# Service difficulty reports: N489FE, cancelled Dec 18, 2013

A list on [N489FE, cancelled Dec 18, 2013](https://openairdocs.org/deregistered/N489FE-2013-12-18.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 163 reports

- [SDR FDEA201212204343](https://openairdocs.org/sdr/FDEA201212204343.md): Unknown · smoke · Dec 20, 2012 · N489FE · Boeing 727227 · Air Distribution System
  > ON SHUTDOWN OF APU DURING TAXI, ALL GB`S TRIPPED. WHILE RUNNING STABILIZERS AND QRH, NOTICED SMOKE ODOR IN COCKPIT. SUSPECTED PACK OVERHEAT. ACFT BEGAN TO ROLL DURING ATTEMPT TO START APU TO REGAIN POWER. APPLIED PNEUMATIC BRAKE TO STOP. ONCE POWER WAS BA
- [SDR FDEA201207252666](https://openairdocs.org/sdr/FDEA201207252666.md): Accessory Unit · malfunctioned · Jul 25, 2012 · N489FE · Boeing 727227 · Landing Gear Retraction/Extension System
  > AFTER T/O LANDING GEAR LEVER COULD NOT BE MOVED BEYOND THE "OFF" POSITION. COMPLIED WITH QRH. R & R THE LANDING GEAR ACCESSORY UNIT PER MM 32-09-121-4.PERFORMED OPS TEST REF MM 32-09-122-5. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.
- [SDR FDEA201205261972](https://openairdocs.org/sdr/FDEA201205261972.md): Skin · dented · May 26, 2012 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT IN SKIN AT BS 1129 S29L. CUT OUT DAMAGED AREA IAW SRM 53-30-3, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 1 AND SRM 53-30-2, FIG 2.
- [SDR FDEA201205231941](https://openairdocs.org/sdr/FDEA201205231941.md): Skin · damaged · May 23, 2012 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > SKIN DENTED AND GOUGED BS 1050 TO 1060 BETWEEN STRINGERS 26-28R. CUT OUT DAMAGED AREA IAW IAW SRM 53-30-3, FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-30-3, FIG 1 AND SRM 51-30-2.
- [SDR FDEA201205221932](https://openairdocs.org/sdr/FDEA201205221932.md): Frame · cracked · May 22, 2012 · N489FE · Boeing 727227 · Fuselage Main, Structure
  > CRACK AT NR 1 CARGO DOOR AFT FRAME BS 620, S25R. CUT OUT DAMAGED AREA IAW SRM 51-40-3, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-2, FIG 3 AND SRM 51-40-2, FIG 1.
- [SDR FDEA201205221927](https://openairdocs.org/sdr/FDEA201205221927.md): Web · dented · May 22, 2012 · N489FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > DENT ON LT AIRSTAIR TORQUE BOX WEB AT BS 1313. DENT OUT OF LIMITS IAW SRM 53-10-1, FIG 1. CUT OUT DAMAGED AREA IAW SRM 51-40-02, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, FIG 1.
- [SDR FDEA201205221920](https://openairdocs.org/sdr/FDEA201205221920.md): Stringer · damaged · May 22, 2012 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > ON REMOVAL OF DAMAGED STRINGER 28L FOUND SKIN CORRODED AT BS 585. CUT OUT DAMAGED SKIN IAW SRM 51-10-1 AND EA 7-5330-143992. FABRICATED FILLER, STRUCTURAL FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3 AND EA 7-5330-143992. INSTALLED IAW SRM 51-30-2, 53-30-3 FIG
- [SDR FDEA201205191887](https://openairdocs.org/sdr/FDEA201205191887.md): Frame · cracked · May 19, 2012 · N489FE · Boeing 727227 · Fuselage Main, Frame
  > STATION 720 FRAME CRACKED AT SKIN ATTACH FASTENER HOLE BETWEEN STR 28L AND 27L. CUT OUT DAMAGED AREA IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991.
- [SDR FDEA201205191886](https://openairdocs.org/sdr/FDEA201205191886.md): Stringer · corroded · May 19, 2012 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 28L FROM BS 580 TO 600. CUT OUT CORRODED PORTION OF STRINGER IAW SRM 51-10-1. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2, REV 103.
- [SDR FDEA201204111363](https://openairdocs.org/sdr/FDEA201204111363.md): Line · leaking · Apr 11, 2012 · N489FE · Boeing 727227 · Hydraulic System, Main
  > TOTAL LOSS OF "A" SYS HYD QTY AND PRESSURE WHEN GEAR RETRACTED FOLLOWING TAKEOFF. ON POST FLIGHT DEBRIEF CREW REPORTED THAT WHEN THEY RETRACTED THE GEAR THEY LOST HYD FLUID AND PRESSURE AND THAT THEY HAD TO EXTEND THE GEAR MANUALLY. OPENED ACCESS PANEL 8505
- [SDR FDEA201203231070](https://openairdocs.org/sdr/FDEA201203231070.md): Fitting · leaking · Mar 23, 2012 · N489FE · Boeing 727227 · Turbine Engine Oil System
  > NR 3 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS, CRUISING AT FL 330. NR 3 OIL QUANTITY STARTED TO DECREASE APPROX 1 QT PER 2 MINUTES. AT FIRST INDICATION OF SECONDARY CONFIRMATION COMPLETED SHUTDOWN CHECKLIST AND DIVERTED. SHUTDOWN TO LANDING WINDMILL 15 MIN
- [SDR FDEA201109203980](https://openairdocs.org/sdr/FDEA201109203980.md): Window · obstructed · Sep 20, 2011 · N489FE · Boeing 727227 · Flight Compartment Windows
  > CAPT'S WINDOW WILL NOT OPEN. FOUND TRIM AROUND WINDOW IS NOT INSTALLED PROPERLY. TOO MUCH OF TRIM PROTRUDING ABOVE WINDOW CHANNEL THUS NOT ENOUGH CLEARANCE FOR WINDOW TO CLEAR PANEL. LOOSENED FASTENERS AROUND TRIM PANEL BELOW L-2 WINDOW. PANEL WILL NOT
- [SDR FDEA201001290291](https://openairdocs.org/sdr/FDEA201001290291.md): Floorbeam · corroded · Jan 29, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT BS 1130 RBL 30 TO RBL 46. CUT OUT DAMAGED AREA, FABRICATED 2 FLOORBEAM REPAIRS, 1 STRAP, 1 FILLER, 2 ANGLES, 1 STRAP AND 1 FILLER. HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A AND INSTALLED PARTS IAW 53-10-8
- [SDR FDEA201001290290](https://openairdocs.org/sdr/FDEA201001290290.md): Floorbeam · corroded · Jan 29, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 1070, RBL 5 TO RBL 10. CUT OUT DAMAGED AREA, FABRICATED 2 FILLERS, 2 REPAIR ANGLES AND INSTALLED IAW SRM 53-10-8, 51-10-2 AND 51-30-2.
- [SDR FDEA201001270285](https://openairdocs.org/sdr/FDEA201001270285.md): Floorbeam · damaged · Jan 27, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > DOUBLE DRILLED HOLES IN FLOORBEAM STA 1130 LBL 47. CUT OUT DAMAGE IN FLOORBEAM DIMS 1" X 1", FABRICATED NEW ANGLE, HEAT TREATED PART TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, FILLERS AND INSTALLED IAW SRM 51-30-2, 53-10-8, AND 51-
- [SDR FDEA201001260269](https://openairdocs.org/sdr/FDEA201001260269.md): Skin · bent · Jan 26, 2010 · N489FE · Boeing 727227 · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT EDGE AT STR 10 LT IS BENT OUT. TRIMMED OUT DAMAGED AREA, HFEC INSPECTED CUTOUT WITH NO DEFECTS NOTED IAW NDTM 51-00-00, HFEC INSPECTED HOLES WITH NO DEFECTS NOTED NDTM 51-00-00, FABRICATED DOUBLER, TRIPLER, FILLER AND INSTALLED IAW EA 7-
- [SDR FDEA201001230268](https://openairdocs.org/sdr/FDEA201001230268.md): Skin · corroded · Jan 23, 2010 · N489FE · Boeing 727227 · Horizontal Stabilizer, Plate/Skin
  > SURFACE CORROSION UNDER BASE OF NR 2 STATIC WICK ON RT HORIZ STAB OTBD T/E. REMOVED CORROSION AND FOUND OUT OF LIMITS AND CRACKED. TRIMMED OUT DAMAGE, FABRICATED DOUBLER PLATE, TWO FILLERS AND INSTALLED IAW SRM 51-30-2, 51-10-6, 55-20-3 AND 51-80-7.
- [SDR FDEA201001230281](https://openairdocs.org/sdr/FDEA201001230281.md): Beam · damaged · Jan 23, 2010 · N489FE · Boeing 727227 · Fuselage Main, Structure
  > AFTER REMOVING MAIN CARGO DOOR FWD UPPER SILL, FOUND EXISTING OPEN HOLES WITH SHORT SPACING AT STA'S 480, 490, 500 AND 520. DAMAGE REPAIR DOCUMENTED.
- [SDR FDEA201001220253](https://openairdocs.org/sdr/FDEA201001220253.md): Skin · gouged · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 620 TO 640 STR 4L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.
- [SDR FDEA201001220252](https://openairdocs.org/sdr/FDEA201001220252.md): Skin · gouged · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, Structure
  > MAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 640 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.
- [SDR FDEA201001220251](https://openairdocs.org/sdr/FDEA201001220251.md): Skin · gouged · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, Structure
  > MAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 480 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.
- [SDR FDEA201001220226](https://openairdocs.org/sdr/FDEA201001220226.md): Bulkhead · cracked · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, Bulkhead
  > RT W/W FWD BULKHEAD IS CRACKED BELOW APU LOAD CONTROL VALVE AT BS 870 RBL 18. REPAIRED RT WHEEL WELL BULKHEAD APU LOAD CONTROL VALVE AREA BS 870 RBL18 IAW SRM 53-10-9 FIG 5, REV 102.
- [SDR FDEA201001220225](https://openairdocs.org/sdr/FDEA201001220225.md): Hinge · worn · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage, Door Hinge
  > MAIN CARGO DOOR AFT HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTION USING 5212791 PO NR 79014501 DIMS 48 1/2" LONG FOR UPPER SECTION AND 20 1/4" LONG FOR LOWER SECTION AND INSTALLED IAW DWG B27-53-070 REV B.
- [SDR FDEA201001220224](https://openairdocs.org/sdr/FDEA201001220224.md): Hinge · worn · Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage, Door Hinge
  > MAIN CARGO DOOR FWD HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTIONS AND INSTALLED IAW DWG B27-53-070 REV B.
- [SDR FDEA201001210213](https://openairdocs.org/sdr/FDEA201001210213.md): Skin · damaged · Jan 21, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > L-1 DOOR UPPER AND LOWER HINGE CUTOUT DOUBLERS HAVE COUNTERSUNK FASTENERS INSTALLED. REMOVED DOUBLERS, FABRICATED 2 NEW DOUBLERS, CADMIUM PLATED DOUBLERS IAW SOPM 20-40-01 AND INSTALLED IAW EO 7-5330-7-2345 PT 2 AND SRM 51-30-2.
- [SDR FDEA201001210208](https://openairdocs.org/sdr/FDEA201001210208.md): Skin · cracked · Jan 21, 2010 · N489FE · Boeing 727227 · Ailerons
  > LT INBD AILERON LOWER SURFACE SKIN IS CRACKED AT FWD EDGE. SKIN CRACK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 4 1/2" X 5 1/8", FABRICATED DOUBLER, FILLER AND INSTALLED IAW SRM 57-50-1, 57-50-5, 51-10-1, AND 51-30-2.
- [SDR FDEA201001200264](https://openairdocs.org/sdr/FDEA201001200264.md): Seat Track · corroded · Jan 20, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 970-990 RBL 24. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 144" AND SPLICE ANGLES USING BAC1503-100122 7178-T6511 PO NR 2912649 DIMS 1
- [SDR FDEA201001190190](https://openairdocs.org/sdr/FDEA201001190190.md): Seat Track · corroded · Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK BS 950 - 950, 10" LBL 24 OB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 91" AND INSTALLED IAW SRM 51-10-
- [SDR FDEA201001190189](https://openairdocs.org/sdr/FDEA201001190189.md): Stringer · cracked · Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > AFT PIT STR 27L HAS CORROSION WITH EXFOLIATION AROUND FASTENERS BTWN BS 950D-950F. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED 3 EACH STRINGER SECTIONS, FABRICATED 3 FILLERS AND 4 EACH SPLICES. INSTALLED IAW SRM 51-10-6, 53-10-2, 53-10-3, AND 51-30-2.
- [SDR FDEA201001190187](https://openairdocs.org/sdr/FDEA201001190187.md): Skin · corroded · Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FWD PIT - CORROSION ON SKIN AT BS 660 (AFT SIDE) BETWEEN STRINGERS 28R AND 29L. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 102. FABRICATED REPAIR DOUBLER, FABRICATED FILLER, INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2. FABRICATION IAW SRM 53-30-3, FIG.
- [SDR FDEA201001190188](https://openairdocs.org/sdr/FDEA201001190188.md): Seat Track · corroded · Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK BS 640 -660 LBL 56 IB FLANGE HAS SEVERAL SPOTS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED SEAT TRACK SUPPORT FLANGE. FABRICATED NEW SEAT TRACK SUPPORT FLANGE AND INSTALLED IAW SRM 51-30-2, 51-20-1 AND 51-10-2.
- [SDR FDEA201001160267](https://openairdocs.org/sdr/FDEA201001160267.md): Floorbeam · corroded · Jan 16, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FWD LAV AREA FLOORBEAM ANGLE IS CORRODED AT BS 310 LBL 20. TRIMMED DAMAGE. FABRICATED 2 REPAIR, FABRICATED FILLER, HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, AND INSTALLED IAW DWG SR27-53-017 REV A.
- [SDR FDEA201001160223](https://openairdocs.org/sdr/FDEA201001160223.md): Stringer · corroded · Jan 16, 2010 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION AROUND FASTENERS AT AFT PIT STA 1030 TO STA 1070 STRINGER 27L. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUTOUT STRINGER DAMAGE, FABRICATED FILLER USING BAC1498-145 7075T-6 PO NR 2905741 DIMS 19" AND SPLICES USING BAC1498-131 7075T-6 PO NR 2912086 D
- [SDR FDEA201001160191](https://openairdocs.org/sdr/FDEA201001160191.md): Skin · cracked · Jan 16, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LWR SIDE, HAS CRACK STA 720, STR 27R. REPAIRED IAW SRM 53-10-3 FIG 3 AND REPAIRED STRINGER 27R FWD PIT BETWEEN STA 700 TO 720 IAW SRM 53-10-3 FIG 1.
- [SDR FDEA201001150192](https://openairdocs.org/sdr/FDEA201001150192.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK BS 950, 10" - 950A LBL 24 OB UPPER FLANGE HAS CORROSION AT FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION AND SPLICE ANGLES AND ONE PLATE. INSTALLED IAW SRM 51-10-6, 53-10-
- [SDR FDEA201001150158](https://openairdocs.org/sdr/FDEA201001150158.md): Frame · bent · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage Main, Frame
  > CABIN FRAME BS 580 AT STRINGER 17 RT INSIDE FLANGE IS BENT IN. CUT OUT DAMAGED SECTION. FABRICATED FRAME DOUBLER REPAIR AND FILLER, HEAT TREATED MATERIAL TO T6 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A AND INSTALLED IAW SRM 51-40-3, 51-30-5, 51-
- [SDR FDEA201001150182](https://openairdocs.org/sdr/FDEA201001150182.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STA 720B LBL 45 OUTBD FLANGE UPPER SURF. HAS CORROSION. REMOVED SEAT TRACK SECTION LBL 45 BETWEEN STA 690 TO 740 AND 1EA SPLICER IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1 TREATED AND PRIMED IAW SRM 51-10-2,
- [SDR FDEA201001150181](https://openairdocs.org/sdr/FDEA201001150181.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STA 658 LBL 45 INBD FLANGE IS CORRODED. REMOVED SEAT TRACK SECTION BETWEEN STA 650 TO 690 LBL 45 AND 1EA SPLICER IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK AND FABRICATED 1 EA SPLICER 2 EA ANGLES, AND 1 EA STRAP IAW SRM 53-10-5
- [SDR FDEA201001150156](https://openairdocs.org/sdr/FDEA201001150156.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR TRACK B.S. 556 BL 0 LOWER SURF. HAS A CORROSION BULGE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION AT STA 480 TO 600 BL0 AND 2 EACH SERVICEABLE SPLICER SEAT TRACKS, LOCATED AND DRILLED NEW SEAT TRACK SECTION USING BAC152
- [SDR FDEA201001150180](https://openairdocs.org/sdr/FDEA201001150180.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727277 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT STA 695 RBL 24 INBD FLANGE AND SPLICE CORRODED REMOVED SEAT TRACK SECTION BETWEEN STA 690 TO 740 RBL24 AND 1 EA SPLICER IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAE 1526-729-7178 T6 511 PO NR 9006020, DIM 172" LONG IAW SRM 5
- [SDR FDEA201001150193](https://openairdocs.org/sdr/FDEA201001150193.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK BS 960-950A RBL 24 IB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND FABRICATED SPLICE FOR 2EA ANGLES AND 1EA STRAP IAW SRM 53-10-5 FIG1. TREATED AND PRIMED I
- [SDR FDEA201001150186](https://openairdocs.org/sdr/FDEA201001150186.md): Keelbeam · cracked · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage Main, Keel
  > LT KEELBEAM CRACKED BS 872 BETWEEN FASTENERS. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER, CAD PLATED DOUBLER, HEAT TREATED DOUBLER AND INSTALLED IAW EA 7-5310-137782.
- [SDR FDEA201001150160](https://openairdocs.org/sdr/FDEA201001150160.md): Stringer · cracked · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CABIN STRINGER 15 RT BS 720B PLUS 15" HAS END CRACKED AT FASTENER. REMOVED FASTENERS AND CUTOUT DAMAGED AREA, FABRICATED REPAIR "U" CHANNEL, FILLER AND FILLER TAPER. INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-2.
- [SDR FDEA201001150159](https://openairdocs.org/sdr/FDEA201001150159.md): Stringer · cracked · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CABIN STRINGER 15 RT B.S. 720B PLUS 4" HAS END CRACKED AT FASTENER. REMOVED FASTENERS AND CUTOUT DAMAGED AREA, FABRICATED REPAIR "U" CHANNEL, FILLER AND FILLER TAPER. INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-2.
- [SDR FDEA201001150179](https://openairdocs.org/sdr/FDEA201001150179.md): Seat Track · corroded · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK STA 680-690 RBL 24 FLANGE AND SPLICE CORRODED. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK AND SPLICER IAW SRM 53-10-2, INSTALLED NEW SEAT TRACK AND SPLICER IAW SRM 51-30-2.
- [SDR FDEA201001150157](https://openairdocs.org/sdr/FDEA201001150157.md): Floorbeam · cracked · Jan 15, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FWD LAV AREA -FLOOR SUPPORT ANGLE IS CRACKED AT FASTENER HOLE, BS 312, BL 0. TRIMMED DAMAGE. FABRICATED 2 REPAIR ANGLES, FABRICATED FILLER, HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, AND INSTALLED IAW DWG SR27-53-017 REV A.
- [SDR FDEA201001140194](https://openairdocs.org/sdr/FDEA201001140194.md): Floorbeam · corroded · Jan 14, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 560 LBL 24- 45 UPPER FLANGE LOWER SURF HAS CORROSION AT N/P'S. REMOVED CORROSION IAW SRM 51-10-6, UT INSPECTED AREA IAW NDTM 51-00-00 FIG 3 PART 4, FOUND OUT OF LIMITS IAW PF SRM (ER 01-049) 53-10-1 FIG 4B REV C, REMOVED STIFFENER F
- [SDR FDEA201001140127](https://openairdocs.org/sdr/FDEA201001140127.md): Structure · cracked · Jan 14, 2010 · N489FE · Boeing 727227 · Trailing Edge Flaps
  > LT INBD MID-FLAP T/E LOWER CHORD CRACKED WBL106. REMOVED CRACKED ANGLES AT WBL 106 AND 146, FABRICATED NEW ANGLES AND INSTALLED AT WBL 106 AND 146 IAW SRM 51-30-2, 51-40-4, 51-10-2 AND 51-10-1.
- [SDR FDEA201001130174](https://openairdocs.org/sdr/FDEA201001130174.md): Sill · cracked · Jan 13, 2010 · N489FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR UPPER SILL STA 495 STR 3L CRACK ORIGINATING FROM FASTENER. REMOVED FASTENER AND VERIFIED CRACK, REMOVED MAIN CARGO DOOR UPPER SILL AT STA 480 TO 530 AND ATTACHING SUPPORTS, LOCATED AND DRILLED NEW SILL AND INSTALLED NEW SILL AND ATTACHING SUPP
- [SDR FDEA201001110079](https://openairdocs.org/sdr/FDEA201001110079.md): Angle · cracked · Jan 11, 2010 · N489FE · Boeing 727227 · Trailing Edge Flaps
  > RT OTBD MID-FLAP AFT UPPER CHORD ANGLE CRACKED WS 470. FLAP REMOVED AND REPLACED DUE TO DAMAGE BEYOND REPAIR LIMITS.

Next page: https://openairdocs.org/deregistered/N489FE-2013-12-18/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 n_number = 'N489FE' AND deregistration_id = 'N489FE-2013-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N489FE-2013-12-18/reports

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