# Service difficulty reports: N453FE

A list on [N453FE](https://openairdocs.org/aircraft/N453FE.md).

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

- [SDR FDEA201512194038](https://openairdocs.org/sdr/FDEA201512194038.md): Fairing · damaged · Dec 19, 2015 · N453FE · Airbus A310222 · Trailing Edge Flaps
  > LEFT WING INBD FLAP FAIRING HANGING DOWN ON ARRIVAL. RELEASED FOR SERVICE IAW CDL 27-01, B CATEGORY. FLAP TRACK FAIRING MISSING, REFER TO CDL 27-01-B FOR RESTRICTIONS. REMOVED LT WING FARING NR 2 WITH ASSOCIATED HARDWARE & SENT TO STRUCTURES FOR POSSIBLE RE
- [SDR FDEA201512023853](https://openairdocs.org/sdr/FDEA201512023853.md): Adapter · loose · Dec 2, 2015 · N453FE · Airbus A310222 · Fuel Indicating System
  > DEPARTED WITH 62,000 POUNDS OF FUEL, AT LANDING FUEL QTY INDICATES 61,400 POUNDS OF FUEL. REMOVED AND REPLACED LEFT OUTER ADAPTER PLUGS 42QT1 & 43QT1 PER AMM 28-42-37-04.
- [SDR FDEA201511043464](https://openairdocs.org/sdr/FDEA201511043464.md): Computer · failed · Nov 4, 2015 · N453FE · Airbus A310222 · Central Warning
  > SHORTLY AFTER CLEANUP ON TAKEOFF, MULTIPLE & VARIOUS AURAL & ECAM ALERTS & WARNINGS BEGAN. DECLARED AN EMER & RETURNED, WARNINGS CONTINUED ALL THE WAY TO BLOCK IN. REPLACED NR 1 AND NR 2 FLIGHT WARNING COMPUTERS 1WW1 & 1WW2 IAW AMM 31-53-34-04. PERFORMED FW
- [SDR FDEA201507092174](https://openairdocs.org/sdr/FDEA201507092174.md): Seat Track · damaged · Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > RAMP REPORTS AFT LOCK IN POSITION 8R LOOSE IN FLOOR, LATCH N1288. LATCH RESTRAINT DEVICE N1288 AT 8R INOPERATIVE, BROKEN OR MISSING. INSTALLED NEW SEAT TRACK SECTION IN IAW SRM 53-10-16. INSTALLED FLOORING & LOADING SYS IAW SRM 51-40-20.
- [SDR FDEA201507092173](https://openairdocs.org/sdr/FDEA201507092173.md): Seat Track · damaged · Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT POS 8R, LOCK S1288 TO HAVE SEAT TRACK LOBE DAMAGE CAUSING LOCK TO BE LOOSE. LOBE DAMAGE AT LOCK S1288 POS 8R, LOCK INSTALLED BUT LOOSE IN FLOOR. ACFT OK FOR SERVICE. RESTRAINT HAS BEEN REMOVED IAW SR 30-53-003 & MEL HAS BEEN APPLIED. REF WRI 25-5
- [SDR FDEA201505221623](https://openairdocs.org/sdr/FDEA201505221623.md): Switch · faulty · May 22, 2015 · N453FE · Airbus A310222 · Landing Gear Position and Warning
  > LOWERED GEAR, GOT SAFE INDICATION OF GEAR DOWN. A FEW SECONDS LATER GOT UNSAFE GEAR WARNING. LIGHT & HORN IN POS 2 SELECTED SYS 1 & THE LIGHT QAND WARNING HORN WENT OUT.. 3 GREEN DOWN INDICATIONS INSYS 1. SYS 2 HAD 2 GREEN LIGHTS FOR MAIN WHEELS AND NO G
- [SDR FDEA201502120515](https://openairdocs.org/sdr/FDEA201502120515.md): Engine · vibration · Feb 12, 2015 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, ACFT STARTED VIBRATING VERY BADLY. FELT MORE LIKE AN AIRFRAME FLUTTER RATHER THAN ENG VIBRATION. CHECKED ENG PAGE, ALL NORMAL. CLIMBING THROUGH 2500' PULLED THROTTLES BACK & FLUTTER DECREASED. AS SPEED STARTED TO INCREASE FLUTTER INCREASED. SL
- [SDR FDEA201407131756](https://openairdocs.org/sdr/FDEA201407131756.md): Damper · leaking · Jul 13, 2014 · N453FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > ON DEPARTURE LG WOULD NOT RETRACT. TRIED BOTH SYS 1 & SYS 2 & QRH, NO HELP. RT GEAR PITCH DAMPER POPPED WITH THE REAR SEAL BLOWN ALL THE WAY OUT. R & R RT MAIN GEAR PITCH DAMPER IAW AMM 32-11-15-04-01. FOUND RT MLG BOGIE SENSOR SUPPORT BROKEN CAUSING GEAR
- [SDR FDEA201406021269](https://openairdocs.org/sdr/FDEA201406021269.md): Skin · cracked · Jun 2, 2014 · N453FE · Airbus A310222 · Wing, Plate/Skin
  > POSSIBLE CRACK ON LT WING INBD SLAT CUT OUT, BOTH CORNERS. PERFORMED HFEC OF AREA IAW NTM 51-10-08 BLOCK 601, TWO CRACK INDICATIONS. REPAIRED AREAS, INSTALLED FILLERS AND DOUBLER IAW EA 6-5730-T0308606.
- [SDR FDEA201310062421](https://openairdocs.org/sdr/FDEA201310062421.md): Lug · damaged · Oct 6, 2013 · N453FE · Airbus A310222 · Wing, Attach Fittings
  > LEFT MLG WW RIB 5 FITTING FWD LUG DAMAGED. REPAIRED IAW EA 6-5750-T0302477 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- [SDR FDEA201310042404](https://openairdocs.org/sdr/FDEA201310042404.md): Lug · corroded · Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous Structure
  > CORROSION WAS FOUND ON THE LUG BORE AND AFT SPOTFACE OF RT RIB5 FWD LUG. ACCOMPLISHED CORROSION REPAIR IAW GMM 6-2-100 REPAIR CLASSIFIEID AS MINOR.
- [SDR FDEA201310042403](https://openairdocs.org/sdr/FDEA201310042403.md): Lug · corroded · Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous Structure
  > CORROSION WAS FOUND ON LUG BORE AND FWD SPOTFACE OF LT RIB 5. ACCOMPLISHED THE CORROSION REPAIR IAW GMM 6-2-100, IAW EA 6-5750-T0302477 P1. REPAIR CLASSIFED AS MINOR.
- [SDR FDEA201309302338](https://openairdocs.org/sdr/FDEA201309302338.md): Beam · cracked · Sep 30, 2013 · N453FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > THREE CRACKS WERE FOUND AT LT INNER LONGITUDINAL BEAM FLANGE STR 11 BETWEEN FRAMES 73A AND 74A. CUT OUT DAMAGE PORTION OF BEAM AND REWORK MILLED STEP. INSTALL THE REPAIR ANGLE AND FILLER IAW SRM 53-18-18, FIG 205A.
- [SDR FDEA201309232283](https://openairdocs.org/sdr/FDEA201309232283.md): Floor Panel · damaged · Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 132RF IN LOWER FWD CARGO BAY WAS FOUND SOFT. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201309232282](https://openairdocs.org/sdr/FDEA201309232282.md): Floor Panel · dented · Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 162HF IN BULK CARGO, FOUND SERIOUS DENT IN SKIN. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201005031430](https://openairdocs.org/sdr/FDEA201005031430.md): Crease Beam · corroded · May 3, 2010 · N453FE · Airbus A310222 · Fuselage Main, Structure
  > L-3 DOOR INBD CREASEBEAM CORRODED AT STA 1348 LBL 60. REMOVED CORROSION FROM LT SIDE IB CREASE BEAM CHORD AT STA 1290-1370 IAW SRM 51- 10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 FIG 101 DETAIL VII. ORIG MATERIAL.100 AFTER REWORK.083 L=1.0 W=1.0.
- [SDR FDEA201003240978](https://openairdocs.org/sdr/FDEA201003240978.md): Pressure Switch · failed · Mar 24, 2010 · N453FE · Airbus A310222 · Engine Fuel Distribution
  > T/O, 1 MIN NR 1 ENG FUEL FILTER CLOG LT ILLUMINATED FOLLOWED QRH NO RELIEF RTB LAND WT 271.5K LBS. RELEASED FOR SERVICE IAW MEL: 73-36-03-01. ONCE EACH FLIGHT DAY." NR 1 ENG FUEL FILTER INSPECTED & NO CONTAMINATION FOUND. R & R FUEL FILTER IAW AMM 73-12-0
- [SDR FDEA201003210950](https://openairdocs.org/sdr/FDEA201003210950.md): Switch · inoperative · Mar 21, 2010 · N453FE · Airbus A310222 · Engine Fuel Distribution
  > NR 1 ENG FUEL FILTER CLOG AT 19000 FT IN CLIMB - RETURNED PWR TO IDLE. WARNING REMAINING ON. MEL 21MAR10 RELEASED FOR SERVICE IAW MEL: 73-36-03-02 CATEGORY: C EXPIRATION: 31MAR10 NR1 ENG FUEL FILTER INSPECTED & NO CONTAMINATION FOUND. REPLACED FUEL FILTER
- [SDR FDEA201001210207](https://openairdocs.org/sdr/FDEA201001210207.md): Actuator · damaged · Jan 21, 2010 · N453FE · Airbus A310222 · Drag Control System
  > DURING T/S FOUND RT NR 2 SPEEDBRAKE ACTUATOR'S ROD END BROKEN ALSO THE INBD FLAP NEAR THE SPEEDBRAKE ACTUATOR DAMAGED ABOUT 2IN X 1.5 IN. R & R RT INBD FLAP VANE IAW AMM 27-50-11-4. OPS CHECK NORMAL. REF DISCREPANCY 2760 9380 FOR SPEEDBRAKE ACTUATOR CHA
- [SDR FDEA200909113287](https://openairdocs.org/sdr/FDEA200909113287.md): Switch · inoperative · Sep 11, 2009 · N453FE · Airbus A310222 · Central Warning
  > 45 MINS AFTER T/O DEPARTUE AT FL 340, NR 2 OIL CLOG LIGHT ILLUMINATED. FOLLOWED QRH PROC, SHUTDOWN NR 2 ENG AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. RAN NR 2 ENG IAW JRH - NO " OIL
- [SDR FDEA200902250721](https://openairdocs.org/sdr/FDEA200902250721.md): Smoke Warning · false activation · Feb 25, 2009 · N453FE · Airbus A310322 · Smoke Detection
  > JUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP FAULT, BOTH A AND B ON AFT DECK, MAIN DECK CARGO SMOKE ILLUMINATED AND REMAINED ON. JUST PRIOR T
- [SDR FDEA200902250720](https://openairdocs.org/sdr/FDEA200902250720.md): Smoke Warning · false activation · Feb 25, 2009 · N453FE · Airbus A310222 · Smoke Detection
  > JUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP FAULT, BOTH A AND B ON AFT DECK, MAIN DECK CARGO SMOKE ILLUMINATED AND REMAINED ON. JUST PRIOR TO
- [SDR FDEA200812175191](https://openairdocs.org/sdr/FDEA200812175191.md): Control Module · malfunctioned · Dec 17, 2008 · N453FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > AFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR PWR SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS AND RETRACT CTL CB OF LDG PROX DETECTOR POPPED OUT. FOLLOWED T/S PER TSM 32-30-00 FIG 1
- [SDR FDEA200812175188](https://openairdocs.org/sdr/FDEA200812175188.md): Control Handle · failed · Dec 17, 2008 · N453FE · Airbus A310222 · Landing Gear Selector
  > AFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR PWR SUPPLY 1 LOSS. INTERROGATED MTP AND GOT 28V GEAR POWER SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS & RETRACT CONTROL C/B OF MLG PROX
- [SDR FDEA200811134875](https://openairdocs.org/sdr/FDEA200811134875.md): Attach Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.
- [SDR FDEA200811134874](https://openairdocs.org/sdr/FDEA200811134874.md): Attach Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.
- [SDR FDEA200811134873](https://openairdocs.org/sdr/FDEA200811134873.md): Attach Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. FREE OF CRACK AT THE REWORKED AREA. REMAINING THICKNESS IS 0.481 INCH, IT IS WITHIN LIMIT PER SRM 55-30-0
- [SDR 08FDEA04875](https://openairdocs.org/sdr/08FDEA04875.md): Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION.
- [SDR 08FDEA04874](https://openairdocs.org/sdr/08FDEA04874.md): Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION.
- [SDR 08FDEA04873](https://openairdocs.org/sdr/08FDEA04873.md): Attach Fitting · corroded · Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION.
- [SDR FDEA200811124869](https://openairdocs.org/sdr/FDEA200811124869.md): Bellcrank · corroded · Nov 12, 2008 · N453FE · Airbus A310222 · Rudder Structure
  > NR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21. PERFORM RUDDER MECHANICAL CONTROL OPERATIONAL AND FUNCTIONAL TEST PER AMM 27-21-00-5.
- [SDR FDEA200811124868](https://openairdocs.org/sdr/FDEA200811124868.md): Attach Fitting · corroded · Nov 12, 2008 · N453FE · Airbus A310222 · Rudder/Tab, Attach Fittings
  > RUDDER, NR 1 ATTACH FITTING HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21.
- [SDR 08FDEA04869](https://openairdocs.org/sdr/08FDEA04869.md): Bellcrank · corroded · Nov 12, 2008 · N453FE · Airbus A310222 · Rudder Control System
  > NR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION.
- [SDR 08FDEA04868](https://openairdocs.org/sdr/08FDEA04868.md): Attach Fitting · corroded · Nov 12, 2008 · N453FE · Airbus A310222 · Rudder Structure
  > RUDDER, NR 1 ATTACH FITTING HAS CORROSION.
- [SDR FDEA200811104881](https://openairdocs.org/sdr/FDEA200811104881.md): Engine · inoperative · Oct 10, 2008 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > ENG NR 2 FAILURE DURING CLIMB-OUT. CLIMB POWER PASSING 1800 FT, FELT SHUDDER, HEARD A BANG, HAD YAW. COMPLETED SINGLE ENGINE LANDING. NO SMOKE OR FIRE PULLED NR 2 ENG FIRE HANDLE AND AGENT 1 DISCHARGED. EGT SPIKE TO 780. R AND I NR 2 ENGINE AND PERFORMED
- [SDR 08FDEA01206](https://openairdocs.org/sdr/08FDEA01206.md): O-Ring · leaking · Mar 30, 2008 · N453FE · Airbus A310222 · Drag Control System
  > DURING CRUISE GREEN SYSTEM LOW QUANTITY ALERT. LOSS OF GREEN HYD KRUEGER FLAP ALERT DURING APPROACH. CREW DECLARED FOR EMERGENCY LANDING. ACCORDING TO CREW THE A/C LANDED SMOOTHLY AT WSSS 02L AND NO OVERWEIGHT. THE GREEN HYD FLUID QTY INDICATION AT LOWER
- [SDR 07FDEA05007](https://openairdocs.org/sdr/07FDEA05007.md): Switch · loose · Dec 5, 2007 · N453FE · Airbus A310222 · Engine Thrust Reverser
  > DURING TAKEOFF ROLL WITH POWER ADVANCING TO TAKEOFF POWER (MAX), THE NR 2 REV UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS REJECTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15DEC07, SFS BKK/06 T/S FOUND ENG NR 2 RT STOW SWITCH
- [SDR 07FDEA02876](https://openairdocs.org/sdr/07FDEA02876.md): Pitot Head · obstructed · Aug 14, 2007 · N453FE · Airbus A310222 · Pitot/Static System
  > REJECTED TAKEOFF AT APPROX 90 KNOTS DUE TO NO F/O A/S. FOUND BUG DEBRIS IN F/O PITOT PROBE CLEANED. INSPECTED PROBE PER AMM 34-11-15-6, NO DEFECTS NOTED. F/O'S AIRSPEED CHECKED GOOD WITH PITOT TESTER. INSPECTED A/C BRAKES PER AMM 05-51-16-0. NO DEFECTS NO
- [SDR 06FDEA2677](https://openairdocs.org/sdr/06FDEA2677.md): Stringer · corroded · Jul 25, 2006 · N453FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > AVIONICS COMPART RT SIDE CORRSION ON STR 44R AT FR 17R REF N00188. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 51-10-17 REPAIRED IAW EA 6-5310-102502.
- [SDR 06FDEA2625](https://openairdocs.org/sdr/06FDEA2625.md): Adapter · corroded · Jul 18, 2006 · N453FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > CLS ADAPTER AT FR 46 BETWEEN SEAT TRACK R2 & R3 BENT REF N00300. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.
- [SDR 06FDEA2623](https://openairdocs.org/sdr/06FDEA2623.md): Seat Track · gouged · Jul 18, 2006 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK R2 & R3 HAS GOUGE IN SCALLOP REF N00298. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.
- [SDR 04FDEA02606](https://openairdocs.org/sdr/04FDEA02606.md): Fairing · cracked · Sep 2, 2004 · N453FE · Airbus A310 · Aerodynamic Fairings
  > SMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENANCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DATE:01AUG04 AT: LIS-VN
- [SDR 04FDEA02593](https://openairdocs.org/sdr/04FDEA02593.md): Seal · worn · Sep 1, 2004 · N453FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND DAMAGED DRIP PAN SEAL AND WORN SUPPORT HOLES ON PANEL 147CZ AND 148CZ. GEN ITEM 41C0508. PANELS REPAIRED ON N00056 AND N00057 PER EA 6-5315-81014.
- [SDR 04FDEA01541](https://openairdocs.org/sdr/04FDEA01541.md): Cable · out of rig · May 31, 2004 · N453FE · Airbus A310222 · Power Lever
  > ON TAKEOFF NR 2 THROTTLE WOULD NOT GO PAST V2WAY, DUE TO BINDING. ABORTED BELOW 70 KTS. RETURNED TO GATE. THROTTLE LEVER FEEDBACK CABLE MECHANISM FOUND OUT OF RIGGING RANGE. T/L FEEDBACK MECHANISM RIGGED IAW MM 78-31-38-2.
- [SDR 01FDEA00860](https://openairdocs.org/sdr/01FDEA00860.md): Engine · malfunctioned · Sep 27, 2001 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > 01-324 ON T/O NR 2 ENGINE N1 STAGNATED & W/N ACCELERATE PAST 49 PERCENT, ALL PARAMETERS NORMAL AND PROCEEDED TO T/O.
- [SDR 00FDEA00862](https://openairdocs.org/sdr/00FDEA00862.md): Warning Light · illuminated · Dec 8, 2000 · N453FE · Airbus A310222 · Engine Thrust Reverser
  > 00-344 ON T/O ROLL NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. ** S/D ** COMING
- [SDR 00FDEA00200](https://openairdocs.org/sdr/00FDEA00200.md): Skin · damaged · Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FRAME 19/20, STR 29-31 RT DAMAGED FUSELAGE SKIN AT ACCESS DOOR CONTROL PNL CORNERS. BLEND OUT DAMAGE IAW THE REFERENCED DWG EFW 632-99 & PROTECT SURFACE AP SRM.
- [SDR 00FDEA00199](https://openairdocs.org/sdr/00FDEA00199.md): Skin · cracked · Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FRAME 79, STR 10 LT/RT DENTS ON OUTER FUSELAGE SKIN MAX DENT DEPT 1.3 MM LT AND 0.9 MM RT. REMOVED AND REPLACED DAMAGE PER SRM DWG TD/K4/51/11742/1999.
- [SDR 00FDEA00198](https://openairdocs.org/sdr/00FDEA00198.md): Skin · cracked · Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FRAME 54.1-54.2, STR 39-41 LT EXT FUSELAGE SKIN CRACKED. REMOVED AND REPLACED REINFORCEMENT DOUBLER (16R539H0126) PER DWG 16R539H0111, SHEET 2 IAW DWG 74626/99-04 PC.

## 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 = 'N453FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N453FE/reports

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