# Service difficulty reports: N465FE, cancelled Aug 10, 2015

A list on [N465FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N465FE-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 2 · 85 reports

- [SDR FDEA201203221062](https://openairdocs.org/sdr/FDEA201203221062.md): Slide · dislodged · Mar 22, 2012 · N465FE · Boeing 727225 · Escape Slide
  > EMERGENCY SLIDE CAME OUT OF DOOR WHEN OPENING. DID NOT DEPLOY. INSTALLED EMERGENCY ESCAPE SLIDE IAW MM 25-60-015-2-0.
- [SDR FDEA201008313206](https://openairdocs.org/sdr/FDEA201008313206.md): Light · loose · Aug 31, 2010 · N465FE · Boeing 727225 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT POPS OUT OF ITS HOUSING ON ROTATION AND LANDING. FOUND LIGHT NOT PROPERLY SET, RE-SET SAME, OPS CHECK NORMAL AND NOW IS SECURE. ACCOMPLISHED IAW MM 33-50-101-2-0.
- [SDR FDEA201008313205](https://openairdocs.org/sdr/FDEA201008313205.md): Light · damaged · Aug 31, 2010 · N465FE · Boeing 727225 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT DOES NOT TEST ON PRE-FLIGHT. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD.
- [SDR FDEA200910163595](https://openairdocs.org/sdr/FDEA200910163595.md): Rib · cracked · Oct 16, 2009 · N465FE · Boeing 727225 · Leading Edge Devices
  > NR 3 SLAT HAS 2 CRACKED RIBS, INBD AND OTBD OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIBS, FABRICATED NEW RIBS, HEAT TREATED RIBS TO T4 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLED IAW SRM 51-30-2 AND 51-20-1.
- [SDR FDEA200910143576](https://openairdocs.org/sdr/FDEA200910143576.md): Angle · cracked · Oct 14, 2009 · N465FE · Boeing 727225 · Leading Edge Devices
  > NR 1 SLAT LWR AFT CHORD ANGLE IS CRACKED BELOW ACTUATOR. REMOVED ACCESS PANEL IAW SRM 51-30-2, CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED NEW LOWER CHORD, AND 1 EACH SPLICER IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1 REV 101, TREATED AND PRIMED
- [SDR FDEA200910143588](https://openairdocs.org/sdr/FDEA200910143588.md): Structure · cracked · Oct 14, 2009 · N465FE · Boeing 727225 · Trailing Edge Flaps
  > R/WING INBD MIDFLAP T/E CHORD CRACKED AT NR 2 AFT FLAP HINGE CUTOUT. REMOVED LOWER CHORD SECTION IAW SRM 51-30-2 LOCATED AND DRILLED NEW LOWER CHORD, INSTALLED NEW CHORD IAW SRM 51-30-2 REV 101 INSTALLED LOWER MIDFLAP PANEL IAW SRM 51-30-2 REV 101.
- [SDR FDEA200910133624](https://openairdocs.org/sdr/FDEA200910133624.md): Shear Tie · corroded · Oct 13, 2009 · N465FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > AFT PIT CORROSION AT SHEAR TIE STA 950E STR 29R REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT SHEAR TIE, FABRICATED REPAIR ANGLE USING 7075-0.080 PO NR 9008557 DIMS 6" X 2", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLE
- [SDR FDEA200910133553](https://openairdocs.org/sdr/FDEA200910133553.md): Skin · gouged · Oct 13, 2009 · N465FE · Boeing 727225 · Trailing Edge Flaps
  > LT INBD MIDFLAP UPPER SURFACE IS GOUGED WBL 80. MIDFLAP REMOVED AND REPLACED DUE TO DAMAGE BEING OUT OF LIMITS AND BEYOND ECONOMICAL REPAIR.
- [SDR FDEA200910123625](https://openairdocs.org/sdr/FDEA200910123625.md): Frame · corroded · Oct 12, 2009 · N465FE · Boeing 727225 · Fuselage Main, Frame
  > E AND E COMPARTMENT BS 400 STR 19R CORROSION NEXT TO TOOLING HOLES. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1" DIAMETER, FABRICATED NEW FRAME REPAIR USING 7075-0.050 PO NR 29016223, DIMS 9 3/4" X 5 1/2", HEAT TREATED PART TO T6
- [SDR FDEA200910123546](https://openairdocs.org/sdr/FDEA200910123546.md): Skin · gouged · Oct 12, 2009 · N465FE · Boeing 727225 · Trailing Edge Flaps
  > RT OTBD FOREFLAP, GOUGED AND CHAFED AT OTBD L/E. GOUGE OUT OF LIMITS IAW SRM 51-30-2, FABRICATED REPAIR DOUBLER, IAW SRM 57-50-4, FIG 1 REV 101, TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REV 101.
- [SDR FDEA200910103545](https://openairdocs.org/sdr/FDEA200910103545.md): Lap Joint · damaged · Oct 10, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > STA 620, STR 27L, LAP SEAM LWR ROW, NO DISTANCE BETWEEN RIVETS. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED REPAIR AND FASTENERS IAW SRM 51-30-2, 53-30-3, 51-30-8 AND 51-10-2.
- [SDR FDEA200910093552](https://openairdocs.org/sdr/FDEA200910093552.md): Floor Support · corroded · Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > L-1 ENTRANCE WALK WAY BS 300-340, LBL 56- RBL 30, FLOOR SUPPORTS LWR SURFACES HAVE CORROSION AT N/P HOLES AS MARKED. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 2" X 1", FABRICATED 2 EACH REPAIR ANGLES USING 7075-0.063 PO 9008655 D
- [SDR FDEA200910093531](https://openairdocs.org/sdr/FDEA200910093531.md): Angle · cracked · Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1273 ON FWD SIDE RADIUS. REMOVED ANGLE SUPPORT IAW SRM 51-30-2, LOCATED AND DRILLED NEW ANGLE SUPPORT IAW SRM 51-30-5 REV. 101. INSTALLED NEW UPPER WEB SUPPORT ANGLE IAW SRM 51-30-2
- [SDR FDEA200910093533](https://openairdocs.org/sdr/FDEA200910093533.md): Vertical Beam · misinstalled · Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Main, Structure
  > FUSELAGE STA 1183 LWR CHORD LT INBD 17.8 VERT BEAM FASTENERS SPACING SHORT. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851.
- [SDR FDEA200910093532](https://openairdocs.org/sdr/FDEA200910093532.md): Frame · cracked · Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LWR TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1263 ON AFT SIDE RADIUS. REMOVED WEB DOUBLER, REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE USING 7075-0.090 PO 9008486 DIMS 18" X 5 7/8", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI F
- [SDR FDEA200910083518](https://openairdocs.org/sdr/FDEA200910083518.md): Skin · corroded · Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 1050, STR 27L. FOUND EXFOLIATED CORROSION OUT OF LIMITS ON SKIN, CUT OUT DAMAGED AREA, CUT OUT DAMAGED STRINGER SECTION, FABRICATED REPAIR DOUBLER AND FILLERS, FABRICATED STRINGER REPAIR AND SPLICES, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2,
- [SDR FDEA200910083519](https://openairdocs.org/sdr/FDEA200910083519.md): Stringer · damaged · Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA, STA 450, STR 3L NO EDGE DISTANCE BETWEEN RIVET AND HOLE. REMOVED FASTENERS AND CUT OUT DAMAGED AREA, FABRICATED ONE FILLER, ONE PLATE, TWO PLATES, TWO PLATES AND INSTALLED IAW SRM 51-30-2, 53-10-3 AND 51-10-2.
- [SDR FDEA200910083517](https://openairdocs.org/sdr/FDEA200910083517.md): Keelbeam · cracked · Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Keel
  > LT KEELBEAM CHORD IS CRACKED AT BS 870, LBL 4. CUT OUT DAMAGE AREA DIM 2" IAW FEDEX 727 EA 7-5310-135501, FAB REPAIR DOUBLER MAT USED 15-5 PH.071" PO # 290342001 DIM (85/8" X 4") IAW EA 7-5310-135501. ACCOMPLISHED HARDNESS TEST VERIFICATION OF FABRICATE
- [SDR FDEA200910083516](https://openairdocs.org/sdr/FDEA200910083516.md): Vertical Beam · damaged · Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Structure
  > AFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM WEB HAS SEVERAL DOUBLE DRILLED HOLES AT WL 190. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851, REFERENCE SDR 09-3493.
- [SDR FDEA200910073499](https://openairdocs.org/sdr/FDEA200910073499.md): Stringer · corroded · Oct 7, 2009 · N465FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT- CORROSION ON STRINGER 27R AT END SPLICE, BS 740. CUT OUT DAMAGE STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED NEW SECTION STRINGER AND 1EA SPLICE IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED STRINGE
- [SDR FDEA200910063491](https://openairdocs.org/sdr/FDEA200910063491.md): Stringer · damaged · Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO AREA, STA 580, STR 21L, DRILL START ON STRINGER. CUT OUT DAMAGED AREA DIM 17 5/8" LONG IAW SRM 51-10-3 FIG 1 REV 101, FABRICATED HAT SECTION, AND 2 EACH SPLICERS 2 EACH CHANNELS, 2 EACH ANGLES AND 2 EACH FILLERS IAW SRM 53-10-3 FIG 1 AND 53-1
- [SDR FDEA200910063493](https://openairdocs.org/sdr/FDEA200910063493.md): Angle · cracked · Oct 6, 2009 · N465FE · Boeing 727225 · Leading Edge Devices
  > NR 7 SLAT AFT LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW T-DUCT. REMOVED ACCESS PANEL IAW B 727 SRM 51-30-2. REMOVED LOWER CHORD ANGLE IAW SRM 51-30-2. FABRICATED A NEW LOWER CHORD AND 1 EA SPLICE IAW SRM 57-50-2 FIG 2, AND 51-40-4 FIG 1. TREATED AND PRIMED IA
- [SDR FDEA200910063495](https://openairdocs.org/sdr/FDEA200910063495.md): Skin · damaged · Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > DRILL START STA 261 STR 21L. CUT-OUT DAMAGED AREA AND FABRICATED REPAIR FILLER AND DOUBLER IAW B727 SRM 53-30-3 FIGURE 3A. TREATED AND PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS AT BS 261 STRINGER 21LT IAW SRM 53-30-3 FIGURE 3A.
- [SDR FDEA200910063490](https://openairdocs.org/sdr/FDEA200910063490.md): Web · cracked · Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > STA. 1323, STR 20, LEFT AFT AIRSTAIR EQUIPMENT AREA, CRACK ON WEB. TRIMMED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 5 REV 101 AND SRM 53-10-2 FIG 6 TREATED AND PRIMED IAW 51-10-2 REV 101 INSTALLED DOUBLER AT STA 1323 STR 2
- [SDR FDEA200910063492](https://openairdocs.org/sdr/FDEA200910063492.md): Skin · cracked · Oct 6, 2009 · N465FE · Boeing 727225 · Leading Edge Devices
  > NR 7 SLAT INBD HOOK AFT MOUNTING FASTENER IS LOOSE AND EDGE OF COUNTERSINK HAS CRACK INDICATION. HFEC INSPECTED AREA IAW NDTM 51-00-00 PART 6 FIG 23 VERIFIED CRACK ENDS AT EXISTING FASTENER HOLE. FABRICATED DOUBLER FOR NR 7 SLAT INBD AREA IAW SRM 57-50-3 FIG
- [SDR FDEA200910063494](https://openairdocs.org/sdr/FDEA200910063494.md): Vertical Beam · misinstalled · Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, Structure
  > AFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM INBD FLANGE FASTENERS HAVE IMPROPER SPACING IN 4 AREAS. REPAIRED AFT CARGO COMPARTMENT BS 1183 PRESSURE BULKHEAD IAW EA NR 7-53-10-126851.
- [SDR 07FDEA04774](https://openairdocs.org/sdr/07FDEA04774.md): Accessory Unit · failed · Nov 13, 2007 · N465FE · Boeing 727225 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WITH GEAR RETRACTED, WHEN WE WENT FROM FLAPS 5 TO FLAPS 2 GOT THE TAKEOFF WARNING HORN, WOULD ONLY EXTINGUISH BY REDUCING POWER. ALSO GOT THE HORN WHEN WE WENT FROM FLAPS 25 TO FLAPS 30 AT LANDING. R & R MLG ACCESSORY UNIT IAW MM 32-09-121-4
- [SDR 07FDEA04138](https://openairdocs.org/sdr/07FDEA04138.md): Wire · damaged · Sep 20, 2007 · N465FE · Boeing 727225 · Door System Wiring
  > AFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 30SEP07 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT, INOP. PLEASE WORK IN CONJUNCTION WITH TSI: 52-62 9704. REPAIRED WIRE AT SW S273 (UPLOC
- [SDR 07FDEA02223](https://openairdocs.org/sdr/07FDEA02223.md): Display · burned · Jun 20, 2007 · N465FE · Boeing 727200 · Central Warning
  > PDIS 465 26-12 0009505 20JUN07 PIT OPEN R LOGPAGES: 01339908 APPROX 1 00 HOURS INTO FLIGHT, ALL CREWMEMBERS SMELLED A BURING SMELL AND SAW LIGHT SMOKE, SOURCE UNKNOW. PREFORMED PHASE ONES RED TAB PROCEDURE. DIVERTED INTO KPIT ENT BY: 001395 RP
- [SDR 07FDEA02041](https://openairdocs.org/sdr/07FDEA02041.md): Seat Track · corroded · Jun 1, 2007 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK HAS CORR, FS 460-620, RBL-24". REMOVED CORRODED SEAT TRACK AT RBL 24, STA 480 TO 620 IAW B727 SRM 53-10-5. FAB NEW SECTION OF SEAT TRACK PO 1142187. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-
- [SDR 07FDEA01985](https://openairdocs.org/sdr/07FDEA01985.md): Stringer · corroded · May 26, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS- 720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N
- [SDR 07FDEA01984](https://openairdocs.org/sdr/07FDEA01984.md): Stringer · corroded · May 26, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS-720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N#6
- [SDR 07FDEA01980](https://openairdocs.org/sdr/07FDEA01980.md): Skin · misrepaired · May 25, 2007 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > EXTERNAL REPAIR ON FUSELAGE SKIN STA 1111-1127 AND STR 21R-23R DOES NOT COMPLY PER SRM. REMOVED OLD REPAIR IAW SRM 51-30-2. FABBED NEW DOUBLER IAW SRM 53-30-3 FIG 1 FROM MAT.2024T3 0.05, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAW SRM 53-3
- [SDR 07FDEA01979](https://openairdocs.org/sdr/07FDEA01979.md): Seat Track · corroded · May 25, 2007 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK HAS CORROSION FS 640 LBL 1". REMOVED CORROSION IAW 727 SRM 51--10-2 FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL IAW SR 53-10-1. FABBED NEW SEAT TRACK IAW SRM 51-30-2,TREATED AND PRIMED IAW SRM 51-10-1. REMOVED AND INSTALLED SEA
- [SDR 07FDEA01978](https://openairdocs.org/sdr/07FDEA01978.md): Stringer · corroded · May 25, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT FS 720D-720E STR-26L HAS CORROSION. CUT OUT DAMAGE IAW SRM 53-30-3 FIG 5. FABBED REPAIR DOUBLERS AND FILLER IAW SRM 53-30-3 FIG 5. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA01841](https://openairdocs.org/sdr/07FDEA01841.md): Web · corroded · May 17, 2007 · N465FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT CARGO STA 970 S-28R WEB HAS CORROSION. REMOVED CORROSION ON WEB AT STA 970 STR 28R CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-6, FABED NEW WEB ON MAE TR T7/679785. INSTALLED THE NEW WEB IAW SRM 51-30-2. INSTALLED STIFFENERS THAT WERE REMOVED PREVIOUSLY
- [SDR 07FDEA01840](https://openairdocs.org/sdr/07FDEA01840.md): Seat Track · corroded · May 17, 2007 · N465FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MAIN CABIN SEAT TRACK CORRODED UPPER SURFACE FROM FSTA 848 - 870, LBL 45 BLENDED SEAT TRACK AT 848 - FS870 LBL 45 FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-30-1 (FIG 1); ORDERED NEW SEAT TRACK PART NR BAC1520-841 BATCH NR 3370-1 AND LOCATED AND DRILLED
- [SDR 07FDEA01712](https://openairdocs.org/sdr/07FDEA01712.md): Bracket · cracked · May 7, 2007 · N465FE · Boeing 727225 · Nacelle/Pylon Miscellaneous Structure
  > NR 3 PYLON HOLE "P" BRACKET CRACKED FWD OUTBD SEEN INSIDE PYLON AS PER STEP4. 2 ON W/C 7-5410-7-3304. REMOVED AND REPLACED ANGLE( 69-16917-2) IAW SRM 51-30-2 AND 51-10-4. NDT CHECKED "P" HOLE FOR CRACK AND NO CRACK NOTED IAW NTM 51-00-11.
- [SDR 07FDEA01711](https://openairdocs.org/sdr/07FDEA01711.md): Spar Cap · cracked · May 7, 2007 · N465FE · Boeing 727225 · Wing Spar
  > RT WING UPPER SURFACE AT SPOILER PANEL NR 11 AREA SPAR CAP HAS CRACK AROUND 3RD HINGE FITTING. NDT NOTED NO CRACKED PER NTM 51-00-00 PT6 (AFTER STOP DRILL). STOP DRILLED 0.025" HOLE AT THE END OF CRACKED IAW SRM 57-30-4 FIG10 SHEET 1/3. TREATED AND PRIMED I
- [SDR 06FDEA04136](https://openairdocs.org/sdr/06FDEA04136.md): Steering Sys · malfunctioned · Nov 29, 2006 · N465FE · Boeing 727225 · Landing Gear Steering System
  > DURING TAKEOFF ROLL, A/C DRIFTED LEFT OF CENTERLINE WITH NO ABILITY TO CONTROL, TAKEOFF ABORTED. SUSPECTED ICY RUNWAY. DURING TAXI IN, NOTICED THAT THE RUDDER PEDALS WOULD NOT STEER A/C TO RIGHT, TILLER WAS REQ'D TO EFFECT RIGHT TURN. RIGHT RUDDER PEDAL DOE
- [SDR 05FDEA04388](https://openairdocs.org/sdr/05FDEA04388.md): Switch · malfunctioned · Dec 21, 2005 · N465FE · Boeing 727200 · Leading Edge Slat Control System
  > PASSING FL250 RECEIVED INTERMITTENT LE FLAPS AMBER INDICATOR ON FORWARD PANEL WITH INTERMITTENT NR1 SLAT INDICATOR ON S/O AUX PANEL. RAN RED TABS WITH NORMAL EXTENSION TO FLAPS 30. REPLACED NR 1 SLAT RETRACT SWITCH IAW 27-82-011-4, REPLACED NR1 SLAT ACTUA
- [SDR 05FDEA03246](https://openairdocs.org/sdr/05FDEA03246.md): Seat Track · corroded · Oct 5, 2005 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 600-620 AT LBL 45 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK REPAIR AT STA 590-690 ON LBL45 ALL IAW FX B727-200 SRM 53-10-5, 51-3-2 AND 51-10-2.
- [SDR 05FDEA03245](https://openairdocs.org/sdr/05FDEA03245.md): Seat Track · corroded · Oct 5, 2005 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 480-620 LBL 24 FLANGE HAS CORROSION. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 ON LBL 24 ALL IAW FX B727 SRM 53-10-5, 53-10-2, 51-30-2 AND 51-10-2.
- [SDR 05FDEA03244](https://openairdocs.org/sdr/05FDEA03244.md): Seat Track · corroded · Oct 5, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45 STA 690-740 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 680-740 AT LBL45 ALL IAW FX B727-200 SRM 53-10-5,53-10-1 FIG 3, 51-30-2 AND 51-10-2.
- [SDR 05FDEA03181](https://openairdocs.org/sdr/05FDEA03181.md): Floorbeam · corroded · Sep 30, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT STA. 344 FROM BL 12 L TO BL 12 R. REMOVED CORROSION FROM FLOOORBEAM UPPER CAP IAW FED-EX SRM 53-10- 1. REMOVED, FABRICATED AND INSTALLED SPLICES AND FLOORBEAM IAW SRDM SR27-53-007, B727 SRM 51-10-2,51-30-2.
- [SDR 05FDEA03178](https://openairdocs.org/sdr/05FDEA03178.md): Seat Track · corroded · Sep 30, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 24 HAS 2 SPLICES AND CORROSION STA 380 - STA 480. REMOVED CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS, ORIGINAL THICKNESS.085 MATERIAL REMOVED.029 RAMAINING.056, REMOVED SEAT TRACK. FABRICATED, DRILLED TO FIT, ALODINED, PRIMED AND INSTALLE
- [SDR 05FDEA03146](https://openairdocs.org/sdr/05FDEA03146.md): Floorbeam · corroded · Sep 27, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM FS 620 FROM LBL 24 - LBL 45 THREE HEAVY AREAS. REMOVED, FABRICATED, ALODINED, PRIMED, HEAT TREATED, CAD PLATED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM LBL24-45 ALL IAW FX DWG SR27-53-034E REPAIR NR 4 B727SRM 51-10-2,BAC5619H AND A
- [SDR 05FDEA03063](https://openairdocs.org/sdr/05FDEA03063.md): Seat Track · corroded · Sep 22, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK INBOARD FLANGE HAS CORROSION BS 700 TO BS 740 LBL 24.
- [SDR 05FDEA01759](https://openairdocs.org/sdr/05FDEA01759.md): Transmitter · malfunctioned · Jul 1, 2005 · N465FE · Boeing 727200 · Power Indicating System
  > ON TAKEOFF WITH STANDARD EPR SET NR3 N1,N2 AND FUEL FLOW WERE LOW. AC RELEASED FOR SERVICE IAW MEL/CDL: 77-01-01 01JUL05 14:55 ORF REMOVED PT2 SENSOR FROM ENG, BLEW AIR THROUGH LINE TO INSURE NO OBSTRUCTIONS PRESENT. RE-INSTALLED SAME. DISCONNECTED NR3
- [SDR 05FDEA00230](https://openairdocs.org/sdr/05FDEA00230.md): Warning Light · illuminated · Feb 2, 2005 · N465FE · Boeing 727200 · Landing Gear Position and Warning
  > DURING MANUAL EXTENSION WHEN NOSE GEAR WAS UNLOCKED, BOTH MAINS SHOWED UNSAFE. JACKED ACFT, PERFORMED NOSE GEAR MANUAL EXTENSION, SYSTEM TEST SEVERAL TIMES WITH FLAPS AT DIFFERENT SETTINGS AND PRESSURE ON AND OFF. SYSTEM FUNCTIONAL CHECKS GOOD IAW FED EX M/M

Next page: https://openairdocs.org/deregistered/N465FE-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 = 'N465FE' AND deregistration_id = 'N465FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N465FE-2015-08-10/reports

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