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 FDEA200905211763Stringer · corrodedSNAKE PIT FWD CARGO, CORROSION AT STR 27 R, STA 740. REMOVED SNAKE PIT FLOOR PANEL TO FOM IAW SRM 51-30-2. CUT OUT SECTION OF STRINGER FOR REPAIR IAW SRM 51-10-1 AND 53-10-3 FIGURE 1. CUT OUT 26.7500 INCH. FABRICATED NEW STRINGER SECTION AND FABRICATED STRINMay 21, 2009 · N278FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200905211762Spar · crackedCRACK ANGLE FALSE SPAR LT WING STA 244 AT NR 7 SPOILER ACTUATOR BRACKET. REMOVED DOUBLER AND WEB SECTION. CUT OUT DAMAGED ANGLE SECTION IAW DWG NR SR27-57-038 REV C. INSTALLED ALL PARTS IAW DRW NR SR27-57-038 REV. C.May 21, 2009 · N278FE · Boeing 727233 · Wing SparSDR FDEA200905191744Wire · damagedAFTER TAKEOFF AND GEAR RAISED. "MAIN CARGO DOOR B" LIGHT ILLUMINATED. FOLLOWED QRH. DOOR LIGHT EXTINGUISHED RETURNED TO IND. DOOR LIGHT REILLUMINATED ON SHORT FINAL FOR 10 SECONDS. DURING T/S FOUND PIN B PUSHED BACK AT SW S9056 C/P D9834J. THIS IS THE GROUNMay 19, 2009 · N274FE · Boeing 727233 · Door System WiringSDR PCSA2009051801Sensor · out of positionNR1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR1 ENGINE AND RETURNED TO DEPARTURE. WINDMILLING 15 MINUTES, OIL PRESSURE WITHIN LIMITS. MX FOUND NR 1 STRUT SENSING ELEMENT OUT OF POSITION. THE ELEMENT WAS REPOSITIONED AND A PNEUMATIC LEAK CHECK WAS May 9, 2009 · N395AJ · Boeing 727233 · Overheat DetectionSDR FDEA200905041529Accessory Unit · failedAFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE INTO UP POSITION. RAN QRH THROUGH P6-3 L/G LEVER/LATCH C/B PULL/RESET. GEAR WOULD NOT RETRACT. RTB DUE TO FUEL CONSIDERATIONS. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC MODULE IAW 727-200 AMM 32-09-May 4, 2009 · N268FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR FDEA200905031496Angle · corrodedANGLE AT BS 740 AND STRINGER'S 27L TO 28L IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED ANGLE AND FABRICATED A NEW ONE, HEAT TREATED TO T6 CONDITION AND INSTALLED IAW SRM 53-10-1, 51-10-6, 51-30-2 AND DWG 69-43695.May 3, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200905031495Stiffener · corrodedFWD PIT, CORROSION ON OTBD SIDE OF VERTICAL STIFFENER AT BS 740, BETWEEN STRINGERS 26L AND 25L. REMOVED AND REPLACED DAMAGED CHORD WITH NEW PART IAW DWG 65-15940, SRM 51-30-5 AND SRM 51-30-2.May 3, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200904301481Skin · chafedRIGHT AFT OVERWING HATCH LOWER SKIN CHAFED ON THE EDGE. BURNISHED AREA AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER USING 2024T-3 .063 PO NR 9008186 DIMS 12 INCH BY 5 INCH AND FILLER USING 2024T-3 .050 PO NR 9008452 DIMS 1 INCH BY 1 IApr 30, 2009 · N280FE · Boeing 727233 · Emergency ExitsSDR FDEA200904251415Structure · crackedNR 7 SLAT TRAILING EDGE CHORD IS CRACKED AT INBD UPSTOP PAD REMOVED PANEL FOR ACCESS IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA DIM 29 1/2 INCH IAW B727 SRM 51-40-4. FABRICATED REPAIR PARTS FROM BAC 1514-1559 PO NR 2903470 DIM 29 1/2 INCH AND SPLICE 11 1/2 Apr 25, 2009 · N280FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200904251414Skin · corrodedAFT CARGO COMPARTMENT, FUSELAGE SKIN IS CORRODED NEXT TO STRINGER 29 L AT BS 1145 FOUND CORROSION OUT OF LIMITS IAW SRM 53-30-1, CUT OUT DAMAGED AREA. REMOVED PREVIOUS REPAIR AND U CHANNEL IAW SRM 51-30-2 FIG 3. CUT OUT DAMAGED AREA IAW SRM 53-30-2 FABRICATApr 25, 2009 · N280FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904241398Structure · crackedLEFT INBOARD MIDFLAP LOWER TRAILING EDGE CHORD CRACKED AT WBL100. CUT OUT DAMAGED AREA DIM 48 INCH, FABRICATED NEW CHORD, SPLICE ANGLE AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 57-50-2 AND 51-30-2.Apr 24, 2009 · N280FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200904241397Seat Track · corrodedCORROSION ON SEAT TRACK STA 783-804 LBL 25. REMOVED CORROSION ON SEAT TRACK AND FOUND OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK SECTION USING BAC1506-1108 PO NR 29034128 DIMS 110 INCH BY 4 INCH AND INSTALLED IAW SRM 51-30-2 AND Apr 24, 2009 · N280FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904211374Bracket · crackedLT WING L/E CAVITY NR 1 SLAT ACT ATTACH BRACKETS HAVE BOTH INSIDE PLATES CRACKED. REMOVED 2 EA WEB AND STEEL DOUBLERS ON NR 1 SLAT ACTUATOR. BRACKETS IAW EA 7-5750-126809. FABRICATED 2 EA WEBS & STEEL DOUBLERS IAW EO 7-5750-126809 HEAT TREAT WEBS FROM "O" TOApr 21, 2009 · N280FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200904211373Skin · dentedL-1 DOOR FWD HINGE AREA HAS LARGE OIL CANNED DENT IN BETWEEN UPPER AND POWER HINGE CUTOUT REPAIR DOUBLER. REPAIRED HINGE IAW EA 7-5330-126813.Apr 21, 2009 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904211372Frame · corrodedNOSE WHEEL WELL STA 294.5, RBL 18 FRAME IS CORRODED AT LOWER FLANGE REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED DAMAGED FRAME AND FABRICATED NEW FRAME IAW DRW NR 65-16312. HEAT TREATED TO T6 PER ER 2-37153-801 REV "A" ATTACHED. Apr 21, 2009 · N285FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200904211367Switch · out of adjustRIGHT GEAR AFTER DEPARTURE FROM PVD, WHEN FIRST OFFICER MOVED LANDING GEAR LEVER FROM UP TO OFF THE LIGHT REMAINED ILLUMINATED WITH A R GEAR DOOR LIGHT ILLUMINATED ON SECOND OFFICERS DOORS PANEL. COMPLIED WITH QRH AND LEFT HANDLE IN THE UP POSITION WHERE NO LApr 21, 2009 · N281FE · Boeing 727233 · Landing Gear Position and WarningSDR FDEA200904201366Stringer · corrodedFWD PIT, FWD SIDE OF BS 720 STRINGER 28 LEFT CORRODED. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1, CUT OUT DAMAGED SECTION IAW SRM 53-10-1 FIG 1, FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1, TREATED AND PRIMED REPAIR PARTS IAW SApr 20, 2009 · N280FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200904201365Skin · corrodedFWD PIT STA 720 STRINGER 28L SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-6, AREA FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA IAW SRM 53-30-2 FIG 1, FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 53-10-2, TREATED AND PRIMED REPAIApr 20, 2009 · N280FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904171328Seat Track · corrodedMAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT OUTER FLANGE, LBL 45 STA 640-680. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 PO NR 9006020 APPROX LENGTH 18 FT IAW SRM 53-10-5 FIG 1 AND 53-10-5. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INApr 17, 2009 · N280FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904161324Intercostal · corrodedFWD CARGO COMPARTMENT, CORROSION ON INTERCOSTAL AT BS 580 BETWEEN STRINGERS 28R AND 27R REMOVED INTERCOSTAL IAW B727 SRM 51-30-2. REMOVED CORROSION ON SKIN IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1. FABRICATED INTERCOSTAL. CUT OUT DAMAGED AREA OApr 16, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200904151308Skin · damagedNR 5 SLAT OUTBD LOWER SURFACE IS DAMAGED ROUTED OUT EDGE IAW SRM 51-10-1. AREA FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 2. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR IAW SRM 57-50-3 FIG 1. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-Apr 15, 2009 · N280FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200904151306Doubler · crackedAFT AIRSTAIR AREA - LOWER RT TORQUE BOX LIGHTNING HOLE HAS 2 STOP-DRILLED CRACKS AT BS 1243 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED 2 EA DOUBLERS IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. ALODINED AND PRIMED PARTS AND AREA IAW SRM 51-10-2. INSTAApr 15, 2009 · N280FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200904131286Angle · crackedLEFT WING T/E NR 7 SPOILER ACTUATOR FITTING "L" ANGLE TO LOWER PANEL IS CRACKED. REMOVED AND RETAINED NR 7 SPOILER AND FLAP TRACK FITTINGS, REMOVED AND DISCARDED DOUBLER PER DRAWING SR27-57-038 REV C. TRIMMED WEB AT LOCATION SHOW AND REMOVED INBD SECTION PERApr 13, 2009 · N285FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200904131285Skin · damagedFUSELAGE SKIN BULGING AT BS 1070 STRINGER 28R. CUT OUT DAMAGED SECTION IAW SRM 51-10-1 AND 53-10-3 FIG 1. NO CORROSION FOUND ON SKIN IAW SRM 51-10-6 PAR 3. FABRICATED REPAIR FILLER AND REPAIR SPLICE IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMApr 13, 2009 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904131284Skin · damagedFUSELAGE SKIN AT BS 1090 RBL 3 HAS A DOUBLE DRILLED HOLE. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 53-30-3 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SApr 13, 2009 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904131283Seat Track · corrodedCABIN SEAT TRACK AT BL 0 IS CORRODED BETWEEN STA 1176 AND 1140. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 51-30-5 AND DRAWING NR 53FX976 REV B. DRILLED NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND PRIMED NEW SEAT TRACK IAApr 13, 2009 · N285FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200904131282Skin · bentE/E COMPT DOOR EXTERIOR SKIN BENT ON SIDES AND AFT LIP. REMOVED INNER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED DAMAGED SKIN IAW B727 SRM 51-30-2. FABRICATED SKIN FROM 2024T3 0.040 INCH PO NR 9008450 DIM APPROX 25 I NCH BY 2 INCH IAW B727 SRM 52-40-1 FApr 13, 2009 · N285FE · Boeing 727233 · Electrical/Electronic Compartment DoorsSDR FDEA200904111268Angle · crackedNR 2 SLAT LOWER TRAILING EDGE CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD CUT OUT DAMAGED AREA DIM 25 5/8 INCH IAW SRM 51-10-1. FABRICATED ANGLE SECTION FROM BAC 1514-1559 PO NR 8307196 DIM 25 5/8 INCH AND SPLICE FROM BAC 1514-1559 PO NR 8307196 DIM 11 1/2 INCApr 11, 2009 · N280FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200904091244Spar · crackedRT WING T/E FALSE SPAR LOWER CHORD ANGLE CRACKED WBL 118 REPAIRED RT WING T/E SPAR LOWER CHORD ANGLE IAW FEDEX DRAWING SR27-57-038 REV C, STD REWORK DRAWING INBD SPOILER SUPPORT BEAM CRACK REPAIR.Apr 9, 2009 · N285FE · Boeing 727233 · Wing SparSDR FDEA200904091243Skin · corrodedOUTER SKIN BULGED AT RT SIDE STA 1303, BELOW NR 3 ENGINE PYLON CUT OUT BULGED AREA, DIM 1 1/2 INCH BY 2 INCH IAW B727 SRM 53-30-3 FIG 24, DETAIL 1. FABRICATED REPAIR PARTS AND STRUCTURAL FILLER, & DOUBLER IAW SRM 53-30-3 FIG 24. TREATED AND PRIMED REPAIR PARApr 9, 2009 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904091241Stringer · dentedFWD CARGO COMPT STR 27L UPPER FLANGE IS DENTED BETWEEN STA 480-500. REMOVED WEB FOR ACCESS IAW SRM 51-30-2. CUTOUT STRINGER SECTION FROM BS 490 TO 510 IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED PApr 9, 2009 · N285FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200904091240Stringer · gougedFWD CARGO COMPT STR 27L UPPER FLANGE IS GOUGED JUST AFT OF STA 480 BLEND OUT DAMAGE IAW SRM 51-10-1. FOUND OUT OF LIMITS IAW SRM 53-10-3 FIG 1. CUTOUT DAMAGED SECTION OF STRINGER FROM BS 476 TO 490 IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND SPLIApr 9, 2009 · N285FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200904081229Skin · dentedPROTRUDING DENT, EXTERIOR SKIN OF C-3 DOOR, TOP OF DOOR BETWEEN RIBS, BS 1110 CHECKED DENT LIMITS AND FOUND OUT OF LIMITS IAW SRM 52-00-2. CUT OUT DAMAGED AREA IAW SRM 52-00-3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-3 FIG 3. TREATED AND PRIMED DOUBLER REPAApr 8, 2009 · N280FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200904041180Skin · gougedMAIN CARGO AREA STA 660 S2L GOUGE ON SKIN NEXT TO UPPER INTERCOSTAL EXTENSION. REPAIRED GOUGE ON INNER SKIN AT STA 660 STR 2L IAW FX P - F SRM STC SA1767SO AND SA1768SO FIG 1B SRM 53-30-3. BLENDED GOUGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1. CUT OUApr 4, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904021163Skin · crackedLT AFT SERVICE DOOR (L-2) FWD LOWER SIDE SKIN HINGE CUT-OUT AT UPPER AFT CORNER HAS ABOUT 1/2 INCH LONG CRACK AT SKIN RADIUS. TRIMMED OUT CRACK AREA IAW FX EA 7-5210-126807 ITEM 1. NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. FABRICATED FILLER AND REPAIR ANGLApr 2, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200904021162Skin · crackedLT AFT SERVICE DOOR (L-2) FWD UPPER SIDE SKIN HINGE CUT-OUT AT LWR AFT CORNER HAS ABOUT 1 INCH LONG CRACK AT SKIN RADIUS. TRIMMED OUT CRACK AREA IAW EA 7-5210-126807 ITEM 1. HFEC INSPECTED AREA IAW NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. FABRICATED FILLApr 2, 2009 · N283FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200903261076Web · crackedNR 1 NOSE COWL INTERIOR WEB IS CRACKED, 2 PLACES AT LIGHTNING HOLE, NAC STA 77.5 REMOVED AFT LOWER PANEL AT NR 1 ENG NOSE COWL FOR FOM IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. HFEC INSPECTION PERFORMED IAW NDTM 51-00-00 FIG 23, PT 6. NO DEFECTMar 26, 2009 · N283FE · Boeing 727233 · Nacelle/Pylon Miscellaneous StructureSDR PCSA2009031101Fire Warning · false activationFIRE WARNING LOWER CARGO ACTIVATED AFTER TAKEOFF. DID AIR RETURN TO MKJP. INSPECTED LOWER CARGO COMPARTMENTS FOR EVIDENCE OF FIRE. NO EVIDENCE OF FIRE FOUND. PERFORMED OPERATIONAL TEST OF THE LOWER SMOKE DETECTION SYSTEM. CHECK NORMAL PER THE AM.Mar 10, 2009 · N994AJ · Boeing 727233 · Fire DetectionSDR FDEA200903070860Skin · dentedWING STATION 544 NR 6 SLAT L/E SKIN HAS LARGE DENT. EVALUATED DENT & FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 2, CUT-OUT DAMAGE & FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2 AND INSTALLED IAW SRM 57-50-3 FIG 1 Mar 7, 2009 · N282FE · Boeing 727233 · Leading Edge DevicesSDR PCSA2009030901Actuator · brokenON GEAR RETRACTION LEFT MAIN GEAR RED GEAR LIGHT AND DOORS LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND THE LEFT MAIN GEAR LOCK ACTUATOR ROD END BROKEN. THE LOCK ACTUATOR WAS REPLACED, A RETRACTION TEST WAS PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE.Mar 7, 2009 · N994AJ · Boeing 727233 · Landing Gear ActuatorSDR FDEA200903020788Spar · looseNR 8 RIGHT WING FALSE SPAR LOWER CHORD ABOVE MLG HAS LOOSE FASTENERS AND FOUND CRACKED. REPAIRED IAW STANDARD REPAIR DRAWING SR27-57-038 REV. C.Mar 2, 2009 · N282FE · Boeing 727233 · Wing SparSDR FDEA200902270760Angle · crackedLEFT WING T/E BELOW NR 7 SPOILER HAS CRACKED ANGLE AT FALSE SPAR LOWER CHORD. REPAIRED IAW STANDARD REWORK DRAWING SR27-57-038 REV. C.Feb 27, 2009 · N282FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200902270759Structure · misrepairedFASTENERS WITH IMPROPER ED STA 460 STR 27L IN MCD DOUBLER. REMOVED FASTENERS FROM AREA FOR ACCESS IAW SRM 51-30-2. TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3 FIG. 1A. FABRICATED DOUBLER & FILLERS IAW SRM 53-30-3 FIG 1A. TREATED AND PRIMED IAW SRM 51-10-2. INSTFeb 27, 2009 · N282FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200902270758Frame · puncturedFORWARD CARGO AREA BS 540 STR 22L HAS PUNCTURED FRAME. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG. 1. FABRICATED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1.Feb 27, 2009 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200902270757Bulkhead · crackedRT WHEEL WELL BS.870 BULKHEAD WEB CRACKED IN 2 PLACES AT LOAD CONTROL VALVE CUTOUT RBL10-16. CUT-OUT DAMAGE AREA IAW SRM 53-10-9 FIG 5. C/W HFEC INSP OF CUT-OUT EDGE IAW NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. CAD PLATED REPAIR PARTS IAW SRM 51-10-6. Feb 27, 2009 · N282FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA200902270753Attach Bracket · crackedNR 8 SLAT ACTUATOR INBD AND OTBD ATTACH BRACKET INSIDE PLATES ARE CRACKED. REMOVED I/B & O/B BRACKETS AT NR 8 SLAT ACTUATOR IAW EA 7-5750-126801 AND SRM 51-30-2 AND S.B. B727-57-0130. FABRICATED 2EA. STEEL DOUBLERS AND 2EA. WEBS IAW EA 7-5750-126801 AND S.B. Feb 27, 2009 · N282FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200902270750Skin · crackedLEFT WING T/E OUTBD AILERON INBD EDGE LOWER SKIN CRACKED AND BENT WBL 492.0. TRIMMED OUT DAMAGE IAW SRM 51-10-1 & 57-50-1 FIG 4. CW HFEC AND NO CRACKS INDICATED, MATERIAL LOSS 0.100 IN LENGTH & FOUND WITHIN LIMITS IAW SRM 57-50-1 FIG 4. TREATED & PRIMED EFeb 27, 2009 · N282FE · Boeing 727233 · AileronsSDR FDEA200902230670Structure · crackedRT WING INBD MID FLAP REAR CHORD CRACKED AT 2ND CUTOUT FROM INBD WBL 96. REMOVED MID FLAP LWR SKIN FOR ACCESS, REMOVED DAMAGED EXTRUDED SECTION. FABRICATED NEW EXTRUDED SECTION USING 7075T-6 PO NR 8306161 DIMS 48 INCH LONG AND INSTALLED NEW EXTRUDED SECTION,Feb 23, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR CA090224001Windshield · failed(CAN) THE ACFT SUFFERED AN OUTER PANE FAILURE ON RT WINDSHIELD AT THE TOP OF THE CLIMB. THE ACFT DIVERTED AND LANDED WITHOUT FURTHER PROBLEM. MX REPLACED THE WINDSHIELD AND THE ACFT WAS RETURNED TO SERVICE.Feb 22, 2009 · Boeing 727233 · Flight Compartment WindowsSDR FDEA200902210623Web · crackedAFT AIRSTAIR RT WEB AT BS 1223 LIGHTENING HOLE HAS A CRACK. ROUTED OUT CRACKED AREA OF RT TORQUE BOX WEB AT STA 1223 IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-40-2 FIG 1Feb 21, 2009 · N258FE · Boeing 727233 · Fuselage Miscellaneous Structure
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