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 C8G2008F00018Turbine · damagedON TAKEOFF, JUST AFTER V2 THE NR 2 ENGINE FAILED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED TURBINE DAMAGE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. OPS CHECK GOOD. NO OTHER DEFECTS WERE Sep 10, 2008 · N808EA · Boeing 727225 · Turbine SectionSDR CA080911003Actuator · failed(CAN) DURING CLIMB THROUGH APPROX 2,000 FT NR1 ENGINE LOW HYDR PRESSURE LIGHT ILLUMINATED, SYS `A` HYDRAULIC OIL AND PRESSURE LOSS. ACFT RETURNED TO DEPARTURE. NR5 KRUGER FLAP ACTUATOR FOUND FAILED AND ATTACH BRACKET DAMAGED. REPLACED ACTUATOR AND TESTED IAW ASep 5, 2008 · Boeing 727225 · Leading Edge Slat ActuatorSDR C8G2008F00017Fcu · unserviceableSHORTLY AFTER TAKEOFF DURING CLIMB OPERATION THE NR 1 ENGINE SPREAD 28 HIGH AND ALL ENGINE INDICATORS BEGAN TO DECREASE INDICATING A FAILURE. THE ENGINE THEN RELIT DUE TO CONTINUOUS IGNITION BEING ENGAGED. 2 OR 3 MINUTES LATER THE SAME EVENT OCCURRED. THE AC RSep 3, 2008 · N801EA · Boeing 727225 · Fuel Control/Turbine EnginesSDR C8G2008F00015Indicator · inoperativeAFTER TAKEOFF FOUND RADAR UNSUITABLE FOR FLIGHT OPERATIONS INTO KNOWN CONVECTIVE ACTIVITY. ON ROTATION WX RADAR DOES NOT STABILIZE REGARDLESS OF PITCH KNOB SELECTION, RADAR SHOWS COMPLETELY COVERS SCREEN. DURING CRUISE RADAR INDICATES FALSE TARGETS ON ALL PITCAug 23, 2008 · N755DH · Boeing 727225 · Weather Radar SystemSDR CA080730002Smoke Detector · failed(CAN) ON CLIMB THROUGH FL290 CARGO SMOKE 6TH POSITION LIGHT ILLUMINATED AND FIRE WARNING BELL SOUNDED. ACFT RETURNED. ON ARRIVAL, NO SMOKE DETECTION LIGHTS WERE ILLUMINATED ON FE PANEL. CARGO AREA INSPECTED FOR SMOKE. NONE FOUND. SUSPECTED FAILURE OF NR 6 SMOKJul 30, 2008 · Boeing 727225 · Smoke DetectionSDR C8G2008F00010Antenna · inoperativeFLT 1204, AFTER TAKEOFF, THE RADAR WAS SPOOKING AND WOULD NOT PAINT KNOWN BAD WEATHER . THE AIRCRAFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE RADAR ANTENNA AT FAULT. REMOVED AND REPLACED RADAR ANTENNA PERFORMED OPERATIONAL CHEJul 22, 2008 · N808EA · Boeing 727225 · Weather Radar SystemSDR C8G2008F00008Antenna · faultedAFTER TAKEOFF, THE RADAR WAS SPOKING AND WOULD NOT PAINT KNOWN BAD WEATHER. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE RADAR ANTENNA AT FAULT. REMOVED AND REPLACED RADAR ANTENNA, PERFORMED OPS CHECKS GOOD. Jul 22, 2008 · N808EA · Boeing 727225 · Weather Radar SystemSDR C8G2008F00012Smoke Detector · inoperativeDURING CLIMB OUT OPERATION, THE MAIN DECK FIRE WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE LT WARNING LIGHT ILLUMINATED STEADY. VERIFIED THAT NO SMOKE OR FIRE WAS PRESJul 17, 2008 · N808EA · Boeing 727225 · Smoke DetectionSDR 08FDEA02942Stringer · crackedLT WING STATION 686.5 STRINGER S-10 S CRACKED REPAIRED STRINGER S-10, AT STA 686.5 WITH REPAIR KIT 65C26139-12 REF EO NR 7-5710-7-4322 PT 1, THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 16, 2008 · N467FE · Boeing 727225 · Wing, Longeron/StringerSDR 08FDEA02861Retainer · crackedLT WING TE FLAP WELL LWR PNL BULB SEAL RETAINER IS CRACKED 15 INCHES OUTBOARD OF NR 2 FLAP TRANSMISSION (MKD). REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED RETAINER REF DWG 65-21658 AND GMM 7-0-1001. INSTALLED SEAL RETAINER REF SRM 51-30-2 AND IDENTIFIJul 14, 2008 · N467FE · Boeing 727225 · Trailing Edge FlapsSDR 08FDEA02842Spar · corrodedCORROSION ON LT HORIZ STAB FRONT SPAR UPPER CHORD, STAB STA 4.5 BLENDED CORROSION, ORIGINAL THICKNESS IS .120 INCHES. MATERIAL REMOVED .052 INCHES. MATERIAL REMAINING .088 INCH REPAIRED UPPER CHORD REF EA NR 7-5510-114204 DATED 7-11-08. THIS IS CLASSIFIED AJul 12, 2008 · N467FE · Boeing 727225 · Horizontal Stabilizer, Spar/RibSDR 08FDEA02840Spar · corrodedCORROSION ON LT HORIZ STAB REAR SPAR LOWER CHORD, STAB STA 108.5 BLENDED CHORD, ORIGINAL THICKNESS .110 INCH, MATERIAL REMOVED .027 INCH MATERIAL REMAINING .083 INCH. REPAIRED CHORD REF EA 7-5510-114006 DATED 7-11-08. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N467FE · Boeing 727225 · Horizontal Stabilizer, Spar/RibSDR 08FDEA02838Channel · crackedGENERATED BY EO NR 7-5710-7-4322 RT WING, STA 686.5 WEB FWD ATTACH "Z" CHANNEL CRACKED, OUTBD. REMOVED DAMAGED "Z" CHANNEL, LOCATED AND DRILLED NEW "Z" CHANNEL AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS A MINOR REPAIR.Jul 12, 2008 · N467FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA02837Bracket · misalignedRIGHT WING TANK UNIT (PROBE) CONTACTING STRINGER 11 REPAIR AT WS 686.5. FABRICATED NEW QUANTITY INDICATOR BRACKET AND INSTALLED. REF EA NR 7-5710-114010. THIS IS CLASSIFIED AS A MAJOR.Jul 12, 2008 · N467FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA02833Stringer · crackedGENERATED BY EO 7-5710-7-4322 RT WING STA 686.5, VENT STRINGER STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS REF EO NR 7-5710-7-4322. CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N467FE · Boeing 727225 · Wing, Longeron/StringerSDR 08FDEA02811Stringer · crackedSTRINGER 5R CRACKED BOTH IND/UPPER AND INB/LOWER FLANGES AT STA 340 FWD LAV AFT WALL MOUNTS REMOVED DAMAGED SECTION OF STRINGER, FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS REF PART 1 OF EA 7-5310-113998. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 10, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 08FDEA02788Skin · chafedCHAFE MARKS ON FUSELAGE SKIN FROM WING-TO BODY FAIRING ATTACH SCREWS, RT SIDE OF FUSELAGE BS 950D 9 TO 950D 12 BLENDED OUT DAMAGE. REF SRM 53-30-1 DETAIL 1. ORIGINAL THICKNESS .140 INCH, REMOVED .037 INCH REMAINING THICKNESS .103 INCH OUT OF LIMITS. REF SRJul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02787Skin · chafedHEAVY CHAFE MARK FROM WING-TO-BODY FAIRING ON RT SIDE OF FUSELAGE AT BS 950D 10 TO 950D 13 WL 197 BLENDED DAMAGE REF SRM 53-30-1. ORIGINAL THICKNESS .140 REMOVED .038 AT DEEPEST BLEND OUT REMAINING MATERIAL .102 MATERIAL LOSS OUT OF LIMITS REF SRM 51-30-1. Jul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02786Skin · gougedEXTERIOR FUSELAGE SKIN RT SIDE AT BS 950E 1 INCH STR S-18R 4 INCH SKIN IS GOUGED. REMOVED DAMAGE REF SRM 53-30-1. NDT'D ORIGINAL MATERIAL THICKNESS .140. REMOVED .044 .096 MATERIAL REMAINING. REPAIRED ON N00256. THIS IS CLASSIFIED AS A MAJOR REPAIR. MAJul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02785Skin · wornLT LOWER FUSELAGE JUST FWD OF LT LANDING LIGHT, BS 727D 14 STR19L, SKIN LAP HAS WEAR REMOVED DAMAGED AREA. REMOVED INTERNAL REPAIR, FABRICATE SKIN DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR. REF SRM 53-30-3 FIG 5, SRM 51-30-02 PG 1-10. THIS IJul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02784Stringer · crackedLT FUSELAGE OVERWING BS 945, STR18A (L) REMOVED DAMAGED SECTION OF LT S-18A, INSPECTED SKIN AREA UNDER REMOVED STRINGER SECTION AND FUSELAGE SKIN (NO DEFECTS NOTED). DRILLED HOLES IN REPAIR ANGLES, FABRICATED SHIMS AND INSTALLED ALL REPAIR PARTS. REFERENCE EJul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 08FDEA02779Crease Beam · crackedFUSELAGE OUTER CREASE BEAM CHORD (STR 17L) CRACKED REMOVED CREASE BEAM CHORD, STR 17L, FROM STE 620 TO STA 663. VERIFIED MATERIAL TO BE BAC1506-1133 7075-T-6, ATAG NR A00531. LOCATED AND DRILLED FASTENER HOLES IN NEW CHORD. TREATED AND PRIMED NEW CHORD. INJul 9, 2008 · N467FE · Boeing 727225 · Fuselage Main, StructureSDR 08FDEA02756Bulkhead · crackedFUSELAGE STA 1183 BULKHEAD RT LOWER MIDDLE FLOOR WEB CRACKED. REF EO 7-5320-7- 310 PT 1. REPLACED WEB AND ANGLE REF SRM 51-30-02 PG 4.Jul 8, 2008 · N467FE · Boeing 727225 · Fuselage Main, BulkheadSDR 08FDEA02755Frame · crackedCRACK IN MAIN FRAME STA 380, BETWEEN STRINGER 7R AND RIGHT FWD DOOR, CUTOUT FRAME. REPAIRED FRAME REF SRM 53-10-4 FIG 2, REMOVED AND REINSTALLED DOOR TRIM AND DOOR TRIM SUPPORT REF SRM 51-30-02 PG'S 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 8, 2008 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR 08FDEA02754Stringer · corrodedCABIN S3L HAS CORROSION FROM BODY STA 720A-740 REMOVED CORROSION FROM STA 720A - 740 STR 3L. MATERIAL THICKNESS .045 AND .056, MATERIAL LOSS .008 TO .015 ALL AREAS OUT OF LIMITS. REMOVED DAMAGED STR 3L STA 720A 12 TO 740. REMOVED AND REINSTALLED STR 3L CLIPJul 8, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 08FDEA02751Retainer · crackedMAIN DECK GILL LINER RETAINER RAIL, HOLE CRACKED, BS 1170 STR 8R REMOVED GILL LINER RETAINER RAIL, DRILLED UP NEW RETAINER RAIL, AND INSTALLED NEW RETAINER RAIL, IN REF TO SRM 51-30-2 PG 1-15 AND SRM 51-30-5 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 8, 2008 · N467FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR CA080707002Indicator · broken(CAN) AFTER TAKE-OFF WHEN RETRACTING FLAPS THE INBD FLAPS STUCK AT APPROXIMATELY 5 DEGREES WITH AN ASYMMETRY. THE ACFT DECLARED AN EMERGENCY WITH A FLAP PROBLEM AND RETURNED TO CYYC. THE ACFT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING WAS CARRIED OUT ANDJul 5, 2008 · Boeing 727225 · Trailing Flap Position Indicating SystemSDR 08FDEA02713Retainer · corrodedLT WING LOWER T/E PANEL SEAL RETAINER IS CORRODED WS 167 TO 222 JUST AFT OF AFT SPAR LWR CHORD FABRICATED NEW, 2 EA SEAL RETAINERS ON LT WING LOWER T/E PANEL FROM WS 162 TO 222. REF DWG 65-21656-88, TREATED, PRIMED, AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-3Jul 5, 2008 · N467FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA02712Skin · wornBLENDED AREA LT LOWER FUSELAGE AFT WING TO BODY FAIRING OUT OF LIMITS. DAMAGE AT FR 950F AND 3.5 INCH FWD AND BELOW STR 25L AND INCH OF FR 950F ON STR 25L. REPAIRED BY INSTALLING A DOUBLER REF SRM 53-30-3 FIG 5. REMOVED AND REINSTALLED WING TO BODY PANEL REJul 5, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02711Web · crackedFUSELAGE 1183 BULKHEAD LT SIDE LOWER OTBD FLOOR WEB CRACKED REMOVED DAMAGED PART (DITCHING PAN AND ANGLE ). FABRICATED, HEAT TREATED, ALODINED, PRIMED AND INSTALLED IAW REF SRM 51-30-02 51-10-02, 51-20-5. BOEING DWG 65-29567 THIS IS CLASSIFIED AS A MINOR Jul 5, 2008 · N467FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 08FDEA02710Skin · damagedRT EXT FUSE SKIN IS GOUGED FROM CONTACT WITH FASTENER TAIL BS 950D 11 INCHES, STR 26R.Jul 5, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02709Stringer · corrodedCABIN S-6L LOWER SURFACE HAS CORROSION BETWEEN BS 720A AND 720D REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REF SRM 53-10-1 FIG 1. REMOVED DAMAGE SECTION OF STRINGER REF SRM 53-10-3, PG 6. VERIFIED ALL REPAIR MATERIALS. REF A TAG A93213, AND A48139. ALLJul 5, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 08FDEA02652Frame · damagedTOOLING DAMAGE AT STA 783 FRAME JUST I/B OF STR 4R REMOVED DAMAGE PER SRM 53-10-4. FABRICATED REPAIR PARTS PER SRM 53-10-4. TREATED AND PRIMED PER SRM 51-30-02. INSTALLED REPAIR PER SRM 51-30-02 PG 1-13 AND 53-10-04. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 3, 2008 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR 08FDEA02649Door Frame · crackedFWD GALLEY DOOR LWR AFT CORNER CRACKED REMOVED FWD GALLEY DOOR AND OPENED UP LOWER AFT INNER SKIN FOR ACCESS. REMOVED LOWER AFT STOP FITTING REMOVED PRESSURE SEAL, LOWER GATE, AFT LOWER SEAL RETAINER, REMOVED DAMAGE SECTION OF FRAME, AND DRILLED AND INSTALLEJul 3, 2008 · N467FE · Boeing 727225 · Galley DoorsSDR 08FDEA02637Stringer · corrodedLOWER SIDE SURFACE ON STR 8L AT 720A 10 INCH TO FS HAS AREAS OF SURFACE CORROSION REMOVED CORROSION BY BLENDING, NDT FOUND BLENDED AREA TO BE WITHIN LIMITS WITH ORIGINAL BEING .045". BLENDED AREA TO BE AT .041' ON LOWER SURFACE ON STR 8L AT FS 720A 10 INCHES Jul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 08FDEA02634Skin · wornLT LOWER FUSELAGE WING TO BODY FAIRING BLENDED AREA OUT OF LIMITS. DAMAGE AT LAP JOINT STR 26L - 2.6' FWD OF FR 950E AND DAMAGE AT 2.7L BELOW STR 26L REMOVED AND REINSTALLED FAIRING SUPPORT, REMOVED DAMAGE AREA, OUT OF LIMITS. FABRICATED DOUBLER AND STRUCTURJul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA02633Web · crackedLEFT WING INBD T/E NR 4 JACKSCREW/ELEPHANT EAR FAIRING. CRACKED AT UPPER AFT INBD CLOSER WEB INSTALLED DOUBLER AND FILLER REF SRM 51-40-2 PG 6, THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 2, 2008 · N467FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA02631Crease Beam · crackedMID CABIN CREASE BEAM WEB CRACKED AT STA 945, LBL 47, WL 208. REPLACED WEB REF SRM 51-30-02 PG 6, DRAWING NR 65-21905. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, StructureSDR 08FDEA02629Angle · corrodedPANEL NR 3338 HAS FRETTING CORROSION AROUND EDGE AT MOUNT HOLE. REMOVED CORROSION, ORIGINAL THICKNESS .036". REMOVED .010", .026" REMAINING. MATERIAL IS OUT OF LIMITS REF SRM 53-10-1 PG 1 DETAIL 1. FABRICATED NEW STIFFENER ANGLE 7075-O- .040, HEAT TREATEDJul 2, 2008 · N467FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 08FDEA02628Skin · delaminatedLEFT WING INBD TE MID FLAP S/N BN 492 HAS LWR SURFACE DELAM AT 3 INCH FWD OF AFT EDGE AND 20 INCH THROUGH 336 INCH OB OF INBD END. REPLACED MID FLAP, NEW SERVICEABLE MID FLAP. INSTALLED ON W/C 75C075-00, THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 2, 2008 · N467FE · Boeing 727225 · Trailing Edge FlapsSDR 08FDEA02627Fitting · corrodedLOWER FUSELAGE, CORROSION ON TIE FITTING, STA 337 EXTIOR RBL 17", BELOW LANDING GEAR DRAG BRACE FITTING SUPPORT BEAM. REMOVED AND REPLACED TIE FITTING STA 337, RBL 17 BELOW AND 13-14.Jul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, Attach FittingsSDR 08FDEA02626Keelbeam · corrodedLOWER FUSELAGE INTERIOR OF KEEL BEAM, BS 760 TO 761, LBL 5 TO RBL5, WL 146, TO WL 146, KEAL BEAM FRAME T LOWER ATTACH ANGLE CORRODED. REMOVED DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER 65-23555-67, PER REF SRM 51-30-02 PG 1-15. THIS IS CLASSIFIED AJul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, KeelSDR 08FDEA02624Frame · damagedTWO DRILL STARTS AT AFT LIP OF STA 740 FRAME BETWEEN STR 7R AND 8R. REMOVED DAMAGE .197 REMOVED FROM EDGE .200 INCH ALLOWED WITHIN LIMITS REF SRM 53-10-1 FIG 1 DETAIL 7, AND EA NR 7-5310-11400, THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR 08FDEA02619Stringer · corrodedCABIN S-2L HAS CORROSION FROM BS 720A - 740 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE SECTION, INSTALLED REPAIR AND RESTORED STRINGER TO ORIGINAL FINISH IAW REF SRM 53-10-01 AND 53-10-3 AND 53-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 2, 2008 · N467FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2008F00004Structure · crackedNON-ROUTINE 068119 LT WING NR 3 I/E SLAT AT INBOARD TRACK HAS CRACK IN SKIN AT RADIUS. THIS IS A MINOR REPAIR. STOPPED DRILLED CRACK AND INSTALLED REPAIR DOUBLER. ALL WORK ACCOMPLISHED IAW SRM 51-40-2. NON-ROUTINE 068125 LT WING NR 3 I/E SLAT AT OUTBOARD TJul 1, 2008 · N748DH · Boeing 727225 · Leading Edge DevicesSDR 08FDEA02582Support · corrodedDOT 9 AFT PIT, RT Z-ANGLE, LOWER SURFACE CORRODED AROUND TIE DOWN FITTING, LOCATED STA 1030 14", RBL 20" TO RBL 22" WATER LINE 149 Z-ANGLE IS REPLACED WITH NEW, P/N 65-57570-2 AND WILL BE INSTALLED ON W/C 5310-7-2354 E2 P1R.Jun 30, 2008 · N467FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 08FDEA02581Frame · damagedMULTIPLE UNFILLED HOLES ON FRAME 804 BETWEEN 4L AND STR 5L INSTALLED DOUBLER ON FRAME REF SRM 51-40-3, THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 30, 2008 · N467FE · Boeing 727225 · Fuselage Main, FrameSDR 08FDEA02579Bracket · corrodedSEAL RETAINER ON SNRM NR N00362 IS CORRODED. FOUND BRACKET UNDER RETAINER CORRODED AT WS 167 TO 222 AFT OF SPAR LOWER CHORD. REPLACED BRACKET (STIFFENER) ON NON ROUTINE W/U NR N00362. SEE ITEM NR 16 ON JPF. THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 30, 2008 · N467FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA02578Shear Tie · corrodedLOWER FUSELAGE, CORROSION ON TIE FITTING STA 337 EXTERIOR, LBL17 INCH. BELOW LANDING GEAR SUPPORT BEAM TO DRAG BRACE FITTING. REMOVED AND REPLACED TIE FITTING STA 337 LBL17 BELOW NOSE LANDING GEAR DRAG BRACE FITTING SUPPORT BEAM REF SRM 51-30-2 PG'S 8-9 AND Jun 30, 2008 · N467FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR 08FDEA02575Shim · crackedPANEL RACK, LT WING I/B FLAP ASSY O/B FWD NR 3 FAIRING HAS CRACK ON INTERIOR TAPERED/CHAFF SHIM. REMOVED SHIM AND REINSTALLED NEW SHIM. REF MM 51-51-011-8 PGS 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 30, 2008 · N467FE · Boeing 727225 · Trailing Edge Flaps
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