Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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  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 FDEA201005071485Angle · crackedSPLICE DOUBLER CRACKED - NR 7 SLAT T/E CHORD ANGLE BENEATH TAI DUCT, APPROXIMATE WING STA 619. REMOVED T/E CHORD ANGLE OF NR 7 SLAT IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND TRIMMED CHORD ANGLE, 114" LONG, IAW SRM 57-50-2 FIG 2 AND 51-30-5. May 7, 2010 · N483FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201005061476Structure · crackedUPON REMOVAL OF T/E ACCESS PANELS, FOUND NR 4 SLAT T/E STRUCTURE CRACKED NEAR TAI DUCT CUTOUT. REMOVED T/E STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STRUCTURE USING EXTRUSION, BAC1514-1559 2024 T3511, DIMENSIONS 120", IAW SRM 57-50-2 FIG 2, 51-30-5, AND 51-30-May 6, 2010 · N483FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201005041462Pcu · failedTOTAL LOSS OF HYD SYS A QUANTITY AFTER TAKEOFF, HYD SYS A PUMPS WERE SHUTOFF AT 0235Z, HYD SYS A FLUID SHUTOFF SWITCHES WERE CLOSED AT 0240Z AND ENGINES NR 1 AND NR 2 WERE SHUTDOWN AT 0303Z. BROKE SHEAR WIRE ON ALT FLAP AND GPWS FLAP INHIBIT. PREVIOUSLY ENTEMay 4, 2010 · N285FE · Boeing 727233 · Hydraulic System, MainSDR FDEA201005011419Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 1010 BETWEEN STRINGERS 30 AND 29 L. REMOVED DAMAGE, .7500" X 3.5" IAW SRM, REV 102, 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER FOR BS 1010 FRAME BETWEEN STRINGERS 30 AND 29L IAW SRM 53-10-4, FIG 15. INSTALLED DOUBLER IAWMay 1, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201005011420Stringer · corrodedFWD CARGO HAS EXFOLIATION CORROSION ON STRINGER 28R BETWEEN STA 680 TO 700. CUT OUT DAMAGED SECTION OF STRINGER 28R, 29.5" IN LENGTH IAW SRM, REV 102M 53-10-3 FIG 1 AND 51-10-1. FABRICATED (2) STRINGER SECTIONS USING BAC1498-143, 7075-T62, 18.5" AND 11" IN May 1, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201005011520Support Angle · crackedCRACKED SUPPORT ANGLE - INSIDE RT TORQUE BOX, AFT SIDE OF STA 1263 AT AFT AIR STAIR ACTUATOR SUPPORT ASSY. REMOVED SUPPORT ANGLE FROM RT SIDE OF TORQUE BOX, AFT SIDE OF STA 1263 IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND CUT TO LENGTH EXTRUSIONMay 1, 2010 · N483FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201004291406Shear Tie · crackedSHEAR TIE CRACKED AT BS 344 BETWEEN STRINGERS 27 AND 26L CUT-OUT DAMAGE AREA DIM 3" X 1.2500" IAW SRM 53-10-4 FIG 14. FABRICATED DOUBLER REPAIR FROM 7075T6 .050 DIM 4.7500" X 4.3750" IAW SRM 53-10-4, FIG 14. INSTALLED REPAIR IAW SRM 53-10-4 AND 51-30-2, REV 1Apr 29, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201004231337Stringer · damagedSTR REPAIR "17 X 11" REQUIRED EVALUATION AT STA 1166 - STA 1183, STR 23L IAW WORK CARD 7-5100-7-5005 PT 1. REMOVED DOUBLER IAW SRM, REV 102, 51-30-2. FABRICATED REPAIR DOUBLER USING 2024-T3, .100" X 23 1/2" X 21 5/8" IAW EA 7-5330-135540. INSTALLED REPAIR Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR Y2PA2010042310007Connector · looseON FINAL APPROACH LT MLG INDICATIONS WERE ABNORMAL. GREEN "GEAR DOWN" LIGHT EXTINGUISHED. THE RED "GEAR UNSAFE" LIGHT WAS MOMENTARILY FLICKERING. ELECTED TO EXECUTE GO-AROUND TO RUN APPROPRIATE COM PROCEDURES. PROCEEDED TO HOLD. GOT THE GEAR DOWN WITH 3 GREEN Apr 22, 2010 · N45NA · Doug DC933F · Landing Gear System WiringSDR FDEA201004161211Spar · crackedCRACKED FALSE SPAR AT NR 8 SPOILER ATTACHMENT, WS 171. REMOVED DOUBLER, TRIMMED WEB 12.2500" X 9.5", LOWER CHORD 20.5" LONG IAW DWG NR SR27-57-038 REV C. FABRICATED CHORD SPLICE ANGLES FROM 7075 - 0 .071" X 6" X 14" (2) RADIUS FILLERS FROM 7075 T6 .Apr 16, 2010 · N483FE · Boeing 727227 · Wing SparSDR FDEA201004041077Stringer · damagedAFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DRILLED NEW STRINGER SECTION USING BAC1498-145 7075T-6 PO 29057141 DIMS 43.1250" AND INSTALLED NEW STRApr 4, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003271021Skin · damagedRT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DAMAGED AREAS DIMS .5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3 .050 DIMS 7" XMar 27, 2010 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201003261018Skin · corrodedCORROSION ON SKIN FROM STA 580 TO 600 BETWEEN STR 27L AND 28L. THIS NR WAS INCOPORATED IN REPAIR.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003251008Skin · crackedL-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN IS CRACKED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE DIM .1250" IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO 9009253 DIM 1" X 3.7500" IAW SRM 51-40-2, FIG 1. INSTALLED REPAIRMar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew DoorsSDR FDEA201003251009Skin · damagedL-1 DOOR LOWER LIGHTNING HOLE INNER SKIN IS DAMAGED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE, DIM .1250" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO NR 9009253, DIM 1" X 3.2500" IAW SRM 51-40-2 FIG 1 AND 52-10-1, FIG 1Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew DoorsSDR FDEA201003251011Skin · dentedDENTS 3EA EXTERIOR FUSELAGE BS 1042 STR 24R - 25R. DENTS FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NR 9009120 DIM: 8.6" X 6.7" IAW SRM 53-30-2, FIG 2 AND 53-30-3 FIG 1. Mar 25, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003251012Skin · dentedDENT EXTERIOR FUSELAGE BS 1080 STR. 20L. CUT-OUT DAMAGED AREA DIM: 6.5" X 1.75" AND FABRICATED REPAIR DOUBLER SROM 2024T3 .063 PO NR 9009362 DIM: 13.5" X 6.4" & STRUCTURAL FILLER FROM 2024T3 .050 PO NR 9009327, DIM: 13.5" X 3.5" IAW SRM 53-30-2 FIG 2 & 53-30-3Mar 25, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003130807Structure · corrodedE/E COMPARTMENT, RT MID CHORD CORRODED AT STA 294.5. REMOVED CORROSION FROM RT MID CHORD AT STA 294.5 IAW SRM, REV 102, 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1. R & R MID CHORD PN 65-19862-20 AND 2 VERTICAL STIFFENERS, PN 65-19863-10 AND 65Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003130815Frame · damagedWIRE BUNDLE STAND OFF BROKEN AND FRAME DAMAGED, STA 460, STR 8R. REMOVED DAMAGED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGE AT FRAME UP TO .125 DIA IAW SRM 53-10-1, FIG 1 AND INSTALLED .1250" SOLID FASTENER AT FRAME IAW SRM 51-30-2. INSTALLED NEW STAND OMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201003130816Frame · damagedFRAME DAMAGED BY TOO LONG HARDWARE INSTALLED IN WIRE BUNDLE STAND OFF CLAMP, STA 500, STR 8R. REMOVED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGED AREA .125 DIA IAW SRM 53-10-1, FIG 1 INSTALLED .1250" SOLID FASTENER IAW SRM 53-10-1 FIG 1 & 51-30-2. INSTMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201003130810Skin · dentedDENT BS 400 STR 17L - 19L EXTERIOR FUSELAGE. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 2.6250" X 2.8750" IAW SRM 53-30-3 FIG 3. HFEC INSP CUT-OUT AREA IAW NDTM 51-00-00, FIG 23, PART 6, NO DEFECTS NOTED. FMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003130814Skin · crackedRT INBD FOREFLAP CARRIAGE ATTACH FITTING AREA AT STA 224, SKIN CRACKED FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA, DIMENSIONS .750" X .218" IAW SRM, REV 102, 57-50-4, FIG. 1. FABRICATED FILLER USING 2024 T-3, PO NR 9002222, DIMENSIONS .050" X .750" X .218" Mar 13, 2010 · N479FE · Boeing 727227 · Wing, Plate/SkinSDR FDEA201003130811Skin · chafedFUSELAGE SKIN CHAFED AT LAP SEAM, STR 19R, STA 720E. CUT-OUT DAMAGED AREA DIM: 5.5" X 2.7500" IAW SRM 53-30-3 FIG 6. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23, PART 6, NO DEFECTS NOTED. FABRICATED DOUBLER FROM 2024T3 .071 DIM: 13" X 9" AND 2 EA TAPER FILMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003110778Beam · mismanufacturedFWD BS 1183 BULKHEAD LBL 18 VERTICAL BEAM HAS FASTENER WITH NO SPACING. CUT-OUT DAMAGED AREA AT VERTICAL BEAM, FABRICATED REPAIR PARTS & INSTALLED. REPAIR PARTS AT BS 1183 LBL 18 VERTICAL BEAM IAW EA 7-5310-135529.Mar 11, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003110782Rib · crackedNR 6 SLAT HAS 2 CRACKED RIBS AT ACTUATOR FWD MOUNT. NBD SIDE IS CRACKED AT AFT NUTPLATE AND OTBD SIDE CRACKED IN BOTTOM RADIUS. REMOVED ACCESS PANELS AND CRACKED RIBS AT NR 6 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW SRM 51-30-5. INSTALLED NEWMar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110783Angle · crackedNR 7 SLAT LOWER AFT CHORD ANGLE IS CRACKED BELOW T-DUCT.Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110784Rib · crackedNR 7 SLAT HAS 1 RIB CRACKED ON OTBD SIDE OF ACTUATOR FWD MOUNT.Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110780Rib · crackedNR 5 SLAT HAS ONE RIB CRACKED INBD SIDE OF ACTUATOR FWD MOUNT. REMOVED WEB PNL FOR ACCESS AND REINSTALLED IAW B727 SRM 51-30-2. REMOVED 2 EA. RIBS FOR CRACKS AND FABRICATED 1 RIB FROM 2024-0 .040 PO 24146179 DIMS: 16 3/4" X 6" IAW SRM 57-20-2 FIG 2 & 51-30-Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110781Rib · crackedNR 5 SLAT RIB OTBD OF ACTUATOR FWD MOUNT, PREVIOUS REPAIR DOUBLER IS MISSSING 1 FASTENER AND DOUBLER IS INSTALLED ON TOP OF BUTTON HEAD RIVET. ACCOMPLISHED NR 5 SLAT RIBS REPLACEMENT ON NR N00260 SO 00047694, SDR 10-0780Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003040634Valve · malfunctionedACFT WOULD NOT PRESSURIZE. TROUBLESHOOTING RAN NR 3 ENGINE PRESSURIZED AC PERFORMED CABIN DECAY. CHECK IAW JRH DECAY CHECK GOOD. PERFORMED BLEED SYS CHECK IAW JRH AND SYS CHECKED GOOD. AC PRESSURIZED TO 6 PSID NORMALLY NO FAULTS NOTED. LT FWD PACK VALVE WAS Mar 4, 2010 · N490FE · Boeing 727227 · Cabin Cooling SystemSDR FDEA201002160434Skin · damagedEVALUATE TRIM OUT EXTERIOR FUSELAGE LAP SEAM BS 178 STR 18R CUT OUT DAMAGE ON UPPER SKIN 2" X 2 1/8" AND REMOVED FASTENERS COMMON TO REPAIR DOUBLER IAW EA 7-5330-135526, FABRICATED REPAIR PARTS, DOUBLER AND FILLER USING 2024-T3, 0.071" PO NR 9009068 DIMENSION Feb 16, 2010 · N482FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR CA100205001Spring · broken(CAN) ACFT YAWED ABRUPTLY TO THE LT ON TAKEOFF, RUDDER PEDALS FELT ABNORMALLY LOOSE, NO RESISTANCE/FRICTION. ACFT CONTINUED SHORT FLIGHT AND LANDED WITHOUT INCIDENT. MX FOUND INBD RUDDER CONTROL SPRING BROKEN. SPRING REPLACED. (TC 20100205001)Feb 4, 2010 · Boeing 727231 · Rudder Control SystemSDR FDEA201001290287Engine · malfunctionedTHRUSH LEVER BROUGHT BACK TO IDLE FOR DESCENT. NR 2 LOW OIL PRESSURE OR FILTER BYPASS LIGHT CAME ON, WENT OUT, CAME BACK ON. AT THAT TIME OIL QTY SLOWLY REDUCED TO 1 GALLON WITH OIL PRESSURE IN YELLOW BAND. FOLLOWED QRH WITH ENG SHUTDOWN. ENG WINDMILLED FOR Jan 29, 2010 · N278FE · Boeing 727233 · Engine Oil PressureSDR CA091224001Window · cracked(CAN) DISCREPANCY: AT FL 37.0 VERY LOUD CRACKING NOISE FROM VICINITY OF F/O NR 3 WINDOW DESCENT TO 10,000 AND DEPRESSURIZED AIRCRAFT. MX NOTE: AS PER CREW COMMENTS AIRCRAFT DID NOT LOOSE CABIN PRESSURE DUE TO THIS INCIDENT AND AS A PRECAUTIONARY MEASURE AIRCDec 24, 2009 · Boeing 727247 · Flight Compartment WindowsSDR CA091106006Bearing · seized(CAN) TO MAINTAIN STRAIGHT FLIGHT IN CLIMB (HAND FLYING), REQUIRED AILERON TRIM 3 1/2 UNITS, CONTROL COLUMN AT 18 DEG. MX FOUND CABLE ROD END BROKEN AT SPOILER MIXER MECHANISM. BRG IN ROD END SEIZED. ROD END REPLACED.Nov 5, 2009 · Boeing 727225 · Aileron Control SystemSDR CA091022004Windshield · cracked(CAN) DURING CRUISE AT FL320, THE CAPTAINS L1 WINDOW OUTER PANE CRACKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND THE WINDOW WAS REPLACED BY MAINTENANCE PERSONNEL. WHEN COMPLETE THE AIRCRAFT WAS RETURNED TO SERVICE. (TC 20091022004)Oct 20, 2009 · Boeing 727260 · Flight Compartment WindowsSDR CA091009003Warning Switch · faulty(CAN) IN POSITION ON RWY FOR DEPARTURE. THRUST LEVERS ADVANCED TO TAKEOFF THRUST FOLLOWED BY THE TAKEOFF WARNING HORN. THRUST RETARTED TO IDLE. FLAPS RESELECTED UP THEN BACK TO FLAPS 15, STAB TRIM MOVED TO ZERO THEN BACK TO TAKEOFF POSITION, SPD BRAKES DEPLOYEOct 8, 2009 · Boeing 727247 · Stabilizer Position IndicatingSDR ABXR200910060038Skin · delaminatedDURING A HEAVY MX INSP, THE LT WING NR2 SPOILER WAS FOUND DELAMINATED OUTSIDE OF THE MFG LIMITS. REMOVED AND REPLACED THE NR2 SPOILER AND ACCOMPLISHED THE ADJUSTMENT AND TEST IAW THE AMM. ITEM WAS RETURNED TO SERVICE.Oct 6, 2009 · N898AA · Boeing 727223 · SpoilersSDR CA090928001Wire · broken(CAN) AFTER DEPARTURE FROM YVP, THE FLIGHT CREW ADVISED OF A NOSE LANDING GEAR DISAGREEMENT LIGHT. THE GEAR WAS RECYCLED SEVERAL TIMES AND THE DISAGREEMENT LIGHT REMAINED. MAINTENANCE DISCOVERED A BROKEN WIRE IN THE NOSE LANDING GEAR DOWNLOCK WIRE HARNESS. WISep 23, 2009 · Boeing 727233 · Landing Gear System WiringSDR CA090827005Switch · unserviceableAFTER GEAR SELECTED UP ON DEPARTURE, NR 3 "REVERSER OPERATING" LIGHT ILLUMINATED. THRUST REVERSER WAS VIEWED TO BE IN NORMAL POSITION AFTER LANDING AND ACFT TAXIED BACK TO RAMP. LIGHT REMAINED ILLUMINATED UNTIL GROUND PWR WAS APPLIED TO THE ACFT. NR 3 "THRUAug 27, 2009 · Boeing 727225 · Engine Thrust ReverserSDR C8GA20090176B-Nut · brokenWHILE ACFT WAS PASSING THRU 26000 FT THE NR 3 ENG BEGAN TO COMPRESSOR STALL. CREW PERFORMED APPROPRIATE PROCEDURES AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 3 ENG PRBC WAS REMOVED AND REPLACED. WHILEAug 11, 2009 · N713AA · Boeing 727223 · Compressor Bleed ValveSDR CA090702003Bolt · damaged(CAN) WHILE PERFORMING, ACFT DAILY INSP, IT WAS VISUALLY NOTED THAT RT INBD MID FLAP, INBD CARRIAGE, DEAD WEIGHT ROLLER BOLT WAS DAMAGED. CARRIAGE HSG ASSY WAS REPLACED WITH A SERVICEABLE UNIT AND THE ACFT WAS RETURNED TO SERVICE.Jun 27, 2009 · Boeing 727225A · Trailing Edge FlapsSDR CA090625004Actuator · failed(CAN) DISCREPANCY ON DESCENT. HYD SYS A, ENG 1 PUMP LOW PRESSURE LIGHT ILLUMINATED WHEN FLAPS WERE EXTENDED. PRESSURE READ NORMAL QUANTITY 0. ENGINE NR 2 PUMP LIGHT ILLUMINATED. BOTH LIGHTS THEN EXTINGUISHED. FLAPS AND GEAR EXTENDED BY NORMAL SYS. ACFT Jun 24, 2009 · Boeing 727247 · Trailing Edge Flap ActuatorSDR CA090625006Clamp · leaking(CAN) ENROUTE, HAD AN ENGINE FIRE WARNING. ENG NR 3 DRILL AND CHECK LIST COMPLETED AND NR 1 BOTTLE DISCHARGED. TROUBLESHOOTING CARRIED OUT AND COULD NOT FAULT ON GROUND. WITH ENGINE RUNNING, CARRIED OUT A LEAK CHECK OF PNEUMATIC DUCTS ON THE ENG AND AROUNDJun 24, 2009 · Boeing 727247 · Engine Bleed Air SystemSDR CA090622005Window · cracked(CAN) JUST AFTER TAKEOFF, R1 WINDOW CRACKED EXTERIOR PANE WITH EVIDENCE OF BURNED HEAT ELEMENT. ACFT PROCEDED TO DESTINATION, NORMAL OPERATION, ACFT LANDED WITHOUT INCIDENT.Jun 18, 2009 · Boeing 727223 · Flight Compartment WindowsSDR CA090622011Dome · damaged(CAN) UPON LEVELING AT FL380 AND REDUCING THRUST TO CRUISE POWER SETTINGS, FLIGHT CREW NOTICED THAT NR 2 ENG EXPERIENCED AN ENG STALL. THERE WERE NO FURTHER PROBLEMS DURING REMAINDER OF FLIGHT. UPON ARRIVAL AT DESTINATION, MX CARRIED OUT TROUBLESHOOTING OF NJun 18, 2009 · Boeing 727225 · Turbine Engine Air Inlet SectionSDR CA090619007Shroud · delaminated(CAN) FUEL NOZZLE PHENOLIC HEAT SHROUD DELAMINATED AS VIEWED THROUGH THE ENGINE COLD STREAM IN GROUND INSP. UPON FURTHER INSP DETERMINED DIFFUSER CASE CRACKED 7-8 IN. ENG REPLACED.Jun 12, 2009 · Boeing 727225 · Fuel Injector NozzleSDR CA090619008Diffuser · cracked(CAN) DURING INSP, FOUND DIFUSSER CASE CRACKED 7-8 IN. ENGINE REPLACED.Jun 12, 2009 · Boeing 727225 · Turbine Engine Combustion SectionSDR C8GA20090153Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LT OTBD FOREFLAP IS CRACKED AT INBD ATTACK CUTOUT. STOP DRILLED CRACK, PERFORMED HFEC INSP FOR CRACK CONTAINMENT NO FURTHER CRACKS. FABRICATED REPAIR DOUBLER FROM 2024 T3 .063 INCH DIM 6.5 INCH X 7 INCHJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090181Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT WING INBD MID-FLAP UPPER T/E IS DELAMINATED. DAMAGED AREA WAS REMOVED DIM 12.5 INCH X 4 INCH. FABRICATED REPAIR FILLER FROM 2024 T3 .016 INCH DIM 12.5 INCH X 4 INCH AND DOUBLER FROM 2024 T3 .020 INCHJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge Flaps
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