N565AS

Service difficulty reports · 509

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N565AS' AND registry_match = 'registration'
  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 ASAA1058664Unknown · malfunctionedLEFT SIDE WINDOW OVERHEAT LIGHT ON.UNABLE TO CONFIRM DISCREPANCY KEPT SYSTEM ON FOR 45 MINUTES THEN 30 MINUTES LATER ON IN EVENING NEVER HAD OVERHEAT LIGHT COME ON. PERFORMED GROUND VERIFICATION CHECK IAW MM 30 41 00 710 801 OPS CHECK GOOD.Dec 20, 2010 · N565AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1058619Display · damagedF/O'S MCDU (FMC) BUTTON R6 RUBBER TORN. REMOVED & REPLACED F/O'S MCDU REF MM 34 61 01 400 802, OPS NORMAL.Dec 11, 2010 · N565AS · Boeing 737890 · Central DisplaySDR ASAA1058512Warning System · activatedPRIOR TO DEPARTURE THE BATTERY DISCHARGE LIGHT ILLUMINATED DC AMPS 6 DC VOLTS 27. PERFORMED FIM TASK 24 31 00 810 801, NO FAULTS FOUND AND NO HISTORY IN THE PAST 90 DAYS. AS A PRECAUTION REPLACED MAIN BATTERY CHARGER AND BOTH MAIN BATTERIES.AS PER AMM 24 31 Nov 16, 2010 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1058430Warning System · intermittentDURING PREFLIGHT HF NR 2 FAIL LIGHT ILLUMINATED IN BOTH WINDOWS. CONFIRMED FAULT HF2 "FAIL" MESSAGE IN ACTIVE AND STANDBY ON BOTH CAPT'S AND F/O'S RADIO FREQ WINDOWS RESET AIRCRAFT POWER FAULT DID NOT REOCCUR PERFORMED FIM TASK 23 11 00 810 801 FOUND TO BE ANOct 25, 2010 · N565AS · Boeing 737890 · HF Communications SystemSDR ASAA1058422Valve · failedAFTER ENG START AND BOTH PACKS TURNED ON AND RECALL OF MASTER CAUTION PUSHED "ZONE TEMP" LIGHT ON "CONT CAB" CONTROLLER ILLUMINATED. "MASTER CAUTION PUSH TO RESET" WOULD EXTINGUISH LIGHT. QRH "ZONE TEMP" PROCEDURE RAN AND MAINT (SEA) CONTACTED. REPLACED CONOct 20, 2010 · N565AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058412Roller · defectiveR 1 DOOR HARD TO CLOSE. INITIATED MIG 2C 235292 FOR PARTIAL WORK (ASA09711). INITIATED MIG 2C 235293 (ASA88353). FOUND UPPER AFT LATCH ROLLER HITTING OUTSIDE LATCH ROLLER FITTING. ADJUSTED GUIDE ARM PER MM 52 41 00 820 801 PARA I. NO HELP. FOUND GUIDE ROOct 18, 2010 · N565AS · Boeing 737890 · Service DoorsSDR ASAA1058287Relay · failedDURING FLIGHT AT CRUISE CAPTAINS INBOARD DU DISPLAYED WXR FAIL. FIRST OFFICER'S DISPLAY REMAINED NORMAL. FAULT CODE IS 34405031. FOR FAULT CODE 34405031 C/W FIM 34-43-00-810-801. PERFORMED WEATHER RADAR SYS BITE SIX TIMES. OPS NORMAL CAPT & F/O POS. REPLSep 20, 2010 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA1058285Transceiver · malfunctionedCAPTAIN'S WEATHER RADAR FAILED. DISPLAY ON I/B DU INTERMITTENT. WXR FAIL ANNUNCIATOR ILLUMINATED INTERMITTENTLY. WXR WORKED FINE ON F/O SIDE. PERFORMED WXR OPERATIONAL TEST REF MM 34 43 00 NO FAULT NOTED. NR 1 DEU LOGGED FAULT 31 68861 FOR PREVIOUS FLT PESep 18, 2010 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA1058267Warning System · malfunctionedRIGHT PACK LIGHT COMES ON DURING RECALL. PERFORMED FIM TASK 21 62 00 810 801 FAULT CLEARED & DID NOT RETURN. NO HISTORY 60 DAYS. A/C OK FOR SERVICE. SEAMC CONSULTED.Sep 12, 2010 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1058083Warning System · malfunctionedON RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATED. LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. VERIFIED DISCREPANCY. ACCOMPLISHED FIM 21 62 TASK 801. FAULT CLEARED & GROUND VERIFICATION TEST NORMAL. NO PREVIOUS HISTORY.Jul 18, 2010 · N565AS · Boeing 737890 · Cabin Temperature IndicatorSDR ASAA1058009Packing · wornDURING ENG NR 2 OIL SERVICING FOUND OIL CAP PACKING IS WORN. REPLACED OIL CAP PACKING PER AMM 79 11 01.Jun 25, 2010 · N565AS · Boeing 737890 · Engine Oil Storage (Airframe Furnished)SDR ASAA1057877Valve · failedNR 1 LEFT BLEED TRIP OFF LIGHT CAME ON DURING CRUISE AT 400 RESET AND RE-TRIPPED 2 MINUTES LATER AND WOULD NOT RESET. REPLACED PRECOOLER VALVE REF MM 36 12 02 000 400 801. REPLACED HIGH STAGE REGULATOR REF MM 36 11 07 000 400 801. COMPLETED ENG BLEED AIR SYMay 27, 2010 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057866Unknown · malfunctionedWHILE PERFORMING ETOPS PDC FOUND ELECT LIGHT ON P5 13 MODULE ILLUMINATED. ACCOMPLISHED FIM TASK 24 31 TASK 801. AUX BAT CHGR I STATINV INOP I SPCU INOP I MESSAGES WERE LISTED. PER THIS FIM TASK ALL ARE INTERMITTENT FAULTS. CLEARED FAULTS PER TASK 801 ALL FMay 25, 2010 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1057865Charger · failedBATTERY DISCHARGE LIGHT CAME ON, RAN THE QRH CHECK LIST BATTERY INDICATOR SHOWED A NEGATIVE DISCHARGE OF 5. DIVERSION TIME 52 MINUTES. REPLACED BOTH MAIN AND AUX BATTERIES REF AMM 24 31 11 000 802 002. OP TEST GOOD REF AMM 24 31 11 400 802 002. REPLACED MAMay 25, 2010 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1057853Valve · leakingRIGHT BLEED TRIP OFF LIGHT ILLUMINATED BEGINNING DESCENT FROM FL400. EXTINGUISHED AFTER TRIP RESET WAS PUSHED. REPLACED LEAKING PRSOV AND PRECOOLER CONTROL VALVES. PRSOV NOT SMOOTH PER 36 10 00 810 809 STEP 3B FAILED STEP 5C OF SAME. OPS CHECK NORMAL AFTERMay 21, 2010 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057779Unknown · malfunctionedLEFT (CAPT) FMC SCREEN MOMENTARILY BLANKED APPROX 5 SECS THEN OPS NORMAL. C/W TASK 34 61 00 CAPT CDU GROUND FUNCTIONAL CHECK GOOD. A/C OK FOR CONTINUE SERVICE, NO DEFECTS NOTED.May 4, 2010 · N565AS · Boeing 737890 · Central DisplaySDR ASAA1057763Engine · oil consumptionPER SEAMC NR 1 AND NR 2 ENGINE OIL CONSUMPTION RATE OUT OF LIMITS. AT .83 QTS PER HOUR ON EACH ENGINE MANUALLY CALCULATED RATES FOR EACH ENGINE ARE .51 QTS PER HOUR. AIRCRAFT RESTRICTED FROM ETOPS SERVICE PER SEAMC UNTIL OIL CONSUMPTION FALLS WITHIN NORMAL LApr 26, 2010 · N565AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA1057727Magnetic Plug · brokenMAG PLUG ON NR 1 ENG STARTER DAMAGED. REPLACED MAG PLUG ON NR 1 ENG STARTER.Apr 20, 2010 · N565AS · Boeing 737890 · Engine StarterSDR ASAA1057701Wire Harness · no testNR 2 ENGINE PERFORMED TASK CARD 78273000 HAD FAULT CODE 77 20872 LONG TIME FAULT, THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE. VERIFIED EGT PROBE S4 AND HARNESS CJ10 TO BE BAD REPLACED IAW MM 77 21 00, ALL GROUND VERIFICATION TESTS PASS.Apr 12, 2010 · N565AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA1057655Indication Sys · malfunctionedC/W T/C 78273000 ENG 2 LONG TIME FAULT 77 20872 TOP LEFT EGT SIGNAL (T495S4) OUT OF RANGE LEGS 1 6 8 10. FMC ENGINE T/C 78273000 COMPLETED NO FAULTS FOUND.Apr 5, 2010 · N565AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA1057602Eec · faultedREF T/C 78273000 FOUND FAULT CODE 73 20012. INTERNAL EEC FAULT ON NR 2 ENG. REMOVED AND REPLACED EEC IAW MM 73 21 60 ACTUATORS TEST PASSED DISCREET TEST PASSED.Mar 24, 2010 · N565AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA1057589Probe · out of toleranceREF T/C 78273000 (ENGINE FMC CDU FAULTS). THE TOP LEFT EGT SIGNAL (T49514) IS OUT OF RANGE NR 2 ENG. VERIFIED S4 UPPER LEFT PROBE IS OUT OF TOLERANCE. REPLACED S4 PROBE ON NR 2 ENG REF MM 77 21 01, OPS NORMAL REF 71 00 00 800 811 F00. ALSO RAN NR 2 ENG ANDMar 23, 2010 · N565AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA1057477Fmc · malfunctionedON DESCENT LEFT FMC WENT BLANK FOR 30 SECONDS & THEN CAME BACK NORMALLY. PERFORMED MM 34 61 00 FMC BITE CHECKS WITH NO FAULTS NOTED. VERIFICATION FLIGHT SUCCESSFUL.Feb 28, 2010 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057374Unknown · malfunctionedWEATHER RADAR FAIL LIGHT ILLUMINATED ("WXR FAIL") ON DISPLAY UNIT (FUNCTIONED INTERMITTENTLY FOR APPROX 30 SECONDS BEFORE FAIL LIGHT ILLUMINATED). UNABLE TO CONFIRM DISCREPANCY PERFORMED SUCCESSFUL GROUND VERIFICATION IAW MM 34 43 00, NO HISTORY LAST 60 DAYS.Feb 14, 2010 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA1057185Fmc · unknownFMC DISAGREE ON GROUND IN PDX. GROUNDED YES. ACCOMPLISHED FMC DISAGREE CHECK LIST AND RESTORED TO NORMAL OPS.Dec 31, 2009 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0957159Unknown · malfunctionedAFTER LANDING AND STARTING APU NR 2 ENGINE GENERATOR TRIPPED OFF & GEN OFF BUS LIGHT ILLUMINATED. GENERATOR RESET ON FIRST ATTEMPT. OPS CHECK OF APU GEN NR 1 AND NR 2 ENG GENERATORS GOOD. BITE CHECK OF ELECTRICAL SYS SHOWS NO FAULT HISTORY ON P 5 OVERHEAD. Dec 18, 2009 · N565AS · Boeing 737890 · AC Generation SystemSDR ASAA0957130Controller · failedRIGHT PACK LIGHT ILLUMINATES ON "RECALL". EXTINGUISHES WITH MASTER CAUTION "RESET". REPLACED RAM AIR TEMP SENSOR 21 51 50/401 PRECAUTIONARY AS SENSOR AND WIRING CHECK GOOD. REPLACED NR 2 TEMP CONTROLLER REF MM 21 61 20/401. BITE TEST GOOD. OPS CHECK RT PADec 3, 2009 · N565AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA0957129Warning System · malfunctionedRT PACK LIGHT ILLUMINATED ON GROUND PRIOR TO TAKEOFF. RAN QRH, WOULD NOT EXTINGUISH. FOUND THAT RT PACK LIGHT WOULD RESET W/MASTER CAUTION. NR 2 CONTROLLER SHOWS RAM AIR SENSOR FAULT IN BIT & LAST FLT. VERIFY TEST GOOD. RESET FAULT. FAULT DID NOT RETURN.Dec 3, 2009 · N565AS · Boeing 737890 · Central WarningSDR ASAA0957113Warning System · malfunctionedRIGHT PACK LIGHT IS ON W/ RECALL. RESET W/ MASTER CAUTION RESET. REF FIM 21 62 00 810 848. NO LIGHTS OR FAULTS FOUND AFTER RECALL PERFORMED. AS PRECAUTIONARY DID BITE ON CONTROLLER. NO FAULTS FOUND. RAN PACK NO FAULTS FOUND. NO HISTORY FOR 60 DAYS. SEADec 1, 2009 · N565AS · Boeing 737890 · Central WarningSDR ASAA0957071Door · out of rigRT RAM AIR DEFLECTOR DOOR OUT OF RIG. PERFORMED BITE CHECK ON RAM DOOR SYSTEM IN GROUND AND AIR MODE OPS CHECK NORMAL. PERFORMED RAM AIR MODULATION RESTORATION PER MM 21 00 00 440 802.Nov 23, 2009 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0957053Battery · defectiveAUX BATT AMPS REMAINED AT +2 FOR ENTIRE FLIGHT. REQUEST AUX BATT CHARGER BE REMOVED FROM BATT TO SEE IF AUX BATT IS HOLDING A CHARGE. REMOVED AND REPLACED AUX MAIN BATTERY IAW MM 24 31 11 000 802 002 GROUND VERIFICATION COMPLETED SYSTEM CHECKED IAW FIM 24 31Nov 22, 2009 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA0956859Wire Harness · faultyWHILE PERFORMING TC 78273000 ENG FMC CDU FAULTS FOUND FC 77 10842, TOP RIGHT EGT SIGNAL T495S1 IS OUT OF RANGE. FOUND HIGH RESISTANCE & CORROSION ON TOP RT T495 PROBE & CONN DP0912. CLEANED CORROSION & REPLACED TOP RT NR 2 ENG T495 PROBE REF MM 77 21 01. PROct 23, 2009 · N565AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA0956824Converter · faultyFOUND MAINT BLUE LIGHT ON FOR APU. FOUND FAULT CODE 49 41244. REPLACED APU START CONVERTER UNIT REF MM 49 41 61 000 801. RAN APU & TESTS OK PER SAME REF NO FAULTS. ACCOMP FIM 49 40 TASK 806. REPLACED STARTER GENERATOR LEAK & OPS NORMAL REF M/M 49 41 21 00Oct 18, 2009 · N565AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0956775Unknown · malfunctionedWHEN "OFFSET" USED FOR LATERAL DEVIATIONS LNAV ENGAGED AIRCRAFT ASSUMES A 30 DEG ANGLE OF BANK TURN REGARDLESS OF ANGLE OF BANK SELECTED ON THE HEADING KNOB. FOUND FAULT CODE 22 11822 PERFORMED FIM 22 11 00 810 811. OPS TEST NORMAL.Oct 7, 2009 · N565AS · Boeing 737890 · Autopilot SystemSDR ASAA0956641Transceiver · failedPWS FAIL ILLUMINATED ON NAV DISPLAY. DUPLICATED FAULT TWICE. SHOW PWS FAIL WITH WXR FAIL RT. REPLACED WXR TRANSCEIVER. OPS TEST GOOD. REF MM 34 43 41. FIM 34 43 00 810 802.Sep 15, 2009 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA0956579Warning System · malfunctionedWITH RECALL SELECTED PACK LIGHT ILLUMINATES (L) WITH RESET SELECTED LIGHT EXTINGUISHES. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST ON LEFT CONTROLLER. BITE TEST GREEN PREV FLT RED RAM AIR SENSOR VER, GREEN RESET. SUBSEQUENT BITE TEST ALL GREEN. AIR CSep 9, 2009 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0956577Acm · failedLEFT PACK LIGHT ILLUMINATED AFTER LANDING DURING TAXI. LEFT PACK TEMPERATURE HIGH 85'. GROUND RAN LT PACK VERIFIED NO COOLING AIR COMING FROM LT PACK HEAT EXCHANGER. FAILED LT ACM. NEW ACM P/N VERIFIED SEAMC 2206400 2 IPC 21 51 04 01 ITEM 25J. REMOVED ANDSep 8, 2009 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0956565Filter · dirtyVERY DIFFICULT TO CONTROL AFT CABIN TEMP. FOUND AFT CABIN TEMP SENSOR FILTER VERY DIRTY. REMOVED AND CLEANED FILTER, RE-INSTALLED FILTER. PERFORMED OPERATIONAL TEST OF CABIN TEMP CONTROL REF AMM 21 61 00. OPS NORMAL AT THIS TIME.Sep 7, 2009 · N565AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0956542Transceiver · faultyWXR FAIL FLAG ILLUMINATED ON CAPTAIN ND. ACCOMPLISHED WEATHER RADAR SYSTEM BITE REF 34 43 00 810 801. NO FAULTS NOTED. DEU 1 LOGGED FAULT 31 68861 NO ARINC 708 CAPT DATA. ACCOMPLISHED TASK 31 63 00 810 822 AND 823 WITH NO FAULTS. CDS BITE OK REF 31 62 TASSep 6, 2009 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA0956413Shim · wornNR 2 ENGINE FAN BLADE SHIMS NEED REPLACED PER T/C 78472002 STEP 4. REPLACED NR 2 ENGINE FAN BLADE SHIMS WITH PREFERRED SHIMS P/N 340 252 307 0 PER T/C 78472002.Aug 17, 2009 · N565AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA0956401Unknown · malfunctionedWX STAB AND WX FAIL AMBER FLAGS ON DISPLAY WITH ASSOC ACTUAL FAILURE. SUCCESSFULLY CAME BACK TWICE AFTER CYCLING RADAR OFF THEN BACK ON. NO TRAX WEATHER RADAR ENTRIES IN 60 DAYS. PER FIM 34 43 00 810 801 PERFORMED WEATHER RADAR SYSTEM BITE PROCEDURE. OPS NAug 13, 2009 · N565AS · Boeing 737890 · Weather Radar SystemSDR ASAA0956001Connector · dirtyENGINE NR 2 WILL NOT TEST ON "B" LOOP FOR FIRE OVERHEAT DET. GROUNDED YES. CONFIRMED FAULT NR 2 ENGINE B FIRE LOOP WOULD NOT TEST. PERFORMED FIM TASK 26 10 00 810 805 FOUND DIRTY CONNECTOR DP1601, CLEANED SAME. PERFORMED ENG FIRE DETECTION OPSL TEST IAW MM 26Jun 20, 2009 · N565AS · Boeing 737890 · Fire Protection System WiringSDR ASAA0956000Terminal · damagedWHILE ACCOMPLISHING TSR813008, FOUND POSITIVE TERMINAL LUG DAMAGE AUX BATTERY CHARGER. GROUNDED YES. REPLACED TERMINAL LUG (POSITIVE) ON AUX BATT CHARGER (POSITIVE) IAW SWPM 20 30 11 OPS NML IAW MM 24 31 31.Jun 19, 2009 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA0955946Battery · failedAUX BATT AMPS REMAINED AT +2 AMPS FOR OVER 180 MINUTES. VOLTS STEADY AT 27 VOLTS. CONFIRMED BAD AUX BATT BY PULLING AUX BATT CHARGER CB BATT VOLTAGE IMMEDIATELY DROPPED. AUX BATT WAS ALSO HOT TO THE TOUCH AFTER REMOVED. REMOVED & REPLACED BOTH A/C BATTERIEJun 15, 2009 · N565AS · Boeing 737890 · Battery/Charger SystemSDR ASAA0955821Shim · wornTWENTY FOUR (24) FAN BLADE SHIMS REQUIRE REPLACEMENT DUE TO WEAR, NR 1 ENGINE. INSTALLED 24 FAN BLADE SHIMS. P/N 340 252 307 0 PER T/C 78472002.Jun 2, 2009 · N565AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA0955820Structure · nickedWHILE C/W T/C 78472002 FOUND 9 PLATFORMS P/N 340 001 816 0 WITH NICKS EXCEEDING .008 IN AREA C NR 1 ENGINE. RE-INSTALLED NEW PLATFORMS 9 EACH P/N 340 001 816 0 PER T/C 78472002 STEP 48.Jun 2, 2009 · N565AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954828Fmc · malfunctionedFMC R FAILED SELECTED FMC BOTH ON LEFT F/O'S DISPLAY RETURNED TO NORMAL. FMC NR 2 CHECKS GOOD REF MM 34 36 01 NO RECENT HISTORY, OPS NORMAL.Mar 16, 2009 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954796Hf Comm · malfunctionedARINL REPORTED NR 1 HF RADIO XSMIESIONS BROKEN SWITCHED PRIMARY FREQ TO NR 2 HF RADIO REPORTED LOUD/CLEAR. NR 1 HF SWITCHED TO DATA MODE. TESTED NR 1 HF RADIO WORKS NML REF MM 23 11 00/501. VERIFICATION FLIGHT SUCCESSFUL. OPS NORMAL.Mar 15, 2009 · N565AS · Boeing 737890 · HF Communications SystemSDR ASAA0954754Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG FOUND FAN BLADE SHIMS MISSING MOLYDAG COATING GREATER THAN 25 PERCENT REF MM 72-21-02-200-801-F00 PARA I (1)(A). 24 EA SHIMS P/N 340-252-307-0 ORDERED ON FR 16675. A CONTINUE IN SERVICE LIMIT OF 250 CYCLES IS PEMar 14, 2009 · N565AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA0954753Shroud · damagedPER TECH SVC REQUEST REINSPECT OF NR 1 ENG ABRADABLE SHROUD. FOUND DAMAGE TO BE OUT OF SERVICEABLE LIMITS REF AMM 72 24 02 200 801 STEP F (1) PARAGRAPH (E) 1A CUMULATIVE DAMAGE TO BE GREATER THAN 1.5 FOR A CIRCUMFENTIAL DEFECT. MIG 2 C 235588 INIT (02030) ABRMar 12, 2009 · N565AS · Boeing 737890 · Turbine Section
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