# Service difficulty reports: N469FE, cancelled Aug 10, 2015

A list on [N469FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N469FE-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 3 · 108 reports

- [SDR FDEA201208032828](https://openairdocs.org/sdr/FDEA201208032828.md): Light · failed · Aug 3, 2012 · N469FE · Boeing 727225 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE, TOP FWD ENTRY DOOR. R & R EMERGENCY LIGHT IAW AMM 33-50-101-2.
- [SDR FDEA201204121389](https://openairdocs.org/sdr/FDEA201204121389.md): Indicator · failed · Apr 12, 2012 · N469FE · Boeing 727225 · Hydraulic Indicating System
  > DURING CRUISE FLIGHT HYD SYS A QTY DECREASED TO 2.4 GALLONS. QRH PROCEDURES WERE FOLLOWED AND AFTER THE SYS A SPOILERS SWITCH WAS CLOSED LEAK APPEARED TO STOP. INSPECTED ACFT FOR EVIDENCE OF HYD LEAK IAW MM 29-00-000-6 PARA 1.B. NO LEAKS NOTED QTY AT BLOCK
- [SDR FDEA201204041248](https://openairdocs.org/sdr/FDEA201204041248.md): Battery · discharged · Apr 4, 2012 · N469FE · Boeing 727225 · Emergency Lighting
  > RT EMERGENCY ESCAPE SLIDE LIGHT AT L1 DOOR INOPERATIVE. BATTERY DISCHARGED. REPLACED BATTERY IAW MM 33-50-121-2. OPS TESTED GOOD.
- [SDR FDEA201202170628](https://openairdocs.org/sdr/FDEA201202170628.md): Battery Pack · inoperative · Feb 17, 2012 · N469FE · Boeing 727225 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER L1 DOOR IN INOPERATIVE. INSTALLED SERVICABLE BATTERIES INTO EMERGENCY EXIT LIGHT OPS CHECKED GOOD. OK TO CONTINUE.
- [SDR FDEA201201070044](https://openairdocs.org/sdr/FDEA201201070044.md): Accessory Unit · failed · Jan 7, 2012 · N469FE · Boeing 727225 · Landing Gear Position and Warning
  > AFTER TAKEOFF, GEAR WARNING HORN SOUNDED AND 3 GEAR RED LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION. QRH CALLED FOR A RECYCLE OF THE LANDING GEAR. RECYCLE ATTEMPTED WITH THE SAME RESULT, GEAR HORN AND 3 RED GEAR LIGHTS, DOOR LIGHT AND T
- [SDR FDEA201109133861](https://openairdocs.org/sdr/FDEA201109133861.md): Light · failed · Sep 13, 2011 · N469FE · Boeing 727225 · Emergency Lighting
  > DURING STANDBY POWER CHECK, EMEGENCY LIGHT OVER MAIN ENTRY DOOR INOPERATIVE. LIGHT UNIT WAS NOT INSTALLED FULLY. RESEATED ASSY, NO HELP. REPLACED LIGHT BULBS AND LIGHTS ILLUMINATED FOR A SPLIT SECOND AND DIED. R & R L1 DOOR EMERGENCY LIGHT ASSY IAW MM. OP
- [SDR FDEA201109133856](https://openairdocs.org/sdr/FDEA201109133856.md): Light · inoperative · Sep 13, 2011 · N469FE · Boeing 727225 · Emergency Lighting
  > DURING STANDBY POWER CHECK, EMEGENCY LIGHT OVER MAIN ENTRY DOOR INOPERATIVE. LIGHT UNIT WAS NOT INSTALLED FULLY. RESEATED ASSY, NO HELP. REPLACED LIGHT BULBS AND LIGHT ILLUMINATED FOR A SPLIT SECOND AND DIED. R & R L1 DOOR EMERGENCY LIGHT ASSY IAW MM. OPS
- [SDR FDEA201109093783](https://openairdocs.org/sdr/FDEA201109093783.md): Sliding Window · out of adjust · Sep 9, 2011 · N469FE · Boeing 727225 · Flight Compartment Windows
  > UNABLE TO CLOSE F/O WINDOW. ADJUSTED F/O SLIDING WINDOW IAW MM 56-12-011-05. OPS CKS. FINAL CLOSED.
- [SDR FDEA201109073747](https://openairdocs.org/sdr/FDEA201109073747.md): Coalescer Bag · odor · Sep 7, 2011 · N469FE · Boeing 727225 · Humidity Control System
  > FAINT ELECTRICAL ODOR AFTER DEPARTURE, ODOR GOT MUCH WORSE AFTER 10 MINUTES AND LEVEL OFF AT 320. VERY IRRITATING ELECTRICAL SMELL ALSO ALMOST A VERY STRONG ONION - LIKE SMELL GOT WORSE ON INITIAL DESCENT. PUT O2 MASKS ON AND BY THE TIME WE LANDED AND REMOVE
- [SDR FDEA201107262980](https://openairdocs.org/sdr/FDEA201107262980.md): Battery Pack · inoperative · Jul 26, 2011 · N469FE · Boeing 727225 · Emergency Lighting
  > MAIN DECK & MAIN ENTRY EMERGENCY LIGHTING DID NOT TEST PROPERLY. DURING S/O STBY CHECK LIGHTS CAME ON FOR APPROX 3 SECONDS AND DIMMED & WENT OUT. (B.P.B) REPLACED EMERGENCY LIGHT BATTERIES FOR CABIN AND L1 EXITS IAW SMP FOR 33-50-101-2-0. SDR ENTERED IN E
- [SDR FDEA201107212981](https://openairdocs.org/sdr/FDEA201107212981.md): Light · no test · Jul 21, 2011 · N469FE · Boeing 727225 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT DOES NOT TEST. (CLOSED)
- [SDR FDEA201107192982](https://openairdocs.org/sdr/FDEA201107192982.md): Battery Pack · inoperative · Jul 19, 2011 · N469FE · Boeing 727225 · Emergency Lighting
  > MAIN DECK & MAIN ENTRY EMERGENCY LIGHTING DID NOT TESET PROPERLY DURING S/O STBY CHECK. LIGHTS CAME ON FOR APPROX 3 SECONDS AND DIMMED & WENT OUT. (B.P.B) REPLACED EMERGENCY LIGHT BATTERIES FOR CABIN AND L1 EXITS.
- [SDR FDEA201106252420](https://openairdocs.org/sdr/FDEA201106252420.md): Skin · damaged · Jun 25, 2011 · N469FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > L1 DOOR UPPER HINGE CUT OUT DOUBLER HAS THE MAX OVERSIZED FASTENER HOLES. REMOVED DOUBLER AT L-1 DOOR UPPER HINGE, FABRICATED NEW DOUBLER AND FILLER REPAIR, AND INSTALLED DOUBLER AND FILLER REPAIR IAW EA 7-5330-136770 AND EO 7-5330-7-2345 PT2 SECTION 4.A.
- [SDR FDEA201106242407](https://openairdocs.org/sdr/FDEA201106242407.md): Frame · corroded · Jun 24, 2011 · N469FE · Boeing 727225 · Fuselage Main, Frame
  > CORROSION ON UPPER FLANGE OF FRAME AT BS 950E BETWEEN STRINGER 28L AND 27L. CUT OUT DAMAGED SECTION OF UPPER FRAME FLANGE IAW SRM 51-40-3 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 REV 103
- [SDR FDEA201106242412](https://openairdocs.org/sdr/FDEA201106242412.md): Skin · gouged · Jun 24, 2011 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > INNER SKIN IS GOUGED IN NUMEROUS PLACES FROM BS 480 TO 620 BETWEEN STR 2L AND 3L. CUTOUT DAMAGED AREA AT MCD INNER SKIN BS 480 AND BS 620 BETWEEN STR 2L AND 3L, FABRICATED REPAIR FILLERS AND REPAIR DOUBLERS, AND INSTALLED REPAIR PARTS IAW EA 7-5310-152402.
- [SDR FDEA201106232404](https://openairdocs.org/sdr/FDEA201106232404.md): Skin · damaged · Jun 23, 2011 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR CUT-OUT, SKIN LAP JOINT - THRU DAMAGE AT STA 440, STR 14L. CUTOUT DAMAGED AREA AT FUSELAGE SKIN MCD CUTOUT LAP JOINT, FABRICATED DOUBLER, STRUCTURAL FILLER, TAPER FILLER, AND INTERNAL FILLER. INSTALLED REPAIR PARTS IAW EA 7-5330-126868.
- [SDR FDEA201106212392](https://openairdocs.org/sdr/FDEA201106212392.md): Frame · damaged · Jun 21, 2011 · N469FE · Boeing 727225 · Fuselage Main, Frame
  > CABIN BS 783, LT FRAME 6.2500" ABOVE CUSP WEB HAS HOLE BELOW FASTENER HOLE. REMOVED DAMAGED AREA AT CABIN. FABRICATED FREEZE PLUG, INSTALLED FREEZE PLUG AND FASTENER IAW EA 7-5310-136773 AND SRM 51-10-7.
- [SDR FDEA201106202343](https://openairdocs.org/sdr/FDEA201106202343.md): Skin · cracked · Jun 20, 2011 · N469FE · Boeing 727225 · Elevator, Plate/Skin
  > LT ELEVATOR TIP LOWER SKIN IS CRACKED AROUND RIVET. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-20-3 FIG 2.
- [SDR FDEA201106202345](https://openairdocs.org/sdr/FDEA201106202345.md): Torque Box · misrepaired · Jun 20, 2011 · N469FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS RT LOWER TORQUE BOX, BS 1273 MISREPAIRED. REMOVED ANGLE AT AFT AIRSTAIRS RT LOWER TORQUE BOX IAW SRM 51-30-2. FABRICATED AND INSTALLED ANGLE IAW DWG 65-17518 AND SRM 51-30-2.
- [SDR FDEA201106202344](https://openairdocs.org/sdr/FDEA201106202344.md): Support Angle · cracked · Jun 20, 2011 · N469FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS RT LOWER TORQUE BOX BS 1263 FWD SIDE OF ANGLE IS CRACKED IN 2 PLACES. REMOVED ANGLE AT AFT AIRSTAIRS RT LOWER TORQUE BOX BS 1263 FWD SIDE IAW SRM 51-30-2. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED ANGLE IAW DWG 65-17517.
- [SDR FDEA201106162281](https://openairdocs.org/sdr/FDEA201106162281.md): Frame · corroded · Jun 16, 2011 · N469FE · Boeing 727225 · Fuselage Main, Frame
  > CORROSION ON UPPER FLANGE OF FRAME AT BS 970, BETWEEN STRINGER 28L AND 27L. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 REV 103
- [SDR FDEA201106152280](https://openairdocs.org/sdr/FDEA201106152280.md): Reinforcement · damaged · Jun 15, 2011 · N469FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > UPPER REINFORCEMENT DAMAGED AT BS 950E BETWEEN 28L AND 27L. CUT OUT DAMAGED REINFORCEMENT SECTION IAW SRM 51-40-4 FIG 1. FABRICATED NEW REINFORCEMENT SECTION AND 2 EACH ANGLE DOUBLERS AND RADIUS FILLER IAW SRM 51-40-4 FIG 1. INSTALLED SECTION, 2 EACH DOUB
- [SDR FDEA201106112244](https://openairdocs.org/sdr/FDEA201106112244.md): Skin · cracked · Jun 11, 2011 · N469FE · Boeing 727225 · Galley Doors
  > GALLEY DOOR EXTERIOR SKIN CRACKED SERVERAL PLACES AROUND ROW OF RIVETS BELOW LOWER HINGE ARM. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLER, AND INSTALLED REPAIR PARTS IAW SRM 52-00-3 FIG 4 AT GALLEY DOOR EXTERIOR SKIN BELOW LOWER HINGE AR
- [SDR FDEA201106102187](https://openairdocs.org/sdr/FDEA201106102187.md): Frame · damaged · Jun 10, 2011 · N469FE · Boeing 727225 · Fuselage Main, Frame
  > AFT PIT - ELONGATED FASTENER HOLE IN FRAME AT BS 1070 RBL 30 CUT OUT DAMAGED AREA OF UPPER FLANGE OF FRAME IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER, FILLER AND SHIM IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR DOUBLER, FILLER AND SHIM IAW SRM 51-30-2 AN
- [SDR FDEA201106102186](https://openairdocs.org/sdr/FDEA201106102186.md): Shear Tie · corroded · Jun 10, 2011 · N469FE · Boeing 727225 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 450 BETWEEN STRINGER 28R AND 28L. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15 REV 103.
- [SDR FDEA201106092293](https://openairdocs.org/sdr/FDEA201106092293.md): Seat Track · corroded · Jun 9, 2011 · N469FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AT BS 760-850 LBL 45.5. REMOVED SEAT TRACK SECTION AT BS 760-850 LBL 45.5 IAW SRM 51-30-2. LOCATED NEW SECTION IAW DWG 65-19601 AND SRM 51-30-5. INSTALLED SECTION IAW SRM 51-30-2.
- [SDR FDEA201106092292](https://openairdocs.org/sdr/FDEA201106092292.md): Seat Track · corroded · Jun 9, 2011 · N469FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AT BS 740-850, RBL 45.5. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. LOCATED SECTION IAW DWG 65-19601 AND SRM 51-30-2. INSTALLED SECTION IAW SRM 51-30-2.
- [SDR FDEA201106082184](https://openairdocs.org/sdr/FDEA201106082184.md): Spar · cracked · Jun 8, 2011 · N469FE · Boeing 727225 · Wing Spar
  > LT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL118. REMOVED WEB AND DOUBLER IAW SRM 51-30-2 REV 103. CUT OUT CRACKED LOWER SPAR CHORD IAW DRAWING SR 27-57-038 REV C. FABRICATED NEW WEB, DOULER, SPAR CHORD SECTION, RADIUS FILLER, 2EA RADIUS BLOCKS AND
- [SDR FDEA201106072183](https://openairdocs.org/sdr/FDEA201106072183.md): Stringer · corroded · Jun 7, 2011 · N469FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > E&E COMPARTMENT- CORROSION ON STRINGER 28R AT BS 450. REMOVED CORRODED SECTION OF STRINGER IAW SRM 51-30-2. FABRICATED NEW SECTION OF STRINGER IAW SRM 51-30-5 AND 51-20-1 FIG 2. INSTALLED STRINGER IAW SRM 51-30-2 REV 103
- [SDR FDEA201106032238](https://openairdocs.org/sdr/FDEA201106032238.md): Support · damaged · Jun 3, 2011 · N469FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > BS 1183, PRESSURE BULKHEAD VERT BEAM HAS FASTENER WITH SHORT SPACE AT LBL 17.8. TRIMMED DAMAGED AREA OFF THE AFT FLANGE TEE VERTICAL BEAM AT STA 1183 LBL 17.8 PRESSURE BULKHEAD, FABRICATED TEE VERTICAL BEAM REPAIR DOUBLER, FILLER, AND INSTALLED REPAIR TEE
- [SDR FDEA201104271640](https://openairdocs.org/sdr/FDEA201104271640.md): Line · leaking · Apr 27, 2011 · N469FE · Boeing 727225 · Hydraulic System, Main
  > LOSS OF A SYS PRESSURE AND ALL A SYS HYD FLUID AFTER SUSPECTED LIGHTNING STRIKE. CREW COMPLIED WITH ALL QRH PROCEDURES TO SAFELY RECOVER ACFT. HYD SYS A FLUID SHUTOFF SWITCHES WERE OFF FOR APPROX 50 MINUTES WITH ENGINES 1 AND 2 OPERATING. CREW COMPLETED M
- [SDR FDEA201102070486](https://openairdocs.org/sdr/FDEA201102070486.md): Altimeter · failed · Feb 7, 2011 · N469FE · Boeing 727225 · Altimeter, Barometric/Encoder
  > CLIMBING THROUGH 20,000 MSL STANDBY ALTIMETER INDICATED AN ALTITUDE THAT WAS 10,000 HIGHER THAN THE ACTUAL ALTITUDE AS INDICATED ON THE CAPTAIN'S AND F/O'S ALTIMETERS. REMAINED IN ERROR THROUGHOUT THE FLIGHT. UPON ARRIVAL FOUND STANDBY ALTIMETER INDICATING
- [SDR FDEA201012244751](https://openairdocs.org/sdr/FDEA201012244751.md): Switch · out of adjust · Dec 24, 2010 · N469FE · Boeing 727225 · Door Warning System
  > AFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.
- [SDR FDEA201012244750](https://openairdocs.org/sdr/FDEA201012244750.md): Switch · out of adjust · Dec 24, 2010 · N469FE · Boeing 727225 · Door Warning System
  > AT FL 360" AFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.
- [SDR FDEA201009023244](https://openairdocs.org/sdr/FDEA201009023244.md): Relay · burned · Sep 2, 2010 · N469FE · Boeing 727225 · Light System Wiring
  > DURING COCKPIT PREFLIGHT, NOTICED HEAVY WHITE SMOKE COMING FROM OVERHEAD CONTROL PANEL. ADVISED 2ND OFFICER TO REMOVE ELECTRICAL POWER FROM ACFT. ADVISED CREW TO EVACUATE. INSP O/H PANEL AREA & FOUND NO SIGNS OF BURNED WIRES, SWITCHES, CONNECTOR'S OR RELAYS
- [SDR FDEA200812235263](https://openairdocs.org/sdr/FDEA200812235263.md): Indicator · failed · Dec 23, 2008 · N469FE · Boeing 727225 · Fuel Indicating System
  > NUMBER 2 FUEL GAUGE INDICATED ZERO DURING CRUISE THEN PASSING THROUGH APPROX 12000 FT GAUGE STARTED TO COME UP TO READ FUEL QUANTITY. SUMPED NR 3 TANK. NO WATER FOUND. NO FAULT CODES ON INDICATOR. CLEANED CANNON PLUG ON NR 3 VTO ON FWD SPAR. R&RD NR 3 FUEL
- [SDR FDEA200812125134](https://openairdocs.org/sdr/FDEA200812125134.md): Support Bracket · cracked · Dec 12, 2008 · N469FE · Boeing 727225 · Wing Miscellaneous Structure
  > LT WING L/E SLAT ACTUATOR SUPPORT BRACKET CRACKED INBD SIDE AT NR 1 SLAT. REMOVED AND REPLACED NR 1 SLAT STA 390.9 RIB, WEB, AND DOUBLER IAW EA 7-5750-126863.
- [SDR FDEA200812115121](https://openairdocs.org/sdr/FDEA200812115121.md): Bracket · cracked · Dec 11, 2008 · N469FE · Boeing 727225 · Wing, Attach Fittings
  > RT WING NR 7 SLAT ACTUATOR MOUNTING BRACKETS BOTH INBD AND OTBD ON WING SIDE ARE CRACKED AT WS 635. REMOVED AND REPLACED INBD AND OTBD NR 7 SLAT ACTUATOR MOUNTING BRACKETS AND STEEL DOUBLERS IAW FEDEX EA 7-5750-126869, WINGS, RT NR 7 SLAT STA 281.4 AND 288.6
- [SDR FDEA200812095117](https://openairdocs.org/sdr/FDEA200812095117.md): Support · cracked · Dec 9, 2008 · N469FE · Boeing 727225 · Wing Miscellaneous Structure
  > LT WING NR 1 SLAT ACTUATOR RIB SUPPORT INBD SIDE IS CRACKED REPAIRED BY ACCOMPLISHING EA 7-5750-126863 WINGS - LT NR 1 SLAT STA 390.9 ACTUATOR SUPPORT RIB. REPAIR OF DOUBLER CRACKS PER SB 727-57-0130.
- [SDR FDEA200812095116](https://openairdocs.org/sdr/FDEA200812095116.md): Skin · damaged · Dec 9, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > INNER AFT EDGE OF MCD CUTOUT HAS NUMEROUS AREAS DAMAGED BY GILL LINER FASTENERS. REPAIRED BY ACCOMPLISHING EA 7-5310-126861 "FUSELAGE - AD 98-11-03 R1 - SSI 6.19A - P-F MOD MCD CUTOUT LOWER CORNER INNER SKIN, REPAIR OF GOUGE MARKS AT BS 620 S16L - EO 7-5100
- [SDR FDEA200812085109](https://openairdocs.org/sdr/FDEA200812085109.md): Skin · corroded · Dec 8, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPT STR 26R IS CORRODED WITH EXFOLIATION BETWEEN STA 720E AND 720F. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330-126860 FUSELAGE AD 98-03-01 SECTION 43 SKIN REPAIR OF SKIN CORROSION AT STA 720E-720F AND S26R-S27R EO 7-5100-7-4304.
- [SDR FDEA200812085108](https://openairdocs.org/sdr/FDEA200812085108.md): Skin · misrepaired · Dec 8, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING STA 460 STR 10L. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330-126862 AD 98-11-03 R1 MAIN CARGO DOOR TRIPLER, DOUBLER AND FUSELAGE SKIN THRU DAMAGE AT STA 460 S10L EO 7-5100-7-4304.
- [SDR FDEA200812085107](https://openairdocs.org/sdr/FDEA200812085107.md): Skin · damaged · Dec 8, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FASTENERS WITH IMPROPER SPACING STA 440 ABOVE AND BELOW STR 14L. REPAIRED AREA IAW EA 7-5330-126868 FUSELAGE SKIN AD 98-11-03 MAIN CARGO DOOR CUTOUT FUSELAGE SKIN LAP JOINT THRU DAMAGE AT STA 440 S14L.
- [SDR FDEA200812085105](https://openairdocs.org/sdr/FDEA200812085105.md): Beam · corroded · Dec 8, 2008 · N469FE · Boeing 727225 · Fuselage Main, Structure
  > E AND E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION RBL 12 BS 344. REMOVED AND REPLACED LWR CHORD WALKWAY BEAM AT RBL12 BS 294-360 WITH NEW CHORD P/N 65-19861-8 PO NR 827074 IAW SRM 51-30-5 AND SRM 51-30-2.
- [SDR FDEA200812085104](https://openairdocs.org/sdr/FDEA200812085104.md): Frame · corroded · Dec 8, 2008 · N469FE · Boeing 727225 · Fuselage Main, Frame
  > NOSE WHEEL WELL "T" ANGLE CORRODED STA 280 STR 26R. FABRICATED NEW "T" ANGLE FROM 60-10936 7075-0 EXTRUSION PO NR 8270223 DIMS 19 INCH BY 3 INCH, HEAT TREATED EXTRUSION TO T-6 CONDITION INSTALLED NEW "T" ANGLE AT BS 280 STR 26R IAW MM 51-30-5 AND BOEING DWG 6
- [SDR FDEA200811254976](https://openairdocs.org/sdr/FDEA200811254976.md): Beam · corroded · Nov 25, 2008 · N469FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > E/E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION LBL 12 BS 32. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED LT LWR CHORD AND INSTALLED NEW LWR CHORD PART NUMBER 5715216 PO NR 827075 AT E/E COMPT STA 328 LBL12 IAW SRM 51-30-02.
- [SDR 08FDEA04956](https://openairdocs.org/sdr/08FDEA04956.md): Floorbeam · corroded · Nov 21, 2008 · N469FE · Boeing 727225 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BETWEEN BL0 AND RBL25 STA 1110. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SECTION DIMS 2 3/4 INCH BY 2 1/2 INCH. FABRICATED REPAIR ANGLES USING BAC1490-2785 PO NR 9007702 DIMS 11 3/4 INCH BY 2 1/2 INCH AND BAC1490-2831 PO NR 9006
- [SDR 08FDEA04955](https://openairdocs.org/sdr/08FDEA04955.md): Seat Track · corroded · Nov 21, 2008 · N469FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK STA 1090 TO 1130 ANS BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SECTION OF SEAT TRACK FROM BS 1010 TO 1130 AT BL0. FABRICATED NEW SECTION OF SEAT AND INSTALLED SECTION IAW SRM 51-10-2 AND 53-10-5.
- [SDR 08FDEA04943](https://openairdocs.org/sdr/08FDEA04943.md): Skin · corroded · Nov 20, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPT CORROSION ON SKIN AT BS 680 STR 26L TO 27L. FOUND CORROSION OUT OF LIMITS CUT OUT DAMAGED AREA DIMS 2 5/8 INCH BY 2 INCH. FABRICATED DOUBLER USING 2024-T3.063 PO NR 9008017 DIMS 8 1/2 INCH BY 2 INCH INSTALLED REPAIR PARTS IAW SRM 51-10-2 AND
- [SDR 08FDEA04933](https://openairdocs.org/sdr/08FDEA04933.md): Seat Track · chafed · Nov 19, 2008 · N469FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK STA 1130 TO 1180 BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED SEAT TRACK IAW DWG 53FX976.

Next page: https://openairdocs.org/deregistered/N469FE-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 = 'N469FE' AND deregistration_id = 'N469FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N469FE-2015-08-10/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.