# Service difficulty reports: N811FD, cancelled Mar 2, 2024

A list on [N811FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N811FD-2024-03-02.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 3 · 123 reports

- [SDR FDEA201903010528](https://openairdocs.org/sdr/FDEA201903010528.md): Linkage · broken · Mar 1, 2019 · N811FD · Airbus A310324 · Landing Gear Retraction/Extension System
  > PDIS 811 32-30 4584 01MAR19 GRR DURING LANDING GEAR RETRACTION. L/G RETRACTION FAULT. THE LEFT GEAR DOOR AMBER LIGHT WAS LIT AND THE RED UNLOCKED LIGHT WAS LIT. FOLLOWED QRH ECAM. RETURNED TO KGRR. FACT 02MAR19 23:19 GRR JACKED AIRCRAFT REF 07-11-00-00. C
- [SDR FDEA201901030010](https://openairdocs.org/sdr/FDEA201901030010.md): Actuator · malfunctioned · Jan 3, 2019 · N811FD · Airbus A310324 · Drag Control Actuator
  > AT FL340 GOT YELLOW SYS HYD RESERVOIR ECAM WITH CONFIRMED LOW QTY. EMER RTN TO MEM. COMPLETED INSTALL OF #4 LH SPOILER ACTUATOR REFERENCE AIRBUS A310-300 AMM 27-64-14-04. OPERATION T
- [SDR FDEA2018121863510](https://openairdocs.org/sdr/FDEA2018121863510.md): Circuit Breaker · burned · Dec 16, 2018 · N811FD · Airbus A300* · AC Power Distribution System
  > 811 24-50 4376 15DEC18 MEM FACT LOGPAGES:3011783 DURING APPROACH PHASE, RECEIVED "BUS 2 FAIL". COMPLIED WITH QRH. FOUND HEAT DAMAGE ON C/B 2XN. R&R'D C/B 2XN PA
- [SDR FDEA201709182589](https://openairdocs.org/sdr/FDEA201709182589.md): Stiffener · corroded · Sep 18, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > LOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201709132525](https://openairdocs.org/sdr/FDEA201709132525.md): Stiffener · corroded · Sep 13, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > LOWER SKIN STIFFENER CORRODED,BETWEEN FRAMES 43 AND 47, Y-1456. COMPLIED WITH EA 6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201709072463](https://openairdocs.org/sdr/FDEA201709072463.md): Stringer · damaged · Sep 7, 2017 · N811FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > AFT CABIN UNDERFLOOR COMPT FR74-FR75, S45R STRINGER 1EA FASTENER HOLE DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75,S-45R STRINGER 1EA FASTENER HOLE DAMAGED. REPAIRED THE DAMAGED STRINGER PER SRM53-10-14 FIG 201 SHT 2 VIEW H & J.
- [SDR FDEA201708282387](https://openairdocs.org/sdr/FDEA201708282387.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 1 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282385](https://openairdocs.org/sdr/FDEA201708282385.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 4 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282384](https://openairdocs.org/sdr/FDEA201708282384.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 10 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282383](https://openairdocs.org/sdr/FDEA201708282383.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 52 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282382](https://openairdocs.org/sdr/FDEA201708282382.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 60 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282381](https://openairdocs.org/sdr/FDEA201708282381.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > LEFT REAR SPAR INTERNAL ANGLE NR 62 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282380](https://openairdocs.org/sdr/FDEA201708282380.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > RIGHT REAR SPAR INTERNAL ANGLE NR 2 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282379](https://openairdocs.org/sdr/FDEA201708282379.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > RIGHT REAR SPAR INTERNAL ANGLE NR 8 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282378](https://openairdocs.org/sdr/FDEA201708282378.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar
  > RIGHT REAR SPAR INTERNAL ANGLE, NR 14 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708282377](https://openairdocs.org/sdr/FDEA201708282377.md): Frame Angle · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Fuselage Main, Frame
  > RIGHT REAR FRAME INTERNAL ANGLE NR 23 HOLE, NDT INSPECTION FOUND A CRACK. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201703180949](https://openairdocs.org/sdr/FDEA201703180949.md): Aoa · malfunctioned · Mar 18, 2017 · N811FD · Airbus A310324 · Stall Warning System
  > DURING CLIMB THRU FL 340, PROBES & STAT ALPHA CONTROL CIRCUIT BREAKER TRIPPED. MULTIPLE PROBE HT FAILS. FOLLOWED ECAM & QRH PROCEDURES. ATS LEVER TRIPPED OFF IN SEQUENCE WITH THE NR 2 ENGINE LIGHT. R & R RELAY LT 213 IAW WDM 30-31-04. DURING OPS CHECK IAW
- [SDR FDEA201701050043](https://openairdocs.org/sdr/FDEA201701050043.md): Limit Switch · failed · Jan 5, 2017 · N811FD · Airbus A310324 · Door Warning System
  > WHILE TROUBLE SHOOTING R1 DOOR ARMING PROBLEM, SLIDE TRIED TO DEPLOY. REMOVED AND REPLACED RI DOOR LIMIT SWITCH 14WN AND TESTED IAW AMM 52-73-13-04-09.
- [SDR FDEA201701050045](https://openairdocs.org/sdr/FDEA201701050045.md): Switch · malfunctioned · Jan 5, 2017 · N811FD · Airbus A310324 · Escape Slide
  > R1 SLIDE INDICATOR WAS BLINKING ON & OFF AT BLOCK IN PRIOR TO DISARMING. R & R THE R1 DOOR LIMIT SWITCH 14WN.
- [SDR FDEA201701050044](https://openairdocs.org/sdr/FDEA201701050044.md): Slide · unknown · Jan 5, 2017 · N811FD · Airbus A310324 · Escape Slide
  > DURING TROUBLESHOOTING OF THE R1 DOOR ARMING PROBLEM, THE SLIDE TRIED TO DEPLOY. COMPLIED WITH R1 SLIDE REMOVAL ONLY IAW EA 6-5210-T0330666 PART 1.
- [SDR FDEA201612314582](https://openairdocs.org/sdr/FDEA201612314582.md): Relay · failed · Dec 31, 2016 · N811FD · Airbus A310324 · Door Warning System
  > R1 SLIDE INDICATION FLASHES CONTINUOUSLY WHEN SLIDE IS ARMED ON RIGHT ECAM. RELEASED FOR SERVICE PER MEL 52-30-04. REMOVED AND REPLACED RELAYS 9ES AND 10ES REF ESPM 20-46-50. PERFORMED ADJUSTMENT TEST OF ESCAPE SLIDE WARNING REF MM 52-73-00-05. OPS CK OK O
- [SDR FDEA201612034317](https://openairdocs.org/sdr/FDEA201612034317.md): Limit Switch · inoperative · Dec 3, 2016 · N811FD · Airbus A310324 · Door Warning System
  > AFTER PARKING, THE R1 DOOR SLIDE INDICATION WAS FLASHING. R & R THE DOOR LIMIT SWITCH IAW AMM 52-73-13-04-09 OPS CHECKED GOOD IAW 73-13-05-09.
- [SDR FDEA201611274258](https://openairdocs.org/sdr/FDEA201611274258.md): Battery Pack · inoperative · Nov 27, 2016 · N811FD · Airbus A310324 · Escape Slide
  > DURING LANDING, SLIDE INDICATION ON ECAM FOR R1 WAS FLASHING. REMOVED AND REPLACED ASPU BATTERY NR 1 IAW AMM 52-73-18-04, ASPU BITE CHECKED GOOD. SLIDE INDICATION TEST CHECKED GOOD SEVERAL TIMES IAW AMM 52-73-00-5. ACFT OK FOR SERVICE.
- [SDR FDEA201611224197](https://openairdocs.org/sdr/FDEA201611224197.md): Bottle · low pressure · Nov 22, 2016 · N811FD · Airbus A310324 · Passenger/Crew Doors
  > R1 DOOR SLIDE ARMED INDICATION FLASHING WHILE TAXING IN AFTER LANDING. RT DOOR DAMPER AND EMERGENCY OPERATING CYLINDER PRESSURE FOUND TO BE LOW. SERVICED CYLINDER IAW AMM 52-10-14-03-09. ARMED R1 DOOR, RECEIVED SLIDE INDICATION ON ECAM. CYCLED R1 DOOR ARM
- [SDR FDEA201610263703](https://openairdocs.org/sdr/FDEA201610263703.md): Relay · failed · Oct 26, 2016 · N811FD · Airbus A310324 · Fuel Boost Pump
  > AT FL 370, THE NR 2 LEFT INNER PUMP FAULTED. PUMP FAULTED AND STRONG ACRED ODOR IN THE COCKPIT AND THE AVIONICS COMPARTMENT, ON DESCENT THE REMAINING THREE INNER PUMPS FAULTED AND FUEL FEED RESORTED TO OUTER TANK TO ENGINE. ACCESSED THROUGH THE COCKPIT
- [SDR FDEA201601050025](https://openairdocs.org/sdr/FDEA201601050025.md): Selector Valve · malfunctioned · Jan 5, 2016 · N811FD · Airbus A310324 · Landing Gear Selector
  > AFTER TAKEOFF, LG RETRACTION FAULT SYS NR 1, GEAR REMAINED DOWN. RETURNED FOR LAND. CANNOT OPEN THE LT LG DOOR ON GND. RT LG DOOR OPENED OK ON GND. R&R LG NORMAL CONTROL MICROSWITCH UNIT 2GA PER AMM 32-31-11-04. R&R LANDING GEAR SELECTOR VALVE 3GA PER AMM
- [SDR FDEA201507072165](https://openairdocs.org/sdr/FDEA201507072165.md): Hydraulic Line · leaking · Jul 7, 2015 · N811FD · Airbus A310324 · Hydraulic System, Main
  > EN-ROUTE, GREEN HYD LEVEL DECREASING SLOWLY. DESCENDING THRU FL 150, ECAM WARNING, HYD LEVEL LO, RAN QRH. LEAK FOUND AT LT MAIN GEAR FLEX HOSE PN 00624AE711082-4 FOR STRUT BRACE ACTUATOR. REPLACED WITH ALTN FROM HYD SPARE KIT PN 24060610-0240. PERFORMED PR
- [SDR FDEA201505061396](https://openairdocs.org/sdr/FDEA201505061396.md): Skin · cracked · May 6, 2015 · N811FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > RIGHT WING ROOT REAR SPAR BOTTOM SKIN FOUND ONE EACH FASTENER HEAD POPPED OUT. REMOVED THE HEAD POPPED OUT FASTENER IAW SRM 51-40-21. CARRIED OUT ROTOTEST INSPECTION TO FASTENER HOLE IAW NTM 51-10-18, FOUND CRACK. REAMED THE HOLE TO REMOVE CRACK IAW SRM 51-
- [SDR FDEA201504291321](https://openairdocs.org/sdr/FDEA201504291321.md): Fairing · cracked · Apr 29, 2015 · N811FD · Airbus A310324 · Wing Main, Frame Structure
  > RIGHT WING TIP FENCE FAIRING RIB CRACKED, WY495. REPLACED THE CRACKED RIB OF RT WING TIP FENCE FAIRING AT WY 501 IAW SRM 51-40-21.
- [SDR FDEA201504291320](https://openairdocs.org/sdr/FDEA201504291320.md): Rib · cracked · Apr 29, 2015 · N811FD · Airbus A310324 · Wing, Rib/Bulkhead
  > RIGHT WING TIP FENCE FAIRING AROUND FASTENER HOLES CRACKED AT WY501. REPLACED IAW SRM 51-40-21.
- [SDR FDEA201504291319](https://openairdocs.org/sdr/FDEA201504291319.md): Frame · corroded · Apr 29, 2015 · N811FD · Airbus A310324 · Fuselage Main, Frame
  > AV COMPARTMENT FOUND FRAME 17 CORRODED BETWEEN STRINGER 42 & 43L. BLENDED OUT THE CORROSION IAW SRM 51-74-10 & EA 6-5310-T0317322 P1.
- [SDR FDEA201504291318](https://openairdocs.org/sdr/FDEA201504291318.md): Frame · nicked · Apr 29, 2015 · N811FD · Airbus A310324 · Fuselage Main, Frame
  > MDCC LT FRAME 34 SURFACE FOUND NICK BETWEEN STRINGER 12LT & 22LT. BLEND OUT & SMOOTHED THE NICK AREA IAW SRM51-73-10. APPLIED ALODINE IAW SRM 51-21-10. NO CRACK FOUND IAW NTM 51-10-08. COMPLIED WITH EA6-5310-T0317082.
- [SDR FDEA201504161242](https://openairdocs.org/sdr/FDEA201504161242.md): Door Frame · cracked · Apr 16, 2015 · N811FD · Airbus A310324 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR ACTUATOR ATTACH FITTING. SDI FOUND CRACK WITH A HFEC INSPECTION. REMOVED THE FWD CARGO DOOR IAW AMM 52-31-11-04. REPLACED THE CRACKED FRAME OF FWD CARGO DOOR IAW SRM 51-40-21. INSTALLED THE FWD CARGO DOOR IAW AMM 52-31-11-04 & TESTED OK.
- [SDR FDEA201504161241](https://openairdocs.org/sdr/FDEA201504161241.md): Fitting · cracked · Apr 16, 2015 · N811FD · Airbus A310324 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR ACTUATOR FITTINGS. FOUND CRACK WITH A HFEC INSPECTION. REPLACED THE CRACKED FRAME OF AFT CARGO DOOR AT FRAME 61A IAW SRM 51-40-21. INSTALLED THE AFT CARGO DOOR IAW AMM 52-31-11-04 & TESTED OK. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201504141229](https://openairdocs.org/sdr/FDEA201504141229.md): Crossbeam · corroded · Apr 14, 2015 · N811FD · Airbus A310 · Fuselage Miscellaneous Structure
  > AFT CARGO CROSSBEAM RT SIDE FITTING, CORRODED AT FRAME 62. REPLACED THE RT SIDE CORRODED FITTING, CROSSBEAM, IAW SRM 51-40-21.
- [SDR FDEA201406251546](https://openairdocs.org/sdr/FDEA201406251546.md): Windshield · cracked · Jun 25, 2014 · N811FD · Airbus A310324 · Flight Compartment Windows
  > CAPTAIN`S COCKPIT WINDOW CRACKED AT FLIGHT LEVEL 340, ARCING BEGAN IMMEDIATELY. NORMAL QRH PROCEDURES STOPPED THE ARCING. REMAINDER OF FLIGHT NORMAL. R & R CAPTAIN'S WINDSHIELD IAW AMM 56 -11-11-04, PERFORMED WINDSHIELD PANEL ANTI-ICING & DEFOGGING. OPERAT
- [SDR FDEA201405211114](https://openairdocs.org/sdr/FDEA201405211114.md): Engine · stalled · May 21, 2014 · N811FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE HAD A SUSPECTED STALL ON ROLLOUT. TOWER REPORTED LT ENGINE ON FIRE. STOWED THRUST REVERSERS BY 60 KIAS & STOPPED ACFT, SHUTDOWN ENGINE, NO OTHER FIRE INDICATIONS, VISUALLY CONFIRM NO SMOKE. ON SHUTDOWN IN RAMP ADC 1 FAULT OCCURRED & STAYED ON.
- [SDR FDEA201403130495](https://openairdocs.org/sdr/FDEA201403130495.md): Smoke Detector · malfunctioned · Mar 13, 2014 · N811FD · Airbus A310324 · Smoke Detection
  > IAW WRI 26-22 8151 FWD CARGO COMPARTMENT DET INDICATION. AGENT 1 DISCH, NO SECONDARY INDICATION, NO SMOKE INDICATION IN THE COCKPIT. TESTED BOTH SMOKE DET OK & TESTED 26-16-00-05-01, ACFT OK FOR SERVICE. R & R 42WH SMOKE DETECTOR.
- [SDR FDEA201310162517](https://openairdocs.org/sdr/FDEA201310162517.md): Skin · dented · Oct 16, 2013 · N811FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED ON BELLY FWD OF FRAME 4. REPAIRED DENT IAW EA 6-5330-T0302970A.
- [SDR FDEA201308191952](https://openairdocs.org/sdr/FDEA201308191952.md): Jackscrew · worn · Aug 19, 2013 · N811FD · Airbus A310324 · Trailing Edge Flap Control System
  > AFTER TAKEOFF DURING FLAP RETRACTION, RECIEVED A WARNING BELL AND FLAP SYS 1, FLAP SYS 2FAULT. FLAPS WERE STUCK BETWEEN 15-20, CYCLED HANDLE AND DID NOT CLEAR RAN QRH AND RTB. DURING AFTER LANDING CHECK, FLAPS RETRACTED. REVIEWED FAULT CODE FORM NR 1 SFCC
- [SDR FDEA201308151902](https://openairdocs.org/sdr/FDEA201308151902.md): Unknown · unknown · Aug 15, 2013 · N811FD · Airbus A310324 · Trailing Edge Flap Control System
  > ON APPROACH, FLAPS SYS 1 AND 2 FAULTED. RECYCLED FLAPS, RETRACTED BUT ON EXTENSION STOPPED AT APPOX 18. RAN QRH AND ON FINAL WITH FLAP HANDLE EXTENSION TO 30/40 SLATS EXTEND TO 30 BUT FLAPS REMAINED LESS THAN 20'. BITE TEST ON SFCC NR 1 GOT FAULT CODE 011
- [SDR FDEA201308011728](https://openairdocs.org/sdr/FDEA201308011728.md): Computer · failed · Aug 1, 2013 · N811FD · Airbus A310324 · Auto Throttle System
  > DURING TAKEOFF ROLL, APPROX 10 SECONDS INTO ROLL, ATS LEVER TRIPPED OFF. ENGINE NR 2 EPR MODE FAULTED, ENGINE NR 2, N1 MODE, ATS OFF ON ECAM. CLEARED RUNWAY. RESET CIRCUIT BREAKER ON OUH 31 PANEL AS DIRECTED BY MX. ALSO RESET NR 2 ENGINE EPR MODE FAULT, AS
- [SDR FDEA201305070933](https://openairdocs.org/sdr/FDEA201305070933.md): Wire · damaged · May 7, 2013 · N811FD · Airbus A310324 · Engine Exhaust System Wiring
  > WHEN SETTING TAKEOFF POWER, NR 1 ENGINE REVERSE UNLOCK LIGHT ILLUMINATED. DURING REACTIVATION OF NR 1 THRUST REVERSER, FOUND WIRE CHAFING IN WIRING BUNDLE 21W4082-509 NEXT TO CONNECTOR DS307, FOUND THE WIRE ROUTING TO PIN 4 ON DS307 TO NR 1 THRUST REVERSER
- [SDR FDEA201304090756](https://openairdocs.org/sdr/FDEA201304090756.md): Limit Switch · failed · Apr 9, 2013 · N811FD · Airbus A310324 · Cargo/Baggage Doors
  > CLIMBING THROUGH 5,100 METERS RECEIVED ECAM ALERT. FORWARD CARGO DOOR UNLOCK, PROCEEDED ACCORDING WITH ECAMS SET LANDING ELEVATION AT 10,000 ALERT WENT AWAY AND CAME BACK IN FINAL AGAIN. EXECUTED OVER WEIGHT LANDING IAW QRH. GROUND CHECKED THE FWD CARGO D
- [SDR FDEA201111305081](https://openairdocs.org/sdr/FDEA201111305081.md): Controller · inoperative · Nov 30, 2011 · N811FD · Airbus A310324 · Cabin Pressure Controller
  > ACFT CABIN PRESS CLIMB ABOVE 10000. REQUESTED LOWER ALTITUDE FROM ATC. BRIEFING WITH FLIGHT CREW, NO WARNING MESSAGE DISPLAYED ON ECAM. PERFORMED CPC 1 AND CPC 2 OPS TEST SATIS IAW AMM21-31-00-05-0. R & R THE NR 2 CPC IAW AMM21-31-11-04-0, AND PERFORMED TH
- [SDR FDEA201110214611](https://openairdocs.org/sdr/FDEA201110214611.md): Battery · inoperative · Oct 21, 2011 · N811FD · Airbus A310324 · Escape Slide
  > R1 DOOR WILL NOT ARM. R & R THE EMERGENCY POWER SUPPLY BATTERY NR 1 AND NR 2, AND THE AUTO STANDBY UNIT IAW AMM 52-73-18-04-0, AND PERFORMED THE TEST IAW AMM 52-73-00, P BLOCK 501, TESTED NORMAL. ECAM SLIDE DOOR R1 INDICATION NORMAL. AC OK FOR SVC. R & R B
- [SDR FDEA201108103196](https://openairdocs.org/sdr/FDEA201108103196.md): Indicator · failed · Aug 10, 2011 · N811FD · Airbus A310324 · Cabin Pressure Control System
  > AT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESECNDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2950 (ORANGE) CABIN ALTITUDE 20460 (RED) WHEN EVENT OCCURRED BOTH CREW HAD EARS POP. BELL SOUNDE
- [SDR FDEA201108103195](https://openairdocs.org/sdr/FDEA201108103195.md): Controller · failed · Aug 10, 2011 · N811FD · Airbus A310324 · Cabin Pressure Control System
  > AT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESCENDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2950 (ORANGE) CABIN ALTITUDE 20460 (RED) WHEN EVENT OCCURRED BOTH CREW HAD EARS POP. BELL SOUNDE
- [SDR FDEA201009303819](https://openairdocs.org/sdr/FDEA201009303819.md): Filter · leaking · Sep 30, 2010 · N811FD · Airbus A310324 · Hydraulic System, Main
  > DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QTY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. FOUND HYD LEAKAGE CAME FROM THE GREEN SERVO CONTRO FILTER. REMOVED AND REPLACED THE PUMP DELIV
- [SDR FDEA201009303821](https://openairdocs.org/sdr/FDEA201009303821.md): Filter · leaking · Sep 30, 2010 · N811FD · Airbus A310 · Hydraulic System, Main
  > DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QUANTITY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. PERFORMED GREEN HYD SYS LEAK CHECK FOUND HYD LEAKAGE CAME FROM THE FILTER 1049 WHICH ON G

Next page: https://openairdocs.org/deregistered/N811FD-2024-03-02/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 = 'N811FD' AND deregistration_id = 'N811FD-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N811FD-2024-03-02/reports

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