Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR FDEA201006021802Structure · corrodedCORROSION AT REINFORCEMENT CHORD, BS 1176, MAIN CABIN, LBL 46. REMOVED REINFORCEMENT CHORD BS 1176, LBL 46, IAW SRM 51-30-2 AND FABRICATED NEW REINFORCEMENT CHORD, MATERIAL PN 65-31773-1 DIM: 33" IAW DWG NR 65-31773. INSTALLED NEW REINFORCEMENT CHORD IAW IAW Jun 2, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006011764Fitting · corrodedCORROSION BS 740 FITTING EXTERIOR FUSELAGE KEELBEAM AREA LBL 10. REMOVED KEEL BEAM FITTING AT BS 740 LBL 10 IAW SRM 51-30-2 REV 103 AND FABRICATED FITTING FROM 70750 .190 DIM: 190" X 10 1/4' X 7" IAW DWG 69-43695 OF AND HEAT TREATED TO T6 CONDITION IAW FAS EJun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201006011758Stringer · crackedCRACK AFT END OF STRINGER 27L AT BS 740, AC DISTRIBUTION COMPARTMENT. CUT OUT DAMAGED SECTION OF STR 27L AT BS 740, 11.5" LONG IAW SRM, REV 103, 53-10-3 FIG 1. FABRICATED STRINGER USING BAC 1498-146, 7075-T6, 11.5" LONG AND SPLICE USING BAC1498-131, 7075-T6,Jun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201005311747Angle · crackedCRACKED ANGLE CHORD FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. CUT OUT DAMAGED SECTION OF WEB, 9.5" IAW DWG SR27-57-038, REV C. FABRICATED NEW DOUBLER USING 20245-T3, .050" X 12" X 9.7500" IAW DWG SR27-57-038, REV C. INSTALLED DOUBLER IAW DWG SR27May 31, 2010 · N267FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA201005281703Intercostal · crackedNR 1 CARGO DOORWAY FRAMES, BS 560, BETWEEN STR 23R AND 24R, CRACKED INTERCOSTAL. REMOVED INTERCOSTAL NR 1 CARGO DOOR WAY BS 560 STR 23R - 24R IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL USING 7075 O .063" PO 9009533 DIM 19.7500" X 6.2500" IAW MM 51-20-1 May 28, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201005281704Connector · defectiveCREW PERFORMED AN AIR TURN BACK TO MEM FOR AN UNSAFE INDICATION ON THE NR 3 L/E SLAT. WHEN CREW WENT FROM FLAPS 5 TO 2 THEY HAD AN UNSAFE INDICATION ON NR 3 L/E SLAT. WHEN CREW RETURNED TO FLAPS 5 THE UNSAFE INDICATION WENT AWAY. NR 3 LED UNSAFE WHEN RAISINMay 28, 2010 · N283FE · Boeing 727233 · Flight Control System WiringSDR FDEA201005241637Skin · gougedRT INBD FOREFLAP OTBD END L/E PREVIOUS REPAIR, GOUGED. REMOVED PREVIOUS REPAIR ON RT INBD FOREFLAP OTBD END IAW SRM 51-30-2 FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 1, REV 102. INSTALLED NEW REPAIR IAW SRM 51-30-2.May 24, 2010 · N268FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201005221733Rib · crackedRIB CRACKED AT OTBD TRACK OF NR 6 SLAT REMOVED RIB IAW SRM 51-30-2. FABRICATED NEW RIB FROM 2024-0 .050" DIM 15" X 6" IAW SRM 51-20-1 AND 57-50-2. HEAT TREATED PART FROM 2024-0 TO 2024T4 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A INSTALLED RIB IAW SRM 51May 22, 2010 · N268FE · Boeing 727233 · Wing, Rib/BulkheadSDR FDEA201005201595Angle · crackedNR 6 SLAT LOWER AFT T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED ACCESS PANELS NR 6 SLAT IAW SRM 51-30-2, FABRICATED NEW T/E ANGLE. MATERIAL USED BAC1514-1559 2024T3511 PO 20035137 DIM 9' 6" LONG IAW SRM 57-50-2 FIG 2, 51-30-5 TREATED AND PRIMED IAWMay 20, 2010 · N268FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201005201594Angle · crackedNR 8 SLAT LOWER T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED NR 8 SLAT LOWER T/E ANGLE IAW SRM REV 102, 51-30-2. FABRICATED NEW ANGLE USING BAC1514-1559, 2024 T3511 86 1/4" LONG IAW SRM 51-30-5 AND 57-50-2 FIG 2. INSTALLED NEW ANGLE IAW 51-30-2.May 20, 2010 · N268FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201005191583Stiffener · damagedBULKHEAD 1183 HORIZONTAL CHORD AT WL 190 BETWEEN LBL 4 AND RBL 6 HAS NUMEROUS HOLES WITH NO SPACING. CUT OUT, WEB DIM. 29" X 7" AND HORIZ CHORD DIM. 9" IAW EA 7-5310-135541 AND SRM 51-10-1. FABRICATED WEB FROM 7075T6 .063" DIM. 51.38" X 17.60", VERTICAL LEG SMay 19, 2010 · N268FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA201005191582Stringer · corrodedSTRINGER CORRODED ON STR 27L AT BS 950F, 10". CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 19", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 19", SPLICE USING BAC1498-131 7075T-6 DIMS 14" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AND 51-10-2.May 19, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201005171769Beam · damagedAFT PIT BS 1183, VERTICAL BEAM AT LBL 17.8 HAS FASTENERS WITH ZERO SPACING. TRIMMED OUT BEAM AFT FLANGES AND BULKHEAD WEB 8 PLACES IAW EA 7-5310-135541. FABRICATED REPAIR DOUBLER, REPAIR ANGLES, FILLERS, BULKHEAD WEB FILLERS, STRAP DOUBLER, STIFFENER SHIMS, May 17, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201005171748Doubler · gougedGOUGES ON INNER DOUBLER BS 620, STR 16L. TRIMMED OUT DAMAGED AREA DIM. 1.75" X 1" IAW EA 7-5330-135544. FABRICATED FILLER FROM 2024T3 .125" DIM. 1.75" X 1" AND DOUBLER FROM 2024T3 .125" DIM. 4.75" X 3.75" IAW EA 7-5330-135544. INSTALLED REPAIR PARTS IAW SRM May 17, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005141731Skin · gougedGOUGES IN MCD INNER DOUBLER SKIN STA 620-640 STRINGERS 5L - 8L REMOVED INNER WEB SKIN IAW P-F SRM 51-30-2. FABRICATED INNER WEB SKIN FROM 2024T3 .125" DIM. 80" X 48" IAW P-F SRM 53-10-2. INSTALLED INNER WEB SKIN IAW P-F SRM 51-30-2.May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005141592Stringer · corrodedCORROSION ON STRINGER 27L AT BS 985. CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 15.5", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 15.5", SPLICES USING BAC1498-131 7075T-6 DIMS 13.7500" AND 10.2500" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AMay 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201005141591Stringer · corrodedCORROSION ON STRINGER 27L AT BS 950B 5". CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 18", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 18", SPLICES USING BAC1498-131 7075T-6 DIMS 13" AND 12.5" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AND 51-May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR PCSA2010051801Check Valve · leakingWHEN THROTTLES RETARDED FOR DESCENT A STRANGE ODOR IS DETECTED FOLLOWED BY A HAZE. THEN A SHORT BURST OF SMOKE. LEFT AND RIGHT PACK TEMPS 40 DEGREES. ADVANCED AND RETARDED 1 AND 3 THROTTLES. MORE SMOKE APPEARED AFTER NR 1 THROTTLE ADVANCED AND RETARDED. MMay 14, 2010 · N994AJ · Boeing 727233 · Hydraulic System, MainSDR FDEA201005141531Switch · misinstalledON CLEAN UP OF FLAPS. NR 1 PORT L/E FLAPS WOULD NOT RETRACT FROM 5 DEGREES TO 2 DEGREES POSITION. GSP U TRIED JUMPER PLUG NO HELP. ON FURTHER TROUBLESHOOTING FOUND WEAR MARKS WHERE SWITCH LINKAGE WAS CONTACTING AIRFRAME. NR1 L/E FLAP SWITCH IMPROPERLY INSTMay 14, 2010 · N266FE · Boeing 727233 · Leading Edge Slat Control SystemSDR FDEA201005131619Door Frame · crackedL-1 ENTRY DOOR FRAME, STA 303.9, STR 16L, CRACK ON WEB CUTOUT. CUTOUT AREA ON WEB DIM 1.25" X .70" AT BS 303.9 AT STR 16L IAW FEDEX EO 7-5310-7-3362 P7. DRILLED AND LOCATED PARTS FROM FEDEX KIT P/N 5314757 IAW SRM 51-30-5. INSTALLED WEB REPAIR AT BS 303.9 AMay 13, 2010 · N268FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA1005121525ABulkhead · crackedCRACK FOUND AT BS 1183 BULKHEAD WEB AT RBL 24 WL 170 CUT OUT WEB DIM. 2.8750 " X 1.3750 " IAW EA 7-5310-135543 AND SRM 51-10-1. FABRICATED FILLER FROM 2024T3 .050" DIM. 2.7500" X 1.3750", FABRICATED DOUBLER FROM 2024T3 .071" DIM 7" X 6", FABRICATED FILLER FROMMay 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA201005121523Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REMOVED LOWER CHORD DIM. 20.5", WEB AND DOUBLER IAW DWG NR SR 27-57-038, REV C. FABRICATED 2 ANGLES FROM 7075-0 .071" DIM. 14.5" X 2.75" AND 12.5" X 2.75" IAW DWG NR SR 27-57-038 REV C. HEAT TREATED ANGLES FROM 7May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR FDEA201005121590Skin · damagedMAIN CARGO AREA, BS 660, STR 3L-4L, DOUBLE DRILLED HOLES ON BONDED STRAP. CUT OUT AREA DIM. 1.5" X 3.5" AND 1" X .75" IAW SRM 53-30-3. FABRICATED FILLER FROM 2024T3 .090" DIM. 19.5" X 8", DOUBLER FROM 2024T3 .080" DIM. 17.6" X 11.5", TRIPLER FROM 2024T3 .May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005121589Skin · damagedMAIN CARGO DOOR AREA, BS 660, STR 3L, NOT ENOUGH DISTANCE BETWEEN FASTENERS. CUT OUT AREA DIM, 2.75" IAW SRM 53-10-3. FABRICATED STRINGER SECTION FROM BAC-1498-139-7075T6 DIM. 2.75", 2 SHIMS FROM 2024T3 .080" DIM. .75" X 4", PLATE FROM 2024T3 .125" DIM 13" X May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201005121525ABulkhead · crackedCRACK FOUND AT BS 1183 BULKHEAD WEB AT RBL 24, WL 170.May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA201005121525Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118.May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR FDEA201005121521Spar · crackedLT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REPAIRED LT WING T/E FALSE SPAR CHORD WBL 118 IAW DWG NR SR27-57-038, REV C.May 12, 2010 · N268FE · Boeing 727233 · Wing SparSDR 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 FDEA201004141182Manifold · failedAFTER T/O NR 1 ENG FIRE LIGHT ON NR 1 FIRE DETECT LOOP. PWR REDUCED ON NR 1 ENG IAW QRH. NR 1 FIRE LIGHT WENT OUT. FIRE DETECT LIGHT REMAINED ON. FIRE DETECT LIGHT OUT WHEN FIRE HANDLE PULLED. NO OTHER ABNORMAL INDICATIONS NOTED. R & R FUEL HEAT MANIFOLD. Apr 14, 2010 · N278FE · Boeing 727233 · Fuel HeaterSDR FDEA201004141180Fire Loop · false activationAFTER T/O NR 1 ENG FIRE LIGHT ON NR 1 FIRE DETECT LOOP. POWER REDUCED ON NR 1 ENG IAW QRH. NR 1 FIRE LIGHT WENT OUT. FIRE DETECT LIGHT REMAINED ON. FIRE DETECT LIGHT OUT WHEN FIRE HANDLE PULLED. NO OTHER ABNORMAL INDICATIONS NOTED. TRACKING NR 10-1182.Apr 14, 2010 · N278FE · Boeing 727233 · Fire DetectionSDR FDEA201003170859Actuator · failedNR 1 LED FAILS TO RETRACT BETWEEN 5 AND 2 DEGREES. INSTALLED JUMPER AND NO HELP. AMBER LIGHT STAYED ON IN RETRACT POSITION. R & R NR 1 L/E SLAT ACTUATOR IAW AMM 27-81-032-4. LEAK AND OPS CHECK NORMAL. L/E FLAP LIGHT OUT. RETURN TO SERVICE. PREMATURE REMOMar 17, 2010 · N284FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA201003160838Transmitter · failedHYD SYS A QTY WENT TO ZERO WHEN GEAR RAISED AFTER TAKEOFF. PRESSURE REMAINED STEADY AT 3000 PSI. LOWERED GEAR NORMALLY QTY INDICATION RETURNED TO NORMAL AS GEAR CAME DOWN. GEAR FLAPS & SPOILERS WORKED OK. RAN QRH CK LIST WITH NO AFFECT. RELEASED FOR SERVIMar 16, 2010 · N275FE · Boeing 727233 · Hydraulic Quantity IndicatorSDR FDEA201003140819Valve · unknownSHORTLY AFTER T/O HEARD LOUD POP. OBSERVED FLUCTUATING EPR ON ENG NR 2 WITH OIL TEMP APPROX 115 DEGREES C. RESTARTED NR 2 ENG AT REDUCED POWER SETTING REMAINDER OF FLIGHT WITH NORMAL INDICATIONS INCLUDING NORMAL OIL TEMP. INSPECTED INLET AND EXHAUST OF NR 2Mar 14, 2010 · N286FE · Boeing 727233 · Engine Bleed Air SystemSDR FDEA201003110775Manifold · shearedAFTER TAKEOFF WITH STANDARD POWER SET, NR 3 ENGINE FIRE WARNING ALARM. ENGINE WAS SHUTDOWN IAW QRH FIRE LIGHT WENT OUT WITH START LEVER TO CUT OFF. GOOD FIRE WARNING TEST. FOUND SEVERED TUBING COMING TO FUEL HEATER S/O VALVE INLET PORT. ALSO FOUND GROUNDING Mar 11, 2010 · N223FE · Boeing 727233 · Fire DetectionSDR FDEA201003100769Landing Gear · malfunctionedON DEPARTURE RETRACTED GEAR AND RT GEAR DOWN AND RT GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED RED TABS TO NO AVAIL. PERFORMED VISUAL INSP OF THE RT MLG, NO GEAR PIN INSTALLED, NO OBVIOUS DEFECTS NOTED. DEBRIEFED CREW, GEAR DOOR INDICATION WAS CORRMar 10, 2010 · N265FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR FDEA201003050653Seat Track · corrodedUPON REMOVAL OF FLOORBOARD TO ACCESS MLG SIDE STRUT AFT BRG, FOUND SEAT TRACK CORRODED AT STA 950, 12 REMOVED DAMAGED SEAT TRACK SECTION FROM BS 950+ 10 TO BS 950B+10 LBL 24, FABRICATED NEW SEAT TRACK SECTION AND SPLICES, INSTALLED NEW SEAT TRACK SECTION ANDMar 5, 2010 · N220FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002130419Inlet · obstructedLT AND RT PACK "TRIP OFF" LIGHTS W/ "DUCT OVER" LIGHT. ON POST FLIGHT, PACK COOLING DOOR FILLED WITH SNOW. INSPECTED PACK INTAKES AND FOUND SNOW PACKED INSIDE. MELTED SNOW FROM PACK INLET AREA. OPERATED PACKS IAW MM 21-61-000-5 AND 21-55-000-5. OPS CHECK Feb 13, 2010 · N273FE · Boeing 727233 · Cabin Cooling SystemSDR FDEA201002090366Engine · power lossDURING STANDARD PWR TAKEOFF AT 2000 FT, EXPERIENCED SUDDEN VIBRATION IN CTR PEDESTAL ACCOMPANIED BY ABNORMAL NOISE. DISCOVERED RETARDING NR 2 THROTTLE RESOLVED VIBRATION. ALL ENGINE INDICATIONS NORMAL. ENG HAS BEEN APPROVED FOR REMOVAL BY POWERPLANT ENGINEFeb 9, 2010 · N286FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 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 FDEA201001160168Apu · malfunctionedSHORTLY AFTER APU SHUTDOWN, AFT LOWER CARGO SMOKE ILLUMINATED, BOTTLE NR 1 DISCHARGED, (JUST BEFORE BOTTLE NR 1 DISCHARGED, TUG DRIVER CONFIRMED SMOKE AROUND BELLY OF ACFT) SUBSEQUENTLY FORWARD LOWER CARGO SMOKE LIGHT ILLUMINATED, THEN DISCHARGED BOTTLE NR 2. Jan 16, 2010 · N285FE · Boeing 727233 · APU Core EngineSDR PCSA2010011301Fire Warning · malfunctionedAFTER GEAR RETRACTION RECEIVED APU FIRE WARNING. FOLLOWED AMJ PRECEDURES. MAINTENANCE ACCOMPLISHED AN APU INSPECTION. NO SIGNS OF FIRE NOTICED. OPERATIONAL AND FUNCTION CHECKS WERE PERFORMED PER THE AMM ALL OK. THE APU FIRE BOTTLE WAS REPLACED.Jan 11, 2010 · N395AJ · Boeing 727233 · Fire DetectionSDR FDEA200912304566Shutoff Valve · failedAFTER TAKEOFF IN OUR NORMAL CONFIGURATION CABIN STARTED UP A HIGHER THAN NORMAL RATE. AFTER CLOSING THE CABIN OUT FLOW VALVE AND TURNING ON THE RT PACK, CABIN RETURNED TO NORMAL UNTIL WE REACHED 26,000' AT WHICH TIME THE CABIN WAS CLIMBING AT 800'/MIN, SAME ADec 30, 2009 · N223FE · Boeing 727233 · Cabin Cooling SystemSDR FDEA200912244513Actuator · failedON FLAP RETRACTION FROM 5 TO 2 DEGREE THE NR 5 SLAT WOULD NOT RETRACT. THE OTBD AND INBD FLAP NEEDLES TRAVEL FURTHER INTO THE WHITE BAND WHEN OPS TESTED ON THE GROUND. AIRPLANE FLEW WITH NO SIGNIFICANT ROLL. REPLACED NR 5 SLAT ACTUATOR REF AMM 27-81-032-4. Dec 24, 2009 · N264FE · Boeing 727233 · Trailing Edge Flap ActuatorSDR FDEA200912104399Door Frame · damagedFWD ENTRY DOOR FRAME STA 303.9 WEB CUT-OUT AT STR 15L HAS TOOLING MARK ON INBD EDGE. TRIMMED OUT GOUGE AREA AND INCREASED CORNER RADIUS, TREATED AND PRIMED IAW EA NR 7-5310-135516.Dec 10, 2009 · N264FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200912094415Skin · crackedRT FWD OVERWING HATCH UPPER EDGE EXT SKIN IS BENT OUT AND CRACKED AT FASTENER. STOP DRILLED CRACK IAW IAW SRM 52-00-3 FIG 4. FABRICATED NEW DOUBLER IAW SRM 52-00-3 FIG4. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER ON RT FWD OVERWING HATCDec 9, 2009 · N264FE · Boeing 727233 · Emergency ExitsSDR FDEA200912094393Seat Track · corrodedSURFACE CORROSION ON SEAT TRACK INBD FLANGE BETWEEN BS 1130 TO BS 1110 RBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK SECTION & INSTALLED NEW SEAT TRACK FROM BS 1010 - 1130 RBL 45 IAW SRM 53-10-1 FIG 3, SRM 51-30-2 & SRM 51-10-2 & SRM 53-10-5Dec 9, 2009 · N264FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912094391Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720A AFT SIDE BETWEEN STRINGERS 28R AND 27R. CUT-OUT DAMAGED AREA OF SHEAR TIE. FABRICATED SHEAR TIE REPAIR AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4, FIG 15, REV 101 AND SRM 51-30-2.Dec 9, 2009 · N264FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA200912084384Skin · damagedLT ELEVATOR OTBD LWR SKIN DAMAGED AT STATIC WICK BASE, ELEV STA 215. FABRICATED DOUBLER REPAIR ON LT ELEVATOR OTBD LOWER SKIN AT STATIC WICK BASE IAW SRM 55-20-3, INSTALLED REPAIR PARTS, DOUBLER AND FILLER IAW SRM 51-30-2, REV 101.Dec 8, 2009 · N264FE · Boeing 727233 · Elevator, Plate/SkinSDR FDEA200912054398Structure · corrodedCORROSION ON CHORD AT STA 1176, LBL 65 TO RBL 65. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-31773-1 PO NR 2911891 AND INSTALLED IAW SRM 51-10- 6, 53-10-1, 53-10-2 AND 51-30-2.Dec 5, 2009 · N263FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200912044361Seat Track · corrodedCORROSION ON SEAT TRACK FLANGES RBL 24 BETWEEN BS 1130 TO BS 1183. REMOVED SECTION OF SEAT TRACK IAW SRM 51-30-2, REV 101, FABRICATED NEW SEAT TRACK SECTION IAW DWG 53FX976, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-30-5 AND DWG 53FX976, TREATED AND PRIDec 4, 2009 · N264FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
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