# Service difficulty reports: Boeing 727-230

A list on [Boeing 727-230](https://openairdocs.org/model/boeing-727-230.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 181 reports

- [SDR ABXR2011110700050](https://openairdocs.org/sdr/ABXR2011110700050.md): Support Fitting · corroded · Nov 7, 2011 · N357KP · Boeing 727230 · Fuselage, Landing Gear Attach Fittings
  > DURING NLG REPLACEMENT, FOUND RT NLG SUPPORT FITTING CORRODED AT AFT BOLT HOLE SPOT FACE. REPLACED FITTING IAW SB727-53-0119.
- [SDR ABXR2011110700049](https://openairdocs.org/sdr/ABXR2011110700049.md): Attach Fitting · corroded · Nov 7, 2011 · N357KP · Boeing 727230 · Fuselage, Landing Gear Attach Fittings
  > DURING NLG REPLACEMENT FOUND OTBD FACE OF NARROW LUG OF NLG DRAG BRACE ATTACH FITTING CORRODED. REPAIRED IAW SRM AND EA NR 2357-5301.
- [SDR C8GA20111021022](https://openairdocs.org/sdr/C8GA20111021022.md): Motor · leaking · Oct 21, 2011 · N357KP · Boeing 727230 · Trailing Edge Flap Actuator
  > DURING 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 & R
- [SDR FOTR2105317107](https://openairdocs.org/sdr/FOTR2105317107.md): Skin · damaged · Apr 9, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/Skin
  > ACFT 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.
- [SDR FOTR2105317127](https://openairdocs.org/sdr/FOTR2105317127.md): Stringer · corroded · Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR FOTR2105317126](https://openairdocs.org/sdr/FOTR2105317126.md): Shear Tie · corroded · Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Internal Mounting Structure
  > SHEAR 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
- [SDR FOTR2105317118](https://openairdocs.org/sdr/FOTR2105317118.md): Sill · damaged · Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Miscellaneous Structure
  > C-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.
- [SDR FOTR21053](https://openairdocs.org/sdr/FOTR21053.md): Frame · buckled · Apr 6, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > FRAME 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 RE
- [SDR FOTR2022202146](https://openairdocs.org/sdr/FOTR2022202146.md): Nose Cowl · punctured · Feb 21, 2011 · N357KP · Boeing 727230 · Nacelle/Pylon, Main Frame
  > HOLE 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 2
- [SDR FOTR2022202114](https://openairdocs.org/sdr/FOTR2022202114.md): Skin · damaged · Feb 11, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/Skin
  > STA 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. COMP
- [SDR FOTR2022202122](https://openairdocs.org/sdr/FOTR2022202122.md): Skin · misrepaired · Feb 11, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/Skin
  > REMOVED 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
- [SDR FOTR2022202133](https://openairdocs.org/sdr/FOTR2022202133.md): Skin · misrepaired · Feb 10, 2011 · N357KP · Boeing 727230 · Fuselage Main, Plate/Skin
  > REMOVE 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 IN
- [SDR FOTR2022201811](https://openairdocs.org/sdr/FOTR2022201811.md): Hinge · broken · Feb 10, 2011 · N357KP · Boeing 727230 · Fuselage, Door Hinge
  > EXTERNAL 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 19
- [SDR FOTR2022201681](https://openairdocs.org/sdr/FOTR2022201681.md): Frame · dented · Feb 10, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > MAIN 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 TREAT
- [SDR FOTR2022201989](https://openairdocs.org/sdr/FOTR2022201989.md): Frame · dented · Feb 8, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > STA 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 51-40
- [SDR FOTR2022201865](https://openairdocs.org/sdr/FOTR2022201865.md): Frame · cracked · Feb 4, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > STATION 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 R
- [SDR FOTR2022201826](https://openairdocs.org/sdr/FOTR2022201826.md): Frame · damaged · Feb 4, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > STATION 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 REP
- [SDR FOTR2022201925](https://openairdocs.org/sdr/FOTR2022201925.md): Frame · gouged · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > AFT 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 51-40-2
- [SDR FOTR2022201405](https://openairdocs.org/sdr/FOTR2022201405.md): Bulkhead · cracked · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, Bulkhead
  > LT 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
- [SDR FOTR2022201968](https://openairdocs.org/sdr/FOTR2022201968.md): Seat Track · cracked · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach Fittings
  > STA 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.
- [SDR FOTR2022202046](https://openairdocs.org/sdr/FOTR2022202046.md): Frame · elongated · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > 3 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 DI
- [SDR FOTR2022201962](https://openairdocs.org/sdr/FOTR2022201962.md): Rib · cracked · Feb 2, 2011 · N357KP · Boeing 727230 · Leading Edge Devices
  > NR 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.
- [SDR FOTR2022202060](https://openairdocs.org/sdr/FOTR2022202060.md): Rib · cracked · Feb 2, 2011 · N357KP · Boeing 727230 · Leading Edge Devices
  > NR 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 IN
- [SDR FOTR2022201970](https://openairdocs.org/sdr/FOTR2022201970.md): Frame · cracked · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage Main, Frame
  > PREVIOUS 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 IA
- [SDR FOTR2022201943](https://openairdocs.org/sdr/FOTR2022201943.md): Seat Track · damaged · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 AE727-2-06
- [SDR FOTR2022202022](https://openairdocs.org/sdr/FOTR2022202022.md): Seat Track · corroded · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach Fittings
  > STA 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 TRACK
- [SDR FOTR2022201980](https://openairdocs.org/sdr/FOTR2022201980.md): Seat Track · corroded · Feb 2, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach Fittings
  > STATION 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 SPL
- [SDR FOTR202220165](https://openairdocs.org/sdr/FOTR202220165.md): Seat Track · cracked · Feb 1, 2011 · N357KP · Boeing 727230 · Fuselage, Seat/Cargo Attach Fittings
  > STA 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 TRAC
- [SDR C8GA201000005](https://openairdocs.org/sdr/C8GA201000005.md): B-Nut · loose · Mar 14, 2010 · N357KP · Boeing 727230 · Pitot/Static System
  > FLT 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 STAT
- [SDR C8GA2010000003](https://openairdocs.org/sdr/C8GA2010000003.md): Stringer · corroded · Jan 25, 2010 · N357KP · Boeing 727230 · Fuselage Main, Longeron/Stringer
  > WHILE 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.
- [SDR C8GA201000001](https://openairdocs.org/sdr/C8GA201000001.md): Position Switch · faulty · Jan 7, 2010 · N357KP · Boeing 727230 · Trailing Flap Position Indicating System
  > DURING 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 INDI
- [SDR C8GA20090296](https://openairdocs.org/sdr/C8GA20090296.md): Motor · leaking · Nov 18, 2009 · N357KP · Boeing 727230 · Trailing Edge Flap Actuator
  > DURING 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, NO
- [SDR C8GA20090201](https://openairdocs.org/sdr/C8GA20090201.md): Control Valve · inoperative · Sep 10, 2009 · N357KP · Boeing 727230 · Cabin Cooling System
  > DURING 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 REP
- [SDR C8GA20090108](https://openairdocs.org/sdr/C8GA20090108.md): Connector · dirty · Jul 8, 2009 · N357KP · Boeing 727230 · Engine Indicating System Wiring
  > FLT 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 E
- [SDR C8GA20090061](https://openairdocs.org/sdr/C8GA20090061.md): Tab · delaminated · Feb 5, 2009 · N357KP · Boeing 727230 · Aileron Tabs
  > WHILE 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 I
- [SDR C8GA20090060](https://openairdocs.org/sdr/C8GA20090060.md): Skin · delaminated · Feb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge Flaps
  > WHILE 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.
- [SDR C8GA20090059](https://openairdocs.org/sdr/C8GA20090059.md): Tab · damaged · Feb 5, 2009 · N357KP · Boeing 727230 · Rudder, Tab Structure
  > WHILE 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 WERE
- [SDR C8GA20090058](https://openairdocs.org/sdr/C8GA20090058.md): Skin · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Wing, Center Box
  > WHILE 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. A
- [SDR C8GA20090057](https://openairdocs.org/sdr/C8GA20090057.md): Skin · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Wing, Center Box
  > WHILE 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. AIRCR
- [SDR C8GA20090056](https://openairdocs.org/sdr/C8GA20090056.md): Intake Duct · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake System
  > WHILE 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 T
- [SDR C8GA20090055](https://openairdocs.org/sdr/C8GA20090055.md): Intake Duct · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake System
  > WHILE 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 HEAT
- [SDR C8GA2009](https://openairdocs.org/sdr/C8GA2009.md): Intake Duct · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Engine Air Intake System
  > WHILE 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 HEAT
- [SDR C8GA20090053](https://openairdocs.org/sdr/C8GA20090053.md): Hinge · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Fuselage, Door Hinge
  > WHILE 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.
- [SDR C8GA20090052](https://openairdocs.org/sdr/C8GA20090052.md): Plenum · corroded · Feb 5, 2009 · N357KP · Boeing 727230 · Standard Practices/Structures
  > WHILE 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.
- [SDR C8GA20090051](https://openairdocs.org/sdr/C8GA20090051.md): Skin · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge Flaps
  > WHILE 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 REP
- [SDR C8GA20090050](https://openairdocs.org/sdr/C8GA20090050.md): Angle · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Wing Miscellaneous Structure
  > WHILE 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. AIRCR
- [SDR C8GA20090049](https://openairdocs.org/sdr/C8GA20090049.md): Skin · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Trailing Edge Flaps
  > WHILE 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 REP
- [SDR C8GA20090048](https://openairdocs.org/sdr/C8GA20090048.md): Rib · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Leading Edge Devices
  > WHILE 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 FOR
- [SDR C8GA20090047](https://openairdocs.org/sdr/C8GA20090047.md): Mount · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Leading Edge Devices
  > WHILE 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 W
- [SDR C8GA20090046](https://openairdocs.org/sdr/C8GA20090046.md): Mount · cracked · Feb 5, 2009 · N357KP · Boeing 727230 · Leading Edge Devices
  > WHILE 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 NOTE

Next page: https://openairdocs.org/model/boeing-727-230/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/boeing-727-230/reports

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