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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 07FDEA04538Duct · blownHEARD LOUD BANG WHILE CLIMBING PAST 32,000 FEET. BANG APPEARED TO BE BELOW AND FORWARD OF THE INSTRUMENT PANEL. DID NOT NOTICE ANY ENGINE OR PRESSURIZATION FLUCTUATIONS. FOUND GASPER AIR DUCT BLOWN. COMPLETED TEMP REPAIR WITH CARGO PIT TAPE PER EA 7-2120-1Oct 9, 2007 · N278FE · Boeing 727233 · Air Distribution SystemSDR 07FDEA04537Skin · delaminatedRIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 96" FROM INBD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 PARA'S 7, 14, 15, 19, 20, 22. TAP TEST GOOD PRIMED AND PAINTED REPAIR AREA, REF MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 9, 2007 · N218FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA04536Skin · gougedRIGHT WING INBOARD FORE FLAP UPPER SURFACE GOUGE, 93" FROM INBOARD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 PARA, S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. PRIMED AND PAINTED AREA REF MM 51-20-151-7. THIS IS CLASSIFIED A MINOR REPAIR.Oct 9, 2007 · N218FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA04523Frame · crackedFWD LOWER CARGO STUB FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FABRICATED AND INSTALLED NEW STUB FRAME IAW 727 SRM 51-10-01 AND DWG 53FX1370.Sep 30, 2007 · N283FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA04522Frame · crackedFWD CARGO, LOWER STUB FRAME EXTENSION AT STA 600 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FAB'D AND INSTALLED A NEW STUB FRAME IAW SRM 51-10-01 AND DWG 53FX1370.Sep 30, 2007 · N283FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA04366Floorbeam · corrodedMAIN DECK FLOORBEAM AT STA 720A LBL62 WL 208 T-CAP CORRODED OUT OF LIMITS. REMOVED CORRODED AREA, INSTALLED T-ANGLE AND SPLICE PLATE REPAIR IAW SRM 51-30-2.Sep 28, 2007 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA04361Frame · corrodedAFT CARGO STA 950 S-26L HAS A CRACK AND CORROSION ON FRAME STA 950 REMOVED CORROSION IAW SRM 51-10-6, AREA WITHIN LIMITS IAW EA 7-5310-110790, HFEC ACCOMPLISHED, NO DEFECTS NOTED.Sep 28, 2007 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA04352Floorbeam · corrodedAFT CARGO STA 950F LBL 44 MAIN DECK FLOORBEAM HAS CORROSION AROUND FASTENER HOLE. REMOVED AND REPLACED T-CAP IAW SRM 51-30 AND SRM 27-53-034.Sep 27, 2007 · N263FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA04351Floorbeam · corrodedMAIN CARGO DECK, STA 560 RBL 1-24, WL 208, FLOORBEAM TOP SURFACE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM TEE CAP AND ANGLES IAW SR 27-53-034.Sep 27, 2007 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 9182007Hose · damagedNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON IN CLIMBOUT 6000 FT. LIGHT WENT OUT ON REDUCING POWER TO 1.4 EPR. THE AIRCRAFT RETURNED TO MIA. THE THRUST REVERSER FLEXIBLE HOSE WAS FOUND DAMAGED. THE HOSE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Sep 18, 2007 · N994AJ · Boeing 727233 · Engine Thrust ReverserSDR 07FDEA03867Frame · corrodedAFT LWR CARGO PIT FUSE. CUTOUT FOR NR 3 DOOR, STA 1130 PLUS 13" AFT SIDE FRAME HAS CORROSION DOWN LOW WHERE SCUFF PLATE MOUNTS AT STR 26R. REMOVED FRAME AT STA 1130 PLUS 13, FROM STRINGER 18R-28. REPLACED WITH NEW FRAME STA 1130 PLUS 13, FROM STRINGER 18R -Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03873Support Beam · inoperativeLT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 4 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF SR-27-57-038. REMOVED AND REINSTALLED LOWER WING T/E PANELS, REMOVED EXISTING DOUBLER. REMOVED AND REINSTALLED NR 4 SPOILER ACTUATOR MOUNT, FLAP TORQUSep 17, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA03872Floorbeam · corroded"PREVIOUS REPAIR'" FLOORBEAM AT STA 620, RBL 29-42 HAS CORROSION ON UNDERSIDE FROM AREA NOT TREATED AND PRIMED. REMOVED DAMAGED PORTION OF UPPER FLOORBEAM AT STA 620, RBL 29-42. FABRICATED AND INSTALLED UPPER CAP REPAIR. REF FED EX EA NR 7-5310-113099, THISSep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03870Channel · corrodedLWR AFT CARGO PIT NR 3 CUTOUT THRESHOLD SUPPORT CHANNEL, STA 1130 STR 26R IS CORRODED. SUPPORT CHANNEL FOR NR 3 DOOR CUTOUT THRESHOLD IS REMOVED AND REPLACE ON WO NR 37678/N00602 ITEM 17 AND 18 ON JPF. THIS IS CLASSIFIED AS A MAJOR REPAIR.Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03791Bracket · crackedLT WING T/E PANEL BRACKET IS CRACKED, 2 EA. PLACES ABOVE AND JUST INBOARD OF THE NR 7 SPOILER ACTUATOR REPLACED PANEL BRACKET AS PER SRM 51-30-02, AT WBL 71 TO 153, LT. THIS IS CLASSIFIED AS A MINOR REPAIR.Sep 14, 2007 · N262FE · Boeing 727233 · Wing, Attach FittingsSDR 07FDEA03789Frame · dentedFWD PIT FRAME, STA 660 UPPER FLANGE HAS A DENT BETWEEN STR 23R-24R FOUND 3 DENTS ON UPPER FLANGE OF STA 660, BETWEEN S-22R -S-25R AND FOUND OUT OF LIMITS, CUTOUT DAMAGE, FORMED NEW FRAME SPLICE DOUBLER OUT OF 7075 O .050, HEAT TREATED MATERIAL 7075-T6 THEN DSep 14, 2007 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03669Skin · crackedLEFT WING INBD MID FLAP, LOWER SURFACE, VERY AFT ANGLE STRUCTURE IS CRACKED AT NUTPLATE, 55" FROM INBD EDGE INSTALLED ANGLE IAW 51-40-4 THIS IS CLASSIFIED AS A MINOR REPAIR.Sep 13, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA03664Bracket · crackedUPPER TRAILING EDGE PANEL BRACKET IS CRACKED ABOVE ACTUATOR REMOVED AND REINSTALLED UPPER WING ROOT PANEL AT TRAILING EDGE. REMOVED AND REINSTALLED NR 8 SPOILER MOUNT. REMOVED AND REPLACED TRAILING EDGE PANEL BRACKET REPLACED STIFFENERS ON PANEL BRACKET, Sep 13, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA03721Beam · corrodedRT MLG BEAM LOWER SURFACE AND FASTENER HOLES EXPOSED BY REMOVAL OF LOWER T/E PANELS NEED TO BE CLEANED AND INSPECTED. FOUND CORROSION INSIDE HOLES REPAIRED DAMAGE HOLE. REF FED EX EA NR 7-5720-113948 CLEANED HOLES/ REWORKED HOLES REF EA. THIS IS CLASSIFIED Sep 13, 2007 · N262FE · Boeing 727233 · Wing Main, Frame StructureSDR 07FDEA03715Floorbeam · corrodedUPPER DECK FLOORBEAM, STA 1130, LBL 18, WL 208, CORROSION AROUND 1 EA FASTENER HOLE REMOVED CORROSION, REF SRM 51-10-6, ORIGINAL MATERIAL .160" AFTER BLENDING, MATERIAL REMAINING .147" AND IS WITHIN LIMITS PER EA NR 7-5310-113090, SHOT PEENED AREA REF SOP 20Sep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03711Frame · corrodedFLOORBEAM T-CAP CORRODED STA 560, LBL 2-25 BLENDED AREA, MAPPED OUT DAMAGE, REF SRM 51-10-6. REMOVED OLD FLOORBEAM REPAIR REF SRM 51-30-02. REMOVED AND REINSTALLED WEB AT STA 560-580, BL 0, REF SRM 51-30-02. REMOVED AND REINSTALLED WEB AND ATTACH BRACKETS ASep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03709Floorbeam · corrodedFLOORBEAM T- CAP CORRODED, STA 620, LBL 1-25 REMOVED CORROSION REF SRM 51-10-6, DUE TO SSI LOCATION NO BLENDING IS ALLOWED. TRIMMED T- CAP AND MFG REPAIR PARTS REF SR27-53-034 AND INSTALLED REPAIR PARTS. REF SR27-53-034 AND SRM 51-30-2.Sep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03708Floor Support · corrodedFWD PIT, CARGO FLOOR SUPPORT, HAS CORROSION AROUND NUTPLATED AT BS 640-646, RBL 3" REMOVED CORROSION REF SRM 51-10-2. ORIGINAL MATERIAL THICKNESS .071", AFTER BLEND .010 MATERIAL REMOVED FOR A REMAINING THICKNESS OF .061 AND IS OUT OF LIMITS REF SRM 53-10-1. Sep 13, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03692Spar · crackedRIGHT WING NR 6 LEADING EDGE ACTUATOR MOUNT ON FRONT SPAR IS CRACKED IN THE UPPER INBD CORNER (FLAP). REMOVED AND REPLACED NR 6 LEADING EDGE ACTUATOR MOUNT UPPER I/B CORNER (KRUGER FLAP) REF MM 27-81-022, SRM 51-30-2 LEAK CHECK AND OPS CHECKED GOOD.Sep 13, 2007 · N262FE · Boeing 727233 · Wing SparSDR 07FDEA03685Floorbeam · corrodedFLOORBEAM AT STA 500, RBL 28 - 42, HOLES ARE CORRODED UNDERNEATH FROM PREVIOUS REPAIR WITH NO TREAT AND PRIME REMOVED CORROSION FROM DAMAGED AREA, REF SRM 53-10-1. REMOVED DAMAGED AREA REF DWG SR27-53-034 REV F, ORIGINAL THICKNESS .125, REMAINING THICKNESS .Sep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03677Skin · damagedAFT LOWER FUSELAGE STA 1183 BETWEEN STR 27L AND 29L SKIN DAMAGED. AFTER REMOVAL OF SKIN, FOUND TAIL SKID DRAG LINK HINGE FITTING HAS A DRILL START, (HIDDEN DAMAGE) ON LT SIDE OF JACK CUTOUT. REMOVED DAMAGED HINGE FITTING, DRILLED UP AND INSTALLED NEW FITTINGSep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA03665Skin · damagedAFT LOWER FUSELAGE, STA 1183 BETWEEN STR 27L AND 29L, SKIN PANEL AT FWD EDGE OF TAIL STAND COMPARTMENT IS DEFORMED AND HAS NUMEROUS LOOSE/WORKING FASTENERS REMOVED TAIL STAND DOOR AND SURROUNDING STRUCTURE, DRAG LINK, FABRICATED SKIN PANEL FILLER AND SKIN ATTASep 13, 2007 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA03629Support Beam · failedRT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 5 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF DWG SR 27-57-038. REMOVED T/E PANELS, REPAIRED LOWER CHORD ANGLES IB OF NR 5 FLAP TRACK. REINSTALLED T/E PANELS REF SRM 51-30-2 PG 4, 3 AND 2, AND FED Sep 12, 2007 · N262FE · Boeing 727233 · Wing Main, Frame StructureSDR 07FDEA03586Valve · leakingCALLED BACK BY RAMP. MX NOTICED HYD LEAK/PUDDLE ON GND AFTER WE TOOK OFF. REPLACED NR 3 BRAKE SHUTTLE VALVE PER B727 AMM 32-41-051-4. LK CKS GOOD.Sep 11, 2007 · N270FE · Boeing 727233 · Master Cylinder/Brake ValveSDR 07FDEA03468Floorbeam · corrodedFLOORBEAM IN THE MAIN CARGO COMPARTMENT HAS CORROSION AT BS 1010, RBL 10.5 (UPPER T CAP) REMOVED CORROSION ORIGINAL MAT.THICKNESS .125, REMOVED .032, .093 REMAINING, OUT OF LIMITS. REPAIRED FLOORBEAM USING .063 17-7 PH STEEL, .125 7075 T6. REF SRM 51-10-18 Sep 7, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03430Floorbeam · corrodedFWD CARGO PIT, FLOORBEAM LOWER FOWARD FLANGE UPPER SURFACE HAS CORROSION AT NUTPLATE HOLES, BS 720, RBL 3-34. REMOVED CORRODED LOWER FLANGE FROM RBL 3-34. FABRICATED NEW FLANGE, FILLERS AND 4 REPAIRS ANGLES, AND HEAT TREATED 4 REPAIR ANGLES REF DWG SR 27-53-Sep 6, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03300Seat Track · corrodedSEAT TRACK FROM STA 560 - 572, LBL 24 - 25 CORRODED REMOVED CORRODED SEAT TRACK, MANUFACTURED NEW SEAT TRACK AND INSTALLED REF SRM 51-30-02 FOR REMOVAL, AND SRM 5-30-02 FOR INSTALL. SEAT TRACK WAS REPLACED FROM STA 480 TO 689, LBL 24. THIS IS CLASSIFIED AS ASep 1, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03258Actuator · failedCLIMBING THRU FL190 A/P CRUSE TRIM WOULD NOT WORK IN EITHER DIRECTION, NOR WOULD THE MAIN ELC TRIM WORK IN THE NOSE DOWN DIRECTION. RECYCLED THE CUTOUT SWITCHES, BUT STILL DIDN'T WORK. NO STAB TRIM C/B'S WERE POPPED ON THE DESCENT THE TRIM STARTED TO WORK Aug 30, 2007 · N282FE · Boeing 727233 · Speed-Attitude Correction SystemSDR 07FDEA03257Floorbeam · misrepairedPREVIOUS REPAIR STA 720A, RBL 29-42, CORRODED ON UNDERSIDE FROM NO TREATING OR PRIMING REPAIR FLOORBEAM 720A, RBL 29-42 REF. FED EX DRAWING SR-53-034 REV F, SRM 53-10-1, 51-10-2 51-30-2. REMOVED AND REINSTALLED SEAT RAIL HARDWARE, RBL 24, STA 690 TO 720B ANDAug 30, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03255Skin · corrodedRT HORIZONTAL STAB ELEVATOR, OB MOST UPPER SURFACE STATIC WICK. CORROSION ON SKIN SURFACE, AROUND AND UNDER STATIC WICK BASE, AND ON WICK BASE ALSO REMOVED CORROSION ON UPPER RT OUTBOARD ELEVATOR STATIC WICK, FOUND TO BE OUT OF LIMITS BY NDT. MATERIAL LOSS Aug 30, 2007 · N286FE · Boeing 727233 · Elevator, Plate/SkinSDR 07FDEA03252Skin · gougedLT WING, O/B FORE FLAP, HAS A DEEP GOUGE ON UPPER SKIN, APPROX 70" IN FROM I/B END AND 6 INCH LONG. REMOVED DAMAGE AND BONDED FILLER AND DOUBLER, REF 51-40-20 PARA'S 6, 7, 14, 15, 18, 20, 21, 22. PRIMED AND PAINTED REF MM 51-20-151-7, THIS IS CLASSIFIED AS Aug 30, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA03246Floorbeam · corrodedFRAME 680 FLOORBEAM LBL 4", CORRODED ON UNDERSIDE OF SCREW HOLE. REMOVED CORROSION, MEASURED MATERIAL. ORG MATERIAL THICKNESS .125". REMOVED .035" REMAINING .090" FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA. FABRICATED REPAIR ANGLES AND FILLER. TREATEAug 30, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03241Seat Track · damagedUPPER MAIN DECK FLOOR STRUCTURE, UPPER BEAM CAP HAS MULTIPLE DRILL HOLES UNDER REMOVED SEAT TRACK STA 1166, RBL 25. INSTALLED TWO FREEZE PLUGS IN 1166 FLOORBEAM. PLUG TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO TO BLUE Aug 30, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03231Floorbeam · corrodedAFT UPPER MAIN DECK, CORROSION ON UPPER SURFACE OF UPPER T- CAP ON FLOOR BEAM, STA 950, LBL 10.5 AND LBL 21". REMOVED CORROSION FROM SURFACE ON UPPER T-CAP REF SRM 51-10-01. REMOVED SEAT TRACK SRM 51-30-2. REMOVED WEB SUPPORT AND BRACKET AT 950. REMOVED TWAug 29, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03201Motor · failedLOST SYS "A" HYD QUANTITY. "A" PUMPS WERE OFF FOR LESS THAN 15 MINUTES. QUANTITY REMAINED JUST ABOVE ZERO AFTER COMPLETE QRH PROCEDURES THEREFORE DID NOT TURN OFF FLUID SHUTOFF. REMOVED AND REPLACED LT AND RT FLAP PWR UNIT HYD MOTORS PER MM 27-51-062-4. OPAug 28, 2007 · N223FE · Boeing 727233 · Hydraulic Pump, AuxiliarySDR 07FDEA03175Stringer · damagedBS 740, VERTICAL ANGLE AND BULKHEAD SKIN, ABOVE STR S-28 HAS 2 EA PLUG RIVETS THROUGH ALL PARTS (PREVIOUS DAMAGE) ACCOMPLISHED WORK INSTRUCTION ON EA NR 7-5310-11068 FOR REPAIR OF 2 (EA) PLUG RIVETS THROUGH VERTICAL ANGLE, AND BULKHEAD.Aug 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA03123Skate Angle · crackedLT WING IB TE NR 3 FLAP TRACK FWD FRG IB SKATE ANGLE IS CRACKED AT 2 WING SKIN FASTENERS WBL 199, 3" FWD AND AFT OF SPAR. REPAIRED NR 3 FLAP TRACK SKATE ANGLE IAW B 272-200 SRM 51-40-3 AND 51-30-2. ALL LEAK CK'S GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 25, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA03124Skin · damagedFOUND DOUBLE DRILLED HOLE AT STA 720F PLUS 5", STR 27R IN NEW SKIN. REMOVED DAMAGE, FABRICATED REPAIR FILLER, STRUCTURAL FILLER AND REPAIR DOUBLER. TREATED AND PRIMED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS. REF SRM 53-30-3/FIG NR 3/PAGES 12-14, CAug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA03122Frame · corrodedFWD PIT BILGE, BODY FRAME CHORD IS CORRODED, BS 740, STR 27L- 28L, WL149 REMOVED AND REPLACED CHORD ANGLE REF B727 SRM 51-30-02 PG 2 DUE TO CORROSION BEING OUT OF LIMITS REF SRM 727 SRM 51-10-1, CLASSIFIED AS A MAJOR REPAIR.Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03121Stringer · crackedLWR FWD CARGO PIT FUSELAGE STRINGER UPPER O/B FLANGE HAS CRACK, STA 720 PLUS 14.5" STR 25R. REMOVED DAMAGE REF SRM 53-10-3. FABRICATED REPAIR REF SRM 53-10-3 FIG 2, SHEET 2. INSTALLED REPAIR REF 51-30-2 PG 1, PG 1-3, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA03120Frame · corrodedLWR FUSELAGE RT SIDE STA 743, RBL 7", SUPPORT FRAME AT IB SIDE OF ACCESS DOOR 3449R IS CORRODED OB SIDE REMOVED BEACON, REMOVED PANELS 3449R AND 3346. CORROSION THROUGH SUPPORT FRAME. REMOVED SUPPORT FRAME. FABRICATED NEW PARTS, ASSEMBLED NEW FRAME. INSTALAug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03119Seat Track · corrodedSEAT TRACK CORRODED FROM STA 363-372, LBL 24-25 AREA AT STA 363-372, LBL 24-25 BLENDED AND MAPPED, REF SRM 53-10-1. NDT, FOUND NO DEFECTS. AREA ROTO - PEENED REF REF SOPM 20-10-03. TREATED AND PRIMED REF SRM 51-10-2. REF EA NR 7-5310-113091, CORROSION IS Aug 25, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03118Seat Track · corrodedSEAT TRACK CORRODED, STA 386-390, LBL 44-45 AREA AT STA 386-390, LBL 44-45, BLENDED AND MAPPED, REF SRM 53-10-1. NDT, FOUND NO DEFECTS. AREA ROTO PEENED REF SOPM 20-10-03, TREATED AND PRIMED REF SRM 51-10-2 REF EA NR 7-5310-113091, LEVEL 1 CORROSION. THIS IAug 25, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03117Skin · crackedFWD ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT REPAIR, 5 HOLES ARE CRACKED NEED EVALUATION PER WIC 53308429 ITEM 5, HOLES ARE CIRCLED IN BLACK. ALSO FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT UPPER HINGE ON WO NR 36352/N00076 COMPLIED WITH EA NR 7-Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA03116Skin · crackedFWD ENTRY DOOR CUTOUT, LOWER HINGE REPAIR, 3 HOLES ARE CRACKED. NEED ENGINEERING EVALUATION PER WIC 53308429 ITEM 5. HOLES CIRCLE IN BLACK, ALSO ON NR00077 LT FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT LWR HINGE CUTOUT. REPAIR OF LOWER HINGAug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
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