Boeing 737-752

Service difficulty reports · 2,590

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duckdb -csv -c "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 = '737752'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASMF201303012Window · leakingACFT RETURNED, DURING CLIMB A STRONG NOISE IN THE FLIGHT DECK WAS DETECTED, CAUSED BY PRESSURIZATION PROBLEM ON THE CAPTAIN WINDOW. MX PERSONNEL PERFORMED CABIN PRESSURIZATION CONTROL SYSTEM VERIFICATION AND WAS NOT FOUND PRESSURIZATION PROBLEM IN THE FLIGHT Jan 25, 2013 · N857AM · Boeing 737752 · Flight Compartment WindowsSDR ASMF201303009Warning Light · illuminatedACFT REJECTED TAKEOFF AT 20 KNOTS DUE TO FORWARD ENTRY DOOR LIGHT TURNED ON. DURING MX REVISION, THE FORWARD ENTRY DOOR WAS DETECTED LIGHTLY OPENED; THE FORWARD ENTRY DOOR WAS CHECKED IAW MM 52-11-00, NO DAMAGES WERE FOUND. THE HIGH ENERGY STOP INSPECTION WASJan 23, 2013 · N853AM · Boeing 737752 · Door Warning SystemSDR ASMF201303003Bolt · looseDURING CLIMB, RT ENGINE VIBRATION REACHED 3.7 UNITS AND DURING CRUISE THE VIBRATION WAS STABILIZED IN 1.5 UNITS. AIRCRAFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK 71-00-00-700-847-G01, DETECTING 2 RT ENGINE FAN WEIJan 14, 2013 · N904AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR EE4Y2013021200006Window Frame · crackedUPPER FUSELAGE FLIGHT CONTROL COMPARTMENT AT BS 219.75, RBL 33 NR 1 WINDOW FRAME ASSY WITH CRACK. THE NR 1 WINDOW FRAME WAS RELPACED IAW SB 737-53-1316, COO-AMX-13-0003-02 (R1), UNDER THE NON ROUTINE WO A1B038, SUB JOB: 2, ITEM: 92.Jan 10, 2013 · N850AM · Boeing 737752 · Fuselage Main, StructureSDR ASMF201301005Line · damagedDURING TRANSIT CHECK, DETECTED A HYD LEAK IN THE RT MLG. MX PERSONNEL PERFORMED REVISION DETECTING THE HYD LINE DAMAGED; SO THE HYD LINE WAS REPLACED IAW MM 29-00-00, TESTED CORRECT.Jan 6, 2013 · N788XA · Boeing 737752 · Hydraulic System, MainSDR ASMF201301004Seal · leakingAIRCRAFT RETURNED TO PLATFORM, NLG SHOCK STRUT HYD LEAK. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE ACTIVE SEALS IAW MM 32-21-11, TESTED CORRECT.Jan 6, 2013 · N906AM · Boeing 737752 · Nose/Tail Landing Gear Strut/AxleSDR ASMF201301003Engine · unknownAIRCRAFT RETURNED TO PLATFORM, LEFT ENGINE WOULD NOT START. FLIGHT CREW ACCOMPLISHED THE QRH 7.14 PROCEDURE, CONFIRMING FAILURE. MX PERSONNEL PERFORMED THE LT ENGINE START IAW MM 74-00-00 AND ENGINE LEAKING INSPECTION IAW MM 73-21-00, NO CONFIRMING FAILURE.Jan 6, 2013 · N842AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201212015Seal · leakingCAPTAIN REPORTED THAT DURING LANDING, A STRONG NOISE IN CREW CABIN, WAS LISTENING WHEN LOWERED THE LANDING GEAR. MX REPLACED THE ACTIVE SEALS AND PERFORMED SERVICE, A NLG SHOCK STRUT IAW MM 12-15-41 AND MM 32-21-11, TESTED CORRECT.Dec 30, 2012 · N788XA · Boeing 737752 · Nose/Tail Landing Gear Strut/AxleSDR ASMF201212013Check Valve · stuckACFT RETURNED TO PLATFORM, DURING TAXI THE LT ENGINE HAD AN UNCOMMANDED SHUTDOWN. MX PERFORMED BITE TO LT ENGINE EEC IAW MM 73-21-00, NO SHOWING MESSAGES. CHECK VALVE ON 5TH STAGE LT ENGINE WAS STUCK. CHECK VALVE WAS REPLACED IAW MM 36-11-02 AND PERFORMEDDec 26, 2012 · N857AM · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF201212006Actuator · leakingDURING OVERNIGHT CHECK, MX DETECTED A HYD LEAK IN THE RT INBD L/E FLAP NR 3 ACTUATOR. RT INBD L/E FLAP NR 3 ACTUATOR WAS REPLACED IAW MM 27-81-31, TESTED CORRECT.Dec 4, 2012 · N850AM · Boeing 737752 · Leading Edge Slat Position Indicating SystemSDR ASMF201212003Drain · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED. MX PERSONNEL DETECTED THE TRANSIENT BLEED VALVE DRAIN WITH FUEL LEAK IAW MM 75-20-00; SO RT ENGINE START WAS PERFORMED AGAIN AND THE LT ENGINE WAS ACCELERATED, ELIMINATING THE FUEL LEAK IAW MM 71-00-00, TEST 3ANov 26, 2012 · N842AM · Boeing 737752 · Fuel Controlling SystemSDR ASMF201212002Eec · failedACFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. DURING MX REVISION, THE MESSAGE 73-21322 WAS SHOWN, SO THE FIM 73-22 TASK 803 PROCEDURE WAS PERFORMED, CONTINUING THE MESSAGE; THE RT EEC WAS REPLACED IAW MM 73-21-Nov 24, 2012 · N855AM · Boeing 737752 · Fuel Controlling SystemSDR ASMF201212001Warning Light · false activationACFT REJECTED TAKEOFF AT 50 KNOTS WITH A GROSS WEIGHT OF 58 000 KG, THE CONFIGURATION ALARM WAS ACTIVATED. DURING MX REVISION, THE MESSAGE 27-62001 WAS SHOWN, SO THE FIM 27-62 TASK 808 PROCEDURE WAS PERFORMED DETERMINING TO ADJUST AND CHECK THE SPEED BRAKE TANov 24, 2012 · N842AM · Boeing 737752 · Central WarningSDR ASMF201211013Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT MLG RETRACT ACTUATOR. AIRCRAFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE RT MLG RETRACT ACTUATOR IAW MM 32-32-11, TESTED CORRECT.Nov 21, 2012 · N857AM · Boeing 737752 · Landing Gear ActuatorSDR ASMF201211010Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT MLG RETRACT ACTUATOR. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE RT MLG RETRACT ACTUATOR IAW MM 32-32-11, TESTED CORRECT.Nov 19, 2012 · N853AM · Boeing 737752 · Landing Gear ActuatorSDR ASMF201211005Brake · lockedTHE MLG SHIMMY DAMPER AND TORSION LINK APEX ASSY WERE CHECKED IAW MM 32-11-81 TASK 32-11-81-200-801 AND MM 32-11-51; DETECTING THE MLG BRAKE NR 2 LOCKED, REPLACED IAW MM 32-41-41, ALL CORRECT.Nov 13, 2012 · N908AM · Boeing 737752 · BrakeSDR ASMF201211001Regulator · damagedREJECTED TAKEOFF AT 60 KNOTS DUE TO LT ENGINE PRESSURE DROP OF 15 PSI IN PNEUMATIC DUCT AND LT OVER WING LIGHT TURNED ON. MX PERSONNEL REPLACED THE BLEED AIR REGULATOR, 450 DEGREE THERMOSTAT, PRSOV AND PRECOOLER CONTROL VALVE WERE REPLACED IAW MM 36-11-03, MMOct 21, 2012 · N906AM · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF201210013Wire · damagedCAPTAIN REPORTED THAT DURING CLIMB, THE L/E FLAPS TRANSIT LIGHT TURNED ON AND DURING DESCENT WITH SLIGHT VIBRATION; SO FLIGHT CREW ACCOMPLISHED THE QRH 9.12 PROCEDURE AND L/E FLAPS TRANSIT LIGHT TURNED OFF. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED REVISIONOct 7, 2012 · N857AM · Boeing 737752 · Leading Edge Slat Control SystemSDR ASMF201210005Warning Light · false activationACFT REJECTED TAKEOFF BETWEEN 40 AND 50 KNOTS WITH A GROSS WEIGHT OF 55 10 KG DUE TO EICAS MESSAGE MASTER CAUTION AND ENGINE CONTROL LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 7.14 PROCEDURE, NO CONFIRMING THE FAILURE. MX PERSONNEL PERFORMED BITE TO BSep 19, 2012 · N842AM · Boeing 737752 · Central WarningSDR ASMF201210001Actuator · damagedCAPTAIN REPORTED THAT DURING APPROACH, THE AILERONS CONTROL FELT HARD. MX PERSONNEL PERFORMED FLIGHT CONTROL TEST, DETECTING THAT THE AILERONS CONTROL DID NOT RETURN TO NEUTRAL POSITION IAW MM 27-11-00. THE LT WING FLIGHT SPOILER ACTUATOR NR 4 WAS REPLACED ISep 11, 2012 · N851AM · Boeing 737752 · Drag Control ActuatorSDR ASMF201208009Pressure Switch · damagedCAPTAIN REPORTED THAT DURING DESCENT, THE LT ENGINE FUEL FILTER BYPASS LIGHT TURNED ON, SO FLIGHT CREW ACCOMPLISHED THE QRH 7.22 PROCEDURE, CONFIRMING THE FAILURE; THE LT ENGINE WAS SHUTDOWN AND ACFT CONTINUED TO LANDING. MX PERFORMED THE FIM 73-05 TASK 801 AAug 21, 2012 · N857AM · Boeing 737752 · Engine Fuel DistributionSDR ASMF201208004Skin · damagedCAPTAIN REPORTED THAT DURING CLIMB, A BIRD STRIKE ON FUSELAGE SKIN AND LT WING L/E FLAPS. PERFORMED INSPECTION FOR BIRD STRIKE IAW 05-51-18, FOUND 1 DENT ON STA 260 BETWEEN S-15 TO S-16L LENGTH 1.5" WIDTH 1.0" DEPTH 0.023", ONE DENT ON BS 262 BETWEEN S15L TOAug 7, 2012 · N904AM · Boeing 737752 · Fuselage Main, Plate/SkinSDR ASMF201208003Lubrication Unit · damagedDURING TRANSIT CHECK, DETECTED AN OIL LEAK ON LT ENGINE, THE OIL INDICATION WAS 11 QTS. REPLACED THE LUBRICATION UNIT, IAW MM 79-21-01, TESTED CORRECT.Aug 5, 2012 · N855AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF201208001Blades · lack of lubeCAPTAIN REPORTED THAT DURING CLIMB, RT ENGINE VIBRATION REACHED 3.6. MX PERSONNEL PERFORMED LUBRICATION OF THE FAN ROTOR BLADES AND FAN DECK OF THE RT ENGINE IAW MM 71-21-02 AND VIBRATION TEST NR 7 WAS PERFORMED IAW MM 72-00-00, BEING WITHIN LIMITS.Aug 1, 2012 · N908AM · Boeing 737752 · Turbine Engine Compressor SectionSDR ASMF201207008Engine · making metalCAPTAIN REPORTED THAT DURING DESCENT, THE RT ENGINE OIL FILTER BYPASS LIGHT TURNED ON. MX PERSONNEL REMOVED THE FILTER ASSY AND CHIP DETECTOR ABG/TGB, DETECTED METAL PARTICLES. RT ENGINE NR 2 WAS REPLACED AND TESTED IAW AMM 71-00-02 AND IAW AMM 71-00-00, ALLJul 26, 2012 · N851AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201207007Skin · damagedDURING TRANSIT CHECK, DETECTED A LIGHTNING STRIKE, RIGHT WINGLET AND RIGHT OTBD THRUST REVERSER. MX PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW MM 05-51-19, DETECTING DAMAGES OUT OF LIMITS IN RIGHT WINGLET AND RIGHT OTD THRUST REVERSER AJul 20, 2012 · N857AM · Boeing 737752 · Wing, Plate/SkinSDR ASMF201207006Antenna · damagedCAPTAIN REPORTED A LIGHTNING STRIKE DURING DESCENT, IN THE FUSELAGE RADOME. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING VHF ANTENNA NR 3 DAMAGED; SO IT WAS REPLACED IAW MM 23-12-11, TESTED CORRECT.Jul 15, 2012 · N842AM · Boeing 737752 · VHF Communications SystemSDR ASMF201207005Drive Shaft · brokenDURING TRANSIT CHECK, IT WAS DETECTED THAT THE RIGHT INBD FLAP DID NOT HAVE MOVEMENT. MX PERSONNEL DETECTED BROKEN DRIVE ROD; SO THE RIGHT INBD DRIVE ROD WAS REPLACED IAW MM 27-51-18, TESTED CORRECT.Jul 14, 2012 · N850AM · Boeing 737752 · Trailing Edge Flap Control SystemSDR ASMF201207004Shuttle Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT MLG. MX PERSONNEL DETECTED A LEAK IN THE BRAKE SHUTTLE VALVE; SO IT WAS REPLACED IAW MM 32-41-95, TESTED CORRECT.Jul 4, 2012 · N842AM · Boeing 737752 · Hydraulic System, MainSDR ASMF201207003Valve · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED. MX PERSONNEL DETECTED THE ACTUATOR DRAIN VBV WITH LEAK WITHIN OPERATION LIMITS IAW MM 71-71-00; 3A IDLE PWR LEAK TEST WAS PERFORMED IAW MM 71-71-00, WITHOUT LEAK IN THE ACTUATOR DRAIN VBV, ALL CORRECT.Jun 28, 2012 · N852AM · Boeing 737752 · Aircraft Fuel Distribution SystemSDR ASMF20120615003Magnetic Seal · leakingDURING TRANSIT CHECK, TECH ADDED 02 QTS OF OIL IN THE RT ENGINE. DURING TRANSIT CHECK, IT WAS DETECTED AN OIL LEAK THROUGH THE RT ENGINE IDG, SO ACFT WAS SENT TO THE HANGAR AND MX PERFORMED AN ENGINE REVISION DETECTING OIL LEAK IN THE IDG DRAIN SEAL. THE RT Jun 14, 2012 · N904AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF201206001Spring · brokenDURING FLIGHT AILERONS CONTROLS TEST, THE AILERONS CONTROL DID NOT HAVE RESISTANCE AT BOTH SIDES. MX PERFORMED THE AILERON SYS INSPECTION IAW MM 27-11-00. DETECTED BROKEN CENTERING MECHANISM SPRING; SPRING WAS REPLACED IAW MM 27-11-81, TESTED CORRECT.Jun 5, 2012 · N904AM · Boeing 737752 · Aileron Tab Control SystemSDR ASMF201205013Shutoff Valve · damagedDURING FUELING, A IMBALANCE BETWEEN LT AND RT FUEL TANKS WERE OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. FLIGHT CREW DECIDED TO CONTINUE TO DESTINATION. SHUTOFF VALVE WAS REPLACED IAW MM 28-21-51, TESTED CORRECT.May 27, 2012 · N784XA · Boeing 737752 · Fuel Selector/Shut-Off ValveSDR ASMF201205011Shutoff Valve · damagedDURING FUELING, A FUEL SPILLAGE IN THE LT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. MX PERSONNEL CLOSED THE VALVE MANUALLY. THE SHUTOFF VALVE WAS REPLACED IAW MM 28-21-51, TESTED CORRECT.May 27, 2012 · N784XA · Boeing 737752 · Fuel Selector/Shut-Off ValveSDR ASMF201205009Engine · making metalCAPTAIN REPORTED THAT DURING APPROACH, THE RT ENGINE OIL FILTER BY PASS LIGHT TURNED ON, SO FLIGHT CREW ACCOMPLISHED THE QRH 7.22 PROCEDURE, CONFIRMING THE FAILURE AND ACFT CONTINUES TO LANDING. DURING MX REVISION, THERE WERE DETECTED METAL CHIPS IN THE MAIN May 20, 2012 · N908AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201205007Skin · damagedDURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN LT WINGLET T/E. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTED A DENT OF 0.200 INCHES LONG AND 0.250" WIDE ON NEXT TO LT WINGLET T/E; SO IT WAS REPAIRED IAW SRM 57-30-01 ALLOWABLMay 14, 2012 · N852AM · Boeing 737752 · Wing, Plate/SkinSDR ASMF201205003Carbon Seal · leakingDURING TRANSIT CHECK IT WAS DETECTED AN OIL LEAK THROUGH THE RT ENGINE FUEL PUMP DRAIN, SO ACFT WAS SENT TO THE HANGAR FOR ATTENTION; MX PERSONNEL REPLACE THE RT ENGINE FUEL PUMP CARBON SEAL AND TEST WAS PERFORMED IAW AMM 72-60-00 AND AMM 71-00-00 TESTS 2, 3A May 4, 2012 · N857AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF201205002Line · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT ENGINE REVERSER. MX PERSONNEL DETECTED THE LEAK AT REVERSER LINE, SO IT WAS REPLACED IAW MM 78-31-04, TESTED CORRECT.Apr 29, 2012 · N908AM · Boeing 737752 · Hydraulic System, MainSDR ASMF20120403001Regulator · failedACFT PERFORMED AN EMERGENCY LANDING, DURING CRUISE AL 41,000 FT, THE RT BLEED TRIP OFF LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE AND DESCENDING AT 14,000 FT. MX PERSONNEL PERFORMED THE FIM 36-10 TASK 801 DEApr 3, 2012 · N784XA · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF20120321004Sleeve · puncturedDURING TRANSIT CHECK, THE RT ENGINE THRUST REVERSER WAS HIT, CAUSING A PERFORATION OF 10.0" LONG, 8.5 WIDE ON INTERIOR TRANSLATING SLEEVE THRUST REVERSER. THE RT ENGINE TRANSLATING SLEEVE WAS REPLACED IAW MM 78-31-02, ALL CORRECT.Mar 21, 2012 · N857AM · Boeing 737752 · Engine Thrust ReverserSDR ASMF20120307002Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK DETECTED IN THE RT ENGINE. MX PERSONNEL DETECTED THE LEAK BETWEEN FUEL PUMP AND GEAR BOX, FOUND OUT OF ITS OPERATIONAL LIMITS IAW MM 73-11-00; FUEL PUMP WAS REPLACED IAW MM 73-11-01, TESTED CORRECT.Mar 7, 2012 · N852AM · Boeing 737752 · Engine Fuel PumpSDR ASMF201202001Skin · damagedDURING TRANSIT CHECK, FOUND A 2 INCH CRACK AND A .750 INCH HOLE ON FUSELAGE SKIN AT BS 308, AND STRINGER 22R WITH DEFORMATION. SKIN AND STRINGER REPAIRED IAW AMX-AMX-12-0033-3B, SRM 53-00-01 AND NDT INSPECTION WERE PERFORMED, NO CRACKS WERE FOUND IAW NDTM PAJan 28, 2012 · N788XA · Boeing 737752 · Fuselage Main, Plate/SkinSDR ASMF20111221007Nose Cowl · dentedDURING TRANSIT CHECK, DETECTED A BIRD IN RT ENGINE, SO BIRD STRIKE CONDITIONAL INSP WAS PERFORMED IAW MM 05-51-18, DETECTING A DENT OF 8.0" LONG, 5.0" WIDE AND 0.375" DEPTH IN THE NOSE COWLING AT 12 HRS POSITION, THIS DENT WAS FOUND OUT OF LIMITS IAW SRM 54-10Dec 21, 2011 · N784XA · Boeing 737752 · Nacelle/Pylon, Main FrameSDR ASMF201112005Skin · damagedDURING TRANSIT CHECK, MX DETECTED A ONE INCH HOLE IN FLEX SKIN OF SLAT NR 8, IT WAS CONFIRMED THAT HOLE WAS WITHIN LIMITS IAW SRM 57-42-01, AND WAS TEMPORARY COVERED WITH ALUMINUM FOIL TAPE IAW SRM 57-42-01 PAGES 103 AND 110. SLAT NR 8 WAS REPLACED IAW MM 27-Dec 9, 2011 · N788XA · Boeing 737752 · Leading Edge DevicesSDR ASMF201112003Skin · dentedDURING OVERNIGHT CHECK, MX DETECTED A DENT IN THE RT HORIZONTAL STAB L/E AT STA 181.23 OF 4.150" LONG AND 0.270" DEPTH, IT WAS CONFIRMED THAT DENT WAS OUT OF LIMIT IAW SRM 55-10-01. THE HORIZONTAL STAB L/E WAS REWORKED IAW SRM 55-10-01 PARAGRAPH 4 (D) (3) FIGUDec 2, 2011 · N906AM · Boeing 737752 · Horizontal Stabilizer, Plate/SkinSDR ASMF201111010Slide · unwanted deployDURING TRANSIT CHECK, A F/A ACTIVATED THE RT DOOR SLIDE. MX REPLACED THE RT DOOR SLIDE IAW MM 25-66-01, ALL CORRECT.Nov 14, 2011 · N851AM · Boeing 737752 · Escape SlideSDR ASMF20111107006Motor · inoperativeACFT RETURNED, DURING CLIMB, THE HORIZONTAL STAB TRIM INOPERATIVE. MX PERFORMED THE FIM 27-41-00, TASK 804 PROCEDURE, NOT CONFIRMING THE FAILURE. AS PRECAUTIONARY ACTION, THE STAB TRIM MOTOR WAS REPLACED IAW MM 27-41-71, TESTED CORRECT. THE OVERWEIGHT INSP WNov 7, 2011 · N908AM · Boeing 737752 · Stabilizer Position IndicatingSDR ASMF2011102911005Engine · vibrationCAPTAIN REPORTED THAT DURING CLIMB, THE RT ENGINE VIBRATION REACHED 3.2 OF N2; SO FLIGHT CREW ACCOMPLISHED THE QRH 7.24 PROCEDURE AND CONTINUING TO DESTINATION. ACFT WAS SENT TO THE HANGAR AND MX REPLACED THE RT ENGINE, WAS REPLACED IAW MM 71-00-02, TESTED COOct 29, 2011 · N842AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201111001Carbon Seal · leakingDURING TRANSIT CHECK,DETECTED AN OIL LEAK IN THE RT ENGINE HYD PUMP SEAL WITH 118 DROPS PER MINUTE. ACFT WAS SENT TO THE HANGAR AND THE RT ENGINE HYD PUMP CARBON SEAL WAS REPLACED IAW MM 72-60-00, TESTED CORRECT.Oct 23, 2011 · N851AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF201110006Bleed Valve · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED. MX PERSONNEL PERFORMED REVISION DETECTING THE BLEED VALVE WITH LEAK OUT OF OPERATION LIMITS IAW MM 75-20-00. REPLACED IAW MM 75-23-01 AND OPS TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT.Oct 18, 2011 · N784XA · Boeing 737752 · Compressor Bleed Valve
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