# Service difficulty reports: N418FE, cancelled Feb 18, 2016

A list on [N418FE, cancelled Feb 18, 2016](https://openairdocs.org/deregistered/N418FE-2016-02-18.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA201204131398](https://openairdocs.org/sdr/FDEA201204131398.md): Valve · inoperative · Apr 13, 2012 · N418FE · Airbus A310222 · Pressure Regulator/Outflow Valve
  > PASSING 10000 FT, RECEIVED ECAM ALERT ROR EXCESS CABIN ALTITUDE, ALSO OBSERVED ECAM ADVISORY FOR EXCESS CABIN VERTICAL SPEED (APPROX 3800') CLIMB. TRIED CONTROLLING WITH MANUAL PRESS CONTROL COULD NOT STOP RATE OF CLIMB. DONNED OXYGEN MASKS DESCENDED TO 1
- [SDR FDEA201111235007](https://openairdocs.org/sdr/FDEA201111235007.md): Landing Gear · malfunctioned · Nov 23, 2011 · N418FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > NOSE GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES, INDICATED UNLOCKED ON BOTH PRIMARY AND SECONDARY INDICATORS USED ALTERNATE PROCEDURE TO EXTEND. EMERGENCY WAS DECLARED. TROUBLESHOOTING AT THIS TIME.
- [SDR FDEA201010023862](https://openairdocs.org/sdr/FDEA201010023862.md): Skin · corroded · Oct 2, 2010 · N418FE · Airbus A310 · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN AFT EDGE FOUND CORROSIN. REMOVE TOP SKIN UNTIL THE REAR SPAR. PERFORM SRM 55-21-11 CONG-1 FIG 209 WITH THE FOLLOWING PROVISIONS: INSTALLED STRAP FILLER.
- [SDR FDEA201009093324](https://openairdocs.org/sdr/FDEA201009093324.md): Sleeve · out of position · Sep 9, 2010 · N418FE · Airbus A310222 · Cabin Cooling System
  > ADVANCING THROTTLES FOR TAKEOFF, RECEIVED A ENG 2 BLEED LEAK. FACT OPEN NR 2 ENG COWLS AND INSPECTED FOUND NO EVIDENCE OF BLEED LEAK WITH APU AIR. REMOVED RT WING L/E PANEL FOUND NO AIR LEAK AT PNEUMATIC DUCT. ALL LEAK CHECK USING APU AIR. FUTHER CHECK FOUND
- [SDR FDEA201006222111](https://openairdocs.org/sdr/FDEA201006222111.md): Uplock · damaged · Jun 22, 2010 · N418FE · Airbus A310222 · Landing Gear Door Retract Section
  > AFTER TAKEOFF RECEIVED LANDING DOOR NOT CLOSED ECAM. CONFIRMED IT WAS THE NOSE FEAR DOOR (AMBER ON BOTH LANDING GEAR PANELS), IAW MX INSTRUCTION, RECYCLED GEAR, BOTH LIGHTS SAME ON AND ECAM RETURNED, MX WANTED GEAR RECYCLE AGAIN, BUT NOSE GEAR AREA VERY NO
- [SDR 08FDEA04623](https://openairdocs.org/sdr/08FDEA04623.md): Mount · corroded · Oct 30, 2008 · N418FE · Airbus A310222 · Engine Mount Section
  > AFT MOUNTING MATING SURFACE ON NR 2 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA NR 6-5450-125471 PART 2.
- [SDR 08FDEA04624](https://openairdocs.org/sdr/08FDEA04624.md): Fitting · corroded · Oct 30, 2008 · N418FE · Airbus A310222 · Engine Mount Section
  > AFT MOUNTING MATING SURFACE ON NR 1 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA 6-5450-125471 PART 2.
- [SDR 08FDEA04465](https://openairdocs.org/sdr/08FDEA04465.md): Arm · cracked · Oct 21, 2008 · N418FE · Airbus A310222 · Elevator Structure
  > EMPENNAGE, RT ELEV NR 5 HINGE ARM FOUND CRACKED/CORROSION AT UPPER END REPLACED RT ELEV NR 5 HINGE ARM AS PER AMM 55-16-45-4.
- [SDR 08FDEA04464](https://openairdocs.org/sdr/08FDEA04464.md): Skin · delaminated · Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge Flaps
  > LT WING, INBD FLAP TRAILING EDGE UPPER SURFACE PREVIOUS REPAIR LOCATED 44.0 INCH FROM OTBD EDGE DELAMINATED APPROX 3.0 BY 3.0 IN SIZE. REMOVED EXISTING REPAIR BY A NEW REPAIR PER SRM 57-52-12 FIG 204.
- [SDR 08FDEA04463](https://openairdocs.org/sdr/08FDEA04463.md): Skin · delaminated · Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge Flaps
  > RT WING, INBD FLAP TRAIL EDGE LWR SURFACE PREVIOUS REPAIR LOCATED 17.0 INCHES FROM INBD EDGE, DELAMINATED APPROX 22.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER EA 6-5750-125477.
- [SDR 08FDEA04462](https://openairdocs.org/sdr/08FDEA04462.md): Skin · delaminated · Oct 21, 2008 · N418FE · Airbus A310222 · Trailing Edge Flaps
  > LT WING, INBD FLAP TRAIL EDGE LWR SKIN PREVIOUS REPAIR LOCATED 54.5 INCHES FROM INBD EDGE DELAMINATED APPROX 3.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER SRM 57-52-12 FIG 204.
- [SDR 08FDEA04449](https://openairdocs.org/sdr/08FDEA04449.md): Lug · corroded · Oct 20, 2008 · N418FE · Airbus A310222 · Wing, Attach Fittings
  > WHILE COMPLYING WITH EO 6-5710-7-5010 CORROSION WAS FOUND ON BOTH LEFT AND RIGHT WING RIB 5 FORWARD LUG. COMPLIED WITH EA 6-5710-125482 IN THE REMOVAL OF CORROSION ON THE AFFECTED AREAS IN ACCORDANCE WITH EO 6-5710-7-5010.
- [SDR 07FDEA02433](https://openairdocs.org/sdr/07FDEA02433.md): Regulator Valve · failed · Jul 10, 2007 · N418FE · Airbus A310222 · Engine Thrust Reverser
  > ENG 1 REV UNLOCK LIGHTS ILLUMINATED ON T/O ROLL LESS THAN 80KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C 11JUL SFS. REMOVED AND REPLACED ENG 1 PRSOV, PERFORMED OPERATIONAL TEST, NORMAL PER MM 78-32-11-4 AND MM78-32-11-5.
- [SDR 07FDEA02411](https://openairdocs.org/sdr/07FDEA02411.md): Unknown · unknown · Jul 10, 2007 · N418FE · Airbus A310222 · Engine Thrust Reverser
  > UNLOCK LIGHTS ILLUMINATED ON T/O ROLL, LESS THAN 80KTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 20JUL07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSI
- [SDR 06FDEA04174](https://openairdocs.org/sdr/06FDEA04174.md): Skin · damaged · Dec 5, 2006 · N418FE · Airbus A310222 · Drag Control System
  > R-WING NR 4 SPOILER PANEL CENTER I/B HINGE AND O/B HINGE HAS WORN BUSHING. EXCESSIVE PLAY DURING MOVEMENT OF PANEL REMOVED AND REPLACED NR 4 RT WING SPOILER BUSHING IAW AMM 310/200 27-61-51-4 AND CMM 57-73-11. REMOVED AND REINSTALLED NR 4 RT WING SPOILER, O
- [SDR 06FDEA04130](https://openairdocs.org/sdr/06FDEA04130.md): Frame · damaged · Nov 28, 2006 · N418FE · Airbus A310203 · Fuselage Main, Frame
  > WHILE WORKING LT FS 12A DUE TO TOOLING MALFUNCTION DAMAGE TO FRAME 12A APPROX STR 29 COMPLIED WITH EA6-5310-105011.
- [SDR 06FDEA04129](https://openairdocs.org/sdr/06FDEA04129.md): Skin · unknown · Nov 28, 2006 · N418FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR, RT FUSELAGE SKIN HAS EXTERNAL REPAIR DOUBLER MEASURES 8.3 IN X 5.5 IN, LOCATED AT FS 77 BETWEEN STRINGERS 52RT AND 54R REMOVED EXISTING REPAIR AND REPAIRED SKIN PER A310/200 SRM 53-10-12 FIG 217. ALSO, COMPLIED WITH FRAME 77 SHEARTIE TO FRAME
- [SDR 06FDEA04091](https://openairdocs.org/sdr/06FDEA04091.md): Rib · corroded · Nov 22, 2006 · N418FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB FRONT SPAR FWD FACE ENTIRE LENGTH OF RT VERT STAB L/E HAS CORROSION UNDER NUT PLATES AND FASTENER HOLES. REMOVED CORROSION FROM RIB12-26 RT CHORD FLANGE CHECKED AND FOUND TO BE IN LIMITS IAW A310/200 SRM'S 51-74-10, 55-31-21.
- [SDR 06FDEA2855](https://openairdocs.org/sdr/06FDEA2855.md): Engine · bird ingestion · Aug 6, 2006 · N418FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > FELT A JULT ON T/O. SUSPECT COMPRESSOR STALL. CHECKED PER MM 72-00-00-6 03 AND FOUND BIRD STRIKE AT NR 2 ENGINE. COMPLIED ITEM 13B. NOTED NO ABNORMALITIES. ENGINE PARAMETER INDICATION OK. A/C OK FOR SERVICE.
- [SDR 05FDEA02690](https://openairdocs.org/sdr/05FDEA02690.md): Fire Loop · malfunctioned · Aug 26, 2005 · N418FE · Airbus A310222 · Fire Detection
  > REPLACED FIRE DET ASSY (H2/H4) FOR BOTH LOOP A AND B, THIS ALSO CLEARED MEL ON "A" LOOP WRI 26-10/9082 PER MM 26-12-12-4. OPS CHECK SATIS AND PERFORMED ENG RUN PER A-310 JRH OK.
- [SDR 04FDEA02875](https://openairdocs.org/sdr/04FDEA02875.md): Fitting · cracked · Oct 5, 2004 · N418FE · Airbus A310222 · Fuselage Main, Structure
  > MOD TYPE H MOD NR C-CHECK REV NO, PS ACCOMPLISH MAINTENANCE C-CHECK NR 004. DURING C-CHECK WHILE ACCOMPLISHING EO 6-5710-7-3322 FOUND CRACK AT FWD FITTING FRAME 47, HOLE NR 41. ITEM WAS REPAIRED ON N00606 PER FEDEX EA 6-5710-77088.
- [SDR 04FDEA00390](https://openairdocs.org/sdr/04FDEA00390.md): Thrust Reverser · out of rig · Feb 10, 2004 · N418FE · Airbus A310 · Engine Thrust Reverser
  > ON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT ECAM SCREEN. ABORTED T/O COMPLIED WITH QRH, RETURNED TO GATE. MAINTENANCE PROCEDURE PERFORMED IAW MEL 78-30-01-C. MANUALLY CLOSED PRSV AND
- [SDR 01FDEA01040](https://openairdocs.org/sdr/01FDEA01040.md): Crossbeam · cracked · Dec 7, 2001 · N418FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO FLOOR CROSSBEAM DAMAGED AT BS 37 BETWEEN LBL 26.5 & 37.5. R&R CROSSBEAM PER SRM 53-10-15 FIG 201.
- [SDR 00FDEA00617](https://openairdocs.org/sdr/00FDEA00617.md): Floorbeam · cracked · Sep 2, 2000 · N418FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FRAME 37 AT AXIS LHS Y + 1800,.5 INCH BELOW UPPER FLANGE, FOUND CRACK.5 INCH LONG. *S/D* REMOVED AND REPLACED PER FEDEX EA 6-5100-52045 & A310 SRM SUPL MANUAL 53-10-15, FIG 201.
- [SDR 00FDEA00463](https://openairdocs.org/sdr/00FDEA00463.md): Skin · dented · Jul 18, 2000 · N418FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > THREE OFF DENTS IN FUSELAGE SKIN, RHS FWD OF BULK CARGO DOOR CUTOUT DURING C-CHECK. REPAIRED IN ACCORD WITH FEDEX EA REF EA 6-5330-49662.
- [SDR 00FDEA00030](https://openairdocs.org/sdr/00FDEA00030.md): Unknown · smoke · Jan 20, 2000 · N418FE · Airbus A310222 · Air Distribution System
  > 00-17 - UPON TAXI OUT, ODOR OF SMOKE FILLED THE COCKPIT, RETURN TO RAMP. WHEN NR 2 ENGINE WAS SHUT DOWN, THE ODOR WAS GONE. PERF FAULT CONFIRM AND RESTARTED NR 2 ENGING NIL ABNLR OR ODOR OBSERVED.
- [SDR 99FDEA00210](https://openairdocs.org/sdr/99FDEA00210.md): Smoke Detector · failed · Jun 10, 1999 · N418FE · Airbus A310222 · Smoke Detection
  > 99-129 AT 17,000 MSL, LT ECAM RED/CRC AVIONICS SMOKE NOT NOTICABLE FUMES/ODORS. REMOVED AND REPLACED 13WA SMOKE DETECTOR PER MM 26-15-12. OPS CK GOOD MM A310-26-15-00. OK FOR SERVICE.
- [SDR 98FDEA00120](https://openairdocs.org/sdr/98FDEA00120.md): Smoke Detector · defective · Feb 18, 1998 · N418FE · Airbus A310222 · Fire Detection
  > APPROACHING LEVEL OFF AT FL 370, FWD CARGO COMPT SMOKE LIGHT AND ASSOC ECAM CAUTIONS ACTIVATED. NR 1 BOTTLE WAS DISCHARGED AND NR 2 BOTTLE WAS ACTIVATED ON APPROACH. LIGHT WENT OUT AFTER DISCHARGE. REMOVED AND REPLACED SMOKE DET A AND B, OPS CHK NORMAL. IN
- [SDR 96FDEA01238](https://openairdocs.org/sdr/96FDEA01238.md): Hyd Line · leaking · Jul 11, 1996 · N418FE · Airbus A310221 · Hydraulic System, Main
  > STA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THAN HAT ARC. T/S FOUND HYD FLUID LEAKING FROM LT INSIDE WING SPAR BETWEEN PYLON AND 1ST FLAP TRACK IT IS A RIDGID LINE FOR AILERON DROOP RUBB

## 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 = 'N418FE' AND deregistration_id = 'N418FE-2016-02-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N418FE-2016-02-18/reports

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