Boeing 727-223

Service difficulty reports · 5,313

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727223'
  ORDER BY difficulty_date DESC"

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SDR C8GA20080040Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION OF # 4 RIGHT LAP SEAM BS 720-720A NOTED 7 EA FASTENER HOLES CRACKED. CUT OUT DAMAGED HOLES AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER FROM 2024 T3 .071" AND FABRICATED DOUBLER FROM 2024 T3 .080". INSAug 24, 2008 · N713AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080054Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR OB MOUNTING BRACKET HAD A 1" CRACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER AND NEW STIFFNER. INSTALLED NEW SUPPORT PARTS IAW SB 727-57-0130. NO OTHER DEFECTS WERAug 23, 2008 · N713AA · Boeing 727223 · Leading Edge DevicesSDR C8GA20080053Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR IB MOUNTING BRACKET HAD A 1" CRACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER FROM 301 1/2 HD .100" (7.5 X 3) AND NEW STIFFNER FROM BAC 1503-100145 (9" X 4"). INSTAAug 23, 2008 · N713AA · Boeing 727223 · Leading Edge DevicesSDR C8GA20080049Seat Track · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION THE SEAT TRACK LOCATED AT BS. 760-850 RBL .5 HAD SEVERAL GOUGES. DAMAGED SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS FABRICATED. INSTALLED SEAT TRACK ALL WORK ACCOMPLISHED IAW DWG AEI 727-2-063. NO OTHER DEFAug 23, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080048Seat Track · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK CORRODED AT BS. 860 RBL 0.5. REMOVED SEAT TRACK AT RBL 0.5 BS 860, FABRICATED AND INSTALLED SEAT TRACK PER DWG. AE727-2-063 NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SAug 23, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080047Seat Track · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS 3 EA AREAS OF CORROSION / GOUGE AT BS. 590-720 RBL 0.5. REMOVED SEAT TRACK AT RBL 0.5 BS 590-720, FABRICATED AND INSTALLED SEAT TRACK PER DWG AE727-2-063, NO OTHER DEFECTAug 23, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080046Seat Track · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS DEEP QOUGE AT BS 740-760 LBL 45.5. REMOVED SEAT TRACK AT LBL 45 BS 740-760 DISPLACED SPLICE PER VENTURA AEROSPACE DWS 2902 INSTALLED NEW SEAT TRACK IAW SRM 53-10-5, 53-10Aug 23, 2008 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080036Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION OF THE LEFT #4 LAP SEAM, 2 EA CRACKS WERE NOTED AT FASTENER LOCATIONS BS 435. THE DAMAGE WAS CUT OUT AND REMOVED. VERIFIED CRACK CONTAINMENT, FABRICATED FILLER FROM 2024 T3 .040", FABRICATED DOUBLER FROM 20Aug 23, 2008 · N713AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080056Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP HAS 1 LARGE DENT NEAR CENTER ON BOTTOM SIDE. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRMAug 20, 2008 · N713AA · Boeing 727223 · Trailing Edge FlapsSDR C8GA20080055Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP BOTTOM SIDE UNDERNEATH TEARDROP AREA DELAMINATED. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAAug 20, 2008 · N713AA · Boeing 727223 · Trailing Edge FlapsSDR 08FDEA03504Seat Track · wornSEAT TRACK WORN STA 640 BL 0. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED SEAT TRACK SECTION USING PREVIOUS GOOD CONDITION SPLICES IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7.Aug 19, 2008 · N223FE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA20080058Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT CARGO COMPARTMENT SHEAR TIE LOCATED AT S29-30L CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, DAMAGE WAS CUT OUT. FABRICATED SHEAR TIE, HEAT TREATED TO T6. FABRICATED DOUBLER. INSTALLEDAug 18, 2008 · N713AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080042Structure · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION CORROSION WAS NOTED BETWEEN STR. 29L & 29R AT BS 1010. CORROSION WAS BEYOND LIMITS, DAMAGE WAS REMOVED. FABRICATED FILLER, FABRICATED DOUBLER. INSTALLED REPAR IAW SRM 53-30-2, 53-30-3. NO OTHER DEFECTS WAug 16, 2008 · N713AA · Boeing 727223 · Fuselage Main, StructureSDR C8GA20080059Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT CARGO COMPARTMENT SHEAR TIE LOCATED AT BS 985 STR 30-29R CORRODED. FRAME CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED SECTION. FABRICATED FRAME. FABRICATED ANGLE. INSTALLED REPAAug 15, 2008 · N713AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR C8GA20080051Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE THE NR 2 KFLAP ACTUATOR UPPER MOUNT WAS CRACKED AT THE UPPER INBOARD CORNER. REMOVED DAMAGED MOUNT AND FABRICATED NEW. INSTALLED NEW MOUNT IAW SRM 57-20-02. NO OTHER DEFECTS WERE NOTED. AIRCRAFTAug 13, 2008 · N713AA · Boeing 727223 · Leading Edge DevicesSDR DHLA200800075Battery Pack · inoperativeEMERGENCY ENT LIGHTS INSIDE LIGHT INOP. REMOVED AND REPLACED BATTERIES IN LIGHT PACK, OPS CHECK GOOD IAW MM 33-50-71. FLT 119. A/C WAS GROUNDED. (A)Jun 17, 2008 · N752DH · Boeing 727223 · Emergency LightingSDR G8G2008F00001Fitting · faultyDURING CLIMB, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND OIL FILTER BYPASS SWITCH GEARBOX FITTINGJun 11, 2008 · N708AA · Boeing 727223 · Engine Oil System (Airframe Furnished)SDR C8GA200800Fitting · damagedFLT 720 FROM TOL TO MCO. DURING CLIMB OPERATION OUT OF TOL THE NR 2 ENG LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN TOL WITHOUT INCIDENT. POST FLIGHT INSPECTIOJun 11, 2008 · N708AA · Boeing 727223 · Nacelle/Pylon, Attach FittingsSDR C8G2008F00003Fitting · looseDURING CLIMB OPERATION, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENG WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 2 ENGINE OIL FILTER BYPASS SWJun 11, 2008 · N708AA · Boeing 727223 · Turbine Engine Oil SystemSDR C8G2008F00014Acm · inoperativeDURING CLIMB OPERATION, THE AC WAS UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10000 FEET WITH ONE PACK OPERATION. AC RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED LT ACM INOPERATIVE. REMOVED AND REPLACED LT ACM AND LT PACK SHUMay 29, 2008 · N715AA · Boeing 727223 · Cabin Cooling SystemSDR C8GA20080014Acm · failedFLT 711 FOR DEN TO TOL. DURING CLIMB OPERATION FROM DEN THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10000 FEET WITH ONE PACK OPERATION. AIRCRAFT RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED LEFT ACM INOP. REMay 29, 2008 · N715AA · Boeing 727223 · Cabin Cooling SystemSDR C8GA20080015Accessory Unit · malfunctionedFLT 245 FROM EWR TO BDA. DURING CRUISE OPERATION CAPTAIN'S RMI CARD AND F/O'S HSI CARD STOPPED TURNING IN FLIGHT, BOTH RMI NEEDLES FROZE IN POSITION. AIRCRAFT RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THE FLIGHT INSTRMay 28, 2008 · N713AA · Boeing 727223 · Integrated Flight SystemSDR DHLA200800045Light · inoperativeFLT NR 197 - CABIN EMERGENCY EXIT LIGHT HAS ONE BULB INOPERATIVE. RELAMP CABIN EMERGENCY EXIT LIGHT PER M/M 33-10-00 P/N 1315. AIRCRAFT WAS GROUNDED.May 13, 2008 · N749DH · Boeing 727223 · Flight Compartment LightingSDR DHL2008780005Stiffener · corrodedREMOVED CORRODED MATERIAL ON VERTICAL STIFFENER IN LT W/WELL AT BS 930, FABRICATED TYPICAL EXTRUSION REPAIR, AND INSTALLED REPAIR PER B727 SRM 53-10-2 FIG 4 AND 51-40-4 FIG 1.May 12, 2008 · N780DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008780004Stiffener · corrodedREMOVED CORRODED VERTICAL STIFFENER AT LT W/WELL KEEL AREA BS 920, FABRICATED NEW STIFFENER, AND INSTALLED PER B727 SRM 53-10-2 FIG 4, 51-30-5, 51-30-2, AND 51-10-2.May 12, 2008 · N780DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008780007Web · crackedCUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1240, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1.May 11, 2008 · N780DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008780006Web · crackedCUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1220, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1.May 11, 2008 · N780DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008780003Web · crackedCUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1230, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1.May 11, 2008 · N780DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHLA200800042Gasper Fan · odorFLT NR 213 WITH GASPER FAN ON, ELECTRICAL ODOR NOTED. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD IAW MM 21-23-00. AIRCRAFT WAS GROUNDED.May 6, 2008 · N753DH · Boeing 727223 · Air Distribution FanSDR DHL2008753518Bracket · crackedNR 3 KRUEGER FLAP ACTUATOR I/B MOUNT ANGLE (BRACKET) CRACKED. REMOVED, FABBED AND INSTALLED IAW BOEING DWG 65-16263 REVC AND B727 SRM 51-20-1 FIG 2, 51-10-2 AND 51-30-2 MATERIAL 7075 T6 .063 INCH 9 INCH BY 6 1/4 INCH.Apr 10, 2008 · N753DH · Boeing 727223 · Wing, Attach FittingsSDR DHL2008753517Mount · crackedWHILE AT C CHECK, NR 1 KRUEGER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3.5 INCH.Apr 10, 2008 · N753DH · Boeing 727223 · Wing, Attach FittingsSDR DHL2008752516Mount · crackedWHILE AT C CHECK, NR 1 KRUEBER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3 1/2 INCH.Apr 10, 2008 · N753DH · Boeing 727223 · Wing, Attach FittingsSDR CA080411004Line · leakingAFTER TAKEOFF WHEN GEAR SELECTED UP, HYDRAULIC SYSTEM "A" LOW LEVEL LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO 2.0 GAL. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED FOR APPROACH. PER FLIGHT CREW CHECKLIST GEAR WAS MANUALLY LOWERED HOWEVER FLIGHT CApr 8, 2008 · Boeing 727223 · Hydraulic System, MainSDR DHL2008753512Nose Cowl · crackedWHILE AT C CHECK, NR 1 ENG NOSE COWL IB SIDE UPPER, CRACKED AT FASTENER HEAD AT PANEL CUTOUT NAC STA 77. FABRICATED AND INSTALLED REPAIR, CUT-OUT AREA NAC 69-77 8 3/4 INCH BY 6 1/2 INCH 3 DOUBLERS 2 INNER 6 INCH BY 4 INCH OUTER 1 11 INCH BY 8 1/2 INCH 1 FILLEApr 7, 2008 · N753DH · Boeing 727223 · Nacelle/Pylon, Main FrameSDR DHL2008753511Skin · damagedC CHECK, AFT COMPT FUSELAGE SKIN HAS OPEN HOLES BETWEEN STA 1148- 166 BETWEEN STR30- 29R AT PREVIOUS REPAIR. REMOVED, FABRICATED AND INSTALLED EXTERNAL DOUBLER 18" BY 7" IAW SRM 53-30-3 FIG 3 AND EA38100001-001-B INTERNAL DOUBLER 18" BY 4" IAW SRM 53-30-3 FIGApr 3, 2008 · N753DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR C8GA20080013Overheat Loop · faultedCLT TO BNA - DURING CLIMB OPERATION, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 STRUT OVERHEAT DETECTOR LOOP AT FAULT. REMOVED AND REPLACED NApr 1, 2008 · N708AA · Boeing 727223 · Overheat DetectionSDR C8GA20080012Helicoil · damagedFLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE NR 1 ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT Mar 25, 2008 · N899AA · Boeing 727223 · Turbine Engine Accessory DriveSDR DHL2008753516Vent · chafedL/WING TANK VENT TUBES CHAFED, WS 519, 546, 601, 629, AND 656. ACCOMPLISHED BLEND OUT AT CHAFED AREAS, FABRICATED 5 DOUBLER REPAIRS, AND INSTALLED AS PER ASTAR AIR CARGO EVA: B228-00050 REV IR DATED 3/13/08 AND COTNEY AEROSPACE ED: EDAF28-1 REV IR DATED 3/1Mar 24, 2008 · N753DH · Boeing 727223 · Fuel StorageSDR DHL2008753514Angle · crackedL/WING FIXED L/E VERT SPT ANGLE CRACKED, LWR END, AT WBL 92. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE FROM 7075T6, .063 INCH BY 7.25 INCH BY 2.5 INCH, AND INSTALLED PER B727 SRM 51-10-1, 57-10-2 FIG 3, AND 51-40-3 FIG 1.Mar 14, 2008 · N753DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008754001Wedge · delaminatedUPON INSPECTING THE EXTERIOR OF THE AIRCRAFT, FOUND THE RIGHT INBOARD TRAILING EDGE MID FLAP WEDGE DELAMINATED AT THE INBOARD END. ABOUT 20 INCHES FROM THE INBOARD END HAS A DELAMINATION APPROX 6 INCHES LONG SPANWISE AND THE WIDTH OF THE WEDGE. PART REPAIREDMar 12, 2008 · N754DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008753513Seat Track · gougedMAIN CABIN SEAT TRACK GOUGED, BS 700, RBL 25. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK FROM BAC1503-792 PO NR 9006020, 172" LONG, AND REPAIR ANGLE FROM BAC1503-100122, PO NR 9006027, 12 INCH LONG, AND INSTALLED SEAT TRACK PER B727 SRM 53-10-5 FIG 1 AMar 10, 2008 · N753DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008753510Door Frame · crackedWHILE AT C CHECK, AFT CARGO COMPARTMENT DOOR FRAME AT STA 950E CRACKED. REPAIRED WEB AND CHORD IAW B727 S/B 727-53A0199 FIG 2 DETAIL 2 AND 13.5 INCH BY 4.5 INCH WEB 1 1/2 INCH BY 12 INCH CHORD IAW B727 S/B 727-53A0199 FIG 1 TABLE 1.Mar 8, 2008 · N753DH · Boeing 727223 · Fuselage Main, StructureSDR DHL2008753500Stiffener · corrodedC CHECK REF N/R 096608, LT WHEEL WELL STA 930 LBL 8, VERTICAL STIFFENER HAS CORROSION AT LOWER END AROUND NUT PLATE, ANCHOR NUT AND SURFACE. REMOVED CORROSION ON LT WHEEL WELL STA 930 LBL 8, VERTICAL STIFFENER IAW B727 SRM 51-10-6, PER SRM 53-10-2 FIG4 ORIGINMar 8, 2008 · N753DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080009Strainer · unknownFLT 724 FROM TOL TO ROC - DURING CLIMB OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT, REMOVED AND INSPECTED THE MAIN OIL STRAINEMar 6, 2008 · N898AA · Boeing 727223 · Engine Oil Distribution (Airframe Furnished)SDR C8GA20080008Oil Filter · dirtyFLT 719 FROM ALT TO TOL - DURING CRUISE OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. THE NR 3 ENGINE OIL FILTER WAS REMOVED AND INSPECTED, CARBON CONTAMINATION WAS NOMar 6, 2008 · N898AA · Boeing 727223 · Engine Oil Distribution (Airframe Furnished)SDR DHLA200800022Battery Pack · dischargedCOCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED COCKPIT EMERGENCY EXIT LIGHT BATTERIES MODEL NR-106PER MM 33-50-71. OPS CK SERVICEABLE. AIRCRAFT WAS GROUNDED.Mar 5, 2008 · N749DH · Boeing 727223 · Emergency LightingSDR DHL2008753515Angle · crackedNR 2 K-FLAP ACTUATOR I/B MOUNT ANGLE CRACKED, AT WS 236.2. REMOVED, FABRICATED NEW WEB FROM 7075T6, .063 INCH BY 11 INCH BY 7.5 INCH, AND INSTALLED PER B727 SRM 57-50-2 FIG 1 AND 51-30-2.Mar 2, 2008 · N753DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008753507Panel · cracked"C" CHECK, CRACK INDICATION INSIDE LT ELEVATOR PANEL 9305 ON LWR RIB ELEV STA 20. REMOVED CRACKED ANGLE LT ELEVATOR AT LOWER RIB AT PANEL NR 9305 STA 20 IAW SRM 51-30-2. FORMED NEW ANGLE PER DRAWING 65-25634, REV G AND 51-10-3 AND 51-20-1 OF THE SRM. TREATEMar 1, 2008 · N753DH · Boeing 727223 · Elevator, Plate/SkinSDR DHL2008753505Skin · chafed"C' CHECK, RT O/B FORE FLAP UPPER L/E 400 (WBL) HAS DEEP CHAFE MARK. BLENDED OUT AREA AT RT OB FORE FLAP UPPER L/E WBL400 IAW SRM 51-10-6. MAT LOSS 50 PERCENT. FOUND OUT OF LIMITS IAW SRM 57-50-1. CUTOUT DAMAGED AREA APPROX 1 1/8 INCH BY 1 7/8 INCH AND FABFeb 28, 2008 · N753DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008753503Structure · crackedDURING "C" CHECK LT I/B MIDFLAP T/E CHORD CRACKED WBL 124. OPENED SECTION OF LOWER PANEL I/B MID FLAP T/E IAW SRM 51-30-2. REMOVED FASTENERS AND CUTOUT DAMAGED AREA AT CHORD APPROX 46 1/4 INCH. FAB NEW PART AND ONE SPLICE IAW SRM 57-50-2 FIG 5 AND 51-40-4 FFeb 28, 2008 · N753DH · Boeing 727223 · Trailing Edge Flaps
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