GE CF34 series

Service difficulty reports · 1,368

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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 = 'CF34'
  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 ASOA201001331Lens · crackedLEFT FUSELAGE EMERGENCY LIGHT JUST AFT OF EMERGENCY EXIT IS CRACKED. R & R LT FUSELAGE EMERGENCY LIGHT LENS AS REQUIRED IAW AMM 33-51-15-400-801 & 33-51-15-000-801-A01.Sep 15, 2010 · N750EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001333Post · corrodedCOCKPIT DOOR POST LT AND RT SIDE AT FS 280 CROSSBEAM HAS CORROSION. REMOVED TEO CLIPS AND BLENDED CORROSION ON COCKPIT DOOR POST LT AND RT AT FS 280 CROSSBEAM IAW SRM 51-21-06-001-001-A01, 51-42-06-001001-A01. CUT AWAY CORRODED SECTION OF DOOR POST AS SHOWN Sep 15, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001335Web · corrodedRT WEB AT FS 280 HAS CORROSION. BLENDED CORROSION ON RT WEB AT FS 280 IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON RT BULKHEAD WEB AT FS 280.00 IAW MAC NDT INSP PROCEDURES. PERFORMED LPI TYPE 1, METHOD C ON BLEND AREAS ON RT BSep 15, 2010 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001336Floorbeam · corrodedBS 280 FLOORBEAM HAS CORROSION SEVERAL AREAS. REMOVED FS280 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01, 51-42-21-001-001-A01. DRILLED NEW SERVICEABLE FS 280 FLOORBEAM IAW SRM 51-40-11-001-001-A01. TRANSFERED HOLES FROM NEW 280 BEAM INTO Sep 15, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001337Floor Support · corrodedAVIONICS BAY FWD FLOOR SUPPORT AT FS 280 HAS CORROSION. REMOVED FLOOR SUPPORT, PICKED UP EXISTING FASTENER HOLES ON NEW SUPPORT DRILLED TO FINAL SIZE AND DEBURRED IAW SRM 51-40-11. READY TO INSTALL NEW SUPPORT. INSTALLED SERVICABLE FLOOR SUPPORT REF SRM 51-42Sep 15, 2010 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001338Glowstrip · inoperativeRT EMER TRACK PHOTOLUMINESCENT INSERT FAILED TO WHITE COLOR AND NO LONGER LUMINATES IN ONE SECTION. R & R RT FADED EMER TRACK INSERT IAW AMM SUPPLEMENT ASA 33-51-00. (CLOSED)Sep 15, 2010 · N823AS · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201001339Attach Angle · corrodedSERVICE DOOR SILL FWD ATTACH ANGLE LOCATED ON AFT SIDE OF FS 319.70 IS CORRODED AND REQUIRES REPLACEMENT, PN 601R3838-1. REMOVED SERVICE DOOR FWD ANGLE AT FS 319.70 IAW SRM 51-42-21 AND SRM 51-41-02. SERVICEABLE ANGLE REQ'S INSTALL. LOCATED & DRILLED NEW SERSep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001340Support Angle · corrodedRT FLOOR SILL SUPPORT ANGLE LOCATED BETWEEN FS 310.00 AND FS 319.70 IS CORRODED BEYOND REPAIRABLE LIMITS PN 601R38669-49. LOCATED & DRILLED SERVICEABLE DOUBLER FOR GALLEY MOUNT BETWEEN FS 310 & FS 319 IAW SRM 51-40-11. INSTALLED DOUBLER ON THRESHOLD IAW SRM Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001341Floorbeam · corrodedFLOOR SUPPORT CHANNEL LOCATED AT FS 349.00, RBL 36.00, WL 73.50 IS CORRODED ON OTBD SIDE MAX DEPTH .030". REPAIRED TRANSVERSE BEAM BY COMPLYING WITH STEPS 1-11 OF REO 601R-53-21-1178. ECTC REQUIRED. REO 601R-53-21-1178 REV HAS BEEN ACCOMPLISHED AND ALL STEPS Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001342Seat Track · corrodedLT SEAT TRACK SEGMENT ON FLOOR LBL 9 FROM FS 364.00 TO FS 394.00 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK SEGMENT ON FLOOR LBL 9 FROM FS 364 TO FS 394 IAW MM 53-01-11-000/400-802.Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001319Floorbeam · corrodedCORROSION ON FLOORBEAM AT RBL 9.0 BETWEEN FS 469.00 FS 597 MULTIPLE LOCATIONS COMING FROM UNDER FLOOR TRACK. BLENDED CORROSION AND REMOVED 2 NUTPLATES IAW SRM 51-21-06-001-001-A01. AND 51-42-10-001-001-A01. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON FLOORSep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001321Floor Support · corrodedLT FLOOR TRACK AT LBL 9.0 CORRODED BETWEEN FS 469 - 597 MULTIPLE LOCATIONS. BLENDED CORROSION ON FLOOR TRACK AT LBL9.0 BETWEEN FS 469-FS 597 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-A01. REMOVED FLOOR TRACK AT LBL9 BETWEEN FS 469-597 IAW AMM 53-00-49-0Sep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001322Floor Support · corrodedRT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 469 - 597 MULTIPLE LOCATIONS. REMOVED SEAT RAIL RBL9 FROM FS 485- FS 581 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK AT RBL9 469-597 IAW AMM 53-00-49-400-801.Sep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001323Floor Support · corrodedLEFT FLOOR TRACK CORRODED AT LBL 9.0 BETWEEN FS 597 - FS 661.0 MULTIPLE LOCATIONS. REMOVED FLOOR TRACK IAW AMM 53-00-49-000-801. STOPPED HOLES TO FOR SCREWS, COUNTERSUNK ALL HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW FLOOR SEAT TRACK AT LBL9.0 597-66Sep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001324Floor Support · corrodedRT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 629 - FS 661.0. REMOVED CORROSION FROM SEAT RAIL RBL9 BETWEEN FS 629 + FS 661 IAW SRM 51-21-06-001-001 AFTER CORROSION REMOVAL SEAT RAIL IS WITHIN ALLOWABLE LIMITS IAW SRM 53-31-49-101-001 TREATED BARE METAL IAW SSep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001325Floor Support · corrodedLT FLOOR TRACK LBL 9.0 CORRODED AT APPROX FS 752-797, MULTIPLE LOCATIONS. REMOVED FLOOR SEAT TRACK IAW AMM 53-00-49-000-801. LOCATED HOLES IN NEW FLOOR SEAT TRACK IAW SRM 51-40-11-001-001-A01. STEPPED HOLES UP TO NOMINAL AND COUNTERSUNK AS REQUIRED IAW SRM Sep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001326Floor Support · corrodedRT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 752-797. REMOVED CORROSION FROM SEAT RAIL RBL9 BETWEEN FS 752- FS 797 IAW SRM 51-21-06. BLENDED AREA NEEDS MEASURED TREATED. PERFORMED DIMENSIONS LIMIT CHECK OF BLENDED AREAS OF RT FLOOR SEAT TRACK BETWEEN FS752-FSep 13, 2010 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001327Handle · bindingRT OVERWING EMERGENCY EXIT HANDLE REQUIRES TO MUCH FORCE TO OPEN 52 LBS. ADJUSTED OVERWING EXIT DOOR IAW AMM 52-21-00-820-801. SATISFACTORY IAW SP607, IAW AMM 52-21-00-820-801.Sep 13, 2010 · N740EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA201001328Handle · bindingPAX DOOR UNLATCH HANDLE REQUIRES TOO MUCH FORCE TO BREAK FREE. LUBED PAX DOOR LATCH PINS IAW AMM 12-20-2-640-809-A01. RT GOOD IAW AMM 52-11-00-720-801-A01.Sep 13, 2010 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201001329Skin · corrodedEXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT HAS CORROSION. REPAIRED EXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT, BLENDED TO WITHIN SERVICEABLE LIMITS IAW SRM 51-21-06 AND SRM 53-00-31.Sep 13, 2010 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001330Handle · out of adjustPAX DOOR FAILED FUNCTIONAL TEST ON HANDLE FORCE AND OPENING TIME. ADJUSTED PAX DOOR INNER HANDLE IAW AMM SUBTASK 52-11-25-820-003, STEPS AC.1 THRU 7 AND REACCOMPLISHED FUNCTIONAL TEST IAW AMM 52-11-00-720-802. NO DEFECTS NOTED.Sep 13, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR QXEA2010090700506Track · gougedC-CHECK - AFT BAGGAGE BAY DOOR FWD AND AFT TRACK DAMAGED. CLEANED GOUGED IAW SRM 51-12-00-001-001-A01. FWD TRACK GOUGE MEASURES 0.3"L 0.056"W .002"D ORIGINAL THICKNESS IS .100", NO DAMAGE ALLOWED ON AFT BAGGAGE BAY STRUCTURE IAW SRM 53-61-58-101-001-A01, SENSep 7, 2010 · N616QX · Cndair CL6002C10 · Cargo/Baggage DoorsSDR QXEA2010090700507Sill · corrodedC-CHECK - AFT BAGGAGE BAY DOOR SILL HAS EVIDENCE OF CORROSION. BLENDED AREA OF CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED ECI IAW NDTM ECI IAW 51-20-006-250-A01, NO CRACKS NOTED AT THIS TIME. ALL BLENDS WITHIN LIMITS OF REO 670-53-61-654. TREATED, PRSep 7, 2010 · N616QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010090700508Skin · chafedC CHECK - AFT BAGGAGE BAY DOOR LOWER COATING SCRATCH AND CHAFED. BLENDED OUT SCRATCHES AND CHAFE IAW SRM 51-12-00-001-001-A01. PERFORMED ECI IAW NDTM ECI 51-20-006-250-A01 AND RE0670-53-61-196. BLENDS FOUND WITHIN LIMITS OF REO 670-53-61-196. TREATED, PRIMSep 7, 2010 · N616QX · Cndair CL6002C10 · Cargo/Baggage DoorsSDR QXEA2010090700509Sill · corrodedC CHECK - DURING INSP, FOUND LIGHT CORROSION AROUND AVIONIC BAY DOOR SILL. REMOVED CORROSION AROUND AVIONICS DOOR SILL IAW REO 670-53-21-242 REV A. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01 NO CRACKS OR CORROSION FOUND AT THIS TIME. MEASURED BLENDS AND FOSep 7, 2010 · N616QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010090700510Angle · corrodedC-CHECK - DURING INSP FOUND CORROSION ON SERVICE DOOR MOUNTING ANGLE UNDER MID CAP. REMOVED GALLEY SERVICE DOOR FWD LOWER FITTINGS FOR ACCESS IAW SRM 51-41-02-001-001-A01. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THIIS .063", REMAINSep 7, 2010 · N616QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010090700511Seat Track · corrodedC-CHECK - RT FWD FLOOR SEAT TRACK HAS CORROSION. BLENDED AREAS OF CORROSION FROM FS 349-469 IAW SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-ASep 7, 2010 · N616QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010090700513Stringer · damagedC-CHECK - OVERSIZED RIVET FOUND AT S19R BETWEEN FS 517-533. REMOVED 1 RIVET IAW SRM 51-42-06-001-001-A01. PERFORMED ECI ON BLENDED AREA AROUND, REMOVED RIVET, NO CRACKS FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. WET INSTALLED SOLID FASTENER IAW REOSep 2, 2010 · N616QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR QXEA2010090700515Frame · corrodedC-CHECK - DURING INSP, FOUND CORROSION ON FRAME AT FS349 ON ATTACH ANGLE LOCATED JUST FWD OF ATTACHMENT ANGLE 26R. REMOVED RIVETS FROM ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. BLENDED CORRODED AREAS ON WEB AND ATTACH FLANGE IAW SRM 51-21-06-001-001-A01. BLESep 2, 2010 · N616QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010090700519Bulkhead · corrodedC-CHECK - LT SIDE, FS 280 BULKHEAD WEBBING SHOWS SIGNS OF CORROSION. BLENDED CORROSION, BLEND MEASURE .030 DEEP AND EXCEED LIMITS IAW REO 670-53-11-052. WEB IS CORRODED BEYOND LIMITS IAW REO 670-53-11-052. DRILLED OFF WEB IAW SRM 51-42-06-001-001-A01, 51-42Sep 2, 2010 · N616QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR QXEA2010090700520Support Angle · corrodedC CHECK - DURING INSP, FOUND CORROSION ON CRAWL WAY SUPPORT ANGLE AT FS 280 FOR THE AVIONICS FLOOR. REMOVED THE CRAWL WAY SUPPORT ANGLE IAW SRM 51-42-00-001-001-A01. DRILLED UP NEW SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SUPPORT ANGLE SRM 5Sep 2, 2010 · N616QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010090700521Doubler · chafedC CHECK - DURING INSP FOUND CHAFE MARK AND DAMAGED FASTENER ON DOUBLER FOR CONNECTOR ADJACENT TO AFT POTABLE WATER FILL PORT. REMOVED DAMAGED FASTENER IAW SRM 51-42-06-001-001-A01. BLENDED CHAFE MARK, BLEND IS WITHIN LIMITS IAW SRM 53-00-01-101-001-A01. ETCSep 2, 2010 · N616QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010090700504Structure · chafedC-CHECK - FOUND CHAFE DAMAGE TO RT INBD FLAP LOCATED AROUND INBD FLAP HINGE ARM. BLENDED 2 CHAFED AREAS IAW SRM 51-12-00-001-001-A01. ORIGINAL SKIN THICKNESS IS .063, REMAINING MATERIAL IS.055 AND .057. CHAFES ARE WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. Sep 2, 2010 · N616QX · Cndair CL6002C10 · Trailing Edge FlapsSDR QXEA2010090700505Skin · chafedC-CHECK - DURING INSP, FOUND GOUGES ON OUTSIDE OF AVIONICS DOOR AFT OF DOOR. BLENDED CHAFE AREA ON DOOR SKIN IAW SRM 51-12-00-001-001-A01, CHAFE MEASURES 1.3"L 1.3"W AND .002"D. ORIGINAL THICKNESS IS .100 REMAINING MATERIAL IS .098, CHAFE WITHIN LIMITS OF SRSep 2, 2010 · N616QX · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR QXEA2010083100500Proximity Sensor · out of adjustAFT CARGO DOOR CAUTION MESSAGE ILLUMINATES. RETURNED TO THE FIELD. LANDING UNEVENTFUL. INTERROGATED MDC FOUND "PX102 FAILED/WIRING DI126: UNREASON/OPEN WIRE". C/W ADJUSTMENT OF THE AFT BAGGAGE BAY DOOR PROX SENSOR PX102 IAW AMM 52-70-02-820-802(A02). OPS TEST Aug 31, 2010 · N618QX · Cndair CL6002C10 · Door Warning SystemSDR ASOA201001199Battery Pack · inoperativeEMERGENCY LIGHTS EXTERIOR FWD OF PASSENGER DOOR AND AFT OF SERVICE DOOR WILL NOT ILLUMINATE MORE THAN 5 SECONDS. R & R NR 1 BATTERY PACK IAW MM 33-51-04. OPS TEST CHECK GOOD. R & R NR 1 BATTERY PACK IAW MM 33-51-04 . OPS TEST CHECK GOOD.Aug 29, 2010 · N878AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001194Bulb · burned outRT NR 2 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. (CLOSED)Aug 28, 2010 · N842AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001188Priority Valve · malfunctionedON TAKEOFF-GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AND WOW INPUT CAUTION AND STEERING INOP CAUTION MESSAGE. ADDITIONALLY WOW OUTPUT FAIL STATUS MSG. NOSE GEAR INDICATED DOWN AND LOCKED. COMPLIED WITH QRH WOW INPUT CAUTION WAS THE ONLY MEESAGE WE CAug 25, 2010 · N903EV · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR CA100825002Inverter · failed(CAN) DEFECT ON 1 OF THE 3 CIRCUITS IN THE INVERTER, MADE AN OVERVOLTAGE AND BURNED 1 OF THE 2 FLUORESCENT TUBE PN: 6845-375 IN LT GLARESHIELD FLOOD LIGHT PN: 10-701T-2LR16-00 MAKING ODOR AND DUST IN LT COCKPIT FOR 15 SECONDS THEN STOPPED.Aug 24, 2010 · Cndair CL6013A · AC InverterSDR ASOA201001175Light · inoperativeREFER TO DMIL 565309-2 CEILING EMERGENCY FLOODLIGHT AT ROW 4 INOP. FOUND PUSHED PIN AT FLOODLIGHT ASSY, RESEATED PIN IAW ESPM 20-26-03. OPS CHECK IAW AMM 33-51-00. OPS GOOD DEFER CLEARED PLACARD REMOVED. (CLOSED)Aug 23, 2010 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001153Floor Support · corrodedCARGO COMPARTMENT FLOOR STRUT RAILS AT LBL 9 BETWEEN F.S. 559+91 AND F.S. 617 ARE CORRODED. REMOVED RAILS 601238663-21 2 EA AND 601R31032-51 IAW SRM 51-41-02. REMOVED 2 FWD RAILS BY REMOVING SCREWS. INSTALLED FWD RAIL SEGMENT AT FS 559+91 AND 2 HOLD DOWN CLAug 20, 2010 · N686BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001154Cargo Track · corrodedCARGO COMPARTMENT FLOOR CARGO RAILS AT RBL 9 BETWEEN FS 559+91 AND FS 569.00 ARE CORRODED. R & R SEAT RAILS AT STA RBL 9 BETWEEN FS 559+91 AND 569.00. WORK PERFORMED IAW 51-41-02.Aug 20, 2010 · N686BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001156Floor Support · corrodedFOUND LBL 27 FLOORBEAM CAP BETWEEN FS 568.00 AND FS 621.00 CORRODED BEYOND LIMITS. REMOVED FLOORBEAM CAP FROM FS 568.00 TO FS 621.00 AND LBL 27. ALL HOLES FOUND TO BE SERVICEABLE IN ACFT STRUCTURE IAW SRM 51-42-06 AND 51-42-21. LOCATE AND INSTALL NEW FLOORBAug 20, 2010 · N686BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001157Skin · corrodedFS 574 RT SIDE BETWEEN STR 27R & 24R HAS MINOR CORROSION ON EXTERNAL SKIN WHERE BELLY FAIRING MEETS SKIN ON STR 26R JUST AFT OF BELLY FAIRING. BLENDED OUT CORROSION IAW REO 601R-53-61-3785 STEP 1. PERFORMED EDDY CURRENT IAW REO 601R-53-61-3785 STEP 2. NO INDAug 20, 2010 · N921EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001158Light · inoperativeRT EXTERIOR NR4 EMERGENCY LIGHT INOP. R & R NR 4 RT EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. R & R NR 4 RT EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Aug 20, 2010 · N867AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001160Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED, PREVIOUS REPAIR SPLICE ANGLE. R & R 1 ANGLE SEC IAW REO 601R-52-11-513, REV A, DATED 3-9-05. (CLOSED)Aug 20, 2010 · N932EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001145Door · bindingPAX DOOR HARD TO OPEN, OUTER HANDLE HARD TO DEPLOY. COMPLIED WITH OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.Aug 18, 2010 · N843AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001130Door · bindingPAX DOOR HARD TO OPEN. OPENED AND CLOSED PAX DOOR 5 TIMES, OPS CKD GOOD IAW AMM 52-11-01. (CLOSED)Aug 15, 2010 · N857AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001094Motor · malfunctionedPAX DOOR JAMMED WILL NOT OPEN ( PASSENGER DOOR POWER ASSIST SYS ) R & R PAX DOOR ASSIST MOTOR IAW AMM 52-11-08. DEFER CLEARED. PLACARD REMOVED.Aug 11, 2010 · N686BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001095Lamp · burned outNR 1 EMERGENCY LIGHT FWD OF PAX DOOR INOP. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. (CLOSED)Aug 11, 2010 · N880AS · Cndair CL6002B19 · Emergency Lighting
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