Boeing 727-230

Service difficulty reports · 181

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '727230'
  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 ABXR2011110700050Support Fitting · corrodedDURING NLG REPLACEMENT, FOUND RT NLG SUPPORT FITTING CORRODED AT AFT BOLT HOLE SPOT FACE. REPLACED FITTING IAW SB727-53-0119.Nov 7, 2011 · N357KP · Boeing 727230 · Fuselage, Landing Gear Attach FittingsSDR ABXR2011110700049Attach Fitting · corrodedDURING NLG REPLACEMENT FOUND OTBD FACE OF NARROW LUG OF NLG DRAG BRACE ATTACH FITTING CORRODED. REPAIRED IAW SRM AND EA NR 2357-5301.Nov 7, 2011 · N357KP · Boeing 727230 · Fuselage, Landing Gear Attach FittingsSDR C8GA20111021022Motor · leakingDURING CRUISE OPERATION IT WAS NOTED THAT THERE WAS A LOSS OF "A" HYD SYS. AN EMERGENCY WAS DECLARED, MANUAL GEAR EXTENSION WAS EXECUTED AND THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT THE FLAP DRIVE MOTOR WAS LEAKING. R & ROct 21, 2011 · N357KP · Boeing 727230 · Trailing Edge Flap ActuatorSDR FOTR2105317107Skin · damagedACFT STRUCK BY BELT LOADER AT AFT CARGO DOOR CUTOUT LOWER SILL, STA 970. REPAIRED ON FASI WO 21053 NR'S 17107, 09002. IAW CAPITAL ER/A 2357-5302, REV 03 EXTERNAL DOUBLER REPAIR.Apr 9, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/SkinSDR FOTR2105317127Stringer · corrodedSTRINGER S8R HAS HEAVY CORROSION DAMAGE AT STATION 950E+5. REMOVED DAMAGED STR 28R FROM BS 950 TO 1010 IAW SRM 51-30-2 LOCATED AND DRILLED NEW STR 28R SECTION PN 65-58387-2, PO 2105315 IAW SRM 51-30-5. INSTALLED STR 28R IAW SRM 51-30-2 AND DWG 65-58387.Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Main, Longeron/StringerSDR FOTR2105317126Shear Tie · corrodedSHEAR TIE CORRODED AT BS 950F STR 27R AND 28R. REMOVED SHEAR TIE AT BS 950F BETWEEN STR 28R TO 27R IAW SRM 51-30-2. FABRICATED SHEARTIE FROM 7075-0 .063" PO 90011223, DIM 7.25' X 2.1' IAW SRM 53-10-4, FIG 15. HEAT TREATED PART FROM 7075-0 TO 7075T6 IAW ENG Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Internal Mounting StructureSDR FOTR2105317118Sill · damagedC-2 DOOR LOWER SILL CHORD AT STR 27R IS OUT OF LIMITS, AT 3 LOCATIONS BETWEEN BS 960-990. R & R STR 27R CHORD PN 65-56129Y10 PO 210539 IAW DWG 65-56129 AT AFT CARGO COMPT STA 950 TO 1010.Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Miscellaneous StructureSDR FOTR21053Frame · buckledFRAME AT BS 970 IN AFT PIT IS BUCKLED BETWEEN STRR AND STR28R. REMOVED DAMAGED FRAME SECTION FROM BS 970 BETWEEN STR 25L TO 27R. FABRICATED NEW FRAME SECTION FROM 7075-0 .063" PO 2105316 DIM 71" X 11". HEAT TREATED PART FROM 7075-0 TO 7075T6 IAW FASI ENG REApr 6, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022202146Nose Cowl · puncturedHOLE IN NR 1 ENGINE NOSE COWL AT APPROX 9 O`CLOCK POSITION LOOKING AFT. CUTOUT DAMAGE FROM NR 1 ENGINE COWLING DIM. 5" X 2" IAW SRM 54-30-2 FIG 2. FABRICATED 2 EA STRAPS 5.3" X 1.3" AND 2 EA 3.4" X 1.3" FROM 2024T3 .071 PO 90010564. FABRICATED FILLER FROM 2Feb 21, 2011 · N357KP · Boeing 727230 · Nacelle/Pylon, Main FrameSDR FOTR2022202114Skin · damagedSTA 910-930, STRINGER 17R ABOVE WING TO BODY FAIRING .007 SCRIBE MARK. BLENDED OUT SCRIBE DAMAGE FROM STA 910 TO 929, STR 17R IAW SRM 53-30-1, FIG 1 COMPLIED WITH UT THICKNESS INSP IAW NDTM 51-00-00, PART 4, FIG 2. ORIGINAL MATERIAL .144 REMAINING .137. COMPFeb 11, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/SkinSDR FOTR2022202122Skin · misrepairedREMOVED EXISTING LAP SEAM REPAIR AT STA 496 AND STRINGER 26R TO COMPLY WITH INSP REQUIREMENTS OF EO 7253-0002 R2, INSTALL APPROVED REPAIR AFTER INSP COMPLETE. REMOVED EXISTING REPAIR IAW EO 7253-0002 R2, C/W HFEC INSP OF OPEN HOLES AND CUT OUT AREA COMMON TO Feb 11, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/SkinSDR FOTR2022202133Skin · misrepairedREMOVE EXISTING LAP SEAM REPAIR AT STATION 1148 AND STRINGER 19R TO COMPLY WITH INSP REQUIREMENTS OF EO 7253-002 R2, INSTALL APPROVED REPAIR AFTER INSP IS COMPLETE. REMOVED EXISTING LAP SEAM REPAIR IAW SRM 51-30-2. COMPLIED WITH HFEC OF OPEN FASTENER HOLES INFeb 10, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/SkinSDR FOTR2022201811Hinge · brokenEXTERNAL FUSELAGE MAIN CARGO DOOR AFT FUSLEAGE HINGE HAS AFT LOBE BROKEN OFF. REMOVED HINGE SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SECTION OF HINGE FROM MS20001-16-7200, PO 2022248 DIM 22.6250" IAW SRM 51-30-2 AND ACI FMM CH 52, PAGE 15 THRU 19Feb 10, 2011 · N357KP · Boeing 727230 · Fuselage, Door HingeSDR FOTR2022201681Frame · dentedMAIN CABIN - FRAME DENTED AT BS 380 BETWEEN STRINGER 5R AND STRINGER 6R. CUTOUT DENTED AREA DIM. 2.75" X 2" AT BS 380 STRINGER 5R-6R IAW SRM 51-40-3, FABRICATED REPAIR DOUBLER DIM 12" X 5" .050 AND FILLER 2.75" X 2" .050 PO 90010501 IAW SRM 51-40-3. HEAT TREATFeb 10, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022201989Frame · dentedSTA 1166, STR 16R FRAME DENTED. CUTOUT DAMAGED AREA AT STA 1166, STR 16R, DIM.1.6" X 1.75" IAW SRM 51-40-3, FIG 1. FABRICATED DOUBLER FROM 7075T6 .063" DIM 4" X 9" IAW SRM 51-40-3, FIG 1, PO 90010179. INSTALLED FRAME REPAIR AT BS 1166, STR 16R IAW SRM 51-40Feb 8, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022201865Frame · crackedSTATION 800, STRINGER 14R FRAME CRACKED. CUTOUT DAMAGED AREA DIM .8" X 1" IAW SRM 51-40-4 FIG 1, FABRICATED REPAIR ANGLE FROM 7075-0 .090" DIM. 9" X 1.9" IAW SRM 51-40-4 FIG 1 PO 9009880. HEAT TREATED REPAIR ANGLE 7075T6 IAW ENGINEERING REPORT 2-37153-801 RFeb 4, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022201826Frame · damagedSTATION 400, FRAME AT STRINGER 16L INBD SIDE DOUBLER DRILLED. CUTOUT DAMAGED AREA DIM. 2.25" X 2" IAW SRM 51-40-3. FABRICATED REPAIR DOUBLER AND FILLER FROM 7075T6 .050 PO 90010944, DIM. DOUBLER 3.6" X 10" AND FILLER 2.25" X 2" IAW SRM 51-40-3. INSTALLED REPFeb 4, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022201925Frame · gougedAFT CARGO STA 1070, STR 27R FRAME GOUGED IN RADIUS. REMOVED DAMAGED PORTION OF FRAME ANGLE IAW SRM 51-40-2, FABRICATED REPAIR ANGLE DIM. 8" X 1" AND FILLER 1" X 1" FROM 7075T6 .090 PO 9009762 IAW SRM 51-40-2. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-40-2Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR FOTR2022201405Bulkhead · crackedLT MLG WHEEL WELL BS 870 BULKHEAD CRACKED OTBD SIDE. REMOVED DAMAGED WEB FROM BS 870 BULKHEAD IAW SRM 51-30-2. FABRICATED NEW UPPER WEB FROM 7075T6 .050" PO 90010289 DIM. 12" X 7" IAW DWG 65-25370. FABRICATED NEW CHORD FROM BAC1505-100617 PO 90010656 14" X Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, BulkheadSDR FOTR2022201968Seat Track · crackedSTA 620, LBL 24 FLANGE CRACKED. REMOVED DAMAGED SEAT TRACK AT LBL24 STA 480-700 IAW SRM 51-30-2. FABRICATED SEAT TRACK FROM PN BAC1520-792T6511 PO 90010776 IAW SRM 53-10-5, INSTALLED SEAT TRACK AT LBL 24, STA 480-700 IAW SRM 51-30-2.Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2022202046Frame · elongated3 EA ELONGATED HOLES ON BS 188 AROUND STR 27L. CUTOUT DAMAGED CHORD AT BS 188 BETWEEN STR 26L AND 28R, DIM. 10.75", CUT DAMAGED WEB AT BS 188, STR 27 DIM. 1" X 2.75" IAW SRM 51-40-2, FIG 1 AND 51-40-3, FIG 1. FABRICATED DOUBLER FROM 7075T6 .032" PO 9008186 DIFeb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, FrameSDR 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 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 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 FOTR2022201943Seat Track · damagedSEAT TRACK FLANGE HOLES DRILLED ON EDGE OF FLANGE BETWEEN STA 360-380 BL-0-. REMOVED SEAT TRACK STRAP FROM BL-O STATION 360-440 IAW SRM 51-30-2. LOCATED AND DRILLED, AND INSTALLED NEW STRAP PN AE727-2-063-17, REF 16816 DIM 3.2500" X 6.6 FT IAW DWG AE727-2-06Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2022202022Seat Track · corrodedSTA 1130 AT RBL 24 SEAT TRACK FLANGE CORRODED TOP AND BOTTOM. REMOVED DAMAGED SEAT TRACK AT STA 1020 TO 1130, RBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC1520-792-7178-T6511, PO 90010746, DIM 115" IAW SRM 53-1-5, FIG 1. INSTALLED NEW SEAT TRACKFeb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2022201980Seat Track · corrodedSTATION 950, RBL 44, FLANGE CORRODED ON SEAT TRACK. REMOVED DAMAGED SEAT TRACK BS 950+10 TO BS 1030, RBL 45.5, LOCATED AND DRILLED NEW SEAT TRACK AND TRIMMED NEW SEAT TRACK PN BAC1520-792-7178-T6511. PO 90010776, DIM 11' 57.5" LONG, FABRICATED 2 EA ANGLE SPLFeb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR202220165Seat Track · crackedSTA 760.95, LBL 45 SEAT TRACK SUPPORT ANGLE BOTTOM SIDE CRACKED. REMOVED DAMAGED SECTION OF SEAT TRACK SUPPORT IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SUPPORT FROM BAC1506-1108-7075T6, DIM 110" LONG PO 20222108 IAW SRM 53-10-2, FIG 7. INSTALLED SEAT TRACFeb 1, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA201000005B-Nut · looseFLT 1716 FROM CVG TO MEM. DURING TAKEOFF ROLL THE CAPTAINS AND F/O'S AIRSPEED INDICATORS SPLIT BY 30 KNOTS. THE CREW PERFORMED ABORTED TAKEOFF WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING A LOOSE "B" NUT ON THE CAPTAINS AIR DATA SYSTEM STATMar 14, 2010 · N357KP · Boeing 727230 · Pitot/Static SystemSDR C8GA2010000003Stringer · corrodedWHILE PERFORMING MX ON THE PITOT STATIC SYS, CORROSION WAS NOTED AT STA 468 STR 24L. DAMAGED WAS REMOVED AND NEW SECTION OF STR WAS INSTALLED. NO OTHER DEFECTS WERE NOTED ACFT WAS RETURNED TO SERVICE.Jan 25, 2010 · N357KP · Boeing 727230 · Fuselage Main, Longeron/StringerSDR C8GA201000001Position Switch · faultyDURING CLIMB OPERATION THE NR 2 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. CREW PERFORMED APPROPRIATE CHECKLIST AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE NR 2 L/E FLAP POSITION INDIJan 7, 2010 · N357KP · Boeing 727230 · Trailing Flap Position Indicating SystemSDR C8GA20090296Motor · leakingDURING CLIMB OPERATION PASSING THROUGH 9000 FT A COMPLETE "A" HYD SYS FLUID LOSS WAS ENCOUNTER. AN EMERGENCY WAS DECLARED, APPROPRIATE CHECKLIST PERFORMED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, NONov 18, 2009 · N357KP · Boeing 727230 · Trailing Edge Flap ActuatorSDR C8GA20090201Control Valve · inoperativeDURING CLIMB THE ACFT CABIN WAS UNABLE TO MAINTAIN CABIN PRESSURE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE RT FLOW CONTROL VALVE WAS FOUND NOT FULLY CLOSING. RT FLOW CONTROL VALVE WAS REMOVED AND REPSep 10, 2009 · N357KP · Boeing 727230 · Cabin Cooling SystemSDR C8GA20090108Connector · dirtyFLT 724 FROM TOL TO EWR ON TAKE OFF ROLL THE NR 3 ENGINE EGT INDICATOR WENT TO ZERO AND BECAME INTERMITTENT. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO THE BLOCKS. POST FLIGHT INSPECTION WAS PERFORMED, CLEANED CONNECTORS AT JUNCTION BOX, CLEANED AND TIGHTENED EJul 8, 2009 · N357KP · Boeing 727230 · Engine Indicating System WiringSDR C8GA20090061Tab · delaminatedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT LT OTBD END OF THE OTBD AILERON TAB IS DELAMINATED. DAMAGE WAS REMOVED APPROX DIM 2 INCH BY 4.5 INCH. FABRICATED CORE FROM 5052-44-3/16 DIM 2 INCH BY 4 INCH, HOT BONDED CORE. FABRICATED FILLER FROM 2024 T3 .012 IFeb 5, 2009 · N357KP · Boeing 727230 · Aileron TabsSDR C8GA20090060Skin · delaminatedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT LT OTBD AFT FLAP HAS DELAMINATION AT WBL 300. DAMAGE WAS REMOVED APPROX DIM 5.5 INCH BY 2 INCH, FABRICATED FILLER FROM 2024 T3 .016 INCH DIM 5.5 INCH BY 2 INCH AND DOUBLER FROM 2024 T3 .016 DIM 7 INCH BY 3.5 INCH. Feb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge FlapsSDR C8GA20090059Tab · damagedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE UPPER RUDDER TAB HAS APPROX .5 INCH DIAMETER HOLE ON THE RT SIDE OF TAB. REMOVED DAMAGE, CLEANED AND PREPARED RT SIDE OF UPPER RUDDER TAB. APPLIED FIBERGLASS REPAIR AND RESTORED FINISH. NO OTHER DEFECTS WEREFeb 5, 2009 · N357KP · Boeing 727230 · Rudder, Tab StructureSDR C8GA20090058Skin · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE WING CENTER SECTION UPPER SKIN LBL 45 BS 760 HAS CORROSION. REMOVED CORROSION, PERFORMED NDT INSPECTION, SHOT PEENED AREA, OVER SIZED FASTENER HOLES AND INSTALLED NEW FASTENERS. NO OTHER DEFECTS WERE NOTED. AFeb 5, 2009 · N357KP · Boeing 727230 · Wing, Center BoxSDR C8GA20090057Skin · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE WING CENTER SECTION UPPER SKIN LBL 24 BS 760 HAS CORROSION. REMOVED CORROSION PERFORMED NDT TESTING, SHOT PEENED AREA, OVER SIZED FASTENER HOLES AND INSTALLED NEW FASTENERS. NO OTHER DEFECTS WERE NOTED. AIRCRFeb 5, 2009 · N357KP · Boeing 727230 · Wing, Center BoxSDR C8GA20090056Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN BY THE DUCT ACCESS DOOR BS 1342.40. CUT OUT DAMAGE DIM 19.68 INCH BY 8 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 26 INCH BY 14 INCH. HEAT TFeb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake SystemSDR C8GA20090055Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN AT UPPER AFT CORNER OF DUCT ACCESS DOOR. CUT OUT DAMAGE DIM 9.25 INCH BY 5 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 16 INCH BY 11.5 INCH HEATFeb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake SystemSDR C8GA2009Intake Duct · corrodedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT THE NR 2 ENGINE S DUCT HAS CORROSION ON THE LOWER INNER SKIN AT UPPER AFT CORNER OF DUCT ACCESS DOOR. CUT OUT DAMAGE DIM 9.25 INCH BY 5 INCH. FABRICATED DOUBLER FROM 7075-O .080 INCH DIM 16 INCH BY 11.5 INCH HEATFeb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake SystemSDR C8GA20090053Hinge · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE MAIN CARGO DOOR AFT HINGE SEGMENT IS CRACKED SEVERAL PLACES BS 680. REMOVED AFT HINGE SEGMENT, INSTALLED NEW HINGE. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Feb 5, 2009 · N357KP · Boeing 727230 · Fuselage, Door HingeSDR C8GA20090052Plenum · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE LT RAM AIR PLENUM LOWER WING SKIN CORRODED AT PREVIOUS REPAIR. REMOVED FASTENERS, CLEANED CORROSION, PERFORMED NDT INSPECTIONS AND REWORKED FASTENER HOLES. FABRICATED DOUBLER, TRIPLER, QUADRUPLER AND FILLER. Feb 5, 2009 · N357KP · Boeing 727230 · Standard Practices/StructuresSDR C8GA20090051Skin · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING INBD AFT FLAP LEADING EDGE IS CRACKED AT 4TH TRACK. STOP DRILLED CRACK PERFORMED HFEC INSP NO CRACKS NOTED. FABRICATED REPAIR DOUBLER FROM 2024 T3 .050 INCH DIM 5.375 INCH BY 3.125 INCH. INSTALLED REPFeb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge FlapsSDR C8GA20090050Angle · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING LEADING EDGE VERTICAL ANGLE IS CRACKED AT THE BOTTOM WS 110. CUT OUT DAMAGED SECTION DIM 4.25 INCH BY 3. FABRICATED REPAIR ANGLE AND FILLER. INSTALLED ANGLE REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRFeb 5, 2009 · N357KP · Boeing 727230 · Wing Miscellaneous StructureSDR C8GA20090049Skin · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING OUTBOARD AFT FLAP LEADING EDGE IS CRACKED AT THE 2ND TRACK. STOP DRILLED CRACK, PERFORMED HFEC INSP, NO CRACKS WERE NOTED. FABRICATED DOUBLER FROM 2024 T3 .050 INCH DIM 5.75 INCH BY 4 INCH INSTALLED REPFeb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge FlapsSDR C8GA20090048Rib · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 7 SLAT OTBD HOOK HAS 2 CRACKED RIBS ON THE SIDES OF THE ACTUATOR FWD MOUNT AT THE LOWER AFT RADIUS. REMOVED BOTH RIBS, STOP DRILLED CRACK IN OTBD RIB, PERFORMED HFEC, NO CRACKS NOTED. FABRICATED DOUBLER FORFeb 5, 2009 · N357KP · Boeing 727230 · Leading Edge DevicesSDR C8GA20090047Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 6 SLAT OTBD HOOK AFT MOUNT HAS A CRACK BETWEEN FASTENERS. REMOVED HOOK AND FASTENERS, PERFORMED HFEC, FABRICATED DOUBLER FROM 2024 T3 .125 INCH DIM 7 INCH BY 3.125 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WFeb 5, 2009 · N357KP · Boeing 727230 · Leading Edge DevicesSDR C8GA20090046Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 8 SLAT INBD HOOK AFT MOUNT HAS CRACK BETWEEN RIVETS. REMOVED FASTENERS AND PERFORMED HFEC. FABRICATED DOUBLER FROM 2024 T3 .125 INCH DIM 8.75 INCH BY 3.15 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTEFeb 5, 2009 · N357KP · Boeing 727230 · Leading Edge Devices
Back to Boeing 727-230