Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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 = 'JT8D17'
  ORDER BY difficulty_date DESC"

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SDR DALA1036149855Floorbeam · crackedDURING M-CHECK FOUND MAIN CABIN STA 775, RBL-54 FLOORBEAM IS CRACKED. REMOVED CRACKED FLOORBEAM SECTION STA 775, RBL 16-RBL 60 IAW SRM 51-30-2 AND 51-30-5. LOCATED AND DRILLED NEW FLOORBEAM SECTION IAW SRM 51-10-4. INSTALLED NEW FLOORBEAM SECTION IAW SRM 51-3Dec 20, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1036159855Floor Panel · crackedDURING M-CHECK FOUND CABIN, FLOOR PANEL NR 80 HAT CHANNEL CRACKED ON FWD END. CUTOUT CRACKED HAT CHANNEL AT CABIN FLOOR PANEL NR 80 IAW SRM 53-05, FIG 1. RECEIVED NEW HAT CHANNEL FABRICATED SPLICE IAW SRM 53-05, FIG 1. INSTALLED HAT CHANNEL W/SPLICE IAW SRM 53Dec 20, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1036169855Longeron · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN, STA 237, LONGERON L17 BACK AT UPPER HILOCK CRACKED. REMOVED EXISTING SPLICE AND CUT AND REMOVED DAMAGED SECTION OF LONGERON 17L F.S. 231-266 IAW SRM 51-10-4, 53-02, FIG 18. FABRICATED NEW LONGERON AND NEW REPAIR SPDec 20, 2010 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1035889873Floor Panel · damagedCABIN CREW REPORTED SOFT FLOOR IN CTR AISLE NEAR ROW 12 FLOOR PANEL 60C. REPAIRED AND REINSTALLED FLOOR PANEL 60C IAW ER/A 488286-14.Dec 18, 2010 · N782NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035849864Floorbeam · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 196, LBL 44-55 FLOOR SUPPORT PANEL HAS CORROSION. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. FABRICATED AND PICKED UP HOLES IAW SRM 51-10-2 & 51-10-4. INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.Dec 16, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035859864Floor Panel · damagedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 60, SEVERAL RIBS CHAFED, CRACKED AND BROKEN. FABRICATED NEW SKIN AND 5EA RIBS IAW SRM 53-23-0, 53-05, FIG 1. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED SKIN AND RIBS IAW SRM 51-30-2.Dec 16, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035869864Floorbeam · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 200, RBL 44 - 55 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION ON FLOOR SUPPORT STA 200, RBL 40-55 IAW SRM 53-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-Dec 16, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR C8GA2010000078Circuit Breaker · poppedON TAKE-OFF, WHILE DOING A ROLLING POWER CHECK, ENGINE NR 1 AND NR 3 EPR GAUGES FAILED TO COME UP. ABORTED TAKE-OFF AT LOW SPEED AND TAXIED BACK TO THE RAMP. MX FOUND CIRCUIT BREAKERS POPPED, RESET BREAKERS, RAN ENGINES. OPS CHECK GOOD IAW MM 77-11-00, ACFT RDec 15, 2010 · N308AS · Boeing 727227 · Engine Indicating SystemSDR C8GA2010000079Warning Light · illuminatedON TAKEOFF, THE RED "GEAR DOOR" LIGHT ON THE FWD PANEL REMAINED ILLUMINATED. SYS FOUND TO BE PERVIOUSLY DEFERRED IAW MEL 32-1, ACFT RETURNED TO SERVICE.Dec 15, 2010 · N308AS · Boeing 727227 · Landing Gear Position and WarningSDR DALA1035639855Web · crackedDURING M-CHECK FOUND E & E COMPARTMENT LT SIDE STA 146 CUTOUT WEB IS CRACKED. STOP DRILLED END OF CRACK, HFEC INSP IAW NDT SPM 06-10-01. VERIFIED CRACK CONTAINED. FABBED DOUBLER AND INSTALLED REPAIR IAW 53-01, FIG 2.Dec 14, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035649855Floor Panel · gougedDURING M-CHECK, FOUND CABIN FLOOR PANEL 58 GOUGED. CUT OUT DAMAGED AREA IAW SRM 53-05, FIG 1 & FABRICATED 1EA DOUBLER AND 1EA FILLER IAW SRM 53-05, FIG 1. TREATED AND PRIMED 1EA FILLER AND 1EA DOUBLER IAW SRM 51-10-3. INSTALLED 1EA DOUBLER AND 1EA FILLER IADec 14, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035659855Cusp Web · damagedDURING M-CHECK FOUND MAIN CABIN FS 237-256, LBL 45 CUSP WEB HAS ELONGATED HOLES. INSTALLED CUSP WEB REPAIR IAW SRM A-53-10-16-801-663A-A AND 51-10-2 P138.Dec 14, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035669855Floor Panel · damagedDURING M-CHECK, FOUND DAMAGE TO MAIN PASSENGER FLOOR PANEL NR98, STA 1138. REMOVED DAMAGE IAW SRM 51-70-4, FIG 1, FABRICATED FILLER AND DOUBLER IAW SRM 51-70-4 TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED REPAIR PARTS IAW 51-70-4.Dec 14, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035679855Floorbeam · corrodedDURING M-CHECK, FOUND MAIN CABIN STA 237, RBL 1 TO RBL 20 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION 237, RBL 1 TO RBL 20 FLOOR SUPPORT OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED FLOOR SUPPORT IAW SRM 53-13-1, FIGDec 14, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035689855Floorbeam · corrodedDURING M-CHECK FOUND MAIN CABIN STA 237, LBL 24 TO LBL 42 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION STA 237, LBL24 TO LBL42 OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED FLOOR SUPPORT IAW SRM 53-13-2 FIG 4, 51-10Dec 14, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1051129871Connector · malfunctionedDURING INDUCTION INTO THE HANGAR, MX FOUND THEY HAD NO CONTROL OF THE EXTERIOR EMERGENCY LIGHTS AS THEY WOULD NOT TURN OFF WITH SWITCH. MX DISCONNECTED AND THEN RECONNECTED THE CONNECTOR PLUG AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDIDec 13, 2010 · N780NC · Doug DC951 · Light System WiringSDR DALA1035439853Skin · crackedDURING M-CHECK, FOUND FUSELAGE EXTERIOR STA 200 BETWEEN L20L AND L21L SKIN CRACKED AT FASTENER. TRIMMED SKIN CRACKED AREA IAW DWG SR09530219. FABRICATED 4 EA FILLERS, 2 EA SKIN DOUBLERS, 1 EA FINGER DOUBLER, IAW DWG SR09530219 & SRM 53-05 FIG 57A, TREAT & PRIMDec 12, 2010 · N762NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1051099886Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE LT SIDE EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.Dec 12, 2010 · N600TR · Doug DC951 · Emergency LightingSDR DALA1051109886Connector · brokenDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 23 AND AFT IN THE CABIN WERE INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS BROKEN. THE CONNECTOR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYS SATISFIED.Dec 12, 2010 · N600TR · Doug DC951 · Light System WiringSDR DALA1035449853Frame · crackedDURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT RT SIDE STA 1209 BETWEEN STRINGER 13-14, LARGE CRACK IN WEB. CUTOUT SECTION OF WEB FROM LONGERON 7 TO 14 IAW SRM 51-70-4, NO DEFECT IAW NDT SPM 06-10-01-001 FABRICATED AND INSTALLED NEW SECTION DOUBLER IAW SRM 51Dec 11, 2010 · N762NC · Doug DC951 · Fuselage Main, FrameSDR DALA1035629853Longeron · corrodedDURING MX, CORROSION WAS FOUND ON LONGERON L17R BETWEEN STA 1136 AND STA 1117. WHEN THE FASTENERS IN THE SKIN PANEL WERE REMOVED, THE FASTENER HOLES WERE ELONGATED. WORK IAW ER/A 487366-14 AS FOLLOWS: SECTION I - COMPLETED DURING MX, SECTION II - WITHIN 8,000 Dec 10, 2010 · N762NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1035349853Web · chafedDURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT LT SIDE STA 1209, STR 5 JUST AFT OF ACTUATOR WEB REPAIR CHAFED THROUGH. REMOVED OLD REPAIR. FABRICATED NEW WEB AND REPAIR PARTS IAW DWG 9912246, REV DE AND SRM 53-13-4 NDT FORMED AREAS IAW SPM 08-10-00 AND HFEC. Dec 9, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035359853Floor Panel · looseDURING M-CHECK, FOUND MAIN PASSENGER CABIN FLOOR PANEL NR 60C AFT END OLD REPAIR LOOSE. FABRICATED NEW FLOOR PANEL AND HAT CHANNELS IAW ERA 482363-14.Dec 9, 2010 · N762NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035369853Floor Panel · corrodedDURING M-CHECK FOUND COCKPIT FLOOR PANEL NR 14B HAS CORROSION IN SEVERAL PLACES ON TOP OF PANEL. REMOVED AND FABRICATED, INSTALLED NEW PANEL IAW ERA 4861146-14.Dec 9, 2010 · N762NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035619853Skin · crackedWHILE ACCOMPLISHING A SID INSP OF PSE 53.09.028, IAW AD2006-21-06, EM5330-01148-01B, A 1.8" LONG CRACK WAS FOUND IN THE SKIN, STA 1247, L1 TO L2R. WORK IAW ER/A 482375-14AD AS FOLLOWS: SECTION I ACCOMPLISHED DURING MX - DEC 2010, SECTION II - ON OR BEFORE 24MODec 9, 2010 · N762NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1035079853Channel · crackedDURING M-CHECK (AD-FAR) AFT ACCY COMPARTMENT-APB RT LOWER CORNER -37 SEAL CHANNEL HAS APPROX 2 INCH CRACK. FABRICATED REPAIR CHANNEL. TREATED AND PRIMED AND INSTALLED ON APB RT LOWER CORNER IAW SRM 51-30-5, SRM 51-10-3 AND SRM 53-05, FIG 40 H.Dec 7, 2010 · N762NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA1035089853Channel · crackedDURING M-CHECK FOUND CABIN FLOOR PANEL NR76 HAS 1EA HAT CHANNEL CRACKED AND 1EA CHAFED THRU FABRICATED NEW PANEL IAW ERA 486157-14. REMOVED HAT CHANNELS FROM PANEL 76. DRILLED, DEBURRED AND COUNTERSUNK HOLES. ALODINED AND PRIMED FLOOR PANEL AND HAT CHANNELS.IDec 7, 2010 · N762NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035109853Hinge · corrodedDURING M-CHECK FOUND FWD AIRSTAIR DOOR HINGE AND ATTACH FASTENERS CORRODED. CORROSION WAS REMOVED IAW SRM 51-10-3. ORIG MAT .071 IAW SRM 53-33-0. REMOVED .026 REMAINING .045 OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED AIRSTAIR DOOR ON FORM 8130-3 TRACKING Dec 7, 2010 · N762NC · Doug DC951 · Entrance StairsSDR DALA1034899853Support Angle · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 750, LBL44 SUPPORT ANGLE ON TOP OF CTR WING TANK IS CRACKED. REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR SPLICES, ANGLE & FILLER IAW SRM 57-01, FIG 3 AND 51-10-4 INSTALLED REPAIR PIECES IAW SRM 57-01, FIGDec 6, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1050459882Bulb · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 4CD OF THE CABIN AND IN THE TAIL COMPARTMENT WERE INOPERATIVE. MX REPLACED THE LIGHTBULBS AS REQUIRED AND FUNCTIONALLY CHECKED EACH LOCATION.Dec 5, 2010 · N670MC · Doug DC951 · Emergency LightingSDR DALA1034929855Floor Panel · damagedDURING M-CHECK, FOUND HOLE IN MAIN PASSENGER CABIN FLOOR PANEL NR98 AT BS1138. REMOVED DAMAGE IAW SRM 51-70-4 FIG 1. 9.2500"X 1.6250" ORIGINAL MATERIAL .020. FABRICATED FILLER AND DOUBLER IAW SRM 51-10-3.Dec 4, 2010 · N762NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034839853Strap · corrodedDURING M-CHECK, FOUND AFT CARGO DOOR PAN WEB AFT INBD STRAP CORRODED. R & R AFT CARGO DOOR PAN WEB AFT INBD STRAP. INSTALLED NEW CUSTOMER FURNISHED PART IAW SRM 51-30-2 & 51-30-5.Dec 3, 2010 · N762NC · Doug DC951 · Cargo/Baggage DoorsSDR DALA1034849853Strap · corrodedDURING M-CHECK, FOUND AFT CARGO DOOR PAN WEB FWD OTBD STRAP HAS CORROSION. R & R AFT CARGO DOOR PAN WEB OTBD STRAP GUSSETT AND INSTALLED NEW OTBD STRAP GUSSETT CUSTOMER FURNISHED PART IAW SRM 51-30-2 & 51-30-5.Dec 3, 2010 · N762NC · Doug DC951 · Cargo/Baggage DoorsSDR DALA1034859853Pan · corrodedDURING M-CHECK FOUND AFT CARGO DOOR PAN HAS CORROSION FROM STA 1070-1100. REMOVED AFT CARGO DOOR PAN & WEB AND REPLACED WITH NEW CUSTOMER FURNISHED PARTS IAW DWG NR J060228 & SRM 53-05 FIG 44, SHEET 12. INSTALLED NEW PARTS IAW SRM 51-30-2 & SRM 51-30-5.M.Dec 3, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034869853Floor Support · gougedDURING M-CHECK, FOUND MAIN PASSENGER CABIN LBL 18 TO RBL 18 AFT ENTRY DOORJAMB LOWER FLOOR PANEL SUPPORT ANGLE HAS 2EA GOUGES. R & R BOTTOM SECTION OF FRAME R & R FLOOR SUPPORT LT AND RT DOOR JAMB SUPPORT AND 3EA STRIKER SECTIONS IAW DWG 5917463 AND SRM 51-30-Dec 3, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1050449870Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 15-18 AND THE AFT LT OVERWING EXIT SIGN WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.Dec 3, 2010 · N779NC · Doug DC951 · Emergency LightingSDR DALA1100909864Skin · chafedLT MLG SKIN BETWEEN GEAR DOORS CHAFED AT PANEL NR 5502NW. CHAFED AREA WAS FOUND OUT OF LIMITS. SUPPORT ANGLES FOUND CORRODED OUT OF LIMITS IAW SRM 57-01 FIG 1, FABRICATED RT AND LT SUPPORT IAW SRM 51-30-2.Dec 3, 2010 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1034759853Structure · damagedDURING M-CHECK FOUND AFT ACCESSORY COMPARTMENT, LT SIDE, BETWEEN CANTED FRAMES 1275 & 1292 UNDER INBD ATTACH POINTS FOR AIRSTAIR RELEASE MOUNT FITTING. PREVIOUS REPAIR CRACKED PAST STOP DRILLS ALSO DOUBLER CRACKED. CUT OUT DAMAGED SECTION 2 FT X 2 IN. SPLICE Dec 2, 2010 · N762NC · Doug DC951 · Fuselage Main, StructureSDR DALA1034549853Door · corrodedDURING M-CHECK, FOUND FUSELAGE EXTERIOR AIR STAIR DOOR HAS CORROSION ALONG BOTTOM EDGE IN CHANNEL. REMOVED CORROSION FROM DOOR EDGE IN CHANNEL. FOUND TO BE OUT LIMIT IAW SRM 53-01, FIG 1 REMOVED SKIN FROM DOOR EDGE. RECEIVED NEW PN 5915064-501, INSTALLED IAWDec 1, 2010 · N762NC · Doug DC951 · Entrance StairsSDR DALA1034369853Intercostal · corrodedDURING M-CHECK, FOUND FWD CARGO BETWEEN STA 218 AND 237 JUST OTBD OF LT LONG 28 INTERCOSTAL HAS CORROSION AND CRACKS APPROX 1 INCH. REMOVED CORROSION ORIGINAL MATERIAL .063. REMOVED .003 REMAIN .060 IN LIMITS IAW SRM 53-01 FIG.1 DRILLED STOP HOLE IN INTERCOSNov 30, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034409864Floor Panel · corrodedDURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL NR37 CORROSION OTBD EDGE ALONG FASTENERS. WHILE REMOVING CORROSION FOUND CRACK, CUT AWAY DAMAGE CRACKS. REMOVED DOUBLER AND FILLER FABRICATED. INSTALLED REPAIR IAW SRM 53-01, FIG 4.C.Nov 30, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034359853Skin · damagedDURING M-CHECK FUSELAGE EXTERIOR AFT CARGO DOOR JAMB FWD LOWER CORNER HAS ELONGATED FASTENER HOLE THRU SKIN AND INTERNAL DOUBLERS AND DOOR PAN AND PAN SPLICE HOLE CLEANED UP AT .3680 IAW SRM 51-20-03. INSTALLED FREEZE PLUG IAW SRM 51-20-03-801-663A-A.Nov 30, 2010 · N762NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1033959853Angle · crackedDURING M-CHECK FOUND AFT ACC COMPT STA 1209 AT L12L FRAME SHEAR ANGLE CRACKED. REMOVED 5 EA ANGLES AND CRACKED SHEAR TIE BETWEEN LONGERON 10 AND 14 RH STA 1209. FABRICATED, LOCATED, DRILLED NEW SHEAR TIE IAW SRM 51-13-4, FIG 1 AND 51-60-00 FIG.1, 51-30-2, 51-Nov 29, 2010 · N762NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1033939853Attach Angle · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN APB LT NR2 FORMER FROM FLOOR LEVEL UPPER OTBD ATTACH ANGLE IS CRACKED. REMOVED CRACKED ATTACH ANGLE IAW DC-9A53-10-25-801-663A-A. FABRICATED NEW ATTACH ANGLE FROM MAT .025 6A1-4V PO1022791 IAW DWG 9915558. LOCATED, Nov 28, 2010 · N762NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1035429853Skin · crackedDURING M-CHECK FOUND VERTICAL STAB, TOP AFT T/E OF RUDDER IS CRACKED, RUDDER ASSY OFF 09-5541-9-9003. UPON EVALUATION VERT STAB TOP AFT T/E OF RUDDER HAS SEPARATION, NO FIBER DAMAGE INJECTED RESIN HYSOL EA 9396 CURED USING HEAT THERMOCOUPLER HT7581 APPLIED WETNov 26, 2010 · N762NC · Doug DC951 · Rudder, Plate/SkinSDR DALA1033449853Cargo Track · corrodedDURING M-CHECK FOUND FWD CARGO LT SIDE FS 426 BETWEEN LONGERON 28-29 CARGO TIE DOWN TRACK CORRODED. TIE DOWN TRACK FOUND TO BE OUT OF LIMITS. NEW TIE DOWN TRACK SRM 53-23, FIG 9 LOCATED AND DRILLED, DEBURRED IAW SRM 51-10-4. TREATED & PRIMED IAW SRM 51-10-3.Nov 23, 2010 · N762NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1033469853Floorbeam · crackedDURING M-CHECK FOUND MAIN CABIN STA 775, FLOORBEAM HAS 3 CRACKS AT LT FRAME TO FLOORBEAM ATTACH POINT. ALL REPAIRS INCLUDING SRM REPAIRS REQUIRE EA APPROVAL MANAGER ACO, FORM 5100-3201 REQUIRED. PRIOR TO FLIGHT PSE 53-09-015 REF EM 5320-01037-01A STEP 9. REMONov 23, 2010 · N762NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1033519853Floor Panel · corrodedDURING M-CHECK FOUND COCKPIT, FLOOR PANEL NR15 HAS CORROSION SEVERAL PLACES ON TOP OF PANEL. REMOVED CORROSION ORIG MAT .025 REMOVED .014 REMAINING .011 OUT OF LIMITS IAW SRM 53-01 FIG 1 LOCATED DRILLED AND INSTALLED NEW CUSTOMER FURNISHED PANEL IAW SRM 51-10Nov 23, 2010 · N762NC · Doug DC951 · Fuselage Floor PanelSDR DALA1033529853Floorbeam · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237, LBL 1-20 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS IAW SRM 53-1, FIG 1. REMOVED 1 EA FLOOR SUPPORT IAW SRM 51-30-2 IAW SRM 53-13-2, FIG 4. Nov 23, 2010 · N762NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1033539853Longeron · crackedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 1136, LONG 16L CRACKED. FWD EXISTING SPLICE HAS WRONG FASTENERS INSTALLED & FWD END OF LONGERON SECTION DOES NOT MEET GAP REQUIREMENTS. REMOVED L16L AT STA 1136 FABED NEW LONGERON PN S2777922-4 AND INSTALLED IAW Nov 23, 2010 · N762NC · Doug DC951 · Fuselage Main, Longeron/Stringer
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