# Service difficulty reports: N420FE, cancelled Sep 17, 2009

A list on [N420FE, cancelled Sep 17, 2009](https://openairdocs.org/deregistered/N420FE-2009-09-17.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 · 68 reports

- [SDR 08FDEA04730](https://openairdocs.org/sdr/08FDEA04730.md): Skin · damaged · Nov 5, 2008 · N420FE · Airbus A310 · Rudder, Plate/Skin
  > THERMOGRAPHY INSPECTION OF RUDDER S/N HF1005 SHOWS 3 AREAS OF POSSIBLE DEFECTS, LT SIDE- CONFIRMED BY ULTRASONIC INSP. DEFECTS AT NEAR FASTENERS 9,13 AND 20 COUNTED FROM TOP OF RUDDER REMOVED DAMAGED AREAS AND REPAIRED LT SIDE OF RUDDER IAW EA 6-5540-118
- [SDR 07FDEA02788](https://openairdocs.org/sdr/07FDEA02788.md): Skin · debonded · Jul 31, 2007 · N420FE · Airbus A310222 · Trailing Edge Flaps
  > RT WING, INBD FLAP WITH DEBONDING T/E BETWEEN RIB 14 AND RIB 15. IT WAS REPAIRED IN ACCORDANCE WITH SRM 57-52-12.
- [SDR 07FDEA02735](https://openairdocs.org/sdr/07FDEA02735.md): Seat Track · cracked · Jul 25, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.
- [SDR 07FDEA02734](https://openairdocs.org/sdr/07FDEA02734.md): Seat Track · cracked · Jul 25, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > NR 2 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-450 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.
- [SDR 07FDEA02733](https://openairdocs.org/sdr/07FDEA02733.md): Seat Track · cracked · Jul 25, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > NR 2 LT SEAT-TRACK BETWEEN FR 38.2 AND FR40 AT Y450 FOUND CRACKED. IT WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.
- [SDR 07FDEA02731](https://openairdocs.org/sdr/07FDEA02731.md): Seat Track · cracked · Jul 25, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > NR 3 LT SEAT-TRACK, BETWEEN FR 38.2 AND FR 40 AT Y953, FOUND CRACKED. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-15-15.
- [SDR 07FDEA02790](https://openairdocs.org/sdr/07FDEA02790.md): Frame · cracked · Jul 20, 2007 · N420FE · Airbus A310222 · Horizontal Stabilizer Structure
  > ELEVATOR - ARTIFICIAL FELL UNIT LOWER FRAME FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH AMM27-31-26 AND FEDEX EA 6-2730-113153.
- [SDR 07FDEA02754](https://openairdocs.org/sdr/07FDEA02754.md): Seat Track · corroded · Jul 13, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > N00738 MDCC - SEAT TRACK AT Y-953 BETWEEN FR 45 AND FR 54 FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02750](https://openairdocs.org/sdr/07FDEA02750.md): Seat Track · corroded · Jul 13, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > N00736 MDCC - SEAT TRACK AT Y0 FOUND CORRODED BETWEEN FR 45 AND FR 54. SEAT TRACK REPLACED IN ACCORDANCE SRM 51-72-10.
- [SDR 07FDEA02749](https://openairdocs.org/sdr/07FDEA02749.md): Seat Track · corroded · Jul 13, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC - SEAT TRACK AT Y-450 FOUND CORRODED BETWEEN FR 45 AND 54. THE PART WAS REPAIRED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6- 5310-113152.
- [SDR 07FDEA02776](https://openairdocs.org/sdr/07FDEA02776.md): Adapter · cracked · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > MDCC - CLS ADAPTER AT FR38 BETWEEN Y-450 AND Y-950 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02775](https://openairdocs.org/sdr/07FDEA02775.md): Adapter · cracked · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > MDCC - CLS ADAPTER AT FR 36 BETWEEN Y1456 AND Y1459 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02774](https://openairdocs.org/sdr/07FDEA02774.md): Seat Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC - SEAT TRACK WITH CORROSION BETWEEN FR18 AND FR19 AT Y950. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02751](https://openairdocs.org/sdr/07FDEA02751.md): Seat Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > N00547 MDCC - SEAT TRACK AT YO FOUND CORRODED BETWEEN FR 58 AND FR 72. SEAT TRACK WAS REPAIRED IN ACCORDANCE SRM 53-10-16 FIG 202.
- [SDR 07FDEA02701](https://openairdocs.org/sdr/07FDEA02701.md): Seat Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY-TRACK AT Y-1456 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.
- [SDR 07FDEA02700](https://openairdocs.org/sdr/07FDEA02700.md): Seat Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY-TRACK Y-953 BETWEEN FR 4 AND FR 54.2 WITH CORROSION AND CRACK AT KIT CARGO ATTACHMENT AREA. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.
- [SDR 07FDEA02699](https://openairdocs.org/sdr/07FDEA02699.md): Seat Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY TRACK Y-450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.
- [SDR 07FDEA02698](https://openairdocs.org/sdr/07FDEA02698.md): Track · corroded · Jul 12, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY TRACK Y450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. IT WAS REPLACED IAW SRM 53-15-16.
- [SDR 07FDEA02789](https://openairdocs.org/sdr/07FDEA02789.md): Skin · misrepaired · Jul 10, 2007 · N420FE · Airbus A310222 · Trailing Edge Flaps
  > PREVIOUS REPAIR LOCATED ON LT OUTBD FLAP, RIB 2/3 (UPPER SKIN). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS
- [SDR 07FDEA02777](https://openairdocs.org/sdr/07FDEA02777.md): Skin · misrepaired · Jul 10, 2007 · N420FE · Airbus A310222 · Trailing Edge Flaps
  > PREVIOUS REPAIR FOUND LOCATED ON INBD FLAP, RIB 2/4 (UPPER SKIN, TRALING EDGE). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM. NEW REPAIR ACCOMPLISHED
- [SDR 07FDEA02773](https://openairdocs.org/sdr/07FDEA02773.md): Adapter · cracked · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y953 AND Y1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02772](https://openairdocs.org/sdr/07FDEA02772.md): Adapter · cracked · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM.
- [SDR 07FDEA02771](https://openairdocs.org/sdr/07FDEA02771.md): Adapter · cracked · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > MDCC - CLS ADAPTER ON CABIN FLOOR FR 37 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02753](https://openairdocs.org/sdr/07FDEA02753.md): Seat Track · cracked · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > N00568 MDCC - SEAT TRACK AT Y1447 BETWEEN FR 74 AND FR 78 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02752](https://openairdocs.org/sdr/07FDEA02752.md): Seat Track · corroded · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > N00577 MDCC - SEAT TRACK FOUND CORRODED AT Y1137 BETWEEN FR74/80. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.
- [SDR 07FDEA02696](https://openairdocs.org/sdr/07FDEA02696.md): Frame · corroded · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, CORROSION FOUND ON FR 59, BETWEEN STR 28 AND 30 RH. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-13-13 FIG 202 AND FEDEX ENGINEERING AUTHORIZATION EA 6-5310-112435.
- [SDR 07FDEA02641](https://openairdocs.org/sdr/07FDEA02641.md): Skin · misrepaired · Jul 10, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, PREVIOUS REPAIR FOUND LOCATED ON FR 74/75 AND STR 41/44 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR W
- [SDR 07FDEA02617](https://openairdocs.org/sdr/07FDEA02617.md): Panel · cracked · Jul 10, 2007 · N420FE · Airbus A310222 · Nacelle/Pylon, Plate/Skin
  > PYLON NR 2, RIB 8 LT WITH CRACK AT UPPER AREA. IT WAS REPAIRED IN ACCORDANCE WITH SRM 54-51-31 FIG 201.
- [SDR 07FDEA02697](https://openairdocs.org/sdr/07FDEA02697.md): Skin · misrepaired · Jul 9, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON CENTER LINE, FR 1/2 UPPER CL. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW R
- [SDR 07FDEA02682](https://openairdocs.org/sdr/07FDEA02682.md): Skin · misrepaired · Jul 9, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT, FR 17/18 AND STGR26/27. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REP
- [SDR 07FDEA02640](https://openairdocs.org/sdr/07FDEA02640.md): Skin · misrepaired · Jul 9, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT FR360/61 AND STGR 42/43. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVAL. THE EXISTING REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM RE
- [SDR 07FDEA02695](https://openairdocs.org/sdr/07FDEA02695.md): Skin · worn · Jul 6, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FUSELAGE, MISSING MATERIAL AT AFT CARGO COMPARTMENT DOOR LOWER FORWARD FRAME SKIN SURFACE AT FRAME 59A AND BETWEEN STR 41 AND 43 RT. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-17-12 AND EA 6-5310-112433.
- [SDR 07FDEA02643](https://openairdocs.org/sdr/07FDEA02643.md): Floorbeam · cracked · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FR 37 BETWEEN Y1456 AND Y1959. IT WAS REPAIRED IAW FEDEX EA 6-5310-112431.
- [SDR 07FDEA02642](https://openairdocs.org/sdr/07FDEA02642.md): Skin · gouged · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FUSELAGE, RT FUSELAGE SKIN SURFACE WITH MISSING MATERIAL BETWEEN FR 25 AND 26/32 AT STR 29 RT AN APPROVAL FOR THE MISSING MATERIAL WAS OBTAINED. FEDEX EA 6-5330-113154 WAS ACCOMPLISHED.
- [SDR 07FDEA02639](https://openairdocs.org/sdr/07FDEA02639.md): Floorbeam · cracked · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FRAME 36 BETWEEN Y450 AND Y953. IT WAS REPAIRED IAW SRM SUPP 53-10-15 FIG 201 SHEET 2.
- [SDR 07FDEA02623](https://openairdocs.org/sdr/07FDEA02623.md): Floorbeam · cracked · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, CABIN FLOOR CROSSBEAM CRACKED AT FR 33 BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 4A.
- [SDR 07FDEA02621](https://openairdocs.org/sdr/07FDEA02621.md): Floorbeam · cracked · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FRAME 25 BETWEEN Y- 450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 4A.
- [SDR 07FDEA02619](https://openairdocs.org/sdr/07FDEA02619.md): Floorbeam · cracked · Jun 29, 2007 · N420FE · Airbus A310222 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FR21, BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 2.
- [SDR 05FDEA04112](https://openairdocs.org/sdr/05FDEA04112.md): Sequence Valve · malfunctioned · Dec 4, 2005 · N420FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > RIGHT LANDING GEAR TAKES 10 SECONDS LONGER THAN THE LEFT GEAR TO RETRACT. ECAM GEAR NOT YET WARNING FOR ABOUT 2 SECONDS. THEN NORMAL OPS WHEN GEAR EXTENDED. CLEANED RESTRICTOR VALVE. REPLACED MAINGEAR ACTUATIN G ASSEMBLY RH IAW AMM 32-31-46. REPLACED LA
- [SDR 05FDEA02042](https://openairdocs.org/sdr/05FDEA02042.md): Fire Loop · damaged · Jul 19, 2005 · N420FE · Airbus A310 · Fire Detection
  > AFTER T/O AT 15000FT, RECEIVED FIRE WARNING ON ENGINE NR 2. DID PROCEDURES AND RETURNED TO LLBG. TLV U-INSPECTION & T/S PERFORMED ON MTSI 26-10/9536. FIXED DIFFERED LOOP-B, FOUND TWO PLUGS ON LOOP-A SENSING ELEMENTS IN BAD CONDITION (ONE WITH RUBBER ISOL
- [SDR 05FDEA00546](https://openairdocs.org/sdr/05FDEA00546.md): Line · leaking · Mar 15, 2005 · N420FE · Airbus A310222 · Hydraulic System, Main
  > AFTER GEAR EXTENSION GOT GREEN HYDRO SYS LOW AIR PRESSURE LIGHT. DECLARED AN EMERGENCY AND LANDED STRAIGHT AHEAD. AFTER LANDING LOW AIR LIGHT WENT OUT. TURNED BOTH GREEN PUMPS BACK ON IAW QRH. GREEN SYSTEM RECOVERED AND CLEARED THE RUNWAY. GREEN HYD SYSTE
- [SDR 05FDEA00281](https://openairdocs.org/sdr/05FDEA00281.md): Skin · damaged · Feb 13, 2005 · N420FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > ACCOMPLISH MAINTENANCE C-CHECK, DURING AGING AIRCRAFT INSPECTION AN EXISTING REPAIR DOUBLER WAS FOUND ON THE LOWER FWD CARGO DOOR. DOUBLER WAS REMOVED DURING C4 CHECK AT LIS SCRATCH MARK BLENDED. HFEC INSPECTION OF THE AREA. NEW FASTENERS PAINTED.
- [SDR 05FDEA00083](https://openairdocs.org/sdr/05FDEA00083.md): Warning Light · illuminated · Jan 12, 2005 · N420FE · Airbus A310222 · Engine Thrust Reverser
  > NR 2 ENG REV GREEN LIGHT WITH ECAM WARNING AFTER T/O. NO BUFFETING. AIR TURNBACK TO LIM. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C. ENGINE 2, THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. T/R VISUALLY INSPECTED, NO D
- [SDR 04FDEA01635](https://openairdocs.org/sdr/04FDEA01635.md): Fitting · corroded · Jun 8, 2004 · N420FE · Airbus A310222 · Horizontal Stabilizer, Attach Fittings
  > A/C 420 WAS IN FOR B-CHECK, FOUND VERT STAB FITTING HAD CORROSION. REMOVED AND REPLACED VERT STAB FITTING.
- [SDR 03FDEA00545](https://openairdocs.org/sdr/03FDEA00545.md): Indicator · inoperative · Apr 18, 2003 · N420FE · Airbus A310 · Engine EGT/TIT Indicating System
  > ON ROTATION ECAM WARNING ACTIVATED AND NR 1 ENGINE EGT SPIKES TO OVER 900 DEG AND NR 1 ENG N2 SPIKES TO NEAR 119 PERCENT. RETURN FOR LANDING WITH NR 1 ENG AT IDLE. REMOVED AND REPLACED NR 1 EGT INDICATOR AND NR 1 N2 INDICATOR PER A310 MM 77-21-21-4 AND MM 77
- [SDR 02FDEA00699](https://openairdocs.org/sdr/02FDEA00699.md): Actuator · malfunctioned · Sep 25, 2002 · N420FE · Airbus A310 · Rudder Actuator
  > RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, FAULTED PASSING 170KIAS. REPLACED NR 2 ADC PER A310 MM34-11-34. OPERATIONAL CHECK AND PITOT/STATIC LEAK TEST GOOD. R&R RUDDER VARIABLE STOP ACTUATOR AS PER A-310, MM 27-23-23-4. R&R NR 1 FEEL LIMITATION COMPUTER
- [SDR 02FDEA00684](https://openairdocs.org/sdr/02FDEA00684.md): Relay · failed · Sep 24, 2002 · N420FE · Airbus A310 · Rudder Control System
  > RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, WOULD NOT RESET. RUDDER TRAVEL SYSTEM ONE ALREADY DEFERRED. CHECKED FAULT AT FLC NR 2 RUDDER TRAVEL POWER LOOP. PERFORMED T/S PER TSM 27-23-03 REPLACED 309 CY2 RELAY, BITE TEST FLC NR 2 PER MM 27-23-00. OK, NO FA
- [SDR 02FDEA00583](https://openairdocs.org/sdr/02FDEA00583.md): Torque Box · corroded · Aug 13, 2002 · N420FE · Airbus A310 · Fuselage Main, Structure
  > CORROSION AROUND FASTENER HEADS IN AVIONICS COMPT NOSE GEAR WHEEL WELL TOP TORQUE BOX (FROM FRAME 13 TO 15A).
- [SDR 02FDEA00538](https://openairdocs.org/sdr/02FDEA00538.md): Actuator · damaged · Aug 1, 2002 · N420FE · Airbus A310222 · Stabilizer Actuator
  > THS ACTUATOR LWR CLAW STOP RUBBER BUFFER BETWEEN INNER & OUTER RACE SHOWS AXIAL MIGRATION OF 5 MM. THS ACTUATOR SCREW THREAD HAS SCRATCH MARK ON UPPER FACE 27.5 CM ABOVE LWR CLAW STOP. REMOVED AND REPLACED ACTUATOR PER AMM 27-44-11-4.
- [SDR 02FDEA00537](https://openairdocs.org/sdr/02FDEA00537.md): Control Cable · corroded · Aug 1, 2002 · N420FE · Airbus A310222 · Elevator Control System
  > CAPT SIDE & COPILOT SIDE ELEVATOR CONTROL CABLES CORRODED AT PULLEYS IN STAB COMPARTMENT. REMOVED AND REPLACED CABLES PER AMM 27-30-00-4.

Next page: https://openairdocs.org/deregistered/N420FE-2009-09-17/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 = 'N420FE' AND deregistration_id = 'N420FE-2009-09-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N420FE-2009-09-17/reports

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