N782NC, cancelled Nov 19, 2014

Service difficulty reports · 125

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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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 n_number = 'N782NC' AND deregistration_id = 'N782NC-2014-11-19'
  ORDER BY difficulty_date DESC"

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SDR DALA13056240873Floorbeam · damagedFLOORBEAM AT RBL 4 BS 446 DAMAGED FROM FLOORBOARD. CLEANED AREA IAW SRM 53-05, FIG 20. TREATED AND PRIMED. REPAIRED IAW SRM 53-05.Oct 27, 2013 · N782NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA13056230873Floorbeam · damagedFLOORBEAM AT RBL 4 BS 427 DAMAGED FROM FLOORBOARD . CLEANED AREA IAW SRM 53-05, FIG 20A. TREATED AND PRIMED. REPAIRED IAW SRM 53-05.Oct 27, 2013 · N782NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA13056220873Floor Panel · damagedFLOOR HAS SOFT SPOT IN FIRST CLASS AT ROW 4 BETWEEN B & C. REMOVED FLOOR PANEL AND FOUND HAT CHANNEL DAMAGE. REMOVED TWO DAMAGED CHANNELS IAW SRM 51-30-02. FABRICATED & DRILLED NEW CHANNELS IAW SRM 51-10. PAINTED AND SECURED NEW CHANNELS TO FLOOR PANEL IAOct 27, 2013 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA13056210873Floorbeam · corrodedFLOORBEAM RBL 4, BS 408 DAMAGED FROM FLOORBOARD. CLEANED AREA IAW SRM 53-05, FIG 20A. REPAIRED FLOORBEAM IAW SRM 53-05. OK FOR SERVICE.Oct 27, 2013 · N782NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA12002300873Lanyard · unsecureDURING LINE CHECK, MAINTENANCE FOUND THE R1 DOOR SLIDE LANYARD TO BE DETACHED FROM THE DOOR SLIDE COVER. MAINTENANCE SECURED THE 1R DOOR SLIDE LANYARD AND RETURNED THE AIRCRAFT TO SERVICE.Jun 28, 2012 · N782NC · Doug DC951 · Escape SlideSDR DALA1142569873Floor Panel · damagedCABIN FLOOR PANEL HAS VERY SOFT SPOT IN ISLE AT ROW 11. REMOVED DAMAGED FLOOR PANEL 60C. REPLACED FLOOR PANEL IAW ERA 489362-14.Jul 2, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1128399873Acm · overservicedACFT RETURNED TO DEPARTURE DUE TO SMOKE IN THE CABIN. LAV SMOKE DETECTORS SOUNDED AND LT AIR COND SUPPLY TEMP HIGH LIGHT ILLUMINATED. QRH WAS COMPLIED WITH AND THE LT PACK WAS SHUTDOWN. MX RAN BOTH ENGINES AT TAKEOFF POWER AND CRUISE POWER FOR 5 MINUTES EAApr 20, 2011 · N782NC · Doug DC951 · Cabin Cooling SystemSDR DALA1120659873Doubler · crackedFUSELAGE EXTERIOR POTABLE WATER DOOR CUTOUT AFT LOWER CORNER INNER DOUBLER IS CRACKED APPROX .75 INCH. CUT OUT DAMAGED PORTION OF DOUBLER, NO CRACKS NOTED. FABBED DOUBLER TITANIUM 6AL-4V .032" FILLER 2024-T3 .063". INSTALLED DOUBLER AND FILLER IAW DC-9-53-3Mar 18, 2011 · N782NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1119219873Shear Tie · crackedTHE 1F/62 AFT ACC COMPT STA 1247 BETWEEN L1-L2R SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-11-00 114725. INSTALLED IAW DC9 SRM 53-03 FIG 3.P-127 284425.Mar 15, 2011 · N782NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1118749873Door Frame · corrodedFWD CARGO DOOR CUTOUT STA 370-427 CORROSION ON WEB REMOVED CORROSION ORIG MAT .040 REMOVED .010 REMAINING .030 OUT OF LIMITS PER SRM 53-01. RECEIVED NEW WITH PART NUMBER 5910142U11. CUT OUT 2 06-10-001. FAB AND INSTALLED DOUBLERS .050 2024-T3 AND FILLER .04Mar 14, 2011 · N782NC · Doug DC951 · Fuselage Main, StructureSDR DALA1118529873Skin · chafedRIGHT WING NR 2 SLAT CENTER SLAT TRACK L/EDGE SKIN CHAFED I/B SIDE OF CUTOUT. BLENDED CHAFE 3"X 2". FOUND TO BE OUT OF LIMITS IAW DC9 SRM 57-01 WITH AN ORIGINAL THICKNESS .190 IAW DC9 SRM 57-31-1 AND A MAT LOSS OF .062. REMAINING THICKNESS .128 CUT OUT DAMAMar 11, 2011 · N782NC · Doug DC951 · Leading Edge DevicesSDR DALA1117199873Floor Panel · crackedMAIN CABIN FLOOR PANEL 80 CRACKED ON EDGE. REMOVED DAMAGE ON FLOOR PANEL 1 X 2 INCHES PER ERA 490094-14 AND IAW DC9 SRM 53-01 FIG 4.NDT VERIFIED CRACK IS REMOVED IAW NDT SPM 06-10-01. FABBED REPAIR DOUBLER 3 X 2.5 INCHES & FILLER 2 X 1.5 INCHES. LOCATED ANDMar 10, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1116419873Floor Panel · crackedMAIN CABIN-FLOOR PANEL, NR 80, AFT END IS CRACKED AND HAS CORROSION AT FASTENER HOLE. REMOVED CORR & CRACK BY CUTTING OUT DAMAGE 11.5" X 5" IAW SRM 51-10-4 & 51-10-4 NDT. FOUND DAMAGE REMOVED IAW NDT SPM 06-10-01 FABRICATED REPAIR DOUBLER IAW SRM 53-23-0, FIMar 8, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1116079873Intercostal · crackedMAIN CABIN BETWEEN STA 617 AND 636 BL-0 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-30-2. REMOVED CRACK IAW SRM 53-01, FIG 1. HFEC INSP IAW NDT SPM 06-10-01. VERIFIED CRACK REMOVED. FABBED REPAIR ANGLE AND FILLER FROM .025 FILLER AND .032 ANGLE IAMar 7, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1115869873Vane · delaminatedLEFT WING CENTER FIXED FLAP VANE DELAMINATED 0N IB END. REMOVED L/WING FLAP CENTER FIXED VANE IAW DC-9 MM 27-51-03. REPLACED FLAP FIXED VANE DUE TO DELAMINATION OUT OF LIMITS PER TRAVELER 2477NO1195. INSTALLED NEW SERVICEABLE VANE IAW DC9 MM 27-51-03. OPSMar 5, 2011 · N782NC · Doug DC951 · Trailing Edge FlapsSDR DALA1115529873Floor Panel · corrodedMAIN CABIN METAL FLOOR PANEL NR 21 HAS CORROSION FASTENER HOLES. REMOVED CORROSION FROM FLOOR PANEL IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FABBED FLOOR PANEL & 2 EA HAT CHANNELS IAW SRM 51-10-2. DRILLED, COUNTERSUNK FASTENER HOLES IAW SRM 51-10-4. Mar 4, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1115859873Vane · delaminatedRIGHT WING FLAP FIXED VANE NR 2 FROM I/B HAS SOME DELAMINATION ON UPPER SURFACE AT PREVIOUS REPAIR. REPLACED RT WING FLAP NR 2 FIXED VANE WITH NEW SERVICEABLE NR 2 FIXED VANE DUE TO DELAMINATION BEING UNREPAIRABLE IAW DC9 MM 27-03 ITEM 7 FIGURE 11 SHEET 2. IMar 3, 2011 · N782NC · Doug DC951 · Trailing Edge FlapsSDR DALA1115299873Floor Panel · corrodedMAIN CABIN METAL FLOOR PANEL NR 79 HAS CORROSION AROUND EDGES AND 2 EA HAT CHANNELS CRACKED PARTS RACK 22B. REMOVED CORROSION FROM SEVERAL SPOTS IAW SRM 51-10-3. ORIG MAT .020 REMOVED, .010 REMAINING, .010 FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEMar 3, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1114909873Skin · damagedDURING INSPECTION OF LIGHTNING STRIKE MONITORS FOUND AREAS OF PREVIOUS BLENDS ON FASTENER HEADS AND SKIN STA 370 L22R. BLENDED LIGHTNING STRIKE PER DWG NR S60590000.ORIG .050 PER SRM 53-33-0 FIG 2. LOST .016 PER NDT SPM 04-00-06. REMAINING.034, FOUND TO BE Mar 2, 2011 · N782NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1114779873Floor Panel · corrodedMAIN CABIN METAL FLOOR PANEL NR 17 HAS CORROSION ON SKIN. PARTS RACK 22B. REPLACED FLOOR PANEL NR 17 WITH SERVICEABLE COMPOSITE FLOOR PANEL IAW DC-9 SRM 51-30-1, 51-10-4. P-109.Mar 2, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1114769873Floorbeam · crackedMAIN PASSENGER CABIN-FLOOR SUPPORT CRACKED STA 617 LBL1 TO LBL18. REMOVED CRACKED FLOOR SUPPORT/ZEE IAW SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT/ZEE FROM .050 2024T3 PO 1120351 IAW SRM 53-13-3 FIG 4 SHEET 1 AND 2 AND 51-10-4. INSTALLED NEW FLOOR SUPPORT/ZMar 2, 2011 · N782NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1114539873Cargo Track · corrodedFWD CARGO SURFACE CORROSION ON RT TIE DOWN TRACK FROM STA 427-579. REMOVED CORROSION FROM TIEDOWN TRACK 50 PERCENT MATERIAL LOSS. FABRICATED 2 SPLICES FROM .071 7075-0, HEAT TREATED ON TRAVELER 2477NO1494 TOM T-6 IAW AMS 2770. INSTALLED TIE DOWN TRACK IAW SMar 1, 2011 · N782NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1114489873Cusp Web · crackedMAIN CABIN STA 694 RIGHT SIDE CUSP WEB CRACKED UNDER HORSESHOE COLLAR. REMOVED AND INSTALLED CUSP WEB FROM 693-753 IAW DC9 SRM 51-30-2. FABBED NEW WEB USING 7075-T6 .020. FABBED AND INSTALLED RING DOUBLER USING .050 7075T6, .080 7075T6, .090 7075T6 IAW DWMar 1, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1114479873Cusp Web · damagedFOUND ELONGATED HOLES IN CUSP AT STA 680 RT CUSP AT ZEE SPLICE. REMOVED AND INSTALLED CUSP WEB FROM STA 674-693 IAW SRM 51-30-2. FABRICATED NEW WEB FROM .020 7075T6. FABRICATED AND INSTALLED RING DOUBLERS USING .050 7075T6.063 7075T6, .080 7075T6.O90 7075TMar 1, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1114469873Attach Angle · crackedMAIN PASSENGER CABIN STA 1167 APB RT BOTTOM HORIZ SUPPORT OTBD BOTTOM ATTACH ANGLE CRACKED. REMOVED ATTACH ANGLE FROM HORIZ SUPPORT IAW DC-9 SRM 51-30-02 AND SRM 51-30-05. TRIM CRACK IAW DC-9-A-53-10-25-801-663A-A NDT SPM 01-10-01.001. CRACK WAS 04, DC9-A-5Mar 1, 2011 · N782NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1114209873Frame · corrodedSTA 579 BET L 26-27 RT CORROSION FOUND UNDER TIE DOWN TRACK ON FRAME. REMOVED CORROSION PER SRM 53-01 FIG 1. MATERIAL LOSS OUT OF LIMITS PER SRM 53-01 FIG 1. REMOVED FORMER PER SRM 51-30-2, ORG MAT .063 2024-T6 PER SRM 53-13-2 FIG 2. MATERIAL SUBSTITUTED PFeb 26, 2011 · N782NC · Doug DC951 · Fuselage Main, FrameSDR DALA1114199873Attach Fitting · crackedC-1 PIT STATION 579 RT TIE DOWN TRACK ATTACH FITTING CRACKED. REMOVED CRACKED TIE DOWN TRACK ATTACH FITTING IAW SRM 51-30-5. RECEIVED NEW FITTING PN 5956034-557. LOCATED, DRILLED AND DEBURRED FITTING IAW SRM 51-10-4. TREATED 2 HOLES IAW DC9 SRM 51-10-3 ANFeb 26, 2011 · N782NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1114189873Attach Fitting · crackedC-1 PIT STATION 579 RT TIE DOWN TRACK ATTACH FITTING CRACKED. REMOVED CRACKED TIE DOWN TRACK ATTACH FITTING IAW SRM 51-30-5. RECEIVED NEW FITTING PN 5956034-557. LOCATED AND DRILLED AND DEBURRED FITTING DC9 SRM 51-10-4. TREATED 2 HOLES IAW SRM 51-10-3 AND Feb 26, 2011 · N782NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1113969873Frame · crackedAFT ACCESSORY COMPARTMENT STA 1209 L13R FRAME WEB CRACKED. REPAIRED CRACKED WEB AT AFT ACC COMPT IAW DC-9 SRM 51-70-4 FIG 2. REMOVED CRACKED WEB SECTION FROM STR 10R-14 STA 1209. FABRICATED NEW WEB SECTION. ALODINED, PRIMED, INSTALLED WEB ATTACH PARTS IAWFeb 26, 2011 · N782NC · Doug DC951 · Fuselage Main, FrameSDR DALA1114029873Floor Support · corrodedFORWARD WET AREA STA 256-275 LBL 18 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION 1 INCH BY 3 INCH IAW DC9 SRM 51-10-3 ORIG MATL .060, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG1. REMOVED FLOOR SUPPORT IAW DC9 SRM 51-30-1 AND 51-30-5. LOCATED DRILLED Feb 25, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1114019873Floor Panel · corrodedMAIN CABIN METAL FLOOR PANEL NR 99 HAS CORROSION AROUND FASTENER HOLES. PARTS RACK 22B. FABRICATED NEW PANEL FROM .025 7075-T6 SKIN AND HAT CHANNEL PN S2912282FT IAW DOUGLAS DRAWING NR 9957930 AND ERA 2477N01382. REQUIRED INSPECTION COMPLETED.Feb 25, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1114009873Floor Panel · crackedMAIN CABIN FLOOR PANEL 102C CRACKED AT FASTENER HOLE. TRIMMED OUT CRACKED AREA IAW DC-9 SRM 53-05. FABRICATED DOUBLER AND FILLER FROM .032 7075T6 IAW DC-9 SRM 53-05 PO NR 1022537. TRIMMED OUT AREA 1 INCH 1.9 INCH TOOL NR 9573 .1 OZ DOUBLER AND FILLER .3 OZ Feb 25, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1113999873Seat Track · damagedMAIN CABIN-FS 200-240 RBL 22 SEAT TRACK HAS 1 MISDRILLED HOLE. REMOVED DAMAGED SEAT TRACK. RECEIVED NEW SEAT TRACK PN52772660 PO 1022910 IAW DC-9 SRM 53-23 FIG 3 PAGE 4. TRIMMED, LOCATED, DRILLED AND INSTALLED IAW DC-9 SRM 51-10-04 AND 53-05 FIG 4E PAGE 32.Feb 25, 2011 · N782NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1113959873Frame · chafedAFT ACCESSORY COMP LT SIDE CANTED FRAME STA 1139 AFT SIDE HAS DEEP CHAFE. BLENDED CHAFE ON LT SIDE CANTED FRAME IAW DC-9 SRM 51-10-3. ORIG MAT .063 REMOVED OVER 50 PERCENT MAT OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. REMOVED FRAME IAW DC-9 SRM 51-30-1. LOFeb 25, 2011 · N782NC · Doug DC951 · Fuselage Main, FrameSDR DALA1113949873Frame · chafedAFT ACCESSORY COMP RT SIDE CANTED FRAME STA 1339 AFT SIDE HAS DEEP CHAFE. BLENDED CHAFE AREA ORIG MAT .063 LOST OVER 50 PERCENT MATERIAL. FOUND TO BE OUT OF LIMITS PER DC-9 SRM 53-01. REMOVED AND REPLACED CANTED FRAME PER DC-9 SRM 51-30-2, 51-30-5, 51-30-Feb 25, 2011 · N782NC · Doug DC951 · Fuselage Main, FrameSDR DALA1113939873Longeron · crackedMAIN CABIN STA 753 LEFT LONGERON 18 JUST BELOW FLOOR MAIN FRAME CRACKED APPROX 2 INCHES ON FWD SIDE NDT VERIFIED #A2700. REPLACE MAIN FRAME PN 9923407-501N STA 753 //H IAW DC9 SRM 51-01 AND ENGINEERING REPAIR/AUTHORIZION #486359-14. REQUIRED INSPECTION COMPLFeb 25, 2011 · N782NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1113729873Support Angle · cracked6C/161 MAIN CABIN LBL-44 BETWEEN STA 750 AND 770 SUPPORT ANGLE FROM WEB TO CENTER TANK CRACKED AT FASTENERS. REMOVED, ORDERED, AND INSTALLED NEW ANGLE PART NR 5410464U23 IAW DC-9 SRM 51-01 AND 51-30-5,1, PC AND DAC DWG 5910414P-226 Q-967 284419.Feb 24, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1113719873Floor Support · cracked6C/299 MAIN CABIN-FS 1136 LBL 1 TO LBL 22 FLOOR SUPPORT IS CRACKED AT INBD END APPROX 1.5 IN. RII: Y. REMOVED DAMAGED ANGLE. FABBED NEW ANGLE IAW DC9 SRM 53-13-3 AND SRM 51-10-4 AND INSTALLED PER DC9 SRM 51-30-02 AND 51-30-05 AS REQ`D, P-109. REQUIRED INSPEFeb 24, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1113709873Floor Panel · corroded6C/203 MAIN CABIN METAL FLOOR PANEL NR 26 HAS CORROSION AROUND FASTENER HOLES PARTS RACK 22B CPCP TASK 58-53303 RII: Y. REMOVED CORROSION FROM END OF PANEL NR 26. AREA 1 INCH BY 11 1/2 INCH ORG THICKNESS 0.020 REMOVED 0.010 REMAINING 0.010. OUT OF LIMITS CUFeb 24, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1113699873Cusp Web · cracked6C/194 MAIN CABIN APPROXIMATELY STATION 1134 RT CUSP WEB CRACKED AT AFT HOLE. REMOVED AND REPLACED CUSP WEB STA 1068-1136 IAW DWG SG09537 PN 09-5300-3-3408. REQUIRED INSPECTION COMPLETED.Feb 24, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1113689873Floor Panel · cracked6C/298 CABIN FLOOR PANEL NR 98 CRACKED AT AFT INBOARD CORNER. TRIMMED OUT CRACKED AREA 3 1/8 INCH BY 2 3/8 INCH PER DC9 SRM 53-05 FIG 1. HFEC CHECK COMPLETED PER NDT SPM 06-10-01. VERIFIED CRACK REMOVED. FABRICATED NR 2 DOUBLER AND FILLER. INSTALLED DOUBLFeb 24, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1113679873Floor Panel · corroded6C/85 COCKPIT FLOOR PANEL NR 14 HAS CORROSION AT AFT END CPCP 46-53303. FABRICATED NEW FLOOR PANEL FROM .025 7075-T6 PO 1120200 AND HAT CHANNELS S2912282 PER ER 489365-14 P-226 Q-967 284419 Q-967 284419.Feb 24, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1113649873Frame · corroded1C/30 ACCESS FROM COCKPIT-UPPER FACE OF PRESSURE PANEL BELOW RUDDER PEDAL STA 110 JUNCTURE AT FUSELAGE FRAME HAS CORROSION AT RT END OF ANGLE 4 INCHES BY 3 INCHES CPCP TASK 45-53302. FABRICATED AND INSTALLED NEW ANGLE IAW DOUGLAS DRAWING NR 3911397 AND DC-9 SFeb 24, 2011 · N782NC · Doug DC951 · Fuselage Main, FrameSDR DALA1113089873Seat Track · corrodedMAIN CABIN-FS 218-275 RBL 45 SEAT TRACK HAS CORROSION ON UPPER SURFACE. FOUND CORROSION TO BE BEYOND BLEND OUT LIMITS. REMOVED AND REPLACED TRACK STA RBL 45 AT STA 200-280 RT SIDE AS REQ PER DC9 SRM 51-30-05 AND SRM 53-23-0.P-183. REQUIRED INSPECTION COMPLEFeb 23, 2011 · N782NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1113069873Floor Panel · damagedMAIN CABIN METAL FLOOR PANEL 60C HAS ELONGATED HOLES AND NO ED PARTS RACK 22B. FABRICATED NEW FLOOR PANEL FROM .025 7075-T6 AND HAT CHANNELS IAW ERA 489362-14.P-226 Q-971. REQUIRED INSPECTION COMPLETED BY Q-971 280318.Feb 23, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1112779873Floor Panel · damagedCABIN COMPOSITE FLOOR PANEL 17 DOES NOT LINE UP WITH HOLES IN A/C. REPAIRED HOLES ON PANEL NR 17 IAW DC9A-53-22-01-801-663A-A AND LOCATED AND DRILLED HOLES IAW DC9 SRM 51-10-4. INSPECTION COMPLETED BY Q-953 186938.Feb 22, 2011 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1112409873Cusp Web · puncturedMAIN PAX CABIN RT SIDE CUSP WEB HAS 1 PUNCTURE APPROX 1/4 INCH DIA AT FUS FRAME STA 351 RBL 57 IN. REPAIRED PUNCTURE AT STA 351 RBL 57 IAW SRM 53-01 FIG 1 SHEET 3.Feb 21, 2011 · N782NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1112399873Longeron Splice · corrodedFORWARD CARGO L29L BETWEEN STA 636 AND 655 LONGERON SPLICE HAS CORROSION. REMOVED CORROSION ON SPLICE. FOUND TO BE OUT OF LIMIT. RECEIVED NEW LONGERON SPLICE ON TRAVELER 2477NO1509.LOCATED AND DRILLED AND DEBURRED THE HOLES PER DC9 SRM 51-10-4. TREATED, PRFeb 21, 2011 · N782NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1112379873Longeron · crackedMAIN CABIN STATION 484 L17L IS CRACKED. REMOVED DAMAGED L17L STA 455-513. EXISTING SPLICE TO EXISTING SPLICE. REPLACED SECTION L17L WITH NEW. REINSTALLED 2 SPLICES 56 INCHES TOTAL IAW DC9 SRM 53-13-2 FIG 3, 51-10-4, 51-10-3, 51-10-0, 51-30-2, 51-30-5. TAGFeb 21, 2011 · N782NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1112369873Longeron · crackedMAIN CABIN STATION 427 L16L IS CRACKED. REMOVED LONGERON SECTION FROM STA 360 TO 434 AT EXISTING SPLICES. INSTALLED NEW SECTION OF LONGERON FROM S2777922-1 AND SPLICES IAW DC9 SRM 53-02 FIG 18, P-226. REQUIRED INSPECTION COMPLETED BY Q-995 485522.Feb 21, 2011 · N782NC · Doug DC951 · Fuselage Main, Longeron/Stringer
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