# Service difficulty reports: N485FE, cancelled Aug 27, 2013

A list on [N485FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N485FE-2013-08-27.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 6 · 255 reports

- [SDR FDEA201210023546](https://openairdocs.org/sdr/FDEA201210023546.md): Control Panel · inoperative · Oct 2, 2012 · N485FE · Boeing 727227 · Door Warning System
  > GALLEY DOOR INDICATION INOPERATIVE. R & R EXT DOOR ANNUNCIATOR PANEL. OPS NORMAL IAW MM 52-70-001-0-1. FINAL CLOSED.
- [SDR FDEA201207182600](https://openairdocs.org/sdr/FDEA201207182600.md): Battery Pack · inoperative · Jul 18, 2012 · N485FE · Boeing 727227 · Emergency Lighting
  > ON PRE-DEPARTURE CHECKS, NOTED EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. BOTH COCKPIT AND ENTRY WAY DOOR LIGHTS FUNCTION NORMALLY. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACK IAW AMM 33-50-051-2. REINSTALLED LENS COVER IAW SMP, LIGHT OPS CHECK GOOD.
- [SDR FDEA201207032478](https://openairdocs.org/sdr/FDEA201207032478.md): Light · shorted · Jul 3, 2012 · N485FE · Boeing 727227 · Passenger Compartment Lighting
  > DURING CRUISE, FOUND CIRCUT BREAKER LABLED "FIN & ENG" TRIPPED. AIRSTAIR AREA LT MID LIGHT ASSY SHORTED OUT. INSTALLED LIGHT ASSY TO EXISTING WIRES PER SWPM 20-30-12. OPS CHECKED GOOD PER AMM 33-30-000-0. LIGHT ILLUMINATED FOR 30 MINUTES WITH NO BREAKERS TR
- [SDR FDEA201111235063](https://openairdocs.org/sdr/FDEA201111235063.md): Slide · dislodged · Nov 23, 2011 · N485FE · Boeing 727227 · Escape Slide
  > ESCAPE SLIDE HAS APPEARED TO FALLEN OUT OF IT'S CONTAINER. R & R ESCAPE SLIDE IAW MM 25-60-015-2, OPS NORMAL.
- [SDR FDEA201108033079](https://openairdocs.org/sdr/FDEA201108033079.md): Slide · unsecure · Aug 3, 2011 · N485FE · Boeing 727227 · Escape Slide
  > ESCAPE SLIDE NOT FULLY CONTAINED IN DOOR CASING. RESECURED DOOR ESCAPE SLIDE MM REF: 25-60-015-2-0.
- [SDR FDEA201107293022](https://openairdocs.org/sdr/FDEA201107293022.md): Light · inoperative · Jul 29, 2011 · N485FE · Boeing 727227 · Emergency Lighting
  > REPLACED L1 EMERGENCY LIGHT ASSY AND BATTERIES IAW MTSI 33-50-2465, MM REF 33-50-101-2-0. OPS CHECK GOOD. REPLACED L1 EMERGENCY LIGHT ASSY AND BATTERIES IAW MTSI 33-50-2465, MM REF 33-50-101-2-0, OPS CHECK GOOD.
- [SDR FDEA201107293015](https://openairdocs.org/sdr/FDEA201107293015.md): Battery · inoperative · Jul 29, 2011 · N485FE · Boeing 727227 · Emergency Lighting
  > EMERGENCY LIGHT BATTERIES ABOVE FWD ENTRY DOOR ARE DEAD. R & R BATTERIES IAW AMM 33-50-101-2-0. OPS CHECKED NORMAL.
- [SDR FDEA201107222889](https://openairdocs.org/sdr/FDEA201107222889.md): Battery Pack · inoperative · Jul 22, 2011 · N485FE · Boeing 727227 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOPERATIVE. REPLACED BATTERIES IAW MM 33-50-101-2-0,2. (CLOSED)
- [SDR FDEA201107152720](https://openairdocs.org/sdr/FDEA201107152720.md): Lamp · inoperative · Jul 15, 2011 · N485FE · Boeing 727227 · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED OPS GOOD 33-50-101-2-0, 33-50-001-5-0.
- [SDR FDEA201107022555](https://openairdocs.org/sdr/FDEA201107022555.md): Battery Pack · discharged · Jul 2, 2011 · N485FE · Boeing 727227 · Emergency Lighting
  > L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT BATTERIES. OPS CHECK NORMAL, REF MM 33-50-101-2-0.
- [SDR FDEA201104151501](https://openairdocs.org/sdr/FDEA201104151501.md): Slat System · malfunctioned · Apr 15, 2011 · N485FE · Boeing 727227 · Leading Edge Slat Control System
  > NR 1 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION COMPLIED WITH QRH LED STILL FAILED TO RETRACT, RETURNED TO MEM, ACFT DID NOT HAVE A NOTICEABLE ROLL, BOTH FRONT "L/E FLAPS" & NR 1 SLAT ON AUX PANEL "POSITION TEST" WERE AMBER INDICATION NR 1 LED STILL NOT
- [SDR FDEA201103070902](https://openairdocs.org/sdr/FDEA201103070902.md): Skin · gouged · Mar 7, 2011 · N485FE · Boeing 727227 · Trailing Edge Flaps
  > RT WING INBD T/E FORE FLAP GOUGED, L/E LOWER SKIN NEAR OTBD END, APPROX WBL 240. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER AT RT WING I/B T/E FORE FLAP L/E LOWER SKIN NEAR O/B END IAW SRM 57-50-4 FIG 1, 51- 10-1, AND 51-
- [SDR FDEA201103070897](https://openairdocs.org/sdr/FDEA201103070897.md): Ring · dented · Mar 7, 2011 · N485FE · Boeing 72723 · Nacelle/Pylon, Main Frame
  > NR 3 ENGINE NOSE COWL LIP RING DENTED AT 6 O'CLOCK POSITION. CUT-OUT DAMAGED AREA AT NR 3 ENGINE NOSE COWL LIP RING AT 6 O'CLOCK POSITION, FABRICATED REPAIR PARTS AND DOUBLER, AND INSTALLED REPAIR PARTS AND DOUBLER IAW SRM 54-30-3 FIG 2, 51-10-2, AND 51-30-2
- [SDR FDEA201102250765](https://openairdocs.org/sdr/FDEA201102250765.md): Skin · misaligned · Feb 25, 2011 · N485FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOORWAY FUSELAGE SKIN RAIN GUTTER HAS SEVERAL RIVETS WITH LOW SPACING CUTOUT DAMAGED AREAS, FABRICATED DOUBLER, FILLER, FREEZE PLUGS, AND RAIN GUTTER, AND INSTALLED AT FWD ENTRY DOOR WAY FUSELAGE SKIN RAIN GUTTER IAW EA 7-5330-143941.
- [SDR FDEA201102250777](https://openairdocs.org/sdr/FDEA201102250777.md): Seat Track · cracked · Feb 25, 2011 · N485FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CABIN STRINGER 15L IS CRACKED AFT OF ICE LIGHT INSTALLATION BETWEEN BS 720B - 720C CUT-OUT DAMAGED AREA AT STRINGER 15L BETWEEN STA 720B TO 720C, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 3, 51-30-2, AND 51-10-2 REV 103.
- [SDR FDEA201102250775](https://openairdocs.org/sdr/FDEA201102250775.md): Skin · dented · Feb 25, 2011 · N485FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT EXTERIOR FUSELAGE SECTION 48 STA 1263 STR 25L. CUT OUT DAMAGED AREA STA 1263 STR 25L, FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-2 FIG 3, SRM 53-30-3 FIG 3, SRM 51-10-2 AND SRM 51-30-2.
- [SDR FDEA201102250766](https://openairdocs.org/sdr/FDEA201102250766.md): Stringer · cracked · Feb 25, 2011 · N485FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CABIN STRINGER 15 R IS CRACKED AFT OF ICE LIGHT INSTALLATION BETWEEN BS 720B - 720C CUT-OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 FIG 5, 51-30-2, AND 51-10-2.
- [SDR FDEA201102240731](https://openairdocs.org/sdr/FDEA201102240731.md): Angle · cracked · Feb 24, 2011 · N485FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS RT LOWER TORQUE BOX UPPER ANGLE IS CRACKED AND LOCK FASTENERS ARE WORKING AT BS 1263, FWD SIDE. REMOVED AFT AIRSTAIRS RH LOWER TORQUE BOX UPPER ANGLE AT BS 1263 FWD SIDE, FABRICATED ANGLE, AND INSTALLED IAW SRM 53-10-2 FIG 6, 51-20-1 FIG 7, 51-
- [SDR FDEA201102240730](https://openairdocs.org/sdr/FDEA201102240730.md): Web · cracked · Feb 24, 2011 · N485FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS LT LOWER TORQUE BOX INBD WEB HAS CRACK AT UPPER ROW OF RIVETS BS 1253. CUT-OUT CRACK SECTION OF WEB, FABRICATED DOUBLER AND FILLER, AND INSTALLED DOUBLER AND FILLER AT AFT AIRSTAIRS LH LOWER TORQUE BOX INBD WEB BS 1253 IAW SRM 51-40-2 FIG 1, 53-
- [SDR FDEA201102240725](https://openairdocs.org/sdr/FDEA201102240725.md): Stringer Clip · damaged · Feb 24, 2011 · N485FE · Boeing 727227 · Fuselage Main, Attach Fittings
  > MISDRILLED STRINGER/FRAME ATTACH CLIP (STRINGER TIE) IN RADIUS AT BS 1010 STR 8R. REMOVED DAMAGED STRINGER TIE IAW B727 SRM 51-30-2, FABRICATED STRINGER TIE IAW BOEING DWG 65-45313, AND INSTALLED IAW B727 SRM 51-30-2.
- [SDR FDEA201102230699](https://openairdocs.org/sdr/FDEA201102230699.md): Structure · damaged · Feb 23, 2011 · N485FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR T/R LOWER TORQUE BOX LIGHTNING HOLE HAS EXCESSIVE ROUTE OUT, BS 1233. TRIMMED OUT DAMAGED ARE, FABRICATED DOUBLER, AND INSTALLED DOUBLER AT AFT AIRSTAIRS RT LOWER TORQUE BOX LIGHTING HOLE BS 1233 IAW 53-10-2, FIG 6 AND 51-40-2, FIG 1.
- [SDR FDEA201102220676](https://openairdocs.org/sdr/FDEA201102220676.md): Floorbeam · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON TOP TEE CAP FLOORBEAM, MAIN CABIN, STA 1030, RBL 45 TO RBL 61. CUT AND REMOVED DAMAGED AREA OF FLOOR BEAM IAW SRM 53-10-8 FIG 3 FABRICATED NEW UPPER TEE, 2 REPAIR ANGLES AND 2 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED UPPER TEE,
- [SDR FDEA201102220683](https://openairdocs.org/sdr/FDEA201102220683.md): Skin · damaged · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > UPON FURTHER EVALUATION OF L-1 FWD ENTRY DOOR LOWER HINGE CUTOUT REPAIR. FOUND SEVERAL FASTENERS PULLING THROUGH DOUBLER. REPLACED PREVIOUS REPAIR DOUBLER AT L1 FWD ENTRY DOOR LOWER HINGE IAW EO 7-5330-7-2345 F2 PT2.
- [SDR FDEA201102220681](https://openairdocs.org/sdr/FDEA201102220681.md): Floorbeam · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON TEE CAP TOP FLOORBEAM MAIN CABIN, STA 680, LBL 45 TO LBL 25. REMOVED CORROSION FROM FLOORBEAM TEE CAP IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 4B. FABRICATED 1 TEE CAP 16" LONG, SUPPORT ANGLE 16" LONG, SUPPORT ANGLE 11" LO
- [SDR FDEA201102220685](https://openairdocs.org/sdr/FDEA201102220685.md): Seat Track · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, STA 1135 TO 970, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.
- [SDR FDEA201102220684](https://openairdocs.org/sdr/FDEA201102220684.md): Seat Track · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, STA 1010 TO 1035, RBL 45. REMOVED CORROSION IAW SRM 51-10-6. FOUND TO OUT OF LIMITS IAW SRM 53-10-1. FABRICATED SEAT TRACK AND SPLICES IAW SRM 53-10-5 REV 103. INSTALLED SEAT TRACK IAW SRM 51-30-2
- [SDR FDEA201102220677](https://openairdocs.org/sdr/FDEA201102220677.md): Floorbeam · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON TEE CAP FLOORBEAM, STA 620, BL 0 TO RBL 25. REMOVED CORROSION. EVALUATED AREA; ORIGINAL THICKNESS.125" MATERIAL LOSS.015" MATERIAL REMAINING.110" FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA APPROX DIM 100". FABRICATED TEE CAP & FILLE
- [SDR FDEA201102220678](https://openairdocs.org/sdr/FDEA201102220678.md): Floorbeam · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM TEE CAP, STA 720D, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA AT FLOORBEAM TEE CAP, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-8 FIG 8.
- [SDR FDEA201102220706](https://openairdocs.org/sdr/FDEA201102220706.md): Skin · cracked · Feb 22, 2011 · N485FE · Boeing 727227 · Elevator, Plate/Skin
  > RT ELEVATOR LOWER SURFACE HAS A POSSIBLE CRACK 16" FROM INBD END. STOP DRILLED CRACK IAW SRM 51-10-1 REV 103 FABRICATED REPAIR DOUBLER FROM 2024 T3.032" IAW SRM 55-20-3 FIG 4 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND EA 7-5750-143944
- [SDR FDEA201102220682](https://openairdocs.org/sdr/FDEA201102220682.md): Floorbeam · corroded · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM TEE, STA 680, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA, FABRICATED FILLER, 2 REPAIR ANGLES, AND INSTALLED IAW SRM 53-10-8 FIG 8.
- [SDR FDEA201102220689](https://openairdocs.org/sdr/FDEA201102220689.md): Frame · cracked · Feb 22, 2011 · N485FE · Boeing 727227 · Fuselage Main, Frame
  > FWD CARGO COMPARTMENT, LOWER STUB FRAME HAS CRACK AT BS 540 BETWEEN STR 22L AND 21L.
- [SDR FDEA201102210647](https://openairdocs.org/sdr/FDEA201102210647.md): Skin · gouged · Feb 21, 2011 · N485FE · Boeing 727227 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZ STAB LOWER SKIN AFT OF ACCESS PANEL 9206 IS GOUGED. REMOVED GOUGE ON RT HORIZONTAL STAB LOWER SKIN IAW SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW SRM 55-10-1 FIG 2 ORIGINAL MATERIAL.063" MATERIAL REMOVED.016" MATERIAL REMAINING.047". REMOVED
- [SDR FDEA201102190633](https://openairdocs.org/sdr/FDEA201102190633.md): Skin · corroded · Feb 19, 2011 · N485FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > AFT LAV ACCESS PANEL CUT OUT INNER DOUBLER IS CORRODED BS 1166 TO 1183. REMOVED CORRODED INNER SKIN DOUBLER AND CUT OUT SKIN SECTION IAW SRM 53-30-3 FIG 12. FABRICATED NEW SKIN SECTION, INNER DOUBLER AND SKIN SPLICE IAW SRM 53-30-3 FIG 12. INSTALLED SKIN
- [SDR FDEA201102190634](https://openairdocs.org/sdr/FDEA201102190634.md): Stringer · corroded · Feb 19, 2011 · N485FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 22L IS CORRODED FROM BS 1166 TO 1183. REMOVED CORRODED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED NEW STRINGER AND SPLICE IAW SRM 51-30-2 AND 53-10-3 FIG 1 REV 103.
- [SDR FDEA201102190632](https://openairdocs.org/sdr/FDEA201102190632.md): Web · corroded · Feb 19, 2011 · N485FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION STA 1166, PLUS 7", LBL 50. REMOVED LAV PAN LOWER WEB AND ANGLE IAW SRM 51-30-2 FABRICATED NEW WEB AND ANGLE IAW SRM 51-20-1 FIG 7 AND 51-30-5 INSTALLED NEW WEB AND ANGLE IAW SRM 51-30-2 REV 103
- [SDR FDEA201102180618](https://openairdocs.org/sdr/FDEA201102180618.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 740-690 LBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE IAW SRM 53-10-5 FIG 1. INSTALLED IAW SRM 51-30-2 REV 103.
- [SDR FDEA201102180614](https://openairdocs.org/sdr/FDEA201102180614.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, STA 740-720, BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-2 FIG 7A AND SRM 51-20-1, 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2 REV 103.
- [SDR FDEA201102180613](https://openairdocs.org/sdr/FDEA201102180613.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, MAIN CABIN, STA 690-740, RBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2 REV 103. FABRICATED SEAT TRACK AND REPAIR SPLICE IAW SRM 53-10-5 FIG 1. INSTALLED IAW SRM 53-10-5 FIG 1 AND 51-30-2.
- [SDR FDEA201102180611](https://openairdocs.org/sdr/FDEA201102180611.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 480-690 RBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2 AND 51-30-2 REV 103.
- [SDR FDEA201102180609](https://openairdocs.org/sdr/FDEA201102180609.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 690-480, BL 0. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-1 FIG 3A, SRM 53-10-2 FIG 7A, SRM 51-30-2, 51-20-1, 51-10-2, 51-30-5, AND 51-10-1.
- [SDR FDEA201102180621](https://openairdocs.org/sdr/FDEA201102180621.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 690-480, LBL 25. REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-20-1, 51-10-1, 51-10-2, AND 51-30-2.
- [SDR FDEA201102180619](https://openairdocs.org/sdr/FDEA201102180619.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE, STA 740-690, LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK AND SPLICE REPAIR, AND INSTALLED IAW SRM 53-10-5 FIG 1, 51-30-2, AND 51-10-2.
- [SDR FDEA201102180616](https://openairdocs.org/sdr/FDEA201102180616.md): Flange · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 1135 TO STA 950 10" LBL 25. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-2, 51-30-5, 51-10-1, AND 51-10-2.
- [SDR FDEA201102180615](https://openairdocs.org/sdr/FDEA201102180615.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK MAIN CABIN STA 1135 TO STA 950, 10" LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-20-1, 51-10-1, AND 51-30-2.
- [SDR FDEA201102180610](https://openairdocs.org/sdr/FDEA201102180610.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 690-480 LBL 45. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-2, 51-20-1, 51-30-5 AND 51-10-2.
- [SDR FDEA201102180612](https://openairdocs.org/sdr/FDEA201102180612.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 690-740, RBL 45. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND SPLICE, AND INSTALLED IAW SRM 53-10-5 FIG 1 AND 51-30-2.
- [SDR FDEA201102180608](https://openairdocs.org/sdr/FDEA201102180608.md): Seat Track · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 480-690, RBL 45. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, AND INSTALLED IAW SRM 53-10-2 FIG 7 AND 51-30-2.
- [SDR FDEA201102180617](https://openairdocs.org/sdr/FDEA201102180617.md): Skin · chafed · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > LT AFT FUSELAGE SKIN CHAFED AT STR 19L, BS 720D, 10". CUT-OUT DAMAGED AREA, FABRICATED DOUBLER AND STRUCTURAL FILLER, AND INSTALLED IAW SRM 53-30-1 FIG 5, 51-10-2, 51-30-8, AND 53-30-3 FIG 4.
- [SDR FDEA201102180620](https://openairdocs.org/sdr/FDEA201102180620.md): Floorbeam · corroded · Feb 18, 2011 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON TOP TEE CAP FLOORBEAM MAIN CABIN ENTRY WAY, STA 328, LBL 35. CUTOUT DAMAGED AREA, FABRICATED TEE CAP AND REPAIR ANGLES, & INSTALLED IAW SRM 53-10-1, FIG 1, 53-10-8 FIG 9, 51-30-5, 51-10-2, 51-30-2, AND FAS ENGINEERING REPORT NR 2-37153-801, REV
- [SDR FDEA201012144660](https://openairdocs.org/sdr/FDEA201012144660.md): Light · intermittent · Dec 14, 2010 · N485FE · Boeing 727227 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. R & R EMERGENCY EXIT PORTABLE LIGHT ASSY, REF MM33-50-101-2-0, OPS CHECK GOOD.

Next page: https://openairdocs.org/deregistered/N485FE-2013-08-27/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 = 'N485FE' AND deregistration_id = 'N485FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N485FE-2013-08-27/reports

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