# Service difficulty reports: N920FT, cancelled Oct 5, 2006

A list on [N920FT, cancelled Oct 5, 2006](https://openairdocs.org/deregistered/N920FT-2006-10-05.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 5 · 247 reports

- [SDR P5CA0601454](https://openairdocs.org/sdr/P5CA0601454.md): Line · cracked · Feb 27, 2006 · N920FT · Boeing 747249F · Engine Fuel and Control
  > CREW REPORTED ON CLIMBOUT THROUGH FL 280, AIRCRAFT YAWED, NR 1 ENGINE SHUT DOWN. ATTEMPT TO RESTART UNSUCCESSFUL. DUMPED FUEL AND RETURNED TO PIK. FOUND SENSE LINE CRACKED AT REAR OF FUEL CONTROL. LINE REMOVED AND REPAIRED PER PRATT WHITNEY EM 72-09-7.
- [SDR P5CA0601450](https://openairdocs.org/sdr/P5CA0601450.md): Module · failed · Feb 26, 2006 · N920FT · Boeing 747249F · Hydraulic System, Main
  > CREW REPORTED ON TAKEOFF ROLL, ANTI-SKID LIGHT CAME ON F/E PANEL, HAD R/F, R/R, L/F, AND L/R LIGHTS ON FOR R/H BODY GEAR. TAKEOFF ABORTED AT 60 KTS. REPLACED ANTI-SKID CONTROL MODULE PER MM 32-42-02, PERFORMED HIGH ENERGY STOP INSPECTION.
- [SDR P5CA0601431](https://openairdocs.org/sdr/P5CA0601431.md): Coupler · defective · Jan 15, 2006 · N920FT · Boeing 747249F · Magnetic Compass
  > DURING APPROACH, CAPTAIN'S HSI AND F/O'S RMI FLAGS IN VIEW. REPLACED COMPASS COUPLER PER AMM 34-21-03. CHECKS OK.
- [SDR P5CA0601430](https://openairdocs.org/sdr/P5CA0601430.md): Coupler · failed · Jan 13, 2006 · N920FT · Boeing 747249F · Magnetic Compass
  > CAPTAIN'S COMPASS SYSTEM HAS TO BE SLAVED EVERY 10 MINUTES. APPEARS THE COMPASS FLUX VALVE IS INOP. REMOVED AND REPLACED NR 1 COMPASS COUPLER AS PER MM 34-21-03. OPS CHECK OK.
- [SDR P5CA0501409](https://openairdocs.org/sdr/P5CA0501409.md): Starter · failed · Oct 31, 2005 · N920FT · Boeing 747249F · Engine Starter
  > AFTER PUSH BACK, CREW REPORTED NR 3 ENGINE WOULD NOT START. PARAMETERS INDICATE NORMAL, NR N1 OR N2 INDICATION. REPLACED STARTER IAW MM 80-10-00. OPS NORMAL.
- [SDR P5CA0501405](https://openairdocs.org/sdr/P5CA0501405.md): Skin · corroded · Oct 13, 2005 · N920FT · Boeing 747249F · Wing, Plate/Skin
  > LEFT WING LOWER SKIN CORROSION ON OUTBOARD JACK PAD AREA AT FSS 1295. REPAIR CARRIED OUT IAW BOEING FAA FORM 8100-9. SUPPLEMENTARY JOB CARDS AFM 0147 AND AFM 1068 FOR DETAILS.
- [SDR P5CA0501403](https://openairdocs.org/sdr/P5CA0501403.md): Beam · cracked · Aug 1, 2005 · N920FT · Boeing 747249F · Fuselage Main, Structure
  > FWD CARGO, FOUND CRACKS PROPAGATED FROM BLANKET HOLE AT STA 300 AND 320 AND LT NOSE WHEEL WELL VERTICAL BEAM WEB AT WL 160. REPAIR CARRIED OUT IAW LO-BY714-072 INTERIM WEB REPAIR. CONTINUE INSPECTION PER SB 747-53A2293.
- [SDR P5CA0501374](https://openairdocs.org/sdr/P5CA0501374.md): Yaw Damper · malfunctioned · Jun 19, 2005 · N920FT · Boeing 747249F · Autopilot System
  > RUDDER WOULD NOT DEFLECT. REPLACED UPPER AND LOWER YAW DAMPER COMPUTERS PER AMM 22-16-02.
- [SDR P5CA0501349](https://openairdocs.org/sdr/P5CA0501349.md): Actuator · malfunctioned · May 12, 2005 · N920FT · Boeing 747249F · Elevator Control System
  > CREW RETURNED AIRCRAFT TO BLOCKS ADVISING ELEVATORS WERE STIFF DURING FLIGHT CONTROL CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER MM 27-31-17. OPS CHECK PER MM 27-31-14, NO DISCREPANCIES NOTED.
- [SDR PCAO501328](https://openairdocs.org/sdr/PCAO501328.md): Pump · malfunctioned · Mar 3, 2005 · N920FT · Boeing 747249F · Engine Fuel Pump
  > CREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL PUMP. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01.
- [SDR P5CAO501327](https://openairdocs.org/sdr/P5CAO501327.md): Fuel Control · malfunctioned · Mar 3, 2005 · N920FT · Boeing 747249F · Fuel Control/Turbine Engines
  > CREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL CONTROL. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01.
- [SDR P5CA0501315](https://openairdocs.org/sdr/P5CA0501315.md): Valve · leaking · Feb 6, 2005 · N920FT · Boeing 747249F · Fuel Dump System
  > DURING WALKAROUND OBSERVED FUEL LEAKING FROM RIGHT FUEL JETTISON MANIFOLD. REMOVED AND REPLACED RIGHT FUEL JETTISON NOZZLE VALVE PER BOEING MM 28-31-03. OPS CHECK OK.
- [SDR P5CA0501305](https://openairdocs.org/sdr/P5CA0501305.md): Line · chafed · Jan 20, 2005 · N920FT · Boeing 747249F · Turbine Engine Oil System
  > NR 3 ENG OIL PRESS FLUCTUATES FROM 35 TO 45 PSI. ENG OIL PRESS LIGHT BLINKS ON & OFF. ALSO OIL QTY WENT FROM 3/4 TO 1/4 AND BACK TO 1/2. FOUND UPPER ENGINE OIL LINE AT OIL FILTER HOUSING CHAFED. REPLACED CHAFED LINE, COI ISSUED/ AMM 20-11-18.
- [SDR P5CA0501304](https://openairdocs.org/sdr/P5CA0501304.md): Actuator · failed · Dec 27, 2004 · N920FT · Boeing 747249F · Landing Gear Actuator
  > WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND DOWN LOCK ACTUATOR FAILED. REPLACED ACTUATOR PER MM 32-33-15.
- [SDR P5CA0501303](https://openairdocs.org/sdr/P5CA0501303.md): Actuator · failed · Dec 27, 2004 · N920FT · Boeing 747249F · Landing Gear Actuator
  > WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND EXTEND/RETRACT ACTUATOR FAILED. REPLACED EXTERNAL/RETRACT ACTUATOR PER MM 32-33-01.
- [SDR P5CA0501302](https://openairdocs.org/sdr/P5CA0501302.md): Actuator · leaking · Dec 27, 2004 · N920FT · Boeing 747249F · Landing Gear Actuator
  > WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYD SYSTEM. LANDING WAS NORMAL. FOUND LEFT BODY GEAR LEVELING CYLINDER FAILED. REPLACED PER MM-13-15.
- [SDR P5CA0401274](https://openairdocs.org/sdr/P5CA0401274.md): Engine · failed · Nov 14, 2004 · N920FT · Boeing 747249F · Engine (Turbine/Turboprop)
  > ON TAKEOFF TOWER REPORTED SPARKS FROM NR 1 ENGINE DURING CLIMB.EGT HIGH (600 DEGREE) AS COMPARED TO OTHER ENGINES.N1 90% N2 94%, EXPERIENCED COMPRESSOR STALL AT FL 250 WHILE CDLIMBING TO FL 350. ENGINE REPLACED PER POLAR WORK CARD M71-00-02.
- [SDR P55CA0401273](https://openairdocs.org/sdr/P55CA0401273.md): Actuator · malfunctioned · Nov 7, 2004 · N920FT · Boeing 747249F · Fuel Control/Turbine Engines
  > IN CLIMB AT 9200 FT, NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASHES OF LIGHT FROM LT SIDE. WIND MILL TIME 50 MINUTES, OIL PRESSURE 5 PSI, N1 22 PERCENT N2 18 PERCENT, FIRE SWITCHED PULLED & NR 1 EDP SUPPLY OFF. REVIEWED
- [SDR P5CA0401277](https://openairdocs.org/sdr/P5CA0401277.md): Engine · malfunctioned · Nov 6, 2004 · N920FT · Boeing 747249F · Engine (Turbine/Turboprop)
  > IN CLIMB AT 9200 FT NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASH OF LIGHT FROM LEFT SIDE OF A/C, WINDMILL TIME 50 MINUTES,MINIMUM OIL PRESSURE 5 PSI. REVIEWED EXCEDANCE,FOUND WITH IN LIMITS.VISUAL INSPECTION ACCOMPLISHED
- [SDR P5CA0401272](https://openairdocs.org/sdr/P5CA0401272.md): Valve · failed · Nov 1, 2004 · N920FT · Boeing 747249F · Engine Starter
  > NR 4 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. NR 4 ENGINE START VALVE MANUAL OPS OK DEFERRED PER DDPG 80-2.
- [SDR P5CA0401271](https://openairdocs.org/sdr/P5CA0401271.md): Start Valve · failed · Nov 1, 2004 · N920FT · Boeing 747249F · Engine Starter
  > NR 3 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. REPLACED START VALVE NR 3 ENGINE, AMM 80-11-04, OPS CHECK OK.
- [SDR P5CA0401270](https://openairdocs.org/sdr/P5CA0401270.md): Fuel Sys · leaking · Nov 1, 2004 · N920FT · Boeing 747249F · Aircraft Fuel Distribution System
  > A/C RETURN TO BLOCK DUE TO FUEL GOING OVERBOARD FROM RIGHT WING VENT BOX. DRAINED SURGE TANK, CHECKED FUELING SYSTEM PER AMM 28-21-00, CHECKS NORMAL WITH ALL PUMPS RUNNING & FUELING DUCTS PRESSURIZED.
- [SDR P5CA0401267](https://openairdocs.org/sdr/P5CA0401267.md): Connector · dirty · Oct 31, 2004 · N920FT · Boeing 747249F · Engine Control System Wiring
  > FUEL CONDITION ACTUATOR NR 1 ENGINE CIRCUIT BREAKER POPPED ON ENGINE START. REMOVED, CLEANED & REINSTALLED CONNECTOR AT J14-P, PERFORMED SYSTEM CHECK, GOOD PER AMM 76-11-00.
- [SDR P5CA0401264](https://openairdocs.org/sdr/P5CA0401264.md): Generator · malfunctioned · Oct 29, 2004 · N920FT · Boeing 747249F · AC Generator-Alternator
  > NR 1 ENGINE GENERATOR FEEDER FAULT. REMOVED AND REPLACED NR 1 ENGINE GENERATOR PER AMM 24-21-01, SYSTEM OPS CHECK OK.
- [SDR P5CA0401265](https://openairdocs.org/sdr/P5CA0401265.md): Generator · failed · Oct 29, 2004 · N920FT · Boeing 747249F · AC Generator-Alternator
  > NR 2 ENGINE GENRATOR WILL NOT COME ON LINE. REMOVED AND REPLACED NR 2 ENGINE GENERATOR, OPS CHECK OK PER AMM 24-21-01.
- [SDR P5CA0401258](https://openairdocs.org/sdr/P5CA0401258.md): Gearbox · malfunctioned · Oct 18, 2004 · N920FT · Boeing 747249F · Turbine Engine Accessory Drive
  > WHEN STARTING NR 2 ENGINE, N2 WENT 62.5 PERCENT IMMEDIATELY. NR 2 GENRATOR CAME ON LINE IMMEDIATELY, NO N1 INDICATION, OIL QTY WENT FROM FULL TO 3/4. REPLACED GEARBOX ANGLE PER AMM 72-61-03. OPERATIONAL & LEAK CHECK OK PER AMM 71-00-00.
- [SDR P5CA0401227](https://openairdocs.org/sdr/P5CA0401227.md): Skin · damaged · Sep 27, 2004 · N920FT · Boeing 747249F · Cargo/Baggage Doors
  > PRIOR TO DEPARTURE FOUND DAMAGE ON FWD CARGO DOOR LWR SKIN. REPAIRED DAMAGE AT LWR CORNER SKIN PER SRM 52-30-06, FIGURE 1 SHEET 7.
- [SDR P5CA0401189](https://openairdocs.org/sdr/P5CA0401189.md): Computer · malfunctioned · Sep 9, 2004 · N920FT · Boeing 747249F · Autopilot Trim Servo
  > AFTER T/O AFTER GEAR UP, FELT A/COLL TO THE LEFT, GOT CONTROL OF A/C THAN IT HAPPENED AGAIN. FLIGHT CONTROL SHOWING UPPER RUDDER MOVING TO THE LEFT, THEN SLOWLY GOING BACK TO CENTER. DECLARED EMERGENCY & SHUTOFF UPPER YAW DAMPER COMPUTER, PROBLEM SEEMED TO G
- [SDR P5CA0401184](https://openairdocs.org/sdr/P5CA0401184.md): Engine · malfunctioned · Sep 5, 2004 · N920FT · Boeing 747249F · Engine (Turbine/Turboprop)
  > NR 1 ENGINE SHUT DOWN, EGT WENT OFF SCALE, N1 WENT 20 PERCENT, N2 14 PERCENT & OIL PRESSURE 5 PSI. REPLACED NR 1 ENGINE PER WORK CARD MM 71-00-02 & 71-08-07, ALL OPS CK NORMAL.
- [SDR P5CA0401178](https://openairdocs.org/sdr/P5CA0401178.md): Filter · damaged · Aug 24, 2004 · N920FT · Boeing 747249F · Aircraft Fuel Filter/Strainer
  > NR 2 ENGINE COMPRESSOR STALL. VISUAL INSPECTION, REMOVED AND REPLACED FUEL & OIL FILTER, ENGINE IDLE RUN ACCEPTABLE PER AMM 71-00-00.
- [SDR P5CA0401170](https://openairdocs.org/sdr/P5CA0401170.md): Frame · cracked · Aug 14, 2004 · N920FT · Boeing 747249F · Nacelle/Pylon, Main Frame
  > FRETTING & CRACKS IN FRAME AFT EDGE OF HYD COMPT. CUT OUT DAMAGE AREA PER SRM 53-10-04, FABRICATED ANGLE & PLATE INSTALLED PER SRM 53-10-02.
- [SDR P5CA0401169](https://openairdocs.org/sdr/P5CA0401169.md): Fitting · corroded · Aug 14, 2004 · N920FT · Boeing 747249F · Fuselage, Landing Gear Attach Fittings
  > CORROSION ON RIGHT MLG FITTING BB 1480 RBL 22. REPAIRED AREA PER SAA SK 920-001(SR)FAA FORM 811-3.
- [SDR P5CA0401141](https://openairdocs.org/sdr/P5CA0401141.md): Access Panel · delaminated · Aug 12, 2004 · N920FT · Boeing 747249F · Fluid Service Doors
  > REFUELING PANEL 521BB IS DELAMINATED INSIDE RIGHT WING. REMOVED DELAMINATED AREA PER SRM 51-40-04, REPAIRED PER SRM 51-40-15.
- [SDR P5CA0401142](https://openairdocs.org/sdr/P5CA0401142.md): Panel · dented · Aug 12, 2004 · N920FT · Boeing 747249F · Fuselage Miscellaneous Structure
  > MAIN CARGO RT SIDE STA 1790 FRAME PROTECTION PANEL DENTED, REMOVED AND REPLACED PANEL AND INSP FRAME FOR ANY DAMAGE. DAMAGED INSULATION MOUNT BRACKET, SEVERAL AREA OF COVERS, BLENDED AREA OUT, REPAIR IAW SRM 51-10-04, SRM 51-30-02, SRM 51-40-03.
- [SDR P5CA0401143](https://openairdocs.org/sdr/P5CA0401143.md): Floor Support · cracked · Aug 11, 2004 · N920FT · Boeing 747249F · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR SUPPORT IS CRACKED AT STA 240. REMOVED DAMAGED AREA, FABRICATED SUPPORT ANGLE & SPLICED IN PER SRM 57-30-02 & SRM 53-11-03, 51-10-02 & 51-10-06.
- [SDR P5CA0401167](https://openairdocs.org/sdr/P5CA0401167.md): Floor Panel · cracked · Aug 10, 2004 · N920FT · Boeing 747249F · Fuselage Floor Panel
  > CARGO PIT FLOOR PANEL STA 1680 THRU 1780 IS CRACKED & CORRODED. CUT OUT AND REMOVED DAMAGE, NO CRACK FOUND. CUT OUT FABRICATED & INSTALLED AS PER SRM 51-40-08 & 51-10-02.
- [SDR P5CA0401168](https://openairdocs.org/sdr/P5CA0401168.md): Support · corroded · Aug 10, 2004 · N920FT · Boeing 747249F · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT STRUCTURE STA 940 LBL 3 TO RBL 3 REF KEEL BEAM AREA. REMOVE CORROSION AREA, FABRICATED WEB FLANG SRM 53-50-04, INSTALLED PER SRM 51-30-05.
- [SDR P5CA0401138](https://openairdocs.org/sdr/P5CA0401138.md): Flap Track · delaminated · Aug 10, 2004 · N920FT · Boeing 747249F · Trailing Edge Flaps
  > DELAMINATION SEVERAL AREA, I/B FORE FLAP L/E RIGHT WING B/W FLAP TRACK. CLEANED AREA & REPAIRED PER SRM 51-40-15.
- [SDR P5CA0401148](https://openairdocs.org/sdr/P5CA0401148.md): Panel · corroded · Aug 9, 2004 · N920FT · Boeing 747249F · Aerodynamic Fairings
  > FUSELAGE PANEL 191OA, BOTH HAVE HEAVY CORROSION. REMOVED 2 EA SPLICE PLATES IAW 51-30-01. FOUND TO BE OUT OF LIMIT, FABRICATED NEW PLATES PER BOEING DRAWING 65B3878.
- [SDR P5CA0401145](https://openairdocs.org/sdr/P5CA0401145.md): Angle · broken · Aug 9, 2004 · N920FT · Boeing 747249F · Fuselage, Equipment Attach Fittings
  > L-ANGLE BROKEN AT STA 1940, L1 BIL 20 AFT CARGO AREA. REMOVED AND REPLACED BROKEN BRACKET PER SRM 51-30-02. NEW BRACKET FABRICATED PER SRM 53-11-23.
- [SDR P5CA0401147](https://openairdocs.org/sdr/P5CA0401147.md): Panel · delaminated · Aug 9, 2004 · N920FT · Boeing 747249F · Aerodynamic Fairings
  > PANEL NR 194 LR DELAMINATED IN SEVERAL PLACES. REMOVED DAMAGE & PREP PER SRM 51-40-15.
- [SDR P5CA0401144](https://openairdocs.org/sdr/P5CA0401144.md): Nose Cowl · delaminated · Aug 9, 2004 · N920FT · Boeing 747249F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE NOSE COWL T/E TO CORE COWL HAS DELAMINATION. REPAIRED PER SRM 54-31-03.
- [SDR P5CA0401146](https://openairdocs.org/sdr/P5CA0401146.md): Support Angle · corroded · Aug 9, 2004 · N920FT · Boeing 747249F · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SIDE OF WING TO BODY FAIRING SUPPORT ANGLE, AT BS 980 & AT RBL 36 AT I/B END OF PANEL 192. REMOVED CORROSION AREA PER 51-10-01 & SRM 51-30-02, FABRICATED REPAIRED.
- [SDR P5CA0401150](https://openairdocs.org/sdr/P5CA0401150.md): Panel · delaminated · Aug 9, 2004 · N920FT · Boeing 747249F · Nacelle/Pylon, Plate/Skin
  > NR 4 ENGINE PYLON PANEL 481C HAS DELAMINATION. REMOVED DAMAGE IAW SRM 51-40-15, BONDED APPLIED PER SRM 51-40-15.
- [SDR P5CA0401149](https://openairdocs.org/sdr/P5CA0401149.md): Skin · delaminated · Aug 9, 2004 · N920FT · Boeing 747249F · Fuselage Main, Plate/Skin
  > LWR FUSELAGE PANEL NR 1913, EXTENSION SIDE HAS DELAMINATION. REMOVED DAMAGED AREA PER SRM 51-40-15, REPAIR PER SRM 51-40-15.
- [SDR P5CA0401140](https://openairdocs.org/sdr/P5CA0401140.md): Support Angle · corroded · Aug 9, 2004 · N920FT · Boeing 747249F · Fuselage Miscellaneous Structure
  > CORROSION AT FUSELAGE EXTERNAL STRUCTURE, AT STA 1180 AFT OF LWR BEACON. REMOVED SUPPORT ANGLE, FABRICATED NEW ANGLE & INSTALLED PER SRM 51-10-01.
- [SDR P5CA0401139](https://openairdocs.org/sdr/P5CA0401139.md): Fairing · damaged · Aug 9, 2004 · N920FT · Boeing 747249F · Aerodynamic Fairings
  > DAMAGED TO WING TO BODY FAIRING PANEL 192RR. REMOVED DAMAGED AREA REPAIR PER SRM 51-40-15.
- [SDR P5CA0401155](https://openairdocs.org/sdr/P5CA0401155.md): Panel · delaminated · Aug 6, 2004 · N920FT · Boeing 747249F · Aerodynamic Fairings
  > FUSELAGE FITTED PANEL 191WL HAS DELAMINATION ON EXTERIOR SIDE. REPAIRED PANEL 191WL PER SRM 51-40-15.
- [SDR P5CA04011054](https://openairdocs.org/sdr/P5CA04011054.md): Skin · cracked · Aug 6, 2004 · N920FT · Boeing 747249F · Passenger/Crew Doors
  > CRACK IN LWR CORNER OF MAIN ENTRY DOOR. REPAIRED IN LWR FWD CORNER L1 DOOR IAW SRM 52-10-02.
- [SDR P5CA04011053](https://openairdocs.org/sdr/P5CA04011053.md): Stop Fitting · corroded · Aug 6, 2004 · N920FT · Boeing 747249F · Fuselage, Equipment Attach Fittings
  > STOP FITTING STA 1490 L1 BL20 HAS CORROSION AFT PIT. REMOVED FASTENERS TO FOM IAW 51-40-02, REMOVED CORROSION, MAX MATERIAL REMOVED IAW 53-10-01, OK TO TREAT.

Next page: https://openairdocs.org/deregistered/N920FT-2006-10-05/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 = 'N920FT' AND deregistration_id = 'N920FT-2006-10-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N920FT-2006-10-05/reports

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