# Service difficulty reports: Boeing 737-217

A list on [Boeing 737-217](https://openairdocs.org/model/boeing-737-217.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 308 reports

- [SDR CA140908023](https://openairdocs.org/sdr/CA140908023.md): Overheat Loop · open · Sep 7, 2014 · Boeing 737217 · Overheat Detection
  > (CAN) AT THE TOP OF DECENT, OUR ACFT ILLUMINATED AN ENGINE OVERHEAT INDICATION ON NR 1 ENGINE. THE CREW FOLLOWED THEIR NON-NORMAL CHECKLIST WHICH SAID TO RETURN THE ENGINE TO IDLE, WHICH IT ALREADY WAS, CUT FUEL TO THE ENGINE AND FIRE THE BOTTLE. THE OVERHEA
- [SDR CA140806001](https://openairdocs.org/sdr/CA140806001.md): Line · leaking · Aug 1, 2014 · Boeing 737217 · Engine Bleed Air System
  > (CAN) 1 ENGINE OVERHEAT ILLUMINATED. SHUTDOWN NR 1 ENGINE BOTH EXTINGUISHER BOTTLES DISCHARGED. UPON INVESTIGATION MAINTENANCE FOUND NR 1 ENGINE, 13TH STAGE BLEED AIR AND MODULATING VALVE SENSE LINE, PN BACH7D0137DD, BRAIDED HOSE ASSY LEAKING BLEED AIR ONTO
- [SDR CA110520002](https://openairdocs.org/sdr/CA110520002.md): Window · broken · May 17, 2011 · Boeing 737217 · Flight Compartment Windows
  > DURING CRUISE, THE FLIGHT CREW REPORTED THAT THE OUTER PANE OF THE L-1 WINDOW HAD SHATTERED. THE ACFT RETURNED TO POINT OF DEPARTURE, WHERE THE WINDOW WAS REPLACED.
- [SDR CA100526002](https://openairdocs.org/sdr/CA100526002.md): Gearbox · leaking · May 25, 2010 · Boeing 737217 · Turbine Engine Accessory Drive
  > ENGINE WAS LEAKING OIL FROM AROUND THE BANJO FITTING, ENGINE APPROX 70HRS SINCE SHOP VISIT - GEARBOX TO BE REPLACED. THIS IS A PRELIMINARY REPORT ONLY
- [SDR CA090514001](https://openairdocs.org/sdr/CA090514001.md): Window · cracked · May 11, 2009 · Boeing 737217 · Flight Compartment Windows
  > (CAN) DURING CRUISE AT 35,000, THE NR 4 WINDOW CRACKED, CREW DESCENDED TO 14,000 AND CONTINUED THE FLIGHT. WINDOW WAS REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA100215002](https://openairdocs.org/sdr/CA100215002.md): Gcu · smoke · Apr 22, 2009 · Boeing 737217 · AC Generator-Alternator
  > (CAN) DURING ENGINE START THE GCU STARTED TO SMOKE, THE CREW REMOVED THE GCU, MX INSTALLED A SERVICEABLE GCU. (TC 20100215002)
- [SDR CA090323005](https://openairdocs.org/sdr/CA090323005.md): Turbine · failed · Mar 22, 2009 · Boeing 737217 · Turbine Section
  > (CAN) AFTER TAKEOFF, THE CREW OBSERVED A SUDDEN LOSS OF POWER ON NR 2 ENGINE COINCIDENT WITH AN UNUSUAL VIBRATION AND NOISE. THE CREW CARRIED OUT AN INFLIGHT SHUTDOWN OF NR 2 ENGINE. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER DIFFICULTY
- [SDR CA080630001](https://openairdocs.org/sdr/CA080630001.md): Engine · failed · May 22, 2008 · Boeing 737217 · Engine (Turbine/Turboprop)
  > (CAN) - ON DESCENT, A "BUZZING" SOUND WAS HEARD IN THE FLIGHT DECK FOR APPROX 5-10 SEC. THIS WAS FOLLOWED BY 1 OR 2 "POPS" AND THEN A LOUD "BANG" AT WHICH TIME THE NR 2 ENGINE LOST THRUST. NR 2 ENG TEMP CLIMBED BUT THERE WAS NO ENG OVERHEAT OR FIRE WARNING. A
- [SDR CA080121003](https://openairdocs.org/sdr/CA080121003.md): Wire · inoperative · Jan 2, 2008 · Boeing 737217 · Navigation System Wiring
  > (CAN) TAIL 523 ON JAN 2ND APPROACH BACK COURSE ON RWY 15 YELLOWKNIFE 1040FT ASL 350FT AGL LEVEL FLIGHT 140K IN THIS CASE THE FLIGHT CREW EXPERIENCED A TAWS GENERATED A PICTORIAL DISPLAYED IMPACT WARNING. THE CREW WAS IN VISUAL CONDITIONS AND SAW NO DANGER OF
- [SDR CA070911003](https://openairdocs.org/sdr/CA070911003.md): Valve · malfunctioned · Sep 7, 2007 · Boeing 737217 · Fuel Heater
  > (CAN) APPROXIMATELY 25 MINUTES AFTER DEPARTING, THE CREW OBSERVED THE NR 1 ENGINE OIL TEMPERATURE CLIMBING THROUGH THE YELLOW BAND. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE NR 1 FUEL HEAT VALVE AND CONDU
- [SDR CA060829004](https://openairdocs.org/sdr/CA060829004.md): Bearing · seized · Aug 5, 2006 · Boeing 737217 · Elevator Control System
  > (CAN) AIRCRAFT ENCOUNTERED INTERMITTENT REPEAT SNAGS FOR STIFF ELEVATOR MOVEMENT. FINAL RECTIFICATION CAME ON AUGUST 5 2006 WHEN THE REFERENCED BEARING AND RETAINER WERE REPLACED. REFERENCED BEARING WAS FOUND SEIZED. CURRENT MAINTENANCE PROGRAM WAS REVIEWE
- [SDR CA040625004](https://openairdocs.org/sdr/CA040625004.md): Actuator · inoperative · Jun 24, 2004 · Boeing 737217 · Leading Edge Slat Actuator
  > (CAN) NR 6 LEADING EDGE SLAT WAS SLOW TO RETRACT ON DEPARTURE. AFTER IT DID RETRACT IT RE-EXTENDED FOR ABOUT 5 MINUTES THEN RETRACTED AGAIN. CREW WAS ALERTED BY SLAT INDICATION OF THE REDEPLOYMENT AND VISUALLY CONFIRMED THE EXTENSION AND RETRACTION. NO OTHER A
- [SDR CA040519014](https://openairdocs.org/sdr/CA040519014.md): Actuator · failed · May 18, 2004 · Boeing 737217 · Drag Control Actuator
  > (CAN) DURING TAXI TO GATE LOSS OF NOSE WHEEL STEERING OCCURRED WITH TOTAL LOSS OF HYDRAULIC A PRESSURE AND QUANTITY AT ZERO. MAINTENANCE FOUND THE NR 8 GROUND SPOILER ACTUATOR TO BE THE CAUSE. THE ACTUATOR BODY HAD STRUCTURAL FAILURE CAUSING FLUID LOSS. ACTU
- [SDR CA040510004](https://openairdocs.org/sdr/CA040510004.md): Ring · damaged · May 7, 2004 · Boeing 737217 · Engine Fuel Distribution
  > HAVE HAD SEVERAL OCCURRENCES OF FUEL LEAKS FROM THE JT8D FUEL FLOW TRANSMITTERS. THE LEAKS ARE EVIDENT AT VERY HIGH POWER SETTINGS. A FLEET CAMPAIGN HAS BEEN COMPLETED WHICH CHECKED ALL ENGINES FOR LEAKS AND RECTIFIED DEFECTS. AN EXTENSIVE INVESTIGATION IS BE
- [SDR CA031218008](https://openairdocs.org/sdr/CA031218008.md): Fitting · broken · Dec 12, 2003 · Boeing 737217 · Trailing Edge Flaps
  > (CAN) ON WALK AROUND, MAINTENANCE FOUND THE RT OB FOREFLAP OB LINK BROKEN. MAINTENANCE REPLACED THE FOREFLAP AND AIRCRAFT RETURNED TO SERVICE. CAUSE UNKNOWN. WILL UPDATE IF ADDITIONAL INFORMATION AVAILABLE.
- [SDR CA031027005](https://openairdocs.org/sdr/CA031027005.md): Module · failed · Oct 25, 2003 · Boeing 737217 · Hydraulic System, Main
  > (CAN) ON DECENT NR1 A SYS LOW PRESSURE LIGHT ILLUMINATED. SHORTLY, NR 2 A SYS LOW PRESSURE LIGHT ILLUM. CREW ACCOMPLISHED QRH FOR LOSS OF SYS A. EMERGENCY DECLARED & LANDED. MAINT CHECKED SERVICEABLE HYD SYS RES STANDPIPE & PRESSURE. ENG RAN AND HYD PRESSURE S
- [SDR CA031015003](https://openairdocs.org/sdr/CA031015003.md): Link · broken · Oct 7, 2003 · Boeing 737217 · Landing Gear Door Retract Section
  > (CAN) A LOUD BANG WAS HEARD UPON GEAR RETRACTION. ONCE GEAR WAS RETRACTED A STRONG VIBRATION WAS FELT. WHEN GEAR EXTENTED, VIBRATION WENT AWAY. RETURNED TO YYC FOR A NORMAL LANDING. RT NOSE LANDING GEAR DOOR DOG LINK FOUND BROKEN. LINK REPLACED, SWING CARRIED
- [SDR CA030929006](https://openairdocs.org/sdr/CA030929006.md): Actuator · malfunctioned · Sep 28, 2003 · Boeing 737217 · Drag Control Actuator
  > (CAN) ON CLIMB OUT THE AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC SYSTEM A FLUID. AIRCRAFT TURNED BACK TO YUL AND LANDED WITHOUT INCIDENT. THE NR 3 SPOILER ACTUATOR WAS FOUND TO BE THE CAUSE OF THE FLUID LEAK.ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SER
- [SDR CA030805001](https://openairdocs.org/sdr/CA030805001.md): Landing Light · fire · Aug 2, 2003 · Boeing 737217 · Exterior Lighting
  > (CAN) DURING TROUBLESHOOTING OF AN OUTBOARD (LT HAND) LANDING LIGHT SNAG MAINTENANCENOTICED SMOKE ODOR IN THE COCKPIT AND THEN SEVERAL C/BS POPPED. MAINTENANCE SHUT ALL AIRCRAFT POWER DOWN. SMOKE WAS NOTICED BY MAINTENANCE COMING FROM THE LT PYLON AREA FWD. P
- [SDR CA030318018](https://openairdocs.org/sdr/CA030318018.md): Actuator · leaking · Mar 15, 2003 · Boeing 737217 · Drag Control Actuator
  > (CAN) DURING CRUISE THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID. THE AIRCRAFT WAS DIVERTED TO WHERE EMERGENCY VEHICLES MET THE AIRCRAFT ON LANDING.THE LOSS OF FLUID WAS ATTRIBUTED TO THE NR 2 FLIGHT SPOILER ACTUATOR. THE ACTUATOR IS BEING TESTED AND ASS
- [SDR CA030321011](https://openairdocs.org/sdr/CA030321011.md): Control Unit · misoverhauled · Feb 26, 2003 · Boeing 737217 · Stabilizer Control System
  > (CAN) UNSCHEDULED REMOVAL OF RUDDER PCU, OCCURRED ON FEB 25/26/2003 WAS IN RESPONSE TO A REQUEST FROM MATERIAL SERVICES BASED ON A FAA UNAPPROVED PARTS NOTIFICATION NR 2001-0089 DATED AUG 12,2002. SUSPECT PCU P/N 1U1150-3 S/N 737 WAS LISTED IN THE NOTIFICATION
- [SDR CA030224004](https://openairdocs.org/sdr/CA030224004.md): Apu · failed · Feb 19, 2003 · Boeing 737217 · APU Core Engine
  > (CAN) PRIOR TO PUSH BACK, AIRCRAFT RAPIDLY FILLED CABIN WITH SMOKE, AIRCRAFT DEPLANNED. CAUSED BY THE BLEED FROM THE APU (BURNED OIL CONTAMINATION) APU CHANGED AND COLLESTER BAGS REPLACED. AC SERVICEABLE
- [SDR CA030221010](https://openairdocs.org/sdr/CA030221010.md): Cooling Fan · unsecure · Feb 19, 2003 · Boeing 737217 · APU Core Engine
  > (CAN) JUST BEFORE PUSH BACK, CABIN RAPIDLY FILLED WITH SMOKE (NON ELECTRICAL IN NATURE). A/C WAS DEPLANED VIA THE LOADING BRIDGE AND SHUT DOWN TO BATTERY. MAINT FOUND THE APU OIL TANK EMPTY AND INLET PLENUM CONTAMINATED WITH OIL. FOUND APU COOLING FAN HAD DE
- [SDR CA030205011](https://openairdocs.org/sdr/CA030205011.md): Strut · overserviced · Jan 20, 2003 · Boeing 737217 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) AFTER TAKE OFF, NOSE GEAR DID NOT STOW. OLEO DID NOT EXTEND FULLY OR MADE CONTACT WITH SNUBBERS. THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. GEAR WAS CYCLED WAS NORMAL. MAINT FIRST CHECKED NOSE OLEO SERVICING AND DISCOVERED OLEO TO BE OVERSERV
- [SDR CA030108011](https://openairdocs.org/sdr/CA030108011.md): Warning System · activated · Jan 6, 2003 · Boeing 737217 · Fire Detection
  > (CAN) DURING CRUISE, THE APU FIRE DETECT LIGHT FLICKERED 3 TIMES. MAINTENANCE GROUND TESTED, NO FAULTS FOUND AND AIRCRAFT RELEASED FOR SERVICE.THE NEXT DAY THE APU FIRE DETECT LIGHT CAME ON BEFORE LANDING. AFTER LANDINGTHE APU FIRE LIGHT AND BELL CAME ON AND T
- [SDR CA030107016](https://openairdocs.org/sdr/CA030107016.md): Computer · failed · Jan 5, 2003 · Boeing 737217 · Speed-Attitude Correction System
  > (CAN) MACH TRIM LIGHT CAME ON IN FLIGHT, CREW REPORTED ELEVATOR FEEL INOPERATIVE. AIRCRAFT RETURNED TO DEPARTURE STATION. ELEVATOR FEEL COMPUTER REPLACED AS PER AMM. AND OPERATION CHECKED SERVICEABLE.
- [SDR CA021227005](https://openairdocs.org/sdr/CA021227005.md): Cam · damaged · Dec 12, 2002 · Boeing 737217 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) UPON ARRIVAL IN YEG, THE NOSE OLEO WAS FOUND LOW AND LEAKING FLUID. AIRCRAFT HAD SOME HISTORY OF HARD BOTTOMING SNAGS. AFTER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE NOSE GEAR REQUIRED DIASSEMBLY FOR A SEAL CHANGE. AIRCRAFT WAS FERRIED TO YVR FOR
- [SDR CA020904007](https://openairdocs.org/sdr/CA020904007.md): Isolation Valve · malfunctioned · Sep 4, 2002 · Boeing 737217 · Engine Bleed Air System
  > (CAN) BOTH ENGINE SURGING AT CRUISE, BLEED SURGING FROM 20PSI TO 52 PSI. NR 2 ENGINE SURGING CONSIDERABLY MORE ON DESCENT.
- [SDR CA020806008](https://openairdocs.org/sdr/CA020806008.md): Engine · failed · Jul 27, 2002 · Boeing 737217 · Engine (Turbine/Turboprop)
  > (CAN) WHEN ADDING THRUST FOR T/O, HEARD LOUD BANG AND NOTICED PARAMETERS DROPPING. SHUT DOWN AND SECURED NR 2 ENGINE. NR 2 ENGINE AND T/R REPLACED AS PER AMM
- [SDR CA020731016](https://openairdocs.org/sdr/CA020731016.md): Actuator · failed · Jul 13, 2002 · Boeing 737217 · Leading Edge Slat Actuator
  > (CAN) L/E FLAP TRANSIT ON AFTER T/O. NR 5 RT WING SLAT FULLY EXTENDED FOR APPROX 2 MIN. WHEN IT RETRACTED AND BEFORE WE RECYCLED THE FLAPS. REPLACED NR 5 SLAT ACTUATOR AS PER AMM. SYSTEM CHECKED SERVICEABLE AND CERTIFIED.
- [SDR CA020726007](https://openairdocs.org/sdr/CA020726007.md): Indicator · failed · Jun 17, 2002 · Boeing 737217 · Weather Radar System
  > (CAN) 30 MINUTES AFTER DEPARTURE, ELECTRICAL BURNING SMELL IN COCPIT, AIRCRAFT LANDED SAFELY, BURNING SMELL ORIGINATED BY WEATHER RADAR INDICATOR. INDICATOR REPLACED.
- [SDR CA020801010](https://openairdocs.org/sdr/CA020801010.md): Indicator · failed · Jun 16, 2002 · Boeing 737217 · Weather Radar System
  > (CAN) FLIGHT WAS DIVERTED DUE TO BURNING SMELL IN COCKPIT FROM WEATHER RADAR INDICATOR. UNIT WAS REPLACED AND SHOP REPORT INDICATED CAUSE OF PROBLEM WAS BURNED OUT DIODES ON RECTIFIER AND FILTER ASSY.
- [SDR CA020725014](https://openairdocs.org/sdr/CA020725014.md): Adc · failed · Jun 13, 2002 · Boeing 737217 · Air Data Computer
  > (CAN) AUTOPILOT ENGAGED IN CRUISE,UNABLE TO UNFREEZE MANUALLY,LEFT WING LEVEL TO A SLIGHT RIGHT BANK. AILERON CONTOL LOST-FROZEN TILL AUTO PILOT RELEASED.CENTRAL AIR DATA COMPUTER REPLACED P/N HG480B13 S/N P-529
- [SDR CA020228001](https://openairdocs.org/sdr/CA020228001.md): Adc · failed · Feb 17, 2002 · Boeing 737217 · Air Data Computer
  > (CAN) JUST AFTER TAKEOFF CAPTAINS AIRSPEED, STANDBY AIRSPEED, GROUND PROX WARNING, AND MACH TRIM INDICATORS FAILED. AIRCRAFT RETURNED TO AIRPORT. NR 1 CENTRAL AIR DATA COMPUTER REPLACED AND OPERATION CHECKED SERVICEABLE.
- [SDR CA020215007](https://openairdocs.org/sdr/CA020215007.md): Arm · dislodged · Jan 28, 2002 · Boeing 737217 · Leading Edge Devices
  > (CAN) MAINTENANCE FOUND NR 2 SLAT FOUND PROTRUDING 4 INCHES ON ONE SIDE ON WALKAROUND CHECK. SLAT MECHANISM FOUND OFF GUIDE TRACK. FLIGHT PERMIT (SPECIFIC PURPOSE, FERRY FLIGHT) ISSUED AND AIRCRAFT FLOWN TO BASE FOR REPAIRS. NR 2 LEADING EDGE SLAT DETENT ARM
- [SDR CA020110002](https://openairdocs.org/sdr/CA020110002.md): Transmitter · failed · Dec 24, 2001 · Boeing 737217 · Engine Oil Pressure
  > (CAN) ENGINE NR 1 OIL PRESSURE DROPPED TO 20 PSI AFTER TAKEOFF. ENGINE FAILURE AND SHUT DOWN COMPLETED. AIRCRAFT RETURNED TO VANCOUVER. OIL PRESSURE TRANSMITTER REPLACED.
- [SDR CA020104010](https://openairdocs.org/sdr/CA020104010.md): Gasper Fan · seized · Dec 7, 2001 · Boeing 737217 · Air Distribution Fan
  > (CAN) AIRCRAFT ENROUTE FROM SAN FRANSISCO TO VANCOUVER, DIVERTED TO KLAMATH FALLS OREGON, DUE SMOKE IN THE CABIN. SMOKE DISIPATED WHEN GASPER FAN SELECTED OFF. GASPER FAN FOUND SEIZED. GASPER FAN REPLACED.
- [SDR CA020121008](https://openairdocs.org/sdr/CA020121008.md): Spar · cracked · Nov 15, 2001 · Boeing 737217 · Elevator, Spar/Rib
  > (CAN) RT ELEVATOR REAR SPAR AT TRIM TAB ATTACHMENT POINT FOUND CRACKED. ELEVATOR REMOVED FOR REPAIR, LOCATION OF DAMAGED LOCATED AT STATION 66.54 REPLACED ELEVATOR. DAMAGE REPAIRED AS PER SRM
- [SDR CA011121010](https://openairdocs.org/sdr/CA011121010.md): Accessory Unit · failed · Nov 6, 2001 · Boeing 737217 · Landing Gear Actuator
  > (CAN) SHORTLY AFTER TAKEOFF OUT OF YYC, THE CREW EXPERIENCED DIFFICULTY GETTING THE LANDING GEAR LEVER TO REMAIN IN THE 'UP' POSTION. THE CREW PERFORMED THE 'NON-NORMAL CHECKLIST', BUT WERE UNABLE TO RECTIFY THE PROBLEM. THE CREW ELECTED TO RETURN TO YYC AN
- [SDR CA011114011](https://openairdocs.org/sdr/CA011114011.md): Selector Valve · failed · Sep 28, 2001 · Boeing 737217 · Landing Gear Selector
  > (CAN) LOUD NOISE AND ALL 3 GEAR INDICATION LIGHTS BOTH GREEN AND RED ILLUMINATED. A/C RETURNED TO YQR, LANDING GEAR EXTENDED AND ALL INDICATION NORMAL. RIGGING CHECK CARRIED OUT ALL NORMAL. LANDING GEAR SELECTOR VALVE REPLACED. LANDING GEAR SWING CARRIED OUT A
- [SDR CA011019010](https://openairdocs.org/sdr/CA011019010.md): Selector Valve · failed · Sep 28, 2001 · Boeing 737217 · Landing Gear Selector
  > (CAN) AFTER NORMAL TAKEOFF, GEAR IN OFF POSITION, LIGHTS OUT, AT 29,000 FT. SPEED AT 290-300 LANDING GEAR CAME DOWN WITH THREE GREEN LIGHTS, AIR DID AN AIR TURN BACK TO REGINA. FOUND TO BE THE SELECTOR VALVE AT FAULT. LANDING GEAR SELECTOR VALVE REPLACED.
- [SDR CA011114010](https://openairdocs.org/sdr/CA011114010.md): Controller · failed · Sep 27, 2001 · Boeing 737217 · Cabin Pressure Controller
  > (CAN) PRESSURE CONTROLLER FAILED ON CLIMB OUT FROM YYC. A/C RETURNED TO YYC. O2 MASKS DEPLOYED. CABIN PRESSURE CONTROLLER FAILED FUNCTION TEST ON GROUND. REPLACED O2 MASKS AND REPLACED PRESSURE CONTROLLER. FUNCTION CHECK CARRIED OUT AND A/C RETURNED TO SERVICE
- [SDR CA010906010](https://openairdocs.org/sdr/CA010906010.md): Oven · failed · Aug 14, 2001 · Boeing 737217 · Buffet/Galleys
  > (CAN) FORWARD GALLEY OVEN BURNING SMELL. OVEN REPLACED.
- [SDR CA010522003](https://openairdocs.org/sdr/CA010522003.md): Generator · failed · May 22, 2001 · Boeing 737217 · AC Generator-Alternator
  > (CAN) 20 MINUTES AFTER DEPARTURE, APU GENERATOR DROPPED OFF LINE. RETURNED DUE #2 CSD WAS ON MEL. REPLACED #2 GENERATOR AND CSD AS PER WORK CARDS 1177-2 AND 1182-2. GROUND RUNUP COMPLETED, APU AND NR 2 GENERATOR CHECKED SERVICEABLE.
- [SDR CA010423002](https://openairdocs.org/sdr/CA010423002.md): Gcu · failed · Apr 13, 2001 · Boeing 737217 · AC Regulator
  > (CAN) NR 1 ENGINE GENERATOR FAILED INBOUND, NR 1 GENERATOR CONTROL PANEL REPLACED AS PER WORK CARD.
- [SDR CA010404007](https://openairdocs.org/sdr/CA010404007.md): Engine · vibration · Mar 12, 2001 · Boeing 737217 · Engine (Turbine/Turboprop)
  > (CAN) A/C 722, MAR 12/2001, YQX, LOG SEQUENCE 0295200. TOP OF DESCENT WHEN THRUST LEVERS RETARDED, NR 2 ENGINE VIBRATION WAS INDICATING 2 MILS ON INLET AND 3.5 ON TURBINE. NR 2 START LEVER WAS VIBRATING. TRIED ENGINE ANTI-ICE AND THROTTLE MOVEMENT, WITH NO CHA
- [SDR CA010105006](https://openairdocs.org/sdr/CA010105006.md): Housing · broken · Jan 3, 2001 · Boeing 737217 · Drag Control Actuator
  > (CAN) DURING INSPECTION, 17C CHECK OF NR 4 GROUND SPOILER, SPOILER FOUND TO BE LOOSE. FOUND NR 4 SPOILER ACTUATOR, BODY END THAT ENCLOSED THE BEARING, BROKEN AWAY. ACTUATOR REPLACED AS PER WORK CARD 51160.
- [SDR CA001201006](https://openairdocs.org/sdr/CA001201006.md): Engine · failed · Nov 13, 2000 · Boeing 737217 · Engine (Turbine/Turboprop)
  > (CAN) A/C 723, NOV 13/2000, FLT 7012, YFC, LOG SEQUENCE 0298768. ON LANDING YFC, WITH REVERSE THRUST SELECTED, A BANG WAS FELT. FLIGHT CREW THOUGHT IT WAS A TIRE. NOTICED NR 1 ENGINE EPR AND OTHER PARAMETERS DECREASING, SHUTDOWN NR 1 ENGINE. INSPECTION OF EN
- [SDR CA001122002](https://openairdocs.org/sdr/CA001122002.md): Clamp · failed · Nov 8, 2000 · Boeing 737217 · Engine Anti-Icing System
  > (CAN) NR 1 ENGINE SHUT DOWN, APPROXIMATELY 12 MINUTES INTO FLT. DUE TO ENGINE OVERHEAT AND START VALVE OPEN LIGHT ON. FOUND THERMAL ANTI-ICE DUCT CLAMP FAILED. REPLACED CLAMP, RT 8TH STAGE BLEED DUCT, AND 13TH STAGE BLEED DUCT TO EXPANSION BELLOWS. ENGINE RUN
- [SDR CA001201013](https://openairdocs.org/sdr/CA001201013.md): Gcu · failed · Oct 25, 2000 · Boeing 737217 · AC Regulator
  > (CAN) DEPARTED WITH MEL ON NR 2 GENERATOR, GENERATOR HAD BEEN DISCONNECTED. 50 MILES SOUTH WEST OF YQB, THE APU GENERATOR FAILED. NR 1 BUS TRANSFER DID NOT TAKE PLACE, FIRST OFFICER WAS WITHOUT INSTRUMENTS. REQUESTED LANDING TO YQB, LANDED WITHOUT INCIDENT. AP

Next page: https://openairdocs.org/model/boeing-737-217/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 = '737217'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-217/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.