Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR C8GA2010000068Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE RT MLG FWD TRUNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2 EA LOWER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage, Landing Gear Attach FittingsSDR C8GA2010000069Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE LT MLG FWD TRUNNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2EA LOWER BUSHINGS AND 2EA UPPER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage, Landing Gear Attach FittingsSDR C8GA2010000070Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE NOSE LANDING GEAR LT TRUNNION FITTINGS HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage, Landing Gear Attach FittingsSDR C8GA2010000071Fitting · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE NLG RT TRUNNION FITTING HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage, Landing Gear Attach FittingsSDR C8GA2010000072Floorbeam · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE FLOORBEAM FLANGE AT STA 1110 LBL 64. REMOVED CORROSION AND FABRICATED REPAIR ANGLES FROM 7075 T6, .090" DIM 13.5" X 4", 10.5" X 4" AND 4" X 1" FILLER INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SNov 6, 2010 · N715AA · Boeing 727223 · Fuselage Main, Floor BeamSDR FDEA201010284185Connector · damagedINFLIGHT ENG SHUTDOWN NR 2 OIL TEMP FLUCTUATED INTO YELLOW RANGE. RAN QRH REDUCED POWER LEVER TO IDLE, THEN TEMP WENT ABOVE RED RADIAL. TROUBLESHOOTING DISCOVERED BROKEN WIRE GROUNDING ON THE D530 PLUG (TEMP BULB CONNECTOR) REPINNED CONNECTOR IAW CHAP 20, AOct 28, 2010 · N483FE · Boeing 727227 · Engine Oil System WiringSDR FDEA201010234156Web · damagedLT HORIZ STAB INTERNAL WEB AT STAB STA 151.81 DAMAGED. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER & FILLER, INSTALLED REPAIR DOUBLER & FILLER AT LT HORIZONTAL STAB STA 151.81 IAW SRM 55-10-2, FIG 2, SRM 53-10-9, FIG 4, SRM 51-30-2, & SRM 51-10-2.Oct 23, 2010 · N490FE · Boeing 727227 · Horizontal Stabilizer StructureSDR FDEA201010234154Skin · gougedLT SIDE LWR SKIN HORIZ STAB APPRX STA 140 TO 155 HAS GOUGE & DENT CAUSED BY HIGH REACH. CUTOUT DAMAGED SECTION OF SKIN ON LT LWR SKIN OF HORIZ STAB AT APPROX STA 140 TO 155, 8.2500" X 9.2500" IAW EX SRM REV 103, 55-10-3 FIG 4. FABRICATED REPAIR DOUBLER FROMOct 23, 2010 · N490FE · Boeing 727227 · Horizontal Stabilizer, Plate/SkinSDR FDEA201010234155Rib · damagedLT HORIZ STAB RIB AT LWR STAB STA 151.81 DAMAGED. CUTOUT DAMAGED SECTION OF LT HORIZ RIB LOWER CHORD AT STAB STA 151.81, 13.6250 " LONG IAW SRM REV 103, 55-10-4 FIG 1. FABRICATED REPAIR ANGLES FROM 2024-O, .071" X 24" X 4", QTY 2, IAW SRM 55-10-4, FIG 1 AND FOct 23, 2010 · N490FE · Boeing 727227 · Horizontal Stabilizer, Spar/RibSDR FDEA201010224147Engine · failedWHILE ADVANCING POWER FOR TAKEOFF, AT 80 PERCENT N1 ON ENG NR 2. EPR SLOW TO INCREASE, COMPRESSOR STALL OCCURED. TOWER WITNESSED FLAMES FROM NR 2 ENGINE. R & R NR 2 ENGINE IAW WORK CARD 70T0002. INSTALLED ENGINE IAW WORK CARD 70T0002.Oct 22, 2010 · N245FE · Boeing 727277 · Compressor Bleed ControlSDR FDEA201010194131Seat Track · corrodedCORROSION SEAT TRACK FLANGE/SCALLOPS MAIN CABIN RBL 25 BS 690 - BS 740. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 690 - BS 740 RBL 25, FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.Oct 19, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010194110Skin · crackedPOSSIBLE CRACK OR DEBONDED L/E INBD FOREFLAP LT WING AT NR4 FLAP ASSY ATTACHMENT. CUTOUT DAMAGE DIM: 1" X 1" AND FABRICATED DOUBLER DIM: 5" X 5 1/4" AND INSTALLED DOUBLER IAW SRM 57-50-4 FIG 1, SRM 51-10-2, SRM 51-30-2, AND NDTM 51-00-00.Oct 19, 2010 · N490FE · Boeing 727227 · Trailing Edge FlapsSDR FDEA201010194112Skin · gougedGOUGE, MCD INNER SURROUND SKIN STA 565, STR 4L. REMOVED DAMAGED MCD INNER SKIN, FABRICATED NEW INNER SKIN & INSTALLED NEW INNER SKIN AT BS 506 - BS 594, MCD INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, SRM 51-30-2.Oct 19, 2010 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201010134038Seat Track · corrodedSEAT TRACK CORRODED, STA 610 TO STA 690, RBL25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK MATERIAL USED BAC 1520-792-7178-T6511 DIMENSIONS: 17FT AND 30 INCHES IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK RBL 25 BS 480 TO BSOct 13, 2010 · N490FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201010134054Skin · gougedGOUGES MCD INNER SURROUND SKIN STA 460-480, STR 4L. REMOVED DAMAGED SKIN SECTION FROM BS 460 - BS 505, FABRICATED NEW FWD INNER SKIN & INSTALLED NEW INNER SKIN IAW SRM 51-30-2, SRM 51-30-5, & SRM 53-10-2 FIG 3A.Oct 13, 2010 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201010124030Frame · puncturedAFT CARGO COMPARTMENT, FRAME AT BS 1090 ABOVE STR 27R HAS PUNCTURE IN THE UPPER FLANGE WITH MATERIAL LOSS ON THE LOWER SURFACE .5" IN DIAMETER. CUT OUT DAMAGED AREA OF FRAME DIM 1" X 1" IAW SRM 51-40-3 FIG 1 FORMED FRAME REPAIR DOUBLER IAW SRM 51-40-3 FIG 1Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201010124031Frame · corrodedCORROSION AT FASTENER HOLE ON UPPER FLANGE OF FRAME AT BS 950C BETWEEN STRINGERS 28R AND 27R. CUT OUT DAMAGED AREA DIM 1 1/4" X 1" IAW SRM 51-40-3 FIG 1, FORMED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 5Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201010124029Bracket · damagedFWD PIT - STAND OFF BRACKET FOR ELEC LEADS IS DAMAGED AT BS 510, STR 27L. FABRICATED STRINGER REPAIR PARTS & INSTALLED STRINGER REPAIR AT BS 510 STR 27L IAW SRM 53-10-3 FIG 1 DETAIL 2 & SRM 51-10-2.Oct 12, 2010 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201010124024Web · gougedC-1 DOOR CUTOUT AFT FRAME BS 620 WEB IS GOUGED ON FWD SIDE AT STR 22R BETWEEN DOOR STOPS NR 3 AND NR 4. REMOVED C-1 DOOR AFT FRAME WEB IAW SRM 51-30-2 FABRICATED NEW FRAME WEB FROM 7075 T6 .071" DIM 106" X 6" IAW 53-10-2 FIG 3 AND 51-30-5 INSTALLED NEW FOct 12, 2010 · N467FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201010124032Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 1166 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED CORRODED SHEAR TIE AT BS 1166, STRINGER 28R TO 27R IAW SRM 51-30-2 REV 103Oct 12, 2010 · N467FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201010114002Contact · dirtyCABIN ENTRY EMERGENCY EXIT LIGHT DOES NOT TEST FROM COCKPIT SWITCH. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GOOD. OK FOR SERVICE. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GOOct 11, 2010 · N262FE · Boeing 727233 · Light System WiringSDR FDEA201010104035Floorbeam · corrodedCORROSION TOP "T" CAP FLOORBEAM MAIN CABIN BS 720A LBL 25 - BL 0. CUTOUT DAMAGE AREA AT TOP "T" CAP FLOORBEAM BS 720A LBL 25 TO BL 0 (ON 720A DIM 1.85" X 0.90" LBL 5.5" TO 7.35") IAW SRM 53-10-8, FIG 8, FABRICATED 2 ANGLES FROM 7075O .090 HEAT TREAT TO T6 COOct 10, 2010 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201010104036Seat Track · corrodedCORROSION SEAT TRACK FLANGE & SCALLOP MAIN CABIN LBL 45 BS 690 - BS 740. REMOVED & REPLACED SEAT TRACK SECTION AT LBL 45 BS 740 - BS 690 & FABRICATED NEW SPLICE AT LBL 45 BS 690 IAW SRM 53-10-5 FIG 1. FABRICATED SEAT TRACK FROM BAC 1520-792-71787T6511 DIM: Oct 10, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010063955Duct · failedENGINE FAIL LIGHT ILLUMINATED AT 100 KTS ON T/O OAT 10. 169,000 TOGW. REJECTED T/O CHECKLIST COMPLIED WITH. R & R NR 2 ENGINE N1 GAUGE AS PRECAUTIONARY IAW AMM 31-00-011-4. RAN NR 2 ENGINE IAW JRH CHAPTER 6, ALL ENGINE PARAMETERS WERE NORMAL. ON RETURN TO Oct 6, 2010 · N283FE · Boeing 727233 · Engine Bleed Air SystemSDR FDEA201010063956Seat Track · corrodedCORROSION SEAT TRACK FLANGE BL 0 BS 550 - BS 670. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 51-30-2 AND SRM 53-10-5 FIG 1.Oct 6, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010053942Seat Track · corrodedCORROSION SEAT TRACK SPLICE MAIN CABIN LBL 45 BS 460 - BS 490. REMOVED SEAT TRACK FROM BS 480 - 390, FABRICATED NEW SEAT TRACK SECTION, CLEANED & EVALUATED SEAT TRACK SPLICE AT BS 490, FOUND NO CORROSION. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1Oct 5, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010053944Seat Track · corrodedCORROSION SEAT TRACK FLANGE & SCALLOPS MAIN CABIN RBL 45 BS 420 - 480. REMOVED SEAT TRACK SECTION FROM BS 420 - BS 480 RBL 45. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6, APPROX DIM: 60". INSTALLED NEW SEAT TRACK SECTION FROM BS 420 - BS 480 ROct 5, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010053946Seat Track · corrodedCORROSION SEAT TRACK FLANGE & INSIDE SCALLOPS LBL 25 BS 850 - 760. REMOVED SEAT TRACK SECTION LBL 25 BS 850 - 760 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-841-7178-T6 IAW SRM 51-30-5, SRM 53-10-2 FIG 7 & SRM 51-10-2 AND INSTALLED Oct 5, 2010 · N490FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009243702Fire Detector · false activationON TAKEOFF APPROX 1000' AGL GOT AN INTERMITTENT FIREBELL AND S/O SAW CARGO SMOKE WARNING LOWER FWD CARGO ON, THEN THE LIGHT WENT OUT. AML REFLECTED A PREVIOUS WRITEUP ON THE SAME SYS. DEEMED TO RETURN AND LAND IMMEDIATELY. REMOVED SMOKE DETECTORS 1,2,3, &Sep 24, 2010 · N498FE · Boeing 727232 · Fire DetectionSDR FDEA201009223652Battery Pack · inoperativeDURING PRE-DISPATCH CHECKS FOUND FWD ENTRY DOOR ESCAPE LIGHT INOP. DEN R RELEASED FOR SERVICE IAW MEL: 33-16-02-A CATEGORY: B EXPIRATION: 24SEP10 "MEL 33-16-02-A: FWD ESCAPE SLIDE LIGHT - INOP." L/E-LAMPED IAW SMP NO HELP.ITEM IS DEFFERED. R & R EMERGENCY Sep 22, 2010 · N286FE · Boeing 727233 · Emergency LightingSDR FDEA201009073307Support Fitting · crackedCRACKED FITTING (SUPPORT) BS 620, MAIN CARGO DOOR CUT OUT. REMOVED CRACKED FITTING AT BS 620 MAIN CARGO DOOR CUTOUT & INSTALLED NEW FITTING IAW SRM 51-30-2 & SRM 51-30-5.Sep 7, 2010 · N494FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA201000032Beam · corrodedWHILE IN HEAVY MX, PERFORMING INSP IT WAS NOTED THAT THE RT MLG BEAM AND OTBD SUPPORT FITTING BORES ARE CORRODED. REMOVED CORROSION, HFEC, SHOT PEENED, INSTALLED BUSHING AND SPACER. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Wing, Landing Gear Attach FittingsSDR C8GA201000034Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT A 2 EA DENTS ON THE RT WING UPPER L/E STA 160 ARE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER FROM 2024 T3 .050" 2" X 3" & 2.5" X 5.25". INSTALLED REPAIRS, NO OTHER DEFECTS NOTED. ACFT WAS Aug 30, 2010 · N755DH · Boeing 727225 · Wing, Plate/SkinSDR C8GA201000046Doubler · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT 2 EA DOUBLER'S REQUIRE REPLACEMENT IAW SB 53A0198R3, AD 2007-12-14 ON THE FUSELAGE AT THE FWD ENTRY DOOR UPPER AND LOWER HINGE CUTOUTS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 30, 2010 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201008283170Frame · damagedNUMEROUS DRILLED HOLES IN FRAME BS 480 RADIUS WHERE NUT-PLATES ARE INSTALLED STR 6L- 9L. ( 7 EA ) REMOVED DAMAGED FRAME, LOCATED & DRILLED NEW FRAME & INSTALLED NEW FRAME IAW SRM 51-30-2 & EA 7-5310-135585.Aug 28, 2010 · N494FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201008253214Fitting · crackedMCD UPPER SILL FITTING BS 460 FWD SIDE BETWEEN STR 3L AND 4L CRACKED. REMOVED AND REPLACED MCD UPPER SILL FITTING IAW SRM REV 103, 51-30-5 AND 51-30-2.Aug 25, 2010 · N494FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR C8GA2010000019Support Fitting · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT WING LANDING GEAR REAR TRUNNION SUPPORT BEAM AT REAR SPAR ATTACH POINT FITTING IS CRACKED APPROX. .4375". MODIFIED FITTING IAW THE SB 57-0153, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Wing, Landing Gear Attach FittingsSDR C8GA2010000016Skin · corrodedWHILE IN HEAVY MX PERFORMING INSPECTIONS CORROSION WAS NOTED AT THE LT WING, LOWER SKIN FWD OF FRONT SPAR WS 250-287 BEHIND THE NR1 & NR2 KRUGER FLAP. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED BLEND-OUT IAW RES-W1 NR 2002564-12 LOSS OF MATERIAL IS .095"Aug 23, 2010 · N755DH · Boeing 727225 · Wing, Plate/SkinSDR C8GA2010000018Failsafe · corrodedWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE RT SIDE OF HORIZ STABILIZER REAR SPAR UPPER CHORD FAIL SAFE STRAP HAS SURFACE CORROSION. R & R STRAP PN 65-16876-50. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Aug 23, 2010 · N755DH · Boeing 727225 · Horizontal Stabilizer StructureSDR FDEA201008203066Stringer · corrodedCORROSION INSIDE CHANNEL OF STR 30, BS 950C TO 950F. REMOVED CORROSION IN CHANNEL OF STRINGER IAW SRM, REV 103, 51-10-6. COMPLIED WITH UT THICKNESS IAW NDTM PT 4, 51-00-00, FIG 2, AND MAPPED DAMAGE LOCATION IAW EA 7-5330-135588. ENGINEERING ANALYSIS FOUND NO Aug 20, 2010 · N494FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR C8GA2010000030Acm · inoperativeDURING CLIMB OPERATION, THE ACFT WAS UNABLE TO MAINTAIN CABIN PRESSURIZATION ON RT PACK. LT PACK WAS DMI. CLEANED CONNECTOR ON LT PACK TEMP BULB, R & R LT PACK FLOW CONTROL VALVE, RE RACKED AUTO PSI CONTROLLER, R & R LT ACM, R & R LT COMPRESSOR DISCHARGE OVEAug 19, 2010 · N898AA · Boeing 727223 · Cabin Cooling SystemSDR FDEA201008143109Skin · gougedMCD INTERIOR SKIN GOUGED STA 618 STR 8L. TRIMMED DAMAGED AREA AT MCD INTERIOR SKIN STA 618 STR 8L, FABRICATED REPAIR DOUBLER FROM 2024T3 0.071" DIM 6" X 10.6250" AND INSTALLED DOUBLER REPAIR IAW EA 7-5230-142192.Aug 14, 2010 · N487FE · Boeing 727227 · Cargo/Baggage DoorsSDR ABXR2010081100034Fairing · crackedDURING A HEAVY MX EVENT THE RT WING OTBD FLAP, INBD FLAP TRACK, FWD FAIRNG WAS FOUND TO BE CRACKED AND DENTED. R & R FAIRING. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR ABXR2010081100035Fairing · crackedDURING A HEAVY MX INSP, EVENT THE RT WING OTBD FLAP, OTBD FLAPTRACK AFT FAIRING WAS FOUND TO BE CRACKED AND DENTED. R & R FAIRING. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR ABXR2010081100036Skin · dentedDURING A STORM DAMAGE REPAIR MX EVENT A DENT WAS DISCOVERED ON THE RT WING L/E. DENT WAS SMOOTH AND FREE FROM SHARP CREASES LOCATED ON THE LOWER SURFACE AND MEASURED 4.00" LONG X 1.20' WIDE 0.162 DEEP. THE DENT WAS COLD WORKED BACK TO ITS ORIGINAL SHAPE AND CAug 11, 2010 · N801EA · Boeing 727225 · Wing, Plate/SkinSDR ABXR2010081100037Intercostal · damagedDURING A STORM DAMAGE REPAIR MX EVENT & DURING A SKIN REPLACEMENT AN INTERCOSTAL WAS DISCOVERED WITH MULTIPLE HOLES IN THE RADIUS. FABRICATED NEW INTERCOSTAL AND INSTALLED. ITEM RETURNED TO SERVICE.Aug 11, 2010 · N801EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201008112930Seat Track · corrodedCORROSION SEAT TRACK MAIN CABIN BS 480 - BS 610, BL 0. REMOVED SEAT TRACK SECTION IAW SRM, REV 103, 51-30-2. FABRICATED REPLACEMENT SEAT TRACK SECTION USING BAC1520-792, 7178-T6511, 130" IN LENGTH IAW SRM 53-10-5 FIG 1 AND IAW P-F SRM 53-10-2 FIG 7A. INSTAug 11, 2010 · N494FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008112931Seat Track · corrodedCORROSION FLANGE SEAT TRACK MAIN CABIN BS 480 - BS 690, LBL 25. REMOVED DAMAGE SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION AT LBL 25 BS 480-610, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 & SRM 51-30-2 & P-F SRM 53-10-2.Aug 11, 2010 · N494FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008112932Seat Track · corrodedCORROSION ON SEAT TRACK RBL 25, STA 1130 - 1183. REMOVED CORRODED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW DWG NR 53FX976 AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.Aug 11, 2010 · N494FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008112933Battery Pack · failedEMERGENCY EXIT LIGHT BY L-1 DOOR IS INOP. R & R EMERGENCY EXIT LIGHT BATTERY PACK (MM 33-50-101-2). OPS CHECKED GOOD. OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.Aug 11, 2010 · N486FE · Boeing 727227 · Emergency Lighting
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