Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR G8GA20080006Actuator · malfunctionedFLT 715 FROM HRL TO MEM. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 2 LEADING EDGE SLAT WOULD NOT RETRACT. CREW PERFORM REQUIRED PROCEDURES AND RETURNED TO HRL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 SLAT ACTUATOR WAS REMOVED AND REPLACED, OPS AND LFeb 15, 2008 · N308AS · Boeing 727227 · Leading Edge Slat ActuatorSDR 08FDEA00442Floor Support · corrodedAFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 16 HAS CORROSION ON UNDERSIDE REPLACED FLOOR SUPPORT ANGLE AT BS 1164 - 1166 LBL 16, SRM 53-10-5 FIG 4 AND SRM 51-30-2.Feb 14, 2008 · N486FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA00439Floor Support · corrodedAFT LWR CARGO BAY BS 1164-1166 FLOOR SUPPORT ANGLE AT RBL 4, HAS CORROSION ON UNDERSIDE. REMOVED CORROSION ON AFT LWR CARGO BAY STA 1164 - 1166 FLOOR SUPPORT ANGLE AT RBL 4, REF SRM 51-10-6, MATERIAL LOSS OF 50 PERCENT, FOUND TO BE OUT OF LIMITS. REF SRM 53Feb 14, 2008 · N486FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA00438Structure · corrodedNOSE W/W AIRCRAFT INTERIOR SURFACE AT BS 301 TO 305 RBL 14", WL 169 TO 171 LONGITUDINAL CHORD ABOVE HORIZONTAL WALKWAY IS CORRODED REMOVED FASTENERS, BLENDED CORROSION, FOUND TO BE WITHIN LIMITS, ORIGINAL MATERIAL .350", MATERIAL REMAINING .330' LOSS IS AT 5Feb 14, 2008 · N486FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA00437Skin · dentedLOWER LEFT SIDE EXTERIOR FUSELAGE SKIN HAS DENT WITH SCRAPE STA 680 3 AND 7" BELOW STR 17L DENT WITHIN 10" OF PRODUCTION SEAM, REPAIR REQUIRED REF SRM 53-30-1 FIG 1. REMOVED DAMAGE IN REF TO SRM 53-30-1 HFEC FOR CRACKS AT CUT OUT . NONE FOUND. VERIFIED MATEFeb 14, 2008 · N486FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA00435Skin · corrodedRT WING OUTBD T/E FLAP, LWR SURFACE OUTBD END, LIGHT SURFACE CORROSION REPAIRED RT OUTBOARD T/E FLAP LOWER SURFACE REF SRM 51-40-20 PAR 7, 8, 14, 15, 18, 20-22 AND APPLIED EXTERIOR PROTECTIVE PAINT FINISH REF MM 51-20-151-7, THIS IS CLASSIFIED AS A MINOR REPFeb 14, 2008 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA00429Fairing · crackedLT WING, I/B FLAP, I/B TRACK AFT FAIRING SKIN CRACKED OUT ON TOP SIDE I/B OF AFT ATTACH BOLT, BOLT MOUNT CUTOUT. REPLACED FAIRING WITH SERVICEABLE UNIT. NR 4 TRACK POSITION. INSTALLATION ACCOMPLISHED ON WORK CARD NR 75C001-01. THIS IS CLASSIFIED AS A MINOR Feb 14, 2008 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA00428Intercostal · crackedNR 1 ENG LOWER COWL FWD END INTERCOSTAL CRACKED AND WORN MANUFACTURED AND INSTALLED NEW INTERCOSTAL FWD END OF NR 1 ENG COWL REF 65-19507 AND SRM 51-30-2.Feb 14, 2008 · N486FE · Boeing 727227 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00427Support · corrodedLOWER AFT CARGO PIT, LT SIDE EDGE SUPPORT FROM FS 950F TO FS 1030 HAS AREAS OF SURFACE CORROSION AS MARKED REMOVED CORROSION. ORIGINAL THICKNESS .056", .017 INCH REMAINING, .036 INCH MAT REMOVED. OUT OF LIMITS. REPAIR DOUBLER FABRICATED, TREATED AND PRIMED Feb 14, 2008 · N468FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 08FDEA00426Skin · delaminatedRT WING OUTBOARD AFT FLAP, LWR SURFACE 1 INCH FROM OUTBOARD END, SKIN DISBONDED. REPAIRED RT OUTBOARD AFT FLAP LOWER SURFACE 1 INCH FROM OUTBOARD END. REF 51-40-20 PAR 7, 8, 14, 15, 18, 20-22. THIS CLASSIFIED AS A MINOR REPAIR.Feb 14, 2008 · N486FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA00425Floor Support · crackedLT EDGE SUPPORT CHANNEL FLOOR IS CRACKED AT CTR HOLE, STA 1030 TO 1070 FABRICATED NEW EDGE SUPPORT P/N 65-57570-1 AND SPLICE P/N 65-57570-3. TREATED AND PRIMED AND INSTALLED NEW EDGE SUPPORT AND SPLICE. REF BOEING DWG 65-57570/SRM 51-10-1 PG 12/SRM 51-10-2 PFeb 14, 2008 · N486FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA20080005Actuator · leakingFLT 707 FROM PHX TO MCI - AFTER LANDING AND DURING TAXI, A NOTICEABLE STIFFENING IN THE NOSE STEERING, FOLLOWED BY THE ILLUMINATION OF THE "A" SYSTEM HYDRAULIC LIGHT AND LOW HYDRAULIC FLUID QUANTITY OCCURRED. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 SLATFeb 8, 2008 · N308AS · Boeing 727227 · Leading Edge Slat ActuatorSDR DHLA200800014Fire Warning · false activationFLT 107, NR 3 ENG FIRE DETECTION AMBER LIGHT ILLUM INTERMITTENTLY ON DESCENT (P6-3). COULDNT DULPLICATE PROBLEM, OPS CHECKS GOOD PER M/M 26-11-00. NO DEFECTES NOTED AT THIS TIME. ACFT GROUNDED.Feb 8, 2008 · N782DH · Boeing 727227 · Fire DetectionSDR 08FDEA00194Duct · separatedDURING CLIMB-OUT WITH CLIMB POWER SET AND PASSING 3500 FT MSL, NR 2 ENG FIRE HANDLE AND BELL ACTIVATED. COMPLIED WITH QRH AND DUMPED 400 LBS OF FUEL. LANDED AT MEM. FOUND NR 2 ENG COWL ANTI-ICE DUCT SEPARATED AFT OF VALVE DUCT DAMAGED. REMOVED AND REPLACED Jan 18, 2008 · N483FE · Boeing 727227 · Air Intake Anti/De-Ice SystemSDR DHL2008782001Angle · crackedUPON INSPECTING THE LEADING EDGE, FOUND WHAT APPEARS TO BE A CRACK ON THE LEFT WING INBOARD MOUNT BRACKET FOR NR 4 LE SLAT ACTUATOR. THE CRACK TRAVELS FROM THE RADIUS TOWARDS THE BOLT AT APPROX WING STATION 393. ANGLE WILL BE REPLACED WITH NEW PART.Jan 9, 2008 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2008782002Firewall · crackedUPON INSPECTING THE NR 2 ENGINE FIREWALL, FOUND AN APPROX 2 1/4 INCH CRACK IN AFT WEB AT 8 O'CLOCK POSITION APPROX 6" FROM FLEX ADAPTER. REPAIR WILL BE MADE IAW SRM 54-10-01, 54-10-03 FIG 1 AND M/M 51-30-0.Jan 9, 2008 · N782DH · Boeing 727227 · Nacelle/Pylon, Bulkhead/FirewallSDR 08FDEA00005Control Valve · failedARM LIGHT AND CARGO DOOR IN TRANSIT LIGHT ILLUMINATED IN FLIGHT. PRESSURIZATION REMAINED NORMAL. REPLACED HYDRAULIC SOLENOID SHUTOFF VALVE PER MM 52-34-129-4. REPLACED HYDRAULIC CONTROL VALVE PER MM 52-34-101-4. OPS OK PER MM 52-34-009-5.Jan 2, 2008 · N483FE · Boeing 727227 · Hydraulic System, MainSDR DHL2007782003Skin · crackedA/C SKIN DAMAGE LT SIDE STATION BS 1110 APP STR 24-23L "C" CONTAINER. STOP DRILLED ENDS OF CRACK IN A/C SKIN PER SRM 51-40, DAMAGE REMAINS IN AIRCRAFT. REFERENCE LOG NR 146871, N/R 138164, AND N/R 138165: CUT OUT DAMAGED AREA, 7" BY 6.625". FABRICATED DOUBDec 23, 2007 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHLA200700094Skin · damagedA/C SKIN DAMAGE LT SIDE STATION BS 1110 APP. STR. 24-23L "C" CONTAINER. STOP DRILLED ENDS OF CRACK IN A/C SKIN PER SRM 51-40, DAMAGE REMAINS IN AIRCRAFT.Dec 23, 2007 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHLA200700091Clamp · looseNR 1 ENG STRUT OVERHEAT DURING CRUISE. PERFORMED ABNORMALS PROCEDURE RESULTED IN IN-FLIGHT ENG SHUTDOWN ALL CHECK LISTS, PROCEDURES DONE. T/S FOUND CLAMP ON PRESSURE MODULATING VALVE LEAKING ON PRECOOLER SIDE TIGHTENED CLAMP IAW MM 36-00-1 MM 36-12-42, RAN EDec 21, 2007 · N782DH · Boeing 727227 · Pneumatic Distribution SystemSDR 07FDEA05094Warning Light · illuminatedAFTER T/O AMBER AFT AIRSTAIR LIGHT ILLUMINATED. RAN QRH. AFTER LANDING LIGHT WENT OUT. REPLACED THE AFT AIRSTAIR SWITCH ACTUATOR PER 727-200 MM 52-62-001-5, 52-70-001-5,OPS C. REPLACED ACTUATOR. COMPLIED WITH MTSI 52-62-9902.Dec 19, 2007 · N492FE · Boeing 727227 · Central WarningSDR DHL2007783002Fairing · crackedRT WING I/B FLAP HAS SMALL 1 1/2 CRACK ON FLAP TRACK FAIRING I/B FAIRING ON FLAP.Dec 18, 2007 · N783DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2007783Skin Panel · debondedUPON VISUAL INSPECTION OF THE LEFT WING UPPER SURFACE FOUND THE PANEL JUST OUTBOARD OF THE NR 1 SPOILER WITH SKIN DISBONDING. W/S629-656.5 IS PANEL LOCATION. DISBONDING AREA IS APPROX 56 SQ IN. PANEL TO BE REPLACED.Dec 14, 2007 · N783DH · Boeing 727227 · Wing, Plate/SkinSDR DHLA200700071Position Switch · failedDURING DEPARTURE AT 300 FEET AGL, LE FLAPS LIGHT WENT FROM GREEN TO YELLOW S/O CONFIRMED SLATE NR 5 YELLOW THEN LIGHT WENT BACK TO GREEN ON BOTH FRONT AND SO PANEL. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW M/M 27-82-01, CK'S NORMAL.Nov 29, 2007 · N782DH · Boeing 727227 · Leading Edge Slat Control SystemSDR 07FDEA04775Skin · corrodedFWD CARGO BILGE 3" FWD OF STA 480 S-28L AT REPAIR SPLICE OTBD SIDE HAS CORROSION. CUT OUT DAMAGE, FABRICATED REPAIR PARTS STR T7/710940. FABRICATED DOUBLER, FILLER, MAT 2024 T3.100C, AND 7075-T6.071C IAW SRM 53-10-3, 53-30-3. INSTALLED REPAIR STRINGER AND FNov 13, 2007 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784Angle · crackedLEFT WING BELOW NR 7 SPOILER HAS FALSE SPAR LOWER CHORD ANGLE REPAIR DOUBLER CRACKED AND WITH GAP UNDER DOUBLER. REPAIR MADE PER BOEING SERVICE BULLETIN 727-57-158 REV 1 DATED MARCH 30, 1989.Nov 9, 2007 · N784DH · Boeing 727227 · SpoilersSDR QPR2007F00000Duct · contaminatedPRIOR TO DEPARTURE, SMELLED SOMETHING LIKE PAPER BURNING. CHECKED THE E/E COMPARTMENT AND OBSERVED COOLING FAN WAS SHUTOFF. COULD NOT LOCATE SOURCE OF SMOKE AND ALL SYSTEMS OPERATED NORMALLY. TEST FLEW AIRCRAFT, OK. LATER, FOUND A BIRD NEST IN THE RADIO RNov 8, 2007 · N614PA · Boeing 727227 · Air Distribution SystemSDR 07FDEA04702Skin · dentedFWD LT LOWER HALF EXTERNAL FUSELAGE BET STA 312-328, STR 22L SKIN HAS DENT. REMOVED PREVIOUS SKIN DOUBLER, FABRICATED SKIN DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR REPAIR.Oct 30, 2007 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 07FDEA04647Warning Light · false activationAFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT AT FL330. LIGHT WENT OUT AT 10000 FT ENGINE ANTI-ICE WAS OPEN WHEN AFT AIRSTAIR LIGHT WAS ON. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C . 10-30-07Oct 18, 2007 · N492FE · Boeing 727227 · Door Warning SystemSDR 07FDEA04380Door Frame · damagedCABIN AFT LT SERVICE DOOR, FWD FRAME HAS 2 WORN AREAS, CAUSED BY A DRILL BIT AND SCREW TOO LONG. LOCATED JUST INBD OF FWD UPPER TORQUE TUBE LATCH CRANK, AREA MARKED. INSTALLED NEW FRAME REF, SRM 51-30-2 PG 2. INSTALLED NEW SEAL REF MM 52-12-011-4 PG 1. REISep 29, 2007 · N489FE · Boeing 727227 · Fuselage Main, StructureSDR 07FDEA04307Support Angle · crackedRT WING ROOT UPPER TE COMPOSITE PANEL INBD SUPPORT ANGLES (2EA ) ARE CRACKED, WBL 70. REMOVED CRACKED ANGLES, REF SRM 51-30-2, DRILLED NEW ANGLES TO FIT, REF 51-10-1. INSTALL, REF 51-030-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Sep 26, 2007 · N489FE · Boeing 727227 · Wing Miscellaneous StructureSDR 07FDEA04305Frame · crackedNR 2 ENG INLET DUCT HOUSING, FRAME IS CRACKED, LOCATED AT BS 1233 AND LT SIDE OF VERTICAL STAB FWD SPAR FWD AND AFT SIDE OF FRAME CRACKED REMOVED DAMAGE BY CUTTING FRAME AND FRAME ANGLE. FABRICATED REPLACEMENT SECTION OF FRAME AND FRAME ANGLE, FRAME REPAIRSep 26, 2007 · N489FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA04289Stringer Clip · crackedPOOR WORKMANSHIP, STRINGER TIE CLIP ON STR NR 1 AT FS 334 BENT/CRACKED CUSTOMER REQUEST REMOVED ELECTRIC BOX (FWD ENTRY LIGHT BALLAST). REMOVED DAMAGED CLIP. FABRICATED NEW CLIP REF BOEING DWG 65-45313. TREATED PRIMED CLIP REF SRM 51-20-1. INSTALLED CLISep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 07FDEA04288Angle · crackedLEFT WING LE NR 2 SLAT, ACTUATOR LWR FAIRING SUPPORT ANGLE CRACKED ON INBD SIDE FWD FASTENER LOCATION. REMOVED CRACKED ANGLE ON L/E NR 2 SLAT ACTUATOR FAIRING SUPPORT IAW SRM 51-30-02 PG 1. LOCATED DRILLED, TREATED, PRIMED AND PAINTED IAW SRM'S 51-10-1 PG 10Sep 25, 2007 · N489FE · Boeing 727227 · Leading Edge DevicesSDR 07FDEA04287Frame · gougedPREVIOUS DAMAGE: LT FUSE (SAT 680) STR 14L, FRAME ABOVE 14L HAS DEEP GOUGES BLENDED DAMAGED AREA ORIGINAL MATERIAL .045" MATERIAL LOSS .015" MATERIAL REMAINING .030" AND IS OUT OF LIMITS REF SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPAIR SPLICE. INSSep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA04286Stringer Clip · corrodedAFT PIT STA 1030 LBL 23" WL 147, STRINGER CLIP HAS LIGHT CORROSION. REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW CLIP TREATED, PRIMED AND INSTALLED REF 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.Sep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 07FDEA04285Stringer Clip · damagedPOOR WORKMANSHIP/CUSTOMER REQUEST, STRINGER TIE CLIP ON STR 2R AT FS 334 DAMAGED FROM MISDRILLED FASTENER HOLE REMOVED DAMAGED STRINGER CLIP. VERIFIED MATERIAL AND FABRICATED NEW STRINGER CLIP. TREATED AND PRIMED STRINGER CLIP, DRILLED UP AND INSTALLED NEW SSep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 07FDEA04284Frame · crackedRIGHT LOWER FUSELAGE PANEL NR 3438, INBOARD FORMER RIB AT CENTER OF ACCESS PANEL CUT-OUT CRACKED AT OUTBOARD ATTACH POINT ON INNER SIDE. REPLACED Z ANGLE IAW BOEING DWG 65-25581, THIS IS CLASSIFIED AS A MINOR REPAIR.Sep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA04283Skin · delaminatedVERTICAL STAB UPPER RUDDER TAB UPPER END POTTING BROKEN OPEN AND SKIN DISBONDED ON BOTH SIDES, LEFT SIDE 6-12" FWD OF T/E, RIGHT 5-13" AND DOWN 4" ALSO T/E TIP CORNER OPEN. REPAIRED UPPER RUDDER TAB ON LEFT AND RIGHT SIDES REF SRM 51-40-20 PAR 7, 8, 14, 15, ASep 25, 2007 · N489FE · Boeing 727227 · Rudder, Plate/SkinSDR 07FDEA04282Skin · delaminatedVERTICAL STAB, UPPER RUDDER TAB HAS SPOT OF SKIN DISBOND, 2" BY 3" AREA AT 25" UP FROM LWR END 1" AFT OF FWD EDGE. REPAIRED UPPER RUDDER TAB REF SRM 51-40-20 PAR 7, 8, 14, 15, 19-22 AND APPLIED EXTERIOR PROTECTIVE FINISH REF MM 51-20-151-7.Sep 25, 2007 · N489FE · Boeing 727227 · Rudder, Plate/SkinSDR 07FDEA04275Skin · damagedAFT FUSELAGE AT FS 1320 IN SECTION 48 ZONE, SKIN HAS 2 PREVIOUS PUNCTURES FILLED WITH SEALANT ON LT SIDE OF A/C BETWEEN STRINGERS 3L AND 6L JUST BELOW VERTICAL STAB. REMOVED DAMAGE SRM 53-30-3 FIG 13A. FABRICATED REPAIR DOUBLER SRM 53-30-3 FIG 13 A. NDT AT Sep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 07FDEA04273Bracket · crackedRT WING, OTBD FLAP, INBD FLAP TRACK FAIRING IS CRACKED, AT CHANNEL SUPPORT ANGLE 16 INCHES AFT OF FWD EDGE, RT SIDE REMOVED DAMAGED TEE AND INSTALLED NEW ONE IAW SRM 51-30-2 AND 51-30-5 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR.Sep 25, 2007 · N489FE · Boeing 727227 · Wing Miscellaneous StructureSDR 07FDEA04270Stringer Clip · corrodedAFT PIT STA 1130 LBL 21 WL 140, STRINGER CLIP UNDER "Z" ANGLE HAS LIGHT CORROSION. REMOVED STRINGER CLIP. FABRICATED AND HEAT TREATED NEW CLIP TO 7075 T6. TREATED, PRIMED, PICKED UP HOLES, AND INSTALLED NEW CLIP. REF: SRM 51-30-2, PG 1-12/51-10-1, PG 12/51-Sep 25, 2007 · N489FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 07FDEA04269Angle · crackedNR 2 ENG INLET DUCT HOUSING FRAME-TO-LEADING EDGE OF VERTICAL STAB ATTACH CLIP ON RT SIDE IS CRACKED LOCATED AT STA 1233 REMOVED CRACKED ATTACH CLIP, FABRICATED NEW CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476/ID NR 0001/ITEM NR 14/FRAME 1 OF 2 AND SRMSep 25, 2007 · N489FE · Boeing 727227 · Nacelle/Pylon, Main FrameSDR 07FDEA04261Angle · crackedNR 2 ENG INLET DUCT HOUSING FRAME-TO-VERTICAL STAB LEADING EDGE ATTACH CLIP IS CRACKED. LOCATED ON LT SIDE STA 1233. REMOVED CRACKED ATTACHED BRACKET, FABRICATED NEW ATTACH CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476 AND SRM 51-30-02. CLASSIFIED ASSep 24, 2007 · N489FE · Boeing 727227 · Nacelle/Pylon Miscellaneous StructureSDR DHLA200700045Engine · power lossNUMBER ONE ENGINE DID NOT MAKE TAKEOFF THRUST, TAKEOFF REJECTED. ABNORMAL PROCEDURE COMPLETED N1 INDICATION 86 PERCENT ALL OTHER ENGINE PARAMETERS NORMAL.Sep 22, 2007 · N781DH · Boeing 727227 · Engine (Turbine/Turboprop)SDR 07FDEA04017Stringer Splice · corrodedAFT PIT STA 1010, LBL 23, WL 150 STRINGER SPLICE HAS CORROSION. REMOVED OLD SPLICE, REMOVED CORROSION FROM STRINGER, ORIGINAL MATERIAL .070". REMOVED .005, REMAINING .065", FOUND TO BE WITH IN LIMITS. FABRICATED NEW STRINGER SPLICE, TREATED AND PRIMED, INSep 19, 2007 · N489FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 07FDEA04010Angle · corrodedAFT CARGO COMPARTMENT "Z" ANGLE HAS CORROSION IN 2 LOCATIONS FROM STA 950B TO 950E, RBL 24, WL 156 BLENDED CORROSION ON "Z" ANGLE STA 950B OUT OF LIMITS PER SRM 51-40-3. BLEND CORROSION AT STA 950D. REMOVED .005' FROM ORIGINAL THICKNESS OF .056, WITHIN Sep 19, 2007 · N489FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA04009Bracket · crackedCROSS BRACKET INSIDE GROUND POWER PLUG ACCESS DOOR HAS CRACKED ATTACH BRACKET AT TOP AFT ATTACH POINT REMOVED CRACKED BRACKET IN REF TO SRM 51-30-2. FABRICATED NEW BRACKET IN REF TO DWG 69-22670-5. INSTALLED NEW BRACKET IN REF TO SRM 51-30-2. THIS IS CLASSep 19, 2007 · N489FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA03800Coalescer Bag · dirtyON DESCENT PASSING THROUGH 17,000 FT, STRONG ODOR SIMILAR TO ELECTRICAL SMOKE DETECTED IN COCKPIT. ODOR SUBSIDED BUT RETURNED ON SHORT FINAL. INSPECTION OF A/C IN PROGRESS. INSPECTED A/C'S CB'S NONE WERE FOUND POPPED. NO LINGERING ODOR OF SMOKE ANYWHERE OSep 16, 2007 · N483FE · Boeing 727227 · Humidity Control System
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