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 DALA1035489855Angle · crackedDURING M-CHECK, FOUND BS 110, BULKHEAD LBL4, 7 IN ABOVE BELLY ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW DWG 9915600. TREATED AND PRIMED ANGLE IAW SRM 51-10-3. INSTALLED NEW ANGLE IAW SRM 51-30-5.Nov 23, 2010 · N765NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1036009855Frame · crackedDURING M-CHECK FOUND LT STA 756 KEEL AREA FORMER CRACKED OTBD END. TRIMMED OFF CRACKED FLANGE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-03, FIG 12, 53-13-3 FIG 2, 51-10-4, 51-10-2, 51-10-3, 51-30-2, 51-30-5.Nov 23, 2010 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1100829864Floor Panel · crackedAFT CARGO CTR FLOOR PANEL NR 3 HAS A CRACK IN RADIUS OF DOOR CUTOUT AREA. REMOVED CRACK BY TRIMMING AREA. NDT VERIFIED NO CRACK EXIST IAW NDT SPM 06-10-01. FABRICATED DOUBLER SEALED & INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW EA98-201837 & SRM (51-1Nov 23, 2010 · N773NC · Doug DC951 · Fuselage Floor PanelSDR FDEA201011224465Shear Tie · crackedUPON REMOVAL OF SHEAR TIE FOR FRAME REMOVAL, FOUND SHEAR TIE CRACKED ON OTBD UPPER CORNER, BS 990, BETWEEN STRINGER 28R AND 29R. REMOVED SHEAR TIE IAW SRM 51-30-2 REV 103 FABRICATED NEW SHEAR TIE FROM BAC1505-39042 7075-T6511 7" LONG IAW BAC DWG 65-16340 Nov 22, 2010 · N488FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR DALA1034579855Floor Panel · bentDURING M-CHECK, FOUND CABIN FLOOR PANEL NR 99, CORNER BENT AT EXISTING REPAIR. REPAIRED IAW SRM 51-30-2, 51-20-0 & 53-23-0, FIG 6, PAGE 9.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR DALA1034769855Floorbeam · crackedDURING M-CHECK FOUND FWD CARGO COMPARTMENT STA 332 RT FLOOR SUPPORT CRACKED. FLOOR SUPPORT REMOVED, TIG WELDED PRIMED AND REINSTALLED IAW SRM 51-10-3,51-30-2,51-30-5, SRP DC-9 A51-71-03.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1034779855Floor Support · crackedDURING M-CHECK FOUND FWD CARGO STA 598. LT FLOOR SUPPORT CRACKED, FLOOR SUPPORT REMOVED, TIG WELDED IAW SRM 51-10-3, 51-30-2, 51-30-5 SRP, DC9-A-51-71-03.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034789855Floor Support · crackedDURING M-CHECK FOUND FWD CARGO COMPARTMENT STA 351 RT FLOOR SUPPORT CRACKED. FLOOR SUPPORT REMOVED AND TIG WELDED. REINSTALLED IAW SRM 51-10-3, 51-30-2, 51-30-5 SRP DC-9 A51-71-03.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035269855Attach Angle · corrodedDURING M-CHECK, FOUND FWD PIT STA 218 L28L-28R LOWER GIL LINER ATTACH ANGLE HAS CORROSION. REMOVED CORROSION OUT OF LIMITS. CUT OUT DAMAGE 1" X 1.5" NDT VERIFIED DAMAGE, REMOVED, FABRICATED AND INSTALLED FILLER HEAT TREATED IAW SRM 51-10-3, 53-01 FIG 1, 53-2Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1035389855Floorbeam · crackedDURING M-CHECK, FOUND CRACK IN RT STRUT LOWER END AT BS 579 STOP DRILLED CRACK . FABRICATED REPAIR DOUBLERS IAW SRM 53-01, FIG 2 AND SRM 53-13-2 FIG 4 TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED REPAIR DOUBLER IAW SRM 51-30-5.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035499855Strut · crackedDURING M-CHECK, FOUND BS 560 RT STRUT CRACKED AT LOWER END. REMOVED FASTENERS IAW SRM 51-30-2, STOP DRILLED CRACK IAW SRM 53-01, FIG 2, FABRICATED REPAIR DOUBLER IAW SRM 51-10-2 & 53-01 FIG 2. LOCATED,DRILLED & DEBURRED IAW SRM 51-10-4 INSTALLED REPAIR DOUBLNov 22, 2010 · N765NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036349855Strut · crackedDURING M-CHECK FOUND FWD CARGO STA 579 LT STRUT CRACKED AT LOWER END. REMOVED FASTENERS IAW SRM 51-30-5 STOPPED DRILLED CRACK IAW SRM 53-01, FIG 2 FABRICATED 2 EA REPAIR DOUBLER'S IAW SRM 53-01, FIG 2, TREATED & PRIMED DOUBLER'S IAW SRM 51-10-3 INSTALLED REPAINov 22, 2010 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036359855Unknown · crackedREMOVED FASTENER'S IAW SRM 51-30-5 STOPPED DRILLED CRACK IAW SRM 53-01, FIG 2. FABRICATED 2 EA REPAIR DOUBLER'S IAW SRM 53-01, FIG.2 TREATED & PRIMED REPAIR DOUBLER'S IAW SRM 51-10-3. INSTALLED REPAIR DOUBLER'S IAW SRM 51-30-5.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036769855Attach Angle · crackedDURING M-CHECK, FOUND AFT ACCESSORY LT SIDE CANTED FRAME 1292 RAIN BOX ATTACH ANGLE CRACKED. REMOVED DOUBLER AND ANGLE IAW SRM 51-30-2. FABRICATED NEW DOUBLER FROM IAW SRM 51-60-0. INSTALLED NEW ANGLE AND DOUBLER IAW SRM 51-30-2 AND 51-30-5 P134.Nov 22, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1100589855Web · crackedAFT ACCESSORY RT SIDE BETWEEN CANTED FRAME 1292 AND 1303, RBL 8 CLOSE OUT WEB CRACKED. STOP DRILLED CRACK IAW SRM 53-04, FIG 2, SHEET 3. VISUALLY VERIFIED CRACK CONTAINED IAW NDT SPM 09-00-06. FABRICATED DOUBLER IAW SRM 53-01, FIG 2, SHEET 3. LOCATED, DRINov 22, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1100599855Web · crackedAFT ACCESSORY LT SIDE BETWEEN CANTED FRAME BS 1292 AND 1303 LBL 8 CLOSE OUT WEB CRACKED. STOP DRILLED CRACK IAW SRM 53-01, FIG 2, SHEET3. VISUALLY VERIFIED CRACK CONTAINED IAW NDT SPM 09-00-06, FABRICATED DOUBLER IAW SRM 53-01, FIG 2, SHEET 3. LOCATED, DRILLENov 22, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1035249855Floorbeam · crackedDURING M-CHECK, FOUND AFT CARGO COMPT STA 908, RT FLOOR SUPPORT CRACKED. REMOVED, TIG WELDED AND INSTALLED IAW SRM 51-30-2, 51-30-5 AND SRP DC9-A51-71-03-801-663A-A.Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035259855Floorbeam · crackedDURING M-CHECK, FOUND AFT CARGO COMPARTMENT STA 908, LT FLOOR SUPPORT CRACKED. REMOVED, REPAIRED AND REINSTALLED FLOOR SUPPORT IAW SRM 51-30-2 AND 51-30-5.Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1035399855Attach Fitting · crackedDURING M-CHECK, FOUND AFT CARGO COMPT STA 1151 AT L28L FRAME TO INTERCOSTAL CLIP CRACKED. REMOVED ATTACH CLIP AT STA 1151, L28L IAW SRM 51-30-5. FABRICATED CLIP IAW SRM 51-10-2 AND DWG PL 9915550 REV E, LOCATED, DRILLED & DEBURRED IAW SRM 51-10-4 AND INSTALLEDNov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1035799855Frame · damagedDURING M-CHECK FOUND AFT CARGO COMPT STA 1108, L29L FRAME HAS A HOLE ON TOP SIDE. RECEIVED MATERIAL FOR REPAIR IAW SRM DC-9-A-53-10-06-663A-A. LOCATED, DRILLED STRAP IAW SRM 51-10-2, 51-10-4. INSTALLED STRAP IAW SRM 51-30-5.Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1036199855Frame · damagedDURING M-CHECK, FOUND AFT CARGO COMPARTMENT BS 1136 AT L26L FRAME HAS A HOLE IN IT ON TOP SIDE. FABRICATED REPAIR STRAP LOCATED, DRILLED, DEBURRED, TREATED PRIMED & INSTALLED STRAP IAW DC9-53-13-3, 51-10-4, 51-10-3, 51-30-5 AND NWA SRP DC-9-A-53-10-05-801-663Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, FrameSDR DALA1036489855Longeron Splice · crackedDURING M-CHECK, AFT CARGO BETWEEN STA 1068 & 1088, L29L SPLICE CRACKED. R & R CRACKED SPLICE IAW SRM 51-30-5.Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1100629855Attach Fitting · crackedAFT CARGO COMPT STA 1167 AT L28L FRAME TO INTERCOSTAL ATTACH FITTING CRACKED. R & R AT AFT CARGO STA 1167, ATTACH FITTING IAW SRM 51-30-3. P245. REQUIRED INSP COMPLETED.Nov 21, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1034599855Cusp Web · crackedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 278, RBL 55 CUSP WEB CRACKED. REMOVED CRACK AND FABRICATED 1 EA DOUBLER AND 1 EA FILLER IAW SRP A-53-10-16-801-553-A-A TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.Nov 20, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1036819855Fitting · misinstalledDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 218, RBL 55 DOUBLE DRILLED HOLE THROUGH CUSP WEB AND FLOORBEAM. REMOVED FLOORBEAM FITTING, STA 218, RBL 55. FABRICATED IAW DWG NR3912075. LOCATED AND DRILLED IAW SRM 51-10-4 TREATED AND PRIMED IAW SRM 51-10-3 ANov 20, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1100809855Longeron · crackedMAIN CABIN, FWD STA 160, LONGERON NR3 CRACKED. CUT OUT CRACKED SECTION AND INSTALLED REPAIR IAW SRM 51-30-2, 53-02, FIG 18, 51-10-3, 51-30-5.Nov 20, 2010 · N764NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1035919864Cargo Track · corrodedDURING M-CHECK, FOUND AFT CARGO STA 1106 TO 1167 RT TIE DOWN TRACK HAS CORROSION IN SEVERAL PLACES. REMOVED CORROSION ON TIE DOWN TRACK, STA 1167, RT SIDE IAW SRM 51-10-3, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, REMOVED TIE DOWN TRACK IAW SRM 51-30-2. RECINov 19, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011184412Door · unsecureACFT WOULD NOT PRESSURIZE. LOUD NOISE AROUND MAIN ENTRY DOOR. NO DOOR LIGHTS. HANDLE IN PROPER POSITION. UPON ACFT ARRIVAL FOUND L-1 DOOR T/E NOT FULLY CLOSED. OPENED AND CLOSED DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. PERFORMED INSP OF L-1 DOOR WITH NONov 18, 2010 · N491FE · Boeing 727227 · Service DoorsSDR FDEA201011184415Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950, LBL 61 - 45. REMOVED DAMAGED UPPER TEE CAP FROM FLOORBEAM, LOCATED AND DRILLED NEW UPPER TEE CAP AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND DWG 65-16338.Nov 18, 2010 · N233FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201011184416Skin · gougedGOUGES INNER SURROUND SKIN STA 620, STR'S 8L-16L. CUT OUT DAMAGED SKIN SECTION, FABRICATED NEW SKIN SECTION USING 2024T-3 .125 DIMS 56" X 22" AND SPLICE USING 2024T-3 .125 DIMS 4" X 22" AND INSTALLED REPAIR PARTS IAW EA 7-5330-143921.Nov 18, 2010 · N233FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DALA1035289864Skin · damagedDURING M-CHECK, FOUND FWD CARGO COMPARTMENT DURING INSP, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 508 MIN. REMAINING MATERIAL .042 DEFER TO ENGINEERING FOR REVIEW. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 ANNov 16, 2010 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1035299864Skin · damagedDURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSPECTION, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 450 MIN. REMAINING MATERIAL .042. DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 AND PNNov 16, 2010 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1035309864Skin · damagedDURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSP MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 395 MIN. REMAINING MATERIAL .045. DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 AND PN 09-530Nov 16, 2010 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1035959864Bulkhead · crackedDURING M-CHECK, FOUND NOSE WHEEL WELL THROUGH ACCESS HOLE, STA 69, RBL 12 BULKHEAD IS CRACKED APPROX .5 INCH. STOP DRILLED CRACK WITH A .250" HOLE ON WEB IN NOSE WHEEL WELL THROUGH ACCESS HOLE STA 69 RBL 12 BULKHEAD WEB, CRACK CONTAINED. FABRICATED DOUBLER IANov 16, 2010 · N773NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA1035979855Hinge Bracket · crackedDURING M-CHECK, FOUND LT WING NR 4 AFT FLAP HINGE OTBD SUPPORT CRACKED APPROX 1 INCH. REMOVED CRACKED HINGE BRACKET, RECEIVED NEW HINGE BRACKET, PN 09-2700-3-0515. LOCATED AND DRILLED HOLES, TREATED AND INSTALLED IAW SRM'S 51-30-2/51-10-3/51-10-4 AND 51-30-1Nov 16, 2010 · N764NC · Doug DC951 · Trailing Edge FlapsSDR DALA1036789855Attach Bracket · corrodedDURING M-CHECK, FOUND FUSELAGE EXTERIOR STA 870 AT L30 ATTACH BRACKET HAS CORROSION. REMOVED CORROSION IAW SRM 53-01, FIG 1 IAW SRM 53-53-0 OUT OF LIMITS. REMOVED BRACKET IAW SRM 51-30-5. FABRICATED NEW BRACKET IAW DWG 5925965. HEAT TREATED ON TRAVLER 2312N0Nov 16, 2010 · N764NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1036809855Stiffener · crackedDURING M-CHECK, FOUND MAIN CABIN-APB LT UPPER HORIZ STIFFENER IS CRACKED AT AFT ENTRY DOOR LT UPPER CORNER. REMOVED CRACKED HORIZ STIFFENER & ATTACH ANGLES IAW SRM 51-30-2 & 51-30-5. LOCATED, DRILLED, REINSTALLED NEW STIFFENER AND ATTACH ANGLES IAW SRM 51-10Nov 16, 2010 · N764NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA1100619855Stiffener · crackedMAIN CABIN-APB RT UPPER CORNER, VERTICAL STIFFENER AT L2R OF APB IS CRACKED BETWEEN FASTENERS. REMOVED CRACKED VERTICAL STIFFENER ON APB IAW SRM 51-30-2 AND 51-30-5. FABRICATED AND INSTALLED STIFFENER IAW SRM 51-30-5. REQUIRED INSP COMPLETED.Nov 16, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR FDEA201011154413Skin · corrodedCORROSION - INTERIOR FUSELAGE SKIN STATION 950D TO STA 950E OTBD SIDE OF STR 29L. REMOVED DAMAGED AREA OF SKIN IAW EA7-5330-123571 AND SRM 51-10-1, REV 103. FABRICATED DOUBLER, TRIPLER, & FILLERS IAW EA 7-5330-123571. INSTALLED DOUBLER, TRIPLER AND FILLERNov 15, 2010 · N233FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DALA1032949855Floor Support · corrodedDURING M-CHECK, FOUND MAIN CABIN STA 200, RBL 1 TO RBL 20 FLOOR SUPPORT HAS CORROSION. FLOOR SUPPORT AT STA 200, RBL 1 TO RBL 20 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. FABRICATED NEW FLOOR SUPPORT FROM EXTRUSINov 14, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1032959855Floor Support · corrodedDURING M-CHECK FOUND MAIN CABIN STA 160 TO 200, LBL 44 FLOOR SUPPORT HAS CORROSION. FLOOR SUPPORT STA 160-200 LBL ORIG MAT .060 CORRODED BEYOND LIMITS. FAB NEW SUPPORT USING PN 60-25767075T6511, PO 216ND946 LOCATED, DRILLED, TRIMMED, DEBURRED, TREAT, PRIMED ANov 14, 2010 · N764NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1034809855Seat Track · corrodedDURING M-CHECK FOUND MAIN CABIN STA 200 TO 285 RBL 22 SEAT TRACK HAS CORROSION SEVERAL PLACES. REMOVED CORROSION. ORIG MAT .090, REMOVED .031 REMAINING .059 R & R SEAT TRACK BS 200-285 IAW SRM 51-10-3,53-01 FIG 1,51-10-1,51-30-5, 51-10-2,51-10-4,53-05 FIG 4F,Nov 14, 2010 · N764NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1035219855Seat Track · corrodedDURING L-CHECK, FOUND MAIN CABIN STA 237, LBL 44 SEAT TRACK HAS CORROSION. REMOVED CORROSION ON SEAT TRACK STA 239, LBL 44 FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SEAT TRACK STA 200 TO 305, LBL 44 RECEIVED NEW TRACK LOCATED DRILLED AND DEBURRED IAW Nov 14, 2010 · N764NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1035479855Floor Panel · corrodedDURING M-CHECK, FOUND COCKPIT FLOOR PANEL NR15 HAS CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS WAS .020. REMOVED .005 OUT OF LIMITS IAW SRM 53- 01 FIG.1. RECEIVED NEW PANEL DRILLED IAW SRM 51-10-4. TRANSFERRED ATTACH BRACKETS FROM OLD PANEL TO NEW PANENov 14, 2010 · N765NC · Doug DC951 · Fuselage Floor PanelSDR DALA1035899864Seat Track · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200-303, RBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-3 & 53-05. REMOVED SEAT TRACK IAW SRM 51-30-1. FABRICATED SEAT TRACK IAW SRM 53-23-0, FIG 4 & LOCATED, DRILLED IAW SNov 14, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011134339Stringer · corrodedSTRINGER CORRODED STA 950C TO 950D, STR 29L. R & R STRINGER 29L FROM BS 950 TO 1010 IAW SRM 51-30-5 AND 51-30-2 REV 103 AND DWG NR65-56441.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201011134347Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620, STR'S 6L AND 10L. REMOVED MCD INNER SKIN AND SPLICES AT BS 594 TO 640 STR 2R TO 6L, FABRICATED INNER SKIN AND SPLICES FROM 2024T3 0.125" APPROX DIM 80" X 48" AND 22" X 11" AND INSTALLED INNER SKIN AND SPLICES IAW SRM 51Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011134332Seat Track · corrodedSEAT TRACK CORRODED STA 360 TO 480 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51- 10-2, AND 51-30-2 REV 103.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011134333Seat Track · corrodedSEAT TRACK CORRODED STA 360 TO 480 BL 0. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7A REV D AND SRM 51-30-5, 51-10-1, 51-10-2 AND 51-30-2 REV 103.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011134335Seat Track · corrodedSEAT TRACK CORRODED STA 360 TO 480 RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 344 TO 480 RBL 45 FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
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