Pratt & Whitney Canada PW118

Service difficulty reports · 873

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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 engine_model_key = 'PW118'
  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 ESPA202510010675Engine · fireTRANSPORTING PASSENGERS FROM KNTD TO KNSI. ONCE THE ACFT BEGAN CLIMBING TO CRUISE ALTITUDE, CAPT & 1ST OFFICER NOTICED SIGNS OF A LT ENGINE FAILURE & RESPONDED TO AN ENGINE FAILURE. FA1 NOTIFIED CAPT OF THE ENG FIRE, & CAPT ATTEMPTED TO PUT OUT THE FIRE WHILEOct 1, 2025 · N405PA · Emb EMB120ER · Engine (Turbine/Turboprop)SDR 2025F00223Engine · fireON JUNE 12TH, 2025, PHOENIX AIR GROUP, INC. (PAG) WAS TRANSPORTING PASSENGERS FROM POINT MUGU NAVAL AIR STATION (KNTD) TO SAN NICOLAS ISLAND NAVAL OUTLYING FIELD (KNSI) USING AIRCRAFT N405PA. ONCE THE AIRCRAFT BEGAN CLIMBING TO ITS CRUISE ALTITUDE, CAPTAIN 1Jun 12, 2025 · N405PA · Emb EMB120 · Engine (Turbine/Turboprop)SDR HKGA20230623001Engine · failedDURING TAKEOFF, LH ENG T6 OVER HEAT, ENGINE WAS SHUT DOWN AS A PRECAUTION. SMOKE WAS PRESENT IN THE COCKPIT. UPON WALKAROUND OIL WAS PRESENT ON THE EXTERIOR OF ENGINE COWING. MAINTENANCE PERFORMED A BORESCOPE AND IDENTIFIED OIL IN THE COMBUSTION CHAMBER WITH PJun 23, 2023 · N235SW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR JIKA2022102601Oil System · lowDURING CRUISE FLIGHT, GOT A MASTER WARNING AND THE OIL PRESSURE FOR RT ENGINE BEGAN TO FLICKER AND EVENTUALLY DROPPED BELOW 40 PSI. FOLLOWED QRH PROCEDURE & PREFORMED ENGINE SHUT DOWN. PILOT DID DECLARE AN EMERGENCY. DIVERTED TO MMIO, LANDED WITHOUT INCIDENT. Oct 26, 2022 · N567SW · Emb EMB120ER · Turbine Engine Oil SystemSDR HALA2022062800121None · noneETOPS - ENG 2 EIU FAULT // REMOVED AND REPLACED ENGINE SEL SW (6KS) PER TSM 73-25-00-810-425A & PERFORMED OPS TEST OF EIU 1 AND 2 PER AMM 73-25-34. OPS GOOD. 6/27/22 19845. PENDING ENGINE RUN. PERFORMED ENG 1 & 2 IDLE RUN. CHECK GOOD. NO FAULTS. OK FOR SVC.Jun 27, 2022 · N209HA · Airbus A300* · Engine Fuel and ControlSDR HALA2022061500113None · noneDESCENDING THOUGHT 5,000' - 3,000 ' ENGINE AT IDLE EXPERIENCE DIRTY SHOCK SMELL AGAIN // FOUND EVIDANCE OF OIL LEAK ON #1 ENG AT 9 O CHOCK POSITION IN THE FIC REPLACED SEAL FROM LP62 OIL PRESSURE TUBE REF AMM PW 10006-C-72-00-30-00A-702A-B LEAK CHECK GOOD 1843Jun 14, 2022 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2022061300112None · noneETOPS - ECAM ENG 2 AIR SYS FAULT DESCENDING THROUGH 12,000' // REMOVED AND REPLACED #2 ENGINE BUFFER AIR VALVE PER AMM 75-26-04, PERFORMED TEST 3 IDLE RUN PER AMM 71-00-00, NO DEFECTS NOTED, SYSTEM CHECKED NORMAL. OK FOR SERVICE.Jun 10, 2022 · N217HA · Airbus A321271N · Compressor Bleed ValveSDR JIKA2021062901Hmu · failedWHILE CRUISING AT 10,000 FEET, WITHOUT WARNING THE NUMBER 2 ENGINE FAILED. FIRST OFFICER CALLED OUT "POWER LOSS" ON NUMBER 2, MEMORY ITEMS AND QRH WERE COMPLETED. ATC AND DISPATCH WAS ADVISED. KRIV WAS CHOSEN AS NEAREST SUITABLE AIRPORT, SINGLE ENGINE APPROACHJun 29, 2021 · N179CA · Emb EMB120 · Engine (Turbine/Turboprop)SDR FXGAEMBN568SWCabin Pressure · erraticCABIN ALTITUDE WARNING CAME ON DURING DEPARTURE OUT OF KOGD TO KLRP. RETURNED TO DEPARTURE AIRPORT (KOGD). PERFORMED PRESSURIZATION SYSTEM OPERATIONS CHECK NORMAL, REFERENCE EMB 120 MM CH 21-30-01.Nov 26, 2020 · N568SW · Emb EMB120ER · Cabin Pressure Control SystemSDR JIKA202006231801Transmitter · defectiveAFTER DEPARTING KPDX THE CREW HAD JUST COMPLETED THEIR CRUISE CHECKLIST AND WHILE FLYING AT THE NORMAL CRUISE ALTITUDE OF 15,000 FEET WHEN THE RIGHT ENGINE OIL PRESSURE BEGAN TRENDING TOWARD LOW PRESSURE. WITHIN 30 SECONDS, THE RIGHT ENGINE OIL PRESSURE SETTLEJun 18, 2020 · N266AS · Emb EMB120ER · Engine Oil PressureSDR KCQA201911010001Eec · malfunctionedDURING FLIGHT RH ENGINE EEC FAILURE ANNUNCIATED WITH POWER REDUCTION TO ZERO PERCENT TORQUE. CREW PERFORMED QRH PROCEDURE, UNABLE TO RESTORE POWER ABOVE FLT IDLE. AIRCRAFT DIVERTED TO SUITABLE AIRPORT WITH PROPELLER IN FEATHER. AFTER LANDING ENGINE POWER AND EOct 7, 2019 · N121CZ · Emb EMB120ER · Fuel Controlling SystemSDR JIKA2019091001Hmu · erraticTHE FLIGHT CREW REPORTED THAT AT APPROXIMATELY 800-1000' AGL, THE LT PROPELLER INADVERTENTLY FEATHERED. THE FLIGHT CREW RAN THE "INADVERTENT PROPELLER FEATHER" QRH AND WAS ABLE TO UNFEATHER THE PROPELLER, PERFORMED A PRECAUTIONARY AIR RETURN WITH BOTH ENGINES Sep 3, 2019 · N567SW · Emb EMB120ER · Fuel Control/Turbine EnginesSDR 2018F00120Hub · fracturedENGINE REMOVED FOR HIGH N2 VIBRATION & HPC STAGE 8 DAMAGED. AFT HUB, KNIFE-EDGEED FRACTURE CONFIRMED.Jun 26, 2018 · Engine (Turbine/Turboprop)SDR 2016FA0000463Duct · tornAPPROX 1245 LOCAL TIME, WHEN RT "DUCT LEAK" LIGHT ILLUMINATED. CREW SECURED THE RT ENGINE BLEED VALVE AND RT AC PACK, WAITED THREE MINUTES FOR COOL DOWN AND ANNUNCIATOR TO EXTINGUISH. "DUCT LEAK" LIGHT DID NOT EXTINGUISH. CREW SECURED RT ENGINE IN FLIGHT ANSep 28, 2016 · N410PA · Emb EMB120 · Air Distribution SystemSDR 2015FA0000467Sending Unit · malfunctionedAFTER 35 MINUTES AT FL150, PILOT OBSERVED LOW FUEL PRESSURE AND LOSS OF TORQUE. AFTER PARKING, TECH TRIED TO START ENGINE BUT THE RESULT WAS NEGATIVE. CONFIRMED THE MAIN FUEL QUANTITY INDICATOR AND THE RT FUEL INDICATOR MEASURES WERE ERRONEOUS REGARDING TO TSep 28, 2015 · Emb EMB120ER · Fuel Quantity SensorSDR JIKA2015091401Engine · power lossSHORTLY AFTER TAKEOFF, THE PILOT HEARD A LOUD BANG FROM THE RT ENG & LOST POWER. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN OF THE RT ENG, RETURNED & LANDED WITHOUT INCIDENT. THE RT ENG IS BEING REPLACED. A FOLLOW UP TO THIS SDR WILL BE SUBMITTED WHEN A TEAR Sep 14, 2015 · N201YW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR JIKA2015091301Wire · brokenSHORTLY AFTER TAKEOFF, THE PILOT OBSERVED THE LT ENG, DUCT LEAK ANNUNCIATOR LIGHT ILLUMINATED & AURAL WARNING SOUNDED. THE PILOT FOLLOWED PROCEDURES IN QRH & PERFORMED PRECAUTIONARY IN FLIGHT SHUT DOWN OF THE LT ENG. PILOT DECIDED TO RETURN & LANDED WITHOUT Sep 13, 2015 · N257AS · Emb EMB120ER · Engine Indicating System WiringSDR 2015FA0000468Sensor · failedAFTER 35 MINUTES AT FL150, PILOT OBSERVED LOW FUEL PRESSURE AND LOSS OF TORQUE. AFTER PARKING, TECHS TRY TO START ENGINE BUT THE RESULT WAS NEGATIVE. CONFIRMED THAT THE MAIN FUEL QUANTITY INDICATOR AND THE RT FUEL INDICATOR MEASURES WERE ERRONEOUS REGARDINGAug 31, 2015 · Emb EMB120ER · Fuel Quantity SensorSDR GN0A20150624001Access Panel · unsecureON TAKEOFF, CREW RECEIVED SERVICE DOOR LIGHT & AURAL WARNING. TAKEOFF WAS ABORTED & ACFT RETURNED TO GATE. CREW FOUND FASTENER ON PRESS REFUELING ACCESS PANEL NOT SECURED. PANEL WAS SECURED & WARNING LIGHT EXTINGUISHED. ACFT RETURNED TO SERVICE.Jun 23, 2015 · N654CT · Emb EMB120ER · Wing, Plate/SkinSDR GN0A20150320001Warning System · false activationDURING TAKEOFF ROLL ABOVE V1, CREW RECEIVED A FLAP ASYMMETRY WARNING ON THE OTBD FLAP PANELS. THE CREW FOLLOWED PROCEDURES & CONTINUED THE TAKEOFF THEN RETURNED TO THE AIRPORT & LANDED WITHOUT FURTHER INCIDENT. PERFORMED FLAP OPERATIONAL TEST & CYCLED THE FLMar 20, 2015 · N654CT · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR GN0A20150222001Unknown · malfunctionedWHILE ON DESCENT, PASSING THROUGH FLIGHT LEVEL 180, THE CABIN PRESS STARTED TO CLIMB TO 10000’. THE CREW USED THE PRESSURIZATION CONTROL SWITCH TO CHANGE CABIN PRESS CONTROL FROM AUTO TO MANUAL. THE CONTROL IS A THREE POSITION GUARDED SWITCH WITH SETTINGS AUFeb 22, 2015 · N653CT · Emb EMB120ER · Cabin Pressure Control SystemSDR FAA2015120900010Blade · crackedCRACK INDICATION OF FILLET RADIUS OF BLADE SHANK, FOUND DURING MAJOR INSPECTION.Dec 9, 2014 · N652CT · Emb EMB120RT · Propeller Blade SectionSDR SWIA201439483Indicator · faultyLOST LT ENGINE OIL PRESSURE INDICATION DURING CRUISE. INDICATION RETURNED WHEN AT IDLE BUT WENT AWAY AT POWER. REPLACED LT OIL PRESSURE TRANSDUCER AND GAUGE.Oct 12, 2014 · N234SW · Emb EMB120ER · Engine Oil Indicating SystemSDR GN0A20141003001Processing Unit · failedWHILE ON TAKEOFF ROLL THE CAPTAIN REPORTED HIS EADI DISPLAY WENT BLANK. THE TAKEOFF WAS ABORTED & THE ACFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. THE LT DPU HAD FAILED. A SERVICEABLE UNIT WAS INSTALLED WITH THE SYS CHECKING NORMAL IAW THE ACFT MM. Oct 2, 2014 · N652CT · Emb EMB120ER · Integrated Flight SystemSDR GN0A20140824001Access Panel · unsecureSHORTLY AFTER DEPARTURE THE DOOR WARNING LIGHT ON OVERHEAD PANEL ILLUMINATED ALONG WITH AN AURAL WARNING ACTUATION. THE ACFT RETURNED & LANDED WITHOUT INCIDENT. THE PRESS REFUELING ACCESS PANEL WAS FOUND IN AN UNSECURE POSITION. THE PANEL WAS SECURED & THE Aug 24, 2014 · N654CT · Emb EMB120ER · Wing, Plate/SkinSDR SWIA201439199Control Unit · malfunctionedRT PROPELLER OVERSPEED AFTER TAKEOFF. CREW SAW 103.5 PERCENT WHEN THEY SHUT THE ENGINE DOWN. RETURNED TO DEPARTURE. R & R RT ENGINE PROPELLER CONTROL UNIT IAW AMM. OPS CHECKED GOOD.Aug 21, 2014 · N581SW · Emb EMB120ER · Propeller Controlling SystemSDR FXGA201408221431Skin · crackedTO REPAIR A CRACK ON THE FUSELAGE SKIN AT FS 2389 AT CENTERLINE. CUT OUT DAMAGE & INSTALL REPAIR DOUBLER ISE RDT2014-120-06-15-20 & EMAIL TITLED EDT2014-120-061520. PERMANENT REPAIR INSPECTION REQUIRED. INTERNAL & EXTERNAL DETAILED INSPECTION REQUIRED AT EVAug 20, 2014 · N1105G · Emb EMB120FC · Fuselage Main, Plate/SkinSDR SWIA201439154Governor · malfunctionedDURING CLIMBOUT, THE CREW NOTICED THE PROPELLERS SUDDENLY FELT OUT OF SYNC. CAPTAIN NOTICED THE RT PROPELLER AT 103 PERCENT. ACFT RETURNED TO THE FIELD. REPLACED RT PROPELLER OVERSPEED GOVERNOR. SYS OPS NORMAL.Aug 18, 2014 · N581SW · Emb EMB120ER · Propeller GovernorSDR SWIA201437647Pcu · out of adjustWITH CL AT MAX LEFT NP CONSISTENT AT 101.5 PERCENT. ADJUSTED LT PCU SPEED CONTROL SCREW .2500" COUNTER CLOCKWISE IAW CMM.May 14, 2014 · N234SW · Emb EMB120ER · Propeller Controlling SystemSDR SWIA201437103Skin · crackedRIGHT ENGINE TOP COWL, WHERE THE FORWARD INBD DOOR HOLD OPEN ROD ATTACHES HAS A CRACK APPROXIMATELY 1.5" LONG. REPAIRED 1.5" LONG CRACK ON HALF FRAME. LOCATED ON RT ENGINE TOP COWL BY FWD INBD DOOR HOLD OPEN ROD ATTACHES IAW ETD.Apr 11, 2014 · N224SW · Emb EMB120ER · Nacelle/Pylon, Plate/SkinSDR SWIA201437102Mount · chafedLEFT ENGINE INBD FRONT MOUNT CHAFED AFT OF MOUNTING BOLT. REPLACED LT ENG FWD INBD UPPER MOUNT IAW SRM AND AMM.Apr 10, 2014 · N224SW · Emb EMB120ER · Engine Mount SectionSDR GN0A20140327001Flap · malfunctionedAFTER TAKEOFF THE CREW SELECTED THE FLAPS UP, THE INBD & NACELLE PANELS RETRACTED TO 0° WHILE THE OTBD PANELS REMAINED AT 15° TAKEOFF POSITION. THIS CONDITION CAUSED THE FLAP DISAGREEMENT WARNING TO ACTIVATE. THE ACFT RETURNED TO FRG & LANDED WITHOUT INCIDENMar 26, 2014 · N654CT · Emb EMB120ER · Trailing Edge Flap Control SystemSDR GLBA2014011000365Oil System · low pressurePILOT REPORTED THAT DURING FLIGHT, NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED & THEN WENT OUT. THE ENGINE OIL PRESSURE WAS BETWEEN 40-55 & FLUCTUATING, POWER WAS REDUCED TO IDLE & PROP FEATHERED. THE ENGINE OIL PRESSURE NEVER WENT BELOW 40. EMERGENCY DEJan 9, 2014 · N293UX · Emb EMB120ER · Engine Oil Indicating SystemSDR CA140107001Blade · cracked(CAN) DURING ROUTINE HOT SECTION INSPECTION OF THE ENGINE A SINGLE BLADE WAS FOUND WITH A CRACK IN THE RIVET SLOT AREA OF THE FIR TREE. THE BLADES HAD ACCUMULATED 9268.5 HRS. TSN. THE BLADES WERE INSTALLED IN THIS ENGINE AT 3038.5 HOURS TSN IN 2004 AND HAVE AJan 7, 2014 · Turbine SectionSDR GN0A11182013Relay · faultyFLIGHT 652 ACY TO ORF WHILE TAXING FOR TAKEOFF THE APU GEN DROPPED OFF LINE. THE FLIGHT CREW FOLLOWED QRH PROCEDURES & RESET THE GEN WHICH CAME BACK ON LINE. ON CLIMB OUT THE APU GEN AGAIN DROPPED OFF LINE. THE CREW SHUTDOWN THE APU AS THE RT EADI & EHSI DINov 17, 2013 · N652CT · Emb EMB120ER · DC Generating SystemSDR GN0A020130701001Unknown · malfunctionedWHEN LANDING GEAR SELECTED UP AFTER TAKEOFF, ALL GEAR REMAINED DOWN AND LOCKED WITH CORRESPONDING DISAGREEMENT LIGHTS (BOTH GREEN & RED) ILLUMINATED ON THE LANDING GEAR SELECTOR INDICATOR. CYCLED THE GEAR SELECTOR HANDLE THREE TIMES WITH THE SAME RESULTS. FOLJun 28, 2013 · N652CT · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR GLBA2013042900244Wire · loosePILOT REPORTED THAT THE WHITE EMERGENCY LIGHT AT ROW 6, LT SIDE IS INOPERATIVE. MX REPAIRED A LOOSE WIRE AT THE CONNECTION, OPS CHECKED GOOD.Apr 27, 2013 · N96ZK · Emb EMB120ER · Light System WiringSDR SWIA201435820Line · chafedLT ENG OIL PRESSURE WARNING LIGHT, AURAL WARNING & FLUCTUATING INDICATION, SHUT DOWN ENG. FLT 7400 CHAFED LINE BETWEEN OIL COOLER & ENG.Jan 28, 2013 · N581SW · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)SDR FXGA201212260001Control Unit · leakingNR 2 OIL PRESSURE WAS FLUCTUATING BETWEEN 55-40 PSI. NR 2 OIL PRESSURE AURAL WARNING ENGINE "OIL" SHUTDOWN. REPLACED NR 2 PCU IAW MM 61-21-00. GROUND OPS AND LEAK CHECK GOOD. PCU WAS FOUND TO BE LEAKING EXTERNALLY AT REAR OF UNIT.Dec 18, 2012 · N1110J · Emb EMB120FC · Turbine Engine Oil SystemSDR GN0A20121110001Line · looseKCMH TO CMI: ON TAKEOFF ROLL THE MASTER WARNING ILLUMINATED "LEFT ENGINE OIL" ALONG WITH THE AURAL WARNING "ENGINE OIL" ACTIVATED. THE TAKEOFF WAS ABORTED AND AFTER THE LEFT ENGINE WAS SHUT DOWN, OIL WAS SEEN LEAKING FROM THE LEFT ENGINE. MAINTENANCE FOUND Nov 10, 2012 · N650CT · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)SDR FXGA20121030001Attach Angle · crackedDURING INSPECTION, FOUND RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT THE AFT PRESSURE BULKHEAD.Oct 26, 2012 · N1110J · Emb EMB120FC · Vertical Stabilizer, Attach FittingsSDR GN0A10042012001Engine · oscillatesFLIGHT 17155 KFRG-KACY: AFTER TAKEOFF AND WHILE CLIMBING THROUGH 5000FT THE RIGHT ENGINE STARTED OSCILLATING WITH AN AIRCRAFT YAWING MOTION. THE RIGHT NP WAS FLUCTUATING BETWEEN 97% AND 104% WITH THE ASSOCIATED ENGINE TORQUE FLUCTUATING 72% TO 84%. THE CREWOct 4, 2012 · N650CT · Emb EMB120ER · Engine (Turbine/Turboprop)SDR GN0A20120930001Control Panel · failedAUO TO (UOX): AFTER TAKEOFF WHILE CLIMBING THROUGH 3500FT THE AUTO-PILOT WAS ENGAGED. WHEN PASSING 5000FT THE LEFT FLIGHT DIRECTOR BARS PITCHED DOWN 2.5° WHICH CAUSED THE AUTO-PILOT TO COMMAND THE AIRCRAFT FOLLOW. THE LEFT AUTO-PILOT WAS DISENGAGED AND AIRCSep 30, 2012 · N652CT · Emb EMB120ER · Flight ControllerSDR SWIA201231748Bearing · failedRIGHT PROPELLER HUB LEAKING OIL. INSPECTED AND FOUND RIGHT PROPELLER NR 4 BEARING RACE FAILURE CAUSING DAMAGE TO RIGHT PROPELLER HUB. REPLACED RIGHT PROPELLER HUB AND ACTUATOR. P/N OFF: 782501-8 S/N OFF: 1785.Sep 8, 2012 · N236SW · Emb EMB120ER · Propeller Hub SectionSDR GN0A07032012Unknown · malfunctionedTHE LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TNN. CREW SELECTED THE LANDING GEAR DOWN AND ALL THREE GEAR INDICATED DOWN AND LOCKED. THE AIRCRAFT RETURNED TO TNN AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM WITH THE AIRJul 3, 2012 · N651CT · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR GN0A05282012Control Panel · contaminatedFLIGHT 15976 (MER) TO (GCN): WHILE CLIMBING THROUGH 11,000FT THE AUTO-PILOT ENGAGED WITHOUT THE CREW SELECTING THE SYSTEM ON. NEITHER CONTROL WHEEL A/P DISCONNECT SWITCH WOULD DISENGAGE THE AUTO-PILOT. THE FIRST OFFICER HAD TO HOLD DOWN THE DISCONNECT BUTTOMay 28, 2012 · N650CT · Emb EMB120ER · Autopilot SystemSDR GLBA201203281Fan · smokeA/C PACKS SMOKE ON GROUND. MX REPLACED THE LT GROUND COOLING FAN, OPS CHECKED GOOD REF MM 21-51-03.Mar 28, 2012 · N297UX · Emb EMB120ER · Air Distribution FanSDR GN0A201204010324Fuel Filter · dirtyON TAKEOFF FROM ATLANTIC CITY (ACY), CREW RECEIVED AN AURAL WARNING CHIME ALONG WITH WARNING LIGHT ON THE MULTIPLE ALARM PANEL FUEL AND THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTMar 24, 2012 · N651CT · Emb EMB120ER · Engine Fuel DistributionSDR FXGA20120323001Skin · corrodedDURING HEAVY MX, FOUND LOWER BELLY SKIN, CORRODED IN SEVERAL SPOTS. SKIN WAS REPLACED.Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Plate/SkinSDR FXGA20120323002Stringer · corrodedDURING HEAVY MX, FOUND LT PROFILE STRINGER CORRODED. STRINGER WAS REPLACED.Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Longeron/Stringer
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