N764NC, cancelled Jun 17, 2014

Service difficulty reports · 233

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 = 'N764NC' AND deregistration_id = 'N764NC-2014-06-17'
  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 DALA13048260855Frame · damagedFOUND FRAME DAMAGE BS 1190 BETWEEN L16-17R. COMPLIED WITH ERA/PRI 519084-14, REV 0.Sep 26, 2013 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA13046530855Wire Harness · damagedEMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 15. REPLACED LIGHT WIRE HARNESS IAW AMM33-53. OPS CHECKED GOOD.Sep 23, 2013 · N764NC · Doug DC951 · Light System WiringSDR DALA13012990855Wire · exposedEXPOSED WIRES IN SEAT TRACK DIRECTLY UNDERNEATH SEAT 6F. SECURED WIRES IN RACEWAY.Mar 24, 2013 · N764NC · Doug DC951 · Light System WiringSDR DALA13006900855Power Supply · inoperativeDURING INSPECTION, FOUND EMERGENCY PATH LIGHTS SEAT 9-13 AND LEFT OVER WING EXIT INOPERATIVE, REPLACED POWER SUPPLY AND TESTED OK.Feb 7, 2013 · N764NC · Doug DC951 · Emergency LightingSDR DALA12008090855Lanyard · brokenR1 DOOR SLIDE LANYARD BROKEN. MX ATTACHED THE LANYARD. ACFT IS NOW OK FOR SERVICE.Sep 19, 2012 · N764NC · Doug DC951 · Escape SlideSDR DALA12006400855O-Ring · damagedFLIGHT CREW NOTED FUEL FUMES IN AIRCRAFT AFTER STARTING AND RUNNING THE APU. ON INSPECTION, MAINTENANCE REPLACED THE O-RING AT THE ATOMIZER B-NUT AND PERFORMED A PNEUMATIC DUCT BURNOUT. AIRCRAFT IS NOW OKAY FOR SERVICE.Sep 3, 2012 · N764NC · Doug DC951 · APU Engine Fuel and ControlSDR DALA12005350855Frame · damagedRT MLG WHEEL WELL DOOR CUTOUT HAS FRAME WITH CHAFE/GOUGES IN 2 AREAS BY DOOR PROX SENSORS. GAINED ACCESS, REMOVED DAMAGE PER PR/I 505955-14, PERFORMED HFEC INSPECTION AT THE TRIMMED EDGE OF THE FORMER PER NDT SPM 06-10-01.003, NO CRACK NOTED. PERFORMED DVI OAug 13, 2012 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA12005270855Skin · delaminatedLT WING SLAT PANEL 1142A IS DELAMINATED AND HAS CORROSION. ACCOMPLISHED REPAIR OF LT WING SLAT PANEL NR 1142A IAW PRI 505669-14 REVISION O, PRI NR 505669-14 REV 1 AND ERA NR 505669-14 REV ORIGINAL SECTION 1.Aug 12, 2012 · N764NC · Doug DC951 · Leading Edge DevicesSDR DALA12005260855Skin · crackedA CRACK INDICATION WAS DETECTED ON SKIN EMANATING FROM FASTENER AT SHEAR CLIP AT BS 160 BETWEEN LONGERONS 2L AND 3L. REMOVED DAMAGE (CUT OUT) ON SKIN UPPER FUSELAGE FROM FASTENERS AT SHEAR CLIP AT STA Y160 BETWEEN LONGERONS 2L AND 3L PER DWG SR 09530129. DIMAug 12, 2012 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA12002930855Lanyard · frayedDURING LINE CHECK, MAINTENANCE FOUND THE R1 DOOR SLIDE LANYARD TO BE FRAYED. MAINTENANCE REPLACED THE R1 DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.Jul 9, 2012 · N764NC · Doug DC951 · Escape SlideSDR DALA12001840855Lock · bindingON WALK AROUND, MAINTENANCE FOUND THE AFT STAIRS DOWN AND THE CATWALK BLOCKING THE REAR EXIT. MAINTENANCE FOUND THE AFT VENTRAL STAIR LOCK BINDING AND FREED IT. AIRCRAFT NOW OKAY FOR SERVICE.Jun 19, 2012 · N764NC · Doug DC951 · Entrance StairsSDR DALA12000300855Fuse · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.May 22, 2012 · N764NC · Doug DC951 · Emergency LightingSDR DALA12000040855Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY CEILING LIGHTS BETWEEN ROWS 16 AND 19 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIVE CONDITION.May 12, 2012 · N764NC · Doug DC951 · Emergency LightingSDR DALA1217819855Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT HAD ALL THREE CATWALK LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE HINGE LINE AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.Mar 22, 2012 · N764NC · Doug DC951 · Light System WiringSDR DALA1171009855Tire · odorBURNING RUBBER SMELL - VERY STRONG IN COCKPIT AND THROUGHOUT THE CABIN, ON TAKEOFF AND CLIMB, CONTINUED TO DESTINATION UNEVENTFULLY. REMOVED EXCESS RUBBER FROM TIRES SUSPECTED FROM HYDROPLANING.Dec 22, 2011 · N764NC · Doug DC951 · TireSDR DALA1148709855Battery · dischargedMAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROWS 14-19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES PER AMM. OPERATIONAL CHECK WAS GOOD.Aug 19, 2011 · N764NC · Doug DC951 · Emergency LightingSDR DALA1126649855Floor Support · corrodedCABIN FLOOR SUPPORT ANGLE AND UPPER CHORD OF FLOORBEAM HAS CORROSION STA 237, BL-0 TO RBL 22. CORR OUT OF LIMITS IAW SRM 51-01, REMOVED CORR ON FLOORBEAM UPPER CHORD IN LIMITS IAW SRM 51-01, PAGE 8. HFEC SURFACE INSP PER NDT SPM 06-10-01.001, NO CRACKS NOTEDMar 29, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1105709855Support · chafedAFT ACCESSORY.9910087-5 SUPPORT CHAFED. RECEIVED -5 SUPPORT. LOCATED AND DRILLED HOLES, INSTALLED -5 SUPPORT IAW SRM 51-30-5, 51-30-2 S.Jan 24, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1105699855Intercostal · damagedAFT ACCESSORY INTERCOSTAL AT -27 ATTACH POINT ELONGATED HOLES, 3 EA. REMOVED DAMAGED .75"X2.5". FABBED DOUBLER FOR -3 AT -27 INTERCOSTAL IAW SRM 53-01, FIG 4 AND INSTALLED REPAIR DOUBLER SRM 51-30-2. REQUIRED INSPECTION COMPLETED.Jan 24, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1105489855Wedge · crackedINCOMING RUDDER HAS A 2" CRACK UPPERMOST T/E WEDGE. CUTOUT DAMAGED SECTION 10" FABRICATED LOCATED DRILLED & INSTALLED T/E SECTION. CUSTOMER FURNISHED & SPLICE IAW SRM 53-03, FIG 6, P205. REQUIRED INSPECTION COMPLETED.Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1105179855Doubler · damagedAFT CARGO DOOR JAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 1068-1108 AT L24R. LOCATED AND DRILLED NEW DOUBLER 5910158-25 IAW SRM 51-10-2. HFEC INSP AREA IAW NDT SPM 06-10Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1105169855Doubler · damagedFWD CARGO DOORJAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 340-440 AT L25R. LOCATED AND DRILLED NEW DOUBLER 9962455-25 IAW SRM 51-10-2. HFEC INSP AREA IAW MDT SPM 06-10-Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1105159855Doubler · damagedFWD CARGO DOORJAMB LOWER INTERIOR DOUBLER HAS INCOMING DRILL STARTS AND NUMEROUS HOLES FROM PREVIOUS REPAIRS. CUTOUT INNER DOOR JAMB DOUBLER STA 340-440 AT L25R LOCATED AND DRILLED NEW DOUBLER 9962455-25 IAW SRM 51-10-2. HFEC INSP AREA IAW NDT SPM 06-10-0Jan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1105119855Longeron · misrepairedAFT ACCY COMP CANTED FRAME STA 1245 AT LONGERON 3L, 4EA FASTENER HOLES ARE MISDRILLED. REMOVED APPROX 12" OF L3L PERFORMED DETAILED VISUAL INSP USING 10X MAGNIFYING GLASS NDT SPM 09-10-06 HFEC INSP CUTOUT IAW NDT SPM 06-10-01.001, A2700. NO INDICATIONS NOTEDJan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1105089855Longeron · misrepairedAFT ACCESSORY CANTED FRAME AT STA 1245, L4L OTBD FRAME TO LONGERON ATTACH FASTENER HAS MISDRILLED HOLE. REMOVED DAMAGED SECTION OF LONGERON IAW SRM 53-02, FIG 18. HFEC INSP IAW NDT SPM 06-10-01 VERIFIED DAMAGE REMOVED. FABRICATED NEW LONGERON AND SPLICES IJan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1104959855Frame · crackedAFT ACCESSORY COMPARTMENT RT CANTED FRAME 1314, CRACKED BELOW AIRSTAIR ACTUATOR. CUTOUT DAMAGED AREA 2" X 2" AREA NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01 FABBED & INSTALLED FILLER & DOUBLER IAW SRP DC9-A-53-10-17-801-663A-A. REQUIRED INSPECTION COJan 22, 2011 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1105059855Frame · misrepairedAFT ACCY COMPARTMENT CANTED FRAME, STA 1245, L3R, FRAME TO LONGERON ATTACH FASTENERS HAVE MISDRILLED HOLES. REMOVED DAMAGE APPROX 15.5". HFEC INSP IAW NDT SPM 06-10-01. VERIFIED DAMAGE REMOVED. LOCATED, FABRICATED AND DRILLED NEW SECTION OF LONGERON AND 2EJan 21, 2011 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1104459855Door Frame · damagedFWD CARGO DOOR CUTOUT-STA 364 FRAME BETWEEN 26L-25 DOOR JAMB WEB HAS 2 EA ELONGATED HOLES. REAMED UP HOLES TO .371. FABED FREEZE PLUGS ON TRAVELER 2312NO2175. FABBED STRAPS IAW EA 488328-14. REQUIRED INSP COMPLETED.Jan 20, 2011 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1104209855Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND RELAMPED THE LIGHT. SYS RETURNED TO AN OPS CONDITION.Jan 19, 2011 · N764NC · Doug DC951 · Emergency LightingSDR DALA1103969855Shear Tie · crackedAFT ACCESSORY COMPARTMENT RT SIDE STA 1190 SHEAR ANGLE CRACKED JUST BELOW L14R. REMOVED CRACKED SHEAR TIE IAW SRM 51-30-2 AND 51-30-5. FABRICATED NEW SHEAR TIE IAW SRM 51-10-2 AND 53-13-4. HEAT TREATED SHEAR TIE ON TRAVELER 2312N02136. INSTALLED NEW SHEAR TIJan 19, 2011 · N764NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1103959855Frame · crackedAFT ACCESSORY RT SIDE CANTED FRAME 1245 CRACKED 3EA PLACES BETWEEN L3R AND L7R. REMOVED CRACKED FRAME IAW SRM 51-30- 1, 51-30-2 AND 51-30-5. LOCATED, DRILLED AND INSTALLED NEW FRAME IAW DWG SRO9530086. REQUIRED INSP COMPLETED.Jan 19, 2011 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1104169855Frame · damagedFWD CARGO DOOR CUTOUT STA 364, FRAME BETWEEN L26L-25. UPPER FLANGE FRAME HAS 2 EACH ELONGATED HOLES. REAMED UP HOLE TO CLEAN AND ROUND. FABRICATED AND INSTALLED FREEZE PLUGS. FABRICATED STRAPS AND INSTALLED REPAIR PARTS IAW EA NR 488328-14. REQUIRED INSP Jan 18, 2011 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1104089855Floor Panel · corrodedMAIN PASSENGER CABIN FLOOR PANEL NR34, BL 0, STA 313, HAVE REMOVED CORROSION IAW SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-01.FABRICATED AND INSTALLED HAT CHANNELS AND WEB IAW ERA 488311-14. REQUIRED INSP COMPLETED.Jan 18, 2011 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1104049855Longeron · damagedAFT ACC COMPT LONGERON 5L CANTED STA 1245 HAS EXISTING DOUBLE DRILLED HOLE. CUT OUT APPROX 15" OF LONGERON 5L, STA 1245. LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2, 51-30-5, 53-02, FIG 18, SHT 2, 51-10-3, 51-10-4. REQJan 18, 2011 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1104069855Shear Tie · crackedCABIN STA 1136 BULKHEAD BETWEEN LONGERON 14L-15L SHEAR TIE CRACKED. REMOVED CRACKED SHEARTIE IAW SRM 51-30-5. RECEIVED REPAIR KIT FOR SHEAR TIE. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-10-4. INSTALLED SHEAR TIE IAW SRM 51-30-5. REQUIRED INSPECTION COJan 17, 2011 · N764NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1104159855Stop Fitting · damagedFWD CARGO DOOR CUTOUT AFT LOWER DOOR STOP T-FITTING ON BACKSIDE OF DOOR STOP DAMAGED. REMOVED DAMAGED FITTING IAW SRM 51-30-5. FABRICATED NEW FITTING IAW SRM 51-10-1 AND 51-10-4 AND DWG 9957909. INSTALLED NEW FITTING IAW SRM 51-30-5.Jan 16, 2011 · N764NC · Doug DC951 · Cargo/Baggage DoorsSDR DALA1104149855Frame · damagedFWD CARGO STA 427 L26R-L25R FRAME HAS DRILL HOLE NEXT TO CORE NUT HOLE. REAMED HOLE TO .625 IAW DWG 5912461. RECEIVED 3 EA FREEZE PLUGS ON TRAV 2312NO2114. INSTALLED 3 EA FREEZE PLUGS IAW ER/A NR 487380-14. FAB 2 EA REPAIR STRAPS. INSTALLED LOWER AND UPJan 16, 2011 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1103829855Rib · damagedLT WING T/E , FOUND TOO MARK O LOWER ANGLE OF RIB NR7 OUT OF LIMITS. REMOVED DAMAGED T-ANGLE IAW SRM 51-30-2. FABBED AND INSTALLED NEW T-ANGLE IAW SRM 51-30-2.Jan 15, 2011 · N764NC · Doug DC951 · Wing, Rib/BulkheadSDR DALA1103819855Door Frame · crackedFUSELAGE EXTERIOR FWD SERVICE DOOR FRAME, FWD UPPER CORNER HAS .1250" CRACK AT FASTENER. REPAIR IAW EM5330-01134-01B, CUTOUT DAMAGED AREA 2.125" X 3". NDT VERIFIED DAMAGE, REMOVED, FABBED AND INSTALLED FILLER IAW SRM 53-05, FIG 112 AND DWG SRO9530172. REQUIJan 15, 2011 · N764NC · Doug DC951 · Flight Compartment WindowsSDR DALA1103809855Skin · damagedFUSELAGE SKIN STA 370, LONG 26L SKIN REQUIRES 53-04, FIG 12C REPAIR TO FACILITATE EA 487370-14 CUT OUT DAMAGED AREA 18.5"X 15.5" NDT VERIFIED DAMAGE, REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED REPAIR PARTS IAW SRM 53-04, FIG 12C. REQUIED INSP COMPLETJan 15, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1103799855Skin · damagedFUSELAGE EXTERIOR STA 1060 AT LONG 26R SKIN REQUIRES REPAIR DUE TO EXISTING REPAIR FASTENER HOLES CUTOUT SKIN SECTION IAW SRM 53-04 FIG 12C. HFEC AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED NEW SKIN SECTION AND REPAIR PARTS IAW SRM 53-04, FIG 12C. REQUIRJan 15, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1103649855Angle · crackedMAIN CABIN STA 748 TO 760, RBL 44, WEB TO CTR WING TANK, ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE IAW SRM 51-30-5 AND 51-30-2. INSTALLED NEW ANGLE PN 591046424, PO 1032365 IAW SRM 51-10-4 AND 51-30-5.Jan 14, 2011 · N764NC · Doug DC951 · Wing Miscellaneous StructureSDR DALA1103639855Skin · damagedFUSELAGE SKIN-STA 1108, L26R SKIN REQUIRES 53-04, FIG 12C, REPAIR TO FACILITATE EA 487369-14. CUT OUT AREA STA 1108 TO 1125, BETWEEN L23R TO 26R (16",18") FROM .071 2024-T3 AND FINGER DOUBLER .025 2024-T3, 6 EA DOUBLERS AND 7 EA STRAPS FROM .071 2024-T3 AND FJan 14, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1103559855Floorbeam · damagedMAIN PASSENGER CABIN STA 180, BL 0, RBL 45, FLOORBEAM REQUIRE REMOVAL FAB REINSTALL IAW CUSTOMER. REMOVED, FABRICATED, & INSTALLED NEW FLOORBEAM IAW SRM 51-10-3, 51-30-5.Jan 14, 2011 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1103509855Floor Panel · corrodedMAIN PASSENGER CABIN CORROSION ON FLOOR PANEL PN37, SEVERAL PLACES. REMOVED CORROSION IAW SRM 51-10-3. ORIGINAL THICKNESS WAS .025 AFTER MATERIAL IS .005. OUT OF LIMITS IAW SRM 53-01. FABRICATED FLOOR PANEL WEB FROM 7075-T6 .025 AND HAT CHANNELS FROM S2912Jan 14, 2011 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1103049855Bulkhead · damagedMAIN CABIN STA 1136 LT PYLON BULKHEAD FWD SIDE UPPER END 2 FASTENERS HAVE NO EDGE DISTANCE. TRIMMED OUT DAMAGED AREA .450 X .680 IAW E-88 NR 8134 IAW SRM 53-01, FIG 4. FABRICATED & INSTALLED 1 EA DOUBLER AND 2 EA FILLERS IAW E88 NR 8134 IAW SRM 53-04, FIG 4 Jan 13, 2011 · N764NC · Doug DC951 · Nacelle/Pylon, Bulkhead/FirewallSDR DALA1103019855Attach Angle · crackedMAIN CABIN STA 756 LBL 44 WEB TO CTR WING TANK ATTACH ANGLE CRACKED. CUTOUT CRACKED AREA 1" X 12" IAW SRM 53-01, FIG 2, FABRICATED 1EA FILLER, 2EA REPAIR ANGLES IAW SRM 53-01, FIG 2. REMOVED & INSTALLED NEW T ANGLE AND 2EA SHIMS IAW DWG NR 9919689. INSTALLJan 13, 2011 · N764NC · Doug DC951 · Wing, Attach FittingsSDR DALA1102669855Cusp Web · crackedMAIN CABIN STA 237, RBL 55, CUSP WEB IS CRACKED IN 2EA PLACES STOP DRILLED CRACK IAW DC-9 A53-10-16. FABRICATED REPAIR DOUBLER IAW SRP DC9-A-53-10-16-801-663A -A. INSTALLED DOUBLER IAW SRP DC-9-A-53-10-16-801-663A-A.P-134 10 JAN 11. REQUIRED INSPECTION COMPLEJan 12, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1102659855Cusp Web · crackedCABIN STA 237, RBL 55, BENEATH CUSP WEB CRACKED DOUBLER AT FASTENER HOLE. REMOVED 1EA FRAME FITTING IAW SRM 51-30-5. REMOVED FASTENERS & REPAIR IAW SRM 51-30-5. CUT-OUT DAMAGED AREA IAW SRM 53-10-16-801-663A-A, NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 0Jan 12, 2011 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1102649855Floor Panel · damagedMAIN PASSENGER CABIN SEVERAL WASHERS PULLING THROUGH SKIN OF FLOOR PANEL NR84. FABRICATED FLOOR PANEL WEB AND HAT CHANNELS FROM IAW DWG 9957919. ASSEMBLED PANEL WEB AND HAT CHANNELS IAW SRM 51-30-2 AND ERA 488336-14. REQUIRED INSPECTION COMPLETED.Jan 12, 2011 · N764NC · Doug DC951 · Fuselage Floor Panel
Back to N764NC, cancelled Jun 17, 2014