Boeing 727-2S2F

Service difficulty reports · 842

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272S2F'
  ORDER BY difficulty_date DESC"

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SDR FDEA201109113826Web · damagedL1 DOOR INTERIOR WEB DAMAGED, INSIDE SECOND LIGHTNING HOLE FROM BOTTOM NEAR CRNTER OF DOOR BS 328. DAMAGE OUT OF LIMITS IAW SRM 52-00-2. REMOVED WEB IAW SRM 51-30-2. FABRICATED NEW WEB IAW SRM 52-10-1 FIG 1, 51-30-5 AND 51-20-1 FIG7. INSTALLED REPAIR PARTSep 11, 2011 · N211FE · Boeing 7272S2F · Passenger/Crew DoorsSDR FDEA201109113992Door · unsecureUPON LANDING THE FWD ENTRY LIGHT ON THE SO DOOR WARNING PANEL ILLUMINATED. UPON INSP, CREW FOUND CREW ENTRY DOOR TO BE OPEN AND UNSECURED. PERFORMED ADJUSTMNET TEST REF AMM 52-11-001-5. NO DEFECTS NOTED. OK FOR SERVICE.Sep 11, 2011 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR FDEA201109103824Transmitter · failedON TAKEOFF ROLL, RECEIVED NO EPR ON NR 3 ENGINE. SET POWER ON EXPECTED N1. AS ACFT ACCELERATED EGT GRADUALLY ROSE INTO CAUTION ZONE CAUSING A REJECTED TAKEOFF. REMOVED AND REPLACED EPR TRANSMITTER PER AMM 77-11-011-4. OPS CHECKED FAILED.Sep 10, 2011 · N207FE · Boeing 7272S2F · Engine Pressure Ratio (EPR)SDR FDEA201109103823Skin · gougedRT WING, NR 7 SLAT OTBD HOOK AREA HAS GOUGE ON T/E SKIN OTBD SIDE. REMOVED DAMAGED DOUBLER IAW SRM REV 103 51-30-2 FABRICATED DOUBLER AND INSTALLED IAW SRM 57-50-3 FIG 10.Sep 10, 2011 · N211FE · Boeing 7272S2F · Leading Edge DevicesSDR FDEA201109093811Rib · crackedLEFT WING NR 3 SLAT INBOARD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED CRACKED RIB IAW SRM 51-30-2 REV 103. FABRRICATED NEW RIB IAW DRAWING 65-17294 AND SRM 51-20-1 FIG.7 INSTALLED NEW RIB IAW SRM 51-30-2Sep 9, 2011 · N211FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR FDEA201109093799Battery Pack · inoperativeDURING STBY POWER CHECK NEITHER EXIT LIGHT ILLUMINATED (INTERIOR) R & R BATTERIES IAW BMM 33-50-101-2, CHECKS NORMALLY. FINAL CLOSED.Sep 9, 2011 · N203FE · Boeing 7272S2F · Emergency LightingSDR FDEA201109083777Rib · crackedLT WING NR 3 SLAT OTBD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED RIB IAW SRM REV 103 51-30-2. FABRICATED NEW RIB IAW DWG 65-17294 AND SRM 51-20-1 FIG 7. INSTALLED NEW RIB IAW SRM 51-30-2 & 51-10-2.Sep 8, 2011 · N211FE · Boeing 7272S2F · Leading Edge DevicesSDR FDEA201109083776Support · corrodedUPPER FUSELAGE INTERIOR, MAIN CARGO DOOR UPPER SILL SUPPORT LOWER SURFACE HAS LIGHT SURFACE CORROSION AT BS 661, STRINGER 2L. REMOVED DAMAGED SILL SUPPORT IAW SRM 51-30-2. FABRICATED NEW SILL SUPPORT IAW SRM 53-10-2, FIG 3 AND 51-20-1, FIG 7. INSTALLED NEW Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR FDEA201109083772Stringer · corrodedUPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 682. REPLACED STRINGER SPLICE.Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201109083771Stringer Splice · corrodedUPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 678 SPLICE. REMOVED SPLICE IAW SRM 51-30-2 REV 103. FORMED NEW SPLICE IAW SRM 53-10-2. INSTALLED NEW SPLICE IAW SRM 51-30-2Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201109083770Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BS 344 LBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED & INSTALLED SEAT TRACK SECTION IAW SRM 53-10-2 FIG. 7.Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109073737Hook And Loop · failedPBE IN AFT CABIN CAME LOOSE ON INITIAL TAKEOFF. REATTACHED HOOK AND LOOP IN REF TO SMP, GOOD FOR SERVICE.Sep 7, 2011 · N217FE · Boeing 7272S2F · Emergency EquipmentSDR FDEA201109063726Skin · corrodedCORROSION ON INNER SKIN AT DRAIN VALVE, FWD. PIT BS 682 - 686, RBL 3.0. CUT OUT DAMAGED AREA IAW SRM REV.103, 53-30-3 FIG 3A. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-3 FIG 3A .Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA201109063725Skin · gougedEXTERIOR SURFACE GOUGE AT BS 520 AT S27L. CUT OUT DAMAGED AREA IAW SRM 53-30-3 REV 103 FIGURE 14. FABERICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER IAW SRM 53-30-3 FIG 14. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA201109063724Stringer · corrodedUPPER FUSELAGE INTERIOR, STRINGER 4 LT HAS CORROSION AT BS 720. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABERICATED REPAIR PARTS IAW SRM 53-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-02.Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201109063723Stringer · corrodedUPPER FUSELAGE INTERIOR, STRINGER 5 LEFT HAS CORROSION AT BS 720A 3 INCHES. CUT OUT DAMAGED AREA IAW SRM REV.103 53-10-3 FIG3 FABRICATED REPAIR STARS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201109043662Stringer · corrodedUPPER FUSELAGE INTERIOR STRINGER 5 LT HAS CORROSION AT BS 702. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABRICATED STRAPS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3.Sep 4, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201109013603Skin · gougedEXTERIOR FUSELAGE, 2 LONG GOUGES UNDER L-1 DOOR. CUTOUT DAMAGE AREA IAW SRM 53-30-3 REV 103 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-30-2 AND 53-30-3 FIG 1.Sep 1, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA201108313717Attach Angle · crackedRIGHT WING, NR 8 SPOILER ACTUATOR SUPPORT FITTING, HAS LOWER LT SIDE ATTACH ANGLE CRACKED AT WBL 120. REMOVED SECTION OF ATTACH ANGLE AND FABRICATED REPAIR PARTS IAW DWG SR27-57-038 REV C. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND DWG SR27-57-038 RAug 31, 2011 · N211FE · Boeing 7272S2F · Wing, Attach FittingsSDR FDEA201108313641Structure · crackedRT WING, INBD FLAP, MID FLAP AFT CHORD IS CRACKED AT 2 EA AREAS, NEAR THE MOST INBD HINGE AND ACTUATING ROD FOR AFT FLAP. CUT OUT DAMAGED AREA IAW SRM 51-40-4 FIG 1. FABRICATED REPAIR FILLER AND SPLICE ANGLE IAW SRM 41-40-4 FIG 1 AND 57-50-2 FIG 5. TREATEDAug 31, 2011 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR FDEA201108303573Web · crackedCRACK IN SIDE WEB AT LIGHTING HOLE RT SIDE AFT VENTRAL STAIRS BS 1239. CUT OUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1.Aug 30, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR FDEA201108303574Web · crackedCRACK IN SIDE WEB AT LIGHTING HOLE LT SIDE AFT VENTRAL STAIR OPENING, BS 1303. CUTOUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-10-1, FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, FIG 1.Aug 30, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR FDEA201108193383Slide · damagedFWD ENTRY DOOR ESCAPE SLIDE, PART OF THE SLIDE DROOPING OUT OF CONTAINER. TROUBLESHOOTING. REMOVED ESCAPE SLIDE FROM ENCLOSURE. SECURED LOOSE ITEMS WITH EXISTING HOOK AND LOOP ON FLAPS. RE-INSTALLED ESCAPE SLIDE INTO ENCLOSURE IAW MM 25-60-015-2. OPS NORMAug 19, 2011 · N211FE · Boeing 7272S2F · Escape SlideSDR FDEA201108033082Light · inoperativeWHILE COCKING ACFT, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP IN ARMED/ON POSITION. REPLACED LIGHT REF MM 33-50-101-2-0. GROUND OPS CK NORMAL AT THIS TIME. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.Aug 3, 2011 · N213FE · Boeing 7272S2F · Emergency LightingSDR FDEA201107182780Line · looseREJECTED TAKEOFF DUE TO LOW N1. ENGINE RUN AFTER RTO. FOUND LINE AT MOISTURE TRAP HOLDING ON BY 1 THREAD. INSPECTED INLET ON NR 1 ENGINE AND FOUND PT2 INLET COMPLETLY PLUGGED WITH DIRT DOBBER NEST. CLEANED SAME. REF MM 77-11-003-2-0. INSTALLED AND SAFTIEDJul 18, 2011 · N215FE · Boeing 7272S2F · Engine Pressure Ratio (EPR)SDR FDEA201107022556Fitting · inoperativeSLIDE FALLS OUT TOO EASILY. REPLACED GIRT BAR PLASTIC CLIPS.Jul 2, 2011 · N211FE · Boeing 7272S2F · Emergency EquipmentSDR FDEA201106142247Actuator · failedNR 2 SLAT FAILED TO RETRACT. RAN QRH AND NO HELP IAW QRH, FLAPS SET TO 5 DEG AND THEN RAN CONFIGURED ON SCHEDULE FOR RTB MEM. DISCONNECTED THE CONNECTOR PLUG ON THE NR 2 LT SLAT ACTUATOR AND LIGHT WENT OUT. REMOVED NR 2 SLAT ACTUATOR AND CHECKED ADJUSTMENT Jun 14, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat ActuatorSDR FDEA201106092182Actuator · failedDURING FLAP RETRACTION, NR 2 SLAT REMAINED IN TRANSIT IAW QRH, EXTENDED FLAPS TO 2 DEGREES. HAD NORMAL INDICATIONS. RETRACTED FLAPS AGAIN AND NR 2 SLAT DID NOT RETRACT. ACFT APPEARED TO FLY NORMAL. NO UNDUE CROSS CORRECTION. INSTALLED NEW NR 2 ACTUATOR PJun 9, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat ActuatorSDR FDEA201106092181Actuator · failedDURING FLAP RETRACTION, NR 2 SLAT REMAINED IN TRANSIT IAW QRH, EXTENDED FLAPS TO 2 DEGREES. HAD NORMAL INDICATIONS. RETRACTED FLAPS AGAIN AND NR 2 SLAT DID NOT RETRACT. ACFT APPEARED TO FLY NORMAL. NO UNDUE CROSS CORRECTION. INSTALLED NEW NR 2 ACCUATOR Jun 9, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat ActuatorSDR FDEA201105111802Stringer · crackedCRACK COMING FROM LOCK FASTENER STR 15L STA 720B 18" NEAR OVER WING LIGHT ASSY MAIN CABIN. CUT-OUT DAMAGED AREA, FABRICATED REPAIR PARTS AT STR 15L BS 720B + 18", AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 5, 51-10-1, AND 51-10-2.May 11, 2011 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201105111804Skin · dentedDENTS 2EA EXTERIOR FUSELAGE STA 1050 BETWEEN STR 16R-17R. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 51-30-2.May 11, 2011 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA201105111800Engine · overheatedNR 2 ENG FIRE LIGHT AT 340, BOTH BOTTLES FIRED AFTER FOLLOWING QRH. FIRE DEPT INDICATED NR 2 ENG HAD SIGNIFICANT HEAT SIGNATURE. R & R NR 2 ENG FIRE SENSING ELEMENTS BOTH BOTTOM & TOP. INSTALLED SQUIBS & FIRE BOTTLES. C/W HIGH POWER RUN.May 11, 2011 · N204FE · Boeing 7272S2F · Engine (Turbine/Turboprop)SDR FDEA201105101793Structure · gougedRIGHT INBD FOREFLAP OUTBD LOWER L/E GOUGED. CUT OUT DAMAGED SKIN IAW SRM 57-30-4 FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 REV 103 AND EA 7-5750-136765May 10, 2011 · N203FE · Boeing 7272S2F · Trailing Edge FlapsSDR FDEA201105101796Line · disconnectedON RUNUP FOR TAKEOFF SET EPR'S AT COMPUTED VALUE. NOMINAL N1'S FOR 2 & 3 ALONG WITH CORRESPONDING EGT & FUEL FLOWS NORMAL. NR 1 ENGINE, WHEN SET TO COMPUTED EPR SETTING FOR T/O HAD ABNORMALLY LOW N1 & FUEL FLOW COMPARED TO ENGINES 2 & 3. NR 1 ALSO VERY SMay 10, 2011 · N217FE · Boeing 7272S2F · Power Indicating SystemSDR FDEA201105091787Stringer · corrodedE AND E COMPARTMENT - STRINGER 28R IS CORRODED AT BS 450 CUT OUT DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR STRINGER SECTION, DOUBLERS AND SHIMS IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER, DOUBLERS, AND SHIMS IAW SRM 53-10-3 FIG 1, REV 10May 9, 2011 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR FDEA201105041931Skin · corrodedFUSELAGE SKIN HAS CORROSION OUTBD OF STR 26R BS 1166 TO 1183. REPAIRED FUSELAGE SKIN S26R BS 1166 TO 1183 IAW EA 7-5330-136759.May 4, 2011 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR FDEA201012304785Indicator · failedREJECTED T/O AT 80 KNOTS. NR 1 EPR GUAGE INOP. RELEASED FOR SERVICE IAW MEL: 77-01-01, "MEL 77-01-01: NR 1 ENGINE EPR INDICATOR - INOP." ACFT OK FOR SERVICE. TO TROUBLSHOOT, FURTHER TROUBLESHOOTING REQUIRED. CODE 'A' ITEM DUE ON OR BEFORE 2-JAN-2011. ACDec 30, 2010 · N207FE · Boeing 7272S2F · Engine Pressure Ratio (EPR)SDR FDEA201012214734Fire Loop · dirtyRECEIVED NR 1 ENGINE FIRE INDICATION ON FINAL APPROACH WITH POWER AT IDLE. SYS TESTED OK & ENGINE WAS SHUTDOWN AND BOTTLE DISCHARGED IAW CHECKLIST. FIRE WARNING SYS STILL DID NOT SILENCE UNTIL ON THE GROUND & NR 1 ENGINE DET "B" CB PULLED. EMERGENCY VEHICLEDec 21, 2010 · N204FE · Boeing 7272S2F · Fire DetectionSDR FDEA201011254486Indicator · failedTHE NR1 EPR GUAGE WAS INOPERATIVE DURING TAKEOFF AND THE TAKEOFF WAS ABORTED, PRIOR TO SETTING TAKEOFF POWER AND REACHING 60 KNOTS. AFTER CLEARING THE RUNWAY AND WHILE TROUBLESHOOTING THE PROBLEM, DURING A JOINT DISCUSSION WITH MX THE NR1 EPR GUAGE STARTED WONov 25, 2010 · N207FE · Boeing 7272S2F · Engine Pressure Ratio (EPR)SDR FDEA201010264168Slide · misalignedDOOR SLIDE PRESSURE GAUGE UNREADABLE. REMOVED AND REPOSITIONED SLIDE IN DOOR COVER REF AMM 25-60-015-2-0.Oct 26, 2010 · N213FE · Boeing 7272S2F · Escape SlideSDR FDEA201010033888Smoke Warning · false activationDURING FLIGHT, LOWER AFT CARGO SMOKE AND ARMED LIGHT ILLUMINATE WITH ASSOCIATED BELL. THIS OCCURED 10 SECONDS AFTER WING ANTI-ICE SELECTED OPEN. LIGHT WENT OUT AFTER THE BOTTLE WAS DISCHARGED AND THE SYSTEM TESTED GOOD. REMOVED FWD/AFT CARGO COMPARTMENT LOct 3, 2010 · N204FE · Boeing 7272S2F · Fire DetectionSDR FDEA201009263714Seat Track · corrodedMAIN CABIN SEAT TRACK AT BS 495 LBL 45 INBD FLANGE LOWER SURFACE IS CORRODED.Sep 26, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009253710Seat Track · gougedAFT CABIN STA 1150-1160 BL0 AFT SEAT TRACK SECTION HAS GOUGES AND DAMAGE AROUND SEVERAL SCALLOPS.Sep 25, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009243705Stiffener · crackedNR 1 ENGINE NOSE COWL EXTERIOR AFT BACKSIDE BULKHEAD I/B AT 5 O'CLOCK POSITION VERTICAL ANGLE STIFFENER SUPPORT IS CRACKED AT TOP END REMOVED VERTICAL STIFFENER NR 1 ENG NOSE COWL AFT AT 5 O'CLOCK BULKHEAD IAW SRM REV 103 51-30-2 FABRICATED NEW STIFFENER FROMSep 24, 2010 · N204FE · Boeing 7272S2F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201009233660Nose Cowl · damagedDAMAGE BOTTOM NR 3 NOSE COWL. REMOVED AND REPLACED NR 3 ENGINE NOSE COWL IAW MM 71-10-021-4. REFERENCE NON-ROUTINE N00917 WORK ORDER 00049152.Sep 23, 2010 · N204FE · Boeing 7272S2F · Nacelle/Pylon, Main FrameSDR FDEA201009223663Seat Track · damagedMAIN CABIN SEAT TRACK AT BS 500-510 BL 0 HAS BROKEN SCALLOPS. REMOVED SEAT TRACK SECTION AT STA 360 TO 550 BL0, FABRICATED SEAT TRACK FROM BAC 1520-1331 7178-T6511 DIM. 189 1/2", TREATED AND PRIMED SEAT TRACK, AND INSTALLED SEAT TRACK AND SPLICE IAW SRM 51-30-Sep 22, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009223666Seat Track · damagedMAIN CABIN SEAT TRACK SEAT TRACK BS 835 LBL 45 HAS BROKEN SCALLOP. REMOVED AND REPLACE SEAT TRACK SECTION FROM BAC 1520-1331 7178-T6511 DIM 95 1/8" IAW SRM 51-30-2, 51-10-1, 53-10-2 FIG 7, 51-20-2 FIG 21, 51-30-5, AND 51-10-2 AT BS 760 TO 850 RBL 45.Sep 22, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009223653Skin · gougedNR 2 SLAT LOWER T/E SKIN GOUGED AT O/B SLAT HOOK AREA TRIMMED OUT DAMAGED AREA DIM: 1/2" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR PLATE FROM 2024 T-3 .125" DIM: 4" X 6" IAW SRM 57-50-3 FIG 10. INSTALLED REPAIR PLATE IAW SRM 51-30-2, REV 103.Sep 22, 2010 · N204FE · Boeing 7272S2F · Leading Edge DevicesSDR FDEA201009203664Seat Track · damagedMAIN CABIN SEAT TRACK AT BS 680-700, LBL 62.5 HAS DAMAGED SCALLOPS. CUT OUT DAMAGED AREA BS 656 TO 728 LBL 62.5, FABRICATED NEW SECTION, SPLICE REPAIR, ANGLES, AND FILLERS IAW SRM 53-10-5 FIG 1. INSTALLED REPAIR IAW SRM 53-10-5 FIG 1.Sep 20, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009183537Handle · unsecureON CLIMB OUT OF DAY FELT A SLIGHT ACFT VIBRATION (LIKE A SPOILER) RECYCLED NOT HELP- CONTINUUTE TO CLIMB AT ABOUT 12,500 HEARD AND FELT SEVERAL LOUD BANGS-LAST FOR SEVERAL SECONDS AFTER SLOWING BANGING STOPPED. RETURN TO BLOCKS, NOTICED L1 DOOR HANDLE NOT SSep 18, 2010 · N207FE · Boeing 7272S2F · Passenger/Crew Doors
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