GE CF34-8C1

Service difficulty reports · 1,415

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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 = 'CF348C1'
  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 QXEA2010040900237Frame · corrodedC-CHECK - CORROSION FOUND ON FWD WEB SIDE OF FRAME 295.00 AROUND STGR 26R CUTOUT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, BLENDS WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-21-06-001-001-AApr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040900238Web · corrodedC-CHECK - CORROSION FOUND ON R/H WEB AT FS 280.00. BLENDED CORROSION, FOUND BLENDS TO BE OUT OF LIMITS IAW SRM 53-11-10-991-805. REMOVED WEB IAW SRM 57-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED ALL FASTENER HOLES IN NEW WEB IAW SRM 51-40-11-001-0Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010040900239Floorbeam · corrodedC CHECK -LT AND RT SIDE OF 280 BEAM SHOWS SIGNS OF CORROSION. BLENDED CORROSION RT 280 BEAM IAW SRM 51-11-00-001-001-A01. FOUND BEAM TO BE CRACKED. REMOVED BEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. CUT NEW 280 BEAM. PERFORMED LPI ON CUTLIApr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010040900240Floorbeam · corrodedC CHECK- COCKPIT PANEL FLOOR SUPPORT ANGLE AT FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION, FOUND CORROSION OUT OF LIMITS IAW SRM5300-00-001-A01 PAGE 3. LOCATED FASTENER HOLE IN NEW ANGLE IAW SRM51-40-11-001-001-A01. INSTALLED NEW A IAW SRM 51-42-21-Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201000500Heater · burnedAFTER T/O A LOUD POP FROM F/O WINDOW FOLLOWED BY STRONG ELECTRICAL SMELL AND SMALL AMOUNT OF SMOKE. RETURN TO DEPARTURE, ALSO RECEIVED R WINDOW HEAT CAUTION. EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O.Apr 7, 2010 · N331CA · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR ASOA201000510Placard · peelingEXIT PLACARD LAMINATED PEELING OFF. REMOVED UNSERVICEABLE EXIT PLACARD. CLEANED AREA WITH SOLVENT SOAKED RAG. INSTALLED NEW SERVICEABLE PLACARD IAW IPC 11-30-02 IG 1K ITEM 145 FOR LOCATION OF NEW PLACARD.Apr 7, 2010 · N355CA · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201000531Seat Track · corrodedUPON FURTHER INVESTIGATION NOT ALL CORROSION WAS REMOVED FROM SIDE SEAT RAIL SECTION BETWEEN FS 785 AND 827 ON RT HANDSIDE. JUST AFT OF EMERG EXIT, NEW TRACK INSTALLED IAW AMM 25-26-01-000-801-A02. (CLOSED)Apr 7, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20100500Window · burnedR & R F/O'S WINDOW IAW AMM 56-12-01 REFER TO AFDL 537395-2FOR LEAK AND OPS CHECKS. (CLOSED)Apr 7, 2010 · N331CA · Cndair CL6002C10 · Flight Compartment WindowsSDR QXEA2010040700224Seat Track · corrodedC CHECK - EVIDENCE OF CORROSION ON RT SIDE SEAT TRACK FROM FS 677.00 TO FS 708.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. TREATED IAW REO 670-53-00-13.Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040700225Seat Track · corrodedC CHECK - EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 784.00 TO FS 863.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. ETCHED AND ALODINED LT SIDE SEAT TRACK IAW SRM 51-21-11-001-001-A01.Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040700227Structure · chafedC CHECK - CHAFING AT STR 27 FS 977.00 UNDER PANEL DL. BLENDED OUT DAMAGED AREA IAW SRM 51-12-00-001-001-A01. BLEND FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-14. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01. ETCHED AND ALODINED IAW SRM 51-21-11-001-001-A0Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010040600222Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 485 TO 572 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUT ALL CORROSION TO .024" DEEP BY .375 WIDE BY 2" LONG. ORIGINAL MATERIAL THICKNESS IS .105", REMAINING MATERIAL AFTER BLENDING .081" CORROSApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600221Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 379 TO 485 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUTT ALL CORROSION TO .031" DEEP BY 1.0" WIDE BY 1.0" LONG. ORIGINAL MATERIAL THICKNESS IS .105" REMAINING MATERIAL AFTER BLAND .074" CORROSApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600220Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON LT SIDE SEAT TRACK FROM FS 485 TO 572. BLENDED LT SIDE SEAT TRACK FS 485 TO 572 CORROSION. ORIGINAL THICKNESS .110, BLENDED .020 MAX ALLOWABLE .035", REMAINING MATERIAL .090" FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013. EApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040700223Seat Track · corrodedC CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK RT FROM FS 572-669.4. BLENDED OUT ALL CORROSION FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-13. TREATED IAW REO 670-53-00-13.Apr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000492Charger · defectiveFOUND THE CTR LIGHTED CEILING EXIT SIGN FWD DIRECTION, CABIN EMERGENCY FLOODLIGHT 2, AND THE EXTERIOR EMERGENCY LIGHT 3 ARE ALL INOP. R & R NR 1 EPSU BATTERY CHARGER IAW AMM 33-51-17. OPS CHECK GOOD AT THIS TIME.Apr 5, 2010 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA20100493Priority Valve · failedR & R NLG PRIORITY VALVE IAW AMM 32-33-15,OPS CK GOOD, NO FURTHER DEFECTS NOTED. ACFT OK FOR FURTHER SERVICE. (CLOSED)Apr 5, 2010 · N753EV · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR QXEA2010040600214Skin · chafedC-CHECK - LT UPPER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED CHAFE DAMAGE ON UPPER L/E AT AILS 365.00 IAW SRM 51-12-00-001-001-A01. BLEND IS A MAX 2.0 INCH LONG AND .75 INCH WIDE. REMAINDER MAX OF .005 OUT OF ORIGINAL .090. BLEND IS WITHIN LIMITS IAW SRApr 4, 2010 · N614QX · Cndair CL6002C10 · AileronsSDR QXEA2010040600215Skin · chafedC-CHECK - RT LOWER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED DAMAGE ON THE RT LOWER L/E SKIN AT AILS 330.68 AND AILS 370.66 TO A SMOOTH AND DAMAGE FREE CONDITION IAW SRM 51-12-00-001-001-A01. ALL BLENDS ARE WITHIN LIMITS IAW SRM 57-61-01-101-001-A01. ETCApr 4, 2010 · N614QX · Cndair CL6002C10 · AileronsSDR ASOA201000481Seat Track · gougedRIGHT FLOOR SEAT TRACK AT FS 597.00 TO FS 629.00 GOUGED AND CORRODED (MARKED). BLENDED OUT CORROSION IN MARKED LOCATIONS ON RT FLOOR SEAT TRACK BETWEEN FS 597.00 AND FS 629.00 AND FOUND TO BE OUT OF LIMITS SO REMOVED IAW AMM 53-00-49-000-801. INSTALL NEW SEApr 2, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000482Floor Skin · corrodedRIGHT FLOOR WEB HAS CORROSION IN MULTIPLE LOCATIONS FROM APPROX FS 1015 TO 1088.2 (MARKED). REPAIRED IAW REO 670-53-61-586.Apr 2, 2010 · N355CA · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA201000483Web · corrodedCORROSION FOUND ON LT LOWER WEB AT FS 280 BETWEEN LBL 10 & LBL 13. REMOVED CORROSION FOUND ON LT LOWER WEB. ALL WORK DONE IAW SRM 53-11-10-201-003-A01. THICKNESS CHECK REQUIRED TO ENSURE THAT MIN WEB THICKNESS OF .0035" WAS NOT EXCEEDED. PERFORMED UT THICKNApr 2, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000484Web · corrodedCORROSION FOUND ON RT LOWER WEB AT FS 280 BETWEEN RBL 11 & RBL 13. REMOVED CORROSION FROM RT LOWER WEB. ALL WORK DONE IAW SRM 53-11-10-201-003-A01. PERFORMED UT THICKNESS INSP OF BLEND AREA ON RT LOWER WEB IAW NDT INSP PROCEDURE UT-3 MINIMUAL MATERIAL REMAApr 2, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000494Floor Support · corrodedCOCKPIT FLOOR SUPPORT ANGLE HAS CORROSION AT FS 280. REMOVED CORROSION FROM COCKPIT FLOOR SUPPORT ANGLE ALL WORK DONE IAW SRM 53-00-00-101-A01 AND SRM 51-12-00-001-001-A01. THICKNESS CHECK NEEDED TO ENSURE THAT THE MIN THICKNESS OF .057" IS NOT EXCEEDED. PERApr 2, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000462Sill · corrodedPAX DOOR SILL ANGLE CORRODED. REMOVED ASD DOOR MID CAP, SILL ANGLE, FWD AND AFT SILL ANGLES, AND FWD AND AFT ASD HANDRAILS BRACKETS IAW SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01. DRILLED UP ASD SILL ANGLE AND INSTALLED ASD SILL ANGLE, FWD AND AFT, SILL Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000464Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 673 AND 713 ON RT SIDE HAS CORROSION IN MULTIPLE LOCATIONS (MARKED). BLENDED OUT CORROSION IN MARKED LOCATIONS ON SIDE SEAT RAIL SECTION APPROX BETWEEN FS 673 AND 713 ON RT SIDE IAW SRM 53-41-49-101-001-A01. EVALUATED SIDEApr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000465Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 673 AND 713 ON THE LT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED CORROSION FROM LT SIDE SEAT RAIL BETWEEN FS 673 AND FS 713 AT ALL MARKED LOCATIONS SEAT TRACK FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SRM 53-41-49-10Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000466Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 713 AND 761 ON THE RT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. (MARKED). BLENDED OUT CORROSION IN MARKED LOCATIONS ON SIDE SEAT RAIL SECTION APPROX. BETWEEN FS 713 AND 761 ON THE RT SIDE IAW SRM 53-41-49-101-001-A01. EVALUATApr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000467Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 713 AND 761 ON THE LT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED CORROSION FROM LT SIDE SEAT RAIL SECTION BETWEEN FS 713 AND FS 761 IN ALL MARKED LOCATIONS REWORKED SEAT TRACK IS FOUND TO BE SERVICEABLE. ALL WORK DONE Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000468Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 785 AND 827 ON THE RT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. BLENDED OUT CORROSION IN MARKED LOCATIONS ON SIDE SEAT RAIL APPROX BETWEEN FS 785 AND 827 ON THE RT SIDE IAW SRM 53-41-49-101-001-A01, TP161741 2. EVALUATED SIDApr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000469Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 827 AND APPROX 861 ON THE RT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. BLENDED OUT CORROSION ON SIDE SEAT RAIL SECTION APPROX BETWEEN FS 827 AND 861 ON THE RT SIDE IN MARKED LOCATIONS IAW SRM 53-41-49-101-001-A01, TP161741 2.Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000470Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN APPROX FS 861 AND 969 ON THE RT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. BLENDED OUT CORROSION IN MARKED LOCATIONS ON SIDE SEAT RAIL SECTION BETWEEN APPROX FS 861 AND 969 ON THE RT SIDE IAW SRM 53-41-49-101-001-A01, TP161741. Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000471Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 785 AND 860 ON THE LT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. BLENDED CORROSION ON LT SIDE SEAT TRACK BETWEEN FS785 AND FS860 FOUND SEAT TRACK PN SH670-36260-3 TO BE OUT OF LIMITS. PART UNSERVICEABLE ALL WORK DONE IAW SRM Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000472Seat Track · corrodedSIDE SEAT RAIL SECTION BETWEEN FS 860 AND 969 ON THE LT SIDE HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED CORROSION FROM LT SIDE SEAT RAIL SECTION BETWEEN FS 860 & FS 969 IN ALL MARKED LOCATIONS REWORKED AREAS ARE FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SApr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000477Crossbeam · corrodedCROSSBEAM FS 349.00 AT RT BEAM HAS CORROSION. (OPEN)Apr 1, 2010 · N355CA · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201000478Bracket · crackedANGLE BRACKET CRACKED AT FS625.30 AND S14L. R & R ANGLE BRACKET AT FS 625.30 & STR 14L IAW SRM 51-40-11.Apr 1, 2010 · N972EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000479Attach Fitting · crackedBS 280 FRAME CLIP AT LBL9 IS CRACKED. REMOVED CRACKED FRAME CLIP & REPLACED WITH NEW AT STA 280, LBL 9 IAW SRM 53-21-43.Apr 1, 2010 · N972EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA201000460Frame · corrodedFS 280.00 BETWEEN STG 17 RT & STG 17 LT HAS CORROSION IN SEVERAL PLACES AND ON THE FWD ENDS OF THE LT & RT BEAMS. REMOVED DAMAGED 280 CROSSBEAM IN REF SP670BA-53-026 AND IS MOD 670531100026, JR161744 4. CUT 280 CROSSBEAM TO MAC & LIT IKE INSTALLATION ALL WORK Mar 31, 2010 · N355CA · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201000475Door Frame · corrodedFWD AVIONICS BAY DOOR SEAL MATTING SURFACE AT FS 364.00 BETWEEN STG 20LT AND STG R 20RT THERE IS CORROSION AND PITTING. BLENDED CORROSION & PITTING ON AVIONICS BAY DOOR SEAL MATING SURFACE. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREAS ON AVIONICS DOOR SMar 31, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000476Intercostal · corrodedFWD OF FS 364.00 BETWEEN S26L & S26R THERE IS CORROSION. REMOVED 15 RIVETS THROUGH OUTER SKIN, REMOVED 3 RIVETS FROM ANGLE-ATTACHMENT, REMOVED 7 LOCK FASTENERS FROM GUSSET, REMOVED 4 LOCK FASTENERS FROM PROXIMITY SWITCH BRACKET, REMOVED RT LATCH PIN INTERCOSTMar 31, 2010 · N355CA · Cndair CL6002C10 · Fuselage Structure (General)SDR ASOA201000457Channel · corrodedCORROSION FOUND ON NUTPLATE CHANNEL BRACKET WHICH IS ATTACHED TO THE BACKSIDE OF FS 280 FRAME AND AT STR27 AND ALSO SECURES FLOORBOARD 141ALF. (OPEN)Mar 30, 2010 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000458Structure · corrodedCORROSION FOUND AT FS 280 AND IN BETWEEN STR 26R AND 25R ON FLOOR. (OPEN)Mar 30, 2010 · N355CA · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201000453Placard · wornCREW ESCAPE HATCH EXTERNAL PLACARDS WORN BD 161723 03/22/10 (LT 03/23/10) (OPEN)Mar 29, 2010 · N355CA · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201000454Light · inoperativeAFT CEILING EMERGENCY FLOOD LIGHT INOP.Mar 29, 2010 · N751EV · Cndair CL6002C10 · Emergency LightingSDR QXEA2010040200210Relay · malfunctionedRT ENG DEGRADED CAUTION AFTER SELECTION OF WING ANTI-ICE. RETURNED TO FIELD. LANDING WEIGHT 66,000. DESCENT RATE LESS THAN 300 AIRSPEED 135. LANDING UNEVENTFUL. R & R K2 & K22 RELAYS - OPS CK GOOD IAW AMM 24-05-07-710-801. RETURNED TO SERVICE.Mar 29, 2010 · N611QX · Cndair CL6002C10 · Power Indicating SystemSDR ASOA201000440Glowstrip · wornFLOOR TRACK GLOWSTRIPS ARE WORN AT LT OVERWING EXIT FWD STRIP & RT OVERWING EXIT AFT STRIP. REMOVED AND REPLACED LT OVERWING EXIT FWD FLOOR TRACK GLOWSTRIP AND RT OVERWING EXIT AFT FLOOR TRACK GLOWSTRIP IAW AMM 33-51-01. OK FOR SVC.Mar 27, 2010 · N379CA · Cndair CL6002C10 · Emergency LightingSDR ASOA201000441Handle · unsecurePASSENGER DOOR LATCH CAUTION MESSAGE RECEIVED AFTER TAKEOFF ACCOMPANIED BY PROX SYS FAULT 1 MESSAGE AND RED DOOR HANDLE MECHANICAL INDICATING RED AND PAX DOOR WARNING AT TOUCH DOWN. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) WHEN ACFT ARRIVMar 27, 2010 · N720EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201000442Seat Track · corrodedSEAT TRACK HAS CORROSION. R & R DAMAGED PORTION OF SEAT TRACK AT FS 349 & RBL 9.00 IAW EC/TC REO 670-53-00-074.Mar 27, 2010 · N738EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000443Floorbeam · corrodedFLOOR SUPPORT FRAME CORRODED. REMOVED CORRODED FLOOR SUPPORT FRAME. NEW FRAME ON REQ. WORK DONE IAW SRM 51-42-02. PICKED UP FASTENER HOLES ,COUNTERSUNK, INSTALLED NUT PLATES AND INSTALLED NEW FRAME SUPPORT. SRM 51-42-06,51-41-02. APPLIED CHEMICAL CONVERSIOMar 27, 2010 · N738EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201000432Drain Mast · inoperativeSMELL OF SMOKE/ELECTRICAL IN GALLEY. REMOVED AND REPLACED FWD HEATED DRAIN MAST IAW AMM 38-32-11, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED. R & R FWD HEATED DRAIN MAST IAW AMM 38-32-11, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED.Mar 26, 2010 · N317CA · Cndair CL6002C10 · Water Line Anti-Ice System
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