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 05FDEA04202Repair · unknownFOUND REPAIR LOCATED AT FUSELAGE RIGHT SIDE STA 1174-1203 STR19-20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH FED EX EA 7-5330-92597 PART 1, FUSELAGE SKIN, REWORK OF EXIDec 9, 2005 · N220FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA04074Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED AT STA 955.0E STRINGER 28R TO 29R. REMOVED AND INSTALLED DOUBLER, SHEAR TIE AND RAILS 1AW B727 SRM 51-10-2, 51-30-02, 51-10-6 AND 53-10-4. MINOR REPAIR SIGNED BY TIMCO MECH.33 NR 7921 QC 362.Dec 2, 2005 · N220FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA04062Repair · unknownEXISTING REPAIR DOUBLER ON C-1 CARGO DOOR FORWARD LOWER CORNER IS NOT PER SRM DATA. REMOVED AND REPLACED REPAIR DOUBLER IAW B727 SRM 52-00-3, FIG 3.Dec 1, 2005 · N220FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA04059Repair · improperEXISTING REPAIR AT STA 1148-1166 STR 25L IS NOT PER SRM DATA. INSTALLED EXTERNAL REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 3.Dec 1, 2005 · N220FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA04055Skin · damagedRESKIN C-3 DOOR DUE TO, TOO MANY REPAIRS ON OUTER SKIN. REMOVED AND REPLACED SKIN P/N 65-56927-2 IAW B727 SRM 51-10-2,51-30-2 AND 51-30-5. MINOR REPAIR SIGNED BY NR 1560 QC334.Dec 1, 2005 · N220FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA04048Repair · unknownFOUND REPAIR LOCATED AT FUSELAGE, RIGHT SIDE STA 1174-1203 STR 19-20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED NEW REPAIR IAW FED EX B727 P-F SRM 53-30-3 FIG.1A.Dec 1, 2005 · N220FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA04022Flap Track · corrodedLEFT WING OUTBOARD FLAP OUTBOARD TRACK, FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED ALL PITTING FROM BORE "D ", FABRICATED AND INSTALL REPAIR BUSHING AND FINAL REAM ID, IAW BOEING OHM 57-40-01 SIGNED BY TIMCO MECH NR 4951 AND QC 280, CARD N0084Nov 29, 2005 · N220FE · Boeing 727233 · Trailing Edge FlapsSDR 05FDEA04021Floorbeam · corrodedFOUND MAIN CABIN FLOORBEAM T-CAP CORROSION BS 560 LBL 3 TO LBL 24. COMPLIED WITH FLOORBEAM UPPER CHORD REPAIR AT STA 560 LBL 3 TO LBL 24, IAW B727 SRM 53-10-8 FIG 3, SIGNED BY TIMCO MECH NR 5154 AND QC 321.Nov 29, 2005 · N220FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03940Repair · corrodedAFT CARGO, DOUBLER CORRODED, BETWEEN STR 21 AND 22L, STA 1165. ALL WORK ACCOMPLISHED ON FED EX N/R N00243, ENTERED IN ERROR.Nov 22, 2005 · N220FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03939Skin · corrodedAFT PIT HAS EXFOLIATED SKIN AT STA 1044 TO 1050 STR 29R TO STR 28R. ALL WORK ACCOMPLISHED ON SDR 05-4182.Nov 22, 2005 · N220FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03938Repair · improperEXISTING REPAIR AT STA 1148-1166 STR 25L IS NOT PER SRM DATA. INSTALLED EXTERNAL REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 3.Nov 22, 2005 · N220FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA11200501Flap System · disconnectedON CLIMBOUT, CREW REPORTED OB TRAILING EDGE FLAPS WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT OB FLAP POSITIONING SYSTEM, THE OB FLAP POSITION INDICATOR CONNECTOR WAS SUSPECTED NONov 20, 2005 · N495AJ · Boeing 727233 · Trailing Edge Flap Control SystemSDR PCSA11190501Flow Valve · defectiveON CLIMBOUT, CREW REPORTED PRESSURIZATION SYSTEM WILL NOT MAINTAIN CABIN ALTITUDE. AIRCRAFT RETURNED BACK TO DEPARTURE AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT PRESSURIZATION SYSTEM AND FOUND FLOW CONTROL AND MODULATING VALVE AT FAULT, Nov 19, 2005 · N994AJ · Boeing 727233 · Cabin Pressure Control SystemSDR 05FDEA03904Stringer · corrodedAFT CARGO COMPARTMENT BILGE AREA, STR 29L HAS CORROSION STA 1010. REMOVED DAMAGED SEGMENT OF KEEL STA 980-1007 STR 29L. REMOVED PRODUCTION SPLICE CHANNEL. REMOVED SECTION OF SHEAR TIE, FRAME 990 STR 29-28. FABRICATED AND INSTALLED NEW KEEL SEGMENT, PRODUCTNov 19, 2005 · N266FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 05FDEA03895Floorbeam · corrodedMAIN CABIN FLOORBEAM TEE CAP CORRODED STA 620 RBL 10 AND RBL15. REMOVED DAMAGED AREA AND INSTALLED FILLER AND 2 (EA.) REPAIR ANGLES IAW B727 SRM 53-10-8 FIG 8. ALODINED AND PRIMED SAME IAW B727 SRM 51-10-2.Nov 18, 2005 · N220FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03891Doubler · corrodedAFT CARGO DOUBLER CORRODED, BETWEEN STR 21L AND 22L STA 1165. COMPLIED WITH FED EX EA 7-5330 91316-FUSELAGE- CORROSION AT AFT LAV SERVICE DOOR CUTOUT-REPAIR . TIMCO MECH #2891 QC227 MAJOR REPAIRNov 18, 2005 · N220FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA03831Cargo · leakingFUMES IN COCKPIT STRONG ODOR, EMERGENCY EVACUATED ON TAXIWAY. DEPLOYED SLIDE. HAZMAT TEAM DETERMINED THE FUMES AND ODOR WERE COMING FROM THE HAZMAT CAN. HAZMAT TEAM DOWNLOADED HAZMAT CAN AND FOUND ONE DRUM LEAKING UN1993 (TERDODECIL MERCAPTANO). CLEANED UPNov 15, 2005 · N219FE · Boeing 727233 · Cargo CompartmentsSDR 05FDEA03827Repair · properFOUND REPAIR AT STA 375 STR 29L TO STR 29R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 375 STR 29L TO 29R WAS DETERMINED TO BE IAW EO NR 7-3450Nov 15, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA11150501Windshield · crackedFLIGHT 8213 DURING CLIMBOUT FROM MIA CREW REPORTED LEFT HAND L1 CAPTAINS WINDSHIELD CRACKED. AIRCRAFT RETURNED BACK TO MIA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS L1 WINDSHIELD IAW B727 MM CH 56-11-11 AND REMOVED AND RENov 15, 2005 · N495AJ · Boeing 727233 · Flight Compartment WindowsSDR 05FDEA03817Repair · properFOUND REPAIR AT STA 303.9 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 303.9 STR 15L WAS DETERMINED TO BE IAW EO 7-5330-7-2345 PT2, BASED ON EXTERNANov 15, 2005 · N266FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA03815Repair · properFOUND REPAIR AT STA 303.9 STR12L, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 303.9 STR 12L WAS DETERMINED TO BE IAW EO NR 7-5330-7-2345 PT.2 BASED ON AN ENov 14, 2005 · N266FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA03814Repair · improperREPAIR AT STA 328 STR 20L, NOT ACCOMPLISHED USING FAA APPROVED DATA, DETERMINED TO BE A MAJOR REPAIR, IAW FEDEX GMM 6-2-100 (REF :N00649). REMOVED NON-CONFORMING DOUBLER, FABRICATED NEW DOUBLER IAW SRM 53-30-3 FIG 1 WITH 2024 T3 .050 BATCH NR 0000999692 AND INov 14, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03813Repair · damagedFOUND REPAIR AT STA 420 STR 20L, NOT ACCOMPLISHED USING FAA APPROVED DATA. FEDEX GMM 6-2-100, DETERMINED TO BE A MAJOR REPAIR(REF:00665). REMOVED EXISTING DOUBLER AND FILLER IAW SRM 51-30-2, FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED NEWNov 14, 2005 · N266FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA03777Repair · undamagedFOUND REPAIR LOCATED AT STA 480 STR 23R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 480 STR 23R WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. BASED ON EXTNov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03783Repair · improperREPAIR AT STA 700 STR 29R-STR 29L. NOT ACCOMPLISHED USING FAA DATA FEDEX GMM 6-2-100 MAJOR REPAIR.(REF:N00637). REMOVED EXISTING REPAIR IAW SRM 51-30-2 SH1. DRILLED NEW HOLES IAW SRM 53-30-3 FIG 1 SH 8, FABRICATED NEW FILLER AND DOUBLER RESPECTIVELY FROM 202Nov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03782Repair · properFOUND REPAIR AT STA 740 STR 3R, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 740 STR 3 WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 5 BASED ON AN EXTERNAL VISUNov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03781Repair · properFOUND REPAIR ON LT HORIZONTAL STAB LEADING EDGE 40" FROM THE INBD END. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR ON LT HORIZONTAL STAB LEADING EDGE 40" FROM INNov 11, 2005 · N266FE · Boeing 727233 · Horizontal Stabilizer StructureSDR 05FDEA03780Repair · properFOUND REPAIR AT STA 1020 STR 26L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1020 STR 26L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 5, BASED ON AN EXTERNNov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03779Repair · undamagedFOUND REPAIR ON LT OUTBD FORE FLAP INBD LEADING EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT OUTBD FORE FLAP I/B L/E WAS DETERMINED TO BE IAW SRM 5Nov 11, 2005 · N266FE · Boeing 727233 · Trailing Edge FlapsSDR 05FDEA03778Repair · undamagedFOUND REPAIR ON LT INBD FORE FLAP LEADING EDGE, 36 INCHES FROM OUTBD END. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B FORE FLAP WAS DETERMINED TO BE IWNov 11, 2005 · N266FE · Boeing 727233 · Trailing Edge FlapsSDR 05FDEA03776Repair · undamagedFOUND REPAIR ON RT NR 5 SLAT UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 5 RT SLAT WAS DETERMINED TO BE IAW SRM 57-50-3 FIG 1 SHT 6 AND 7, BNov 11, 2005 · N266FE · Boeing 727233 · Leading Edge DevicesSDR 05FDEA03764Repair · undamagedFOUND REPAIR AT STA 380 STR 9L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 380 STR 9L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 4 , BASED ON AN EXTERNAL Nov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA03765Repair · undamagedFOUND REPAIR AT STA 1050 STR 29L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1050 STR 29L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON GMM 6-2-100Nov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03766Repair · undamagedFOUND REPAIR AT STA 1223 STR 19R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1223 STR 19R WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 28 BASED ON AN EXTERNNov 11, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03747Repair · undamagedFOUND REPAIR AT STA 1090 FWD EDGE OF LOWER AFT CARGO DOOR CUT-OUT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR AT STA 1090 FWD EDGE OF LOWER AFT. CARGO DOOR CUT-OUT WAS ACCOMPLINov 9, 2005 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03730Fan · failedSTRONG FUMES IN COCKPIT AT FL 320 CRUISE FLT RAN EMERGENCY CHECKLIST AND LANDED AT KSWF. FOUND GASPER FAN C/B POPPED, RESET C/B AND IT POPPED AGAIN. SUSPECT BAD GASPER FAN. REMOVED AND REPLACED GASPER FAN IAW MM 21-23-011-4. 0PS CKS GOOD. R/I FROM FACT PRNov 8, 2005 · N264FE · Boeing 727233 · Air Distribution FanSDR 05FDEA03718Skin · corrodedEXTERIOR FUSELAGE, RAM AIR DOORS ACTUATOR ACCESS PANEL HAS CORROSION ON LANDS BETWEEN STRINGER 28-L AND STRINGER 28-R AT STATION BS 720B. REMOVED CORROSION IAW B727 SRM 51-10-6,ORIGINAL MATERIAL AT AREA .090" MATERIAL REMAINING .053" FOUND OUT OF LIMITS IAW BNov 8, 2005 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA03593Frame · corrodedAFT CARGO COMPARTMENT FRAME HAS CORROSION STA 1030 RBL 18 IN. REMOVED CORROSION FROM SURFACE IAW SRM 51-10-6. ID MAT BEFORE 0.063 AFTER 0.060 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-10 FIG 1. TREATED AND PRIMED SRM 51-10-2.Oct 31, 2005 · N266FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA03589Clamp · out of positionDURING CLIMB-OUT ENG NR 1 STRUT OVHT LIGHT ILLUMINATED ACCOMPLISHED ABNORMAL CHK LIST AFTER BLEED AND PACK SW'S CLOSED AND THRUST LEVER TO IDLE LIGHT OUT. INSPECT ALL THE CLAMPS ON THE NR 1 STRUT. PRESSURIZING THE DUCTS USING APU AIR FOUND CLAMP ADJACENT TOOct 28, 2005 · N220FE · Boeing 727233 · Pneumatic Distribution SystemSDR 05FDEA03508Warning Horn · activatedPASSING THRU FL250 CABIN ALTITUDE WARNING HORN CAME ON AND CABIN WAS AT 10,000FT. BOTH PACKS ON, ENGINE BLEED NR 1 AND NR 3 OPEN. NO OTHER ABNORMAL INDICATIONS (OUTFLOW VALVE CLOSED AND ALL DOES CLOSED). EMERGENY DECLARED AND NO FUEL DUMP REQUIRED.Oct 26, 2005 · N219FE · Boeing 727233 · Cabin Pressure Control SystemSDR 05FDEA03427Clamp · looseCRUISE POWER SETTING , NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. RAN QRH AND LIGHT WENT OUT GOOD SYST TEST, RETURNED TO KMIA. INSPECTED ALL DUCTS, CLAMPS AND SENSE LINES. FOUND NUMEROUS CLAMPS LOOSE AT NR 1 PRECOOLER AND NR 1 BLEED VALVE. TIGHTEN CLAMPS Oct 13, 2005 · N219FE · Boeing 727233 · Engine Bleed Air SystemSDR 05FDEA03389Floor Support · corrodedFLOOR SUPPORT AT BS 1179 RBL 6 HAS CORROSION. COMPLIED WITH FED EX E7-5320-92564. FUSELAGE FLOOR SUPPORT AT 1176.9 HAS CORROSION. REPAIRED. MAJOR REPAIROct 11, 2005 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 05FDEA03169Panel · damagedRIGHT WING LOWER LEADING EDGE PANEL NR 6212 REQUIRES FABRICATION FOR REPLACEMENT ON-N00505. FABRICATED NEW PANEL IAW BAC DRAWING 65-21661. ALODINED, PRIMED AND PAINTED NEW PANEL IAW FED-EX SRDM SR-57-005B.Sep 30, 2005 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 05FDEA03168Panel · erodedRIGHT WING LEADING EDGE PANEL NR 6541 ERRODED. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.Sep 30, 2005 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 05FDEA03167Panel · damagedRIGHT WING LOWER LEADING EDGE PANEL NR 6539 REQUIRES FABRICATION FOR REPLACEMENT ON N00158. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED, AND PAINTED IAW B727 SRM 51-10-2.Sep 30, 2005 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 05FDEA03166Panel · wornRIGHT WING LEADING EDGE FIBERGLASS PANEL NR 6212, BADLY WORN AROUND EDGE. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.Sep 30, 2005 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 05FDEA03157Beam · damagedAFT LOWER CARGO BS 1183 BULKHEAD VERTICAL BEAM AT LBL 20 HAS FASTENERS INSTALLED WITH SHORT PITCH, (SIDE BY SIDE). COMPLIED WITH FED EX EA E7-5310-91297-FUSELAGE, BS 1183 AFT PRESSURE BULKHEAD SHORT ON CENTER FASTENER SPACING REPAIR. MAJOR REPAIR.Sep 29, 2005 · N267FE · Boeing 727233 · Fuselage Main, BulkheadSDR 05FDEA03158Floorbeam · corrodedFLOORBEAM AT STATION 344 BL.0 CORRODED. RERAIRED FLOORBEAM IAW FED EX DWG SR 27-53-007.Sep 29, 2005 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03139Panel · damagedLEFT WING LOWER PANEL NR 6249 REQUIRES FABRICATION FOR REPLACEMENT ON FED, EX NON-ROUTINE N00517. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675-5, ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.Sep 27, 2005 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 05FDEA03113Skin · crackedLT FWD NOSE GEAR DOOR INNER SKIN IS CRACKED 8 INCHES FROM FRONT EDGE, LBL 1 WHEN DOOR IS CLOSED. REPAIRED CRACK IN LH FWD NOSE GEAR DOOR INNER SKIN IAW SRM 51-40-2, AND SRM 52-00-2.Sep 26, 2005 · N268FE · Boeing 727233 · Landing Gear Doors
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