# Service difficulty reports: N435FE, cancelled Feb 3, 2024

A list on [N435FE, cancelled Feb 3, 2024](https://openairdocs.org/deregistered/N435FE-2024-02-03.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 · 94 reports

- [SDR FDEA201309042115](https://openairdocs.org/sdr/FDEA201309042115.md): Selector Valve · failed · Sep 4, 2013 · N435FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > ON LANDING, NOSE TILLER COULD NOT BE MOVED. DIFFERENTIAL BRAKING USED TO CLEAR RWY. TROUBLESHOT IAW TSM 32-51-00 FIG 103 TO STEP 4. NOSE GEAR DOORS WILL NOT RAISE. SUSPECT LANDING GEAR SELECTOR VALVE. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-3
- [SDR FDEA201210313788](https://openairdocs.org/sdr/FDEA201210313788.md): Jackscrew · failed · Oct 31, 2012 · N435FE · Airbus A310203 · Leading Edge Slat Control System
  > DURING DESCENT AT MEM TO 36R, SLATS WOULD NOT EXTEND AT 210 KTS. EXECUTED QRH PROCEDURES, DECLARED EMERGENCY AND REMAINDER OF APPROACH AND LANDING NORMAL. CREW LEFT SLAT/FLAP HANDLE IN 30/40 POSITION TO ASSIST MX PROCEDURES. REMOVED REPLACED RIGHT WING NR
- [SDR FDEA201108193388](https://openairdocs.org/sdr/FDEA201108193388.md): Panel · corroded · Aug 19, 2011 · N435FE · Airbus A310203 · Elevator, Plate/Skin
  > RT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORROSION AT RT ELEVATOR L/E PANEL FASTNER HOLE AND WEB ATTACHMENT STRAP IAW SRM 51-74-10, PAGE 204. F
- [SDR FDEA201108183365](https://openairdocs.org/sdr/FDEA201108183365.md): Skin · gouged · Aug 18, 2011 · N435FE · Airbus A310203 · Wing, Plate/Skin
  > RT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-10 AT RT WING FIX L/E SLAT TRACK 5 AND 6. NDT FOR CRACK AND LIMITS, NO LIMIT REMAINING THICKNESS.
- [SDR FDEA201108183356](https://openairdocs.org/sdr/FDEA201108183356.md): Skin · gouged · Aug 18, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341AB EXTERNAL SKIN IAW SRM 51-73-10; CHECKED LIMITS FOUND AREAS (3EA) WITHIN LIMITS, 1 AREA OUT OF L
- [SDR FDEA201108173303](https://openairdocs.org/sdr/FDEA201108173303.md): Attach Fitting · corroded · Aug 17, 2011 · N435FE · Airbus A310203 · Wing, Attach Fittings
  > LT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY OVERSIZING THE BORE AND SPOT FACING THE AFT LUG FACE, NDT INSPECTED (NIL FINDING) INCLUDED ACID
- [SDR FDEA201108163289](https://openairdocs.org/sdr/FDEA201108163289.md): Adapter · cracked · Aug 16, 2011 · N435FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > CLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW SRM 51-72-10, PG. 1-3.
- [SDR FDEA201108153280](https://openairdocs.org/sdr/FDEA201108153280.md): Channel · bent · Aug 15, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INNER FUSELAGE "U" CHANNEL IS BENT STR 33L BETWEEN FR 83 TO FR 84. R & R CHANNEL AT STR 33L BETWEEN FR 83 TO FR 84 IAW SRM 51-40-21. PARAGRAPH 7.
- [SDR FDEA201108143274](https://openairdocs.org/sdr/FDEA201108143274.md): Intercostal · bent · Aug 14, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AND UPPER ANGLE ARE BENT STR 33R. INNER FUSELAGE BETWEEN FRAME 85 AND FRAME 86. REMOVED AND FAB AND INSTALLED INTERCOSTAL ANGLE ON FR 85 TO 86 RT STRINGER 33R, REF SRM 51-40-21, PG7 REPROTECTED AREA IAW SRM 51-75-10.
- [SDR FDEA201108113220](https://openairdocs.org/sdr/FDEA201108113220.md): Skin · gouged · Aug 11, 2011 · N435FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > UPPER AFT AREA OF AFT CARGO DOOR CUTOUT, EXT SURFACE, HAS MULTIPLE SCRATCHES EXTENDING 10" AFT OF CUTOUT (FR63) BETWEEN STRINGERS 27R & 28R. SMOOTHED AND BLENDED 10" SQ IN AFT CARGO DOOR CUTOUT EXT SURFACE FR63, STR 27 & 28 IAW SRM 51-73-10. MAP AREA FOR N
- [SDR FDEA201108113219](https://openairdocs.org/sdr/FDEA201108113219.md): Panel · cracked · Aug 11, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZ L/E PANEL 341AB, INTERNAL STIFFENER CRACKED AT AFT END, FROM FASTENER TO EDGE OF PART,.3125" LONG, UPPER AFT CORNER OF PANEL. REMOVED FASTENERS HORZ L/E PANEL 341AB STOP-DRILLED CRACK ON INTERNAL STIFFENER, NDT FOR CRACKS. NO CRACKS WERE FOUND, FABR
- [SDR FDEA201108113200](https://openairdocs.org/sdr/FDEA201108113200.md): Frame · corroded · Aug 11, 2011 · N435FE · Airbus A310203 · Fuselage Main, Frame
  > AFT CARGO DOOR AFT EDGE SEAL LANDING STRIP GOUGED AT MULTIPLE PLACES ON FUSELAGE CUTOUT FR 63A R & R 3EA AFT CARGO DOOR AFT EDGE SEAL LANDINGS IAW SRM 51-72-10. UPON FURTHER EVALUATION, FOUND CORROSION AT FR 63A, STR 28R TO 29R, REMOVED CORROSION IAW SRM
- [SDR FDEA201108083139](https://openairdocs.org/sdr/FDEA201108083139.md): Access Door · cracked · Aug 8, 2011 · N435FE · Airbus A310203 · Auxiliary Power Unit (APU) Doors
  > APU RT ACCESS DOOR 316AR AFT MATING FLANGE ON TAILCONE ASSY DEFORMED BELOW LATCH RECEPTACLE, MEASURED 4 IN LENGTH. REMOVED MATING FLANGE IAW SRM 51-40-21. INSTALLED NEW MATING FLANGE IAW SRM 51-40-21 AT AFT APU DOORS AFT MATING FLANGE.
- [SDR FDEA201108083138](https://openairdocs.org/sdr/FDEA201108083138.md): Tray · corroded · Aug 8, 2011 · N435FE · Airbus A310203 · Cargo Compartments
  > AFT CARGO COMPARTMENT LT FWD PDU TRAY FLANGE IS BENT BETWEEN FR55 AND 56 AND NR 2L AND NR 3L TRACK ROLLERS. R & R PDU TRAY IAW SRM 51-40-21, DUE TO CORROSION FOUND OUT OF LIMITS IAW SRM 51-74-10 CORRODED AREA MEASURES 6.00L X 5.00 W X.012. MATERIAL LOSS
- [SDR FDEA201108083133](https://openairdocs.org/sdr/FDEA201108083133.md): Hinge · cracked · Aug 8, 2011 · N435FE · Airbus A310203 · Accessory Compartment Doors
  > BOTTOM EXT FUSE EXT ELECTRICAL POWER PLUG ACCESS DOOR INNER DOUBLER CRACKED.2" IN LENGTH. REMOVED ELECTRICAL POWER PLUG ACCESS DOOR, R & R DAMAGED INNER DOUBLER, AND RE-INSTALLED ELECTRICAL POWER PLUG ACCESS DOOR IAW SRM 51-40-21, PARA 5 AND 6.
- [SDR FDEA201108073130](https://openairdocs.org/sdr/FDEA201108073130.md): Retainer · cracked · Aug 7, 2011 · N435FE · Airbus A310203 · Spoilers
  > RT WING NR1 SPOILER T/E RETAINER STRAP IS CRACKED APPROX 1" LONG INBD END. R & R RETAINER STRIP IAW CMM 57-71-11.
- [SDR FDEA201108073132](https://openairdocs.org/sdr/FDEA201108073132.md): Access Panel · cracked · Aug 7, 2011 · N435FE · Airbus A310203 · Wing, Plate/Skin
  > RT WING L/E ACCESS PANEL NR 624EB CUT OUT LANDING IS CRACKED APPROX 1" LONG. R & R CUT OUT LANDING FOR ACCESS PANEL 624EB IAW SRM 51-40-01, PAR 6 & 7 AND SRM 51-40-44 PG1-16, SRM 51-40-21 PARA 6&7. APPLIED ALODINE, PRIMED AND PAINTED IAW SRM 51-75-10.
- [SDR FDEA201108063117](https://openairdocs.org/sdr/FDEA201108063117.md): Adapter · cracked · Aug 6, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CLEVIS ADAPTER AT FR 45 BETWEEN SEAT TRACK 2 & 3 RT IS CRACKED APPROX 1" LONG AT FWD FLANGE. R & R CLEVIS ADAPTER IN MDCC AT FR 45 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW SRM51-40-21. FLOORBOARD LOCATED AND DRILLED IAW SRM 51-40-44. HOLES TREATED AND PRO
- [SDR FDEA201108053112](https://openairdocs.org/sdr/FDEA201108053112.md): Support Bracket · cracked · Aug 5, 2011 · N435FE · Airbus A310203 · Engine Thrust Reverser
  > NR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. REMOVED CRACKED UPPER COWL GUIDE SUPPORT BRACKET IAW SRM 54-40-21 AND SRM 54-04-01 PG.11. FABRICATE
- [SDR FDEA201108033081](https://openairdocs.org/sdr/FDEA201108033081.md): Stringer · cracked · Aug 3, 2011 · N435FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > RT SIDE STRINGER 9R BETWEEN FR 98 TO 100 HAS 2 PIECES BROKEN OFF. R & R STRINGER 9R FROM FR 95 TO 102 IAW SRM 51-72-10, PARA 5A & 6A. FABRICATED NEW STRINGER IAW DWG 19A53989507. REPROTECTED IAW SRM 51-21-10, 51-23-10, & 51-75-10.
- [SDR FDEA201108033083](https://openairdocs.org/sdr/FDEA201108033083.md): Intercostal · bent · Aug 3, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INNER FUSELAGE INTERCOSTAL IS BENT STR 33L BETWEEN FR85 TO FR84. REMOVED INTERCOSTAL STR 33L BETWEEN FR85 TO FR84 IAW SRM51-40-21, PARA 6, B/S FABRICATED STIFFENER AND WEB IAW DWG A53986749.LOCATED AND DRILLED AND INSTALLED STIFFENER AND WEB,FR85 TO FR84, ST
- [SDR FDEA201108013058](https://openairdocs.org/sdr/FDEA201108013058.md): Intercostal · bent · Aug 1, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IS BENT STR 35R INNER FUSELAGE BETWEEN FR86 TO FR87. REMOVED DAMAGED INTERCOSTAL, REPLACED WITH NEW INTERCOSTAL AND STRIP AT STR 35R BETWEEN FR 86 AND FR87 IAW SRM51-75-10 AND SRM51-21-10.
- [SDR FDEA201107313046](https://openairdocs.org/sdr/FDEA201107313046.md): Structure · gouged · Jul 31, 2011 · N435FE · Airbus A310203 · Spoilers
  > RT WING SPOILER NR 7 LOWER T/E IS GOUGED APPROX.500" WIDE. R & R T/E OF RT WING NR 7 SPOILER IAW SRM 51-72-10.
- [SDR FDEA201107303040](https://openairdocs.org/sdr/FDEA201107303040.md): Seat Track · damaged · Jul 30, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR TRACK L3 HAS DAMAGED RECEPTICLES LOCATED BETWEEN FLOORBEAM 61 AND 60. REMOVED DAMAGED SECTION FROM BETWEEN FRAMES 58 AND FRAMES 62 AND INSTALLED SPLICE REPAIR IAW SRM 53-10-16, FIG 208 SHEET 1. RESTORED PROTECTIVE COATINGS IAW SRM 51-75-10 AND 51-21-10
- [SDR FDEA201107303038](https://openairdocs.org/sdr/FDEA201107303038.md): Mount Bracket · cracked · Jul 30, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon, Attach Fittings
  > AFT UPPER PYLON RIB 21, 3 INCH CRACK AT WING TO PYLON MOUNT BRACKET. R & R TEE PICK-UP ANGLE IAW SRM 51-72-10, PGS 1-3 AND SRM 51-40-21, PGS 31-36.
- [SDR FDEA201107303037](https://openairdocs.org/sdr/FDEA201107303037.md): Access Panel · cracked · Jul 30, 2011 · N435FE · Airbus A310203 · Wing, Plate/Skin
  > LT EXTERNAL PACK AREA INBD LANDING FOR PANEL 143FL HAS.250. CRACK REMOVED LANDING FOR PANEL 143FL, INSTALLED NUTPLATES ON NEW LANDING IAW SRM 51-40-21. INSTALLED NEW LANDING ON LT EXTERNAL PACK AREA FOR PANEL 143FL IAW SRM 51-40-21.
- [SDR FDEA201107293031](https://openairdocs.org/sdr/FDEA201107293031.md): Seal · worn · Jul 29, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL, FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-21.
- [SDR FDEA201107293021](https://openairdocs.org/sdr/FDEA201107293021.md): Bracket · bent · Jul 29, 2011 · N435FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FR 33, STGR 15L, 2 EA ISOLATOR BRACKET BENT. REMOVED 2 EA BRACKETS IAW SRM 51-40-21. FABBED 2 EA BRACKETS IAW DWG A53771078. ALODINED BRACKETS IAW SRM 51-21-10. PRIMED AND TOPCOATED IAW SRM 51-21-10, PARTMARKED IAW GMM 7-0-1001. INSTALLED 2 EA BRAKETS
- [SDR FDEA201107293020](https://openairdocs.org/sdr/FDEA201107293020.md): Frame · corroded · Jul 29, 2011 · N435FE · Airbus A310203 · Fuselage Main, Frame
  > AFT PRESSURE BULKHEAD LWR FWD SIDE CIRCUMFERENCE STRAP CORRODED 2 INCHES LENGTH X 3 INCHES WIDTH BETWEEN STGR 44L AND 46L. REMOVED AND REAPPLIED SEALANT ON AFT PRESS BULKHEAD FWD SIDE IAW SRM 51-74-10 PB 201, R & R ANGLE ANGLE SUPPORT IAW SRM 51-40-21; FABR
- [SDR FDEA201107293019](https://openairdocs.org/sdr/FDEA201107293019.md): Intercostal · bent · Jul 29, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IS BENT STR 33R INNER FUSELAGE BETWEEN FR'S 86 AND 87 FABRICATED. REPLACEMENT INTERCOSTAL, LOCATED, DRILLED, INSTALLED AND REPROTECTED IAW SRM 51-40-44, DWG A539-86751 AND 51-42-11, PG 7-22 AND 51-75-10.
- [SDR FDEA201107252942](https://openairdocs.org/sdr/FDEA201107252942.md): Roller Tray · corroded · Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > INSIDE AFT CARGO COMPT AT THE BOTTOM SURFACE OF 2R ROLLER TRACK, CORROSION 2.5" X 3" AT 10" FWD OF FR62. AFTER REMOVAL OF BALL MATS FOUND 1EA AREA ON ROLLER TRAY TO BE LEVEL 1, OUT OF LIMITS IAW SRM 53-10-15, FIG 102, BEYOND REPAIR, R & R ROLLER TRAY IAW AT F
- [SDR FDEA201107252941](https://openairdocs.org/sdr/FDEA201107252941.md): Seat Track · cracked · Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > CLS ADAPTER AT FS 43 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX 1 INCH LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2 & 3 IAW SRM 51-40-21.
- [SDR FDEA201107252937](https://openairdocs.org/sdr/FDEA201107252937.md): Adapter · cracked · Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CLS ADAPTER AT FS 42 BETWEEN SEAT TRACK 2R AND 3R IS CRACKED APPROX 1.5" LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR42 BETWEEN SEAT TRACKS 2 AND 3RT IAW SRM 51-40-21.
- [SDR FDEA201107252931](https://openairdocs.org/sdr/FDEA201107252931.md): Stringer Splice · corroded · Jul 25, 2011 · N435FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R SPLICE AT FRAME 54 HAS A 1 SQ IN AREA OF CORROSION, AFT SIDE OF FRAME. REMOVED CORROSION AT SPLICE PLATE AND FOUND LEVEL 1 CORROSION TO BE OUT OF LIMITS IAW SRM 51-73-10. R & R SPLICE IAW SRM 51-72-10.
- [SDR FDEA201107242925](https://openairdocs.org/sdr/FDEA201107242925.md): Strap · corroded · Jul 24, 2011 · N435FE · Airbus A310203 · Rudder Structure
  > RUDDER L/E ATTACH LANDING, RT SIDE, INTERNAL STRAP CORRODED, 2SQ IN, 6 INCHES ABOVE NR1 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10, PAR 5, FABRICATED NUT PLATE STRAP IAW DWG A554-71556, ALODINED IAW SRM 51-21-10 PG 6. PRIMED IAW SRM 51-75-10,
- [SDR FDEA201107242929](https://openairdocs.org/sdr/FDEA201107242929.md): Rib · cracked · Jul 24, 2011 · N435FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/Rib
  > LT PYLON AT RIB 22 UPPER AFT SIDE HAS A 2 IN LONG CRACK. R & R TEE PICKUP ON LT NR1 PYLON AT RIB 22 IAW SRM 51-72-10.
- [SDR FDEA201107242924](https://openairdocs.org/sdr/FDEA201107242924.md): Strap · corroded · Jul 24, 2011 · N435FE · Airbus A310203 · Rudder Structure
  > RUDDER L/E ATTACH LANDING, RT SIDE INTERNAL STRAP CORRODED 2SQ IN, 8" ABOVE NR4 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10: FABRICATED PLATE IAW DWG A554-71556, ALODINED NUT PLATE STRAP IAW SRM 51-21-10 PAR.6, PRIMED IAW A310-200 SRM 51-75-10 P
- [SDR FDEA201107242923](https://openairdocs.org/sdr/FDEA201107242923.md): Bracket · cracked · Jul 24, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FR26, STR 15 LT ISOLATOR BRACKET BROKEN IAW AMM 25-50-00-06. R & R ISOLATOR BRACKET AT FR 26 STR 15 LT IAW SRM 51-72-10 & 51-40-21, PARA 6.
- [SDR FDEA201107222908](https://openairdocs.org/sdr/FDEA201107222908.md): Floorboard · damaged · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > AFT CARGO FLOORBOARD 152EF MISSING EDGE FILLER DEFCT MEASURES 2 SQ INCHES. FABRICATED REPLACEMENT FLOORBOARD 152EF IAW DWG SR2 25-005, REV J.
- [SDR FDEA201107222907](https://openairdocs.org/sdr/FDEA201107222907.md): Floor Panel · cracked · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > FLOOR PANEL 252GF HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 262GF IAW DWG SR2 25-005, REV J.
- [SDR FDEA201107222906](https://openairdocs.org/sdr/FDEA201107222906.md): Floorboard · damaged · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > FLOORBOARD 251GF HAS PUNCTURE. FABRICATED REPLACEMENT FLOORBOARD 251GF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222905](https://openairdocs.org/sdr/FDEA201107222905.md): Floor Panel · cracked · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > FLOOR PANEL 251WH HAS 12 IN CRACK FABRICATED REPLACEMENT PANEL 251WH IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222904](https://openairdocs.org/sdr/FDEA201107222904.md): Floor Panel · contaminated · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > FLOOR PANEL 147BF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 147BF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222902](https://openairdocs.org/sdr/FDEA201107222902.md): Floor Panel · damaged · Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > AVIONICS COMPT FLOOR PANEL 121JF HAS 1 EA CORNER BROKEN AND 1 EA CORNER PLIES WORN THRU. FABRICATED REPLACEMENT FLOOR PANEL 121JF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107212888](https://openairdocs.org/sdr/FDEA201107212888.md): Spar · corroded · Jul 21, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB UPPER REAR SPAR TOP FLANGE BOTTOM SIDE CORRODED AT 4EA NUTPLATE HOLES LOCATED 6 TO 18 INCHES OTBD OF FUSELAGE BETWEEN RIBS 3 AND 5 MEASURED 8 SQ INCHES. REMOVED CORROSION IAW A SRM 51-74-10, FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 CO
- [SDR FDEA201107192817](https://openairdocs.org/sdr/FDEA201107192817.md): Floorbeam · cracked · Jul 19, 2011 · N435FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT FR 34 RT SIDE IAW SRM 53-10-15. NDT IAW NTM 51-10-08 SHOW NO CRACK INDICATION AFTER CUTOUT OF DAMAG
- [SDR FDEA201107192816](https://openairdocs.org/sdr/FDEA201107192816.md): Skin · cracked · Jul 19, 2011 · N435FE · Airbus A310203 · Auxiliary Power Unit (APU) Doors
  > APU EXHAUST DOOR 317AL RT LOWER LATCH CUTOUT SKIN HAS A.10 INCH CRACK. ROUTED OUT CRACK, NDT FOUND NO CRACKS, REPROTECTED AREA IAW SRM 52-41-18, PAGE 203 AND SRM 51-75-10. FABRICATED DOUBLER, DRILLED AND INSTALLED IAW SRM 52-41-18, FIG 201, PAGES 207-208.
- [SDR FDEA201107192798](https://openairdocs.org/sdr/FDEA201107192798.md): Clevis · bent · Jul 19, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC AT FS 54.1 BETWEEN SEAT TRACKS 2 & 3 RT CLEVIS ADAPTER FWD FLANGE IS BENT IN 2 EA PLACES. R & R ADAPTER AT FR 54.1 MDCC BETWEEN TRACKS 2 & 3 ON RT SIDE IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW ADAPTER IAW SRM 51-40-44, PG 1-16.
- [SDR FDEA201107192793](https://openairdocs.org/sdr/FDEA201107192793.md): Clevis · cracked · Jul 19, 2011 · N435FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW CLEVIS IAW SRM 51-40-44, PG 16.
- [SDR FDEA201107182783](https://openairdocs.org/sdr/FDEA201107182783.md): Floor Panel · cracked · Jul 18, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
  > FLOOR PANEL 147 AF HAS A 1" INCH CRACK AND IS OIL SOAKED. FABRICATED REPLACEMENT FLOOR PANEL 147 AF USING DWG SRZ 25-005, REV J.

Next page: https://openairdocs.org/deregistered/N435FE-2024-02-03/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 = 'N435FE' AND deregistration_id = 'N435FE-2024-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N435FE-2024-02-03/reports

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