# Service difficulty reports: N466FE, cancelled Mar 8, 2013

A list on [N466FE, cancelled Mar 8, 2013](https://openairdocs.org/deregistered/N466FE-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 · 154 reports

- [SDR FDEA201206242352](https://openairdocs.org/sdr/FDEA201206242352.md): Actuator · failed · Jun 24, 2012 · N466FE · Boeing 727225 · Leading Edge Slat Actuator
  > AFTER TAKEOFF, PERFORMING THE AFTER TAKEOFF CHECKLIST, WHEN FLAPS WERE POSITIONED FROM 5 TO 20, L/E FLAPS AMBER LIGHT ILLUMINATED. PERFORMED LEADING EDGE DEVICE FAILURE DURING FLAP RETRACTION CHECKLIST. RETURNED TO DEPARTURE, INSTALLED NR 6 RT LEADING SLAT
- [SDR FDEA201206062103](https://openairdocs.org/sdr/FDEA201206062103.md): Fairing · damaged · Jun 6, 2012 · N466FE · Boeing 727225 · Trailing Edge Flaps
  > LT WING OTBD FLAP T/E DAMAGED. RT OTBD FLAP TRACK AFT CANOE FAIRING. MM 27-51-031-4. R & R LT OTBD T/E AFT FLAP IAW MM 27-51-012-4. R & R LT OTBD FLAP TRANSMISSION FAIRING IAW MM 27-51-023-4 REQ ADJUSTMENT CK. ADJUSTMENT CHECKED OK FOR LT OTBD FLAP TRANS
- [SDR FDEA201206062102](https://openairdocs.org/sdr/FDEA201206062102.md): Structure · damaged · Jun 6, 2012 · N466FE · Boeing 727225 · Ailerons
  > LT WING OTBD AILERON DAMAGED ON BOTTOM. REMOVED DAMAGED OTBD LT AILERON ASSY. REF MM 27-10-031-2. INSTALLED NEW SERVICEABLE LT OTBD AILERON ASSY. STILL REQ RIG & OPS CK. REF MM 27-10-031-2. ADJ AND OPS CHECK LT OTBD AILERON IAW MM 27-10-000-5, CHECKS NOR
- [SDR FDEA201206062101](https://openairdocs.org/sdr/FDEA201206062101.md): Panel · damaged · Jun 6, 2012 · N466FE · Boeing 727225 · Wing, Plate/Skin
  > PANEL 8108 ON LOWER LT WING DAMAGED. PANEL ROUTED TO COMPOSITE SHOP FOR EVALUATION. COMPLIED WITH REPAIR OF PANEL IAW EA 7-5750-161352, PART 1.
- [SDR FDEA201206062100](https://openairdocs.org/sdr/FDEA201206062100.md): Skin · damaged · Jun 6, 2012 · N466FE · Boeing 727225 · Wing, Plate/Skin
  > ON LOWER LT WING DAMAGED. R & R LT LOWER WING PANEL 7217 AND LEAK CHECKED GOOD IAW AMM 28-11-021-4.
- [SDR FDEA201112165323](https://openairdocs.org/sdr/FDEA201112165323.md): Battery Pack · discharged · Dec 16, 2011 · N466FE · Boeing 727225 · Emergency Lighting
  > RT DOOR MOUNTED EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE, BATTERY DEAD. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY BACK IAW MM 33-50-121-2-0. OPS CHECKED NORMAL.
- [SDR FDEA201109274149](https://openairdocs.org/sdr/FDEA201109274149.md): Gauge · out of position · Sep 27, 2011 · N466FE · Boeing 727225 · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE NEEDS TO BE REPLACED/ADJUSTED TO ALLOW PRESSURE GAUGE TO BE VIEWED. REPOSITIONED SLIDE TO ACCOMODATE THE VIEWING IAW MM 25-60-015-2-0.
- [SDR FDEA201107132687](https://openairdocs.org/sdr/FDEA201107132687.md): Wire · shorted · Jul 13, 2011 · N466FE · Boeing 727225 · Light System Wiring
  > EVACUATION SLIDE LIGHT ON MAIN ENTRANCE DOOR INOP. R & R BATTERY REF MM 33-50-121-2, OPS CHECKED BAD. CHECKED ORIGINAL BATTERY AND IT WAS SHOWING GOOD, REINSTALLED ORIGINAL BATTERY. REPLACED ALL 4 BULBS MM 33-50-121-2, OPS CHECKED BAD. NEW LIGHT ASSY, ATTE
- [SDR FDEA201106212355](https://openairdocs.org/sdr/FDEA201106212355.md): Solenoid Valve · cracked · Jun 21, 2011 · N466FE · Boeing 727225 · Rudder Control System
  > SYSTEM A QTY DECREASED DURING CLIMBOUT AT 10,000 FT. ON LOWER RUDDER POWER UNIT CONTROL, HYD SOLENOID VALVE LEAKING. REPLACED VALVE ASSY AND SEALS IAW MM 27-20-142-4. SYS "A" HYD SYS FILTERS REPLACED IAW MM 29-11-062-3, NO METAL FOUND IN SYS. R & R SYS A
- [SDR FDEA201012014531](https://openairdocs.org/sdr/FDEA201012014531.md): Control Valve · failed · Dec 1, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control System
  > ACFT DID NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE SHOWED CLOSED, CARGO HEAT OUTFLOW CLOSED. ALL DOOR LIGHTS INDICATED CLOSED. PRESSURIZATION SYS APPEARED TO BE WORKING, NORMAL OTHERWISE. ALSO COULD NOT GAIN CONTROL IN STBY MODE. RESEALED NOSE GEAR A
- [SDR FDEA201011274497](https://openairdocs.org/sdr/FDEA201011274497.md): Flap System · malfunctioned · Nov 27, 2010 · N466FE · Boeing 727225 · Leading Edge Slat Control System
  > AT FLAPS 2 POSITION THE AMBER L/E FLAPS LIGHT STAYS ILLUMINATED. L/E DIVICES POSITION INDICATOR SHOWS NORMAL LED CONFIGURATION. RELEASED FOR SERVICE IAW MEL: 27-06-C CATEGORY: C EXPIRATION: 07DEC10 "MEL 27-06-C: AMBER L/E FLAPS LIGHT ON THE FWD INSTRUMENT
- [SDR FDEA201010264174](https://openairdocs.org/sdr/FDEA201010264174.md): Valve · inoperative · Oct 26, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control System
  > RT AIR MIX VALVE STUCK FULL COLD. FOLLOWED BY LOSS OF CABIN PRESSURIZATION. RAN PACKS INDIVIUALY AND TOGETHER. PERFORMED LEAK CK OF DUCTS, PACKS, MIX VLVS. NO DEFECTS NOTED. PERFORMED BITE TEST OF 35 DEG VALVE AND WATCHED VALVES OPERATE. PULLED C/B ON
- [SDR FDEA201008062865](https://openairdocs.org/sdr/FDEA201008062865.md): Stringer · misrepaired · Aug 6, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > ILLEGAL REPAIR (STRINGER) STR 27L BS 540 - BS 560 FWD PIT. CUT OUT STRINGER SECTION FROM STA 550 TO 590 STR 27L IAW SRM 53-10-3 FIG 1. FAB REPAIR PARTS HAT SECTION MAT USED BAC1498-141 7075-T6 2 EA DIM 21" LONG AND 22" LONG. 2 EA SPLICERS, MAT USED BAC1498-13
- [SDR FDEA201008042813](https://openairdocs.org/sdr/FDEA201008042813.md): Stringer · corroded · Aug 4, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STR 23R CORRODED BELOW FRAME AT BS 720E. FOUND DURING CLEANING. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498 -144, 7075-T6 DIM 16 1/4", SPLICES FFROM BAC 1498-132, 7075-T6, DIM 16 1/
- [SDR FDEA201008032789](https://openairdocs.org/sdr/FDEA201008032789.md): Skin · gouged · Aug 3, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620-630, STR 16L. REPAIRED MCD INNER SURROUND SKIN IAW EA 7-5330-135571.
- [SDR FDEA201008032934](https://openairdocs.org/sdr/FDEA201008032934.md): Skin · cracked · Aug 3, 2010 · N466FE · Boeing 727225 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZ STAB HAS PROTRUDING DENT AT ELEV STA 140 WITH CRACK INDICATION. CUTOUT DAMAGED AREA DIM.7500" X.7500" AND FABRICATED REPAIR DOUBLER FROM 2024-T3, 0.032" DIM. 3" X 3" IAW SRM 55-20-3, FIG 4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR
- [SDR FDEA201007312747](https://openairdocs.org/sdr/FDEA201007312747.md): Skin · cracked · Jul 31, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > BS 1290 LIGHTNING HOLE HAS CRACK LBL18 TRIMMED OUT DAMAGE DIM. 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 7075-T6 0.032" DIM. 3 1/2" X 21/2" IAW SRM 51-40-2 FIG. 1. TREATED, PRIMED AND INSTALLED DOUBLER AT BS 1290 LIGHTING HOLE LBL 18 IAW SRM 51-10-2, 51-30-2,
- [SDR FDEA201007312853](https://openairdocs.org/sdr/FDEA201007312853.md): Seat Track · corroded · Jul 31, 2010 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 760 TO 789 RBL 45 IS CORRODED. REMOVED SEAT TRACK AND TEE SECTION BS 760 TO BS 848 RBL 45 IAW SRM 51-30-2. LOCATED AND DRILL NEW TEE SECTION FROM BAC1506-1108 7075-T6 DIM. 110" LONG IAW SRM 53-10-2 FIG. 7 AND 51-30-5. TREATED AND PRIMED NEW
- [SDR FDEA201007302734](https://openairdocs.org/sdr/FDEA201007302734.md): Support · cracked · Jul 30, 2010 · N466FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT INNER UPPER, DOOR FRAME SUPPORT FASTENER HOLE CRACKED STA 620. REPAIRED MAIN CARGO COMPARTMENT INNER UPPER DOOR FRAME SUPPORT STA 620 IAW EA 7-5310-135576.
- [SDR FDEA201007302733](https://openairdocs.org/sdr/FDEA201007302733.md): Skin · gouged · Jul 30, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED MCD INNER SKIN AFT UPPER SECTION BS 620 STR4L IAW SRM 51-30-2. FABRICATED NEW MCD INNER SKIN SECTION FROM 2024 T3 0.125" DEMINSION 79" X 48" IAW SRM 53-10-2 FIGURE 3A REV J. TREATED AND PRIMED AND INSTALL
- [SDR FDEA201007302732](https://openairdocs.org/sdr/FDEA201007302732.md): Floorbeam · damaged · Jul 30, 2010 · N466FE · Boeing 727225 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS DOUBLE DRILL HOLES BS 480 LBL 45. OVERSIZED HOLES TO 5/32" AND INSTALLED FASTENERS IAW SRM 51-30-5. WITHIN LIMITS IAW SRM 53-10-1 FIGURE 4B.
- [SDR FDEA201007292715](https://openairdocs.org/sdr/FDEA201007292715.md): Seat Track · corroded · Jul 29, 2010 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 620 - 660 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 7178-T651 DIM. 17.5 FT. IAW SRM 53-*10-2 FIG 7A REV J AND SRM 51-30-5. TREATED, PRIMED AND INSTALLED MAIN CABIN SEAT TRACK SECTI
- [SDR FDEA201007292714](https://openairdocs.org/sdr/FDEA201007292714.md): Frame · corroded · Jul 29, 2010 · N466FE · Boeing 727225 · Fuselage Main, Frame
  > CORROSION ON UPPER FLANGE OF FRAME AT BS 1148 BETWEEN STRINGER 27L AND 26L. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS.063, MATERIAL LOSS.003. FOUND WITHIN LIMITS IAW SRM 53-10-1 AND 53-10-2.
- [SDR FDEA201007292720](https://openairdocs.org/sdr/FDEA201007292720.md): Skin · gouged · Jul 29, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STR 620 STR 8L. BLENDED OUT DAMAGE AND FOUND ORIGINAL MAT 0.125", REMAINING MATERIAL 0.115", MATERIAL LOSS 0.010", REMOVED INNER SKIN SPLICE AND FABRICATED NEW SECTION FROM 2024-T3 0.125" DEMENSION 22"X11" IAW SRM 51-30-2 AND SR
- [SDR FDEA201007282738](https://openairdocs.org/sdr/FDEA201007282738.md): Skin · chafed · Jul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > BS 720B, 8" RBL 2 RAM AIR DUCT STIFFENING BOLT CHAFING HOLE IN FUSELAGE SKIN. CUT OUT DAMAGED AREA FUSELAGE SKIN BS 720C 8 RBL2. DIMENSIONS (1 3/8" X 1 3/8") IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER MAT USED 2024 T3.125" DIM (12 1/4" X 9 7/8") AND
- [SDR FDEA201007282703](https://openairdocs.org/sdr/FDEA201007282703.md): Skin · misinstalled · Jul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT, STRINGER 25L HAS SEVERAL FASTENERS IMPROPERLY INSTALLED FROM STA 540-600. CUT-OUT SKIN DOUBLER AND TRIPLER (6EA) BS 560 - 620 STR 25L DIM. 2 3/4" X 2 1/8" AND FABRICATED REPAIR FILLER FROM 2024-T3 0.125" DIM. 71.5" X 11.5", REPAIR DO
- [SDR FDEA201007282702](https://openairdocs.org/sdr/FDEA201007282702.md): Skin · corroded · Jul 28, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STA 1070 STR 28L HAS CORROSION AND FASTENER NO E.D. CUTOUT DAMAGED AREA DIMENSION 5 1/8" X 2 7/8" AND 4 1/8" X 1 1/8" AND FABRICATED REPAIR DOUBLER FROM 2024T3.063 DIMENSION 28 1/2" X 9 1/2" AND FILLERS FROM 2024T3.050 DIMENSION 5 1/8" X 2
- [SDR FDEA201007272713](https://openairdocs.org/sdr/FDEA201007272713.md): Stringer · corroded · Jul 27, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27L AT BS 1100. REMOVED CORROSION. EVALUATED AREA ORIGINAL.063 MATERIAL LOSS.015 MATERIAL REMAINING.048 FOUND AREA TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA APPROX DIM: 5". FABRICATED STRINGER FILLER FROM BAC 1498-145 7075T6 APPROX DI
- [SDR FDEA201007262704](https://openairdocs.org/sdr/FDEA201007262704.md): Stringer · damaged · Jul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FASTENER HOLE IS ELONGATED IN STR 25L AT BS 520. CUT OUT DAMAGED SECTION OF STRINGER DIM. 16" LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR PARTS USING BAC1498-139 7075 T6 DIM 16" 7075 T6.050" DIM. 10 1/4" X 5/8" (4 EACH), BAC1493-412 7075 T6 DIM
- [SDR FDEA201007262687](https://openairdocs.org/sdr/FDEA201007262687.md): Stringer · corroded · Jul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27L AT BS 720B. CUT OUT DAMAGED STRINGER SECTION DIMENSION 14" LONG AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-145 DIMENSION 14" LONG AND 2EA SPLICES FROM BAC 1498-131 DIMENSION 10" LONG EACH, TREATED AND PRIMED AND INSTALLED AT
- [SDR FDEA201007262688](https://openairdocs.org/sdr/FDEA201007262688.md): Skin · canning · Jul 26, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN STR 17R BETWEEN BS 1303 TO BS 1323 IS OIL CANNED. CUTOUT DAMAGED AREA ( DIM: 6" X 3") AND FABRICATED REPAIR DOUBLER FROM 2024T3.071 DIMENSION 15" X 10" IAW SRM 53-30-3, FIG 1 & 53-30-2, FIG 3. TREATED AND PRIMED AND INSTALLED REPAIR DOU
- [SDR FDEA201007222701](https://openairdocs.org/sdr/FDEA201007222701.md): Skin · gouged · Jul 22, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR INNER SURROUND SKIN GOUGED STA 460-48- STR 4L. REMOVED MAIN CARGO DOOR INNER SKIN FWD UPPER SECTION IAW SRM 51-30-2. FABRICATED NEW INNER SKIN IAW DWG 53FX2022, REV C AND 53FX1535 REV H, TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED NEW I
- [SDR 08FDEA01368](https://openairdocs.org/sdr/08FDEA01368.md): Seat Track · corroded · Apr 9, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPATRMENT, SEAT TRACK IC CORRODED FROM BS 870-848, LBL 25. REMOVED SEAT TRACK AT MAIN CARGO COMPARTMENT IAW SRM 51-30-2. LOCATED AND DRIILED NEW TRACK, DIM 16 INCH LONG IAW SRM 51-30-5 AND 53-10-2 FIG 7. TREATED AND PRIMED AFFECTED AREAS IAW CS
- [SDR 08FDEA01306](https://openairdocs.org/sdr/08FDEA01306.md): Floorbeam · corroded · Apr 4, 2008 · N466FE · Boeing 727200 · Fuselage Main, Floor Beam
  > MAIN CARGO COMP STA 760-848 LBL 24 T-CAP CORRODED REMOVED SEAT TRACK AND T-CAP IAW SRM 51-30-2. LOCATED AND DRLLED NEW T-CAP IAW SRM 53-10-2 FIG 7 AND 51-30-5. TREATED AND PRIMED NEW T-CAP IAW SRM 51-10-2. INSTALLED NEW T-CAP AND SEAT TRACK AT MAIN CARGO
- [SDR 08FDEA01294](https://openairdocs.org/sdr/08FDEA01294.md): Skin · dented · Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > DENT RT AFT LWR FUSELAGE BS 1243 S21R CUT OUT DAMAGED AREA 3" BY 3/4" IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.
- [SDR 08FDEA01293](https://openairdocs.org/sdr/08FDEA01293.md): Seat Track · corroded · Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK FORM STA 700-720 BL 0. REMOVED SEAT TRACK OUT LIMITS BTW STA 600-720 BL 0 IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK IAW SRM EA-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED IAW SRM 51
- [SDR 08FDEA01292](https://openairdocs.org/sdr/08FDEA01292.md): Seat Track · corroded · Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAI CARGO COMPARTMENT, SEAT TRACK CORRODED STA 570-580 RBL 45 REMOVED SEAT TRACK SECTION OUT OF LIMITS AT STA 530 TO 690 RBL 45 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED PARTS
- [SDR 08FDEA01291](https://openairdocs.org/sdr/08FDEA01291.md): Seat Track · corroded · Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED STA 950B BL 0. REMOVED SEAT TRACK-OUT OF LIMITS BETWEEN STA 890-950C BL 0 IAW SRM 51-30-2 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND 53-10-5 FIG 7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLE
- [SDR 08FDEA01290](https://openairdocs.org/sdr/08FDEA01290.md): Skin · delaminated · Apr 3, 2008 · N466FE · Boeing 727225 · Trailing Edge Flaps
  > LT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLER
- [SDR 08FDEA01283](https://openairdocs.org/sdr/08FDEA01283.md): Skin · dented · Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > DENT LT AFT FUSELAGE STA 1350 STR 17L, FOUND OUT OF LIMITS IAW SRM, EVALUATED DENT AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIM 1 1/2 BY 1 INCH AND FABRICATED REPAIRED DOUBLER IAW SRM 54-30-3 FIG7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED
- [SDR 08FDEA01271](https://openairdocs.org/sdr/08FDEA01271.md): Skin · cracked · Apr 2, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > AFT LOWER CARGO DOOR LOWER AFT FUSELAGE EDGE BENT AND CRACKED AT STA 980-990. REPAIRED BY TRIMMING THE AFFECTED PER EA 7-5330-116976.
- [SDR 08FDEA01203](https://openairdocs.org/sdr/08FDEA01203.md): Floorbeam · corroded · Mar 29, 2008 · N466FE · Boeing 727225 · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED AT BS 560, RBL 0-25. REMOVED CORROSION IAW SRM 51-10-6, AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 4. REMOVED SPLICE ANGLE AND DISPLACED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION FROM RBL 32 T
- [SDR 08FDEA01171](https://openairdocs.org/sdr/08FDEA01171.md): Vertical Beam · sheared · Mar 28, 2008 · N466FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > STA 1183 FWD SIDE VERTICAL BEAM AT APPROX LBL 12 HAS FASTENERS WITH NO EDGE DISTANCE. REPAIRED IAW EA 7-5310-116973.
- [SDR 08FDEA01152](https://openairdocs.org/sdr/08FDEA01152.md): Skin · dented · Mar 26, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > DENT RT AFT FUSELAGE STA 1050 STR 23R (DENT FOUND OUT OF LIMITS). CUT OUT DAMAGED AREA IAW SRM 53-30-1 FIG1. FABRICATED REPAIR DOUBLER TREATED AND PRIMED REPAIR PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR 08FDEA01112](https://openairdocs.org/sdr/08FDEA01112.md): Seat Track · corroded · Mar 23, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN COMPARTMENT, SEAT TRACK CORRODED AT BS 950C, 8 BL 0. REMOVED SEAT TRACK SECTION- OUT OF LIMITS BL 0 STA 950C TO STA 1010 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 FIG7. TREATED AND PRIMED IA
- [SDR 08FDEA01111](https://openairdocs.org/sdr/08FDEA01111.md): Skin · worn · Mar 23, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > LT FUSELAGE SKIN WORN AT BS 310 BTW S10L AND S11L, WORN BY FWD ENTRY DOOR MECHANISM LONG BOLT INSTALLED. REPAIRED FWD ENTRY DOOR MECHANISM IAW SRM 51-30-2 AND EA 7-5330-116972.
- [SDR 08FDEA01110](https://openairdocs.org/sdr/08FDEA01110.md): Beam · cracked · Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous Structure
  > RT WING I/B T/E "J " BEAM AT WING STATION 92 CRACKED, WING T/E SUPPORT BEAM FOR NR 7 SPOILER. TRIMMED OUT CRACKED AREA LENGTH 0.75" IAW SRM 51-10-1. TREATED AND PRIMED AREA "J" BEAM IAW SRM 51-10-2 DRAWING SR27-57-025.
- [SDR 08FDEA01109](https://openairdocs.org/sdr/08FDEA01109.md): Shim · migrated · Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous Structure
  > MIGRATING SHIMS AND LOOSE HARDWARE AT LWR SIDE OF NR 8 SPOILER ACTUATOR SUPPORT BEAM FITTING, WS 198. REPAIRED SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".
- [SDR 08FDEA01108](https://openairdocs.org/sdr/08FDEA01108.md): Support Beam · cracked · Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous Structure
  > MIGRATING SHIMS AND LOOSE HARDWARES AT LWR SIDE OF NR 7 SPOILER SUPPORT BEAM FITTING WS 198. REPAIRED NR 7 SPOILER ACTUATOR SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".
- [SDR 08FDEA01107](https://openairdocs.org/sdr/08FDEA01107.md): Floorbeam · corroded · Mar 22, 2008 · N466FE · Boeing 727225 · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L, B.S. 950D

Next page: https://openairdocs.org/deregistered/N466FE-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 = 'N466FE' AND deregistration_id = 'N466FE-2013-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N466FE-2013-03-08/reports

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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.