Boeing 727-227

Service difficulty reports · 5,082

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727227'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA02410Frame · crackedFRAME CRACKED AT LOCK FASTENER, STA 800 STRINGER 14R. REMOVED DAMAGED PORTION OF FRAME ANGLE, FABRICATED REPAIR ANGLE AND FRAME FILLER. HEAT TREATED, ALODINED AND PRIMED AND INSTALLED. REF SRM 51-40-2 FIG 1, 51-30-2 PG 2, THIS IS CLASSIFIED AS A MAJOR REPAIJun 24, 2008 · N487FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA02404Frame · chafedORIGINAL DISCREPANCY STILL EXISTS. AFT PIT LT SIDE WALL BODY FRAME IB FLANGE CHAFED, 1148, STR 21L - L CHECKED WEAR AREA FOR MATERIAL LOSS, ORIGINAL THICKNESS "T' .065' MATERIAL LOSS MEASURE .017', REMAINING MATERIAL .048' AND IS OUT OF LIMITS REF SRM 53-1Jun 24, 2008 · N487FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA02403Stringer · damagedSTATION 344 STR 11R STRINGER TIE MIS-DRILLED AND HAS A FASTENER WITH ZERO EDGE DISTANCE. INSTALLED FRAME REPAIR, FILLER AND STRINGER CLIP IAW SRM 51-30-2, 53-10-4 FIG 1, 53-10-2 FIG 3 AND 51-20-1.Jun 24, 2008 · N494FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02400Bracket · chafedSTATION 305 BETWEEN STR'S 3R AND 4R WHERE COCKPIT BULKHEAD ATTACHES TO INTERCOSTAL, BRACKET CHAFFING THROUGH INTERCOSTAL. REMOVED INTERCOASTAL WEB IAW SRM 51-30-2. FABRICATED WEB IAW B727 SRM 51-10-3, 51-30-5, AND 53-10-2. TREATED AND PRIMED IAW SRM 51-10-Jun 24, 2008 · N494FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 08FDEA02396Nut · missingMISSING NUT ON BOLT SECURING NR 3 ENGINE THROTTLE CONTROL ROD INBD OF ENGINE. REMOVED AND REPLACED NUT, BOLT AND LOCK IAW FX B727 76-12-000-5.Jun 24, 2008 · N494FE · Boeing 727227 · Power LeverSDR DHLA200800076Battery Pack · inoperativeEMERGENCY EXIT LIGHT FOR MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES PRE MM 33-50-71, OPS CHECK GOOD P/N MISC062. FLIGHT NUMBER 2808. AIRCRAFT WAS GROUNDED.Jun 23, 2008 · N783DH · Boeing 727227 · Emergency LightingSDR 08FDEA02376Aoa · damagedSTALL WARNING ACTIVATED AT ROTATION. AIRCRAFT FLYING NORMALLY. STAYED ON UNTIL CIRCUIT BREAKER PULLED. AMBER WINDSHEAR LIGHT CAME ON. REMOVED AND REPLACED AOA VANE AND SYSTEM OPS CKS NORMAL IAW 727 M/M 34-18-051-4 AND REINSTALLED S/OS HAND MIKE AND BOOM MJun 22, 2008 · N240FE · Boeing 727227 · Stall Warning SystemSDR 08FDEA02374Keelbeam · crackedLEFT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872.Jun 21, 2008 · N494FE · Boeing 727227 · Fuselage Main, KeelSDR 08FDEA02373Keelbeam · crackedLT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER IAW SB727-53-0208 AND EA 7-5310-116992.Jun 21, 2008 · N494FE · Boeing 727227 · Fuselage Main, KeelSDR 08FDEA02372Web · crackedCRACK ON LEFT WING TRAILING EDGE WEB JUST OUTBOARD OF NR 7 SPOILER FITTING. CUT-OUT DAMAGED AREA, FABRICATED NEW DOUBLER, FABRICATED WEB, & INSTALLED REPAIR PARTS IAW SRM 51-30-2, AND DRAWING SR27-57-038.Jun 21, 2008 · N494FE · Boeing 727227 · Wing Miscellaneous StructureSDR 08FDEA02371Skin · dentedEXTERIOR FUSELAGE STA 300 JUST FWD OF L1 DOOR HAS A BULGE IN SKIN STR 9L. 9L REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40-1. HFEC INSPECTED DENT IAW NDTM 51-00-00 FIG 23 PART 6. NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW SRM 51-10-2.Jun 21, 2008 · N494FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA02370Doubler · failedFUSELAGE SKIN DOUBLER IN FRONT OF L1/R1 WINDSHIELDS TORN AWAY AT L/E, BODY STA 178 AT TOP OF NOSE RADOME. REMOVED AND REPLACED TORN SKIN DOUBLER AT BS 178 IN FRONT OF L1 AND R1 WINDOWS. NEW SKIN PART NUMBER 65-45800Y218 PO 819342 IAW SRM 51-30-5 AND SRM 51-3Jun 21, 2008 · N494FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA02294Stiffener · corrodedRT MLG STRUT WELL LWR FIXED PNL SEAL RETAINER ASSY IS CRACKED/CORRODED ALONG WING SPAR CHORD WS 190-220 REMOVED 4 HYD STANDOFFS AND 2 SEAL DEPRESSORS FROM STA 180-220. REMOVED DRAIN TUBE, TE FAIRING PANEL, TE FIXED PANEL RT. FABRICATED 2 NEW SEAL RETAINERS OJun 17, 2008 · N487FE · Boeing 727227 · Wing Miscellaneous StructureSDR 08FDEA02292Stiffener · corrodedSEAL RETAINER STIFFENER RT WING AFT LWR SPAR WS 181-220 IS CORRODED REMOVED CORROSION FROM STIFFENER AT STA 181-220 RT WING ORIGINAL MATERIAL .040 MATERIAL LOSS .010 REMAINING MATERIAL .030 OUT OF LIMITS. REMOVED STIFFENER AND FABRICATED NEW STIFFENER MATERIAJun 17, 2008 · N487FE · Boeing 727227 · Wing Miscellaneous StructureSDR 08FDEA02291Skin · corrodedAFT PIT BILGE SKIN HAS CORROSION AT STATION 1008 OB OF STRINGER 28L REMOVED CORROSION REF SRM 51-10-1 ORIG T .082 REMAINING .047, .035 LOSS USING TOOL IN22-0028, OUT OF LIMITS. REF SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER REF EA 7-5330-113 990. INSTALLJun 17, 2008 · N487FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA02281Stringer · corrodedFWD CARGO COMPARTMENT, STRINGER 27R CORRODED BETWEEN STA 720A AND 720C REMOVED BODY FAIRINGS NR 3420 AND 3437 IAW SRM 51-30-2, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. CUT OUT DAMAGE AREA (DIM 47 INCHES LONG ) AND FABRICATED NEW STRINGER FROM BAC1498-145 AND Jun 16, 2008 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02220Shear Tie · corrodedAFT CARGO COMPARTMENT, SHEAR TIE CORRODED AND FASTENERS PULLING THROUGH AT BS 116 BETWEEN STRINGER 30 AND 29R AFT SIDE.Jun 11, 2008 · N490FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA02219Stringer · corrodedSTR-2R HAS CORROSION, BS: 620-624 REMOVED CORROSION REF SRM 51-10-6 P 12-14, VERIFIED MATERIAL LOSS WITHIN LIMITS REF SRM 53-10-1. ORIGINAL "T" .036", MATERIAL REMOVED .002" REMAINING "T" = .034. TREATED AND PRIMED REF SRM 51-10-2 P. 1-2. THIS IS CLASSIFIEDJun 11, 2008 · N487FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02218Floor Support · corrodedMAIN DECK BS 1140-1146 RBL 11-12 WL 208 FLOOR SUPPORT "T" HAS CORROSION ON UPPER AND LOWER SURFACES OF I/B FLANGE. REMOVED CORROSION, ORIGINAL "T" .080, REMOVED .025, REMAINING .055 - OUT OF LIMITS REF SRM 51-10-1. REMOVED OLD SUPPORT BEAM, FABRICATED, HEAT Jun 11, 2008 · N487FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA02216Shear Tie · corrodedDOT 114-010 AFT PIT BILGE SHEAR TIE IS CORRODED AT STATION 990 FRAME, STRINGER 29 RIGHT TO STR 30. MANUFACTURED AND INSTALLED NEW SHEAR TIE AT STA 990 STR 29 TO 30. FOUND OLD SHEAR TIE OUT OF LIMITS. ORIGINAL T .063 AFTER REMOVAL .051 REF SRM 53-10-1. INSTJun 11, 2008 · N487FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA02215Frame · gougedAFT CARGO PIT FUSELAGE FRAME 1130 HAS GOUGES AND CORROSION ON UPPER FLANGE, RBL: 22-23, UNDER Z ANGLE. REMOVED CORROSION AND GOUGES, ORG MATERIAL THICKNESS .071" REMOVED .030", REMAINING .041". FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PART, TREATED AND PJun 11, 2008 · N487FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA02210Stringer · corrodedFWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 520 AND FS 540 REMOVED CORROSION ON STRINGER L28 FWD LOWER CARGO PIT FS 520-540. FOUND CORROSION AREA TO BE OUT OF LIMITS WITH A .020 MATERIAL LOSS FROM ORIGINAL "T" = .063. REMOVED DAMAGE SECTION OJun 10, 2008 · N487FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02209Stringer · corrodedFWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 540 AND FS 560 CORROSION FOUND ON LOWER CARGO PIT STRINGER L28 BETWEEN FS 540 AND 560 WAS OUT OF LIMITS (EXFOLIATION). REMOVED DAMAGED SECTION OF STRINGER FROM 551-575 FS. FABRICATED, TREATED PRIMED PJun 10, 2008 · N487FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHLA200800054Engine · malfunctionedALL NR 2 ENGINE INSTRUMENTS FLUCTUATING. EPR BETWEEN 2.0 & 2.1 ON TAKEOFF. N2 FLUCT .2, N1 FLUCT .3, PERFORMED ABNORMAL PROC, SHUTDOWN ENGINE INFLIGHT. POSITIVE OIL PRESSURE ENTIRE TIME. INSPECTED NR 2 ENG INLET & EXHAUST IAW P&W MM 72-00-00, INSPECTED NR Jun 9, 2008 · N782DH · Boeing 727227 · Engine (Turbine/Turboprop)SDR 08FDEA02208Skin · delaminatedLT OB FORE FLAP WBL 478 ON T/E IS DELAMINATED CUT OUT DELAMINATED AREA 4 1/2 BY 9 INCH ON LT O/B FOREFLAP WBL 478. FABRICATED FILLER 4 1/2 BY 9 INCH AND DOUBLER 6 INCH BY 12 INCH FROM 0.016" 2024-T3 PO NR 9004174 IAW B727 SRM 57-50-2. BONDED FILLER AND DOUBLJun 9, 2008 · N490FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA02200Stringer · corrodedINTERNAL FUSELAGE FWD CARGO COMPARTMENT, STRINGER 28R CORRODED AT BS 500. REMOVED INTERCOSTAL AT BS 480-500 STR 28 RT IAW B-727 51-30-2, CUT-OUT DAMAGE STRINGER, (DIM 23 1/2 INCH LONG). FABRICATED STRINGER FILLERS FROM BAC1498-205 PO NR 642842 (DIM 13 INCH LJun 8, 2008 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02198Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 660 STRINGER S-2R REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-02 PG-2-8. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW, GMM 6-2-100 PG 2 AND 3.Jun 8, 2008 · N487FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 08FDEA02197Stringer · corrodedSTR-3R HAS CORROSION, BS 576-584 REMOVED CORROSION REF SRM 53-10-1. AREA FOUND TO BE OUT OF LIMITS. REMOVED STRINGER SECTION REF SRM 51-30-02 P 6-7. FABRICATED NEW SECTION REF SRM 53-10-2 FIG 9. INSTALLED NEW SECTION REF SRM 51-30-02. THIS IS CLASSIFIED AJun 8, 2008 · N487FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02195Threshold · crackedRIGHT AFT SERVICE DOOR THRESHOLD CRACKED NEAR STOP PAD. SENT TO SHOP FOR WELD ON NR N00707, THRESHOLD WILL GET INSTALLED ON CLOSE CARD 72C201-01. THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 7, 2008 · N487FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA02194Threshold · crackedR2 DOOR OPENING, THRESHOLD CRACKED 2 PLACES SENT TO SHOP FOR WELD REPAIR ON NR N00707. THRESHOLD WILL BE INSTALLED ON CLOSE CARD 72C201-01 THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 7, 2008 · N487FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA02193Stringer Clip · corrodedCORROSION ON STRINGER CLIPS, BS 520 STRINGER, S-4R AND S-3R REMOVED STR 3R CLIP AT STA 520 AND REMOVED CORROSION ORIG THICKNESS .032' LOSS .005 REMAINING .027. FOUND OUT OF LIMITS. REMOVED STR 4R AND REMOVED CORROSION FOUND TO BE CRACKED. INSTALLED 2 NEWJun 7, 2008 · N487FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 08FDEA02191Stringer · corrodedCORROSION ON INSIDE OF STRINGER S-3R AT STA 520 REMOVED .008' CORROSION FROM ORIGINAL STRINGER. THICKNESS OF .036'. REMAINING THICKNESS IS .028" AND STRINGER WHERE DAMAGE IS OUT OF LIMITS. REMOVED DAMAGE SECTION OF STRINGER, FABRICATED REPAIR PARTS, TREATEDJun 7, 2008 · N487FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02184Frame · crackedLT WHEEL WELL STA 913.5 FRAME IS CRACKED OUT OF UPPER FILLER, END. CRACK IS WITHIN THE SHADED AREA OF JOB CARD FIGURE 1A REPAIRED LT WHEEL WELL FRAME AT STA 913.5, PER EO 7-5310-7-4329 PART 3, THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 6, 2008 · N487FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA02176Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 660, STRINGER, S-1R INSTALLED 1 EA CLIP, NEW CLIP AT STR 1, F/S 660 PER REF SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jun 6, 2008 · N487FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 08FDEA02161Skin · corrodedFWD PIT FUSELAGE SKIN HAS CORROSION, BS 566 - 572, STR 28L REMOVED CORROSION FROM FWD PIT FUSELAGE SKIN, BS 566 - 572 STR 28L. NDT FOR MATERIAL REMOVAL. FOUND TO BE OUT OF LIMITS. .035 INCH REMOVED AT DEEPEST POINT. ORIGINAL .100 INCH REMOVED DAMAGE/PREVIOJun 5, 2008 · N487FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA02160Stringer · corrodedFWD CARGO COMPARTMENT HAS STRINGER 27 RT CORRODED BETWEEN STA 720E AND 720F CUT OUT DAMAGED AREA (DIM 17" LONG) AND FABRICATED NEW FILLER FROM BAC 1498-147, 0.090 PO NR 8150104 (DIMENSION 17 INCH LONG) AND SPLICE FROM BAC-1498-131 7075-T6 PO NR 9006222 (DIMENJun 5, 2008 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02156Web · crackedAIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, LT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUT OUT, CRACKED. DOT ON AFT SIDE OF WEB AND ACCESS THROUGH VERT STAB PANEL 9504 REMOVED DAMAGE, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PJun 4, 2008 · N487FE · Boeing 727227 · Vertical Stabilizer Miscellaneous StructureSDR 08FDEA02153Web · crackedAIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, RT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUTOUT, CRACKED. DOTS ARE ON AFT SIDE ACCESING THROUGH VERT STAB PANEL. REMOVED DAMAGED, FABRICATED, TREATED, PRIMED, AND INSTALLED. REPAIR REFJun 4, 2008 · N487FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA20080016Compressor · stalledFLT 0001 FROM MIA-PTY. DURING APPROACH TO PTY THE NR 3 ENG COMPRESSOR STALLED AND ENG FLAMED OUT. THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 UNMOVEABLE. REMOVED AND REPLACED THE NR 3 ENGINE. OPS AND LEAK CHECKS GOOD. NO OTHER DJun 3, 2008 · N89427 · Boeing 727227 · Turbine Engine Compressor SectionSDR C8G2008F00000Engine · lockedDURING APPROACH, THE NR 3 ENGINE COMPRESSOR STALLED AND ENGINE FLAMED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 WAS UN-MOVEABLE. REMOVED AND REPLACED NR 3 ENGINE, OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. AJun 3, 2008 · N89427 · Boeing 727227 · Engine (Turbine/Turboprop)SDR 08FDEA02137Unknown · smokeON SHORT FINAL AT EWR ALL 3 CREW MEMBERS COULD SEE AND SMELL SMOKE IN COCKPIT. ONLY LEFT PACK WAS ON AT THE TIME, WITH NR 1 AND NR 3 BLEEDS OPEN. RAN LT PACK WITH APU BLEED, NO SMELL OR SMOKE PRESENT. RAN NR 1 WITH LT PACK, NO SMELL. INSPECTED LEFT ACM FORJun 3, 2008 · N492FE · Boeing 727227 · Air Distribution SystemSDR 08FDEA02138Support Angle · crackedFWD LOWER CARGO DOOR, FWD FRAME HAS CRACK IN SUPPORT ANGLE AT 3RD STOP FITTING UP FROM BOTTOM REMOVED DAMAGE PARTS. FABRICATED NEW TEE CLIP AND GUSSET. INSTALLED NEW PARTS. REF SRM 51-30-02, 51-30-05 P 1-34 DWG NR 65-69145. TREATED AND PRIMED (GUSSET AND TJun 3, 2008 · N487FE · Boeing 727227 · Cargo/Baggage DoorsSDR 08FDEA02136Skin · delaminatedLT WING O/B FLAP I/B END BY END FITTING IS DELAMED (TOP SKIN ) OF FORE FLAP REPAIRED LT WING OUTBOARD FORE FLAP REF SRM 51-40-20 PAR'S 7,14,15,18,20,21 PGS 12-62 SRM 57-50-02 FIG 4 PG 7, AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 3, 2008 · N487FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA02135Panel · delaminatedLEFT WING L/E PANEL 6220, CORNER SKIN DISBONDED REPAIRED PANEL 6620 REF SRM 51-20-9 PAR 3D AND 7 PG 3-11 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG1, THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 3, 2008 · N487FE · Boeing 727227 · Wing, Plate/SkinSDR 08FDEA02060Beam · crackedRT WING UPPER TRAILING EDGE "J " BEAM IS CRACKED AT WBL 118, WS 155 - WS 160 REMOVED NR 8 SPOILER FITTING FOR ACCESS IAW B727 SRM 51-30-2. TRIMMED OUT CRACK (DIMENSION 0.280 INCH IN LENGTH ) IAW B727 SRM 51-10-1 AND FEDEX DRAWING SR 27-57-025 REV A. TREATED May 30, 2008 · N490FE · Boeing 727227 · Wing Main, Frame StructureSDR 08FDEA02055Stringer · corrodedFWD CARGO COMPARTMENT, STR 28L HAS BULGING SEAL ON O/B SIDE JUST FWD OF STA 740 EVIDENCE OF CORROSION REMOVED SEALANT AND CLEANED AREA. NO CORROSION NOTED IAW BSOPM 20-30-03. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. RESEALED AREA IAW FX 727-200 51-31-0May 30, 2008 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02054Stringer · corrodedFWD CARGO COMPARTMENT, STR 27R IS CORRODED FWD OF STA 740 REMOVED FASTENERS IAW B-727 SRM 51-30-2, CUT-OUT DAMAGED AREA (DIM 9 1/4 INCH LONG) AND FABRICATED FILLER FROM BAC1498-147 0.090" PO NR 8150104 ( DIM 9 1/4" LONG ) AND STRINGER SPLICE FROM BAC1498-131 7May 30, 2008 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA02053Skin · dentedLOWER FUSELAGE, SEVERAL DENTS WITH BULGING SKIN BETWEEN STA 1050 AND 1070, BETWEEN STR 28R AND 26R LOWER FUSELAGE SEVERAL DENTS WITH BULGING BTW STA 1015 TO 1070 STR 28R - 26R; CUT OUT 2 EA DAMAGE AREA DIM (12 INCH BY 6 1/2 INCH), (2 1/2 BY 1 1/2) IAW SRM 53-3May 30, 2008 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA02052Skin · crackedNR 4 SLAT UPPER SURFACE ON AFT HOOK ATTACHMENT SCREW HAS SKIN CRACKED REMOVED HOOK AS REQ IAW B727 SRM 51-10-2. FAB REPAIR PLATE MAT USED 2024T3-.125 PO NR 810563. DIM (5" BY 4") IAW B727 SRM 57-50-3 FIG 10, TREATED AND PRIMED IAW B727 SRM 51-10-2, C/W HFEC May 30, 2008 · N490FE · Boeing 727227 · Leading Edge DevicesSDR 08FDEA02023Skin · dentedRT FUSELGE EXTERNAL 2 EA OLD REPAIRS AT STA 416 BETWEEN STR 21R AND STR 22R HAVE DENTS.May 29, 2008 · N490FE · Boeing 727227 · Fuselage Main, Plate/Skin
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