N566AS

Service difficulty reports · 575

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 = 'N566AS' 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 ASAA2017041920490Apu · malfunctionedAPU FAULT LIGHT ILLUMINATED ON 1ST APU START ATTEMPT AT FL360. RAN QRH , FAULT LIGHT WENT OUT WITHIN 5 MINS. ACFT GROUNDED. APU BITE TEST SHOWS MSG 49-31171 FUEL CONTROL UNIT FLOW DISAGREES WITH COMMAND. APU DID START ON 2ND ATTEMPT IN FLIGHT PER SEAMC. PERApr 19, 2017 · N566AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2017032120243Fairing · brokenNR 2 ENGINE 3 O`CLOCK FAIRING LOOKS CRACKED. ACFT GROUNDED. FOUND SCREW MISSING UPPER CORNER OF FAIRING AND A CRACK AROUND LOWER SCREW. REMOVED THE FAIRING IAW AMM 73-21-06. REPLACED TWO BROKEN NUTPLATES IAW SRM 51-40-02. INSTALLED FAIRING IAW AMM 73-21-06Mar 21, 2017 · N566AS · Boeing 737890 · Nacelle/Pylon StructureSDR ASAA2017022419919Warning Light · false activationLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. LIGHT GOES OUT WITH RESET. ACFT GROUNDED. TRIED MASTER CAUTION RECALL ON GROUND. LIGHT DOES NOT ILLUMINATE. PERFORMED PACK TEMPERATURE CONTROL BITE ON NR 1 CONTROLLER AND FOUND NO FAULTS. CHECKED GOOFeb 24, 2017 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017021919856Motor · failedLEFT CENTER FUEL PUMP LOW PRESSURE ILLUMINATED DURING CLIMB. ACFT GROUNDED. REMOVED AND REPLACED LEFT CENTER TANK BOOST PUMP IAW AMM 28-22-41. OPS AND LEAK CHECKED GOOD.Feb 19, 2017 · N566AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2017021419814Control Valve · faultyRIGHT PACK LIGHT ON RECALL RESETS WITH MASTER CAUTION. GROUNDED - YES. BITE TEMP CONT SHOWS ON NR 2 SIDE TCV THIS PACK V141. REPLACED RT PACK TEMP CONTROL VALVE PER AMM 21-51-10. LK AND OPS CHECK GOOD. CLEARED MEL 21-32B.Feb 14, 2017 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017021419813Unknown · malfunctionedFLT CREW REPORTED RT HAND PACK LT ON. GROUNDED - YES. REF FIM 21-62 TASK 801 PERFORMED PACK TEMP CONT BITE. FOUND TCV FAULT. REF FIM 21-62 TASK 831. RESET RT HAND TCV FAULT BITE TEST NOW PASSES WITH NO FAULTS. OPERATED RT PACK FOR 15 MINS, PACK OPS NORMAL. NO Feb 14, 2017 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017011919469Valve · faultedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED DURING RECALL. ACFT GROUNDED. ACCOMPLISHED A PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 801. FOUND FLT DECK TRIM VALVE FAULT LATCHED. RESET LATCH. OPS NORMAL.Jan 19, 2017 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016123119202Unknown · malfunctionedHF NR 2 FAIL. GROUNDED - YES. PERFORMED FIM 23-11 TASK 802 HF CONTROL INPUT FAIL. RESET AND OPS CHECK GOOD.Dec 31, 2016 · N566AS · Boeing 737890 · HF Communications SystemSDR ASAA2016120819095Transition Panel · corrodedAFT PIT, LT TRANSITION CORRODED FROM FS 787-800. FS 787 - FS 800. GROUNDED - YES. REMOVED CORROSION, ORIG. MAT. =.040, REMOVED .011, REMAINING =.029, FOUND TO BE OUT OF LIMITS FROM STA 727+4 TO STA 847 IAW SRM 53-00-53-1A-2, REMOVED AND REPLACED. TRANSITION PADec 8, 2016 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016120819093Transition Panel · corrodedAFT PIT, RT TRANSITION CORRODED AT FASTENER HOLES FROM FS 727+4 TO 767. GROUNDED - YES. BLENDED AWAY CORROSION AND CHECKED LIMITS IAW SRM 53-00-53-1A-2. AREA OF CORROSION 144 IN LX 3.5 IN W AND ORIG THICKNESS .040. REMOVED .006 AND REMAINING MAT'L .034 WHICHDec 8, 2016 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016120819075Floor Support · corrodedRIGHT SIDE FLOOR SUPPORT CORRODED BS 500A - 500I, RBL 48 - 55. ACFT GROUNDED. REMOVED DAMAGE IAW SRM 53-00-53-1A-2.2.D. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2.4.A. REPAIRED DAMAGE SECTION IAW SRM 53-00-53-2R-5.Dec 8, 2016 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016120719078Door Sill · corrodedAFT CARGO DOOR SILL HAS CORROSION IN SEVERAL AREAS. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-15-1A-1. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED & REPLACED THE DOOR SILL WEB IAW SRM 51-40-02, DWG 146A8123 REV C & 146A8340 REV A.Dec 7, 2016 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016120719049Skin · crackedCRACK INDICATION AT HSS 129.5, APPROX. 1 INCH IN LENGTH, 4 INCHES AFT OF EXISTING REPAIR EDGE. ACFT GROUNDED. LOCATED AND REMOVED DAMAGE AREA IAW SRM 55-10-01, FABRICATED FILLER AND DOUBLER IAW SRM 55-10-01-2R-11, ALODINED AND PRIMED FILLER AND DOUBLER IAW SRDec 7, 2016 · N566AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016120418926Filter · cloggedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL, EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. REMOVED AND REPLACED A CLOGGED FILTER AND CLEANED TEMP SENSOR. ACCOMPLISHED PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 801, FAULTED FLT DECK TRIM VALVE ODec 4, 2016 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016112518795Control Module · failedCABIN AIR SUPPLY DUCT TEMP INDICATOR SEEMS TO HAVE ERRONEOUS INDICATIONS, MOVING SELECTOR SWITCH WITHIN DETENT CAUSES ERRATIC INDICATIONS. ACFT GROUNDED. REMOVED & REPLACED TEMPERATURE CONTROL MODULE IAW AMM 21-61-15-400-801. OPS NORMAL.Nov 25, 2016 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016112218814Probe · failedNR 2 MAIN FUEL TANK FAILS SYSTEM TEST IAW FQIS SYSTEM TEST IAW AMM 28-41-00-730-801. ACFT GROUNDED. DRAINED NR 2 FUEL AND TAGGED EXTERNAL POWER. REMOVED AND REPLACED NR 2 COMP PROBE (F15), F1 TANK UNIT AND F8 TANK UNIT IAW AMM 28-41-21-400-801. REMOVED AND RNov 22, 2016 · N566AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016112218813Control Unit · failedNR 1 MAIN FUEL TANK FAILS FQIS SYSTEM TEST, IAW AMM 28-41-00-730-801. ACFT GROUNDED. ACCOMPLISHED NR 1 FUEL TANK FQIS TANK AND COMP UNIT TEST IAW AMM 28-41-21-710-801. FOUND TANKS UNITS F1, F2, F6 AND F10 TO BE OUT OF LIMITS. REMOVED NR 1 MAIN FUEL TANK WINNov 22, 2016 · N566AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016101318335Sensor · failedTEMP LIGHT & MASTER CAUTION ON AFTER START. ACFT GROUNDED. REMOVED AND REPLACED FLT DECK CABIN TEMP SENSOR, PERFORMED BITE CHECK OF ZONE TEMP CONTROLLERS BITE CHECK PASSED IAW AMM 21-61-10.Oct 13, 2016 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016093018150Warning Light · false activationZONE TEMP ILLUMINATED ON RECALL LIGHT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED ZONE TEMP CONTROLLER BITE ON BOTH CONTROLLERS IAW AMM 21-61-00, ZONE TEMP CONTROLLER NR 2 FAULTED "FLT DECK TRIM VALVE", CLEANED FLT DECK SENSOR AND FILTER,Sep 30, 2016 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016090619048Floor Panel · damagedAFT CARGO BAY CENTER FLOOR PANEL BS 767 - 887 HAS EDGE DAMAGE AT BOTH FWD AND AFT EDGES. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610 REV E AND INSTALLEDSep 6, 2016 · N566AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016082417789Controller · malfunctionedWITH MASTER CAUTION RECALL RT PACK LIGHT ILLUMINATES. PACK LIGHT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. RESET NR 2 CONTROLLER, TCV FAULT. ACCOMPLISHED BITE TEST OF BOTH PACK/ZONE TEMP CONTROLLER. NO FAULTS NOTED.Aug 24, 2016 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016082217779Lens · detachedMID CABIN OVERHEAD EXIT SIGN PLASTIC COVER CAME OFF. ACFT GROUNDED. REATTACHED MID CABIN OVERHEAD EXIT SIGN AS REQUIRED, OK FOR CONTINUED SERVICE.Aug 22, 2016 · N566AS · Boeing 737890 · Emergency LightingSDR ASAA2016081117682Panel · looseNR 1 ENGINE FAN DUCT PANEL AT 1:00 POSITION HAS LOOSE BOLTS. ACFT GROUNDED. TIGHTEN LOOSE SCREWS IAW AMM 72-23-07.Aug 11, 2016 · N566AS · Boeing 737890 · Nacelle/Pylon, Main FrameSDR ASAA2016080117582Battery · malfunctionedAUX BATTERY SHOWS 27 VOLTS AND A 2 AMP CHARGE THROUGHOUT THE FLIGHT. ACFT GROUNDED. PERFORMED BATTERY INSTALLATION TEST FOR AUX BATTERY IAW AMM 24-31-11 AND AUX BATTERY CHARGER OPS TEST IAW AMM 24-31-31. ALL TESTS NORMAL. P5-13 BITE NORMAL, NO MESSAGES LOGGAug 1, 2016 · N566AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2016060216935Circuit Breaker · trippedCIRCUIT BREAKER P6-2 A2 AFCS INTERLINK IS TRIPPED. ACFT GROUNDED. RESET CIRCUIT BREAKER IAW AMM 20-60-01 AND WDM 22-11-12 ACCOMPLISHED DFCS LIBRARY TEST 32 TEST PASSED AND CIRCUIT BREAKER REMAINED SET.Jun 2, 2016 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA2016052216817Satcom · lockedSATCOM LOCK-UP, DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS, RESTORED NORMAL.May 22, 2016 · N566AS · Boeing 737890 · Communications SystemSDR ASAA2016051516742Lens · detachedMID CABIN EXIT SIGN FELL DOWN. ACFT GROUNDED. REATTACHED MID CABIN OVERHEAD EMERGENCY EXIT LENS TO ASSY. LIGHTS OP GOOD IAW AMM SUB-TASK 33-51-00.May 15, 2016 · N566AS · Boeing 737890 · Emergency LightingSDR ASAA2016051316709Control Panel · failedALTITUDE ALERT KNOB WILL NOT SET ON MCP PANEL. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34. GROUND VERIFICATION TEST PASSED.May 13, 2016 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA2016050616631Filter · cloggedFWD CABIN TEMP CONTROLLER REQUIRES MUCH HIGHER POSITION TO MAINTAIN NORMAL TEMP - SOMEWHAT ERRATIC. ACFT GROUNDED. BITE CKD BOTH ZONE CONTROLLERS REF FIM 21-62, TASK 801, NO FAULTS LOGGED. FOUND FWD ZONE FILTER CLOGGED. CLEANED FILTER AND OPS CHECKED REF AMay 6, 2016 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016040116199Lens · detachedEXIT SIGN AT ROW 16/17 FELL OFF. ACFT GROUNDED. REINSTALLED OVERHEAD EXIT SIGN AT ROW 16.Apr 1, 2016 · N566AS · Boeing 737890 · Emergency LightingSDR ASAA2016032916144Circuit Breaker · trippedAFCS INTERLINK NR 2 CIRCUIT BREAKER TRIPPED. P6-2-A2, AFCS ENGAGE INTERLINK CIRCUIT BREAKER TRIPPED, P18-1-D3. ACFT GROUNDED. PERFORMED GVI OF AREA BEHIND P6-2 AND P18-1, RESET CIRCUIT BREAKERS IAW AMM 20-60-01-860-801. ACCOMPLISHED FIM 22-13/821, MAINTENANCMar 29, 2016 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA2016031615967Switch · failedLEFT THROTTLE LEVER, TAKEOFF WARNING SYSTEM INTERMITTENT. ACFT GROUNDED. R & R LEFT AUTOTHROTTLE SWITCHPACK ASSY, REF AMM 76-11-020-802-F00 AND AMM 76-11-07-400-802-F00. ACCOMPLISHED AUTOTHROTTLE SWITCHPACK ASSY TEST, REF AMM 76-11-07-400-802-F00 PARA, H, ALMar 16, 2016 · N566AS · Boeing 737890 · Power LeverSDR ASAA2016030815848Heater · leakingENGINE NR 2 FUEL LEAK NOTED ON WALK AROUND. ACFT GROUNDED. PERFORMED ENGINE RUN ON NR 2 ENGINE. DURING ENGINE RUN NOTED A LEAK OF 8 DROPS PER MINUTE COMING FROM THE MAIN HEAT EXCHANGER OIL FUEL DRAIN LINE, DRIP IS WITHIN LIMITS IAW AMM 71-71-00-200-801 PARAMar 8, 2016 · N566AS · Boeing 737890 · Fuel HeaterSDR ASAA2016022415657Terminal · looseB LOOP ON RT CORE DETECTOR HAS LOOSE TERMINAL, ALMOST BROKE, UPPER RT. ACFT GROUNDED. REPAIRED DETECTOR TERMINAL LUG. OPS NORMAL, REF AMM 26-11-02.Feb 24, 2016 · N566AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2016021115431Acoustic Panel · wornREF T/C 78472000, NR 2 ENGINE AFT ACOUSTICAL PANEL, 7-8 O`CLOCK ALF, FWD CENTER FASTENER WORN THROUGH PANEL. ACFT GROUNDED. R & R NR 2 ENGINE AFT ACOUSTICAL PANEL 7-8 O`CLOCK POSITION REF AMM 72-23-02.Feb 11, 2016 · N566AS · Boeing 737890 · Nacelle/Pylon, Main FrameSDR ASAA2016021115430Spinner · wornREF T/C 78472002, NR 2 ENGINE FRONT SPINNER BLACK ANODIZED COATING WORN TO LIMITS. ACFT GROUNDED. R & R NR 2 ENGINE FRONT SPINNER REF T/C 78472002.Feb 11, 2016 · N566AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016020815341Warning Message · false activationFMC DISAGREE AFTER PUSHBACK. POWER INTERRUPTION AT THE GATE WHEN RAMP PULLED GROUND POWER BEFORE APU, ON THE BUS. ACFT GROUNDED. ACCOMPLISHED FMC RESET PROCEDURES IAW QRH. NORMAL FMC OPERATION RESTORED.Feb 8, 2016 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016010714694Warning Message · false activationFMC DISAGREE ON CAPT & F/O ND ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC DISAGREE NO LONGER DISPLAYED.Jan 7, 2016 · N566AS · Boeing 72782 · Flight Management Computing Hardware SystemSDR ASAA2015122914555Eec · failedWHILE ACCOMPLISHING T/C 78273000 FOUND THE FOLLOWING SHORT TERM FAULT ON NR 2 ENGINE 73-21272 ALT VOLTAGE INPUT TO THE ELECTRONIC ENGINE CONTROL IS OUT OF RANGE. MUST BE CORRECTED WITHIN 50 FLT HOURS. ACFT GROUNDED. FOUND FAULT STILL ACTIVE IN ELECTRONIC ENGIDec 29, 2015 · N566AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015121614299Regulator · malfunctionedON DESCENT PASSING 39000" GOT A RT ENGINE BLEED TRIP. ACCOMPLISED QRH PROCEEDURE, LIGHT WENT OUT AFTER PUSHING THE TRIP RESET BUTTON. AFTER TRIP THE RT DUCT PRESSURE WAS 10 PSI AND LT DUCT PRESSURE WAS 30 PSI. ACFT GROUNDED. PERFORMED ENGINE BLEED AIR SYS HDec 16, 2015 · N566AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015121414271Line · looseRIGHT BLEED TRIP OFF LIGHT CAME ON. DID QRH PROCEDURE AND RESET. OPS NORMAL. ACFT GROUNDED. PERFORMED FIM TASK 36-10, TASK 801. FAILED STEP F10, 3 FOUND CONTROL PRESSURE SENSE LINE ON THE PRSOV TO BE LOOSE AND LEAKING. TIGHTENED SENSE LINE NO FURTHER LEDec 14, 2015 · N566AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015120214077Sensor · dirtyAIR TEMP SUPPLY DUCT SWITCH DOES NOT READ CORRECTLY WHEN SWITCH IS IN AFT POSITION. TEMP GAGE VARIES BETWEEN 20-40 DEGREES C. ACFT GROUNDED. REPLACED FILTER AND CLEANED TEMP SENSOR, ACCOMPLISH BITE ON BOTH ZONE TEMP CONTROLLERS NO FAULTS REF AMM 21-61-00.Dec 2, 2015 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015112514002Warning Message · activatedFMC CDU INTERROGATION FOR FAULTS IAW TASK CARD 78273000, FOUND MSG 73-31372, UPPER EGT SECTORS READING HIGH, ECONOMIC FAULT NR 2 ENGINE GROUNDED.Nov 25, 2015 · N566AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2015112213942Battery Pack · dischargedEMERGENCY LIGHTS AT ROW 16, 22 ON ACFT RT, ROW 16 ACFT LT AND AFT CEILING IN GALLEY FAILED OPS CHECK IAW TASK CARD 78233001, ACFT GROUNDED. R & R 5 BATTERY PACKS.Nov 22, 2015 · N566AS · Boeing 737890 · Emergency LightingSDR ASAA2015112213924Eec · failedREF TC 78273000 FOUND SHORT TERM FAULT MSG 73-21272, THE ALTERNATOR VOLTAGE INPUT TO THE ELECTRONIC ENGINE CONTROL IS OUT OF RANGE, NR 2 ENGINE. ACFT GROUNDED. FAULT MSG OCCURRED ON FLT 0-10. ACCOMPLISHED FIM 73-27, TASK 804. RESISTANCE CHECKS AT ALTERNATONov 22, 2015 · N566AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015112013908Connector · dirtyDURING COMPLETION OF TC 78273000, FOUND FAULT 73-21272, "THE ALTERNATOR VOLTAGE INPUT TO THE ELECTRONIC ENGINE CONTROL IS OUT OF RANGE" SHORT TIME FAULT, NR 2 ENGINE, ESN 895-406, ACFT GROUNDED. PERFORMED FIM 73-27, TASK 804. FOUND DIRTY CONNECTOR AT NR 2 B Nov 20, 2015 · N566AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2015102913574Engine · faultedNR 2 ENGINE HAS ECONOMIC FAULT 73-31372, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ON DEFERRAL.Oct 29, 2015 · N566AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015101513520Fault Code · activatedWHILE ACCOMPLISHING T/C 78273000, FOUND ECONOMIC FAULT ON NR 2 ENGINE FAULT 73-3172 UPPER EGT SECTORS READING HIGH. 3RD FLT LEG. ACFT GROUNDED. RE-ACCOMPLISHED T/C78273000, NO CURRENT FAULTS LOGGED OR IN HISTORY.Oct 15, 2015 · N566AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015100913430Warning Message · false activationHAD SINGLE FMC OPERATION ON SCRATCHPAD MESSAGE WITH MAP FLAG ON F/O'S SIDE BUT NO VTK FLAG. ACFT GROUNDED. CAPT`S AND F/O'S FMC SYSTEMS, OPS CHECKED NORMAL IAW MM 34-61-00-710-801.Oct 9, 2015 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015100613373Panel · looseNR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION FOUND NR 1 FAN FRAME PANEL AT RT 12 O'CLOCK POSITION AND NR 5 FAN FRAME PANEL HAS ONE FASTENER LOOSE AND HAS DAMAGED THE PANEL. ACFT GROUNDED. REPLACED FAN DUCT PANEL AT RT 12 O'CLOCK, IAW AMM 72-23-07.Oct 6, 2015 · N566AS · Boeing 737890 · Nacelle/Pylon, Main Frame
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