# Service difficulty reports: N423FE, cancelled Apr 23, 2020

A list on [N423FE, cancelled Apr 23, 2020](https://openairdocs.org/deregistered/N423FE-2020-04-23.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 · 145 reports

- [SDR FDEA201410042967](https://openairdocs.org/sdr/FDEA201410042967.md): Warning Light · false activation · Oct 4, 2014 · N423FE · Airbus A310203 · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH LANDING GEAR RETRACTION, NOSE GEAR DOOR INDICATED UNSAFE, AMBER ON BOTH INDICATORS. FELT FLUTTER INDICATING DOOR WAS IN FACT STILL OPEN. AIR TURN BACK. WORK INSPECTING NOSE GEAR DOOR OPERATION & GENERAL NOSE GEAR AREA. NO OBVIOUS FAULTS
- [SDR FDEA201309212274](https://openairdocs.org/sdr/FDEA201309212274.md): Jackscrew · worn · Sep 21, 2013 · N423FE · Airbus A310203 · Leading Edge Slat Control System
  > ON APPLICATION OF SLATS 1 & 2, FAULT LIGHT CAME ON. SLATS LESS THAN 15- CYCLED HANDLE & NO CHANGE. RAN CHECKLIST & MADE NO SLAT LANDING. AFTER LANDING TRIED SLATS AGAIN AND THEY CAME DOWN. PERFORMED BITE TEST ON NR 1 & 2 SFCC IAW FIM 27-80-01/101. ALL IN
- [SDR FDEA201306181339](https://openairdocs.org/sdr/FDEA201306181339.md): Seal · leaking · Jun 18, 2013 · N423FE · Airbus A310203 · Pneumatic Distribution System
  > AFTER TAKE OFF, BLEED LEAK RT SIDE. REF QRH- LIGHT OUT IN FLIGHT. ON APPROACH LOWER ACCESS DOOR LIGHT CAME ON. FOUND LEAK TO BE COMING FROM THE UPPER RT CORNER OF PACK BAY BLEED SUPPLY LINE. REMOVED RT ENG BLEED DUCT SECTION IN FWD A/C BAY IAW MM 36-11-0
- [SDR FDEA201306051198](https://openairdocs.org/sdr/FDEA201306051198.md): Skin · corroded · Jun 5, 2013 · N423FE · Airbus A310203 · Elevator, Plate/Skin
  > RT ELEVATOR NR 2 T/E UPPER SURFACE CORRODED. REPAIRED THE DAMAGE IAW SRM 55-21-11/201 (C-1) FIG 209.
- [SDR FDEA201305150992](https://openairdocs.org/sdr/FDEA201305150992.md): Crossbeam · corroded · May 15, 2013 · N423FE · Airbus A310203 · Fuselage Main, Structure
  > FWD CARGO FR 38.1 -Y140 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW SRM 53-10-15, FIG 207.
- [SDR FDEA201107082612](https://openairdocs.org/sdr/FDEA201107082612.md): Transfer Sys · leaking · Jul 8, 2011 · N423FE · Airbus A310203 · Hydraulic System, Main
  > INFLIGHT YELLOW SYS RESERVOIR DECREASED TO RED DOT. FLUCTUATED SOME BUT NEVER WENT OUT OF YELLOW BAND. R & R GREEN/YELLOW POWER TRANSFER UNIT AS REQUIRED IAW MM 29-23-11-04.
- [SDR FDEA201105061768](https://openairdocs.org/sdr/FDEA201105061768.md): Gcu · failed · May 6, 2011 · N423FE · Airbus A310203 · Alternator-Generator Drive
  > ON TAKEOFF ROLL AT APPROX 50 KNOTS, GEN NR2 FAILED. ABORTED TAKEOFF. INTEROGATED GPCU, SHOWS RT GENERATOR, UNDER FREQ TRIP, IDG /PMG / WIRING, GCU FAILED CODE 9E. REMOVED AND REPLACED ENG.2 GCU(2XU) AND ENG NR 1 GCU IAW MM 24-22-12-04. RAN ENG PER JRH CHP.
- [SDR FDEA201104201538](https://openairdocs.org/sdr/FDEA201104201538.md): Transceiver · inoperative · Apr 20, 2011 · N423FE · Airbus A310203 · HF Communications System
  > STATIC ON RADIOS AT 380 DOWN TO 120 WAS SO BAD AN EMERGENCY WAS DECLARED DUE TO NO RADIO CONDITION. INSTALLED NEW NR1 VHF RECEIVER AND CHECKED GOOD IAW MM 23-12-33-04-0.
- [SDR FDEA201103082037](https://openairdocs.org/sdr/FDEA201103082037.md): Battery · failed · Mar 8, 2011 · N423FE · Airbus A310203 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST USING PUSH-BUTTON OR OVERHEAD PANEL LIGHT SWITCH. R & R EMERGENCY LIGHT BATTERY LOCATED ADJACENT LT PASSENGER ENTRY DOOR IAW MM 33-51-14-04-0. EMERGENCY LIGHT TEST GOOD IAW MM 33-55-0 0-05. R & R EMERGENCY LIGHT BATTERY LOC
- [SDR FDEA201102010445](https://openairdocs.org/sdr/FDEA201102010445.md): Frame · corroded · Feb 1, 2011 · N423FE · Airbus A310203 · Fuselage Main, Frame
  > REAR FUSELAGE FRAME 87- 89, STR 16L, HORIZ STAB CUTOUT. INNER FWD STRAP HAS EXFOLIATION CORROSION APPROX 4 IN. R & R THS CUTOUT FWD UPPER FITTING IAW DWG A53985135 AND SRM 51-40-21.
- [SDR FDEA201101310424](https://openairdocs.org/sdr/FDEA201101310424.md): Skin · damaged · Jan 31, 2011 · N423FE · Airbus A310203 · Rudder, Plate/Skin
  > .5" X.5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITTING IAW SRM 55-41-12 PARA 30 WET LAYUP REPAIR. NO CORE DAMAGE EXIST AT 22" AFT OF NR4 ATTACH FITTI
- [SDR FDEA201101300418](https://openairdocs.org/sdr/FDEA201101300418.md): Rib · corroded · Jan 30, 2011 · N423FE · Airbus A310203 · Emergency Flotation Section
  > LT WING RIB 5 FWD LUG HAS CORROSION. REPAIRED IAW EA 6-5710-145518 WING-AD 2008-17-02 - WING GEAR RIB 5 FWD LUG BORE REWORK (LT SIDE), SB A310-57-2090, EO 6-5710-7-5010.
- [SDR FDEA201101300417](https://openairdocs.org/sdr/FDEA201101300417.md): Rib · corroded · Jan 30, 2011 · N423FE · Airbus A310203 · Emergency Flotation Section
  > RT WING, RIB 5, FWD LUG HAS CORROSION REPAIRED IAW EA 6-5710-145517, WING-AD2008-17-02, WING GEAR, RIB5 FWD LUG BORE REWORK (RT SIDE), SB A310-57-2090, EO 6-5710-7-5010.
- [SDR FDEA201101280401](https://openairdocs.org/sdr/FDEA201101280401.md): Profile · cracked · Jan 28, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > BULK CARGO LONGITUDINAL PROFILE CRACKED 1" PN A53974259202, FR64 - 65 24" LT OF CTR OF ACFT. R & R LONGITUDINAL PROFILE FR 64 TO FR65 Y805 IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101270386](https://openairdocs.org/sdr/FDEA201101270386.md): Seat Track · corroded · Jan 27, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK 1 HAS CORROSION FR 71 TO FR 75 (ABOUT 70 SQUARE INCH). REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, PAGE 101-103. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK NR1 BETWEEN FR71 & FR 75, FABRICATED SEAT
- [SDR FDEA201101270385](https://openairdocs.org/sdr/FDEA201101270385.md): Skin · dented · Jan 27, 2011 · N423FE · Airbus A310203 · Trailing Edge Flaps
  > UPON REMOVAL OF RUBSTRIP ON NR N00391 RT WING OTBD FLAP UPPER MAIN SKIN BETWEEN RIBS 4 AND 5 ALSO BETWEEN THE MAIN SPAR CHORD AND REAR SPAR CORD HAS 8 DENTS WHICH 2 EA ARE VISABLE UNDER THE RUBSTIPS. DAMAGE IS IN A 10 IN X 12 IN AREA. CUTOUT DAMAGE AREA AN
- [SDR FDEA201101210330](https://openairdocs.org/sdr/FDEA201101210330.md): Channel · corroded · Jan 21, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FRAME LOCATION 87, BETWEEN STR 15 AND 16 FOUND CORROSION ON LT SIDE AFT UPPER "U" CHANNEL (CROSS STRUT). 1 AREA OF CORROSION ON UPPER FLANGE APPROX 1 SQ IN. R & R CROSS STRUT AT FR87 BETWEEN STR15 AND 16 IAW SRM 51-40-21.
- [SDR FDEA201101200313](https://openairdocs.org/sdr/FDEA201101200313.md): Floor Support · damaged · Jan 20, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR SUPPORT LONGITUDINAL PROFILE BROKEN BETWEEN FRAMES 65 AND 66 LT STR 52 LT. R & R PROFILE SECTION FR65 TO FR66 LT ABOVE STR52L IAW SRM 51-72-10.
- [SDR FDEA201101200312](https://openairdocs.org/sdr/FDEA201101200312.md): Floorbeam · cracked · Jan 20, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CRACKED IN RADIUS FR36 BETWEEN L2 AND L3 SEAT TRACK. REPAIRED CROSSBEAM AT FR36 BETWEEN SEAT TRACKS 2L AND 3L IAW SRM 53-10-15.
- [SDR FDEA201101200303](https://openairdocs.org/sdr/FDEA201101200303.md): Crossbeam · corroded · Jan 20, 2011 · N423FE · Airbus A310203 · Fuselage Main, Structure
  > REAR FUSELAGE FR 85, APPROX 15 INCHES INBD OF STR16 RT, HORIZONTAL CROSSBEAM HAS EXFOLIATION CORROSION ON LOWER FLANGE REMOVED CORROSION FROM CROSSBEAM AT FR 85 INBD OF STR 16R AND CHECKED LIMITS IAW SRM 53-19-47 AND SRM 53-10-00, FIG 105. REMOVED CROSSBEAM
- [SDR FDEA201101190290](https://openairdocs.org/sdr/FDEA201101190290.md): Seat Track · corroded · Jan 19, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK 1-R HAS CORROSION, FR78 - FR79, 20 SQUARE INCHES. R & R SEAT TRACK BETWEEN FR76 AND FR79 SEAT TRACK 1 IAW SRM 51-40-21, PG 24, 51-27-00, PG1, 51-40-40, PG1, 51-74-10, PG210, 51-21-10, PG6 -7, 53-10-16, PG101 - 103, 51-75-10, PG206.
- [SDR FDEA201101120127](https://openairdocs.org/sdr/FDEA201101120127.md): Seat Track · corroded · Jan 12, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK 1 HAS CORROSION FR 75 TO FR 77 ABOUT 30 SQUARE INCHES, REMOVED, FABRICATED AND INSTALLED SEAT TRACK 1, FR75 TO FR79 ALL IAW SRM 51-40-21, PG 24 PARA 7, 51-27-00, PG 1, 51-27-11 PG 1, 51-40-40 PG 1, 51-75-10 PG 206, PARA 4.
- [SDR FDEA201101100099](https://openairdocs.org/sdr/FDEA201101100099.md): Floorbeam · corroded · Jan 10, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > BULK CARGO COMPARTMENT UNDERFLOOR, FR69, 17" TO 19" RT OF ACFT CENTERLINE, AXIAL FLOOR PANEL SUPPORT ANGLE HAS CORROSION/SWELLING ABOUT 6 SQUARE INCHES. BULK CARGO COMPARTMENT R & R PROFILE SECTION FR66 TO FR69 RBL17 TO RBL19 IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101100098](https://openairdocs.org/sdr/FDEA201101100098.md): Beam · corroded · Jan 10, 2011 · N423FE · Airbus A310203 · Fuselage Main, Structure
  > BULK CARGO, AFTER REMOVING LATERAL BEAM AT FR67 FOUND AXIAL BEAM CORRODED THROUGH 100 PERCENT PN A53974261202, BULK CARGO. R & R PROFILE BEAM FR66 - FR69 (Y535) IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101100097](https://openairdocs.org/sdr/FDEA201101100097.md): Floor Support · damaged · Jan 10, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOORBEAM RUNNING FWD AND AFT BETWEEN FR66 AND FR65 APPROX 2' RT OF ACFT CTR IS BROKEN. R & R PROFILE SECTION FR65 TO FR66, RBL18 TO RBL24 IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101090092](https://openairdocs.org/sdr/FDEA201101090092.md): Floorbeam · corroded · Jan 9, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > BULK CARGO UNDERFLOOR AXIAL FLOOR SUPPORT ANGLE HAS CORROSION/SWELLING, LT 4" TO 7" FR67 ABOUT 6 SQUARE INCHES. R & R PROFILE SECTION FR66 TO FR69 LT 4" TO 7" IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101090091](https://openairdocs.org/sdr/FDEA201101090091.md): Floorbeam · cracked · Jan 9, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT FOUND 1EA CRACK (.1250" DEEP) IN RADIUS OF UPPER FLOORBEAM FR38, BETWEEN UPPER SEAT TRACK 4L AND 5L CROSSBEAM REPAIRED AT CRACKED STIFFENER FR38 BETWEEN SEAT TRACKS 4L AND 5L IAW A310 SRM 53-10- 15 PGS 246 - 251/252 FIG. 203
- [SDR FDEA201101080089](https://openairdocs.org/sdr/FDEA201101080089.md): Floorbeam · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN CABIN COURIER AREA UNDER FLOOR, CORROSION ON LONGITUDINAL MEMBER AT FLOOR SUPPORT ANGLE 7" FWD OF FLOORBEAM AT FR13, 40" TO LT FROM ACFT CENTERLINE. AMM 53-12-00-06, 57" FROM ACFT CENTERLINE ABOUT 2 SQARE INCHES. REMOVED AND INSTALLED NEW T-CAP TO LON
- [SDR FDEA201101080088](https://openairdocs.org/sdr/FDEA201101080088.md): Seat Track · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN CTR TOP OF SEAT TRACK 2L FRAME 51 ABOUT 5"X1". R & R DAMAGED SEAT TRACK 2L FR49.5 TO FR54 AND INSTALLED A SPLICE REPAIR ON SEAT TRACK 2L AT FR49.5 ALL IAW SRM 53-10-16, FIG 205.
- [SDR FDEA201101080087](https://openairdocs.org/sdr/FDEA201101080087.md): Floorbeam · cracked · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, UPPER FLOORBEAM FR33 HAS 1EA CRACK IN RADIUS BETWEEN SEAT TRACKS 2R AND 3R. CROSSBEAM REPAIRED AT FR33 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 53-10-15, FIG 203.
- [SDR FDEA201101080086](https://openairdocs.org/sdr/FDEA201101080086.md): Seat Track · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CORROSION ON SEAT TRACK 5L APPROX 1"X 2" BETWEEN FRAME 35 AND 36. R & R SEAT TRACK 5L AT FR35-FR36 AND 4EA SEAT TRACK SPLICES IAW SRM 53-10-16, PG 244, PGS 250A/250B FIG 208A.
- [SDR FDEA201101080085](https://openairdocs.org/sdr/FDEA201101080085.md): Seat Track · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON OTBD FLANGE OF SEAT TRACK 4R 2" AFT OF FRAME 34 1"X4 ". REMOVED DAMAGED SEAT TRACK 4R FR26 -FR36 IAW SRM 53-10-16, FIG 208. INSTALLED REPLACEMENT SEAT TRACK AND SPLICES IAW SRM 53-10-16, FIG 208.
- [SDR FDEA201101080084](https://openairdocs.org/sdr/FDEA201101080084.md): Floor Support · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > BULK CARGO UNDERFLOOR FR69 10" LT FROM ACFT CENTERLINE, FLOOR SUPPORT ANGLE HAS CORROSION ABOUT 3 SQUARE INCHES. FABRICATED 1 EA FITTING IAW DWG A53974329. R & R FITTING AT FR69 10" LBL IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101080083](https://openairdocs.org/sdr/FDEA201101080083.md): Floor Support · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > BULK CARGO UNDERFLOOR, FR69 CORROSION ON CARGO NET CLEVIS SUPPORT ANGLE, (ABOUT 2 SQUARE INCHES) R & R BULK CARGO UNDERFLOOR CARGO NET CLEVIS SUPPORT FITTING, FR69 IAW SRM 51-72-10, PGS 1-3.
- [SDR FDEA201101080082](https://openairdocs.org/sdr/FDEA201101080082.md): Seat Track · corroded · Jan 8, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 4R HAS CORROSION AT 8" AFT OF FR51 (-1959) R & R SEAT TRACK SEGMENT AND SPLICE REPAIR AT FR51 TO FR52 SEAT TRACK 4R IAW SRM 51-72-10, PGS1-3 AND 53-10-16 FIG 205.
- [SDR FDEA201101060054](https://openairdocs.org/sdr/FDEA201101060054.md): Profile · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Vertical Stabilizer Miscellaneous Structure
  > RT VERTICAL STABILIZER T/E HORIZ PANEL LANDING SUPPORT STRAP BETWEEN RIBS 21-22 HAS 8 INCH CORROSION IN AND AROUND 3 EA FASTENERS AND ALONG UPPER INTERIOR MATING SURFACE. R & R EDGE PROFILE RT VERT STAB T/E PANEL LANDING BETWEEN RIBS 21 AND 22 IAW SRM 51-72
- [SDR FDEA201101060058](https://openairdocs.org/sdr/FDEA201101060058.md): Rib · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER, RIB 1 TOP SURFACE HAS CORROSION (ABOUT 4 SQ INCHES) RT STRINGER 5 RT TO STR 7 RT. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-31-19, PG 209-211, FIG 203.
- [SDR FDEA201101060056](https://openairdocs.org/sdr/FDEA201101060056.md): Mount · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Vertical Stabilizer, Attach Fittings
  > VERT STABILIZER AFT RT MOUNT LUG FITTING HAS CORROSION ON INTERIOR SURFACE BETWEEN STRINGER 1 RT AND STRINGER 2 RT,ABOUT 2 SQ INCHES. REPAIRED VERT STAB AFT RT LUG FITTING INTERIOR SURFACE BETTWEEN STR1R AND STR2R IAW EA 6-5530-145539.
- [SDR FDEA201101060055](https://openairdocs.org/sdr/FDEA201101060055.md): Mount · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER LT AFT MOUNT LUG HAS CORROSION FROM STR 1 LT TO STR 4 LT, ABOUT 70 SQ INCHES. REPAIRED VERT STAB LT AFT MOUNT LUG BETWEEN S1L TO S4L IAW EA 6-5530-145538.
- [SDR FDEA201101060053](https://openairdocs.org/sdr/FDEA201101060053.md): Crossbeam · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Fuselage Main, Structure
  > REAR FUSELAGE FRAME 86, STR 16, LT TO THS DRIVE UNIT SUPPORT, FWD CROSSBEAM HAS EXFOILIATION CORROSION. REMOVED LEVEL 1 CORROSION. REWORKED CROSSBEAM ON FR 86 AT STR 16 LT IAW SRM 51-74-10. MATERIAL LOSS.006 IN. REMAINING THICKNESS WITHIN LIMITS IAW SRM
- [SDR FDEA201101060052](https://openairdocs.org/sdr/FDEA201101060052.md): Support Beam · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Fuselage Main, Structure
  > REAR FUSELAGE FRAME 87-88, STR 16, RT HORIZ STAB CUTOUT SUPPORT BEAM INBD FACE CORRODED AT 1 EA LOCK FASTENER APPROX 1 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, FOUND TO BE WITH IN MFG TOLERANCES IAW DWG A53985426 AND DAN11304 NDT INSP IAW NTM 51-10-08 NO
- [SDR FDEA201101060051](https://openairdocs.org/sdr/FDEA201101060051.md): Stringer · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > REAR FUSELAGE FRAME 87-89, STR 16, LT HORIZ STAB CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 SQ INCHES. R & R THS CUTOUT FWD FITTING IAW DWG A53985135 AND A310 SRM 51-40-21, PG 46.
- [SDR FDEA201101060050](https://openairdocs.org/sdr/FDEA201101060050.md): Fitting · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > REAR FUSELAGE FRAME 87-89, STR 16 RT, THS CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 INCHES AT AFT ATTACH. R & R THS CUTOUT UPPER FWD CORNER FITTING FR87 TO FR89, STR 16R IAW SRM 51-72-10.
- [SDR FDEA201101060049](https://openairdocs.org/sdr/FDEA201101060049.md): Frame · corroded · Jan 6, 2011 · N423FE · Airbus A310203 · Fuselage Main, Frame
  > REAR FUSELAGE FRAME 85, APPROX 15 INCHES INBD OF STR 16 RT HORIZ CROSSBEAM HAS EXFOILIATION CORROSION ON LOWER FLANGE. REMOVED LEVEL 1 CORROSION. FRAME R & R IAW SRM 53-19-47 WITH FABRICATED PART REF SDR NR 11-0303.
- [SDR FDEA201101050015](https://openairdocs.org/sdr/FDEA201101050015.md): Floorbeam · corroded · Jan 5, 2011 · N423FE · Airbus A310203 · Fuselage Main, Floor Beam
  > BULK CARGO FLOOR SUPPORT LATERAL ANGLE AT FR66 HAS CORROSION AT NUT PLATE LOCATIONS, 10 PLACES, FROM RT 19" TO LT 48" FORM CTR LINE OF ACFT TOTALING 10 SQUARE INCHES. AFT CARGO COMPARTMENT R & R FR66 LATERAL FLOORBEAM AND VERTICAL STIFFENER IAW SRM 51-72-10
- [SDR FDEA201101050014](https://openairdocs.org/sdr/FDEA201101050014.md): Rib · corroded · Jan 5, 2011 · N423FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER RIB 1 WEB TOP SURFACE HAS CORROSION ( ABOUT 4 - SQUARE INCHES) RT STRINGER 5R TO STRINGER 7R VERT STAB RT SIDE REMOVED CORRODED SECTION ON RIB1 WEB BETWEEN STR 5R AND 7R IAW SRM 55-31-19, PG 209 - 210 FIG 203. FABRICATED AND INSTALLED RE
- [SDR FDEA201012244749](https://openairdocs.org/sdr/FDEA201012244749.md): Seat Track · worn · Dec 24, 2010 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY SEAT TRACK RT NR6 AT FR 54.2 HAS GAP AT SLOTTED END. ATTACH BOLT OF.026". REMOVED, REPAIRED AND REINSTALLED DUMMY SEAT TRACK RT NR6 IAW EO 6-5310-7-3322, P2 INSTRUCTIONS.
- [SDR FDEA201012244748](https://openairdocs.org/sdr/FDEA201012244748.md): Seat Track · worn · Dec 24, 2010 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY SEAT TRACK L3 AT FRAME 38.2 HAS A GAP AT SLOT OF 0.020 INCH. REMOVED DUMMY SEAT TRACK NR3L, AT FR 38.2. REPAIRED AND REINSTALLED IAW E0 6-5310-7-3322, P2 INSTRUCTIONS.
- [SDR FDEA201012244747](https://openairdocs.org/sdr/FDEA201012244747.md): Plate · corroded · Dec 24, 2010 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPARTMENT ZONE 230, FR 32 BETWEEN SEAT TRACK 5R AND 6R PAN CORRODED TOP SKIN APPROX 1 SQ INCH. REMOVED CORROSION FROM PAN AND CHECKED LIMITS IAW SRM 53-10-00, PAGE 113 FOUND TO BE OUT OF LIMIT. R & R THRUST PLATE AND STIFFENERS IAW SRM 51
- [SDR FDEA201012234744](https://openairdocs.org/sdr/FDEA201012234744.md): Seat Track · worn · Dec 23, 2010 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 AT FR 38.2 HAS A GAP AT THE SLOT OF.031" REMOVED, REPAIRED AND REINSTALLED THE DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 BETWEEN FR 38.2 TO FR 40/41 IAW EO 6-5310-7-3322 P2 INSTRUCTIONS.

Next page: https://openairdocs.org/deregistered/N423FE-2020-04-23/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 = 'N423FE' AND deregistration_id = 'N423FE-2020-04-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N423FE-2020-04-23/reports

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