# Service difficulty reports: N488FE, cancelled Aug 10, 2015

A list on [N488FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N488FE-2015-08-10.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 5 · 214 reports

- [SDR FDEA201207072510](https://openairdocs.org/sdr/FDEA201207072510.md): Slide · dislodged · Jul 7, 2012 · N488FE · Boeing 727227 · Escape Slide
  > SLIDE FELL OFF OF L1 DOOR, DID NOT DEPLOY. INSPECTED THEN REINSTALLED L1 DOOR SLIDE IAW AMM 25-60-015-2.
- [SDR FDEA201205081765](https://openairdocs.org/sdr/FDEA201205081765.md): Gauge · out of position · May 8, 2012 · N488FE · Boeing 727227 · Escape Slide
  > ESCAPE SLIDE AIR BOTTLE PRESSURE GAUGE CAN NOT BE SEEN THROUGH COVER DOOR WINDOW. ADJUSTED ESCAPE SLIDE IN DOOR.
- [SDR FDEA201111034819](https://openairdocs.org/sdr/FDEA201111034819.md): Battery Pack · inoperative · Nov 3, 2011 · N488FE · Boeing 727227 · Emergency Lighting
  > DURING SERVICE CHECK FOUND FLIGHT COMPARTMENT EMERGENCY LIGHT DIM. R & R BATTERIES IAW SMP AND MM 33-50-001-2-0. OP'S CHECKED GOOD. FINAL CLOSED.
- [SDR FDEA201012094626](https://openairdocs.org/sdr/FDEA201012094626.md): Skin · corroded · Dec 9, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AFT OF FRAME AT BS 950F, OTBD ON STR 28R, FOUND DURING PREP TO REINSTALL AFT PIT FRAMES. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3.090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3.071 DIMS 5
- [SDR FDEA201011234481](https://openairdocs.org/sdr/FDEA201011234481.md): Frame · damaged · Nov 23, 2010 · N488FE · Boeing 727227 · Fuselage Main, Frame
  > 2 EACH OPEN HOLES IN FRAME AND REPAIR DOUBLER - STA 950C AT STR 24L. REMOVED REPAIR DOUBLER IAW SRM 51-30-2 REV 103 FORMED NEW REPAIR DOUBLER FROM 7075 O.080" DIM 8" X 4 1/2" IAW SRM 53-10-2 FIG 5 AND 51-20-1 FIG 7 INSTALLED REPAIR DOUBLER IAW SRM 51
- [SDR FDEA201011224465](https://openairdocs.org/sdr/FDEA201011224465.md): Shear Tie · cracked · Nov 22, 2010 · N488FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF SHEAR TIE FOR FRAME REMOVAL, FOUND SHEAR TIE CRACKED ON OTBD UPPER CORNER, BS 990, BETWEEN STRINGER 28R AND 29R. REMOVED SHEAR TIE IAW SRM 51-30-2 REV 103 FABRICATED NEW SHEAR TIE FROM BAC1505-39042 7075-T6511 7" LONG IAW BAC DWG 65-16340
- [SDR FDEA201011164482](https://openairdocs.org/sdr/FDEA201011164482.md): Stringer · damaged · Nov 16, 2010 · N488FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 4L AT BS 1180 TENSION TIE DAMAGED. CUT-OUT DAMAGED AREA ON STRINGER 4L FROM 1160 TO 1181.1250, DIM 21.1250", FABRICATED AND INSTALLED REPAIR AND STRINGER SECTION FROM STR. BAC 1498-145 7075T6-2, DIM 21.1250" AND 5EA REPAIR PLATES NR1 FROM 2024T3 0.250
- [SDR FDEA201011134351](https://openairdocs.org/sdr/FDEA201011134351.md): Frame · gouged · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Frame
  > FRAME GOUGED STA 1070 STR 27L, AT RADIUS OF UPPER CHORD FLANGE CUT OUT DAMAGED SECTION OF UPPER FRAME DIM 3/4" X 2 1/2 " IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075 O.071" DIM 14" X 6" IAW SRM 53-10-2, FIG 5 AND 51-40-3, FIG 1 L
- [SDR FDEA201011134348](https://openairdocs.org/sdr/FDEA201011134348.md): Skin · gouged · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > INNER SKIN GOUGED STA 1177, STR 4L. CUT-OUT DAMAGED AREA AT BS 1177 ON STR 4L DIM. 1.125" DIA., FABRICATED REPAIR DOUBLER AND LAP FILLER FROM 2024T3 0.063" DIM. DOUBLER 10" X 6.8750" FILLER 11" X 4.5", AND INSTALLED DOUBLER AND FILLER IAW EA 7-5330-143918.
- [SDR FDEA201011134350](https://openairdocs.org/sdr/FDEA201011134350.md): Structure · cracked · Nov 13, 2010 · N488FE · Boeing 727227 · Trailing Edge Flaps
  > LEFT INBD MID FLAP AFT LOWER CHORD IS CRACKED AT 3 CUTOUTS. REMOVED CRACKED CHORD SECTION. FABRICATED NEW SECTION USING BAC1503-100046 7075 T6 DIMS 77" AND INSTALLED ALL REPAIR PARTS IAW SRM 57-50-2, 51-30-5 AND 51-30-2.
- [SDR FDEA201011134349](https://openairdocs.org/sdr/FDEA201011134349.md): Skin · dented · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT EXTERIOR FUSELAGE SKIN STA 1100 TO 1148 STR 22R. CUT OUT DAMAGED AREA DIMS 40 1/2" X 3 7/8". FABRICATED REPAIR DOUBLER USING 2024T-3.071 DIMS 49 7/8" X 11 1/2", 3 SHIMS USING 2024T-3.063 DIMS 40 1/2" X 1" EACH, 2 SHEAR TIE SHIMS FOR STA 1148 USNIG 2024T
- [SDR FDEA201011134346](https://openairdocs.org/sdr/FDEA201011134346.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 500 TO 690 RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 RBL 45 FROM BAC 1520-792-7178T6 DIM. 18 FEET IN LENGTH, 2EA SPLICE REPAIR FROM BAC 1503- 100122 -7178 DIM. 15" AND STRAP FROM 7075T6 0.250 DIM
- [SDR FDEA201011134344](https://openairdocs.org/sdr/FDEA201011134344.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 480 TO 600 BL0. REMOVED, FABRICATED, AND INSTALLED NEW SAET TRACK SECTION AT BS 480 TO 600 BL0 FROM BAC 1520-792-7178T6511 DIM. 120" LONG IAW FEDEX B727 P-F SRM 53-10-2 FIG 7A AND B727 SRM 51-30-5, 51-30-8, 51-10-1, 51-10-2, AND 51
- [SDR FDEA201011134340](https://openairdocs.org/sdr/FDEA201011134340.md): Floorbeam · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 620 LBL 45 TO LBL 25. REMOVED PREVIOUS REPAIR AND CUT-OUT FLOORBEAM DIM. 28.75". FABRICATED AND INSTALLED REPAIR UPPER CHORD AND SPLICES FROM BAC 1505-100617 7075T73511 DIM. 105" LONG, SPLICE FROM BAC 1490-2831 7075T62 DIM. 7.3" LONG, AN
- [SDR FDEA201011134337](https://openairdocs.org/sdr/FDEA201011134337.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 480 TO 690 LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 LBL 45 FROM BAC 1520-792-7178T6 DIM 209.375" LONG IAW B727 SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.
- [SDR FDEA201011134343](https://openairdocs.org/sdr/FDEA201011134343.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 480 TO 610 RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480 TO 690 RBL 24.75 AND SPLICE AT BS 690, SEAT TRACK FROM BAC 1520-792-7178T6 DIM. 209 1/2" LONG, SPLICE FROM BAC 1503-100122-7178 DIM. 14 3/4" LONG
- [SDR FDEA201011134334](https://openairdocs.org/sdr/FDEA201011134334.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 360 TO 480, RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2.
- [SDR FDEA201011134341](https://openairdocs.org/sdr/FDEA201011134341.md): Floorbeam · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 560, LBL 25 TO LBL 45. CUT-OUT DAMAGED AREA TOP TEE CAP FLOORBEAM BS 560 LBL 36.40 TO 39 APPROX DIM. 2.6" X.90", FABRICATED REPAIR PARTS 2EA ANGLES FROM BAC 1490-2888-7075T6 DIM.19.5" X 0.90" AND 9.6" X.080". REPAIR FILLER FROM 2024
- [SDR FDEA201011134336](https://openairdocs.org/sdr/FDEA201011134336.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 480 TO 680 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480TO 690 LBL 25 FROM BAC 1520-792-7178T6 DIM. 209.5" LONG, SPLICE REPAIR 2EA. FROM 1503-100122 7178T6 DIM 14.375", AND STRAP FROM 7075T6 0.250" DI
- [SDR FDEA201011134345](https://openairdocs.org/sdr/FDEA201011134345.md): Floorbeam · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 380, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA DIMS 2.3" X.90". FABRICATED 2 REPAIR ANGLES USING BAC1490- 2888-7075T6 DIMS 13.4" X 2.7" AND 10.2" X 2.6" AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10- 2.
- [SDR FDEA201011134342](https://openairdocs.org/sdr/FDEA201011134342.md): Floorbeam · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 440, LBL 25 TO BL 0. CUT OUT DAMAGED AREA DIMS 2.5" X 2". FABRICATED UPPER CHORD USING BAC1505-100617-7075T3 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2785-7075T6 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2831-7075T6 DIMS 11.65", REINFORC
- [SDR FDEA201011134338](https://openairdocs.org/sdr/FDEA201011134338.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 690 TO 740, LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178- T6 DIM. 172" LONG, 2EA ANGLES FROM BAC 1503-100122-7178-T6511 DIM. 16" LONG, AND STRAP FROM 7075T6 0.250" DIM. 8" X 2" IAW SRM 53-
- [SDR FDEA201011134335](https://openairdocs.org/sdr/FDEA201011134335.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 360 TO 480 RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AT BS 344 TO 480 RBL 45 FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2, AND 51-30-2 REV 103.
- [SDR FDEA201011134333](https://openairdocs.org/sdr/FDEA201011134333.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 360 TO 480 BL 0. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178T6 DIM. 136" LONG IAW SRM 53-10-2 FIG 7A REV D AND SRM 51-30-5, 51-10-1, 51-10-2 AND 51-30-2 REV 103.
- [SDR FDEA201011134332](https://openairdocs.org/sdr/FDEA201011134332.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 360 TO 480 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51- 10-2, AND 51-30-2 REV 103.
- [SDR FDEA201011134331](https://openairdocs.org/sdr/FDEA201011134331.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 360 TO 480 LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 344 TO 480 LBL 45 FROM BAC 1520-792-7178T6 DIM 136.5" LONG IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1 51-10-2 AND 51-30-2 REV 103.
- [SDR FDEA201011134330](https://openairdocs.org/sdr/FDEA201011134330.md): Skin · bulged · Nov 13, 2010 · N488FE · Boeing 727227 · Cargo/Baggage Doors
  > C2 DOOR EXTERIOR SKIN HAS A BULGE AFT CORNER. CUT OUT DAMAGED AREA DIMS 1 1/4" X 2". FABRICATED DOUBLER USING 2024T-3.080 DIMS 10" X 5" AND INSTALLED IAW SRM 52-00-3.
- [SDR FDEA201011134329](https://openairdocs.org/sdr/FDEA201011134329.md): Skin · chafed · Nov 13, 2010 · N488FE · Boeing 727227 · Emergency Exits
  > LEFT FORWARD OVERWING EMERGENCY EXIT HATCH PREVIOUS REPAIR AT TOP AFT EDGE HAS CHAFFING DAMAGE. REMOVED PREVIOUS REPAIR AND FILLER. FABRICATED NEW DOUBLER REPAIR USING 2024T-3.050 DIMS 8 1/8" X 4 1/8" AND FILLER USING 2024T-3.050 DIMS 1 5/8" X 1 3/8" AND
- [SDR FDEA201011134328](https://openairdocs.org/sdr/FDEA201011134328.md): Seat Track · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 1010 TO 1130 BL 0. REMOVED DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK USING BAC1520-792-7178T6 DIMS 10' AND INSTALLED IAW SRM 53-10-2, SRM 51-10-1 AND SRM 51-30-2.
- [SDR FDEA201011134347](https://openairdocs.org/sdr/FDEA201011134347.md): Skin · gouged · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620, STR'S 6L AND 10L. REMOVED MCD INNER SKIN AND SPLICES AT BS 594 TO 640 STR 2R TO 6L, FABRICATED INNER SKIN AND SPLICES FROM 2024T3 0.125" APPROX DIM 80" X 48" AND 22" X 11" AND INSTALLED INNER SKIN AND SPLICES IAW SRM 51
- [SDR FDEA201011134339](https://openairdocs.org/sdr/FDEA201011134339.md): Stringer · corroded · Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER CORRODED STA 950C TO 950D, STR 29L. R & R STRINGER 29L FROM BS 950 TO 1010 IAW SRM 51-30-5 AND 51-30-2 REV 103 AND DWG NR65-56441.
- [SDR FDEA201011094616](https://openairdocs.org/sdr/FDEA201011094616.md): Skin · gouged · Nov 9, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > GOUGE EXTERIOR FUSELAGE BOTTOM FWD CORNER OF C2 CUT OUT STA 950E, STR 26R. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3.090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3.071 DIMS 55" X 14" AND 51" X 13", FABRICATED 1
- [SDR FDEA201011084443](https://openairdocs.org/sdr/FDEA201011084443.md): Shear Tie · corroded · Nov 8, 2010 · N488FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT STA 720D BETWEEN STR'S 25L AND 26L. REMOVED PREVIOUS SHEAR TIE REPAIR DOUBLER IAW SRM 51-30-2 FABRICATED NEW SHEAR TIE REPAIR DOUBLER FROM 7075 O.071" DIM 5" X 2" IAW SRM 53-10-2 FIG 3, 51-20-1 FIG 7, AND 53-10-4 FIG 15. INSTALLE
- [SDR FDEA201011074441](https://openairdocs.org/sdr/FDEA201011074441.md): Structure · misinstalled · Nov 7, 2010 · N488FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > L1 DOOR RAIN GUTTER FWD ATTACMENT HAS 2 FASTENERS WITH IMPROPER SPACING STA 300 TO STA 312. CUT-OUT AFFECTED AREAS IAW EA 7-5330-143916. FABRICATED FREEZE PLUGS, FILLERS, AND DOUBLER IAW EA 7-5330-143916. INSTALLED REPAIR PARTS IAW EA 7-5330-143916 AT L-1 DO
- [SDR FDEA201011074442](https://openairdocs.org/sdr/FDEA201011074442.md): Web · cracked · Nov 7, 2010 · N488FE · Boeing 727227 · Fuselage Main, Structure
  > AFT AIRSTAIRS AREA RIGHT HAND LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED STA 1223 RBL 25 CUT OUT DAMAGED AREA DIM 1" X 0.6" IAW SRM 51-10-1 FABRICATED WEB REPAIR FROM 7075 T6.032" DIM 2.6" X 2" IAW 53-10-2 FIG 6 AND 51-40-2 FIG 1 TREATED AND PRI
- [SDR 08FDEA04076](https://openairdocs.org/sdr/08FDEA04076.md): Stringer Clip · damaged · Sep 28, 2008 · N488FE · Boeing 727227 · Fuselage Main, Attach Fittings
  > STRINGER CLIP DAMAGED AT STR 26L, FS 540, LBL 23, WL 152. REMOVED AND REPLACED STRINGER CLIP AT STA 540 STRINGER 26L LBL 23 REF SRM 51-30-2 PG 5. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA04075](https://openairdocs.org/sdr/08FDEA04075.md): Stringer · damaged · Sep 28, 2008 · N488FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER DAMAGED AT BS 540 WL 152 LBL 23. FABRICATED NEW STRINGER SECTION AND TWO SPLICE REPAIRS ON STRINGER 26L BS 540 LBL 23 REF SRM 53-10-3 FIG 1. TREATED, PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2, 51-10-3 FIG 1. THIS IS CLASSIFIED AS A
- [SDR 08FDEA04072](https://openairdocs.org/sdr/08FDEA04072.md): Frame · damaged · Sep 27, 2008 · N488FE · Boeing 727227 · Fuselage Main, Frame
  > RT AFT EMERGENCY EXIT HATCH CUTOUT, AFT FRAME DAMAGED AT RIVET LOCATION BLENDED AREA OF FRAME, FABRICATED REPAIR PARTS, CAD PLATED, TREATED, PRIMED AS NEEDED. INSTALLED ALL PARTS AND REMOVED FASTENERS AND SIDEWALLS FOR ACCESS REF EA 7-5310-114033.
- [SDR 08FDEA04068](https://openairdocs.org/sdr/08FDEA04068.md): Retainer · corroded · Sep 26, 2008 · N488FE · Boeing 727227 · Wing Miscellaneous Structure
  > LT WING SPAR UNDERWING PANEL SEAL RETAINER HAS CORROSION O/B OF APU FIRE BOTTLE AT WS 182 TO 200. FABRICATED SEAL RETAINER REF DWR 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PG 1- 9. INSTALLED SEAL RETAINER REF 51-30-2 P1-3. THIS IS A CLASSIFIED A MIN
- [SDR 08FDEA04066](https://openairdocs.org/sdr/08FDEA04066.md): Retainer · corroded · Sep 26, 2008 · N488FE · Boeing 727227 · Wing Miscellaneous Structure
  > LT WING REAR SPAR LWR CHORD APPROX STA 182, SEAL RETAINER CORRODED REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED NEW RETAINER REF DWG 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-3. INSTALLED SEAL RETAINER REF SRM 51-30-2 PG'S 1-3. THIS IS CLASSI
- [SDR 08FDEA04038](https://openairdocs.org/sdr/08FDEA04038.md): Frame · cracked · Sep 25, 2008 · N488FE · Boeing 727227 · Wing Spar
  > RT WING, I/B AILERON LOWER T/E PANEL FRAME CRACKED WITH MISSING ATTACH FASTENER AT AFT END OF FRAME 10 INCH O/B FROM I/B END OF AILERON REMOVED DAMAGED PANEL FRAME REF SRM 51-30-2. VERIFIED MATERIAL OF FRAME TO BE BAC1506-1625 7075-T6. FABRICATED REPLACEME
- [SDR 08FDEA03933](https://openairdocs.org/sdr/08FDEA03933.md): Channel · cracked · Sep 18, 2008 · N488FE · Boeing 727227 · Wing Miscellaneous Structure
  > RT WING, I/B AILERON O/B L/E SEAL MOUNT BRACKET/UNDERWING PANEL MOUNT BRACKET CRACKED 10 INCH I/B FROM O/B END OF AILERON REMOVED SEAL MOUNT BRACKET AND ATTACH ANGLE, FABRICATED NEW "U" CHANNEL. FABRICATED NEW ATTACH ANGLE, HEAT TREATED TO T4 CONDITION. U CH
- [SDR 08FDEA03928](https://openairdocs.org/sdr/08FDEA03928.md): Seat Track · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK I/B FLANGE FROM FS 1171 - FS 1146, LBL 24, WL 208. REMOVED CORROSION ON SEAT TRACK, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS.135 INCH REMAINING.127 INCH MATERIAL LOSS.008 INCH W
- [SDR 08FDEA03927](https://openairdocs.org/sdr/08FDEA03927.md): Seat Track · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK ATTACH FLANGE, FS 1171 TO 1162, LBL 1, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS. NO DEFECTS WERE FOUND, ORIGINAL THICKNESS.190 INCH, REMAINING.174 INCH, MATERIAL LOSS.016 WITHIN LIMITS, REF EA 7-531
- [SDR 08FDEA03926](https://openairdocs.org/sdr/08FDEA03926.md): Seat Track · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TOP OF SEAT TRACK ATTACH FLANGE, FS 1140-1173, RBL1, WL 208. REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS.190,.175 REMAINING, MATERIAL LOSS.015 WITHIN LIMITS REF EA 7-5310-11403. TREATED AND
- [SDR 08FDEA03925](https://openairdocs.org/sdr/08FDEA03925.md): Seat Track · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED AT FS 1164 TO FS 1160, BL 0, WL 208 REMOVED DAMAGED, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS.175 REMAINING.167 MATERIAL LOSS.008" WITHIN LIMITS REF EA 7-5310-114031. TREATED AND PRIMED ARE
- [SDR 08FDEA03923](https://openairdocs.org/sdr/08FDEA03923.md): Seat Track · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT ATTACH FASTENER ON SEAT TRACK, FS 1174, LBL25, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS.065 INCH REMAINING.061 INCH MATERIAL LOSS.004 INCH WITHIN LIMITS. REF EA NR 7
- [SDR 08FDEA03922](https://openairdocs.org/sdr/08FDEA03922.md): Intercostal · corroded · Sep 17, 2008 · N488FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > LWR EXT FUSE WING BODY FRG SUPPORT FRAME INTERCOSTAL ASSY INT SURF IS CORRODED BS 773, LBL9- RBL 9, WL 140. FABRICATED NEW SPLICE PLATE AND INSTALLED, REF BOEING DWG 65-58504. REMOVED FRAME SUPPORT, REMOVED CORROSION ON SLICE PLATE MATERIAL LOSS 50 PERCENT O
- [SDR 08FDEA03889](https://openairdocs.org/sdr/08FDEA03889.md): Skin · cracked · Sep 16, 2008 · N488FE · Boeing 727227 · Passenger/Crew Doors
  > DOOR L-1, INTERIOR AFT SKIN CRACKED AT 2 STOP PIN LOCATIONS (MKD). REPAIRED 2 DAMAGE AREA'S AT DOOR L-1 INTERIOR AFT SKIN STOP PIN LOCATIONS. HFEC IAW NDT MANUAL PART 6 51-00-00 FIG 23. TOOLING ID NR 0065 19 SEP 08. FOUND CRACKED. REMOVED DAMAGE AND REPAI
- [SDR 08FDEA03888](https://openairdocs.org/sdr/08FDEA03888.md): Skin · damaged · Sep 16, 2008 · N488FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DURING STRINGER REPAIR AT FS 550 AND STR 26L EXISTING HOLE LOCATED IN STRINGER ONLY WAS DRILLED THRU FUSELAGE SKIN. THE HOLE THRU THE SKIN IS BETWEEN 2 MANUFACTURING SKIN FALLING ON THE EDGE OF THE FWD SKIN LEAVING NO EDGE DISTANCE. FABRICATED REPAIR DOUBLER

Next page: https://openairdocs.org/deregistered/N488FE-2015-08-10/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 = 'N488FE' AND deregistration_id = 'N488FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N488FE-2015-08-10/reports

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