# Service difficulty reports: Rolls-Royce RB211-22B-02 A list on [Rolls-Royce RB211-22B-02](https://openairdocs.org/engine/rolls-royce-rb211-22b-02.md). Newest first. General aviation reporting is voluntary. Page 1 of 5 · 211 reports - [SDR CA030526002](https://openairdocs.org/sdr/CA030526002.md): Blade · damaged · May 25, 2003 · Lkheed 1011385115 · Turbine Engine Compressor Section > (CAN) AIRCRAFT RETURNED TO STATION AFTER TAKE OFF DUE TO NR 3 ENGINE HIGH VIBRATION ( 2.5 UNITS) DURING CLIMB. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE STATION WITH NO FURTHER PROBLEM.RECTIFICATION: THE COMPLETE SET OF FAN BLADES WAS REPLACED A - [SDR WRNA200300010](https://openairdocs.org/sdr/WRNA200300010.md): Fire Loop · false activation · May 21, 2003 · N311EA · Lkheed 10113851 · Fire Detection > AFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF IMMEDIATLY AFTER ENGINE SHUTDOWN. FIRE BOTTLES NOT FIRED. FUEL DUMPED (APPROX. 8800 GALLONS) AIRCRAF - [SDR WRNA200300011](https://openairdocs.org/sdr/WRNA200300011.md): Pressure Switch · leaking · May 21, 2003 · N311EA · Lkheed 10113851 · Turbine Section > DURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENGINE SHUTDOWN. FIRE BOTTLE NOT FIRED. APPROX 8800 GALS. OF FUEL DUMPED. A/C RETURNED TO FIELD, LANDED - [SDR CA030428001](https://openairdocs.org/sdr/CA030428001.md): Hose · leaking · Apr 21, 2003 · Lkheed 1011385114 · Crew Oxygen System > (CAN) CREW REPORTED OXYGEN CYLINDER PRESSURE LOW ON ARRIVAL. DURING INVESTIGATION MAINTENANCE FOUND THE LP OXYGEN LINE LEAKING AT THE BOTTLE. LINE WAS REPLACED. SUSPECT DAMAGE WAS CAUSED DURING CYLINDER REPLACEMENT. - [SDR CA030317002](https://openairdocs.org/sdr/CA030317002.md): Valve · open · Mar 16, 2003 · Lkheed 1011385114 · Cargo/Baggage Doors > (CAN) LOSS OF CABIN PRESSURE AT FL 310. CABIN RATE OF CLIMB 1500 FPM. RAPID DEPRESSURIZATION DRILL WAS CARRY OUT. WITH CROSS BLEED CLOSED CABIN CAME BACK TO NORMAL. SAFETY VALVE OPEN LIGHT REMAINED ON UNTIL LANDING. - [SDR CA021223007](https://openairdocs.org/sdr/CA021223007.md): Adc · malfunctioned · Dec 22, 2002 · Lkheed 1011385114 · Air Data Computer > (CAN) SHORTLY AFTER T/O (A/C RETURNED), THE FOLLOWING INDICATIONS CAME UP ON F/O'S SIDE: MACH FLAG IN A/S INDICATOR, SSC FLAG IN ALTIMETER, F/D FLAG IN ADI, OFF FLAGS IN BOTH TAS AND SAT INDICATORS, AND FAIL ANNUNCIATORS IN BOTH MACH TRIM AND MACH FEEL CHANNEL - [SDR CA030113015](https://openairdocs.org/sdr/CA030113015.md): Access Door · separated · Nov 23, 2002 · Lkheed 1011385114 · Doors > (CAN) ON ARRIVAL IN YYZ FROM FLIGHT 651 (PVR-YYZ), NR 1 ENGINE START CONTROL VALVE ACCESS PANEL WAS MISSING. NO DAMAGE TO COWLING. MTCE REPLACED THE DOOR IAW AMM 71-11-00. - [SDR WRNA200200007](https://openairdocs.org/sdr/WRNA200200007.md): Fire Loop · shorted · Oct 22, 2002 · N311EA · Lkheed 10113851 · Fire Detection > Enroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silenced, #1 engine shutdown per procedures. Alt fire bottle discharged, light remained in handle, Main bottle discharged light remained on. Fuel - [SDR CA021108018](https://openairdocs.org/sdr/CA021108018.md): Actuator · cracked · Oct 16, 2002 · Lkheed 1011385114 · Landing Gear Actuator > (CAN) WHILE PERFORMING A MLG RETRACTION TEST, AFTER REPLACEMENT OF ALL GEARS ON A/C, WE NOTICED AFTER A COUPLE RETRACTIONS, THAT THE MLG ACTUATOR PIN (P/N 1523042-101, REF IPC 32-11-03, ITEM 435) OF THE MLGRETRACT ACTUATOR ON THE R/H MLG WAS CRACKED. RETRACTIO - [SDR CA021110003](https://openairdocs.org/sdr/CA021110003.md): Control Box · failed · Oct 10, 2002 · Lkheed 1011385115 · Electrical Power System Wiring > (CAN) CENTER CARGO LT SIDE CIRCUIT BREAKER ON CONTROL RELAY BOX ASSEMBLY POPPED WHEN RESELECTED (PUSHED IN), SPARKS OCCURRED INSIDE OF THE CONTROL RELAY BOX NEAR LOWER CONNECTOR PLUG. THE CONTROL RELAY BOX ASSEMBLY WAS FOUND AT FAULT. PART WAS REPLACED AND TH - [SDR CA020705006](https://openairdocs.org/sdr/CA020705006.md): Actuator · cracked · Jun 22, 2002 · Lkheed 1011385114 · Landing Gear Door Actuator > (CAN) FOUND LT MLG DOOR ACTUATOR CRACKED.250 INCHES AND LEAKING (CONFIRMED BY NDT), IN DOOR CLOSED POSITION. MAINTENANCE REPLACED THE ACTUATOR IAW AMM 32-33-01. - [SDR CA020527007](https://openairdocs.org/sdr/CA020527007.md): Shaft · sheared · May 19, 2002 · Lkheed 1011385114 · Hydraulic Pump (Electric/Engine), Main > (CAN) 'D1' HYD SYSTEM PRESSURE AT 0 PSI WITH SWITCH LATCHED IN LOW PRESSURE LIGHT ON. NO HYD QUANTITY LOSS, NO HIGH TEMP 'CD' PTU SELECTOR TO BRING SYSTEM PRESSURE BACK TO 3000 PSI. D1 PUMP OFF. D SYSTEM ENG DRIVEN PUMP REMOVED AND FOUND SHAFT SHEARED. PU - [SDR CA020527003](https://openairdocs.org/sdr/CA020527003.md): Engine · vibration · May 17, 2002 · Lkheed 1011385114 · Engine (Turbine/Turboprop) > (CAN) ENGINE NR 3, AT 22 000 FT, THE VIB. CHANNEL A + B, 2.6 TO 2.8 UNITS. ENGINE SHUT DOWN WAS CARRIED OUT PER QRH. AT TAKE OFF, THE VIB. WAS AT 2.0 TO 2.2 UNITS. ON CLIMB THE VIB. WAS 1.9 UNITS (BOTH CHANNELS), DID NOT APPEAR TO BE LINEAR WITH THROTTLE MO - [SDR CA020426005](https://openairdocs.org/sdr/CA020426005.md): Pin · corroded · Apr 20, 2002 · Lkheed 1011385114 · Engine Cowling System > (CAN) DURING WALK AROUND, FOUND NR 3 ENGINE GLOVE FAIRING ADRIFT. GLOVE FAIRING FOUND RETAINED BY TWO LANYARD AND PIP PIN NOT IN PLACE FOR SECURITY. THE PIN WAS FOUND CORRODED AND THE PIN LOCKING MECHANISM WAS JAMMED DUE TO CORROSION..IT WAS NOT POSSIBLE TO - [SDR CA020308004](https://openairdocs.org/sdr/CA020308004.md): Sleeve · broken · Mar 8, 2002 · Lkheed 1011385114 · Nose/Tail Landing Gear > (CAN) DURING WALKAROUND FOUND NLG UPPER TORQUE LINK RT DETENT SLEEVE BROKEN IN TWO. REPLACED UPPER TORQUE LINK'S RT SPRING, INDEX AND DETENT SLEEVES AND A/C WAS RETURNED TO SERVICE. - [SDR CA020221018](https://openairdocs.org/sdr/CA020221018.md): Fan Blade · damaged · Feb 2, 2002 · Lkheed 10113851 · Turbine Engine Compressor Section > (CAN) SHORTLY AFTER TAKEOFF NR 2 ENGINE N1 INDICATION SHOWED 10 PERCENT HIGHER THAN NR 1 AND 3 ENGINES. ALL PARAMETERS WERE THE SAME. WHEN THRUST WAS REDUCED TO LOWER N1 SETTING, NR 2 ENGINE HIGH VIBRATION WAS CONFIRMED ON BOTH CHANNELS AT 2.5 UNITS (VIB. - [SDR CA020117007](https://openairdocs.org/sdr/CA020117007.md): Bulkhead · cracked · Jan 11, 2002 · Lkheed 10113851 · Fuselage Main, Bulkhead > (CAN) CRACK FOUND ON PRESSURE BULKHEAD 1363 AT RBL 44.5 & WL 130. STIFFENERS SURROUNDING CRACK REMOVED FOR ACCESS IN ACCORDANCE WITH S.R.M. 51-40-01. CRACK STOP DRILLED, - [SDR ARWA20020110](https://openairdocs.org/sdr/ARWA20020110.md): Engine · malfunctioned · Jan 10, 2002 · N308GB · Lkheed 1011385115 · Engine (Turbine/Turboprop) > NR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN. - [SDR CA020111002](https://openairdocs.org/sdr/CA020111002.md): Blocker Door · broken · Dec 9, 2001 · Lkheed 10113851 · Engine Thrust Reverser > (CAN) FOUND NR 2 ENGINE NOZZLE COLLECTOR DAMAGED, ONE BLOCKER DOOR MISSING. BLOCKER DOOR BROKEN IN TWO PIECES AT HINGE AND ONE PIECE DAMAGE NOZZLE COLLECTOR, RT BLISTER FAIRING, ACCOUSTIC TRAY NR 1 AND FAIRING 438 DR. - [SDR CA011210024](https://openairdocs.org/sdr/CA011210024.md): Lens · loose · Nov 13, 2001 · Lkheed 1011385114 · Flight Compartment Lighting > (CAN) -THE REFLECTOR HAS BEEN FOUND LOOSE IN LENS OF LIGHT ASSEMBLY CAUSING C/B PANEL NR 2, K3 POSITION, POPPED DUE TO BULB CONTACT SHORTED TO LIGHT ASSEMBLY BODY. - [SDR CA011211025](https://openairdocs.org/sdr/CA011211025.md): Wire · burned · Sep 7, 2001 · Lkheed 1011385114 · Equipment/Furnishings Wiring > (CAN) LOWER GALLEY ZONE 130, OVEN FEEDER 1-5 (CB11) PHASE "A" WIRE AT TB 2531-1 TERMINAL NR 5 FOUND BURNED OUT. - [SDR CA010823002](https://openairdocs.org/sdr/CA010823002.md): Acm · contaminated · Aug 19, 2001 · Lkheed 1011385114 · Cabin Cooling System > (CAN) DURING TAXI NR 2 AIR CONDITIONING SYSTEM BECAME NOISY. LOUD GRINDING NOISE WAS NOTICED IN THE FLIGHT DECK. SMOKE AND ODOUR WERE NOTICED IN THE CABIN. NR 2 PACK WAS TURN OFF. SMOKE AND ODOUR WAS STILL COMING INTO THE CABIN. CREW PROCEED WITH AN EMERGENCY - [SDR CA010823007](https://openairdocs.org/sdr/CA010823007.md): Switch · shorted · Aug 19, 2001 · Lkheed 1011385114 · Cabin Temperature Control System > (CAN) DURING TAXI, NR 2 AIR CONDITIONING SYSTEM BECAME NOISY AND PRODUCING SMOKE AND ODOUR IN THE CABIN. NR 2 PACK WAS SHUT DOWN. EMERGENCY EVACUATION WAS EXECUTED DUE TO SMOKE AND ODOUR STILL COMING FROM NR 2 PACK AFTER SHUT DOWN. DURING INVESTIGATION FOUND T - [SDR CA010808060](https://openairdocs.org/sdr/CA010808060.md): Rod · stiff · Aug 1, 2001 · Lkheed 1011385114 · Landing Gear Doors > (CAN) AFTER TAKE OFF, LEFT HAND NOSE GEAR DOOR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE STATION. FOUND THE LEFT HAND GEAR DOOR ROD ACTUATOR VERY STIFF. UNIT WAS SERVICED AS PER MAINTENANCE MANUAL AND CHECKED SERVICEABLE AS PER OVERHAUL MANUAL. SYSTEM WAS VE - [SDR CA010704021](https://openairdocs.org/sdr/CA010704021.md): Fuel Bowl · cracked · Jun 29, 2001 · Lkheed 1011385114 · APU Engine Fuel and Control > (CAN) AFTER ARRIVAL IN PUJ NOT ABLE TO START APU, ON WALK AROUND FOUND FUEL LEAK COMING FROM APU, INVESTIGATED FOUND FUEL BOWL COVER LEAKING. MAINTENANCE REPLACED FUEL BOWL/LEAKCHECKED AND RETURNED AIRCRAFTTO SERVICE. - [SDR CA010704019](https://openairdocs.org/sdr/CA010704019.md): Fuel Bowl · cracked · Jun 19, 2001 · Lkheed 1011385114 · APU Engine Fuel and Control > (CAN) ON PREPARING AIRCRAFT FOR DEPARTURE MAINTENANCE EXPERIENCED AN APU HUNG START ABORTED, ON INVESTIGATION FOUND APU FILTER BOWL CRACKED. 3RD OCCURANCE OF DEFECT. PUMP AND FILTER BOWL ASSEMBLY HAD BEEN PREVIOUSLY REPLACED DUE TO COULD NOT DISCOVER WHY 2ND O - [SDR CA010704020](https://openairdocs.org/sdr/CA010704020.md): Heat Exchanger · cracked · Jun 13, 2001 · Lkheed 1011385114 · APU Engine Fuel and Control > (CAN) FUEL LEAK AT HEAT EXCHANGER CORE. - [SDR CA010531007](https://openairdocs.org/sdr/CA010531007.md): Fuel Bowl · cracked · May 8, 2001 · Lkheed 1011385114 · Airborne Auxiliary Power Unit (APU) System > (CAN) DURING THE TAXI IN THE AIRCRAFT LOST APPROXIMATELY 600 LBS OF FUEL. MAINTENANCE FOUND FUELLEAK FROM APU. UPON INSPECTION FOUND THAT THE FUEL WAS COMING FROM THE LOW PRESSURE FUEL FILTER BOWL CRACKED AT MOUNTING FLANGE. BOWL REPLACED AND AIRCRAFT RETURNED - [SDR CA010706004](https://openairdocs.org/sdr/CA010706004.md): Switch · failed · Apr 29, 2001 · Lkheed 10113851 · Landing Gear System > (CAN) AFTER DEPARTURE FROM YMX, THE TRUCK LIGHT CAME ON, NORMAL PROCEDURES WHERE NOT TO RETRACT THE GEAR, CREW DUMPED FUEL AND RETURNED TO BASE. FOUND TRUCK SWITCH AT FAULT, COMPLETE ACTUATOR REP LACED AND AIRCRAFT RELEASED FOR A FLIGHT TEST, SYSTEM CHECKED SE - [SDR 2001F00004](https://openairdocs.org/sdr/2001F00004.md): O-Ring · pinched · Apr 14, 2001 · N311EA · Lkheed 10113851 · Turbine Engine Oil System > NR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGED (PINCHED) O-RING AT NR 3 ENGINE OIL PRESSURE FILTER BOWL CAP. REMOVED AND REPLACED O-RING IAW MM 72-01-00. R - [SDR CA010430015](https://openairdocs.org/sdr/CA010430015.md): Retainer · broken · Apr 7, 2001 · Lkheed 1011385115 · Cargo/Baggage Doors > (CAN) AFTER TAKEOFF AT 20,000 FEET, AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS AND CREW COULD HEAR A KNOCKING SOUND AGAINST THE FUSELAGE ON THE RT SIDE. CREW PERFORMED RAPID DE-PRESSURIZATION DRILL AND REGAINED CONTROL OF PRESSURIZATION. CREW DUMPED FUEL AND - [SDR CA010430016](https://openairdocs.org/sdr/CA010430016.md): Engine · failed · Apr 7, 2001 · Lkheed 1011385114 · Engine (Turbine/Turboprop) > (CAN) DRUING FLIGHT ENGINE NR 1 EXPERIENCED A SUDDEN VIBS INCREASE TO 3.5 UNITS ON BOTH CHANNELS A & B, WARNING LIGHTS CAME ON, ENGINE SHUT DOWN WAS ACCOMPLISHED.MCD CHECKS WAS C/O NOT DAMAGED, ENGINE BORESCOPE WAS C/O NO DAMAGE FOUND. FAN BLADES REMOVED CLEAN - [SDR CA010402012](https://openairdocs.org/sdr/CA010402012.md): Proximity Sensor · faulty · Mar 3, 2001 · Lkheed 1011385115 · Landing Gear Position and Warning > (CAN) DURING APPROACH AT YMX, NO GREEN LIGHT ILLUMINATE ON LT MLG DOWN & LOCK, PROXIMITY SENSOR AT FAULT, R&R C/OUT, GEAR WING C/OUT, CHECK SERVICEABLE. - [SDR CA010402010](https://openairdocs.org/sdr/CA010402010.md): Light · shorted · Mar 1, 2001 · Lkheed 1011385114 · Passenger Compartment Lighting > (CAN) AFT LOWR GALLEY CEILING LIGHT SHORT OUT (FIRST LIGHT ASSY IN FRONT OF GALLEY LIFT) CAUSING SMELL OR SMOKE IN CABIN. - [SDR CA010402011](https://openairdocs.org/sdr/CA010402011.md): Fuel Line · leaking · Feb 28, 2001 · Lkheed 1011385114 · Aircraft Fuel Distribution System > (CAN) STEEL BRAIDED FLEX FUEL SUPPLY LINE, NR 2 ENGINE & APU, IN HYDRAULIC SERVICE CENTER COMPARTMENT LEAKING APPROXIMATELY 3 FEET FROM FORWARD END DUE TO INTERNAL RUPTURE. FUEL LINE IS UNDER INVESTIGATION BY ENGINEERING DEPARTMENT TO DETERMINE THE CAUSE. - [SDR CA010307015](https://openairdocs.org/sdr/CA010307015.md): Engine · failed · Feb 25, 2001 · Lkheed 1011385114 · Engine/Transmission Coupling > (CAN) AFTER TAKEOFF ENGINE NR 3 VIBS INCREASED TO 2.5 UNITS, THROTTLE RETARDED TO KEEP BELOW LIMITS. AIRCRAFT RETURNED TO MAINTENANCE BASE YMX. TROUBLESHOOTING CARRIED OUT AS PER MM 79-00-00 PAGE 121, ENGINE RUNS CARRIED OUT AS PER TEST NR 21 VIBRATIONS WITHIN - [SDR CA010307017](https://openairdocs.org/sdr/CA010307017.md): Engine · vibration · Feb 18, 2001 · Lkheed 1011385115 · Engine (Turbine/Turboprop) > (CAN) AFTER TAKEOFF (DURING FIRST STAGES OF CLIMB) THE NR 2 ENGINE VIBRATION INCREASED, FLIGHT CREW SHUTDOWN ENGINE IN ACCORDANCE WITH OPERATING PROCEDURE AND RTURNED TO BASE. MAINTENANCE PERFORMED TEST 21 IN ACCORDANCE WITH ROLLS ROYCE PROCEDURES, ENGINE VIBR - [SDR CA010307016](https://openairdocs.org/sdr/CA010307016.md): Pump · cracked · Feb 16, 2001 · Lkheed 1011385115 · Hydraulic Pump (Electric/Engine), Main > (CAN) IN CRUISE AT FL300, HYDRAULIC SYSTEM C, LOST OF PRESSURE, EDP SHUT-OFF ACTIVATED BY FLIGHT CREW AND GEARS EXTENDED USING MANUAL SYSTEM. MAINTENANCE FOUND A 7.5 INCH CRACK IN EDP CASING, EDP REPLACED AND AIRCRAFT RETURNED TO SERVICE. PART IS AVAILABLE. - [SDR DLL10002204](https://openairdocs.org/sdr/DLL10002204.md): Cover · leaking · Nov 10, 2000 · N733DS · Lkheed 10113851 · Turbine Engine Oil System > OIL QTY ON NR 1 ENGINE WENT TO ZERO AND OIL PRESS DROPPED INTO RED. SHUT DOWN ENG AT 1925Z. (ENG SHUT DOWN 18 MIN PRIOR TO LANDING). OIL TEMP REMAINED THE SAME AS OTHER ENGS. FOUND OIL LEAK AT TOP OF ANGLE GEARBOX MATING SURFACE. REPLACED INPUT DRIVE COVE - [SDR CA001212004](https://openairdocs.org/sdr/CA001212004.md): Connector · shorted · Nov 7, 2000 · Lkheed 1011385114 · Fuel Boost Pump > (CAN) NR2 INBOARD FUEL BOOST PUMP C/B POPPED DURING FLIGHT.INVESTIGATION FOUND CANNON PLUG TO PUMP HOUSING PLUG IN TO BE SEVERELY BURNT AND ARCED.SYSTEM DE-ACTIVATED IN ACCORDANCE WITH MEL 28-24-01, AIRCRAFT RETURNED TO OPERATION. - [SDR CA010103019](https://openairdocs.org/sdr/CA010103019.md): Separator · blocked · Nov 2, 2000 · Lkheed 1011385114 · Humidity Control System > (CAN) DURING CLIMB OUT ALL LAVATORYS SMOKE DETECTORS ALARM CAME ON. OIL ODOR IN COCKPIT.ISOLATION VALVE NR 1 AND NR 2 CLOSED AND OIL ODOR WAS ELIMINATED. OIL RESIDUAL WAS FOUND IN NR 2 ENGINE IP COMPRESSOR CAUSING OIL ODOR. ENGINE IS UNDER OBSERVATION. WATER S - [SDR DLL10002139](https://openairdocs.org/sdr/DLL10002139.md): Acm · smoke · Oct 31, 2000 · N1734D · Lkheed 10113851 · Cabin Cooling System > OILY SMOKE IN AFT CABIN ON CLIMBOUT. ISOLATED NR 1 ENG AND PACK, SMOKE DISSIPATED. FOLLOWED AIR CONDITIONING SMOKE PROCEDURE IN POM. ENDED UP WITH 1 PACK OFF AND OTHER SWITCHES LATCHED. REPLACED NR 1 ACM AND INNER DUCT HOUSING TO THE HEAT EXCHANGER. REPLA - [SDR CA001107004](https://openairdocs.org/sdr/CA001107004.md): Wire · broken · Oct 28, 2000 · Lkheed 1011385114 · Air Conditioning System Wiring > (CAN) DURING CRUISE LOST BOTH FORWARD AND AFT OUTFLOW VALVE AUTO CONTROL, COMPLETED FLIGHT ON MANUAL MODE.6 WIRES WERE FOUND BROKEN IN THE CONNECTOR PLUG BACK SHELL OF PLUG 2131-P4 AT ZONE 154 STA 1513. WIRES REPAIRED, FUNCTION CHECKED SERVICEABLE. - [SDR DLL10002127](https://openairdocs.org/sdr/DLL10002127.md): Housing · leaking · Oct 27, 2000 · N1734D · Lkheed 10113851 · Engine Oil Distribution (Airframe Furnished) > NR 1 ENG OIL QTY DROPPED FROM 16 TO 4 QTS IN 1.5 HRS OIL QTY DECREASED TO ZERO, ENGINE SHUTDOWN PER POM 23-107. RAPID DECREASE IN OIL QTY OIL PRESS REMAINED ABOVE 40 PSI UNTIL LANDING. FOUND GEARBOX CHIP DET MISSING FROM HOUSING AND OIL LEAKING OUT. REPLACE - [SDR CA001102003](https://openairdocs.org/sdr/CA001102003.md): Connector · wrong part · Oct 13, 2000 · Lkheed 1011385114 · Rudder Control System > (CAN) DURING DEFECT TROUBLE SHOOTING OF THE YAW SAS 2 FAIL & RUDDER HYDRAULIC LIMITER FOUND WRONG PART INSTALLED, (UNION WITH OUT A RESTRICTOR), INSTALLED ON THE HYDRAULIC SHUTOFF VALVE REPLACED AIRCRAFT DISPATCHED.PART WAS FOUND NOT TO HAVE BEEN INSTALLED BY - [SDR CA001102002](https://openairdocs.org/sdr/CA001102002.md): Circuit Breaker · failed · Oct 8, 2000 · Lkheed 10113851 · DC Power Distribution System > (CAN) SPARKS WHERE SEEN COMING FROM LT MID GALLEY SERVICE OUTLET DURING TAKEOFF, CIRCUIT BREAKERS J19 & C13 PULLED AND COLLARED. SYSTEM DE-ACTIVATED AND AIRCRAFT RELEASED UNDER MEL. - [SDR CA001005016](https://openairdocs.org/sdr/CA001005016.md): Actuator · cracked · Sep 7, 2000 · Lkheed 1011385114 · Landing Gear Actuator > (CAN) DURING TAKEOFF ROLL (80 KNTS), HYDRAULIC ''C'' SYSTEM LOST ALL FLUID. A/C RETURN TO GATE. INVESTIGATION FOUND LOWER FLANGE OF LT MLG ACTUATOR CRACKED AT END CAP AND THE PISTON TRAVELLED OUT OF THE CYLINDER.CYLINDER ASSEMBLY REPLACED, HYDRAULIC SYSTEM RE - [SDR CA000830002](https://openairdocs.org/sdr/CA000830002.md): Cable · sheared · Aug 12, 2000 · Lkheed 1011385114 · Engine Thrust Reverser > (CAN) AUGUST 17,2000 AFTER LANDING IN BORDEAUX THE CREW COULD NOT DEPLOY THE NR2 ENGINE TR EVEN WHEN THE TR UNLOCK LIGHT WAS ON.AFTER ENGINE SHUTDOWN FOUND THAT THE TR WAS APPROX 3 INCHES DEPLOYED. ON INVESTIGATION FOUND THAT THE DRIVE CABLES WHERE SHEARED AT - [SDR CA001004008](https://openairdocs.org/sdr/CA001004008.md): Cable · broken · Aug 12, 2000 · Lkheed 1011385114 · Engine Thrust Reverser > (CAN) AUGUST 17, 2000 AFTER LANDING IN BORDEAUX THE CREW COULD NOT DEPLOY THE NR 2 ENGINE TR EVEN WHEN THE TR UNLOCK LIGHT WAS ON.AFTER ENGINE SHUT DOWN FOUND THAT THE TR WAS APPROX 3 INCHES DEPLOYED.ON INVESTIGATION FOUND THAT THE OTHE CABLES WHERE SHEARED AT - [SDR CA000830013](https://openairdocs.org/sdr/CA000830013.md): Indicator · malfunctioned · Aug 11, 2000 · Lkheed 1011385114 · Engine Oil Indicating System > (CAN) DURING CRUISE F/E STARTED TO SMELL SMOKE AND SAW SPARKS COMING FROM THE NR 2 ENGINE OIL QTY GAUGE, MANUALLY PULLED C.B. INDICATOR STOPPED SPARKING.AIRCRAFT RETURNED TO MAINTENANCE BASE. MAINTENANCE PERSONNEL ACCOMPLISHED A DETAILED VISUAL INSPECTION OF A Next page: https://openairdocs.org/engine/rolls-royce-rb211-22b-02/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 engine_model_key = 'RB21122B02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/rolls-royce-rb211-22b-02/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.