Boeing 727-225

Service difficulty reports · 4,226

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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 aircraft_model_key = '727225'
  ORDER BY difficulty_date DESC"

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SDR DHL2007742043Skin · dentedFUSELAGE EXTERNAL BS 316 ON STRINGER 3L HAS SKIN DENTED. EVALUATED DENTS ON BS 316 STRINGER 3L. A:0.9" Y:0.010" A/Y:90 AND A:1.1" Y:0.017" A/Y RATIO 64.71, A/Y RATIO WITHIN LIMITS BUT FOUND DENTS OUT OF LIMITS DUE TO DENTS ARE LOCATED OVER STRINGER IAW B-727 Nov 15, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA04785Flange · delaminatedNR 1 ENGINE UPPER COWL T/E FLANGE IS CHIPPED AND DISBONDED REMOVED NR 1 ENGINE UPPER COWL T/E FLANGE, LOCATED AND DRILLED NEW FLANGE. INSTALLED NEW FLANGE, REF SRM 51-30-2 PG 1-4 REF DWG 65-19508.Nov 14, 2007 · N464FE · Boeing 727225 · Nacelle/Pylon, Main FrameSDR 07FDEA04788Support · corrodedBODY FAIRING FRAME SUPPORT LOCATED RIGHT OF AIR CONDITION HOOK UP IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, ORIGINAL .040". REMOVED .023", REMAINING .014 IAW 53-101, TOOL AAR 10274 CAL DUE 12-27-07. REMOVED FAIRING AND BRACE. FABRICATED, DRNov 14, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04787Tension Tie · crackedFOUND CLIP CRACKED AT FS 480 AND STR 2. REMOVED FASTENERS IN LOWER WEB. REMOVED CRACKED TENSION CLIP, FABRICATED NEW TENSION CLIP AND INSTALLED NEW TENSION CLIP AND FASTENERS IN LOWER WEB. REFERENCE DRAWING NR 53FX1285 AND SRM 51-30-02 CLASSIFIED AS A MAJORNov 14, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04786Casting · corrodedMAIN DECK 1L DR CUT OUT LWR HINGE UPPER STOP PLATE SUPPORT CASTING IS CORRODED AT FASTENER HOLE, BS 307, STR 13R, WL 238. REMOVED FITTING RER SRM 51-30-2, SENT TO HAVE NEW CASTING MATCHED DRILLED UP FOR BEARING PLATED AND INTO PLACE PER SRM 51-30-5 PG 1,2. Nov 14, 2007 · N464FE · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2007742035Bracket · crackedNR 2 SLAT ACTUATOR UPPER MOUNT HAS PLAY WITH CRACK INDICATION AT INBOARD UPPER BOLT. VERIFIED BY NDT. REMOVED PREVIOUS DOUBLER AT NR 2 SLAT ACTUATOR MOUNT INBOARD BRACKET IAW B-727 SRM 51-30-2 FIGURE 1. C/W HFEC ON STIFFENER/WEB IAW B-727 NDTM PT 6, 51-00-0Nov 13, 2007 · N742DH · Boeing 727225 · Wing, Attach FittingsSDR 07FDEA04774Accessory Unit · failedAFTER TAKEOFF, WITH GEAR RETRACTED, WHEN WE WENT FROM FLAPS 5 TO FLAPS 2 GOT THE TAKEOFF WARNING HORN, WOULD ONLY EXTINGUISH BY REDUCING POWER. ALSO GOT THE HORN WHEN WE WENT FROM FLAPS 25 TO FLAPS 30 AT LANDING. R & R MLG ACCESSORY UNIT IAW MM 32-09-121-4 Nov 13, 2007 · N465FE · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR 07FDEA04766Bulkhead · gougedFUSELAGE STA 178 FORWARD SIDE OF PRESSURE BULHEAD, SKIN HAS A GOUGE 2.5" IN FROM OUTER EDGE AT LEFT SIDE, 4TH RADOME ATTACH NUTPLATE FITTING DOWN BLENDED GOUGE, ORIGINAL MATERIAL IS .030" BONDED TO .056", MATERIAL REMOVED IS .008" MATERIAL REMAINING IS .022Nov 10, 2007 · N464FE · Boeing 727225 · Fuselage Main, BulkheadSDR 07FDEA04765Frame · corrodedBODY FAIRING FRAME HAS CORROSION LOCATED FORWARD END OF PANEL 3455R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIGINAL .050'. REMOVED .025", REMAINING .025", IAW SRM 53-10-1. TOOL AAR23841 CAL DATE .Nov 10, 2007 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 07FDEA04764Skin · gougedFUSELAGE SKIN JUST FWD OF LANDING LIGHT IS GOUGED REMOVED INBD LT LEADING EDGE REF SRM 51-30-2 MANUFACTURED REPAIR DOUBLER AND FILLER REF SRM 53-30-3. TREATED AND PRIMED REPAIR DOUBLER AND FILLER, REF SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER REF SRM Nov 10, 2007 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA04763Frame · corrodedUPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT AREA REMOVED CORROSION AT UPPER FUSELAGE STA 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048" MATERIAL LOSS .016". FOUND TO Nov 10, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04762Skin · corrodedAFT PIT BILGE SKIN CORRODED OB SIDE OF STR 28L, STA 1045-1048, LBL 16-17. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND FR PRIMED. INSTALLED EXTERNAL REPAIR REF SRM 53-30-3 FIGNov 10, 2007 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742033Seat Track · damagedSEAT TRACK LBL 48 STATION 1110 DAMAGED. REMOVED SEAT TRACK FROM STATION 1110 TO 1148 LBL 48 IAW B-727 SRM 51-30-2. FABRICATED SEAT TRACK FROM P/N BAC 1570-792 7075-T6 PO NR 9005692 APPROXIMATE DIMENSION 46" IAW B-727 SRM 53-10-2 FIGURE 7 AND 53-10-5 FIGURE 1Nov 9, 2007 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04758Stringer · crackedAFT PIT STR 27R, END FITTING IS CRACKED AT BS 1056, REMOVED END FITTING, P/N 65-56185-1. INSTALLED PN 65-56185-2, IAW SRM 51-30-1 AND DWG 65-56185.Nov 9, 2007 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 07FDEA04737Battery Box · crackedE/E COMPARTMENT CRADLE (TRAY ASSY) IS CRACKED AT FWD RT CORNER REMOVED AND REPLACED BATTERY TRAY ASSY REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 7, 2007 · N464FE · Boeing 727225 · Battery Box StructureSDR 07FDEA04744Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLG IS FRETTED/CORRODED AT FASTENER HOLE BS 312, LBL 4, WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS, IAW SRM 51-10-6, 53-10-1 53-10-2 FIG 7 SHT 1, ITEM 18, ORIGINAL MAT. .080" REMOVED .026" REMAINING .064" TOOL AAR IN17-0213 CAL DNov 7, 2007 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA04743Angle · crackedLT OTBD AILERON BAY BAFFLE SEAL IS CRACKED AT INBD ANGLE (MKD) TO FASTENER HOLE REMOVED AND REPLACED AILERON BAY BAFFLE ANGLE REF DWG 65-19289 AND SRM 51-30-2. APPLIED PN FX 65-19289-17 REF FED EX GMM 7-0-1001.Nov 7, 2007 · N464FE · Boeing 727225 · Wing Miscellaneous StructureSDR 07FDEA04742Keelbeam · corrodedLOWER FUSELAGE STATION 742, RBL 1 TO RBL 4, KEEL BEAM LOWER WEB CORRODED, REMOVED CORROSION IN REF TO SRM 51-10-1 PG 1, ORIG MAT'L .080, MAT'L REMAINING .045', OUT OF LIMITS. REMOVED DAMAGE AREA OF KEEL BEAM WEB 51-10-2 PG 10. FABRICATED DOUBLER AND FILLER Nov 7, 2007 · N464FE · Boeing 727225 · Fuselage Main, KeelSDR 07FDEA04740Floorbeam · corrodedMAIN CARGO COMP STA 480 RBL 10" FLOORBEAM LOWER SURFACE CORRODED REMOVED CORROSION IAW SRM 53-10-1 PG1, ORIGINAL .135", REMOVED .035' REMAINING .096". FOUND TO BE OUT OF LIMITS AAR TOOL NR 280087 CAL DATE 4-27-08. REPAIRED IAW SRM 53-10-8 FIG 8. TREATED ANNov 7, 2007 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA04739Seat Track · corrodedAFT CABIN CENTER SEAT TRACK RIGHT FLANGE UPPER SURFACE CORRODED BETWEEN BS 1100-1110 REMOVED CORROSION VERIFIED REMOVAL TO BE OUT OF LIMITS ORIG THICKNESS .0947 REMAINING .0536 REMOVED .0411. FABRICATED SEAT TRACK AND REPAIR STRAP AND ANGLES. INSTALLED REPAINov 7, 2007 · N464FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04738Floorbeam · crackedMAIN DECK FLOORBEAM UPPER FLANGE IS CRACKED AT FLOOR PANEL FASTENER HOLE, BS 328 FWD, LBL 19, WL 208. CUT OUT DAMAGE AT BS 328, LBL 18.25 TO LBL 21. FABRICATED AND DRILLED REPAIR PARTS. TREATED AND PRIMED AND TOP COATED REPAIR PARTS. INSTALLED REPAIR TOP Nov 7, 2007 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA04736Frame · corrodedUPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT REMOVED CORROSION AT UPPER FUSELAGE STA 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048", MATERIAL LOSS .016'. FOUND TO BE OUTNov 7, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04734Angle · corrodedMAIN DECK FLOOR SUPPORT IS CORRODED, BS 328-344, LBL 29, WL 208. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS ORIGINAL .080'. REMOVED .025" (DEEPEST POINT ) REMAINING .055', IAW SRM 53-10-01, TOOL AAR IND -0213, CAL DUE 10-15-08. REMOVED FLONov 7, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2007748034Window Frame · corrodedLT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG IAW MM 53-20-00 AND DRAWING NR AE727-1-105. CLEANED WINDOW PLUG PANE FOR EVALUATION NO CORROSION NOTED IAW S0PM 20-30-3. REMOVED CORROSION ON WINDOW FRAME. CORROSION FONov 2, 2007 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2007748033Window Frame · corrodedRIGHT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG AT BS 950F TO 970 RIGHT IAW M/M 53-20-00 FIGURE 1 AND AEI DRAWING NR AE727-1-105 REV B. REMOVED CORROSION FROM WINDOW FRAME, FOUND OUT OF LIMITS IAW SRM 51-10-6, 56-2Nov 2, 2007 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2007743AAngle · crackedFOUND RIGHT WING SPAR ANGLE FITTING AT THE INBOARD SIDE OF NR 5 L/E SLAT ACTUATOR TRUNNION CRACKED AT FORWARD END.Nov 1, 2007 · N743DH · Boeing 727225 · Leading Edge DevicesSDR DHL2007743Mount · crackedRIGHT WING AT NR 7 SLAT ACTUATOR INBD TRUNNION MOUNT HAS DOUBLER THAT APPEARS TO BE CRACKED.Oct 30, 2007 · N743DH · Boeing 727225 · Leading Edge DevicesSDR DHL2007748025Stringer · crackedLEFT WHEEL WELL STRINGER 18A CRACKED AT BS 940. CUT OUT DAMAGED SECTION OF STRINGER 18A LEFT AFT OF STATION 940 NDT AREA IAW B-727 NDTM PT 6 51-00-00 FIGURE 23. NO CRACK BEYOND CUT OUT. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING SVC REQUEST AND REPAIROct 25, 2007 · N748DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007748032Skin · crackedLEFT INBOARD MID FLAP UPPER SURFACE WBL124 AT MID SPAR SKIN IS CRACKED AT LOCK FASTENER. REMOVED FASTENERS ON LEFT INBOARD MID FLAP UPPER SURFACE COMMON TO MID FLAP SPAR STA 124.2 IAW SRM 51-30-2. C/W HFEC IAW NDT PT 6 51-00-00 FIGURE 23, ALUMINUM PART SURFAOct 24, 2007 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2007748001Bulkhead · crackedRIGHT WW BS 870 BELOW LEAD CONTROL VALVE, BULKHEAD HAS 2 INCH CRACK. CUT OUT DAMAGED AREA BELOW APU LEAD CONTROL, CUT OUT 2" BY .75". FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-9 FIGURE 5. HEAT TREATED TO 150-190 KSI PER SPEC PO NR 7307279. ALOct 22, 2007 · N748DH · Boeing 727225 · Fuselage Main, BulkheadSDR DHL2007748028Frame · dentedREWORK DUE TO IMPROPER REPAIR FRAME AT 9G BARRIER BS 348.2 IS DENTED BETWEEN STRINGER 5L AND STRINGER 6L. REMOVED SRM REPAIR AT FRAME STATION 348 STRINGER 5L - 6L IAW SRM 51-30-2. CUT OUT FRAME SECTION IAW DRAWING NR AE727-2-360. FABRICATED AND INSTALLED DOOct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007748024Keelbeam · crackedRAM KEEL BEAM LOWER CHORD CRACKED BS 870. TRIMMED CRACKED AREA OF KEEL BEAM. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SB 727-53-0208 REV 1 MATERIAL USED 0.071" 15-5PH STEEL. HEAT TREATED TO 170-190 KSI PER BRADDOCK METAL SPECS PO NR 7307279 8.75" BY 4" COct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, KeelSDR DHL2007748016Frame · damagedFORWARD CARGO COMPARTMENT FRAME 640 AREA SHOW SEVERAL FASTENER HOLES IMPROPERLY PERFORMED. BLENDED DAMAGED AREA OF STUB FRAME AT STATION 638 BETWEEN 23L AND 25L. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SIE EO NR SIE-N748DH-10-16-07 MATERIAL USED 0.100"Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007748002Angle · crackedRIGHT WHEEL WELL STATION 870 RBL 8, VERTICAL ANGLE IS CRACKED. REMOVED AND REPLACED VERTICAL ANGLE IN RIGHT WHEEL WELL STATION 870 RBL 8 IAW B-727 SRM 51-30-5 AND 51-30-2.Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2007748031Skin · cracked2 EACH DENTS HAVE INDICATION OF CRACK HFEC INSPECTION. REMOVED PREVIOUS REPAIR AT FUSELAGE SKIN RIGHT 1342 STRINGER 19R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MATERIAL USED 2024-T3 0.063" PO NR 9005773 DIMENSION 11.5" BY 5.5" IAW B-727 SRM 54-30-3 Oct 16, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007748026Skin · corrodedPOSSIBLE CORROSION ON SHEAR TIE BS 700 INBOARD OF STRINGER 27R. FABRICATED SKIN DOUBLER REPAIR IAW B-727 SRM 53-30-3 FIGURE 3 AND 53-30-2, AND 2 FRAME SHEAR TIE REPAIR DOUBLERS IAW B-727 SRM 53-10-4 FIGURE 13 AND 14 AT BS 700 STRINGER 27R. MATERIAL USED SKINOct 16, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007748030Shear Tie · crackedFORWARD PIT FORWARD SIDE OF FRAME BOTTOM FLANGE AT BS 720 HAS CRACK OUTBOARD OF STRINGER 28R. CUT OUT DAMAGED SECTION AT SHEAR TIE (FRAME) IN FORWARD PIT BS 720 OUTBOARD OF STRINGER 28R IAW B-727 SRM 53-10-4 FIGURE 13 5" BY 2". FABRICATED AND INSTALLED SHEAROct 15, 2007 · N748DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2007748017Frame · dentedFRAME DENTED AT BS 990 JUST ABOVE STRINGER 27L. CUT DAMAGE AREA AT BS 990 ABOVE STRINGER 27L DIMENSION 1" BY .75" IAW B-727 SRM 51-40-3 FIGURE 1. FABRICATED FRAME REPAIR FROM 7075-O PO NR 9004690 DIMENSION 9" BY 4" IAW B-727 SRM 51-40-3 FIGURE 1. HEAT TREATOct 11, 2007 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007748020Seat Track · corrodedCABIN AREA SEAT TRACK CORRODED AT LBL 25 BS 520 TO 690. REMOVED SEAT TRACK SECTION FROM STATION 480 TO 690 LBL 25 IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIGURE 1 AND 53-10-2 FIGURE 7, SPLICE ANGLE REPAIR INSTALLED ATOct 9, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748029Seat Track · corrodedMAIN CARGO CABIN SEAT TRACK CORRODED AT BS 344 TO 480 RBL 24. REMOVED SEAT TRACK SECTION ON MAIN CARGO CABIN BS 344 TO BS 480 RBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK LOCATED AND DRILLED. MATERIAL USED BAC 1520-792-7178-T6511 PO NR 9005692 DIMENSIOOct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748027Skin · cracked2 EACH DENTS HAVE INDICATION OF CRACKS FROM HFEC INSPECTION. CUT OUT DAMAGED AREA AT RT FUSELAGE SKIN STRINGER 19R BETWEEN BS 1342.4 TO BS 1354.30 IAW SRM 54-30-3 FIGURE 7. FABRICATED DOUBLER REPAIR IAW SRM 54-30-2 FIGURE 4 AND 51-30-2. TREATED AND PRIMED POct 8, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007748022Seat Track · corrodedCABIN AREA SEAT TRACK CORRODED AT LBL 45 BS 344 TO 480. REMOVED DAMAGED SECTION OF SEAT TRACK IAW B-727 SRM 51-30-2 FROM STATION 344 TO 480 LBL 45. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW VENTURA AEROSPACE DRAWING NR 2902 MATERIAL USED BAC 1520-7Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748019Seat Track · corrodedCABIN AREA SEAT TRACK CORRODED AT BS 500 TO 690 RBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, FABRICATED TWO ANGLES AND FABRICATED STRAP IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED SEAT TRACK PARTS AND AREA IAW SRM 51Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04524Carriage · damagedSPLIT FLAPS OUTBOARD ON DEPARTURE. COMPLIED WITH QRH FLAPS WOULD NOT RETRACT VIA ALTERNATE METHOD. CREW DEBRIEFED OUTBD FLAPS STAYED AT 5 DEG WHILE INBD FLAPS CAME TO 2 DEG AS COMMAMDED. L/E VALVE C/B ON P6 PANEL PULLED BY CREW AS PART OF QRH. REF WRI 27-Oct 6, 2007 · N462FE · Boeing 727225 · Trailing Edge FlapsSDR DHL2007748023Seat Track · corrodedCABIN SEAT TRACK CORRODED AT BS 480 TO 680 LBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED 2 NEW SEAT TRACKS, 2 ANGLES AND 1 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS AND SEAT TRACK IAW SROct 5, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748014Seat Track · corrodedSEAT TRACK AT STATION 950F-1030 RBL 45 HAS CORROSION. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK, 2 ANGLES AND 2 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-1Oct 5, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748021Seat Track · corrodedCABIN AREA SEAT TRACK CORRODED AT BS 344-480 LBL 24. REMOVED DAMAGED SEAT TRACK SECTION BS 344-480 LBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM IAW DRAWING NR 2902. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.Oct 4, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748018Seat Track · corrodedCABIN SEAT TRACK CORRODED RBL 24 BS 590 TO 689.5. REMOVED SEAT TRACK IAW SRM 53-10-5 FIGURE 1. FABRICATED NEW SEAT TRACK SECTION. FABRICATED 4 ANGLES AND FABRICATED ONE STRAP IAW SRM 53-10-5 FIGURE 1. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2. SEATOct 3, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748015Seat Track · corrodedMAIN CABIN STATION 870 TO 930 LBL45 SEAT TRACK FLANGE HAS CORROSION. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 870 TO 930 LBL45 IAW B-727 SRM 51-30-2. FABRICATED NEW SECTION SEAT TRACK MATERIAL USED BAC 1520-792-7178-T6 DIMENSION 91" IAW B-727 SRM 53-Oct 3, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007748012Stringer · crackedMAIN CABIN STRINGER 15 CRACKED AT BS 720B. CUT OUT DAMAGE AREA DIMENSION CUT OUT IAW SRM 53-10-3 FIGURE 5. FABRICATED REPAIR CHANNEL, FILLER, & TAPERED FILLER IAW SRM 53-10-3 FIGURE 5 AND 51-30-5. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIROct 3, 2007 · N748DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
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