Pratt & Whitney JT8D-9

Service difficulty reports · 686

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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 = 'JT8D9'
  ORDER BY difficulty_date DESC"

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SDR DALA1035949864Floorbeam · chafedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 237 BETWEEN BL 0-LBL 22 FLOOR SUPPORT CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01-1. REMOVED FLOOR SUPPORT IAW SRM 51-30-05. FABRICATED AND DRILLED HOLES IAW SRM 51-10-4 AND DWG 5914617. INSDec 18, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035989855Floor Support · corrodedDURING M-CHECK FOUND MAIN CABIN STA 218 TO 237, BL 0 FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPORT DUE TO OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT, ALODINED AND PRIMED IAW SRM 51-10-4, 51-10-3.Dec 18, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1051869852Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 1418 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Dec 18, 2010 · N761NC · Doug DC951 · Emergency LightingSDR DALA1035999855Longeron Clip · crackedDURING M-CHECK, FOUND MAIN CABIN STA 1167, APB STIFFENER JUST ABOVE L12L ATTACH CLIP CRACKED AT FASTENER. REMOVED CRACKED STIFFENER CLIP ANGLE IAW SRM 51-30-5 & 51-30-2. LOCATED & DRILLED NEW HOLES IAW SRM 51-10-4. INSTALLED NEW STIFFENER CLIP ANGLE IAW SRDec 17, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR FDEA201012144660Light · intermittentL1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. R & R EMERGENCY EXIT PORTABLE LIGHT ASSY, REF MM33-50-101-2-0, OPS CHECK GOOD.Dec 14, 2010 · N485FE · Boeing 727227 · Emergency LightingSDR DALA1035709864Seat Track · corrodedDURING M-CHECK, FOUND MAIN CABIN RT SIDE OTBD SEAT TRACK AT STA 693 TO 851, RBL 44 TOP SURFACE CORRODED AND CHAFING INSIDE TRACK AREA. CUT AND REMOVED CORRODED SEAT TRACK STA 851-775, RBL 44 IAW SRM 51-30-01. INSTALLED NEW TRACK AND SPLICE IAW SRM 53-05, FIG Dec 14, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1035719864Floor Support · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160-200, LBL 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED SUPPORT IAW SRM 51-30-5.Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035729864Floorbeam · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, RBL22-44 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 53-01, FIG 1 FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABRICATED NEW FLOOR SUPPORT INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-5.Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035739864Shear Tie · crackedDURING M-CHECK FOUND MAIN CABIN CTR WING SECTION AREA STA 832, LBL15, RIVET PULLING THROUGH AT SHEAR TIE. REMOVED FASTENER FOUND CRACK IN SPLICE. REMOVED SPLICE IAW SRM 51-30-2 FORMED SPLICE IAW TRAVELER 2311NG1920. INSTALLED SPLICE AND FASTENER IAW SRM 51-3Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1035749864Floorbeam · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, LBL 44-LBL22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SUPPORT, FABRICATED NEW SUPPORT USING INSTALLED SUPPORT IAW SRM 51-30-5.Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035759864Floor Support · corrodedDURING M-CHECK, FOUND MAIN PASSENGER STA 160-218, BL0 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 53-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R FLOOR SUPPORT IAW SRM 51-30-5.Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035769864Longeron · crackedDURING M-CHECK, FOUND MAIN CABIN FS 237, LONG 17L IS CRACKED AT FRAME ATTACH FASTENER. REMOVED SECTION OF LONGERON 17L FROM STA 231-285 IAW SRM 53-13-2 FIG 3. INSTALLED NEW LONGERON SECTION IAW SRM 51-10-2,-4,-3 AND 51-30-5.Dec 14, 2010 · N773NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1035559855Angle · corrodedDURING M-CHECK FOUND FWD CARGO STA 256 DOUBLER L-ANGLE HAS CORROSION. REMOVED CORROSION FROM FWD CARGO STA 256 DOUBLER L-ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. FABRICATED 1EA L-ANGLE IAW DWG NR5911412 AND 51-60-0. ANGLE WILL BE INSTALLED ON W/CDec 13, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035569855Floorbeam · corrodedDURING M-CHECK, FOUND MAIN CABIN STA 237, LBL 1 TO 20 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION FROM MAIN FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1 & 51-10-1, FIG 22. REMOVED FLOOR SUPPORT FABRICATED IAW SRM 53-13-1, FIG 11, 51-10-1, FDec 13, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035579855Floor Panel · crackedDURING M-CHECK, FOUND CABIN FLOOR PANEL NR 20 HAS 1EA CRACK AT FASTENER HOLE. CRACKED BEYOND REPAIRABLE LIMITS. RECEIVED PANEL, LOCATED AND DRILLED IAW SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3, AND INSTALLED NUTPLATES IAW SRM 51-30-2.Dec 13, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035509864Seat Track · damagedDURING M-CHECK FOUND FWD CARGO COMPARTMENT BETWEEN STA 598-STA 617 BETWEEN L27L-L28L SEAT TRACK INSTALLED IMPROPERLY. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-01. FABRICATED NEW TRACK IAW SRM 51-10-02. PICKED UP HOLES IAW SRM 51-10-04. ALODINED AND PRIMED IDec 11, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1035529864Shear Tie · crackedDURING M-CHECK FOUND LAVATORY RT AFT STA 1151 BELOW LONGERON 14 FRAME SHEAR TIE IS CRACKED. REMOVED SHEAR TIE AT RT AFT LAV RECEIVED NEW PART. PICKED UP HOLES IAW SRM 51-10-4. INSTALLED FASTENERS AT SHEAR TIE IAW SRM 51-10-05.Dec 11, 2010 · N773NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1035519864Cargo Track · corrodedDURING M-CHECK FOUND AFT CARGO COMPARTMENT FROM FWD BULKHEAD TO STA 1003 LT CARGO TIE DOWN TRACK CORRODED AROUND FASTENER HOLES AND TRACK GROOVE. REMOVED CORROSION STA 993-1003, SRM 51-10-3. REPLACED TIE DOWN TRACK FROM FWD BULKHEAD TO STA 993 IAW SRM 51-10-4Dec 10, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1035539864Splice · crackedDURING M-CHECK, FOUND MAIN CABIN CTR WING SECTION AREA BS 832 LBL 7 SPLICE CRACKED. REMOVED SPLICE IAW SRM 51-30-2. FORMED SPLICE IAW SRM 51-10-2, 55-13-3. HEAT TREATED SPLICE 7075-T6. ALODINED & PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.Dec 10, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035209855Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN CORROSION SEVERAL PLACES FLOOR PANEL NR73. REMOVED CORROSION IAW SRM 51-10-3 OUT OF LIMITS IAW SRM 53-01, FIG 1 FLOOR PANEL REPLACED.Dec 9, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035409864Floorbeam · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, LBL 22-BL 0 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT. FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW SRM 51-30-5.Dec 9, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035419864Floor Panel · damagedDURING M-CHECK FOUND MAIN CABIN FLOOR PANEL NR59 FASTENER HOLES ELONGATED AND BROKEN OUT. CUT AWAY DAMAGE IAW 51-70-4 NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01. FABBED DOUBLER AND FILLER INSTALLED REPAIR IAW SRM 51-30-2.Dec 9, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR FDEA201012094626Skin · corrodedCORROSION ON FUSELAGE SKIN AFT OF FRAME AT BS 950F, OTBD ON STR 28R, FOUND DURING PREP TO REINSTALL AFT PIT FRAMES. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3 .090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3 .071 DIMS 5Dec 9, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DALA1035229855Floor Panel · crackedDURING M-CHECK, FOUND CABIN FLOOR PANEL 73 HAS .5" CRACK AT CORNER. REPAIRED .5" CRACK WITH DOUBLER REPAIR IAW SRM 53-05, FIG 1.Dec 8, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035239855Floor Panel · crackedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR98 HAS 1EA CRACKED HAT CHANNEL. REMOVED DAMAGED AREA IAW SRM 53-05, FIG 1, NDT SPM 06-10-01. FABRICATED HAT CHANNEL AND SPLICE REPAIR IAW SRM 53-05, FIG 1. TREATED PRIMED AND INSTALLED IAW SRM 53-05, FIG 1, 51-10Dec 8, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035069855Floor Support · mismanufacturedDURING M-CHECK FOUND CABIN BETWEEN BS 160-200, LBL 45 FLOOR SUPPORT MISDRILLED. REMOVED AND FABRICATED FLOOR SUPPORT, LOCATED AND DRILLED, TREATED AND PRIMED IAW SRM 51-30-5, 51-10-4, 51-10-2, 51-10-3 AND INSTALLED IAW SRM 51-30-5.Dec 8, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035809855Floorbeam · crackedDURING M-CHECK, FOUND CABIN BS 313 BL 0 TO LBL 23. Z-ANGLE FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT AT STA 313 IAW SRM 51-30-2. LOCATED & DRILLED NEW SUPPORT IAW SRM 51-10-2 & 51-10-4. INSTALLED SUPPORT IAW SRM 51-30-5.Dec 8, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035049864Floor Support · damagedDURING M-CHECK FOUND MAIN PASSENGER STA 148-170 RBL 55 FLOOR PANEL SUPPORT HAD DOUBLED DRILLED HOLE. REMOVED FLOOR SUPPORT IAW SRM 51-30-5 FABRICATED, TRIMMED, DRILLED, NEW FLOOR SUPPORT IAW SRM 53-13-3, FIG 11. ALODINED AND PRIMED IAW SRM 51-10-3. INSTALLEDDec 7, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035059864Floor Support · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, BLO-RBL22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION MATERIAL, REMOVED, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, REMOVED FLOOR SUPPORT IAW SRM 51-30-5 FABRICATED NEW FLOOR SUPPORT LOCATED ANDDec 7, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035119855Floor Support · mismanufacturedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 148-170, RBL 55 FLOOR PANEL SUPPORT HAS DOUBLE DRILLED HOLE. REMOVED FLOOR SUPPORT IAW SRM 51-30-5 FABBED, TRIMMED, AND DRILLED NEW FLOOR SUPPORT IAW SRM 53-13--1, FIG 11. ALODINED AND PRIMED IAW SRM 51-10-3 INSTADec 7, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034909862Web · damagedDURING LINE CHECK, FOUND DAMAGE IN NOSE WHEEL AREA WEB ON LT SIDE DENTED AND SALAD BOWL DAMAGED. TRIMMED OUT DAMAGED WEB TO 1.125" DIA, ACCOMPLISHED HFEC INSP OF CUT OUT AREA, NO DEFECTS NOTED, TREATED & PRIMED, FABRICATED DOUBLER FROM 6AL-4V .040", INSTALLEDDec 6, 2010 · N771NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034959855Attach Bracket · crackedDURING M-CHECK FOUND LT STA 756 KEEL AREA LBL 5 INBD END OF FORMER ATTACH BRACKET CRACKED. REMOVED CRACKED ATTACH BRACKET, RECEIVED FITTING PN LOCATED, DRILLED, TREATED AND INSTALLED IAW SRM 51-30-5, 51-10-3 AND 51-10-4.Dec 6, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1035029855Attach Fitting · corrodedDURING M-CHECK FOUND CORROSION ON INTERCOSTAL ATTACH CLIP IN FWD CARGO COMPARTMENT AT BS 389 L28R. REMOVED CORROSION ON ATTACH CLIP IAW SRM 51-10-3 ORIG. FABBED NEW ATTACH CLIP IAW SRM 53-01, FIG 1.Dec 6, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1035909864Skin · corrodedDURING M-CHECK, FOUND FUSELAGE EXTERIOR, REPAIR DOUBLER HAS CORROSION AT FUSELAGE STA 1151 BELOW LONGERON 29R. REMOVED EXTERIOR DOUBLER, FINGER DOUBLER, FILLER, REPLACED WITH NEW ONES, SEALED, IDENTIFIED IAW DWG NR SG09530001 REV REISSUED, NOT VALID AFTER 01-Dec 6, 2010 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1037979864Shear Tie · chafedDURING M-CHECK FOUND MAIN CABIN CTR WING SECTION, STA 794, LBL15 SHEAR TIE TO FRAME IS CHAFED. REMOVED CHAFE FROM SHEAR TIE ORIG MAT .032", LOSS .022" FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABBRICATED NEW SHEAR TIE IAW SRM 51-10-2, INSTALLED NEW SHEAR TIE IDec 5, 2010 · N773NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1034939864Shear Tie · brokenDURING M-CHECK, FOUND MAIN CABIN CTR WING SECTION/ STA 794, LGL7 SHEAR TIE TO FRAME BROKEN. REMOVED DAMAGED PART IAW SRM 51-30-08 FABBED NEW PART INSTALLED IAW SRM 51-30-08.Dec 4, 2010 · N773NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA1034949864Frame · crackedDURING M-CHECK FOUND LT MAIN WHEEL WELL, KEEL AREA BS 712 PREVIOUS FRAME REPAIR IS CRACKED. REMOVED OLD REPAIR DOUBLER AND FABRICATED NEW DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 51-30-5.Dec 4, 2010 · N773NC · Doug DC951 · Fuselage Main, FrameSDR DALA1050469885Wire · damagedDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 9 OF THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.Dec 4, 2010 · N401EA · Doug DC951 · Light System WiringSDR DALA1034969864Floor Panel · corrodedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 26 RIBS PREVIOUS REPAIR CORRODED. REMOVED OLD FILLER AND MADE NEW FILLER IAW SRM 51-70-4, FIG1 NEW FILLER MATERIAL IAW SRM 53-23-0, FIG 4 TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED NEW FILLER IAW SRM 51-70-4, FIDec 3, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034989864Floor Support · brokenDURING M-CHECK, FOUND MAIN CABIN RT STA 832 OTBD FLOOR PANEL ZEE ANGLE SUPPORT BROKEN ON END. REMOVED 26" SECTION OF ZEE ANGLE. FABRICATED 1EA ZEE ANGLE SPLICE IAW SRM 53-13-3 FIG 13, SHEET 1 & 2, 51-10-1 FIG 1, SHEET 2 AND 51-10-2. INSTALLED ZEE ANGLE AND SDec 3, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034999864Floor Support · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160-200, RBL 44, FLOOR PANEL SUPPORT HAD CORROSION. REMOVED CORROSION ON FLOOR SUPPORT MAIN CABIN STA 160-200, RBL 44 IAW SRM 53-01, FIG 1, ORIGINAL THICKNESS .060 IAW SRM 51-13-1. MATERIAL REMOVED .030 MATERIALDec 3, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034799855Floor Panel · damagedDURING M-CHECK FOUND CABIN FLOOR PANEL 33, DAMAGE AT FWD END CUTOUT DAMAGE 2 .1250"X 10 IAW SRM 51-70-4. FABRICATED 1EA DOUBLER IAW SRM 53-23-0 ITEM 6 FIG 4, 51-20-4, 51-10-4. ALODINED AND PRIMED IAW SRM 51-10-3 INSTALLED 1EA DOUBLER AND 1EA FILLER IAW SRM 51Dec 2, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034919855Cusp Web · elongatedDURING M-CHECK FOUND MAIN CABIN-FS 294-300, LBL 45 CUSP WEB HAS ELONGATED HOLES. CUT OUT DAMAGED AREA 6.8" X 1", FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRP DC9-A-53-10-16-801-663A-A, SRM 53-13-2, 51-10-3,51-30-2,51-30-5. NDT SPM 06-10-01-001.Dec 2, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1100819855Floor Panel · crackedMAIN CABIN FLOOR PNL NR 100 HAS SEVERAL CRACKS. DRILLED NEW WEB AND 5 EA HAT CHANNELS AND DEBURRED, TREATED, PRIMED IAW SRM 51-10-4. INSTALLED 5 EA HATS TO WEB IAW SRM 51-30-2. INSTALLED TAPE AND TAG IAW ERA 488334-14.Dec 2, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034559855Floor Panel · crackedDURING M-CHECK, FOUND CABIN FLOOR PANEL 78 CRACKED CUTOUT DAMAGE 2.5"X2" IAW SRM 53-05, FIG 1. FABRICATED FILLER AND DOUBLER IAW SRM 53-05, FIG 1. TREATED AND PRIMED INSTALLED FILLER AND DOUBLER IAW SRM 53-05, FIG 1.Dec 1, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034609864Support Splice · brokenDURING M-CHECK FOUND FWD CARGO COMPARTMENT STA 627, BETWEEN LONGERON 27R TO L28R SEAT TRACK SUPPORT SPLICE IS BROKEN. REMOVED EXISTING SPLICE.FABRICATED,HEAT TREATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-72-01-801-663A-A.Dec 1, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034619864Floor Panel · dentedDURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL NR39C HAS DENT. CUT OUT DAMAGED AREA 2"X 2" FABRICATED NEW FILLER AND DOUBLER IAW SRM 53-05, FIG 1. TREATED & PRIMED FILLER & DOUBLER IAW SRM 51-10-3, VERIFIED NO CRACK EXISTS. INSTALLED FILLER AND DOUBLER IADec 1, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034589855Cusp Web · crackedDURING M-CHECK FOUND BS 268, RBL-55" CUSP WEB HAS 1" CRACK. REMOVED CRACK BY CUT OUT 1.3IN X .850IN CRACK CONTAINED IAW SPM 06-10-01-001. FABRICATED 1 EA DOUBLER AND 1 EA FILLER IAW SRP A-53-10-16-801-663A. TREATED AND PRIMED IAW SRM 51-10-3 INSTALLED IAW SRMNov 30, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035009864Cusp Web · crackedDURING M-CHECK, FOUND MAIN CABIN AT LT STA 706, CUSP WEB HAS EXISTING REPAIR THAT IS CRACKED IN SEVERAL PLACES. REMOVED DOUBLER FABRICATED NEW DOUBLER, PRIMED & INSTALLED IAW SRM 51-30-02 & 53-10-16.Nov 30, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034569855Cusp Web · crackedDURING M-CHECK FOUND MAIN CABIN STA. 762 LBL-56 CUSP WEB CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER IAW; SRP 53-10-16-FIG 1, TREATED AND PRIMED IAW; SRM 51-10-3, INSTALLED DOUBLER IAW SRM 51-30-2.Nov 23, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous Structure
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