# Service difficulty reports: N483FE, cancelled Mar 8, 2013

A list on [N483FE, cancelled Mar 8, 2013](https://openairdocs.org/deregistered/N483FE-2013-03-08.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 · 172 reports

- [SDR FDEA201205302011](https://openairdocs.org/sdr/FDEA201205302011.md): Battery · discharged · May 30, 2012 · N483FE · Boeing 727227 · Emergency Lighting
  > ESSENTIAL IN STANDBY POWER-EMERGENCY LIGHTS IN GALLEY AND FLIGHT DECK DO NOT ILLUMINATE. R & R EMERGENCY EXIT UNIT BATTERIES IAW AMM 33-56-01-2. OPS CK GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201010284185](https://openairdocs.org/sdr/FDEA201010284185.md): Connector · damaged · Oct 28, 2010 · N483FE · Boeing 727227 · Engine Oil System Wiring
  > INFLIGHT ENG SHUTDOWN NR 2 OIL TEMP FLUCTUATED INTO YELLOW RANGE. RAN QRH REDUCED POWER LEVER TO IDLE, THEN TEMP WENT ABOVE RED RADIAL. TROUBLESHOOTING DISCOVERED BROKEN WIRE GROUNDING ON THE D530 PLUG (TEMP BULB CONNECTOR) REPINNED CONNECTOR IAW CHAP 20, A
- [SDR FDEA201005181576](https://openairdocs.org/sdr/FDEA201005181576.md): Seat Track · corroded · May 18, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE MAIN CABIN BS. 620, RBL 24. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK AT RBL 24 BS 540+10" FROM BAC 1520-792-7178-T6511 IAW SRM 53-10-5 FIG 1 REV 102 INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.
- [SDR FDEA201005181577](https://openairdocs.org/sdr/FDEA201005181577.md): Stringer Clip · corroded · May 18, 2010 · N483FE · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORROSION - STRINGER 26L AT STA 1183 TENSION TIE FITTING, INSIDE CHANNEL. REMOVED SECTION OF STRINGER 26L AT STA 1183, 20" IN LENGTH IAW SRM, REV 102, 51-30-2, 51-10-1, AND 53-10-1 FIG 1. FABRICATED STRINGER USING BAC1498-145, 7075-T6, 20" IN LENGTH. FABRIC
- [SDR FDEA201005131535](https://openairdocs.org/sdr/FDEA201005131535.md): Rib · cracked · May 13, 2010 · N483FE · Boeing 727227 · Leading Edge Devices
  > LT WING NR 2 L/E SLAT INBD & OTBD RIBS ARE CRACKED WHERE ACTUATOR ROD END MOUNTS. R & R INBD & OTBD ACTUATOR RIBS PN 65-17310-3 & 65-17310-4, FABRICATED 1 EA OTBD RIB APPROX WS 251 FROM 7075-O.040 DIM: 16.25" X 6" & FABRICATED NEW ACTUATOR RIB CHANNEL FRO
- [SDR FDEA201005121524](https://openairdocs.org/sdr/FDEA201005121524.md): Floorbeam · corroded · May 12, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TOP MAIN CABIN BS 480 BL 0 TO RBL 25. CUT DAMAGE OUT AREA 2.5" X 2", FABRICATED UPPER CHORD FROM BAC 1505-100617 DIM: 14.5" AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3, REV 102 AND SRM 51-30-2.
- [SDR FDEA201005111506](https://openairdocs.org/sdr/FDEA201005111506.md): Skin · corroded · May 11, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > CORROSION, EXTERIOR SURFACE - T/E LOWER RADIUS LIP AT LT AFT LAV SERVICE DOOR CUT OUT. APPROX BS 1180, ABOVE STR 22L. REMOVED SKIN TRIPLER AT EXTERIOR SKIN T/E LOWER RADIUS LIP AT AFT LAV SERVICE DOOR BS 1180 STR 22L IAW SRM 51-30-2 AND FABRICATED NEW SKIN TR
- [SDR FDEA201005111505](https://openairdocs.org/sdr/FDEA201005111505.md): Stringer · cracked · May 11, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 22L CORRODED, BETWEEN STA 1166 - 1183, UPPER SURFACE OF UPPER CHANNEL. CUTOUT DAMAGED SECTION OF STRINGER DIM: 25".3750 AT STA 1166-1183 IAW SRM 53-10-3, FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498-143 7075T62 DIM: 25".3750 & SPLICE FROM BA
- [SDR FDEA201005101522](https://openairdocs.org/sdr/FDEA201005101522.md): Seat Track · corroded · May 10, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER LOWER FLANGE OF MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 850 - BS 870 RBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 850 - BS 870 RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-1466-7178T6 DIM: 16" & INSTALLED NEW SEAT TRACK IAW SRM
- [SDR FDEA201005091518](https://openairdocs.org/sdr/FDEA201005091518.md): Seat Track · cracked · May 9, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK SEAT TRACK MAIN CABIN RBL 24 BS 995 SECTION OF TRACK IS BS 950, 10" TO BS 1135. REMOVED DAMAGED SEAT TRACK BS 950, 10" TO BS 1135 RBL 24 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM BAC 1520-7927178T6511 DIM: 25' LONG IAW SRM 53-10-5 FIG 1. INSTA
- [SDR FDEA201005081517](https://openairdocs.org/sdr/FDEA201005081517.md): Seat Track · corroded · May 8, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION MAIN CABIN SEAT TRACK BS 870 - BS 950, LBL 24. REMOVED SEAT TRACK SECTION, FABRICATION NEW SEAT TRACK SEC FROM BAC 1520-792 717896 DIM: 7' 19", INSTALLED NEW SEAT TRACK SECTION, IAW SRM 51-30-2, 53-10-5 FIG 1 AT MAIN CABIN BS 870 - 950 LBL
- [SDR FDEA201005071488](https://openairdocs.org/sdr/FDEA201005071488.md): Frame · cracked · May 7, 2010 · N483FE · Boeing 727227 · Fuselage Main, Frame
  > CRACK IN MAIN CABIN FRAME AT BS 804.50, STR 14R. REMOVED CRACKED ANGLE CHORD, FABRICATED NEW ANGLE CHORD FROM BAC 1490-2510, DIM: 38.1250" AND INSTALLED NEW ANGLE CHORD AT BS 804.5 STR 14R IAW SRM 51-30-2, SRM 53-10-2, FIG 5, SRM 51-10-2, SRM 51-30-2, AND ER
- [SDR FDEA201005071485](https://openairdocs.org/sdr/FDEA201005071485.md): Angle · cracked · May 7, 2010 · N483FE · Boeing 727227 · Leading Edge Devices
  > SPLICE DOUBLER CRACKED - NR 7 SLAT T/E CHORD ANGLE BENEATH TAI DUCT, APPROXIMATE WING STA 619. REMOVED T/E CHORD ANGLE OF NR 7 SLAT IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND TRIMMED CHORD ANGLE, 114" LONG, IAW SRM 57-50-2 FIG 2 AND 51-30-5.
- [SDR FDEA201005061476](https://openairdocs.org/sdr/FDEA201005061476.md): Structure · cracked · May 6, 2010 · N483FE · Boeing 727227 · Leading Edge Devices
  > UPON REMOVAL OF T/E ACCESS PANELS, FOUND NR 4 SLAT T/E STRUCTURE CRACKED NEAR TAI DUCT CUTOUT. REMOVED T/E STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STRUCTURE USING EXTRUSION, BAC1514-1559 2024 T3511, DIMENSIONS 120", IAW SRM 57-50-2 FIG 2, 51-30-5, AND 51-30-
- [SDR FDEA201005051463](https://openairdocs.org/sdr/FDEA201005051463.md): Floorbeam · corroded · May 5, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION BOTTOM FLANGE FLOORBEAM BS 720 RBL 38 MAIN CABIN. CUT OUT DAMAGED AREA AT FLOORBEAM, BS 720, RBL 38, DIM: 3" X 2" IAW SRM 53-10-8, FIG 2, FABRICATED 2 NEW ANGLES 7075T6.063 DIM: 17" X 2.75", FILLER BAC 1505-100797 7075T6 DIM: 3" X 2", STRAP 707
- [SDR FDEA201005011520](https://openairdocs.org/sdr/FDEA201005011520.md): Support Angle · cracked · May 1, 2010 · N483FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE - INSIDE RT TORQUE BOX, AFT SIDE OF STA 1263 AT AFT AIR STAIR ACTUATOR SUPPORT ASSY. REMOVED SUPPORT ANGLE FROM RT SIDE OF TORQUE BOX, AFT SIDE OF STA 1263 IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED, DEBURRED AND CUT TO LENGTH EXTRUSION
- [SDR FDEA201005011468](https://openairdocs.org/sdr/FDEA201005011468.md): Skin · corroded · May 1, 2010 · N483FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FWD PIT - CORROSION ON SKIN AT BS 680 TO 685, BETWEEN STRINGERS 28R AND 27R. REMOVED CORROSION IAW SRM, REV 102, 51-10-6. FABRICATED REPAIR DOUBLER AND FILLER USING 2024-T3, FILLER DIMENSIONS:.071" X 1.1250" X 3.2500", DOUBLER DIMENSIONS:.080" X 12.7500"
- [SDR FDEA201005011420](https://openairdocs.org/sdr/FDEA201005011420.md): Stringer · corroded · May 1, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > FWD CARGO HAS EXFOLIATION CORROSION ON STRINGER 28R BETWEEN STA 680 TO 700. CUT OUT DAMAGED SECTION OF STRINGER 28R, 29.5" IN LENGTH IAW SRM, REV 102M 53-10-3 FIG 1 AND 51-10-1. FABRICATED (2) STRINGER SECTIONS USING BAC1498-143, 7075-T62, 18.5" AND 11" IN
- [SDR FDEA201005011419](https://openairdocs.org/sdr/FDEA201005011419.md): Shear Tie · corroded · May 1, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 1010 BETWEEN STRINGERS 30 AND 29 L. REMOVED DAMAGE,.7500" X 3.5" IAW SRM, REV 102, 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER FOR BS 1010 FRAME BETWEEN STRINGERS 30 AND 29L IAW SRM 53-10-4, FIG 15. INSTALLED DOUBLER IAW
- [SDR FDEA201004301435](https://openairdocs.org/sdr/FDEA201004301435.md): Seat Track · corroded · Apr 30, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CORRODED BS 870-950 10, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7927178T6511 DIM: 91" LONG IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201004291406](https://openairdocs.org/sdr/FDEA201004291406.md): Shear Tie · cracked · Apr 29, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT BS 344 BETWEEN STRINGERS 27 AND 26L CUT-OUT DAMAGE AREA DIM 3" X 1.2500" IAW SRM 53-10-4 FIG 14. FABRICATED DOUBLER REPAIR FROM 7075T6.050 DIM 4.7500" X 4.3750" IAW SRM 53-10-4, FIG 14. INSTALLED REPAIR IAW SRM 53-10-4 AND 51-30-2, REV 1
- [SDR FDEA201004271367](https://openairdocs.org/sdr/FDEA201004271367.md): Floorbeam · corroded · Apr 27, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TOP MAIN CABIN BS 950 RBL 45 TO RBL 62. CORROSION OUT OF LIMITS, R & R FLOORBEAM TOP BS 950 RBL 62.5 TO 62.5 FROM BAC 1505-100405 7075T6 DIM: 129.5" LONG IAW B. DWG NR 65-16338, SRN 53-10-1, FIG 8.
- [SDR FDEA201004241353](https://openairdocs.org/sdr/FDEA201004241353.md): Shear Tie · corroded · Apr 24, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED ON BS 990 FRAME BETWEEN STRINGERS 29L AND 28L. CUT OUT DAMAGE, 4 1/4" X 3/4" IAW SRM, REV 102, 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR DOUBLER USING 7075-0,.071" X 4 1/4" X 2 1/4" IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. INSTALLED
- [SDR FDEA201004241352](https://openairdocs.org/sdr/FDEA201004241352.md): Shear Tie · corroded · Apr 24, 2010 · N483FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 990 BETWEEN STRINGER 30 AND 29L. CUT OUT DAMAGED AREA DIMENSIONS 4 1/4" X 1 3/4" ON FRAME SHEAR TIE IAW SRM 53-10-4 FIG. 13, REV 102. FABRICATED REPAIR DOUBLER USING 7075 T-6.071" DIM 3 1/4" X 6 1/2" IAW SRM 53-10-4 FIG 13 AND 53-
- [SDR FDEA201004241351](https://openairdocs.org/sdr/FDEA201004241351.md): Floorbeam · corroded · Apr 24, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TOP SECTION MAIN CABIN BS 1130, LBL 45 - LBL 24. CUT-OUT DAMAGED AREA 2 5/8" X 1 3/8" FLOORBEAM BS 1130 LBL 45 TO LBL 24 IAW SRM 53-10-8 FIG 10 REV 102. FABRICATED REPAIR PART FROM 7075T6.050 DIM: 10 1/4" X 3 1/4" IAW SRM 53-10-8 FIG 10 R
- [SDR FDEA201004231337](https://openairdocs.org/sdr/FDEA201004231337.md): Stringer · damaged · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STR REPAIR "17 X 11" REQUIRED EVALUATION AT STA 1166 - STA 1183, STR 23L IAW WORK CARD 7-5100-7-5005 PT 1. REMOVED DOUBLER IAW SRM, REV 102, 51-30-2. FABRICATED REPAIR DOUBLER USING 2024-T3,.100" X 23 1/2" X 21 5/8" IAW EA 7-5330-135540. INSTALLED REPAIR
- [SDR FDEA201004231299](https://openairdocs.org/sdr/FDEA201004231299.md): Frame · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Frame
  > LOWER STUB FRAME EXTENSIONS, BS 540 STR 21L - 22L, CRACK ON RADIUS CUT OUT. REMOVED STUB FRAME AT BS 540 BETWEEN STRINGERS 21L - 22L IAW B727 SRM 51-30-2, REV 102. FORMED STUB FRAME USING 7075-0,.063" X 16" X 6", PO NO. 9009327 IAW B727 SRM 51-20- 1 FIG 7
- [SDR FDEA201004231300](https://openairdocs.org/sdr/FDEA201004231300.md): Frame · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Frame
  > LOWER STUB FRAME EXTENSIONS, BS 580, STR 21L - 22L, CRACK ON RADIUS CUT OUT. REMOVED STUB FRAME AT BS 580 BETWEEN STR 21L AND 22L IAW SRM, REV 102, 51-30-2. FABRICATED STUB FRAME USING 7075 - 0,.063" X 6" X 17" IAW SRM 51-20-1 FIG. 7 AND DWG NR 53FX1350
- [SDR FDEA201004231345](https://openairdocs.org/sdr/FDEA201004231345.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK SPLICE ATTACHED ON FLOOR WEB, MAIN CABIN BS. 1135 - BS 1177, LBL 45. REMOVED SEAT TRACK SECTION IN MAIN CABIN IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK DIM; 44.8750" AND FLAT BAR DIM; 4" X.5" FROM 7075T6 IAW DWG 53FX976. INSTALLE
- [SDR FDEA201004231344](https://openairdocs.org/sdr/FDEA201004231344.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK SPLICE ATTACHED ON FLOOR WEB, MAIN CABIN BS 1135 - 1177, LBL 24. REMOVED DAMAGED SEAT TRACK SECTION AND FABRICATED NEW SEAT TRACK FROM 7075T6. FLAT BAR DIM: 44.7500" & INSTALLED NEW SEAT TRACK FROM BS 1135 - BS 1177, LBL 24 IAW SRM 5
- [SDR FDEA201004231343](https://openairdocs.org/sdr/FDEA201004231343.md): Skin · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CRACK EXTENDING FROM RIVET TAIL, LT SIDE OF STRINGER 1, STA 1100. ACCOMPLISHED REPAIR LT SIDE OF STRINGER 1 STA 1100 IAW EO NR 7-5330-7-2343 F1 PT2 WO NR 00048048.
- [SDR FDEA201004231342](https://openairdocs.org/sdr/FDEA201004231342.md): Web · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > LT STAIRWELL BS 1279 LOWER VERT TORQUE BOX WEB IS CRACKED AT LIGHTENING HOLE. REMOVED DAMAGED AREA IAW SRM 51-10-1, REV 102. FABRICATED NEW DOUBLER USING MATERIAL 7075 T-6.032", PO NR. 9009134, DIM 1" X 4" IAW SRM 53-10-2 FIG 6 AND 51-40-1 FIG 1. INSTA
- [SDR FDEA201004231341](https://openairdocs.org/sdr/FDEA201004231341.md): Web · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > LT STAIRWELL BS 1266 VERT TORQUE BOX WEB IS CRACKED ON LIGHTENING HOLE. ROUTED OUT DAMAGED AREA.3" X.3750" IAW SRM 51-10-1, REV 102. FABRICATED REPAIR DOUBLER USING 7075 T-6.032", DIM 1" X 4" IAW SRM 53-10-2, FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBL
- [SDR FDEA201004231340](https://openairdocs.org/sdr/FDEA201004231340.md): Web · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > LT STAIRWELL BS 1236 VERT TORQUE BOX WEB IS CRACKED AT FASTENER. CUT OUT DAMAGED AREA.7500" X 1.2500" AT BS 1236 VERT TORQUE BOX WEB IAW SRM, REV 102, 51-10-1. FABRICATED.7500" X 1.2500" FILLER USING 7075 T-6,.025" IAW SRM 51- 40-2 FIG 1. FABRICATED REP
- [SDR FDEA201004231339](https://openairdocs.org/sdr/FDEA201004231339.md): Web · cracked · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > LT LOWER STAIR WELL TORQUE BOX BS 1228 HAS LIGHTENING HOLE CRACK. ROUTED OUT DAMAGED AREA.1875" X.5" IAW SRM, REV 102, 51-10-1. FABRICATED DOUBLER FROM MATERIAL 7075 T-6,.032" X 1" X 4" IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER
- [SDR FDEA201004231338](https://openairdocs.org/sdr/FDEA201004231338.md): Floorbeam · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TOP MAIN CABIN BS 380, RBL 25 - RBL 45. CUT-OUT DAMAGED AREA DIM: 34" X 2", FABRICATED UPPER CHORD FROM BAC 1505-100617, DIM: 34" X 2.5". FABRICATED REINFORCEMENT STRAPS FROM BAC 1512 3396-7075-T6 AND BAC 1512-3353 7075-T6 DIM: 34" X 1" AN
- [SDR FDEA201004231336](https://openairdocs.org/sdr/FDEA201004231336.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 360 - 480 LBL 25. REMOVED DAMAGED SECTION FROM STA 360 - 480 LBL 25 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178 T6511 DIM: 136" IAW P - F SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION FROM STA 3
- [SDR FDEA201004231335](https://openairdocs.org/sdr/FDEA201004231335.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 360 - 480 RBL 25. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 360 RBL 25 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 135".2500 IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK SECTION FROM S
- [SDR FDEA201004231334](https://openairdocs.org/sdr/FDEA201004231334.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 360 - BS480 BL 0. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 360 - 480 BL 0 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 136" IAW SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION STA FROM
- [SDR FDEA201004231333](https://openairdocs.org/sdr/FDEA201004231333.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SECTION NUMEROUS AREAS BS 690 - BS 720E PLUS 10" LBL 45. REMOVED SEAT TRACK FROM STA 690 TO 740 LBL 45 IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6 DIM: 171.7500" IAW SRM 53-10-5, FIG 1, INSTALLED NEW SEAT TRACK IA
- [SDR FDEA201004231332](https://openairdocs.org/sdr/FDEA201004231332.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NUMEROUS AREAS SEAT TRACK SECTION BS 690 - BS 720E PLUS 10" LBL 25. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178T6511 DIM: 172" IAW SRM 53-10-5, FIG 1. INSTALLED NEW SEAT TRACK SECTION
- [SDR FDEA201004231331](https://openairdocs.org/sdr/FDEA201004231331.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK MAIN CABIN BS 720 PLUS 18", RBL 45. REMOVED SEAT TRACK SECTION AT RBL 45 FROM BS 690 TO BS 740 IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION FROM BAC 1520-792 7178-T6511 DIM: 172" IAW SRM 53-10-5, FIG 1. INSTALLED SEAT TRACK SECTION AT R
- [SDR FDEA201004231330](https://openairdocs.org/sdr/FDEA201004231330.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON MAIN CABIN SEAT TRACK BS 850 - 870 LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG7 & 51-30-5 FROM BAC 1520-1466 DIM: 16" & INSTALLED NEW SEAT TRACK SECTION AT BS 850-870 LBL 24 IAW SRM
- [SDR FDEA201004231329](https://openairdocs.org/sdr/FDEA201004231329.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON UPPER FLANGE OF MAIN CABIN SEAT TRACK BS 890 - 950, BL 0. REMOVED SEAT TRACK AND FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178 T6511 DIM: 10' IAW SRM 53-10-5 FIG 1, REV 102 AND INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201004231328](https://openairdocs.org/sdr/FDEA201004231328.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON UPPER FLANGE OF MAIN CABIN SEAT TRACK BS 880, RBL 24. REMOVED SEAT TRACK AND FABRICATED NEW SEAT TRACK FROM BAC 1520 792-7178T6 DIM: 7 FT. X 7 IN. IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5, PG 4, FIG 1, REV 102.
- [SDR FDEA201004231327](https://openairdocs.org/sdr/FDEA201004231327.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FLANGE OF MAIN CABIN SEAT TRACK HAS SURFACE CORROSION BS 870 - 950, RBL 45. REMOVED DAMAGED SEAT TRACK FROM BS 870 - 950, 10" RBL 45, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7927178T6511 DIM: 7 FT 19 IN. & INSTALLED NEW SEAT TRACK SECTION IAW SR
- [SDR FDEA201004231326](https://openairdocs.org/sdr/FDEA201004231326.md): Skin · damaged · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage Main, Structure
  > UPON REMOVAL OF RAIN GUTTER FASTENERS ABOVE L-1 DOOR, FOUND DOUBLE DRILLED HOLE THROUGH HUCKBOLT AT BS 328. ACCOMPLISHED EA 7-5330-135539 DATED 05/18/10.
- [SDR FDEA201004231325](https://openairdocs.org/sdr/FDEA201004231325.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SECTION NUMEROUS AREAS MAIN CABIN BS 690 - BS 480, RBL 45. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 AND FABRICATED SEAT TRACK FROM BAC 1520-792-7178-T6511 DIM: 209.5" IAW SRM 53-10-5, FIG 1. FABRICATED SPLICES ANGLES FROM BAC 1503-100
- [SDR FDEA201004231324](https://openairdocs.org/sdr/FDEA201004231324.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SEGMENT NUMEROUS AREAS MAIN CABIN BS 720- BS 600, BL 0. REMOVED DAMAGED SECTION FROM STA 600 - STA 720 BL 0 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 7178 T6511 DIM: 120" IAW SRM 53-10-5 FIG 1, REV 102. IN
- [SDR FDEA201004231323](https://openairdocs.org/sdr/FDEA201004231323.md): Seat Track · corroded · Apr 23, 2010 · N483FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SECTION BS 480 -BS 600 BL 0. NUMEROUS AREAS, MAIN CABIN. REMOVED DAMAGED SEAT TRACK SECTION FROM STA 480- STA 600 BL 0 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 1778 T6511 DIM: 120 ".5 IAW SRM 53-10-2, FIG

Next page: https://openairdocs.org/deregistered/N483FE-2013-03-08/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 = 'N483FE' AND deregistration_id = 'N483FE-2013-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N483FE-2013-03-08/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.