N779NC, cancelled May 16, 2017

Service difficulty reports · 165

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 = 'N779NC' AND deregistration_id = 'N779NC-2017-05-16'
  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 DALA13037350870Wire · brokenSEAT MOUNTED EMERGENCY LIGHT AT 6DE INOPERATIVE. FOUND BROKEN WIRE AND REPAIRED IAW CHAPTER 20 WSPM AND EWIS.Jul 31, 2013 · N779NC · Doug DC951 · Light System WiringSDR DALA13000860870Wire · brokenEMERGENCY LIGHT BLACK WIRE BROKEN & HANGING LOOSE UNDER SEAT 9F. SECURED BROKEN WIRE IAW SWPM 20-20-03. OPS CHECKED NORMAL. OK FOR SERVICE.Jan 10, 2013 · N779NC · Doug DC951 · Light System WiringSDR DALA12013490870Connector · unsecureEMERGENCY PATHWAY LIGHT INOPERATIVE AT SEAT 6R. SECURED CONNECTOR UNDER SEAT. CHECKED GOOD.Nov 19, 2012 · N779NC · Doug DC951 · Light System WiringSDR DALA12005370870Slide · unserviceableDURING LINE CHECK, MAINTENANCE FOUND THE 1R DOOR SLIDE PRESSURE READING ZERO. MAINTENANCE REPLACE THE DOOR SLIDE AND RETURNED THE AIRCRAFT TO SERVICE.Aug 15, 2012 · N779NC · Doug DC951 · Escape SlideSDR DALA12000490870Fastener · looseDURING LINE CHECK, MAINTENANCE FOUND THE LOCK FASTENER LOOSE ON THE TAIL CONE DOOR HATCH. MAINTENANCE REPLACED THE RECEPTICAL, SECURED THE FASTENER AND RETURNED THE AIRCRAFT TO SERVICE.May 25, 2012 · N779NC · Doug DC951 · Aerodynamic FairingsSDR DALA1170639870Battery · dischargedEMERGENCY EGRESS AISLE LIGHTS INOP AT ROWS 19, 20, 21, 22 AND 2R LOWER EXIT SIGN. REPLACED POWER SUPPLY BATTERIES, CHECKS OK.Dec 20, 2011 · N779NC · Doug DC951 · Emergency LightingSDR DALA1167049870Light · inoperativeEMERGENCY EGRESS AISLE LIGHTS INOP AT ROWS 13, 14 AND 16. REPLACED AISLE LIGHT ASSEMBLY, CHECKS OK.Dec 4, 2011 · N779NC · Doug DC951 · Emergency LightingSDR DALA1160479870Battery Pack · dischargedDURING EMERGENCY LIGHT TEST FOUND PATH LIGHT ROW 9 TO ROW 13 AND FORWARD OVER WING EXIT SIGN INOP. THE BATTERY PACK AND FUSE WERE REPLACED AND TESTS OK.Oct 26, 2011 · N779NC · Doug DC951 · Emergency LightingSDR DALA1154699870Connector · disconnectedDURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE RECONNECTED THE ROW 17 EMERGENCY ESCAPE PATH LIGHT WIRE CONNECTOR. OPERATIONAL CHECK WAS NORMAL.Sep 19, 2011 · N779NC · Doug DC951 · Light System WiringSDR DALA1125959870Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT IDENTIFIER AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.Apr 15, 2011 · N779NC · Doug DC951 · Emergency LightingSDR DALA1123829870Cusp Web · damagedMAIN PASSENGER CABIN R1 DOOR PAN REQUIRE CUT FOR R1 DOOR CUSP REPAIR. CUT OUT DOOR PAN IAW DC-9 SRM 53-05 FIG 55. RECEIVED NEW PAN PN 5912492-1. LOCATED, DRILLED AND INSTALLED NEW PAN IAW DC-9 SRM 53-05 FIG 55. WEIGHT FOR REPAIR 8.3 OZ NDT VERIFIED DAMAGE Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1123819870Door Frame · damagedMAIN PASSENGER CABIN FWD SERVICE DOOR JAMB REPAIR 53-05 FIG 55 DOOR SPLICE -43 SPLICE HOLES FALL IN RADIUS. FAB -43 SPLICE FROM MAT .071 2024-0. HEAT TREATED TO .071 2024-T42 ON PEMCO TRAVELER 2469NO1540. DRILLED AND INSTALLED -43 SPLICE IAW DC9 ERA 490833-Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Main, StructureSDR DALA1123809870Cusp Web · corrodedMAIN CABIN CUSP ANGLE UNDER R-1 DOOR PAN HAS CORROSION. LOSS OUT OF LIMITS IAW DC-9 SRM 51-10-3. REMOVED CUSP ANGLE FROM STA 164-227 RBL 59. LOCATED AND DRILLED NEW ANGLE AND INSTALLED ANGLE IAW DC-9 SRM 53-05 FIG 55 WEIGHT OF REPAIR PARTS IS 7.8 INSTALLED Apr 1, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1123799870Floor Panel · corrodedCORROSION ON CABIN FLOOR PNL 21. REMOVED CORROSION IAW DC9 SRM 51-10-3 FIG 1. AFTER BLEND THICKNESS IS .005, OUT OF LIMITS IAW DC9 SRM 53-01. CUT OUT DAMAGE IAW DC9 SRM 53-01. (1) HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED A2700. FABRICATED AND IApr 1, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1123499870Floor Panel · crackedMAIN CABIN FLOOR PANEL 97 IS CRACKED AT FASTENER HOLE AFT END OF PANEL. REMOVED DAMAGE AT AFT END OF PNL IAW SRM 53-01, FIG 4. HFEC INSP IAW NDT SPM 06-10-01.001. FOUND DAMAGE REMOVED. REPAIRED PANEL IAW SRM 53-01, FIG 4, ERA 490832-14 & MFG DWG 9919600. Mar 31, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1123049870Channel · brokenMAIN PASSENGER CABIN FLOOR PANEL 70 AFT END HAT CHANNEL BROKEN AT FASTENER HOLE. REMOVED & REPLACED 4 EA HAT CHANNELS IAW DC-9 SRM 51-30-2 & ERA 490831-14. REMOVED PREVIOUS MISDRILLED REPAIR & REPAIRED PANEL IAW DC-9 SRM 53-05 FIG 1 & 51-30-2. INSTALLED 2 EMar 29, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1123019870Floor Panel · corrodedMAIN CABIN FLOOR PANEL 37 HAS CORROSION ON TOP OF PANEL. REMOVED CORR. 6X1 INCH IAW DC-9 SRM 53-01 FIG 1 AND CARD 5100-01570-01. ORIG MATERIAL .020 REMOVED .013 REMAINING MAT.007 OUT OF LIMITS. FABBED NEW PNL FROM .025 7075-T6 IAW DWG9957918 AND ERA 490827-Mar 29, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1122789870Floor Panel · crackedMAIN CABIN FLOOR PANEL 60C HAS 4EA HAT CHANNELS CRACKED ON BOTTOM OF PANEL. REMOVED 5EA HAT CHANNELS IAW SRM 51-30-2. FOUND WEB CRACKED, FABRICATED, LOCATED, DRILLED AND DEBURRED TO SKIN WITH .025 7075-T6 IAW ERA 490830-14. TRIMMED, LOCATED, DRILLED AND DEBMar 28, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1122739870Frame · crackedAFT ACCESSORY COMPARTMENT CANTED FRAME 1243 IS CRACKED AT L4R. REMOVED CANTED FRAME AT STA 1243 IAW DC-9 SRM 51-30-5 AND 51-30-2. LOCATED AND DRILLED NEW FRAME P/N SR09530086-81 IAW DC9 SRM 51-10-4. INSTALLED NEW FRAME IAW DC9 SRM 51-30-5 P-102.Mar 28, 2011 · N779NC · Doug DC951 · Fuselage Main, FrameSDR DALA1122539870Floor Panel · damagedMAIN PASSENGER CABIN FLOOR PANEL 72 TOP SKIN HOLE PUNCH CUTOUT DAMAGE IAW DC9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. FABRICATED FILLER AND DOUBLER FROM 7075-T6 .025 LOT 1120200 IAW DC9N SRM 53-01. INSTALLED FILLER AND DOUBLER IAW DMar 27, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1122459870Keelbeam · corrodedLEFT KEEL AREA STA 712 BETWEEN L29L AND L30 FRAME HAS CORROSION. REMOVED CORROSION IAW DC9 SRM 51-10-3. 100 PERCENT MATERIAL LOSS. REMOVED FRAME IAW DC-9 SRM 51-30-2. LOCATED, DRILLED AND INSTALLED NEW FRAME P/N 9957740-3 IAW DC9 SRM 51-10-4, 51-30-2 AND 51Mar 27, 2011 · N779NC · Doug DC951 · Fuselage Main, KeelSDR DALA1122569870Support Bracket · crackedMAIN CABIN STATION 200 L4L CRACKED. REMOVED L4L STA 160-228 AND 2 EA SPLICES STA 160-180 & 116-228. INTERCOSTAL SUPPORT BRACKET AND ATTACHMENT CLIP TO GO IN ACCESS. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW 51-10-4, 51-20-2, 51-30-2. REMar 26, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1122529870Cusp Web · crackedMAIN CABIN STA 1132 LBL 44 LEFT SIDE CUSP WEB CRACKED APPROX 2 INCHES UNDER SEAT TRACK. REMOVED DAMAGED AREA 12"X 12". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01.001. FABRICATED, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW WEB AND SPLICE. INSTALLED Mar 25, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1122509870Longeron · crackedMAIN CABIN STATION 200 LONGERON L2L CRACKED. REMOVED 32 INCHES OF L2L & 2 EA SPLICES. REMOVED CENTER AC DUCT STA 180 FOR ACCESS. RECEIVED NEW CAST FORM MAT P/N S2777922-3, LOCATE, DRILL, TRIM, DEBURRED, TREAT, PRIME & INSTALL IAW SRM 51-10-2, 51-30-2, 51-30Mar 25, 2011 · N779NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1121939870Floor Support · corrodedMAIN CABIN STA 200 RBL 47 TO 57 FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPORT IAW DC-9 SRM 51-30-5. REMOVED CORROSION IAW DC-9 SRM 51-10-3. ORIG MAT .060 MAT REMOVED .050 MAT REMAIN.010. FOUND TO BE OUT OF LIMITS L=8.00 W: 1.75D= .050 IAW DC-9 SRM 53-Mar 24, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121879870Cusp Web · crackedMAIN PAX CABIN RT SIDE CUSP WEB HAS 1EA CRACKED AT RBL 40 AFT 1 INCH FROM FLOORBEAM BS 239. REMOVED DAMAGE FROM WEB IAW DC9 SRM 53-10-16-801-663A FIG 2. HFEC INSP IAW DC9 NDT SPM 06-10-01. FOUND DAMAGE REMOVED INSTALLED 1EA REPAIR DOUBLER .020 7075T6 CLAD IMar 23, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121869870Angle · brokenMAIN CABIN STA 225 RBL 56 Z-ANGLE BROKEN OUT AT FASTENER HOLE. REMOVED Z-ANGLE IAW DC-9 SRM 51-30-2. RECEIVED NEW Z-ANGLE IAW DC-9 SRM 51-10-1. LOCATED, DRILLED & DEBURRED Z-ANGLE IAW DC-9 SRM 51-10-4. INSTALLED NEW Z-ANGLE IAW DC-9 SRM 51-30-5.Mar 23, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121819870Frame · damagedMAIN PAX CABIN/GALLEY HOLE IN EXISTING FRAME REPAIR BLOWN OUT AT STA 1151 AND L-17-L. REMOVED EXISTING REPAIR IAW SRM 51-30-2, 51-30-5. FABBED NEW REPAIR PLATE .063 7070-T6. FABBED REPAIR ANGLE & FILLER .050 7075-0. TREATED & PRIMED IAW DC-9 SRM 51-10-3. Mar 23, 2011 · N779NC · Doug DC951 · Fuselage Main, FrameSDR DALA1121579870Gusset · gougedMAIN CABIN STA 832 LBL-10 GUSSET GOUGED. REJECTED FOR GUSSET IMPROPERLY INSTALLED. FABBED, LOCATED, DRILLED, COUNTERSUNK AND DEBURRED GUSSET IAW DC9 SRM 51-10-4 & DOUGLAS DWG 4915719. INSTALLED GUSSET IAW DC9 SRM 51-30-2.Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121559870Floor Support · corrodedMAIN CABIN STA 160 TO 200 RBL 44 FLOOR SUPPORT HAS CORROSION. REMOVED 1 EA FLOOR SUPPORT IAW SRM 51-30-5. REMOVED CORR IAW SRM 53-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABBED 1 EA FLOOR SUPPORT MAT S2652479-7075-T6511. LOCATED, DRILLED & DEBUR IAWMar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121549870Diaphragm · damagedMAIN CABIN - FASTENER HOLE IN DIAPHRAGM TORN STA 172 RBL 44. REMOVED DAMAGE IN 3 EA PLACES .400" IN DIAMETER IAW DC9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. FABBED DOUBLER 7075-T6 IAW DC-9 SRM 53-13-1 FIG 11. TREATED & PRIMED DOUBLMar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121539870Diaphragm · damagedELONGATED HOLE IN DIAPHRAGM AT STA 198 AND RBL 46. REMOVED DAMAGE IN 1EA PLACE .500 IN DIAMETER IAW DC-9 SRM 53-01. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACK NOTED. FABBED DOUBLER 7075-T6 IAW DC-9 SRM 53-13-1 FIG 11. TREATED AND PRIMED DOUBLER IAW DC-9Mar 22, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121279870Frame Splice · corrodedAFT CARGO COMPARTMENT FRAME AT STA 1116 HAS CORROSION ON LOWER AFT FLANGE SPLICE ANGLE BETWEEN LONG 28L AND LONG 30. FOUND SPLICE OUT OF LIMITS IAW DC9 SRM 53-01. REMOVED SPLICE IAW DC9 SRM 51-30-5. FABBED NEW SPLICE FROM 7075-0 .050. HEAT TREATED TO TO 7075T6Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Main, FrameSDR DALA1121269870Attach Bracket · corrodedFWD CARGO STA 365 RBL 6 SURFACE CORROSION. REMOVED CORR 1 X 3 INCHES ON SURFACE OF ATTACH BRACKET. ORIG MAT .100 REMOVED .035 REMAINING .065. FOUND TO BE OUT OF LIMITS. RECEIVED, SEALED AND INSTALLED NEW BRACKET P/N 3457317-1. ALL WORK ACCOMPLISHED IAW DCMar 21, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121249870Cusp Web · crackedMAIN PASSENGER CABIN STA 435 LT CUSP WEB CRACKED. CUT OUT DAMAGED AREA 2"X 3.5". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED DOUBLER AND FILLER FROM 7075-T6 .025 & 7075T6 .020 IAW DC9 SRM 53-10-16.Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1121239870Floor Panel · corrodedCORROSION ON CABIN FLOOR PNL 16. FABRICATED NEW FLOOR PANEL IAW ER/A 490110-14 AND DC08 SRM 51-10-2. ASSEMBLED FLOOR PANEL IAW DC9 SRM 51-30-2. TREATED AND PRIMED PANEL IAW DC9 SRM 51-10-3. DRILLED AND COUNTERSUNK HOLES IAW DC-9 SRM 51-10-4.Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1121229870Floor Panel · crackedMAIN CABIN FLOOR PANEL 84 CRACKED AT FWD I/B EDGE. STOP DRILLED CRACK IAW DC9 SRM 53-01. NDT VERIFIED CRACK CONTAINED IAW NDT SPM 06-10-01. FABBED AND INSTALLED REPAIR DOUBLER FROM 7075 T6 .020 IAW DC-9 SRM 53-01.Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1121219870Longeron Splice · corrodedFWD CARGO COMPT LONG 28L SPLICE HAS EXFOLIATED CORROSION BETWEEN BS 237 AND BS 229. REMOVED DAMAGED SPLICE. SEALED AND REPLACED WITH NEW SPLICE IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3, 51-20-0, 51-30-5.Mar 21, 2011 · N779NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA12012260870Skin · crackedFUSELAGE EXTERIOR BS 1209 BETWEEN L13-14R SKIN CRACKED AT FASTENER. CUTOUT DAMAGED AREA 1.5"X 1.5" NDT VERIFIED CRACK REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED FILLER AND DOUBLER FROM .040" 7075-T6 PO#1023415 IAW SRM 53-01 FIG 4. REPAIR INSTALLED WITHMar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1120699870Hinge · crackedLT WING NR 3 FLAP HINGE FLAP HALF OF THE HINGE IS CRACKED. REMOVED AND REPLACED NR 3 FLAP HINGE HALF IAW CARD 5753-9893M-LT.Mar 18, 2011 · N779NC · Doug DC951 · Trailing Edge FlapsSDR DALA1120649870Skin · crackedFUSELAGE EXTERIOR CANTED FRAME STA 1292 BETWEEN LONG 13-14L SKIN CRACKED AT FASTENER. REMOVED DAMAGE 1 5/8"X 1 1/16". NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED FILLER AND DOUBLER FROM .040" 7075-T6 AND .050" 7075-T6. INSTALLED DOUBLER AND FIMar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1120639870Skin · gougedFUSELAGE EXTERIOR STAIRS CONTROL CUTOUT SKIN BELOW HINGE GOUGED. NDT FOUND CRACK CONTAINED AT FASTENER HOLE. REMOVED STAIR CONTROL DOOR. FABBED DOUBLER FROM .032" 2024-T3 AND INSTALLED DOUBLER AND DOOR IAW SRM 53-01 FIG 4.Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1120609870Floor Panel · corrodedMAIN CABIN FLOOR PANEL 45 HAS CORROSION ALONG FWD I/B EDGE REMOVED CORR. ORIG. MAT. 020" REMOVED .015" FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGE 5.75 X 1.75 INCHES NDT INSP VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED DOUBLER AND Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1120599870Structure · misrepairedMAIN CABIN STA 785 RBL 50 PREVIOUS REPAIR NOT MEETING FASTENER REQUIREMENT. REMOVED EXISTING REPAIR IAW SRM 51-30-2. FABBED AND INSTALLED FILLER.040" 7075-T6 AND DOUBLER .050" 7075-T6 IAW SRP DC-9 A-53-10-16-801-663A-A.Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1120589870Floor Panel · corrodedCORROSION ON CABIN FLOOR PANEL 20. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGED SECTION OF FLOOR PANEL 1.5"X 4". FABBED AND INSTALLED NEW SECTION OF PANEL FROM .032" 2024-T3 IAW DWG 9957828 AND SRM 53-01 FIG 4.Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1120559870Floor Panel · corrodedMAIN CABIN FLOOR PANEL 33 HAS CORROSION ON TOP AROUND FASTENER HOLES. REMOVED CORR OUT OF LIMITS IAW SRM 53-01 FIG 1. CUT OUT DAMAGE IN 4EA PLACES IAW SRM 53-5 FIG 1. FABBED 4EA DOUBLERS AND FILLERS FROM .025 INCH 7075-T-6 AND .032" 7075-T6. INSTALLED DOUBLMar 18, 2011 · N779NC · Doug DC951 · Fuselage Floor PanelSDR DALA1120509870Gusset · gougedMAIN CABIN STA 832 LBL-10 GUSSET GOUGED. GOUGE FOUND TO BE OUT OF LIMITS 90 PERCENT MAT. LOSS IAW SRM 53-01 FIG 1. REMOVED GUSSET, FABBED NEW ONE FROM .032" 7075-0 AND HEAT TREATED TOT6 ON TRAVELER #24961416. INSTALLED NEW GUSSET IAW SRM 51-30-5 AND 51-10-3Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1120499870Support Channel · crackedNLG STA 106 RIGHT LONG 28 DOOR CUTOUT SUPPORT CHANNEL CRACKED APPROX 1.25 INCH. RECEIVED FORMER P/N 5913421023. REMOVED CRACKED FORMER AND REPLACED IAW SRM 51-30-05 AND 51-10-3.Mar 18, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1119509870Stinger · damagedHORIZONTAL STABILIZER STRINGER LT SIDE UPPER ANGLE HAS ELONGATED HOLES. REPLACED ANGLE, FABBED OUT OF .032 2024-T3 IAW SRM 55-31-00 FIG 8. SUBED 2024T43 FOR 2024-T3 IAW DC-9 SRM 51-60-0 FIG.1. LOCATED AND DRILLED IAW DC-9 SRM 51-10-04, 51-30-02 AND 51-30-05Mar 16, 2011 · N779NC · Doug DC951 · Horizontal Stabilizer, Spar/RibSDR DALA1119499870Cargo Track · damagedFWD CARGO STA 446 LT TIE DOWN TRACK HAS 2EA HOLES IN EDGE OF SPLICE. REMOVED DAMAGED SPLICE IAW DC9 SRM 51-30-05. FOUND SPLICE TO BE MISS LOCATED ON TIE DOWN TRACK IAW DWG 5932875. FABBED 2EA SPLICE ANGLES IAW DC9 SRM 53-03. TRIMMED TO FIT & LOCATED & DRILMar 16, 2011 · N779NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
Back to N779NC, cancelled May 16, 2017