Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 engine_model_key = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR FDEA201206282375Stringer · damagedFORWARD CARGO BAY WIRE BUNDLE STAND-OFF BRACKET BROKEN OFF AT BS 570, LBL 15. CUT OUT SECTION OF STRINGER 28L AT BS 570, 3 INCHES LONG IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED FILLER ANDJun 28, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR SPAA20120601Battery Pack · inoperativeAFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT CABIN B EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-31, OPS CHECK NORMAL.Jun 26, 2012 · N712S · Boeing 7372Y5 · Emergency LightingSDR SPAA20120602Power Supply · inoperativeAFT CABIN EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REPLACE AFT CABIN EMERGENCY EXIT LIGHT POWER SUPPLY IAW 33-51-31.Jun 26, 2012 · N712S · Boeing 7372Y5 · Emergency LightingSDR FDEA201203291170Oil System · leaking45 MIN AFTER TAKEOFF NR 3 ENG HAD LOST APPROX 1 GAL DOWN TO 1.5 GALS FROM 2.6 GAL AT TAKEOFF. OIL PRESSURE & TEMP WERE NORMAL ON NR 3. LANDED WITH GAL 1.25 GAL / 42 PSI PRESS / 10C OIL TEMP. ENT BY: 152952 RPT BY: 434068 SHGN 28MAR12 23:57 MEM U OPENEMar 29, 2012 · N257FE · Boeing 727233 · Turbine Engine Oil SystemSDR FDEA201203231070Fitting · leakingNR 3 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS, CRUISING AT FL 330. NR 3 OIL QUANTITY STARTED TO DECREASE APPROX 1 QT PER 2 MINUTES. AT FIRST INDICATION OF SECONDARY CONFIRMATION COMPLETED SHUTDOWN CHECKLIST AND DIVERTED. SHUTDOWN TO LANDING WINDMILL 15 MINMar 23, 2012 · N489FE · Boeing 727227 · Turbine Engine Oil SystemSDR FDEA201112225423Engine · malfunctionedAFTER STANDARD POWER SET AND BRAKE RELEASE HEARD LOUD BANG FOLLOWED BY EPR ON NR 3 GOING TO ZERO, DISCONTINUED TAKEOFF AND TAXIED CLEAR. ON TAXI BACK SAW IDLE NUMBERS ON NR 3 OF N1-26 EGT-410 N2-53 (IE LOWER N1 AND HIGHER EGT). ENGINE SHUTDOWN ON TAXI BACKDec 22, 2011 · N492FE · Boeing 727227 · Engine (Turbine/Turboprop)SDR CA111212015Module · bypassing(CAN) DURING TAXI WHEN FLAPS EXTENDED HYD A SYS PRESS WENT TO 1500 PSI & BOTH A SYS LOW PRESS LIGHTS CAME ON. UPON REMOVAL OF RUDDER MODULE FOUND TEFLON BACK UP RING OUT OF PLACE & WOUND UP INSIDE THE LINE FITTING PORT. REPAIR VENDOR REQUESTED TO SEND STRIP Dec 8, 2011 · Boeing 727260 · Rudder Control SystemSDR FDEA201111224996Oil System · leakingNR 1 ENGINE LOST OIL QTY AND PRESSURE AT FL 320. ENGINE WINDMILLED FOR 30 MINS, OIL PRESSURE WAS ZERO. REMOVED AND REPLACED THE ENGINENov 22, 2011 · N482FE · Boeing 727227 · Turbine Engine Oil SystemSDR C8GA201111150023Turbine Wheel · damagedDURING TAKEOFF ROLL AT APPROX 40 KNOTS THERE WAS A LOUD BANG AND THE NR 3 ENGINE STALLED AND N1 FELL TO 15 PERCENT. AN ABORTED TAKEOFF WAS PERFORMED WITHOUT INCIDENT AND THE ACFT RETURNED TO THE BLOCKS. POST FLIGHT INSPECTION WAS PERFORMED, FOUND TURBINE WHENov 15, 2011 · N801EA · Boeing 727225 · Turbine SectionSDR CA111017003Actuator · miswired(CAN) UPON INSTALLATION OF THE ACTUATOR, FUNCTION CHECK DETERMINED THE ACTUATOR WORKED BACKWARDS. ACTUATOR WAS IN O/H CONDITION. INTERNAL WIRING NOT CORRECT. FOLLOWING UP WITH VENDOR.Oct 4, 2011 · Boeing 727225 · Stabilizer Control SystemSDR FDEA201109103816Engine · overtempNR 2 ENGINE OVERTEMP. R & R NR 2 ENGINE IAW WORKCARD 70T0002, 70T0301-02, AND 70T0003-02, OPS CHECKED GOOD.Sep 10, 2011 · N468FE · Boeing 727225 · Engine (Turbine/Turboprop)SDR FDEA201109103817Engine · overtempNR 3 ENGINE OVERTEMP. R & R NR 3 ENGINE IAW WORKCARD 70T0001-03,70T003-03 AND 70T0301-03, OPS CHECKED GOOD.Sep 10, 2011 · N468FE · Boeing 727225 · Engine (Turbine/Turboprop)SDR PCSA2011090601Oil System · overtempNUMBER 3 ENGINE SHUT DOWN DUE TO HIGH OIL TEMPERATURE.Sep 6, 2011 · N905AJ · Boeing 727231 · Engine Oil TemperatureSDR FDEA201108193384Engine · damagedAFTER TAKEOFF, RECEIVED A RED WINDSHEAR WARNING LIGHT PERFORMED WINDSHEAR ESCAPE MANUVER W/FIREWALL POWER, APPROX 1 MIN. INSPECTED ALL EXHAUST AREAS FOR DAMAGE DUE TO OVERTEMP CONDITION. NO DAMAGE FOUND. R & R ENGINE. OPS CHECKED GOOD.Aug 19, 2011 · N468FE · Boeing 72725F · Engine (Turbine/Turboprop)SDR FDEA201107202853Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 480-600, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM 51-30-2 AND SRM 2489. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202860Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 480 - 550, RBL 45. REMOVED SEAT TRACK SECTION AND SPLICE PARTS AFTER FOUND OUT OF LIMITS IAW SRMR 2489 & SRM 51-30-2. FABRICATED NEW SEAT SECTION AND SPLICE PARTS IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1. INSTALLED NEW SEJul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202858Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 370-480, LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A & SRM 53-10-2 FIG 7, INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 & 51-10-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106212370Turbine Blades · damagedSETTING T/O POWER HAD LOUD BANG AND ALL ENG NR 1 INSTRUMENTS DROPPED. REPEATED T/O PRIOR TO T/O. REJECTED T/O PRIOR TO T/O POWER BEING SET. ENG NR1 WAS RUNNING ROUGH AND SMOOTHED OUT AS ENG WOUND DOWN. OPEN COWLING FOUND MASSIVE AMOUNT OF OIL IN COWL. INSPJun 21, 2011 · N286FE · Boeing 727233 · Turbine SectionSDR C8GA2011000006Power Supply · inoperativeDURING TAKEOFF ROLL OUT, ALL 3 ENGINE FUEL FLOW INDICATIONS FLUXUATED BY + / - 5000 LBS. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING FUEL FLOW POWER SUPPLY AT FAULT. R & R THE FUEL FLOW POWJun 17, 2011 · N715AA · Boeing 727223 · Engine Fuel Indicating SystemSDR C8GA2011000004Engine · damagedON TAKEOFF DEPARTING, WHILE CLIMBING THROUGH 1000' A LOUD BANG EMERGED FROM THE NR1 ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT NR 1 ENGINE REQUIRES REPLACEMEJun 10, 2011 · N715AA · Boeing 727223 · Engine (Turbine/Turboprop)SDR FDEA201104051330Oil System · leakingAIRCREW WROTE UP OIL QUANTIY IN NR 2 PRIOR TO FLT STARTED WITH 4 1/2 GALLONS. QUANTIY WAS 2 1/2 GALLONS STARTING CRUISE. AFTER APPROXIMATELY 40 MINUTES OIL OUANTY WAS ZERO. COMPLIED WITH RED TABS DURING CRUISE. SHUTDOWN NR 2 ENGINE WHEN PRESSURE DROPPED IN TApr 5, 2011 · N237FE · Boeing 727247 · Turbine Engine Oil SystemSDR FDEA201103191082Control Panel · failedAT FL 290 SMELLED STRONG ELECTRICAL ODOR. NO SMOKE NOTED OR CB'S POPPED. DECLARED EMERGENCY AND LANDED. R & R BUSS PROTECTION PANEL CONTROL BOX IAW AMM 20-10-017-2. R & R THE EXTERNAL POWER CONTACT RELAY IAW AMM 24-20-000-5. RAN ALL 3 ENGINES IAW JRH WITHMar 19, 2011 · N463FE · Boeing 727225 · External Power SystemSDR FDEA201103090924Engine · overtempRT WINDSHEAR WARNING ON APPROACH TO RWY 14, MISSED APPROACH WITH FIREWALL POWER AT 640MSL & WENT TO CLIMB AT 1100MSL. NO ENGINE PAREMETERS OBSERVED. ANALYSIS CONFIRMED THE NR 1 & NR 3 ENG EGT, N1 & N2 WERE WITHIN LIMITS. NR 2 ENG EXPERIENCED & EGT OVERTEMP Mar 9, 2011 · N493FE · Boeing 727227 · Engine (Turbine/Turboprop)SDR PCSA20110301Engine · flamed outCREW LOG ITEM "ENGINE NR 3 SURGED 3 TIMES (EPR N1 & N2). ON THIRD SURGE ENGINE 3 FLAMED OUT (EPR DROP FOLLOWED BY N1 AND EGT). RESTARTED ENGINE AND INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. ENGINE WINDMILLED FOR 10 MINS." MAINTENANCE INSPECTED THE ENGINEMar 1, 2011 · N495AJ · Boeing 727233 · Engine (Turbine/Turboprop)SDR FDEA201102210662Wire · damagedTEST FLIGHT: SHUTDOWN ENG NR 3 IAW QRM DUE TO HIGH OIL TEMP. ENG SHUTDOWN AT 2325 Z. ENG MATAINED 5 PSI TO TOUCHDOWN. OIL PRESS & QUANITY PRIOR TO SHUTDOWN WAS NORMAL. REPAIRED WIRE W198-060-18 IAW FX SWPM 20-10-13 AND WDM 79-33-01 PERFORMED. OPS CHECFeb 21, 2011 · N223FE · Boeing 727233 · Turbine Engine System WiringSDR KNNA20112491Line · brokenDISCREPANCY- IN FLIGHT BOTH "A" PUMPS LOW PRESSURE MASTER CAUTION. SYS A QUANTITY 0. FOUND BROKEN FLEX LINE AT SYS A LT WHEEL WELL. R & R LINE IAW AMM 20-10-51. SERVICED HYD FLUID IAW AMM 12-12-0. BLEED BOTH "A" PUMPS AND SYS. OPS CHECK NORMAL IAW AMM 29-1Feb 3, 2011 · N249TR · Boeing 7372K5 · Hydraulic System, MainSDR FOTR2022201970Frame · crackedPREVIOUS REPAIR ON BS 1166 FRAME CRACKED ABOVE STR 17L. REMOVED CRACKED REPAIR FROM BS 1166 FRAME ABOVE STR 17L IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 7075-0 .063' PO 90010605, DIM 10.5" X 6" IAW SRM 53-10-2 FIG 5. HEAT TREATED DOUBLER TO 7075-T6 IAFeb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022202060Rib · crackedNR 3 SLAT RIB NR 8 FROM OTBD IS CRACKED. REMOVED RIB NR 8 FROM OTBD END ON NR 3 SLAT IAW SRM 51-30-2. FABRICATED NEW RIB FROM 7075-0 .032" PO 20017552 DIM. 4" X 17" IAW SRM 57-50-2, FIG 2. HEAT TREATED TO 7075-T6 IAW FASI ENG REPORT NR 2-37153-801, REV A INFeb 2, 2011 · N357KP · Boeing 727230 · Leading Edge DevicesSDR FOTR2022201962Rib · crackedNR 3 SLAT RIB IS CRACKED ON INBD SIDE OF ACTUATOR FWD MOUNT. REMOVED NR 3 SLAT RIB IAW SRM 51-30-2. LOCATED AND DRILLED FASTENER HOLES IN NEW RIB PN 61-17294-13 PO 20222111 IAW SRM 51-20-1. INSTALLED NEW RIB IAW SRM 51-30-2.Feb 2, 2011 · N357KP · Boeing 727230 · Leading Edge DevicesSDR CA110106009Check Valve · frozenAIRCRAFT FAILED TO PRESSURIZE ON DEPARTURE. DUMPED FUEL AND RETURNED. MAINTENANCE GROUND RAN AIRCRAFT, CARRIED OUT PRESSURIZATION CHECKS, NO FAULTS FOUND. AIRCRAFT PRESSURIZED NORMALLY TO MAX DIFF SUBSEQUENT FLIGHTS COMPLETED WITH NO FURTHER PROBLEMS SUSPEJan 5, 2011 · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201012294773Battery Pack · inoperative"EMERGENCY EXIT LIGHTS BATTERIES ARE DEAD. LIGHTS WON'T TEST." REPLACED BATTERIES IN BOTH PORTABLE EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0. (CLOSED)Dec 29, 2010 · N462FE · Boeing 727225 · Emergency LightingSDR FDEA201012284757Controller · malfunctionedON TAKEOFF CLIMB AT 400'AGL, AT CLIMB POWER, EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. ENGINE ANTI-ICE WAS OFF, THE ENGINE RECOVERED AFTER A COUPLE OF BANGS, ALL ENGINE PARAMERTERS WERE NORMAL DURING CLIMB. WE OBSERVED NO OTHER ENGINE PARAMETERS DUDec 28, 2010 · N265FE · Boeing 727233 · Engine Bleed Air SystemSDR FDEA201012164705Frame · dentedAFT CARGO COMPT LEFT FRAME AT STA 1360, S26L FOUND DENTED. DENTED FRAME AT STA 1360, S-26L. REPAIRED IAW SRM 53-00-07 FIG 201, DETAIL III, REPAIR 5, REV 101. REPAIR IS CLASSIFIED AS MAJOR.Dec 16, 2010 · N946FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201012144661Duct · damagedON DESCENT, WITH WING ANTI ICE ON, RECEIVED LOWER AFT BODY LIGHT, WITH LOST AUTO PRESSURIZATION. RAN QRH, RESET WING ANTI ICE & TRIED AGAIN. RECEIVED LOWER AFT BODY LIGHT & AUTO PRESSURIZATION FAIL LIGHT AGAIN. RAN PRESSURIZATION IN MANUAL. TRIED AUTO PREDec 14, 2010 · N266FE · Boeing 727233 · Pneumatic Distribution 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 FDEA201012124643Floorbeam · corrodedCORROSION FLOORBEAM TOP "T" CAP STA 720D, RBL 45- LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED UPPER CHORD, ANGLES AND STRAPS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.Dec 12, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor BeamSDR FDEA201012114636Skin · crackedFS 359 STR 28L EXTERNAL REPAIR CRACKED. CUT OUT DAMAGED SKIN AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW EA 7-5330-123573.Dec 11, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR FDEA201012064638Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 950, PLUS 10" - STA 1010, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-7927178-T65, DIMS 270" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.Dec 6, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012044601Shear Tie · corrodedUPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STATION 1148 FRAME, STRINGER 26L TO 25L. REMOVED SHEAR TIE FROM AFT SIDE OF BS 1148 FRAME BETWEEN STRINGER 26L AND 25L IAW SRM REV 103, 51-30-2. FORMED SHEAR TIE USING 7075-0, .063" X 2" X 4" IAW SRM 51-2Dec 4, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting StructureSDR FDEA201012044602Shear Tie · corrodedUPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STA 1148 FRAME, STRINGER 27L TO 26L. REMOVED SHEAR TIE ON AFT SIDE OF BS1148 FRAME BETWEEN STRINGER 27L AND 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING 7075-0, .063" X 2" X 6" IAW SRM 51-20-1, Dec 4, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting StructureSDR FOTR2019813815Structure · crackedRT SIDE OF AFT AIRSTAR TORQUE BOX UPPER CORD IS CRACKED AT AIRSTAIR ACTUATOR FITTING. REMOVED UPPER CHORD FROM RT SIDE AFT AIRSTAIR TORQUE BOX STA BS 1263 IAW 51-30-2. INSTALLED NEW ANGLE, PN 65-17517-38. PO NR 20198118 IAW SRM 51-30-2 & SB 53-0129, REV 5.Dec 3, 2010 · N713AA · Boeing 727223 · Fuselage Main, StructureSDR FDEA201012034640Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 848 - STA 765, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1506-1108-7075T6 DIMS 9.2', AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.Dec 3, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012024536Control Handle · malfunctionedTHE AFT AIR STAIR LIGHT ON S/O PANEL CAME ON AT 1000FT ON TAKEOFF AND STAYED ON DURING DESCENT THE AFT AIR STAIR LIGHT WENT OUT AT LF 090 AND CAME BACK ON AT 4000 FT. RELEASED FOR SERVICE IAW MEL: 52-06-B. WORKED IN CONJUNCTION WITH TSI 52-30/4231. R & Dec 2, 2010 · N223FE · Boeing 727233 · Entrance StairsSDR FDEA201012024538Skin · bulgedBULGE EXTERIOR SKIN STA 720E- 720F STR 23R. CUT OUT DAMAGED PORTION OF STRINGER 23R, BS 720E PLUS 10" TO 720F PLUS 10" IAW SRM 53-10-3 FIG 1. FABRICATED TWO PORTIONS OF STRINGER USING BAC1498-142-7075T62 DIMENSIONS 17 7/8" AND 8 5/8", AND FABRICATED TWO SPLIDec 2, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR FOTR2019813835Shear Tie · corroded(FOTR) CORROSRION ON SHEAR TIE AT BS 720 BETWEEN STR 28L-28R. REMOVED CORRODED SHEAR TIE FROM STA 720 BETWEEN STR 28L & 28R IAW SRM 51-30-2. FABRICATED SHEAR TIE FROM 7075-T6 .063" PO 90010179 IAW SRM 53-10-2 FIG 3, 53-10-4 FIG 11, 51-30-5, 51-30-6. TREATED ANDec 1, 2010 · N713AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR PCSA2010120101Warning Light · illuminatedNR1 STRUT OVERHEAT LIGHT ILLUMINATED AT 33,000 FT. CLOSED NR 1 POWER LEVER AND LIGHT EXTINGUISHED. MX OPENED NR 1 PYLON, PRESSURIZED PNEUMATIC SYS CHECK FOR LEAKS, NONE NOTED IAW AMM 36-00-00. PERFORMED ENGINE RUN-UP AT PART POWER AND TAKEOFF. NO DEFECT NOTEDec 1, 2010 · N395AJ · Boeing 727233 · Overheat DetectionSDR FDEA201012014531Control Valve · failedACFT DID NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE SHOWED CLOSED, CARGO HEAT OUTFLOW CLOSED. ALL DOOR LIGHTS INDICATED CLOSED. PRESSURIZATION SYS APPEARED TO BE WORKING, NORMAL OTHERWISE. ALSO COULD NOT GAIN CONTROL IN STBY MODE. RESEALED NOSE GEAR ADec 1, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201012014637Stringer · corrodedCORROSION RT WHEEL WELL OTBD SIDE STA 880, STR 18A. REMOVED DAMAGED STR 18A SHELF, FABRICATED NEW STR 18A SHELF AND INSTALLED IAW SRM 51-30-2, SRM 53-10-2, SRM 51-20-1 AND SRM 51-30-5.Dec 1, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FOTR2019813838Intercostal · corroded(FOTR) CORROSION ON INTERCOSTAL BETWEEN BS 720-700 STR 27R-28R. REMOVED CORRODED INTERCOSTAL FROM BETWEEN STA 720-700, STR 27R-28R IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL FROM 7075-T6 .032" 19.5" X 8.5" PO 90010274 IAW SRM 53-10-2, FIG 3. SRM 51-20-1 FIGNov 30, 2010 · N713AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2019813419Intercostal · corroded(FOTR) CORROSION ON LOWER FLANGE OF INTERCOSTAL AT BS700 BETWEEN STR 28R - 27R. REMOVED INTERCOSTAL AT STA 700 BETWEEN STR 28R AND 27R IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .032" PO 90010274 DIM 19.5" X 8.5" IAW SRM 53-10-2 FIG 3, SRM 51-20-1 FINov 30, 2010 · N713AA · Boeing 727223 · Fuselage Miscellaneous Structure
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