# Service difficulty reports: N426FB, cancelled Apr 7, 2017

A list on [N426FB, cancelled Apr 7, 2017](https://openairdocs.org/deregistered/N426FB-2017-04-07.md).

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

- [SDR ARWA20020810](https://openairdocs.org/sdr/ARWA20020810.md): Transducer · Aug 30, 2002 · N426FB · Doug DC85F54 · Flight Control System
  > LOG PAGE # 110608. DISCREPANCY: NEAR END OF TAKEOFF ROLL PTY MAIN GEAR SPOILER INOPERATIVE LIGHT CAME ON. CORRECTIVE ACTION:REMOVED AND REPLACED #5 ANTISKID TRANSDUCER OPERATIONAL CHECK NORMAL IAW 27-35-0.
- [SDR ARWA20020802](https://openairdocs.org/sdr/ARWA20020802.md): Control Panel · malfunctioned · Aug 4, 2002 · N426FB · Doug DC85F54 · AC Power Distribution System
  > AFTER STARTING ENGINE NR 2 AND ENGINE NR 3 HAD SMOKE IN COCKPIT. CREW EVACUATED AIRCRAFT. FOUND NR 2 AC CONTROL PANEL BURNT OUT. REMOVED AND REPLACED NR 2 AC CONTROL PANEL IAW MM 24-5-7, ALSO REMOVED AND REPLACED GENERATOR RELAY IAW MM 24-5-3. OPERATIONS C
- [SDR ARWA20020315](https://openairdocs.org/sdr/ARWA20020315.md): Clutch · failed · Mar 27, 2002 · N426FB · Doug DC85F54 · Alternator-Generator Drive
  > NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE SENT TO REPAIR
- [SDR ARWA20020313](https://openairdocs.org/sdr/ARWA20020313.md): Oil System · fluctuates · Mar 27, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil System
  > AT 1140Z NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE (S/N 6
- [SDR ARWA20020314](https://openairdocs.org/sdr/ARWA20020314.md): Fluid · low · Mar 22, 2002 · N426FB · Doug DC85F54 · Hydraulic System, Main
  > UPON LANDING, HYDRAULIC PRESSURED DROPPED TO ZERO AFTER GEAR EXTENSION. ALL CHECKLIST ACCOMPLISHED. SERVICED HYDRAULIC IAW MM 12-4-0, NO LEAKS NOTED.
- [SDR ARWA20020309](https://openairdocs.org/sdr/ARWA20020309.md): Cylinder · leaking · Mar 21, 2002 · N426FB · Doug DC85F54 · Landing Gear Retraction/Extension System
  > UPON CLEARING THE RUNWAY EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID AND PRESSURE ALL CHECKLIST COMPLIED WITH. AIRBRAKE USED TO STOP AIRCRAFT WITHOUT INCIDENT. FOUND FWD LEFT BOGIE TRIM CYLINDER WITH HYDRAULIC LEAK. REMOVED AND REPLACED MLG FWD LEFT BOGIE T
- [SDR ARWA20020308](https://openairdocs.org/sdr/ARWA20020308.md): Indicator · sticks · Mar 15, 2002 · N426FB · Doug DC85F54 · Engine Pressure Ratio (EPR)
  > ABORTED TAKEOFF DUE TO ENGINE NR 4 MOMENTARY POWER LOSS, ALL ENGINE PARAMETERS NORMAL. RETURN TO RAMP. PERFORMED ENGINE RUN-UP AND NOTICED EPR INDICATOR STICKING. REMOVED AND REPLACED EPR INDICATOR IAW MM 77-1-2 AND SYSTEMS OPS CHECKED NORMAL IAW MM 71-0.
- [SDR ARWA20020307](https://openairdocs.org/sdr/ARWA20020307.md): Volt Regulator · malfunctioned · Mar 13, 2002 · N426FB · Doug DC85F54 · AC Regulator
  > ON FINAL APPROACH SMOKE CAME FROM RT SIDE OF COCKPIT. REMOVED AND REPLACED NR 4 VOLTAGE REGULATOR (BURNT) IAW MM 29-5-11, OPS CHECKED NORMAL IAW MM 24-5-1.
- [SDR ARWA20020304](https://openairdocs.org/sdr/ARWA20020304.md): Housing · damaged · Mar 6, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil System
  > DURING CLIMBOUT THROUGH 16,000 FEET; NR 2 ENGINE OIL PRESSURE GAUGE BEGAN FLUCTUATING AT 180, AND NR 2 OIL PRESSURE LIGHT BEGAN FLICKERING, THEN WENT STEADY. ACCOMPLISHED APPROPRIATE ABNORMAL CHECKLISTS AND SHUTDOWN ENGINE AT 22:15 ENGINE OIL PRESSURE WINDMIL
- [SDR ARWA20020302](https://openairdocs.org/sdr/ARWA20020302.md): Relief Valve · faulty · Mar 5, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil System
  > DURING CLIMBOUT THROUGH 15,000 FT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING, NR 2 OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED APPROPRIATE CHECK LISTS AND SHUT DOWN ENGINE AT 00:15Z, OIL WINDMILLED AT 12 PSI. AIRCRAFT RETURNED TO PTY AND LANDED UNEVENTFUL.
- [SDR ARWA20011215](https://openairdocs.org/sdr/ARWA20011215.md): Line · leaking · Dec 28, 2001 · N426FB · Doug DC85F54 · Engine Oil Distribution (Airframe Furnished)
  > NR 3 ENGINE LOSS OF OIL QUANTITY OSCILLATING OIL PRESS AND OIL PRESS WARNING ON AND OFF. SHUT DOWN NR 3 ENGINE AS PER ABNORMAL CHECKLIST OIL PRESS 15 PSI, 1 HOUR WINDMILLING. AIRCRAFT RETURNED TO KMIA UNEVENTFUL. INSPECTED ENGINE AND FOUND ENGINE OIL COOLER
- [SDR ARWA20011210](https://openairdocs.org/sdr/ARWA20011210.md): Brace · broken · Dec 18, 2001 · N426FB · Doug DC85F54 · Nose/Tail Landing Gear
  > AT FLIGHT LEVEL 31.0 HEARD LOUD BANG NOISE UNDER COCKPIT AREA, ALSO ON APPROACH LOWERING GEAR LARGE BANG AND AIRCRAFT SHOOK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LT NOSE LANDING GEAR SIDE BRACE RETRACT ACT LUG BROKEN. REMOVED AND REPLACED LT NOSE LANDING
- [SDR ARWA20011201](https://openairdocs.org/sdr/ARWA20011201.md): Csd · failed · Dec 1, 2001 · N426FB · Doug DC85F54 · Alternator-Generator Drive
  > ON TAKEOFF AT KMIA, NR 4 GENERATOR ZNS FAULT; ABORTED TAKEOFF AT 90 KTS AND F/O LOST LIGHTS, INSTRUMENTS AND RADIO COMMUNICATION. F/O'S INSTRUMENTS AND LIGHT OPS CK NORMAL AFTER BUS RESET IAW MM 23-2-0 & 24-1-0. REMOVED AND REPLACED NR 4 ENGINE CSD ASSY IAW M
- [SDR ARWA20011124](https://openairdocs.org/sdr/ARWA20011124.md): Blade · failed · Dec 1, 2001 · N426FB · Doug DC85F54 · Turbine Engine Compressor Section
  > ON TAKE OFF MIAMI A LOUD BANG FOLLOWED BY HIGH VIBRATION ON NR 2 ENGINE REJECTED THE TAKE OFF ROLL. FOUND C2 BLADE FAILURE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK NORMAL.
- [SDR ARWA20011120](https://openairdocs.org/sdr/ARWA20011120.md): Skin · corroded · Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Main, Plate/Skin
  > AT STATIONS 960 TO 980 PITTING CORROSION AT INNER SIDE OF FUSELAGE SKIN BETWEEN STRINGERS 28R & 25R. REPAIRED FUSELAGE SKIN BETWEEN STATION 980 TO 1020 STR 28 & 25L IAW DRAWING AS 11354.
- [SDR ARWA20011119](https://openairdocs.org/sdr/ARWA20011119.md): Support · corroded · Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Miscellaneous Structure
  > UPON INSPECTION THE FOLLOWING WAS FOUND: VERTICAL SUPPORT AT STATION 980 RT SIDE LOWER END CORRODED, WHERE SUPPORT ATTACHES TO CIRCUMFERENTIAL FRAME. REPAIRED VERTICAL SUPPORT AT STA 980 LT LOWER END IAW DRAWING NR AS 11355.
- [SDR ARWA2001118](https://openairdocs.org/sdr/ARWA2001118.md): Frame · corroded · Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Main, Frame
  > UPON INSPECTION THE FOLLOWING WAS FOUND: AT STATION 980 AFT BELLY COMPARTMENT, APPROX S-31 CORROSION AT CIRCUMFERENTIAL. REPAIR STA 980 CIRCUMFERENTIAL APPROX S-31L IAW DRAWING AS 11356.
- [SDR ARAWA000901](https://openairdocs.org/sdr/ARAWA000901.md): Fuel Control · malfunctioned · Sep 16, 2000 · N426FB · Doug DC8F54 · Fuel Control/Reciprocating Engines
  > ON APPROACH TO SKCL, NR 4 ENGINE FAILED. PERFORMED EMERGENCY PROCEDURES AS PER FINE AIR PROCEDURES. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL IAW MM 73-22-00. REMOVED AND REPLACED NR 4 ENGINE DRIVEN FUEL PUMP IAW MM 73-01-01.
- [SDR 20001208AP006](https://openairdocs.org/sdr/20001208AP006.md): Fitting · cracked · Jul 6, 2000 · N426FB · Doug DC8F54 · Fuselage Miscellaneous Structure
  > DURING AN INSPECTION FOUND THE FOLLOWING, CRACKED LEFT MLG AUXILIARY SPAR FITTING. REPLACED AUXILIARY SPAR FITTING IAW DOUGLAS DRAWING NR 5802630. (M)
- [SDR 20001208AP002](https://openairdocs.org/sdr/20001208AP002.md): Spar Cap · cracked · Jul 6, 2000 · N426FB · Doug DC8F54 · Wing Spar
  > DURING AN INSPECTION OF THE PYLON FOUND FORWARD SPAR CRACK AT STATION XFS 550. REPAIRED FORWARD PYLON IAW DOUGLAS DRAWING NR 5802712. (M)
- [SDR 20001208AP001](https://openairdocs.org/sdr/20001208AP001.md): Fitting · cracked · Jul 6, 2000 · N426FB · Doug DC8F54 · Fuselage Miscellaneous Structure
  > DURING AN INSPECTION FOUND THE FOLLOWING, CRACKED FITTING LEFT SIDE LONGERON 24. REPLACED CRACK LONGERON FITTING IAW DOUGLAS DRAWING NR 5802709. (M)
- [SDR 2000ZZZM231](https://openairdocs.org/sdr/2000ZZZM231.md): Spar · cracked · Aug 31, 1999 · N426FB · Doug DC8F54 · Wing Spar
  > DURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVICE ENGINEERING FAX FAS-MIA-99-0010RR AND SRO8570012 PER FINE AIR EA G5710-02, 00. (M)
- [SDR 2000ZZZM248](https://openairdocs.org/sdr/2000ZZZM248.md): Skin · cracked · Apr 21, 1999 · N426FB · Doug DC8F54 · Leading Edge Devices
  > DURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711-02:00. (M)
- [SDR 97ZZZX3558](https://openairdocs.org/sdr/97ZZZX3558.md): Fuel Contl Unit · defective · Jul 22, 1997 · N426FB · Doug DC8F54 · Fuel Control/Turbine Engines
  > DURING FLARE AT LANDING MIAMI, NR 3 ENGINE FLAMED OUT. TROUBLESHOOTING ON GROUND REVEALED DEFECTIVE ENGINE FUEL CONTROL UNIT. REPLACED FCU, TRIMMED ENGINE, AND RETURNED ACFT TO SERVICE. (X)
- [SDR 97ZZZM435](https://openairdocs.org/sdr/97ZZZM435.md): Brackets · broken · Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear Doors
  > ON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 97ZZZM434](https://openairdocs.org/sdr/97ZZZM434.md): Brackets · broken · Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear Doors
  > ON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 97ZZZM433](https://openairdocs.org/sdr/97ZZZM433.md): Brackets · broken · Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear Doors
  > ON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 97ZZZM432](https://openairdocs.org/sdr/97ZZZM432.md): Brackets · broken · Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear Doors
  > ON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 96ZZZM1441](https://openairdocs.org/sdr/96ZZZM1441.md): Switch · roller missing · Oct 21, 1996 · N426FB · Doug DC8F54 · Landing Gear Position and Warning
  > AFTER TAKEOFF MIA, RIGHT MAIN GEAR LIGHT UNSAFE LIGHT ON AFTER GEAR RETRACTION. FOLLOWED ABNORMAL PROCEDURES AND LIGHT STAYED ON. RETURNED TO MIA AND MADE LANDING WITHOUT INCIDENT. FOUND RIGHT DOOR LATCH SWITCH ROLLER MISSING. REPLACED SWITCH CHECKS OK PER
- [SDR 96ZZZM1289](https://openairdocs.org/sdr/96ZZZM1289.md): Ballast · defective · Aug 18, 1996 · N426FB · Doug DC8F54 · Flight Compartment Lighting
  > AFTER LANDING MIAMI, INSTRUMENT WHITE LIGHT BALLAST STARTED TO SMOKE. PULLED CIRCUIT BREAKER. INSPECTION REVEALED DEFECTIVE BALLAST. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 96ZZZM1247](https://openairdocs.org/sdr/96ZZZM1247.md): Rod Assy · broken · Aug 6, 1996 · N426FB · Doug DC8F54 · Landing Gear Door Retract Section
  > AFTER TAKEOFF, PARAMARIBO, EXPERIENCED LOUD NOISE AND SLIGHT VIBRATION IN NOSE AREA. DIVERTED TO POS AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A BROKEN ROD ASSY AT THE STRUT END ON THE AFT RIGHT NOSE GEAR DOOR. REPLACED ROD ASSEMBLY, PERFORMED GEAR S
- [SDR 96ZZZX3635](https://openairdocs.org/sdr/96ZZZX3635.md): Clevis · cracked · Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF.125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110-3 ISSUED BY DER SW-713.
- [SDR 96ZZZX3634](https://openairdocs.org/sdr/96ZZZX3634.md): Clevis · cracked · Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF.125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-
- [SDR 96ZZZM1229](https://openairdocs.org/sdr/96ZZZM1229.md): Clevis · cracked · Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF.125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-3 IS
- [SDR 96ZZZM1228](https://openairdocs.org/sdr/96ZZZM1228.md): Clevis · crack · Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE CLEVIS ON THE LEFT WING INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF.125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110 ISSUE
- [SDR 96ZZZM873](https://openairdocs.org/sdr/96ZZZM873.md): Controller · overheated · Apr 19, 1996 · N426FB · Doug DC8F54 · Autopilot System
  > IN CRUISE EXPERIENCED O-ZONE ODOR AND INTERMITTENT SMOKE FROM BEHIND INSTRUMENT PANEL WHEN AUTO-PILOT WAS ENGAGED. GROUND INSPECTION REVEALED AUTOPILOT CONTROLLER WAS SHORTED/OVERHEATED. REPLACED CONTROLLER AND AIRCRAFT RETURNED TO SERVICE.
- [SDR 95ZZZZ234](https://openairdocs.org/sdr/95ZZZZ234.md): Rod Assy · unlocked · May 4, 1995 · N426FB · Doug DC8F54 · Landing Gear Door Retract Section
  > AFTER TAKEOFF MIAMI FELT SEVERE VIBRATION. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RT NOSE LANDING GEAR DOOR OPEN. CLEANED, LUBED AND RESET RT FWD DOOR ROD AND OPS CHECKED OK. PERFORMED OVERWEIGHT LANDING INSPECTION. RETURNED AC
- [SDR 95ZZZX2311](https://openairdocs.org/sdr/95ZZZX2311.md): Cap Assy · leaking · Apr 29, 1995 · N426FB · Doug DC8F54 · Fuel Storage
  > MIAMI - AFTER TAKEOFF, NOTED FUEL LOSS FROM NR 1 ALT FUEL TANK. RETURNED TO MIAMI. LANDED WITHOUT INCIDENT. INSPECTION REVEALED LEAKING FUEL TANK CAP AT NR 1 ALT TANK. REPLACED FUEL TANK CAP. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES 20,256.
- [SDR 95ZZZX1933](https://openairdocs.org/sdr/95ZZZX1933.md): Actuator · motor inop · Mar 27, 1995 · N426FB · Doug DC8F54 · Pressure Regulator/Outflow Valve
  > MIA - AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. RETURNED TO MIAMI AND MADE LANDING WITHOUT INCIDENT. PERFORMED OVERWEIGHT INSPECTION. GROUND INSPECTION REVEALED DEFECTIVE OUTFLOW VALVE ACTUATOR. REPLACED ACTUATOR AND GROUND CHECKED OKAY. RETURNED AIRC

## 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 = 'N426FB' AND deregistration_id = 'N426FB-2017-04-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N426FB-2017-04-07/reports

---
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