# Service difficulty reports: N464FE, cancelled Oct 12, 2012

A list on [N464FE, cancelled Oct 12, 2012](https://openairdocs.org/deregistered/N464FE-2012-10-12.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 · 225 reports

- [SDR FDEA201006182051](https://openairdocs.org/sdr/FDEA201006182051.md): Line · leaking · Jun 18, 2010 · N464FE · Boeing 727225 · Hydraulic System, Main
  > LOST "A" SYSTEM HYDRAULICS AT FL 250. ENG 1 & 2 FLUID SHUTOFF CLOSED FOR 30 MINUTES WITH ENGINE NR 1 & 2 OPERATING. FOUND SPOILER HYD FLUID RETURN LINE NEAR WING STATION 546.5 BROKEN REPLACED SPOILER RETURN LINE PER SPM. LEAK CK`S NORMAL. SYSTEM A PRESSU
- [SDR FDEA201004131198](https://openairdocs.org/sdr/FDEA201004131198.md): Rib · cracked · Apr 13, 2010 · N464FE · Boeing 727225 · Leading Edge Devices
  > NR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O.032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A, LOCATED, DRILLED AND INSTALLED RIB IAW SRM 51-30-2, 51-20-1, AND 51
- [SDR FDEA201004041077](https://openairdocs.org/sdr/FDEA201004041077.md): Stringer · damaged · Apr 4, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DRILLED NEW STRINGER SECTION USING BAC1498-145 7075T-6 PO 29057141 DIMS 43.1250" AND INSTALLED NEW STR
- [SDR FDEA201003301031](https://openairdocs.org/sdr/FDEA201003301031.md): Skin · gouged · Mar 30, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREAS DIMS 2.3750" X 4", 2 3/8" X 5.3125" AND 1" X 3"
- [SDR FDEA201003281121](https://openairdocs.org/sdr/FDEA201003281121.md): Skin · damaged · Mar 28, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA STA 660 BETWEEN STR 3L AND 4L NO EDGE DISTANCE ON FASTENERS. CUT OUT DAMAGED AREA DIMS 3" X 3.4", FABRICATED TRIPLER USING 2024T-3.100 PO 9009120 DIMS 10 7/8" X 11 3/8", FABRICATED DOUBLER USING 2024T-3.080 PO 9009327 DIMS 11 5/8" X 13 1/2",
- [SDR FDEA201003271026](https://openairdocs.org/sdr/FDEA201003271026.md): Floorbeam · damaged · Mar 27, 2010 · N464FE · Boeing 727225 · Fuselage Main, Floor Beam
  > STA 1166 FLOORBEAM HAS DOUBLE DRILLED HOLES LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW UPPER CHORD USING BAC1505-100617 7075T-73 PO 29103139 DIMS 11 5/8" X 2", FABRICATED 2 EACH SUPPORT ANGLES USING BAC1490-2831 7075T-62 PO 9006081 DIMS 11 1/2" X 3" AND B
- [SDR FDEA201003271021](https://openairdocs.org/sdr/FDEA201003271021.md): Skin · damaged · Mar 27, 2010 · N464FE · Boeing 727225 · Trailing Edge Flaps
  > RT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2,CUT OUT 2 DAMAGED AREAS DIMS.5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3.050 DIMS 7" X
- [SDR FDEA201003261016](https://openairdocs.org/sdr/FDEA201003261016.md): Structure · corroded · Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, Structure
  > CORROSION ON NOSE WHEEL WELL RT MID-CHORD, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-19862-20 PO 20017288 AND INSTALLED IAW SRM 51-30-5, 53-10-1 AND 51-30-2.
- [SDR FDEA201003261017](https://openairdocs.org/sdr/FDEA201003261017.md): Sill · damaged · Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > C-2 DOOR CUT-OUT LOWER SILL HAS PILLOWING AT BS 970. REMOVED PREVIOUS REPAIR, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD IAW SRM 51-30-2, LOCATED AND DRILLED NEW CHORD PN 65-56129Y10 IAW SRM 51-30-5 AND INSTALLED CHORD IAW SRM 51-30-2.
- [SDR FDEA201003261018](https://openairdocs.org/sdr/FDEA201003261018.md): Skin · corroded · Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN FROM STA 580 TO 600 BETWEEN STR 27L AND 28L. THIS NR WAS INCOPORATED IN REPAIR.
- [SDR FDEA201003251010](https://openairdocs.org/sdr/FDEA201003251010.md): Frame · corroded · Mar 25, 2010 · N464FE · Boeing 727225 · Fuselage Main, Frame
  > C-2 DOOR CUTOUT AFT FRAME BS 990, UPPER FLANGE IS CORRODED WITH EXFOLIATION ON LOWER SURFACE BTWN STR. 26R-25R. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1.5" X 1", FABRICATED REPAIR ANGLE USING 15-5PH.080 DIMS 28" X 3", 2 FILLER
- [SDR FDEA201003251009](https://openairdocs.org/sdr/FDEA201003251009.md): Skin · damaged · Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew Doors
  > L-1 DOOR LOWER LIGHTNING HOLE INNER SKIN IS DAMAGED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE, DIM.1250" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER OUT OF 2024 T3.040" PO NR 9009253, DIM 1" X 3.2500" IAW SRM 51-40-2 FIG 1 AND 52-10-1, FIG 1
- [SDR FDEA201003251008](https://openairdocs.org/sdr/FDEA201003251008.md): Skin · cracked · Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew Doors
  > L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN IS CRACKED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE DIM.1250" IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER OUT OF 2024 T3.040" PO 9009253 DIM 1" X 3.7500" IAW SRM 51-40-2, FIG 1. INSTALLED REPAIR
- [SDR FDEA201003251007](https://openairdocs.org/sdr/FDEA201003251007.md): Skin · cracked · Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew Doors
  > L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN HAS UNREPAIRED CRACK, STOP DRILLED. ROUTED OUT DAMAGE AT L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN DIM 3/4" X 3/4" IAW SRM 51-10-1 REV 102 FABRICATED REPAIR DOUBLER OUT OF 2024 T3.040" PO NR 9009253 DIM 2
- [SDR FDEA201003241218](https://openairdocs.org/sdr/FDEA201003241218.md): Skin · damaged · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING STA 440 STR 10L. CUT OUT DAMAGED AREA DIMS 11" X 9.4", FABRICATED 3 FILLERS USING 2024T-3.063 DIMS 11" X 6.75", 9.75" X 11" AND 17.75" X 4.30", FABRICATED DOUBLER AND TRIPLER USING 2024T-3.071 AND 2024T-3.090 DIMS 22.50" X 2
- [SDR FDEA201003240986](https://openairdocs.org/sdr/FDEA201003240986.md): Skin · damaged · Mar 24, 2010 · N464FE · Boeing 727225 · Cargo/Baggage Doors
  > C-2 DOOR EXTERIOR SKIN HAS ROUTE OUT GREATER THAN.100" AT FWD LOWER CORNER. CUT OUT DAMAGED AREA DIM 3 1/2" X 1 1/2" ON C-2 DOOR FWD LOWER CORNER OF SKIN IAW SRM 51-10-1 AND 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER FROM 2024 T3.080" PO 9009327 DIM 21 3/8
- [SDR FDEA201003240982](https://openairdocs.org/sdr/FDEA201003240982.md): Stringer · corroded · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD PIT- CORROSION AROUND DOME NUT IN STRINGER 27R AT BS 705. CORROSION OUT OF LIMITS, REMOVED DAMAGED STRINGER, FABRICATED FILLER USING BAC1498-144 7075T-6 PO 29067266 DIMS 9" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO 20017112 AND INSTALLED
- [SDR FDEA201003241049](https://openairdocs.org/sdr/FDEA201003241049.md): Shear Tie · corroded · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT STA 720C STR'S 28R AND 27R. CORROSION OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3.040 PO NR 9009253 DIMS 5 INCH BY 2 INCH AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-2.
- [SDR FDEA201003240988](https://openairdocs.org/sdr/FDEA201003240988.md): Support · cracked · Mar 24, 2010 · N464FE · Boeing 727225 · Elevator Structure
  > CRACK ON SUPPORT ANGLE INSIDE RT ELEVATOR PANEL 9405. REMOVED CRACKED ZEE STIFFENER, FABRICATED NEW ZEE STIFFENER USING 2024T-3.032 PO NR 9009378 DIMS 18 INCH BY 2.5 INCH, LOCATED, DRILLED AND INSTALLED IAW BOEING 727 SERVICE BULLETIN 55-26 AND SRM 51-30-02.
- [SDR FDEA201003240985](https://openairdocs.org/sdr/FDEA201003240985.md): Skin · misrepaired · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR LOCATED AT STA 1223 STR 23R REQUIRES EVALUATION IAW EO 7-5100-7-5005 PH. REPAIR HAS BLIND FASTENERS INSTALLED. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS IAW SRM 53-30-3.
- [SDR FDEA201003240977](https://openairdocs.org/sdr/FDEA201003240977.md): Shear Tie · corroded · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > FWD PIT- CORROSION ON SHEAR TIE AT BS 720, AFT SIDE, BETWEEN STRINGERS 28R AND 28L. CORRSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3.040 PO 9009253 DIMS 11" X 2" AND INSTALLED IAW SRM 51-30-2, 53-10-2 AND 51- 10-6.
- [SDR FDEA201003240987](https://openairdocs.org/sdr/FDEA201003240987.md): Web · cracked · Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > FWD CARGO CUTOUT, STA 620, BETWEEN STR 24R AND 25R, CRACKED WEB. CUT OUT DAMAGED SECTION OF WEB, FABRICATED NEW FILLER USING 7075T-6.071 PO 9009353 DIMS 6" X 4", FABRICATED 2 EACH DOUBLERS USING 7075T-6.080 PO 9008389 DIMS 4" X 4" AND 4" X 3" AND INSTALLED
- [SDR FDEA201003230981](https://openairdocs.org/sdr/FDEA201003230981.md): Stringer · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD PIT BS 740 STR 27R IS CORRODED AT AFT END. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10", FABRICATED SHIMS USING 20
- [SDR FDEA201003230983](https://openairdocs.org/sdr/FDEA201003230983.md): Shear Tie · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > FWD PIT- CORROSION ON SHEAR TIE AT BS 720A (FWD SIDE) BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE, FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 27L. ORIGINAL THICKNESS.063" MATERIAL LOSS.017" MATERIAL REMAINING.046" FOUND OUT OF LIMITS
- [SDR FDEA201003230984](https://openairdocs.org/sdr/FDEA201003230984.md): Shear Tie · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > FWD PIT- CORROSION ON SHEAR TIE AT BS 720B, BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE BS 720B BETWEEN STR 28L AND 27L. ORIGINAL THICKNESS.063", MATERIAL LOSS.008" MATERIAL REMAINING.055" FOUND OUT OF LIMITS IAW SRM 51-10-6 AND SRM 53-
- [SDR FDEA201003230966](https://openairdocs.org/sdr/FDEA201003230966.md): Stringer · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD PIT STA 564 STRINGER 26L CORRODED. CUT OUT DAMAGED STRINGER DIMS 19" X 3" IAW SRM 53-10-3, FABRICATED FILLER USING BAC1498-140 7075T-6 PO 2910023 DIMS 19" X 3" IAW SRM 53-10-3. FABRICATED 2 EACH SPLICES USING BAC1498-132 7075T-6 PO 29067380 DIMS 14"
- [SDR FDEA201003230972](https://openairdocs.org/sdr/FDEA201003230972.md): Shear Tie · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > FWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 26R AND 25R. CORROSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING BAC1505-100155 7075 PO NR 20013256 AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-02.
- [SDR FDEA201003230969](https://openairdocs.org/sdr/FDEA201003230969.md): Web · gouged · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > MCD CUTOUT INNER WEB IS GOUGED IN SEVERAL SPOTS FROM BS 620 - 640 BTWN STR 4L-5L. REMOVED INNER SKIN AND 2 EACH SPLICER TO MAIN CARGO DOOR AFT UPPER AREA IAW SRM 51-30-2. FABRICATED NEW INNER SKIN MATERIAL USED 2024 T3.125" DIM. 80" X 48" IAW SRM 53-10-
- [SDR FDEA201003230967](https://openairdocs.org/sdr/FDEA201003230967.md): Shear Tie · corroded · Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > FWD PIT - CORROSION ON SHEAR TIE AT BS 585, BETWEEN STRINGERS 27R AND 26R - MARKED. REMOVED FRAME TO BS 585 BETWEEN STR 27R AND 26R IAW SRM 51-30-2 FABRICATED NEW FRAME MATERIAL USED 7075 - 0.063" PO NR 9009527 DIM 10" X 6.5" IAW SRM 51-20-1, FIG 7 AND
- [SDR FDEA201003220980](https://openairdocs.org/sdr/FDEA201003220980.md): Stringer · corroded · Mar 22, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD PIT- STRINGER 26R IS CORRODED AT BS 740. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8 1/2" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10 1/4", FABRICATED SHIMS US
- [SDR FDEA201003210970](https://openairdocs.org/sdr/FDEA201003210970.md): Angle · cracked · Mar 21, 2010 · N464FE · Boeing 727225 · Wing Miscellaneous Structure
  > LT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6.032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1/2 INCH, FABRICATED NEW LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO NR 2911884, FABRICATED 2 AN
- [SDR FDEA201003201152](https://openairdocs.org/sdr/FDEA201003201152.md): Skin · damaged · Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING STA 440, STRINGER 19L. CUT OUT DAMAGED AREA, HFEC INSPECTED CUT OUT AND EXISTING HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00. FABRICATED REPAIR STRAP USING 2024T-3.063 PO NR 9009353 DIMS 12.5" X 4.2500", REPAIR DOUBLER USI
- [SDR FDEA201003201025](https://openairdocs.org/sdr/FDEA201003201025.md): Flange · corroded · Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, Attach Fittings
  > SURFACE CORROSION ON FUSELAGE STRUCTURE FLANGE AND MONTING BRACKETS FOR FUSELAGE PANEL AFT OF NWW STA 351. CORROSION OUT OF LIMITS, REMOVED, LOCATED AND DRILLED AND INSTALLED NEW CHORD PART NUMBER 65-19861-8 PO# 79014451 IAW SRM 51-30-02 AND 51-30-5.
- [SDR FDEA201003201024](https://openairdocs.org/sdr/FDEA201003201024.md): Structure · corroded · Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT CARGO BS 950 LOWER CHORD ANGLE IS CORRODED WITH EXFOLIATION BTWN STR 29L- STR 28L. CORROSION OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PART NUMBER 65-16338-11 PO 20017118 AND INSTALLED IAW SRM 53-10-1, 51-30-5 AND 51-30-2.
- [SDR FDEA201003200979](https://openairdocs.org/sdr/FDEA201003200979.md): Angle · corroded · Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, Structure
  > FWD PIT- 740 BULKHEAD LOWER CHORD ANGLE IS CORRODED BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED ANGLE SUPPORT IAW SRM 51-30-2, FABRICATED ANGLE SUPPORT USING 7075-O.190 DIMS 10.7" X 12" IAW DWG 69-64841, HEAT TREATED TO T6 CONDITION IAW FASI ENG REPORT 2-
- [SDR FDEA201003191191](https://openairdocs.org/sdr/FDEA201003191191.md): Skin · misrepaired · Mar 19, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING FWD PIT STA 540, STR 27L CUT OUT DAMAGED AREA THRU SKIN MCD STA 540 STR 27L IAW SRM 53-30-3, FIG 1B FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4, FIG 15 FABR
- [SDR FDEA201003190963](https://openairdocs.org/sdr/FDEA201003190963.md): Stringer · corroded · Mar 19, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > AFT PIT- CORROSION IN STRINGER 27L FROM BS 1005 TO 1010.
- [SDR FDEA201003190935](https://openairdocs.org/sdr/FDEA201003190935.md): Seat Track · corroded · Mar 19, 2010 · N464FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS 1142-1165 BL0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION USING 7075T6510, DIMS 44.7500 INCHES LONG IAW P-F SRM 53-10-2 AND INSTALLED IAW SRM 51-30-2.
- [SDR FDEA201003180881](https://openairdocs.org/sdr/FDEA201003180881.md): Skin · cracked · Mar 18, 2010 · N464FE · Boeing 727225 · Trailing Edge Flaps
  > LT OTBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 348 AREA, CUTOUT, SKIN FWD OF FITTING CRACKED. TRIMMED OUT DAMAGED AREA (DIM:.2500"X.2500") IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3,.063", PO NR 9009353, DIM: 6"X4" IAW SRM 57-50-2, FIG 4. TREATE
- [SDR FDEA201003180960](https://openairdocs.org/sdr/FDEA201003180960.md): Structure · cracked · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT A/S LOWER TORQUE BOX LIGHTENING HOLE CRACKED LT SIDE BS 1326.
- [SDR FDEA201003180902](https://openairdocs.org/sdr/FDEA201003180902.md): Angle · cracked · Mar 18, 2010 · N464FE · Boeing 727225 · Leading Edge Devices
  > NR 7 SLAT LOWER T/E CHORD ANGLE REPAIR DOUBLER AT INBD UPSTOP PAD IS CRACKED. REMOVED NR 7 SLAT T/E CHORD IAW SRM 57-30-2. LOCATED AND DRILLED NEW T/E CHORD. BAC 1514-1559-2024 T3511 PO 2001728 DIM. 113.7500" IN LENGTH IAW SRM 57-30-5 AND 57-50-2, FIG 2. INS
- [SDR FDEA201003180928](https://openairdocs.org/sdr/FDEA201003180928.md): Skin · misrepaired · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR LOCATED AT STA 390 STR 25L REQUIRES EVALUATION IAW EO 7-5100-7-5005 PT1. EVALUATION DETERMINED THE EXISTING REPAIR REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER USING 2024T-3.056, PO 7178367 DIMS 13.5" X 11", F
- [SDR FDEA201003180927](https://openairdocs.org/sdr/FDEA201003180927.md): Stringer · punctured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO AREA, BS 520, STR 21L, STRINGER HAS PUNCTURE. CUT OUT DAMAGED STRINGER DIMS 14" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6. PO NR 2910023 DIMS 14" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 2001711 DIMS 11" X 3" AND 10" X 3"
- [SDR FDEA201003180926](https://openairdocs.org/sdr/FDEA201003180926.md): Stringer · damaged · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO AREA, BS 600, STR 21L, STRINGER HAS DOUBLE DRILLED HOLE. CUT OUT DAMAGED STRINGER DIMS 13" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6 PO NR 2910023 DIMS 13" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 20017112, DIMS 12" X 3"
- [SDR FDEA201003180925](https://openairdocs.org/sdr/FDEA201003180925.md): Tripler · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MCD TRIPLER HAS NUMEROUS FASTENERS WITH IMPROPER SPACING STA 460 STR'S 22L TO 24L. CUT OUT DAMAGED AREAS DIM (13.6250 X 2.7500") AND (2.2500" X 1.7500") IAW PF SRM 53-30-3, FIG 1, CW HFEC INSPECTION IAW B727 NDTM PT 6 51-00-00 FIG 23 & FIG 16, NO CRACKS NOT
- [SDR FDEA201003180921](https://openairdocs.org/sdr/FDEA201003180921.md): Skin · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING FWD PIT STA 675 STR 25L. CUT OUT DAMAGE AREA THRU SKIN TO STA 675 STR 25L IAW SRM 51-10-1. FABRICATED REPAIR PARTS STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW PF SRM 53-3-3 FIG 1B. CUT OUT DAMAGE SHEAR TIE TO STA 660 STR 27L I
- [SDR FDEA201003180920](https://openairdocs.org/sdr/FDEA201003180920.md): Skin · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 600 STR 27L. CUT OUT DAMAGE AREA THRU SKIN STA 600 STR 27L-28L IAW B727 PF 53-30-3 FIG 1B. FABRICATED REPAIR PARTS FILLER, STRUCTURAL FILLER DOUBLER AND TRIPLER IAW PF 53-30-3 FIG 1B. CUT OUT DAMAGE SHEAR TIE
- [SDR FDEA201003180919](https://openairdocs.org/sdr/FDEA201003180919.md): Skin · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING FWD PIT STA 620 STR 27L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER USING 2024T-3.080 DIMS 89" X 29.5", TRIPLER USING 2024T-3,.125 DIMS 87" X 27.5", 2 STRUCTURAL FILLERS USING 2024T-3.125 DIMS 90" X 25.5" AND 2024T-3.
- [SDR FDEA201003180918](https://openairdocs.org/sdr/FDEA201003180918.md): Skin · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING FWD PIT STA 640 STR 27L. CUT OUT DAMAGE AREA TO SKIN STA 640 STR 27L. FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE IAW SRM 53-1
- [SDR FDEA201003180917](https://openairdocs.org/sdr/FDEA201003180917.md): Skin · mismanufactured · Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH ZERO ED FWD PIT STA 680 STR 22L.

Next page: https://openairdocs.org/deregistered/N464FE-2012-10-12/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 = 'N464FE' AND deregistration_id = 'N464FE-2012-10-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N464FE-2012-10-12/reports

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