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 CA050527002Actuator · lack of lubeDURING CRUISE, A/C BEGINNING TO PITCH UP & DOWN SLIGHTLY WITH AUTOPILOT ENGAGED. DISENGAGED AUTOPILOT IN ORDER TO RE-TRIM A/C. DURING PROCEDURE RUDDER TRIM FOUND IMMOBILE. ATTEMPTED SMALL RUDDER DEFLECTION WITH RUDDER PEDALS & FOUND THEM TO BE IMMOBILE. DEMay 19, 2005 · Boeing 727225 · Rudder Tab Control SystemSDR CA050405010Actuator · failed(CAN) DURING CLIMB PHASE, SLATS RETRACTED, NR 1 SLAT, HOWEVER DID NOT SHOW RETRACTED. FLIGHT CREW CONFIRMED THAT AIRCRAFT DID NOT HAVE ANY UNCOMMANDED ROLL IN THE FLIGHT CHARACTERISTICS. THIS INDICATED AN INDICATION FAULT ONLY. CREW RETURNED TO POINT OF DEPMar 30, 2005 · Boeing 727225 · Leading Edge Slat ActuatorSDR DHL2005742003Window · fireSMOKE AND FIRE NOTED FROM R1 WINDSHIELD CONNECTION. COMPLETED CHECK LIST AND NOTED C/B HAD TRIPPED. FIRE EXTINGUISHER HAS BEEN DISCHARGED. INSPECTED WIRING PER SWPM CH-20-10-06. NO DEFECTS NOTED. R & R R2 WINDOW ASSY IAW B727 M/M 56-11-11. PERFORMED OPS CHEMar 23, 2005 · N742DH · Boeing 727225 · Flight Compartment WindowsSDR C1HA200575001Warning Light · illuminatedINFLIGHT NR 3 LOW OIL BYPASS PRESSURE LIGHT ILLUMINATED. INFLIGHT SHUTDOWN PER COM 2.72.12.Mar 19, 2005 · N675MG · Boeing 727225 · Engine Oil PressureSDR DHL2005743001Odor · detectedON CLIMBOUT IMMEDIATELY AFTER TAKEOFF THRU 10,000 FEET, ACRID ODOR SMELL IN COCKPIT. (ELECTRICAL SMELL) RAN GASPER PLUS PACKS FOR 1 HOUR. NO UNUSUAL SMELL NOTED 21-51-00. SEE LOG PAGE 032025 ITEM 1P FOR ORIGINAL ITEM. (ACRID ODOR SMELL IN COCKPIT AFTER TAKEMar 8, 2005 · N743DH · Boeing 727225 · Cabin Cooling SystemSDR C1HA200578001Hydraulic Line · chafedAFTER TAKEOFF HYDRAULIC B-SYSTEM QUANTITY LEAK TO ZERO, ACCOMPLISHED COM EMERGENCY CHECKLIST, RETURNED FOR LANDING. FOUND CHAFED SPOILER PSI LINE IN RT WHEEL WELL AREA WHERE LINES GOES THROUGH WALKING BEAM INSTALLED TEMP FLEX LINE REF SUPPL MM 20-10-12, NO LFeb 12, 2005 · N678MG · Boeing 727225 · Hydraulic System, MainSDR DHL2005742002Warning Light · illuminatedABORTED START OF ENGINE NR 2 AT KIAD. DUE TO ABNORMALLY RAPID EGT RISE. AFTER START LEVER PLACED IN START DETENT THERE WAS A SLIGHT DELAY IN EGT RISE. LIMITS WERE NOT EXCEEDED. SECOND ATTEMPT WAS NORMAL. PERFORMED ENGINE START ON NR 2 ENGINE PER ASTAR JRFeb 12, 2005 · N742DH · Boeing 727225 · Engine Temperature Indicating SystemSDR CA050218003Tube · separated(CAN) DURING CLIMB THROUGH 18000 FT ENGINE NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED ACCOMPANIED BY RAPIDLY DECREASING OIL QUANTITY AND PRESSURE INDICATIONS. CREW CARRIED OUT ENGINE SHUTDOWN CHECKLIST DECLARED AN EMERGENCY, DUMPED FUEL AND RETURNED TO DEPARTURE Feb 10, 2005 · Boeing 727225 · Engine Oil Distribution (Airframe Furnished)SDR CA050214003Switch · failed(CAN) MAIN CARGO DOOR LIGHT AND HOOKS UNLOCKED LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT AND LANDED OVERWEIGHT. CARGO DOOR VERIFIED CLOSED AND LOCKED. MAIN CARGO DOOR INDICATION MEL RAISED AND OVERWEIGHT LANDING INSPECTION C/O IAW MM 5-51-Feb 4, 2005 · Boeing 727225 · Door Warning SystemSDR 2005FA0000116Skin · misdrilledDRILL START NOTED AT L-BAND NR 1 ANTENNA FWD RT MOUNT HOLE. BS410, RBL 1. (IN SKIN) FOUND WHILE PERFORMING INSPECTION OF ANTENNA IAW WORKCARD NR 34X4505. (K)Jan 12, 2005 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005743510Stringer Clip · corrodedMAIN CABIN TENSION TIE FITTING HAS CORROSION STA 1183 LBL 63-65 WL 208.1. REMOVED 17L STA 1183 STRINGER END FITTING AND ATTACH ANGLE, DRILLED NEW END FITTING P/N 65-24276-49, FABRICATED NEW CLOSE OUT ANGLE USING .080 7075-0 PO 0003006. ANGLE HEAT TREATED ON Jan 12, 2005 · N743DH · Boeing 727225 · Fuselage Main, Attach FittingsSDR DHL2005743500Keelbeam · crackedAFT CARGO COMP STA 950F,S29R KEEL BEAM LWR CHORD CRACKED IN VERT LEG LWR RADIUS APPROX 4 INCHES. JACKED AND SHORED A/C REMOVED FLOOR SUPPORT, STR CLIPS, GUSSET, WING TO BODY FAIRINGS, STR 30 STA 950-950A, STR 29R STA 950-1009 AND INTERCOSTAL. CUT HOLE IN SKINJan 8, 2005 · N743DH · Boeing 727225 · Fuselage Main, KeelSDR DHL2005742001Accessory Unit · malfunctionedRIGHT RED GEAR LIGHT ILLUMINATES INTERMITTANTLY. REMOVED AND REPLACED LANDING GEAR ACC BOX AND OPS CHECKED SYSTEM IAW B-M/M 32-62-00, NO DEFECTS NOTED.Jan 4, 2005 · N742DH · Boeing 727225 · Landing Gear Position and WarningSDR C1HA200574002Controller · malfunctionedABOUT 50 MINUTES OUT OF SLC, CLIMBING TO FL250 THE CREW HAD LOST CABIN PRESSURE. ARNC CALL WAS PLACED TO DISPATCH, MXCTL WAS ALSO ON THE LINE. FLT DESCENDED TO FL230, THEN TO FL210, THEN TO FL 190. CABIN WAS HOLDING AT THAT LEVEL. DISPATCH RAN A POINT ALOFJan 3, 2005 · N674MG · Boeing 727225 · Cabin Pressure ControllerSDR C1HA200574001Mixing Valve · failedRT PACK MIXING VALVE WOULD NOT MOVE AFTER DEPARTURE. UPON CLIMBOUT TO ALTITUDE STARTED TO LOSE PRESSURIZATION, LT PACK WOULD NOT HOLD PRESSURIZATION AND THEN GOT A DUCT OVERHEAT ON BOTH SIDE. LOST ALL PRESSURIZATION COM 2.21.2 COMPLY WITH ATC NOTIFIED. EMERJan 3, 2005 · N674MG · Boeing 727225 · Cabin Pressure ControllerSDR DHL2005743509Seat Track · corrodedMAIN CABIN STA 360 BL 0 SEAT TRACK CORRODED (SEAT TRACK SECTION 360-500). REMOVED CORROSION IAW B727 SRM 53-10-1. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW B727 SRM 51-30-2. OBTAINED NEW SEAT TRACK PO 60-6549-0331976. LOCATE, DRILL, DEBURRED TRACKDec 29, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005743503Floor Support · crackedAFT CARGO COMPT STA 1183 RBL 7, LONGITUDINAL FLOOR SUPPORT CRACKED AT END, .375 INCH. CUT OUT DAMAGED SECTION IAW B727 SRM 51-40-3. FABBED REPAIR ANGLE IAW B727 SRM 51-40-3 FROM 7075-0 .071 PO 044327, HEAT TREATED TO T-6 ON PEMCO TRAVELER 76314000863. DRILLDec 22, 2004 · N743DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2005743508Floorbeam · corrodedMAIN PASSENGER CABIN STA 360 LBL 20 FLOORBEAM HAS CORROSION. CUT OUT DAMAGE AREA, FAB NEW UPPER CHORD, 2 EA REPAIR ANGLES, AND 2 EA REINFORCEMENT STRAPS. DRILLED AND DEBURRED, ALODINED AND PRIMED AND INSTALLED IAW BOEING 727 SRM 51-30-2, 53-10-8, 51-10-2 ANDDec 17, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005743507Floorbeam · corrodedMAIN PASSENGER CABIN STA 344 RBL 47 FLOORBEAM HAS CORROSION. CORROSION AT RBL 47 UPPER CHORD FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B727 SRM 53-10-1 FIG 4. REMOVED FASTENERS AND CUT AND REMOVED UPPER TEE CAP FROM LBL 20 TO RBL 66 IAW B727 SRM 53-10-8 FIG 9.Dec 17, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005743506Floorbeam · corrodedMAIN PASSENGER CABIN STA 380 RBL 20 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6 FOUND OUT OF LIMITS. REMOVED FLOORBOARD TO GAIN ACCESS. REMOVED UPPER CHORD FROM STA 380 BL 0 TO RBL 33. MAT ID FOR UPPER CHORD BAC 1505-10061 PO 33-41778 IDec 17, 2004 · N743DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2005743505Seat Track · corrodedMAIN PASSENGER CABIN STA 344 TO 380 RBL 44 SEAT TRACK HAS CORROSION. REMOVED, FAB, TRIMMED, DRILLED, DEBURRED, INSTALLED SEAT TRACK FS 344-380 RBL 44 IAW B727 SRM 53-10-5, 51-10-2, 53-10-2 FIG 7 51-30-2, 53-10-1 FIG 3.Dec 17, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005743501Seat Track · corrodedMAIN PASSENGER CABIN STA 740-770 LBL 23 SEAT TRACK HAS CORROSION. REMOVED CORROSION, FOUND OUT OF LIMITS BETWEEN STA 760-770 IAW B727 SRM 51-20-2. ORIG MAT .420 MAT REMOVED .030 FROM LOBE. MEASURED WITH PEMCO CALIPERS H61290 DUE DATE 17 MAY 05. REMOVED SEATDec 17, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004748008Socket · dirtyEMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR DID NOT ILLUMINATE DURING EMERGENCY POWER TEST. CLEANED CONTACT ON LIGHT & SOCKET OPS CHECKS NORMAL IAW 33-50-10.Dec 17, 2004 · N748DH · Boeing 727225 · Emergency LightingSDR DHL2005743504Seat Track · corrodedMAIN CABIN RT SIDE LUGS OF I/B SEAT TRACK CORROSION BS 380-460. REMOVED CORROSION IAW B727 SRM 51-10-2. REMOVED .120 FROM ORIGINAL0.270 THICKNESS OF MATERIAL LEFT .150 FOUND OUT OF LIMITS IAW B727 SRM 51-10-01 FIG 3 SHEET 3. CALIPERS WJ-6181 DEC. 15,05. FADec 16, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005743502Seat Track · corrodedMAIN CABIN LEFT SIDE, CENTER OF I/B SEAT TRACK CORROSION BS 720E. REMOVED CORROSION. REMOVED .065 ORIG THICKNESS .485 REMAINING MAT`L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK MAT`L. ID 60-6549 7128T6511 PO NR 0331976 IAW SRM B727Dec 15, 2004 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR CA041125001Bracket · broken(CAN) UPON ARRIVAL, MAINTENANCE PERSONEL NOTED THE NOSE LANDING GEAR DOORS HANGING OPEN. FURTHER INSPECTION FOUND THE BRACKET FOR THE DOOR OPERATION ROD BROKEN. SEE IPC 32-30-00-06 ITEM 89. BRACKET AND HARDWARE REPLACED AND GEAR SWINGS CARRIED OUT, AND A/C Nov 22, 2004 · Boeing 727225 · Landing Gear DoorsSDR DHL2004755517Skin · gougedDURING A C-CHECK, LEFT WING I/B AFT FLAP - FORE FLAP HAS A GOUGE ON EXISTING EXTERNAL DOUBLER AT O/B END. CUT OUT EXISTING SKIN O/B FLAP IAW B727 SRM 51-10-1, FABRICATED SKIN 2020T3 .050 PO 9001425 7 X 12.5 INCH FILLER DOUBLER 2024T3.060 PO 9001387, 5.5 X 12.Nov 21, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004743007Indicator · inoperativeRTO F/O'S AIRSPEED DID NOT WORK ON T/O RUN. REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR. OPS CKS GOOD IAW MM 34-12-0. PITOT STATIC CKS GOOD IAW MM 34-11-0.Nov 13, 2004 · N743DH · Boeing 727225 · Airspeed/Mach IndicatorSDR DHL2004755518Skin · damagedDURING A "C" CHECK, REPLACE INTERIM REPAIR ON RT WING I/B MID FLAP UPPER SKIN I/B END WITH A PERMANENT REPAIR. REMOVED INTERIM REPAIR FROM RT I/B MID FLAP UPPER I/B T/E TRIMMED OUT DELAMINATED AREA APPROX 1INCH BY 12 INCHES. FABRICATED FILLER APPROX 1 X 12 ANNov 8, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR CA041117002Connector · shorted(CAN) AT TOP OF CLIMB, THE SECOND OFFICER NOTED AND INFORMED THE CAPTAIN THAT THE NR 3 ENGINE OIL TEMP WAS WELL ABOVE REDLINE. CREW CARRIED OUT HIGH ENGINE OIL TEMP SUPPORT CHECKLIST WHICH RESULTS IN SHUTTING DOWN THE ENGINE. CREW DUMPED APPROX. 13,000 LBS OFNov 5, 2004 · Boeing 727225 · Engine Oil TemperatureSDR HL2004755516Skin · dentedDURING A C-CHECK, RIGHT O/B AFT FLAP LOWER SURF WBL 475 HAS LARGE SMOOTH DENT. CUT OUT DENTED AREA OF AFT FLAP LWR SKIN APPROX 5 INCHES ROUND IAW B727 SRM 51-40-20 FIG 32. FABRICATED ONE FILLER APPROX 5 INCHES ROUND & ONE DOUBLER 8 INCHES ROUND FROM 2024 T3 Oct 24, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004748500Clip · corrodedFLIGHTSTAR NON-ROUTINE:CORROSION ON CLIP ON RIGHT WING TRAILING EDGE. REFER DMI NR 18019E. REMOVED AND REPLACED CLIP ON RT WING T/E WS 180. RESEALED FASTENERS AT CLIP ON RT WING WS 180 IAW B727 SRM 51-30-2 AND M/M 28-11-00. TEE CLIP P/N 65-16201-188 ATTACHOct 23, 2004 · N748DH · Boeing 727225 · Wing, Attach FittingsSDR DHL2004755515Fairing · crackedDURING A C-CHECK, NR 5 FLAP TRACK MID FAIRING T/E CRACK. REMOVED CRACK MEMBER FROM NR 5 FLAP TRACK MID FAIRING IAW B727 SRM 51-30-2, FABRICATED STRAP 2024-T3 .040 PO 9001298, 20 X 4 INCH IAW B727 SRM 51-20-2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLOct 22, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004755509Frame · dentedDURING A C-CHECK, STA 520 FRAME RT ABOVE STR 24 HAS A DENT IN RADIUS. CUT OUT DAMAGED SECTION OF FRAME AT STA 520 ABOVE STR 24 RT IAW B727 SRM 53-10-4 FIG 1. FABRICATED & INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1. MAT USED .071 7075T-6 11 X 4.5 INOct 22, 2004 · N755DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2004755514Skin · dentedDURING A C-CHECK, 2 DENTS SIDE BY SIDE ON LOWER MID SKIN OR RT ELEV APPROX ELEV STA 90. CUT OUT DAMAGED SECTION OF RT ELEV LOWER SKIN 2 X 2 INCH AT ELEV STA 90 & FABRICATED REPAIR DOUBLER 3 X 4 INCH FROM 2024-T3 .032 MAT PO 9001030 & INTERNAL BEADED DOUBLER 7Oct 21, 2004 · N755DH · Boeing 727225 · Elevator, Plate/SkinSDR DHL2004755513Skin · dentedDURING A C-CHECK, RT ELEVATOR HAS A DENT ON BOTTOM INBOARD SKIN APPROX ELEV STA 50. CUT OUT DAMAGED AREA (1 X 1.25 INCH) AND FABRICATED REPAIR DOUBLER FROM 2024T3 PO 9001030 (2 X 2.5 INCH) .032 IAW 727 SRM 55-20-3 FIG 1. PARTS TREATED AND PRIMED IAW 727 SRM Oct 21, 2004 · N755DH · Boeing 727225 · Elevator, Plate/SkinSDR DHL2004755512Skin · corrodedDURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRINGS STA 720 D +14 STR 10 LEFT. REMOVED ANTI ICE DUCTS, HYD LINES & HARDWARE. REMOVED LT WING ROOT HARNESSES, CUT OUT DAMAGED UPPER SKIN 4.5 X 3", FABRICATED DOUBLER REPAIR 9.5 X 12", SHIM 12 XOct 21, 2004 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2004755511Skin · dentedDURING A C-CHECK, DENT RIGHT WING L/E WS 650. CUT OUT DAMAGED AREA SIZE 2 X 1 INCH ON RT WING L/E WS 650 IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SIZE 6 X 6 INCH PO 90024 IAW B727 SRM 57-30-4 FIG 1. TREATED, PRIMED PART AND AREA IAWOct 21, 2004 · N755DH · Boeing 727225 · Wing, Plate/SkinSDR DHL2004755510Skin · corrodedDURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRING STA 720D + 14" STR 19R. REMOVED ANTI ICE DUCTS & HYD LINES HARDWARE. REMOVED RT WING ROOT WIRE HARNESSES AND SUPPORTS. CUT OUT DAMAGE UPPER SKIN 4.5 X 3 INCHES IAW B727 SRM 53-30-3 FIG 5. Oct 21, 2004 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR CA041027002Brake · contaminated(CAN) DURING DECENT, WHEN LEVELING AT 6000FT CREW EXPERIENCED DIFFICULTY IN CAPTURING ALTITUDE. PROBLEM WAS QUICKLY DETERMINED TO BE HORIZ STABILIZER TRIM. TRIM WHEEL WAS VERY STIFF TO MOVE BOTH MANUALLY AND ELECTRICALLY WHEN TRIMMING NOSE UP. AC LANDED WITHOOct 20, 2004 · Boeing 727225 · Horizontal Stabilizer StructureSDR DHL2004755508Skin · damagedDURING A C-CHECK, FUSE BS 1108 STR 19 RT HAS SKIN CREASED AT STRINGER. CUT OUT DAMAGED SECTION OF SKIN AT STR 19R, STA 1108, DIMENSIONS ARE 3.25 X 2.375 INCH. FABRICATED REPAIR FILLER (DIMENSIONS ARE 3.25 X 1 INCH) FROM .050 2024-T3 PO 9001425, FABRICATED REOct 20, 2004 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2004755507Skin · delaminatedDURING C-CHECK, LEFT O/B MID FLAP UPPER T/E WBL 297 & 492 HAVE SKINS DELAMINATED. CUT OUT 2EA UPPER T/E DELAM AREAS APPROX 3 X 6.5 INCH & VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 30. FABRICATED 2EA REPLACEMENT SKINS APPROX 3 X 6.5 INCH & Oct 19, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004755506Doubler · chafedDURING C-CHECK, LEFT I/B FORE FLAP O/B L/E WBL 240 HAS REPAIR DOUBLER CHAFED THRU. REMOVED PREVIOUS REPAIR AT LEFT, I/B FORE FLAP L/E IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR 2024T3.063 PO 9001276, 6 X 5 INCH IAW B727 SRM 57-50-4 FIG 1, TREATED & PRIMOct 19, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004755505Skin · gougedDURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 93 NEAR L/E HAS SKIN GOUGED. GOUGE IN SKIN FOUND TO BE OUT OF LIMITS NDT VERIFY NO FURTHER DAMAGE IAW B727 SRM 57-50-1. REMOVED DAMAGED AREA OF SKIN 1 X 1 INCH IAW B727 SRM 57-50-4. FABRICATED DOUBLER FROM 20Oct 18, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004755504Skin · corrodedDURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 124 HAS CORR BULGES AT SKIN BUTT JOINT, MARKED. CUT OUT CORROSION DAMAGED SECTION OF LEFT I/B MID FLAP UPPER SURFACE SKIN AT BUTT JOINT STA 124 SIZE 7.75 X 1.875 INCH IAW B727 SRM 51-10-1. REMOVED & REPLACED UOct 18, 2004 · N755DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2004755501Structure · crackedDURING C-CHECK, NR 2 SLAT AT I/B TRACK ATTACH WBL 592 HAS OTBD FRAME WITH CRACK IN FWD LOWER RADIUS. STOP DRILLED CRACK NR 2 SLAT I/B TRACK WBL 592 IAW B727 SRM 51-10-1. FABRICATED DOUBLER P/N CRESS AISI 321.032 PO 900878, 5 X 3 INCH IAW B727 SRM 57-50-3, NDOct 18, 2004 · N755DH · Boeing 727225 · Leading Edge DevicesSDR 04FDEA02948Shear Tie · corrodedCORROSION ON SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R. REPAIRED SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R PER SRM 53-10-4 FIG 15.Oct 18, 2004 · N461FE · Boeing 727225 · Fuselage Main, StructureSDR DHL2004755503Web · crackedDURING C-CHECK, LT W/W, WEB AT STA 950 IS CRACKED, FWD OF HYD PUMPS AND AFT OF LT MAIN GEAR DOOR AFT UP STOP SUPPORT. CUT OUT CRACK WEB, 1 X .75 INCH IAW B727 SRM 51-10-1, FABRICATED WED REPAIR P/N 2024T3.050 PO 9001425, 6.5 X 5.5 INCH IAW B727 SRM 51-40-2 FIOct 15, 2004 · N755DH · Boeing 727225 · Fuselage Main, BulkheadSDR DHL2004755500Skin · gougedDURING A "C" CHECK, RT FUSE HAS A GOUGE AFT BS 1133 BELOW STR 24R. CUT-OUT DAMAGED SKIN 2 1/2" BY 1" AT STA 1133 BELOW STR 24R IAW B727 SRM 53-30-3. FABRICATED DOUBLER 10" X 7" P/N 2024 T3.071 PO NR 9001189 IAW B727 SRM 53-30-3,TREATED AND PRIME IAW B727 SROct 13, 2004 · N755DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2004755502Skin · dentedDURING C-CHECK, LT FUSELAGE SKIN HAS A DENT AFT BS 1050 BELOW STR 22L. CUT OUT DAMAGED SKIN, 3 X 1 INCH AT STA BELOW STR 22L IAW B727 SRM 53-30-3, FABRICATED DOUBLER FROM 2024 T3.071, 10 X 7 INCH PO 9001189 IAW B727 SRM 53-30-3, TREATED AND PRIMED IAW B727 SROct 12, 2004 · N755DH · Boeing 727225 · Fuselage Main, Plate/Skin
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