTLE AND STALLED AGAIN. FLIGHT CREW ELECTED TO RETURNED TO WHITEHORSE. ENGINE TRIM RUN CARRIED OUT. IDLE AND EPR ADJUS
- [SDR CA020104012](https://openairdocs.org/sdr/CA020104012.md): Gyro · failed · Nov 30, 2001 · Boeing 737275 · Attitude Gyro and Indicating System
  > (CAN) ON TAKE OFF FROM EDMONTON, ELECTRICAL SPIKE MOMENTARILY FLAG CAPT.'S ADI AUTOPILOT, WHEN SELECTED ON TRIPPED, TRIED ONE MORE TIME AND WITH LIGHT PRESSURE ON ELEVATOR ON AUTOPILOT TRIPPED AGAIN. NUMBER 1 VERTICAL GYRO AND AIR DATA COMPUTER REPLACED. SYSTE
- [SDR CA010905007](https://openairdocs.org/sdr/CA010905007.md): Module · shorted · Aug 15, 2001 · Boeing 737275 · Landing Gear Position and Warning
  > (CAN) ON LANDING IN YHZ LOWER PANEL CAUTION LIGHTS CAME ON & WOULD NOT EXTINGUISH. FOUND SCREW SHORTING TERMINAL OF LANDING GEAR WARNING INDICATION MODULE SOCKET. REMOVED SCREW AND CHECKED INDICATION SYSTEM & ASSOCIATED SYSTEMS. ALL INDICATIONS & OPEATIONS NO
- [SDR CA010906019](https://openairdocs.org/sdr/CA010906019.md): Valve · failed · Jul 29, 2001 · Boeing 737275 · Engine Start Valves/Controls
  > (CAN) TWO AIR TURN BACK DUE TO A #1 START VALVE OPEN LIGHT ILLUMINATED DURING FLIGHT. ACCOMPLISHED #1 ENGINE FAILURE SHUTDOWN TWICE.AFTER THE FIRST INCIDENT, THE STARTER, START VALVE AND ACTUATOR PRESSURE SWITCH WERE CHANGED, & THE SECOND TIME THE START VALVE
- [SDR CA010622013](https://openairdocs.org/sdr/CA010622013.md): Controller · malfunctioned · May 22, 2001 · Boeing 737275 · Cabin Pressure Controller
  > (CAN) AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE IN STANDBY MODE. FLIGHT RETURNED.CABIN PRESSURZATION CONTROLLER REPLACED.
- [SDR CA010522005](https://openairdocs.org/sdr/CA010522005.md): Duct · separated · May 6, 2001 · Boeing 737275 · Airfoil Anti/De-ice System
  > (CAN) ON CLIMB NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. THRUST REDUCED AND LIGHT EXTINGUISHED. RETURNED. MAINTENANCE INSPECTION FOUND RIGHT ANTI-ICE DUCT SEPARATED FROM ANTI-ICE VALVE. DUCT REPLACED GROUND RUN, SYSTEM CHECKED SERVICEABLE.
- [SDR CA010522006](https://openairdocs.org/sdr/CA010522006.md): Case · cracked · May 1, 2001 · Boeing 737275 · Hydraulic System, Main
  > (CAN) AFTER TAKEOFF TRAILING EDGE FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS RETRACTED. FLIGHT CONTINUED, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED TRAILING EDGE FLAP BYPASS VALVE MALFUNCTIONING. VALVE REPLACED. SUBSEQUENT VAL
- [SDR CA010404010](https://openairdocs.org/sdr/CA010404010.md): Control Unit · leaking · Mar 22, 2001 · Boeing 737275 · Aileron Control System
  > (CAN) DURING FLIGHT A SYSTEM HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP, AT A RATE OF 1 GALLON PER HOUR. DUE TO POOR WEATHER ELECTED TO DIVERT. GEAR EXTENDED NORMALLY AND QUANTITY REMAINED STEADY. FLIGHT LANDED WITHOUT INCIDENT. FOUND A SYSTEM AILERON POWER CONTR
- [SDR CA010313023](https://openairdocs.org/sdr/CA010313023.md): Strut · bent · Mar 7, 2001 · Boeing 737275 · Landing Gear Door Retract Section
  > (CAN) ON TAKEOFF WHEN THE GEAR WAS SELECTED UP THE CREW HEARD A BANG FOLLOWED BY A LOUD NOISE AND ACCOMPANIED BY A VIBRATION IN THE AIRFRAME. THE CREW ELECTED TO RETURN. UPON LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE NOSE GEAR ATTACH
- [SDR CA010301022](https://openairdocs.org/sdr/CA010301022.md): Wire · failed · Feb 16, 2001 · Boeing 737275 · Ice/Rain Protection System Wiring
  > (CAN) IN CRUISE, LT ELEVATOR PITOT HEAT SYSTEM INDICATED HEATER SYSTEM UNSERVICEABLE. DUE TO WEATHER CONCERNS DIVERTED. REPAIRED WIRING TO LT PITOT TUBE.
- [SDR CA010105003](https://openairdocs.org/sdr/CA010105003.md): Transmitter · failed · Dec 27, 2000 · Boeing 737275 · Engine Pressure Ratio (EPR)
  > (CAN) EPR INDICATION UNSERVICEABLE. REPLACED INDICATOR AND TRANSMITTER. A/C RETURNED TO SERVICE.
- [SDR CA001214004](https://openairdocs.org/sdr/CA001214004.md): Fire Detector · failed · Dec 1, 2000 · Boeing 737275 · Fire Detection
  > (CAN) ON CLIMBOUT FROM YVR, CREW SAW A MOMENTARY FLASH OF NR 1 ENGINE FIRE HANDLE LIGHT. IT BECAME INTERMITTENT AS CLIMB CONTINUED. CREW ELECTED TO RETURN, REQUESTED CFR ON ARRIVAL. AFTER CLEARANCE TO RETURN RECEIVED AND DESCENT STARTED, FIRE HANDLE WARNING LI
- [SDR CA001214002](https://openairdocs.org/sdr/CA001214002.md): Switch · failed · Nov 29, 2000 · Boeing 737275 · Leading Edge Slat Control System
  > (CAN) TOP OF CLIMB, NR 3 SLAT INTRANSIT LIGHT ON OVERHEAD PANEL AND LEADING EDGE FLAP INTRANSIT LIGHT ON, FORWARD PANEL, INTERMITTENTLY, WITH ASSOCIATED MINOR AIRFRAME VIBRATION. FLIGHT RETURNED. REPLACED NR 3 SLAT ACTUATOR RODEND SWITCH ASSEMBLY, SYSTEM CHECK
- [SDR CA001201010](https://openairdocs.org/sdr/CA001201010.md): Check Valve · leaking · Nov 9, 2000 · Boeing 737275 · Hydraulic System, Main
  > (CAN) NR 2 ''A'' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WHEN FLAPS SELECTED. DECLARED AN EMERGENCY, LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TOWED FROM RUNWAY. FOUND ''A'' SYSTEM HYDRAULIC TANK PRESSURE LEAKING FROM SERVICING PORT. CHECK VALVE CL
- [SDR CA000901007](https://openairdocs.org/sdr/CA000901007.md): Indicator · failed · Aug 15, 2000 · Boeing 737275 · Integrated Flight System
  > (CAN) IN CRUISE CAPTAINS HORIZONTAL SITUATION INDICATOR STOPPED TURNING WHEN AIRCRAFT WAS IN A TURN. COMPARATOR LIGHT CAME ON. RETURNED. CAPTAINS HSI REPLACED.
- [SDR CA000901005](https://openairdocs.org/sdr/CA000901005.md): Filter · obstructed · Aug 14, 2000 · Boeing 737275 · Engine Fuel Distribution
  > (CAN) A/C 741, AUGUST 14/2000, FLT 906, YYC, LOG SEQUENCE 0281117. ENGINES WERE ACCELERATED FOR TAKEOFF AND NR 2 ENGINE COMPRESSOR STALL OCCURRED. TAKEOFF WAS ABANDONED AT 15 KNOTS. AIRCRAFT RETURNED TO RAMP. MAINTENANCE REQUESTED ENGINE TO BE RUN. ENGINE STAL
- [SDR CA000731003](https://openairdocs.org/sdr/CA000731003.md): Splice · overheated · Jul 23, 2000 · Boeing 737275 · AC Generator-Alternator
  > (CAN) SEVERAL RPTS OF REJECTED TAKEOFFS, DUE TO NR 1 GEN DROPPING OFF LINE & LEADING EDGE DEVICES INTRANSIT LIGHT ILLUMINATING. INSP FOUND, NR 1 ENGINE GEN AL TO CU SPLICE OVERHEATED. SPLICE LOCATED AT WING STATION WBL 157, ABOVE ENGINE ELECT. DISCONNECTS IN D
- [SDR CA000804015](https://openairdocs.org/sdr/CA000804015.md): Tire · failed · Jul 22, 2000 · Boeing 737275 · Tire
  > (CAN) CREW REPORTED LOUD BANG FROM NOSE WHEEL AREA ON TAKEOFF ROLL AND JUST BEFORE ROTATION. THEY ALSO NOTICED SOMEHTING GO PAST THE WINDSCREEN. A FLY PAST THE CONTROL TOWER AND DEBRIS FOUND ON THE RUNWAY CONFIRMED TREAD SEPARATION FROM ONE OF THE NOSE WHEEL T
- [SDR CA000718006](https://openairdocs.org/sdr/CA000718006.md): Circuit Breaker · failed · Jul 9, 2000 · Boeing 737275 · AC Generation System
  > (CAN) NEARING TOP OF CLIMB, CIRCUIT BREAKERS BEGAN TO TRIP. FUEL PUMP CIRCUIT BREAKERS FOR LEFT SIDE, TCAS, STALL WARNING, EQUIPMENT COOLING, WINDOW ANTI-ICE, RADIO ALTIMETER. RETURNED TO YUL, NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. REPLACED NR 1 GENER
- [SDR CA000731004](https://openairdocs.org/sdr/CA000731004.md): Connector · loose · Jul 5, 2000 · Boeing 737275 · Fire Detection
  > (CAN) ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND FIRE AND OVERHEAT E
- [SDR CA000718008](https://openairdocs.org/sdr/CA000718008.md): Connector · loose · Jul 5, 2000 · Boeing 737275 · Fire Detection
  > (CAN) 85 MILES OUT OF MEM, NR 2 ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED TO MEM. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INC

Next page: https://openairdocs.org/model/boeing-737-275/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 = '737275'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-275/reports

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