Boeing 727-227

Service difficulty reports · 5,082

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727227'
  ORDER BY difficulty_date DESC"

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SDR FDEA201101180276Frame · corrodedFWD PIT LT SIDE, BS 720B FRAME HAS AREA OF CORROSION JUST BELOW STRINGER 24L. CUT OUT DAMAGED CHORD IAW SRM 51-40-4 FIG 2 LOCATED AND DRILLED NEW FRAME, FABRICATED REPAIR ANGLES, AND RADIUS FILLER IAW SRM 51-40-4 FIG 2 INSTALLED NEW FRAME, 3 EACH REPAIRJan 18, 2011 · N492FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201101180275Frame · corrodedFWD PIT LT SIDE BS 720C FRAME HAS AREA OF CORROSION JUST BELOW STR 24L. CUT OUT DAMAGED FRAME IAW SRM 51-40-4 FIG 2 LOCATED AND DRILLED REPAIR FRAME SECTION, FABRICATED REPAIR ANGLE 1 AND 2 AND REPAIR ANGLE 3. FABRICATED REPAIR RADIUS FILLER IAW SRM 51Jan 18, 2011 · N492FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201101180274Skin · corrodedFWD PIT BILGE AREA LOWER SKIN HAS AREA OF CORROSION AT BS 502, RBL 17. CUT OUT DAMAGED AREA, DIMENSION 7" X 6" IAW SRM 53-30-3 FIG 24. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER AND FILLERS IAW SRM 53-30-3 FIG 24 AND 53-30-2 FIG 2. INSTALLED REPAIR DOUBLER,Jan 18, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101180273Shear Tie · corrodedFWD PIT BILGE AREA HAS CORRODED SHEAR TIE AT BS 540, LBL 2 TO RBL 5. CUT OUT DAMAGED LOWER FLANGE OF SHEAR TIE IAW SRM 53-10-4. FIG 15 FABRICATED. REPAIR DOUBLER FROM 7075 T6 .050" DIM 5" X 3.2500" AND RADIUS FILLER FROM 7075 T6 .063", DIM 5" X .8750" IAJan 18, 2011 · N492FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201101170212Stringer · damagedEVALUATE PREVIOUS STRINGER REPAIR AT STR 8L BETWEEN BS 420 AND 440. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 3, FABRICATED STRINGER SECTION FROM BAC 1498-139 AND REPAIR PLATE 1 (2EA) FROM 2024T3 0.125", PLATE 2 (4EA) FROM 2024T3 0.056", AND PLATE 3 (4EA) FRJan 17, 2011 · N492FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201101170216Skin · gougedINNER SURROUND SKIN GOUGED STA 620, STR 8L TO 10L. REMOVED MCD INNER SKIN AT STA 620 STR 8L TO 10L, FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.Jan 17, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101170217Skin · corrodedCORROSION STA 510, STR 27R FWD PIT. CUT OUT DAMAGED AREA OF SKIN AT BS 510 STR 27R, 4 1/8" X 2 1/8" IAW SRM 53-30-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .100" X 16 3/8" X 10 1/8" AND FILLER FROM 2024-T3, .090" X 4" X 1 1/8" IAW SRM 53-30-3 FIG 1. Jan 17, 2011 · N223FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101170211Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 560 BL0 TO LBL 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG 3. LOCATED AND DRILLED NEW UPPER TEE, AND 4 SUPPORT ANGLES AND 4 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED TEE, SUPPORT ANGLES AND STRAPS IAW SRJan 17, 2011 · N492FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201101170210Torque Box · crackedAFT AIRTSTAIRS AREA , LIGHTING HOLE IS CRACKED AT RT LOWER TORQUE BOX, BS 1233. CUT OUT DAMAGED AREA OF WEB, DIM 1/2" X 1/2" IAW SRM 51-40-2 FIG 1 AND 51-10-1. FABRICATED DOUBLER FROM 7075 T-6 .032" DIM 6" X 2" IAW SRM 51-40-2 FIG 1 AND 53-10- 2 FIG 6. INSJan 17, 2011 · N492FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201101160412Seat Track · corrodedCABIN SEAT TRACK HAS SURFACE CORROSION ON FLANGE RBL 45.5 BETWEEN BS 1010 AND 1050. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK SECTION, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.Jan 16, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101140177Skin · gougedC-2 DOOR IS GOUGED ON PREVIOUS REPAIR AROUND FASTENER HEADS. REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER USING 2024 T-3 .080" X 6.8750" X 4" IAW SRM 52-00-3, FIG 3. INSTALLED NEW REPAIR DOUBLER IAW SRM 52-00-3, FIG 3 AND 5Jan 14, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101140209Floorbeam · corrodedCORROSION ON UPPER SURFACE OF UPPER FLANGE STA 950, FLOORBEAM TOP STRAP, LBL 25 TO LBL 45. REMOVED UPPER TEE CHORD AT STA 950 LBL 63.5 TO RBL 63.5, FABRICATED NEW TEE CHORD FROM BAC 1505-100405 7075T6, AND INSTALLED NEW UPPER TEE CHORD AT STA 950 IAW DWG 65-Jan 14, 2011 · N492FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201101140207Skin · gougedINNER SURROUND SKIN GOUGED STA 620, STR 12L TO 16L. FABRICATED INNER SKIN AND DOUBLER REPAIR FROM 2024T3 0.125", AND INSTALLED INNER SKIN AND DOUBLER REPAIR PER EA 7-5330-143933.Jan 14, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101140206Skin · gougedINNER SURROUND SKIN GOUGED STA 620, STR 4L TO 10L. FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN AT AFT SECTION STA 600 TO 640 STR 4L TO 10L IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10- 2, AND 51-30-2.Jan 14, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101140208Skin · gougedINNER SURROUND SKIN GOUGED STA 480, STR 4L TO 10L. FABRICATED NEW INNER SKIN FROM 2024T3 0.125", AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2 FIG 3A, SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.Jan 14, 2011 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201101140174Web · buckledWEB BUCKLED AT LIGHTNING HOLE - RT HORIZ STABILIZER INTERIOR BOX RIB, APPROX STAB L/E 100.63. CUT OUT DAMAGED AREA OF WEB DIM 1/4" X 1" IAW SRM 55-10-4 FIG 2 REV 103. FABRICATED WEB LIGHTNING HOLE DOUBLER FROM 2024 T3 .032" DIM 9.75" X 13.25" IAW SRM Jan 14, 2011 · N492FE · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR FDEA201101120118Seat Track · corrodedSEAT TRACK CORRODED, STA 698, BL 0. REMOVED SEAT TRACK SECTION AT BS 600 TO 720 BL 0 IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM 120" IN LENGTH IAW SRM 51-30-5 AND SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120117Seat Track · corrodedSEAT TRACK CORRODED, STA 720-740, BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK, MATERIAL USED BAC 1520-792 7178 T6511 DIM 141 1/2" IAW SRM 51-30-5 AND FEDEX P-F SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51Jan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120114Seat Track · corrodedSEAT TRACK CORRODED STA 480-640 BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION, MATERIAL USED BAC 1520-792 7178 T-6511 DIM 120" IN LENGTH IAW SRM 51-30-5 AND SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK IAW SRM 51-30-Jan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120119Seat Track · corrodedSEAT TRACK CORRODED STA 690-740 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK. FABRICATED SPLICER AND 2 EA ANGLES AND SPLICE PLATE IAW SRM 53-10-3, FIG 1 AND 51-30-5 TREAT AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEATJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120116Seat Track · corrodedSEAT TRACK CORRODED STA 690-740 RBL 45. REMOVED SEAT TRACK SECTION STA 690 TO 740, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM 172" LONG, SPLICE REPAIR FROM BAC 1503-100122 7178T6 DIM 15" LONG (2EA), AND STRAP PLATE FROM 7075T6 0.250" DIJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120115Seat Track · corrodedSEAT TRACK CORRODED, STA 690, RBL 45. REMOVED SEAT TRACK SECTION STA 480 TO 690 RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM. 209.5" LONG, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690, RBL 45 IAW SRM 53-10-2 FIG 7, 51-30-Jan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120113Seat Track · corrodedSEAT TRACK CORRODED, STA 480-670, RBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED 2 EA SEAT TRACK SECTIONS FROM BAC1520-792 7178 T6511, AND BAC 1520-792 7178 T6511, AND SPLICER REPAIR TO STA 630, 2EA ANGLES MAT USED BAC 1503-100122-7178, T6511. STRAPJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120112Seat Track · corrodedSEAT TRACK CORRODED STA 480-690 LBL 45. REMOVED SEAT TRACK, LOCATED AND DRILLED 2 EA SEAT TRACK SECTIONS FROM BAC 1520-792 7178-T6511 DIM 150" AND 60" IN LENGTH AND SPLICES FROM BAC 1503-100122 7178 T6511 DIM ( 2 EA ) 14" X 13.5" AND SPLICE STRAP FROM 707Jan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120111Seat Track · corrodedSEAT TRACK CORRODED STA 480-690 LBL 25. REMOVED SEAT TRACK AT BS 480 TO 690, LBL 25, FABRICATED NEW SEAT TRACK FROM BAC 1520-792 7178T6511, SPLICES FROM BAC 1503-100122 7178T6511, AND STRAPS FROM 7075T6, 0.250", AND INSTALLED SEAT TRACK SECTIONS, SPLICES, ANDJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120110Seat Track · corrodedSEAT TRACK CORRODED STA 370-480 LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK, AND INSTALLED NEW SECTION IAW SRM 53-10-2, FIG 7, SRM 51-30-5, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2.Jan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101120109Seat Track · corrodedSEAT TRACK CORRODED STA 360-480, LBL 25. REMOVED SEAT TRACK SECTION BS 344 TO BS 480 LBL 25 IAW SRM 51-30-2. REMOVED SPLICE PLATE BS 460-500, LBL 25 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM 135.75" LONG INSTALLEJan 12, 2011 · N492FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR CA110112005Fairing · tornCREW REPORTED A `BUFFETING` WITH GEAR HANDLE IN THE `OFF` POSITION. UPON ARRIVAL, MAINTENANCE DISCOVERED THE BELLY PANEL AFT OF THE NOSE WHEEL WELL HAD PEELED BACK FROM THE FORWARD SCREW LINE. THE PANEL WAS REPLACED AND ACFT RETURNED TO SERVICE.Jan 11, 2011 · Boeing 727227 · Aerodynamic FairingsSDR FDEA201101100102Seal · failedAFTER GEAR RETRACTION, RED GEAR DOOR LT ON FRONT PANEL WITH NOSE GEAR DOOR LT ON F/E PANEL REMAINED ILLUM. COMPLIED WITH QRH. RECYCLED GEAR NO HELP. RTN TO DEPARTURE. FOUND BULB SEAL ON FWD EDGE OF NOSE WHELL TORN AND FULL OF ICE. BULB WAS SOLID. R & R Jan 10, 2011 · N486FE · Boeing 727227 · Nose/Tail Landing GearSDR C8GA2010000080Duct · crackedSHORTLY AFTER TAKEOFF FROM WHEN THE WING ANTI-ICE WAS TURNED ON, A LOUD POP WAS HEARD FOLLOWED BY A SPIKE IN THE ACFT PRESSURIZATION AND THE LOWER AFTER BODY HEAT LIGHT ILLUMINATED. ACFT DIVERTED AND MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. MX FOUND THE Dec 22, 2010 · N308AS · Boeing 727227 · Airfoil Anti/De-ice SystemSDR CA101217011Actuator · leaking(CAN) WHILE TAXIING FOR DEPARTURE, CREW NOTICED A HYDRAULIC SYSTEM WARNING LIGHT AND A LOSS OF HYDRAULIC PRESSURE. THE A/C WAS TOWED BACK TO THE RAMP WHERE MAINTENANCE DISCOVERED THE NR 5 SLAT ACTUATOR HAD COME APART. THE ACTUATOR WAS REPLACED AND THE AIRCRAFTDec 15, 2010 · Boeing 727227 · Leading Edge Slat ActuatorSDR C8GA2010000079Warning Light · illuminatedON TAKEOFF, THE RED "GEAR DOOR" LIGHT ON THE FWD PANEL REMAINED ILLUMINATED. SYS FOUND TO BE PERVIOUSLY DEFERRED IAW MEL 32-1, ACFT RETURNED TO SERVICE.Dec 15, 2010 · N308AS · Boeing 727227 · Landing Gear Position and WarningSDR C8GA2010000078Circuit Breaker · poppedON TAKE-OFF, WHILE DOING A ROLLING POWER CHECK, ENGINE NR 1 AND NR 3 EPR GAUGES FAILED TO COME UP. ABORTED TAKE-OFF AT LOW SPEED AND TAXIED BACK TO THE RAMP. MX FOUND CIRCUIT BREAKERS POPPED, RESET BREAKERS, RAN ENGINES. OPS CHECK GOOD IAW MM 77-11-00, ACFT RDec 15, 2010 · N308AS · Boeing 727227 · Engine Indicating SystemSDR FDEA201012144672Wire Harness · burnedDURING APU START AT APPROX 55 SECONDS SMOKE POURING FROM APU - EGT APPROX 525. SHUTDOWN USING FIRE HANDLE & SHOT FIRE BOTTLE. STRONG BURNED RUBBER/WIRE INSULATION TYPE ODOR IN W/W. NO FIRE INDICATION IN COCKPIT. AS PRECAUTION APU CONTROL BREAKER PULLED & CDec 14, 2010 · N487FE · Boeing 727227 · APU System WiringSDR FDEA201012144660Light · intermittentL1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. R & R EMERGENCY EXIT PORTABLE LIGHT ASSY, REF MM33-50-101-2-0, OPS CHECK GOOD.Dec 14, 2010 · N485FE · Boeing 727227 · Emergency LightingSDR FDEA201012094626Skin · corrodedCORROSION ON FUSELAGE SKIN AFT OF FRAME AT BS 950F, OTBD ON STR 28R, FOUND DURING PREP TO REINSTALL AFT PIT FRAMES. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3 .090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3 .071 DIMS 5Dec 9, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011234481Frame · damaged2 EACH OPEN HOLES IN FRAME AND REPAIR DOUBLER - STA 950C AT STR 24L. REMOVED REPAIR DOUBLER IAW SRM 51-30-2 REV 103 FORMED NEW REPAIR DOUBLER FROM 7075 O .080" DIM 8" X 4 1/2" IAW SRM 53-10-2 FIG 5 AND 51-20-1 FIG 7 INSTALLED REPAIR DOUBLER IAW SRM 51Nov 23, 2010 · N488FE · Boeing 727227 · Fuselage Main, FrameSDR C8GA2010000076Connector · damagedON APPROACH, THE NLG DID NOT INDICATE GREEN. LIGHT REMAINED RED, ALL 3 LANDING GEAR WERE MANUALLY EXTENDED. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R THE NLG POSITION SWITCH, R & R NLG LOCK SWITCH CONNECTOR PLUG, REPLACED 2 EACH WIRNov 23, 2010 · N308AS · Boeing 727227 · Landing Gear System WiringSDR FDEA201011224465Shear Tie · crackedUPON REMOVAL OF SHEAR TIE FOR FRAME REMOVAL, FOUND SHEAR TIE CRACKED ON OTBD UPPER CORNER, BS 990, BETWEEN STRINGER 28R AND 29R. REMOVED SHEAR TIE IAW SRM 51-30-2 REV 103 FABRICATED NEW SHEAR TIE FROM BAC1505-39042 7075-T6511 7" LONG IAW BAC DWG 65-16340 Nov 22, 2010 · N488FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201011184416Skin · gougedGOUGES INNER SURROUND SKIN STA 620, STR'S 8L-16L. CUT OUT DAMAGED SKIN SECTION, FABRICATED NEW SKIN SECTION USING 2024T-3 .125 DIMS 56" X 22" AND SPLICE USING 2024T-3 .125 DIMS 4" X 22" AND INSTALLED REPAIR PARTS IAW EA 7-5330-143921.Nov 18, 2010 · N233FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011184415Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950, LBL 61 - 45. REMOVED DAMAGED UPPER TEE CAP FROM FLOORBEAM, LOCATED AND DRILLED NEW UPPER TEE CAP AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND DWG 65-16338.Nov 18, 2010 · N233FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201011184412Door · unsecureACFT WOULD NOT PRESSURIZE. LOUD NOISE AROUND MAIN ENTRY DOOR. NO DOOR LIGHTS. HANDLE IN PROPER POSITION. UPON ACFT ARRIVAL FOUND L-1 DOOR T/E NOT FULLY CLOSED. OPENED AND CLOSED DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. PERFORMED INSP OF L-1 DOOR WITH NONov 18, 2010 · N491FE · Boeing 727227 · Service DoorsSDR FDEA201011184411Air Duct · contaminatedSTRONG ODOR OF FUEL FUMES IN COCKPIT, INCREASED AFTER TAKEOFF DURING CLIMB. UPON ARRIVAL, NOTICED STRONG DIESEL ODOR IN ACFT EE AND PIT AREAS ALSO IN FLT DECK. OUR HEAT DUCTING WAS ALSO STRONG ODOR. CHECKING COALASTER BAGS. SUSPECT HEAT CART CONTAMINATION Nov 18, 2010 · N487FE · Boeing 727227 · Air Distribution SystemSDR FDEA201011174410Battery Pack · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT INOP. R & R SHIELD ASSY AND RELAMPED DUE TO CORROSION. NO HELP MM 33-50-041-2. R & R BATTERY PACK ASSY IAW MM 33-50-051-2. OPS CHECK NORMAL. PREMATURE REMOVAL/INSTALLATION.Nov 17, 2010 · N491FE · Boeing 727227 · Emergency LightingSDR FDEA201011164482Stringer · damagedSTRINGER 4L AT BS 1180 TENSION TIE DAMAGED. CUT-OUT DAMAGED AREA ON STRINGER 4L FROM 1160 TO 1181.1250, DIM 21.1250", FABRICATED AND INSTALLED REPAIR AND STRINGER SECTION FROM STR. BAC 1498-145 7075T6-2, DIM 21.1250" AND 5EA REPAIR PLATES NR1 FROM 2024T3 0.250Nov 16, 2010 · N488FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201011154414Skin · corrodedCORROSION ON SKIN AT BS 720A PLUS 5" BETWEEN STRINGER 28R AND 27R. CUT OUT DAMAGED AREA, DIMENSION 5" X 2" IAW SRM 53-30-3 FIG 1. FABRICATED SKIN REPAIR USING 2024 T3, .080" X 14 3/4" X 9 1/4" IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALNov 15, 2010 · N233FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011154413Skin · corrodedCORROSION - INTERIOR FUSELAGE SKIN STATION 950D TO STA 950E OTBD SIDE OF STR 29L. REMOVED DAMAGED AREA OF SKIN IAW EA7-5330-123571 AND SRM 51-10-1, REV 103. FABRICATED DOUBLER, TRIPLER, & FILLERS IAW EA 7-5330-123571. INSTALLED DOUBLER, TRIPLER AND FILLERNov 15, 2010 · N233FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011134351Frame · gougedFRAME GOUGED STA 1070 STR 27L, AT RADIUS OF UPPER CHORD FLANGE CUT OUT DAMAGED SECTION OF UPPER FRAME DIM 3/4" X 2 1/2 " IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075 O .071" DIM 14" X 6" IAW SRM 53-10-2, FIG 5 AND 51-40-3, FIG 1 LNov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201011134348Skin · gougedINNER SKIN GOUGED STA 1177, STR 4L. CUT-OUT DAMAGED AREA AT BS 1177 ON STR 4L DIM. 1.125" DIA., FABRICATED REPAIR DOUBLER AND LAP FILLER FROM 2024T3 0.063" DIM. DOUBLER 10" X 6.8750" FILLER 11" X 4.5", AND INSTALLED DOUBLER AND FILLER IAW EA 7-5330-143918.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011134350Structure · crackedLEFT INBD MID FLAP AFT LOWER CHORD IS CRACKED AT 3 CUTOUTS. REMOVED CRACKED CHORD SECTION. FABRICATED NEW SECTION USING BAC1503-100046 7075 T6 DIMS 77" AND INSTALLED ALL REPAIR PARTS IAW SRM 57-50-2, 51-30-5 AND 51-30-2.Nov 13, 2010 · N488FE · Boeing 727227 · Trailing Edge Flaps
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