# Service difficulty reports: N407FE, cancelled May 14, 2012

A list on [N407FE, cancelled May 14, 2012](https://openairdocs.org/deregistered/N407FE-2012-05-14.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 · 54 reports

- [SDR FDEA200807172947](https://openairdocs.org/sdr/FDEA200807172947.md): Control Unit · malfunctioned · Jul 17, 2008 · N407FE · Airbus A310203 · Landing Gear Brake System
  > NORMAL BEFORE T/O CHECK LIST, PASSING 40 KIAS GOT RED ECAM PARKING BRAKE SET. ABORTED T/O. PARKING BRAKE HANDLE CHECKED STOWED, BUT MOVED FURTHER DOWN.1250 INCH/- NO DRAGGING BRAKING FELT ON INITIAL ROLL. HOWEVER CLEAR OF RWY BRAKE S 4/7/8 WENT UP TO 330 (
- [SDR 08FDEA02947](https://openairdocs.org/sdr/08FDEA02947.md): Control Unit · malfunctioned · Jul 17, 2008 · N407FE · Airbus A310 · Landing Gear Brake System
  > NORMAL BEFORE T/O CHCK LIST, CLEARED FOR T/O RWY 77C DFW PASSING 40 KIAS GOT RED ECAM PARKING BRAKE SET. ABORTED T/O. PARKING BRAKE HANDLE CHECKED STOWED, BUT MOVED FURTHER DOWN 1/8 INCH /- NO DRAGGING BRAKI NG FELT ON INITIAL ROLL. HOWEVER CLEAR OF RWY B
- [SDR 07FDEA00496](https://openairdocs.org/sdr/07FDEA00496.md): Skin · delaminated · Feb 15, 2007 · N407FE · Airbus A310203 · Trailing Edge Flaps
  > LT WING OUTBOARD FLAP LWR SURFACE HAS EVIDENCE OF DELAMINATION. REPAIRED DELAMINATED AREA IAW A310-200 SRM 57-53-12 FIG 207.
- [SDR 07FDEA00474](https://openairdocs.org/sdr/07FDEA00474.md): Skin · misrepaired · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR, LWR RT SIDE FUS SKIN BELOW BULK CARGO DOOR EXTERNAL REPAIR DOUBLER BETWEEN FR67 AND FR68 STR 49 RT TO STR 52 RT, MEASURING 8.8 IN BY 8.4 IN ZONE 160. REPAIR AREA WAS NOT IAW A310 SRM 53-10-12 FIG 225 SHEET 1. AREA REPAIRED CORRECTLY IAW A310
- [SDR 07FDEA00473](https://openairdocs.org/sdr/07FDEA00473.md): Seat Track · corroded · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC FOUND SEAT TRACK NR 2 LT BTN FR72.5 TO FR 73.5 HAS CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 AND CHECKED LIMITS PER SRM 53-10-16 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK NR 3L FR71.5 - FR73.5 IAW A310-200 SRM 51-40-21.
- [SDR 07FDEA00472](https://openairdocs.org/sdr/07FDEA00472.md): Seat Track · corroded · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC FOUND SEAT TRACK NR 2 LT FR 67 IS CORRODED AND GOUGED. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16 FIG 208 SHEET 1. SPLICE REPAIR.
- [SDR 07FDEA00471](https://openairdocs.org/sdr/07FDEA00471.md): Floorbeam · misrepaired · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > PREVIOUS REPAIR MAIN CABIN FLOORBEAM FR 54.3 HAS FLOORBEAM SPLICE SECT REPAIR BETWEEN SEAT TRACKS 3 AND 5 LT, SPLICE SECTION MEASURES 19.9 IN LONG 4EACH REPAIR SPLICE ANGLES 8.8 IN LONG EACH LOCATED ON THE AFT FACE ONLY OF FLOORBEAM ZONE 150. REPAIR AREA WAS
- [SDR 07FDEA00470](https://openairdocs.org/sdr/07FDEA00470.md): Seat Track · misrepaired · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR, MAIN CABIN SEAT TRACK 4 RT HAS REPAIR WITH 2 EACH REPAIR ANGLES MEASURING 9.5 IN LONG EACH, BETWEEN FR74 AND FR75 ZONE 260. REPAIR AREA WAS NOT IAW A310 SRM 53-10-16 FIG 201. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-16 FIG 201 AND COMPLI
- [SDR 07FDEA00469](https://openairdocs.org/sdr/07FDEA00469.md): Structure · misrepaired · Feb 13, 2007 · N407FE · Airbus A310203 · Fuselage Main, Structure
  > PREVIOUS REPAIR, AFT CABIN UNDERFLOOR BEHIND BULK CARGO HAS REPAIR ON STR 56 RT, WITH 1. REPAIR SPLICE MEASURING 7.7 IN LONG AND STRINGER REPAIR SECTION MEASURES 26.5 IN LONG BETWEEN FR72 AND FR74 ZONE 170 REPAIR WAS NOT IAW A310 SRM 53-10-14 FIG 201. AREA R
- [SDR 07FDEA00442](https://openairdocs.org/sdr/07FDEA00442.md): Floorbeam · cracked · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, MDC FLOORBEAM FRAME 21 CRACKED RT SIDE. LENGTH OF CRACK.380 INCH. REPAIRED PER ENG DISPO AND A310-200 SRM SUPP 53-10-15 FIG 201 SHEET 2. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00344.
- [SDR 07FDEA00445](https://openairdocs.org/sdr/07FDEA00445.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK NR 3R AT FR 78 HAS EXFOLIATION CORROSION. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00818.
- [SDR 07FDEA00444](https://openairdocs.org/sdr/07FDEA00444.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK 0 AT FR 77.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW DWG 18A532-79237. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00789.
- [SDR 07FDEA00443](https://openairdocs.org/sdr/07FDEA00443.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK NR 5R AT FR 77.5 HAS CORROSION. BLEND CORROSION, OUT OF LIMITS. REPLACED DAMAGED SEAT TRACK SECTION WITH NEW AND SPLICES IAW A310-200 SRM 51-74-10, 53-10-16. ALSO, INSTALLED FLOORBOARDS 262VF AND 262UF IAW A310 AMM 53-10-23. MAJOR REPAIR IAW
- [SDR 07FDEA00441](https://openairdocs.org/sdr/07FDEA00441.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK 1 AT FR73 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AIRBUS DWG NR 18A532-79237. REPLACED 1 STRAP P/N A5378103620095, MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00791.
- [SDR 07FDEA00440](https://openairdocs.org/sdr/07FDEA00440.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC - FOUND SEAT TRACK 2R AT FS 61 HAS CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. CHECKED LIMITS PER A310 SRM 53-10-16, AREA IS OUT OF LIMITS. REMOVED SEAT TRACK SECTION PER A310 SRM 53-10-16. FABRICATED NEW SEAT TRACK SECTION AND REPAIR PARTS PER
- [SDR 07FDEA00438](https://openairdocs.org/sdr/07FDEA00438.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC - FOUND SEAT TRACK NR 2 L BETWEEN FR 68.0 TO 69.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21 AND 53-10-16.
- [SDR 07FDEA00437](https://openairdocs.org/sdr/07FDEA00437.md): Stringer · misrepaired · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR ON STR 55 RT WITH 2 REPAIR SPLICES DO NOT MEET THE INTENT OS A310 SRM 53-10-14 FIG 201. REMOVED INCORRECTED REPAIR AND REPAIRED AREA IAW A310 SRM 53-10-14 FIG 201.
- [SDR 07FDEA00434](https://openairdocs.org/sdr/07FDEA00434.md): Seat Track · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK NR 3 R AT FR 68 R HAS CORROSION REPAIRED SEAT TRACK IAW A310-200 SRM 53-10-16.
- [SDR 07FDEA00433](https://openairdocs.org/sdr/07FDEA00433.md): Floorbeam · cracked · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FOUND CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FR 58 BETWEEN TRACK 4R AND 5R COMPLIED WITH EA 6-5310-106317 PG 1 REF 4.
- [SDR 07FDEA00432](https://openairdocs.org/sdr/07FDEA00432.md): Door · chafed · Feb 9, 2007 · N407FE · Airbus A310203 · Landing Gear Doors
  > 2 CHAFE MARKS EXIST AT LT MLG PRIMARY DOOR AFT LWR POSITION BLENDED AND SMOOTHED CHAFE MARKS IAW A310-200 AMM 51-73-10-8. REPAIRED AREA IAW A310-20 0 AMM 51-73-10 AND EA 6-5280-106329.
- [SDR 07FDEA00430](https://openairdocs.org/sdr/07FDEA00430.md): Support Bracket · damaged · Feb 9, 2007 · N407FE · Airbus A310203 · Nacelle/Pylon Miscellaneous Structure
  > 5 ELONGATED HOLES EXIST AT NR 2 ENGINE PYLON UNDERNEATH HYD SUPPORT BRACKET ACCESS PNL NR 483 CL. REPAIRED PYLON IAW 6-5450-106327.
- [SDR 07FDEA00429](https://openairdocs.org/sdr/07FDEA00429.md): Skin · delaminated · Feb 9, 2007 · N407FE · Airbus A310203 · Trailing Edge Flaps
  > LT WING OUTBD FLAP TE HAS AREA OF DELAMINATION O/B OF FLAP RIB NR 3, 7" BY 1.5", FOUND DURING AGING ACFT INSP. REPAIRED DAMAGED SKIN ON LT O/B FLAP IAW EA 6-5750-107644
- [SDR 07FDEA00428](https://openairdocs.org/sdr/07FDEA00428.md): Floorbeam · corroded · Feb 9, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MDCC - FLOORBEAM FR 63 HAS CORROSION FROM SEAT TRACK 5L TO 5R. REPAIRED FLOORBEAM AT FR 63 FROM SEAT TRACK 5L TO 5R IAW A310 SRM 51-40-21 AND 53-10-15 FIG 201 SH 17.
- [SDR 07FDEA00193](https://openairdocs.org/sdr/07FDEA00193.md): Floorbeam · cracked · Jan 27, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 34 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD PIT). REMOVED AND REINSTALLED FLOORPANEL FOR FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21. REMOVED CRACK IAW A310
- [SDR 07FDEA00192](https://openairdocs.org/sdr/07FDEA00192.md): Floorbeam · cracked · Jan 27, 2007 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 36 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD CARGO PIT). REMOVED AND REINSTALLED FLOOR PANEL TO FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21. REMOVED CRACK IAW
- [SDR 06FDEA0926](https://openairdocs.org/sdr/06FDEA0926.md): Smoke Detector · false activation · Nov 2, 2005 · N407FE · Airbus A310203 · Smoke Detection
  > CLIMBING THROUGH 12,500 FT RED SMOKE LIGHT ILLUMINATED ON ANNUNCIATOR PANEL (BELOW ENG GAUGES) SIMULTANEOUS ECAM SHOWED AMBER -SMOKE- DIRECTING - DISCH AGENT 2 - NO OTHER INDICATION OF SOURCE OF SMOKE. DISCHARGED AGENT 2 PER ECAM. REMOVED AND INSTALLED THE F
- [SDR 04FDEA02677](https://openairdocs.org/sdr/04FDEA02677.md): Dampener · inoperative · Sep 14, 2004 · N407FE · Airbus A310 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF YYC, ATTEMPTED TO RAISE GEAR, ABLE, TO THE INTERLOCK POSITION, INDICATED GEAR DOWN, UNLOCKED TRIED CYCLING GEAR AND CIRCUIT BREAKERS. NO LT GEAR PITCH DAMPENER POPPET EXTENDED. LT GEAR PITCH DAMPER REPLACED IAW AMM 32-11-15-4. NR 2 MAIN WHEEL R
- [SDR 04FDEA02714](https://openairdocs.org/sdr/04FDEA02714.md): Poppet Valve · tripped · Sep 11, 2004 · N407FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > AFTER T/O YYC, ATTEMPTED TO RAISE GEAR, UNABLE TO THE INTERLOCK POS, LT GEAR PITCH DAMPENER POPPET EXTENDED. REQUIRE PITCH DAMPENER CPN 3212339 DAMPER. LT GEAR PITCH DAMPER REPLACED PER AMM 32-11-15-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MF
- [SDR 04FDEA02159](https://openairdocs.org/sdr/04FDEA02159.md): Crossbeam · cracked · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage Main, Structure
  > ZONE 232 FRAME IS CRACKED UNDER CLS ADAPTER PLATE AT FR 23 BETWEEN SEAT TRACKS 1R & 2R. REPAIRED CRACKED FRAME 23 IAW A310-200 SRM 53-10-15 WITH REPAIR ANGLES AND FILLERS. WORK DOCUMENTED ON NRC N00411.
- [SDR 04FDEA02157](https://openairdocs.org/sdr/04FDEA02157.md): Seat Track · corroded · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK 1L 3 INCHES AFT OF FR 38.2 HAS CORROSION ON SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-20, 51-40-21, AND 51-72-10.
- [SDR 04FDEA02156](https://openairdocs.org/sdr/04FDEA02156.md): Seat Track · corroded · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN DUMMY TRACK 2R FR38.2 TO FR40/41 HAS 3 EA AREAS OF EXFOLIATED CORROSION LEVEL 3. REMOVED AND REPLACED SEAT TRACK IAW 51-40-20 AND 51-40-21.
- [SDR 04FDEA02155](https://openairdocs.org/sdr/04FDEA02155.md): Seat Track · corroded · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK 2R FR45 TO FR54 HAS 6 EA AREAS OF EXFOLIATED CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10.
- [SDR 04FDEA02154](https://openairdocs.org/sdr/04FDEA02154.md): Mount · damaged · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > MAIN CARGO COMPT LAV I/B AFT MOUNTING HOLE IS GOUGED. REPLACED DAMAGED SECTION OF TEE CAP IAW A310 SRM 51-40-21, 51-27-00, 51-23-10, AND 51-21-10.
- [SDR 04FDEA02153](https://openairdocs.org/sdr/04FDEA02153.md): Seat Track · cracked · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK 2R FR 40/41 TO 6 INCHES AFT OF FR 45 IS 1 CORRODED AND CRACKED AT FR 43 ON THE I/B SIDE FLANGE AND 2 CORRODED IN THE SCALLOP AREA 10 INCHES AFT OF FR 44 (LEVEL 2). REMOVED AND REPLACED SEAT TRACK FROM FR40 TO FR 46 IAW SRM 51-72-10.
- [SDR 04FDEA02152](https://openairdocs.org/sdr/04FDEA02152.md): Seat Track · corroded · Jul 22, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC - SEAT TRACK L4 AT FR 16 HAS SEVERE LEVEL 3 CORROSION STARTING AT FR 16 AND GOING FORWARD 26 INCHES. REMOVED AND REPLACED TRACK IAW A310 SRM 51-40-20 AND 51-40-21.
- [SDR 04FDEA02068](https://openairdocs.org/sdr/04FDEA02068.md): Seat Track · cracked · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC, LATERAL SEAT RACK AT FRAME 44 BETWEEN SEAT TRACK R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OF TRACK ON OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-72-10.
- [SDR 04FDEA02067](https://openairdocs.org/sdr/04FDEA02067.md): Seat Track · cracked · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC, LATERAL SEAT RACK AT FR 45 BETWEEN SEAT TRACKS R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW A310 SRM 51-72-10.
- [SDR 04FDEA02066](https://openairdocs.org/sdr/04FDEA02066.md): Floorbeam · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > UPPER MAIN CABIN ZONE 220 AT Y1959, FR14 TO 15A TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-40-20.
- [SDR 04FDEA02065](https://openairdocs.org/sdr/04FDEA02065.md): Floor Support · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > UPPER MAIN CABIN ZONE 220 AT Y1456 FR 15A - FR 14 TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-72-10, ZONE 220 AT Y1456 FR15A-FR14.
- [SDR 04FDEA02064](https://openairdocs.org/sdr/04FDEA02064.md): Seat Track · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC, SEAT TRACK L3 AT FRAME 16 AND GOING FWD 16 INCHES HAS MODERATE LEVEL 2 SURFACE CORROSION. SEAT TRACK FR 16 L3 OUT OF LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-21. SEAT TRACK FABRICATION WAS ACCOMPLISHED ON N00428.
- [SDR 04FDEA02063](https://openairdocs.org/sdr/04FDEA02063.md): Seat Track · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER TRACK BREAK TO BREAK FR 69 TO 59.5, 6 EA PLACES AS MARKED FLOOR TRACKS HAVE LITE SURFACE CORROSION EACH APPROX 1 X 1 X 0.003 INCH DEPTH WITHOUT BLENDOUT, AND 1 EA GOUGE TOP SIDE OF TRACK AS MARKED (FR 60) 0.500 X 0.500 X 0.010 INCH DEPTH WITHOUT BLENDOUT
- [SDR 04FDEA02062](https://openairdocs.org/sdr/04FDEA02062.md): Seat Track · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > ZONE 252, SEAT TRACK 2 RIGHT 4 INCHES AFT OF FR 72 HAS CORROSION ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK SECTION PER A310 SRM 53-10-16.
- [SDR 04FDEA02061](https://openairdocs.org/sdr/04FDEA02061.md): Seat Track · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > ZONE 252, SEAT TRACK 2 RIGHT HAS THREE AREAS OF CORROSION BETWEEN FRAMES 69 TO 10 INCHES AFT OF FRAME 71, 12 INCHES AFT OF FR 69, 12 INCHES AFT OF FR 70, 8 INCHES AFT OF FR 71, ALL ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10, NEW
- [SDR 04FDEA02060](https://openairdocs.org/sdr/04FDEA02060.md): Floorbeam · corroded · Jul 13, 2004 · N407FE · Airbus A310203 · Fuselage Main, Floor Beam
  > AFT CARGO LEFT SIDE FLOORBOARD SUPPORT CROSS MEMBER HAS EXFOLIATION CORROSION AT FRAME 60. CUT DAMAGED SECTION IAW A310-200 SRM 53-10-15, VERIFIED MAT'L TO FAB, FABBED REPAIR ANGLE AND FILLER, LOCATED, DRILLED DEBURRED AND COUNTERSUNK IAW A310 SRM 51-40-44.
- [SDR 04FDEA02054](https://openairdocs.org/sdr/04FDEA02054.md): Crossbeam · corroded · Jul 12, 2004 · N407FE · Airbus A310203 · Fuselage Main, Structure
  > ZONE 152, AFT CARGO FLOOR CROSS MEMBER BEAM, RT CENTER AT FR 58 CORRODED. REMOVED CORRODED BAD SECTION IAW A310-200 SRM 53-10-15 FIG 207. FABBED REPAIR ANGLE AND FILLER IAW A310-200 SRM 53-10-15. LOCATED, DRILLED, DEBURRED, AND COUNTERSUNK IAW A310-200 SRM
- [SDR 02FDEA00187](https://openairdocs.org/sdr/02FDEA00187.md): Pilot Valve · faulty · Mar 6, 2002 · N407FE · Airbus A310203 · Engine Thrust Reverser
  > ON CLIMB AFTER GEAR RETRACTION NR 1 ENG REVERSE UNLOCK LIGHT CAME ON. REMOVED AND REPLACED NR 1 ENG DIRECTIONAL PILOT VALVE AND PDU POS SWITCH MODULE PER MM 78-31-06-02-B, 78-32-09-04-B.
- [SDR 02FDEA00092](https://openairdocs.org/sdr/02FDEA00092.md): Landing Gear · malfunctioned · Feb 7, 2002 · N407FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT, EITHER SYSTEM.
- [SDR 01FDEA00873](https://openairdocs.org/sdr/01FDEA00873.md): Spoiler · malfunctioned · Oct 2, 2001 · N407FE · Airbus A310203 · Drag Control System
  > ON T/O NR 2 SPOILER POPPED UP ON RT WING. RESET FCC 1 & 2, RESET SPOILER PBS. CHECK OK.
- [SDR 01FDEA00072](https://openairdocs.org/sdr/01FDEA00072.md): Roller · dirty · Feb 3, 2001 · N407FE · Airbus A310203 · Passenger/Crew Doors
  > AFT T/O RIGHT FWD ENTRY DOOR LIGHT CAME ON. CLEANED ICE FROM UPR FWD ROLLER HOOK BRACKET. INSP MECHANICAL LINKS AND ROLLERS, NO DEFECTS NOTED. DOOR OPS NORMAL.
- [SDR 97FDEA00592](https://openairdocs.org/sdr/97FDEA00592.md): Lube Pump · failed · Aug 29, 1997 · N407FE · Airbus A310203 · Turbine Engine Oil System
  > 97-0162 NR 1 ENG OIL PRESS DROP TO 0 PSI DURING CLIMBOUT. PASSING FLT LEV 250 LOP WARNING LIGHT ILLUMINATED WITH CONTINUOUS CHIME. QUANTITY REMAINED STEADY AT 20 QT. ENG SHUT DOWN AND RETURNED TO LAND IN MEMPHIS, MOTORED NR 1 ENG AND NO OIL PRESS IS EVIDEN

Next page: https://openairdocs.org/deregistered/N407FE-2012-05-14/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 = 'N407FE' AND deregistration_id = 'N407FE-2012-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N407FE-2012-05-14/reports

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