GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  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 VNAA0512018Sensor · failedDURING CRUISE THE APU OIL TEMP CAUTION MESSSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND, DUE TO A RT IDG MEL AND WEATHER AT BNA, DIVERTED TO TYS. MAINTENANCE REMOVED & REPLACED THE APU HIGH OIL TEMPERATURE SENSOR. THE APU OPERATIONALLY CHECKED GOOD. THEDec 23, 2005 · N216PS · Cndair CL6002B19 · APU Oil SystemSDR VNAA0512019Proximity Sensor · contaminatedDURING CLIMBOUT THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL FROM THE MAIN CABIN DOOR AND THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED INTERMITTENTLY. THE CREW FOLLOWED THE QRH, RETURNED TO FAY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A GOB OF CHEWDec 23, 2005 · N259PS · Cndair CL6002B19 · Door Warning SystemSDR ASOA051138Battery Pack · misinstalledDURING A GROUND INSPECTION, THE LT AND RT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY BATTERY PACK AND CHARGER AND FOUND IT INSTALLED INCORRECTLY. REINSTALLED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT ODec 22, 2005 · N924EV · Cndair CL6002B19 · Emergency LightingSDR ASOA051135Coalescer Bag · odorDURING TAKEOFF, THE CREW RECEIVED A (SMOKE TOILET) CAUTION MESSAGE WITH THE LAVATORY SMOKE DETECTOR PREVIOUSLY DEFERRED. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFELY. MAINTENANCE CLEANED OIL FROM BOTH PACKS AND REMOVED AND REPLACED THE COALESCEDec 21, 2005 · N873AS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0512016Pitot System · contaminatedTHE TAKEOFF WAS ABORTED WHEN THE CREW RECEIVED AN IAS MISCOMPARE WARNING. MAINTENANCE INSPECTED THE PITOT STATIC SYSTEMS FOR CONTAMINATION AND FOUND WATER IN THE NR 2 ADC PITOT DRAIN COLLECTOR TUBE. THE P2 LINE WAS PURGED. THE PITOT SYSTEM TESTED & LEAK CHEDec 20, 2005 · N229PS · Cndair CL6002B19 · Pitot/Static SystemSDR A6WA200540357Landing Gear · malfunctionedAFTER GEAR RETRACTION, NOSE GEAR WOULD NOT RETRACT, GEAR RETRACTION HORN SOUNDED. C/W QRH LANDED IN MSP AT 42000. MEL`D GEAR RET SYS FUNCTION TESTED GEAR SYS. PERFORMED GEAR DISAGREE TEST, FULLY SERVICED NLG STRUT.. PERFORMED LANDING GEAR EXT/RETRACT FUNCTDec 20, 2005 · N442AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR ASOA051128SStructure · corrodedDURING A C-CHECK, THE FS 409+128 TO FS 559.00, AND RBL36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. MAINTENANCE REPAIRED THE FS 409+128 TO FS 559.00, AND RBL 36 TO FLOOR STR IAW REO. (K)Dec 20, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051132SStep · brokenDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 20, 2005 · N914EV · Cndair CL6002B19 · Entrance StairsSDR ASOA051126SFloor Support · corrodedDURING A C-CHECK, THE FS409+128 TO FS 559.00 AND LBL36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FS 409+128 TO FS 559.00, AND LBL 36 TO FLOOR STR, IAW REO, IT WAS FOUND TO BE WITHIN LIMITS. (Dec 19, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA051222003Blades · damagedRT ENG IFSD WHEN AT FLT LVL 30,000 FT, CREW REPORTED EXCESSIVE VIBRATION ON RT ENG WAS FELT AND THEN SHUT DOWN ON ITS OWN. CREW THEN FOLLOWED QRH, DECLARED EMERGENCY AND DID A SINGLE ENGINE LANDING WITH NO FURTHER INCIDENT. A LOT OF BLADES DAMAGED INSIDE INLDec 19, 2005 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA200540355Computer · failedRT AOA HEAT FAIL MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED ADHC NR 2 (AIR DATA HEAT CONTROLLER) IAW AMM. OPS TEST GOOD. (K)Dec 18, 2005 · N454AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR VNAA0512013Apu · failedDURING DESCENT THE CREW RECEIVED THE APU OVERTEMP AND LAV SMOKE WARNINGS. SMOKE WAS REPORTED IN THE CABIN AND COCKPIT. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND NO LEAKS OR EXTERNADec 18, 2005 · N241PS · Cndair CL6002B19 · APU Core EngineSDR VNAA0512014Warning Light · unknownTHE FLAPS FAIL MESSAGE ILLUMINATED WHEN FLAPS WERE AT 25 SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET & TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL 00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WDec 18, 2005 · N250PS · Cndair CL6002B19 · Flight Control SystemSDR A6WA200540365Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR2 UNDER PNL 510AB AT WS 12.245 HAS CORROSION ON IB SIDE APPROX 3 INCH L X .1 INCH W X .004 DEEP IN NON CRITICAL AREA. MAINTENANCE REPAIRED WING PLANK ACCESS HOLE AT WS 12.245 IAW REO. (K)Dec 18, 2005 · N433AW · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA051120SFrame · corrodedDURING A C-CHECK, THE FRAME AT FS 605, BETWEEN STR 27 AND STR 26L, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME AT FS 605, BETWEEN STR 27 AND STR 26L, IAW SRM 51-25-06 AND 51-25-16. (K)Dec 18, 2005 · N840AS · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500222Engine · malfunctionedRIGHT ENGINE LOW OIL PRESSURE ON DESCENT 25PSI, ENGINE SHUTDOWN.Dec 17, 2005 · N650BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200540364Skin · damagedDAMAGE TO FUSELAGE SKIN AT FS640-FS700 STRINGER 18, 19 LT SIDE. MAINTENANCE REMOVED DAMAGE SKIN BETWEEN FS 640- FS 700 AND STRINGER 18 - 19L. FABRICATED DOUBLER AND FILLERS AND INSTALLED IAW EO. (K)Dec 17, 2005 · N433AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA051110SFloor Support · corrodedDURING A C-CHECK, THE FLOOR SUPPORT CAP AT RBL 9, BETWEEN FS 559+64 AND FS 559+80, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR SUPPORT CAP AT RBL 9, BETWEEN FS 559+64 AND FS 559+80, IAW SRM 51-21-06, IT WADec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051109SFloor Skin · corrodedDURING A C-CHECK, THE RT SIDE PRESSURE FLOOR SKIN, AT FS 515.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RT SIDE PRESSURE FLOOR SKIN, AT FS 515.00, IAW SRM 51-21-11 AND 51-42-06, IT WAS FOUND TO BE WITHIN LIDec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA051111SFloor Support · corrodedDURING A C-CHECK, THE FLOOR SUPPORT CAP AT LBL27, FS 574.00 TO FS621, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CAP AT LBL 27, FS 574.00 TO FS 621, IAW SRM 51-42-06 AND 51-42-21. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051112SFloor Skin · corrodedDURING C-CHECK, THE PRESSURE FLOOR SKIN OB OF LBL 9, BETWEEN FS 449.85 AND FS 559+2, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE PRESSURE FLOOR SKIN OB OF LBL 9, BETWEEN FS 449.85 AND FS 559+2, MAINTENANCE DETERMINED IT WAS NOT CORRDec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA051113SFloorbeam · corrodedDURING A C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEN THE RT SIDE FLOOR SILL AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 559+80, BETWEEN THE RT SIDE FLOOR SILL AND RBL 27.00, IAW SRM. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA051114SSeat Track · corrodedDURING C-CHECK, THE FORWARD AND AFT FLOOR TRACKS, AT RBL 27.00, NEAR THE LAVATORY, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT FLOOR TRACKS, AT RBL 27.00, NEAR THE LAVATORY. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA051115SFloor Support · corrodedDURING A C-CHECK, THE FLOOR SUPPORT CAP, AT FS589, LBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE FLOOR SUPPORT CAP, AT FS 589, LBL 9, MAINTENANCE DETERMINED THERE TO BE NO CORROSION AFTER CLEANING THE AREA. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051116SFloorbeam · corrodedDURING A C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEN RBL 9.00 AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 559+80, BETWEEN RBL 9.0 AND RBL 27.00, IAW SRM. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA051117SSeat Track · corrodedDURING C-CHECK, ALL FLOOR TRACKS AT LBL 9 AND RBL 9 HAVE APPARENT CORROSION. MAINTENANCE REMOVED AND REPLACED THE FLOOR TRACKS AT LBL 9 AND RBL 9 IAW SRM. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA051118SSill · corrodedDURING C-CHECK, THE RT SIDE SILL, FROM FS 559+64 TO FS 621.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RT SIDE SILL, FROM FS 559+64 TO FS 621.00, IAW REO, IT WAS FOUND TO BE WITHIN LIMITS. (K)Dec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051119SFloor Support · corrodedDURING C-CHECK, THE FLOOR SUPPORT BEAM CAP AT RBL 9.0, BETWEEN FS 589.00 AND 605, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE FLOOR SUPPORT CAP AT RBL 9.0, BETWEEN FS 589.00 AND 605, MAINTENANCE FOUND NO CORROSION AFTER CLEANING THEDec 17, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0512026Access Panel · missingAFTER FLIGHT THE RT ENGINE NOSE COWL UPPER ACCESS PANEL WAS DISCOVERED MISSING. MAINTENANCE INSTALLED A SERVICEABLE PANEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 16, 2005 · N229PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA051102SBeam · corrodedDURING A C-CHECK, THE LT SIDE STA 349 TRANSVERSE BEAM, UPPER SURFACE AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE ALODINED, PRIMED, AND PAINTED THE LT SIDE STA 349 TRANSVERSE BEAM UPPER SURFACE, AT THE PASSENGER DOOR, IAW SDec 16, 2005 · N840AS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA0512012Skin · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE IN CRUISE AT 15000 FT WITH GEAR AND FLAPS UP. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT HORIZONTAL STABILIZER AND THE LOWER AFT FUSELAGE. ALL DAMAGE WASDec 15, 2005 · N254PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA051098SSill · corrodedDURING C-CHECK, THE PASSENGER DOOR SILL WAS FOUND TO BE CORRODED. AFTER MAINTENANCE ALODINED, PRIMED, AND PAINTED THE PASSENGER DOOR SILL IAW SRM, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K)Dec 15, 2005 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051100SSkin · crackedDURING A C-CHECK, THE LT SIDE OF THE NOSE LANDING GEAR CUTOUT RADIUS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT SIDE OF THE NOSE LANDING GEAR CUTOUT RADIUS IAW REO. (K)Dec 15, 2005 · N840AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA051222002Fuel Control · malfunctionedDURING FLT, DURING DESCENT, RT THRUST LEVER ON RT ENG WAS UNRESPONSIVE AND THAT IND REMAINED AT 40% EVEN AFTER CREW EXERCISED BOTH THRUST LEVER'S POSITION TO CONFIRM THAT RT ENGINE WAS NON-RESPONSIVE. CREW THEN FOLLOWED QRH PROCEDURES, SHUT DOWN RT ENGINE, DEDec 15, 2005 · Cndair CL6002B19 · Fuel Controlling SystemSDR REXA200500157Fuel Control · defectiveON DESCENT, THE FLIGHT CREW DISCOVERED THAT THE RT ENGINE WAS UNRESPONSIVE TO THRUST LEVER INPUTS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE DISCOVERED THE MAIDec 14, 2005 · N824AY · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR REXA200500156Engine · damagedWHEN LEVEL AT FL300 THE RT ENGINE SHUTDOWN. FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND SEVER DAMAGE TO THE ENGINE'S FAN SECTION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. DAMAGED ENGINE WIDec 14, 2005 · N8560F · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA051222001Contactor · burnedPILOT EXPLAINED THAT AT ABOUT 24,000 FEET BEGAN EXPERIENCING ELECTRICAL FAILURES AND LOST AC BUS 2 AND GEN 2. DURING ATTEMPT TO RESET GEN 2 AND BUS 2 HE BEGAN LOSING GEN 1 AND BUS 1 AT THIS TIME PROBABLY AFTER LOSING ESSENTIAL BUS ADG DEPLOYED. AFTER TALKINGDec 14, 2005 · Cndair CL6002B19 · Electrical Power System WiringSDR CA060103002Windshield · crackedFOUND LEFT WINDSHIELD CRACKED. LEFT WINDSHIELD REMOVED AND REPLACED ACCORDING AMM PROCEDURE.Dec 14, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540354Apu · odorSTRONG SMELL OF JET FUEL AFTER APU START IN FLIGHT APU SHUTDOWN. PERFORMED OPS TEST AND LEAK CHECK OF APU. OPS TEST GOOD AT THIS TIME, IAW AMM. NO LEAKS NOTED. NO FAULT CODES NOTED AFTER INTEROGATION OF ECU, OPS CHECK ACM SYSTEM. NO FUEL SMELL NOTED AT THDec 11, 2005 · N429AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA200540352Flap System · failedFLAPS FAILED AT 20 DEGREES ON APPROACH. NO DEFECTS NOTED. (K)Dec 10, 2005 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540351Actuator · failedDEPARTING FLAPS FAIL MSG. WHEN FLAPS WENT FROM 8-0 DEGREES PERFORMED QRH RETURNED. WORK ORDER 90809, REMOVED AND REPLACED NR 3 AND NR 4 FLAP ACTUATORS ON RT WING TRIPPED IAW AMM. OPS CHECK GOOD. (K)Dec 9, 2005 · N418AW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR MASA200501014Element · leakingASH 7012 GSP - ANTI-ICE WARNING ON TAKEOFF RIGHT FUSELAGE SHOWS RED. AIRCRAFT FERRIED TO CAE. MAINTENANCE REPLACED THE BLEED TEMP CONTROL UNIT AND SECURED SENSING ELEMENT.Dec 9, 2005 · N75999 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA051212001Relay · overheatedAT FL230, ALL THE TUBES EICAS AND PFD'S WENT BLANK THEN FLASHED ON AND OFF. NEXT AC BUS1 CAUTION MESSAGE. LEFT AUTO TRANSFER FAIL AND GENERATOR 1 OFF CAUTION. COCKPIT HAD ELECTRICAL OVERHEATING SMELL. NO SMOKE VISIBLE IN COCKPIT OR CABIN. COMPLETED THE QRH Dec 8, 2005 · Cndair CL6002B19 · Electrical Power SystemSDR A6WA200540349Bracket · bentNOSE DOOR WARNING MESSAGE AND GEAR DISAGREE MESSAGE. INSPECTED AND FOUND NOSE GEAR CENTERING/ EXTENDED PROX SENSOR BRACKET BENT. REMOVED AND REPLACED BRACKET IAW CMM. PERFORMED GEAR SWING IAW AMM. OPS CHECK NORMAL. ALL INDICATIONS ARE NORMAL. (K)Dec 7, 2005 · N434AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200540350Door · missingON CLIMB OUT, FELT LURCH. UPON INSPECTION, DISCOVERED LT ENGINE DOOR MISSING. REMOVED AND REPLACED LT LOWER COWL DOOR. (PN 228-50081-141). (K)Dec 7, 2005 · N468AW · Cndair CL6002B19 · Engine Cowling SystemSDR VNAA0512008Warning Light · illuminatedDURING APPROACH WHEN FLAPS WERE SELECTED FROM 20 TO 30 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFDec 7, 2005 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540353Apu · smokeREQUEST INSPECTION OF APU COMPARTMENT DUE TO EXTREME AMOUNT OF SMOKE AFTER AUTO SHUTDOWN. INSPECTED APU AW CRJ AMM. NO DEFECTS NOTED. (K)Dec 6, 2005 · N429AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200540347Intercostal · crackedLT SIDE FS621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. REMOVED AND REPLACED INTERCOSTAL, PN 601-35012-51, IAW REO (UNREADABLE). (K)Dec 5, 2005 · N470ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA051066SHinge · corrodedDURING A C-CHECK, THE PASSENGER DOOR TOP STEP UPPER HINGE HALF WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP UPPER HINGE. (K)Dec 5, 2005 · N882AS · Cndair CL6002B19 · Entrance StairsSDR ASOA051054Intercostal · crackedDURING A C-CHECK, THE INTERCOSTAL AT FS 484, RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Dec 4, 2005 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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