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 08FDEA00207Floorbeam · corrodedFLOORBEAM CORRODED AT STA 1030, LBL 19, WL 208, UPPER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REF FED EX PF SRM 53-10-1 PG 26 AND 38. ORIGINAL THICKNESS IS .125" MATERIAL REMOVED IS .030" MAT. REMAINING IS .095'. INSTALLED REPAIR ANJan 19, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00206Frame · crackedFWD PIT STUB FRAME EXTENSION AT BS 540, 22L IS CRACKED OUT OF RADIUS. MARKED END OF CRACK WITH BLACK DOT ON FWD SIDE. REMOVED STUB FRAME EXTENSION AT STA 540, STR 22R, REF SRM 51-30-2. FABRICATED NEW STUB FRAME, HEAT TREATED ON NR N00785, 8130-3 NR 2008-01-Jan 19, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00205Frame · damagedCABIN FRAME REPAIR INSTALLED AT BS 640, STR S-11R, FRAME HAS TOOLING DAMAGE ON AFT FACE OF FRAME WEB AT UPPER RIVET BUCKTAIL BLENDED DAMAGE AREA AT CABIN FRAME STA 640, STR 11R REF SRM 53-10-1 FIG 1. ORIGINAL MATERIAL .056 INCH. MATERIAL REMAINING .048 INCH'Jan 19, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00204Flange · corrodedRT W/W PRESSURE DECK FUEL SHROUD MOUNTING FLANGE IS CORRODED AT BS 890 TO 888, RBL 63", WL 200. REMOVED CORROSION SRM 51-10-1 PG 15,15. ORIG THICKNESS IS .100", REMAINING "T" IS .061, LOSS OF .039' REF SRM 53-10-1 FIG 1. MEASURED USING TOOL AAR 18172, DUE DJan 19, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00177Stringer Clip · crackedSTRINGER CLIP CRACKED STATION 804, STRINGER 7L REMOVED STRINGER CLIP, STA 804, STR 7, IAW SRM 51-30-2. MATCHED DRILLED NEW CLIP P/N 65-45313-2, REF IPC 53-10-00 IFG 35ZZ SHT 1, PG 1 ITEM 165 IAW DWG 65-45313. INSTALLED NEW CLIP IAW SRM 51-30-2 P1.Jan 16, 2008 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 08FDEA00176Stringer Clip · crackedSTRINGER CLIP CRACKED AT STATION 849 STR 7L REMOVED STRINGER CLIP STA 849, STR 7L, IAW SRM 51-30-2. MATCHED DRILLED NEW CLIP P/N 65-45313-2 REF IPC 53-10-00 FIG 35ZZ SHT 1 PG 1 ITEM 165 DWG 65 -45313. INSTALLED NEW CLIP IAW SRM 51-30-2 P1.Jan 16, 2008 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 08FDEA00174Frame · wornCABIN BS 500 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE, REMOVED MAXIMUM OF .036" FROM ORIGINAL FRAME THICKNESS OF .056" WITH .020" REMAINING. OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED.Jan 16, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00172Structure · crackedMAIN CARGO DOOR CORNER TRIM CRACKED STOP DRILLED CRACK AND NDT, NO DEFECTS NOTED. VARIFIED MATERIAL FOR REPAIR REF DWG 25FX1253 FABRICATED DOUBLER REF SRM 51-40-3. TREATED AND PRIMED REPAIR REF MM 51-20-000. INSTALLED REPAIR REF SRM 51-40-3. THIS IS CLASSIJan 16, 2008 · N267FE · Boeing 727233 · Cargo/Baggage DoorsSDR 08FDEA00171Support Angle · crackedMAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED BS 600, LBL 14. REPLACED SUPPORT ANGLE AT BS 600, LBL 14, REF SRM 51-30-2, PG 7. FABRICATED NEW SUPPORT REF FED EX DRAWING DWG 25FX 1253. THIS IS CLASSIFIED A MINOR REPAIR.Jan 16, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00141Module · failedPRESSURIZATION LOSS AT FL230, CABIN ALT 10,000' DESCEND TO (FL)10,000' PSID 0 (ZERO) LOSS OF HEAT. ACFT HARD TO HEAT ON GROUND. OUTFLOW VLV INDICATED CLOSED BUT DID NOT RESPOND IN "MAN D.C.". FOUND SMOKE CONTROL SWITCH ON P4-78 PANEL STUCK IN THE "ON" POSJan 15, 2008 · N282FE · Boeing 727233 · Cabin Pressure Control SystemSDR 08FDEA00154Strap · crackedCABIN FLOORBEAM STABILIZER STRAP CRACKED AT STATION 344 AIRCRAFT CENTER LINE, WL 200. STOP DRILLED CRACKS AND FAB AND INSTALLED A REPAIR PLATE REF SRM 53-10-8, FIG NR 6. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00153Angle · crackedMAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 600, LBL 14. REPLACED SUPPORT ANGLE AT BS 600, LBL 14, REF SRM 51-30-2 PG 7. FABRICATED NEW SUPPORT REF FED EX DWG 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00152Frame · wornCABIN BS 520 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S-11R, REMOVED DAMAGE FROM INNER CHORD REF SRM 51-10-1 PG 3. NDT ACCOMPLISHED ORG MAT. .056'' MAT. REMOVED UP TO .018'' EXCEEDED 10 PERCENT ALLOWABLE DAMAGE. FABRICATED REPAIR DOUBJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00151Frame · wornCABIN BS 580 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R. BLENDED WORN AREA ON 580 FRAME. VERIFIED MATERIAL BY NDT. ORIGINAL "T" AT .056" MATERIAL LOSS AT LOWEST POINT IS .011", .045 REMAINING. EXCEEDS 10 PERCENT MAX LIMITS REFSJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00150Frame · wornCABIN BS 620 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE ON FRAME INNER CHORD, STA 620 STR 11R, FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .056" .008" BLEND, .048" REMAINING. FABRICATED NEW DOUBLER REF SRM 51-40-3 ANDJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00149Support Bracket · crackedAIR CONDITIONING DISTRIBUTION BAG DUCT SUPPORT BRACKET IS CRACKED AT BOLT HOLES (3) STATION 740, LBL 5. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET AND INSTALLED. REFERENCE SRM 51-30-2 AND BOEING DOCUMENT NR 65-47707/ ITEM NR 2. CLASSIFIED AS A MINOR RJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00148Support Angle · crackedMAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 640, LBL 14. REPLACED SUPPORT ANGLE AT BS 640, LBL 14 REF SRM 51-30-2 PG 7. FABRICATED NEW SUPPORT REF SRM 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00147Support Angle · crackedMAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 620, LBL 14. REPLACED SUPPORT ANGLE AT BS 620, LBL 14 REF SRM 51-30-2 PG 7. FABRICATED NEW SUPPORT REF FED EX DWG 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00146Seat Track · corrodedMAIN CARGO SEAT TRACK IS CORRODED, BS 1090 - 1130 , RBL 46 REMOVED CORROSION ORG THICKNESS 1.36, LOSS OF .012" MIN THICKNESS 1.348". FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATED NEW TRACK. REF SRM 51-30- 02, SRM 53-10-2, BOEING DWG BAC1520-Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00145Splice · corrodedAFT PIT FLOOR BOARD SPLICE STRAP BETWEEN NR 3 AND 4 PANELS HAS LIGHT CORROSION ON BOTH SIDES. REMOVED CORROSION FROM AFT PIT FLOORBOARD SPLICE STRAP BETWEEN NR 3 AND 4 IAW SRM 51-10-1 FIG 1, AMOUNT EXCEED MAX ALLOWABLE LIMITS IAW SRM 53-10-1 FIG 1, SHT 2. FAJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Floor PanelSDR 08FDEA00144Seat Track · corrodedSEAT TRACK CORRODED, STA 849 - 870, LBL 44-47 CORROSION DAMAGE EXCEEDED LIMITS SRM 53-10-1. REMOVED SEAT TRACK REF SRM 551-30-2 PG 1. FABRICATED REPLACEMENT TRACK REF DWG 69-4121. TREATED AND PRIMED REF SRM 51-10-2, INSTALLED REPLACEMENT SRM 51-30-2. THIJan 15, 2008 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00143Frame · wornCABIN BS 680 FRAME INNER CHORD WORN FROM CONTACT WITH LT SIDEWALL FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED DOUBLER IAW SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00142Angle · crackedELECTRIC HYD PUMP MOUNT TRAY CRACKED ON AFT SIDE, BS 955A, LBL 43 WL 143. REMOVED ANGLE FROM ELE HYD PUMP MOUNT TRAY AFT SIDE BS 955A, LBL 43. FABRICATED, TREATED, PRIMED AND INSTALLED.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 08FDEA00140Seat Track · corrodedSEAT TRACK CORRODED (3) THREE PLACES AT STA 1130, LBL, 47, WL 208 REMOVED CORROSION ON SEAT TRACK STA 1130, LBL 47, FOUND TO BE WITHIN LIMITS. REMOVED DOUBLER AND CORROSION. DOUBLER FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNESS .0132", REMAINING Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00139Floor Panel · corrodedFWD PIT NR 1 FLOOR PANEL HAS LIGHT CORROSION AROUND ALL FASTENER HOLES VERIFIED MATERIAL 2024 T3 .050" IAW DWG 65-67205 AND P/N 65-67205-5., A TAG NR A40813 AND PO NR 1022427. FABRICATED NEW FWD PIT NR 1 FLOOR PANEL P/N 65-67205-5 AND SRM 51-10-1 PG 12, ALODIJan 15, 2008 · N267FE · Boeing 727233 · Fuselage Floor PanelSDR 08FDEA00138Frame · damagedCABIN BS 660 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT STR 11R REMOVED DAMAGE FROM INNER CHORD AND FOUND AREA TO BE OUT OF LIMITS, REF SRM 51-10-1 PG 3, B727 NDT MANUAL PART 4, 51-00-0 FUG 2 TOOL NR IN 22-0028 DUE DATE 2/21/08 AND 53-10-3Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00137Floor Panel · corrodedLAV FLOOR PANEL STA 303.6 -344 CORRODED IN NUMEROUS PLACES FABRICATED NEW FLOOR PANEL, PRIMED AND PAINTED REF AMM 51-20-02, MM 51-20-31, 51-20-151. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Floor PanelSDR 08FDEA00136Frame · wornCABIN BS 560 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R INSTALLED DOUBLER IAW SRM 53-10-4 FIG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00135Frame · wornCABIN BS 640 FRAME, INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE AREA, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR REF SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00134Intercostal · crackedMAIN CABIN FLOOR STRUCTURE, STA 303, LBL 50, INTERCOSTAL SUPPORT CRACKED REPAIRED INTERCOSTAL SUPPORT AT BS 303, LBL 50. REF SRM 5I-40-02. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00133Frame · damagedCABIN BS 600 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S-11 REPAIRED FRAME AT STA 600, STR 11 R IN RE WITH SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 15, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00004Support Beam · crackedRT WING INBD UPPER WING PANEL SUPPORT BEAM IS CRACKED JUST FWD OF MLG BEAM 10" O/B OF UPLOCK T/T. REMOVED SUPPORT BEAM FROM A/C REF SRM 51-30-2. STOP DRILLED CRACK REF SRM 51-10-1. FABRICATED AND INSTALLED REPAIR ON SUPPORT REF SRM 51-40-2. REINSTALLED SUPJan 2, 2008 · N268FE · Boeing 727233 · Wing Main, Frame StructureSDR 07FDEA05147Fitting · corrodedNR 2 LOWER CARGO DOOR THRESHOLD TIEDOWN FITTING 23" FROM AFT EDGE OF CUT OUT CORRODED ON UPPER SURFACE. REMOVED AND REPLACED TIEDOWN FITTING REF DWG 69-47673 REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.Dec 27, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA05143Skin · gougedRIGHT WING INBOARD MID FLAP UPPER SURFACE, SKIN GOUGED AT OUTBOARD SIDE. BLENDED DAMAGED AREA, NDT VERIFIED NO DEFECTS. TREATED, PRIMED AND TEFLON PAINTED, REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7 AND EA NR 7-5750-113963 THIS IS CLASSIFIED AS A MINOR.Dec 27, 2007 · N268FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA05142Skin · chafedRIGHT WING INBOARD MID FLAP UPPER SURFACE CHAFED AT INBOARD SIDE BLENDED DAMAGE AREA, NDT VERIFIED NO DEFECTS, TREATED, PRIMED, AND TEFLON PAINTED REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7, AND EA 7-5750-113963. THIS IS CLASSIFIED AS A MINOR REPAIR.Dec 27, 2007 · N268FE · Boeing 727233 · Trailing Edge FlapsSDR 2007FA0001109Bracket · crackedRT PREVENTATIVE MODIFICATION FWD IB ANGLE CRACKED AT BS 760.95. REPAIRED CRACK AT RT BL 70.5, BS 760.95, UPPER AND LOWER MOST FORWARD HOLES. OVERSIZED CRACKED HOLE IAW 57-112. NDT PERFORMED TO CONFIRM CRACK TERMINATION. COMPLIED WITH TERMINATION REPAIR IAWDec 24, 2007 · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA05138Ejector Valve · failedENG ANTI ICE VALVES WERE ON FOR T/O. IMMEDIATELY AFTER T/O, THE NR 2 ENGINE ANTI ICE DUCT TEMP WENT FULL SCALE HOT AND THE OVERHEAT LIGHT ILLUMINATED. WITHIN 30 SECS, LT PACK TRIPPED AND ENG FAIL LIGHT ILLUMINATED. STANDARD BLEED/PACK CONFIGURATION FOR T/O.Dec 24, 2007 · N264FE · Boeing 727233 · Air Intake Anti/De-Ice SystemSDR 07FDEA05122Floorbeam · corrodedCORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM AT FS 1130, LBL 51, WL 208. REMOVED CORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM STA 1130, LBL 51, FOUND TO BE OUT OF LIMITS REF SRM 53-10-8. SAME LOCATION SEAT TRACK FOUND TO BE OUT OF LIMITS. FABRICATED ANDDec 22, 2007 · N268FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA05120Seat Track · corrodedCORROSION ON I/B SIDE OF SEAT TRACK CROWN AND UNDER DOUBLER PLATE, BS 1137 TO BS 1125M RBL 45, WL 208. REMOVED DAMAGED SECTION OF SEAT TRACK STA 1100 - 1135, RBL 45. FABRICATED AND INSTALLED SEAT TRACK AND REPAIR ANGLES REF SRM 53-10-5 FIG 1 SRM 51-30-2 PG Dec 21, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05119Angle · corrodedFORWARD LOWER PIT FLOOR STRUCTURE LEFT SIDE STA 570 TO STA 650, Z- ANGLE CORRODED ON LOWER SURFACE REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED AND INSTALLED. REF SRM 51-40-2 AND SRM 53-10-1.Dec 21, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA05118Floorbeam · corrodedCORROSION AROUND NUT PLATE HOLES ON TOP OF FLOORBEAM AT SEVERAL LOCATIONS, FS 1130, LBL 64 TO RBL 64, WL 208. BLENDED DAMAGE AREA STA 1130, RBL 64, FOUND TO BE OUT OF LIMITS, REF SRM 53-10-8 TOOL NR IN17-0023 CAL DATE DUE 2-13-08. REMOVED DAMAGE AREA, REF SRDec 21, 2007 · N268FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA05117Switch · inoperativeAFTER RAISING LANDING GEAR, RED NOSE GEAR LIGHT REMAINED ILLUMINATED WITHOUT A CORRESPONDING DOORS LIGHT, OR GREEN GEAR LIGHT. CYCLED GEAR PER QRH PROCEDURES WITH NO POSITIVE RESULTS. LIGHT REMAINED ILLUMINATED ENTIRE FLIGHT. AIRCRAFT INCURRED A MAINTENANCEDec 21, 2007 · N266FE · Boeing 727233 · Nose/Tail Landing GearSDR 07FDEA05114Cargo Track · corrodedMAIN DECK FLOOR TIE DOWN FITTING ASSY IS CORRODED BS 950, RBL 57, WL 208 REMOVED CORROSION ON TIE DOWN FITTING, AND IS OUT OF LIMITS. DRILLED HOLES IN NEW TIE DOWN FITTING AND INSTALLED, REF SRM 51-30-2 AND SRM 51-30-5 THIS IS CLASSIFIED AS A MINOR REPAIR.Dec 20, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05105Light · inoperativeUNSAFE NOSE GEAR INDICATION. NO GREEN NOSE GEAR LIGHT WHEN GEAR HANDLE DOWN. FOLLOW CHECKLIST TO LOWER NOSE GEAR MANUALLY, THAT WAS UNSUCCESSFUL. NO GREEN LIGHT. GREEN LIGHT TESTED GOOD WHEN DEPRESSING LENS CAP BUT WOULD NOT TEST GOOD WHEN USING APD TEST Dec 20, 2007 · N266FE · Boeing 727233 · Landing Gear Position and WarningSDR 07FDEA05108Channel · corrodedFORWARD LAV SUPPORT STRUCTURE STA 303 TO 306, RBL 15, HAT CHANNEL CORRODED ON LOWER SURFACE REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, TREATED AND PRIMED AND INSTALLED. REF SRM 51-30-2 AND BAC DWG 65-26173. THIS IS CLASSIFIED AS A MINOR REPAIR.Dec 20, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA05103Stringer · damagedEXT FUSELAGE SKIN 2 RIVETS HAVE LIGHTING STRIKES AT STR S-8R BS 510 AND 513 REMOVED LIGHTNING STRIKE DAMAGE TO SKIN AND STR 8R. INSTALLED SKIN DOUBLER USING .050"2024 T-3 FILLER .040 2024 T-3, REF 53-30-2 FIG 20 STR 8. REPAIRED USING BAC 1598-146 REF SRM 53-Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA05102Floor Support · corrodedLWR FWD CARGO PIT, FLOOR SUPPORT Z-ANGLE HAS WIDE SPREAD CORROSION WITH A CRACK AT STA 720 RBL 25" CORROSION FROM 710-720D REMOVED Z-ANGLE AT FWD CARGO PIT STA 720, RBL 25" FROM 710 TO 720D REF SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW "Z" ANGLE P/N 65C1Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA05101Stringer · crackedSTR 5L CRACKED ON LOWER SIDE UP RIGHT AT ATTACH RIVET AT STA 353 FABRICATED NEW STINGER, TREATED AND PRIMED REF SRM 51-30-2 AND 51-10-2. INSTALLED STRINGER THIS IS CLASSIFIED AS A MAJOR REPAIRDec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA05100Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE, LEFT SIDE STA 560 TO 580, LBL 24 SEAT TRACK, INBOARD FLANGE CORRODED ON UPPER SURFACE, FOUND CORROSION TO BE OUT OF LIMITS. NO CORROSION ALLOWED, IAW P-F SRM 53-10-1, FIG 3A PG 3. REPAIRED SEAT RAIL DAMAGE SECTION, STA 560 TO 670Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05099Frame · damagedMAIN CABIN FRAME HAS DEEP WEAR AT STA 1166 AND STR 8L REMOVED DAMAGE SECTION OF FRAME STA 1166 AT STR 8L. FABRICATED AND INSTALLED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA. THIS IS CLASSIFIED AS A MAJOR REPAIR.Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Frame
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