# Service difficulty reports: N420EA, cancelled May 16, 2006 A list on [N420EA, cancelled May 16, 2006](https://openairdocs.org/deregistered/N420EA-2006-05-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HALA0000055](https://openairdocs.org/sdr/HALA0000055.md): Strut · discharged · Feb 12, 2000 · N420EA · Doug DC951 · Nose/Tail Landing Gear Attach Section > KOA - FLT 247 - AIRCRAFT WAS UNABLE TO RAISE LANDING GEAR (NOSE), GEAR (RED) LIGHT REMAINED ON WITH GEAR HORN. ON RETRACTION, AIRCRAFT RETURNED TO KOA, WHERE A SUCCESSFUL LANDING WAS MADE. FERRIED A/C BACK TO HNL, CHECKED NOSE GEAR FOR CONDITION AND SECURITY - [SDR HALA9900199](https://openairdocs.org/sdr/HALA9900199.md): Valves · inoperative · Oct 14, 1999 · N420EA · Doug DC951 · Brake Anti-Skid Section > HNL - LEFT OUTBOARD TIRE BLEW WHILE TURNING OFF RUNWAY. POSSIBLE ANTI-SKID FAILURE. DAMAGE TO FLAP ARTICULATING ELBOW AND FLYING GEAR DOOR. REPLACED NR 1 AND NR 2 MAIN TIRES. CDL FOR FLY DOOR AND MEL FOR ANTI-SKID FERRIED PLANE W/GEAR DOWN TO HNL. ON ARRI - [SDR HALA9900018](https://openairdocs.org/sdr/HALA9900018.md): Fire Loop · chafed · Jan 19, 1999 · N420EA · Doug DC951 · Fire Detection > FLT 509 - HNL - NR 2 ENGINE FIRE DET LOOP 'A' LIGHT CAME ON DURING FLIGHT. FIRE TEST OK. SELECTED LOOP 'B'. REPAIRED CHAFED WIRE, OPS CHECK OK. (M) - [SDR HALA9800334](https://openairdocs.org/sdr/HALA9800334.md): Light · inoperative · Oct 1, 1998 · N420EA · Doug DC951 · Emergency Lighting > FLT 128 - HNL - SEVERAL OF THE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED INOPERATIVE BULBS AND THE OPERATIONAL CHECK WAS OK. (M) - [SDR HALA9800242](https://openairdocs.org/sdr/HALA9800242.md): Battery · discharged · Jul 15, 1998 · N420EA · Doug DC951 · Emergency Lighting > HNL - TAIL CONE EMERGENCY LIGHTS DIM. FAILED TEST. RELAMPED AND REPLACED BATTERIES, CLEANED CONTACTS. OPS CHECK OK. (M) - [SDR HALA9800085](https://openairdocs.org/sdr/HALA9800085.md): Controller · failed · Apr 5, 1998 · N420EA · Doug DC951 · Cabin Pressure Controller > FLT 561 - HNL - CABIN ALTITUDE INDICATES BELOW SEA LEVEL WHEN CABIN PRESSURE CONTROL IS SET TO SEA LEVEL. CABIN PRESSURE CLIMB RAPIDLY ON TOUCH DOWN. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, PRESSURIZATION AND LEAK CHECK GOOD. (M) - [SDR HALA9800078](https://openairdocs.org/sdr/HALA9800078.md): Controller · failed · Apr 1, 1998 · N420EA · Doug DC951 · Cabin Pressure Controller > OGG - FLT 533 - LOG PAGE A142518. DURING LIFT-OFF AND EXTENSION OF NOSE GEAR, THE CABIN PRESSURE DESCENDS MORE THAN 1,500 FPM. REPLACED CABIN PRESSURE CONTROLLER. (X) - [SDR HALA9800070](https://openairdocs.org/sdr/HALA9800070.md): Fuel Control · malfunctioned · Mar 22, 1998 · N420EA · Doug DC951 · Fuel Control/Turbine Engines > HNL - FLT 508 - DURING CLIMB-OUT AT TAKEOFF POWER 2.05 THE RIGHT ENGINE HAD A FLUCTUATION OF 2.01 TO 2.08 ON THE EPR. ALL OTHER ENGINE GAUGES SHOWED SAME FLUCTUATION ON THE RT ENGINE. REMOVED AND REPLACED NR 2 ENGINE FCU PER HAL 97.6. GROUND RUN CHECK OK. - [SDR HALA9800009](https://openairdocs.org/sdr/HALA9800009.md): Skin · corroded · Dec 23, 1997 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE FUSELAGE SKIN LAP SEAM AT BS 908, LONGERON 26R. REPAIRED BY TRIMMING OUT THE CORRODED OVERLAPPING SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR SKIN FILLER, INTERNAL FINGER DOUBLER AND EXTERNAL - [SDR 98ZZZX562](https://openairdocs.org/sdr/98ZZZX562.md): Skin · corroded · Dec 23, 1997 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE FUSELAGE SKIN LAP SEAM AT BS 908, LONGERON 26R. REPAIRED BY TRIMMING OUT THE CORRODED OVERLAPPING SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR SKIN FILLER, INTERNAL FINGER DOUBLER AND EXTERNAL - [SDR HAL97111](https://openairdocs.org/sdr/HAL97111.md): Prox Switch · malfunctioned · May 21, 1997 · N420EA · Doug DC951 · Landing Gear Position and Warning > HNL - FLT 505 - FROM LOG PAGE 122503: LEFT GEAR UNSAFE LIGHT ON DURING CRUISE. MAINTENANCE CONTROL ADVISED TO RECYCLE LANDING GEAR AND STILL HAD AN UNSAFE LGT WITH A NOSE GEAR UNSAFE LGT ON. OBVIOUS SLIP STREAM NOISE IN AIRCRAFT. REMOVED AND REPLACED NOSE - [SDR HAL9688](https://openairdocs.org/sdr/HAL9688.md): Oil Press Xmtr · malfunctioned · Jul 1, 1996 · N420EA · Doug DC951 · Engine Oil Pressure > HNL - FLT 540 - DURING TAKEOFF ROLL, RIGHT ENGINE OIL PRESSURE GAUGE DROPPED TO ZERO. ABORTED TAKEOFF. RETURNED TO GATE. REPLACED OIL PRESSURE TRANSMITTER ON NR 2 ENGINE. CHECKED CONDITION AND SECURITY OF CANNON PLUG AND WIRING ON ENGINE. OPERATIONAL CHEC - [SDR HALA9657](https://openairdocs.org/sdr/HALA9657.md): Skin · damaged · May 2, 1996 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > HNL - IN C-CHECK, FOUND 2 FASTENERS PULLED THROUGH ON FUSELAGE SKIN NEAR AFT CARGO DOOR AT STATION 1111 AT LONGERON 28R. SKIN BULGING, CORROSION LEVEL 2. MADE INTERIM REPAIR PER HAL M105, CUT OUT CORROSION, FABRICATED DOUBLER, FILLER AND INSTALLED PER DAC TE - [SDR HALA9658](https://openairdocs.org/sdr/HALA9658.md): Skin · corroded · Apr 25, 1996 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > HNL - IN C-CHECK, FOUND LOWER FUSELAGE SKIN BELOW AND UNDER FORWARD CARGO DOOR SCUFF PLATE HAS MODERATE CORROSION, LEVEL 2. MADE REPAIR PER HAL M105, CUT OUT CORROSION, FABRICATED EXTERNAL AND INTERNAL DOUBLER, FILLER AND INSTALLED PER HNL-SVC-060/RPM DATED A - [SDR HALA95165](https://openairdocs.org/sdr/HALA95165.md): Bracket · bent · Dec 1, 1995 · N420EA · Doug DC951 · Landing Gear Door Retract Section > HNL - FLT NR 128 - AFTER TAKEOFF WHEN NOSE WHEEL RETRACTION, LOUD BANG WAS HEARD IN NOSE WHEEL COMPARTMENT ALONG WITH EXCESS VIBRATION. RETURNED FOR LANDING. UPON INSPECTION OF NLG FOUND, HOLE IN NLG LEFT AFT FIXED DOOR INTERIOR FWD SIDE. LEFT AFT FIXED DOO - [SDR HAL95145](https://openairdocs.org/sdr/HAL95145.md): Battery · discharged · Nov 8, 1995 · N420EA · Doug DC951 · Emergency Lighting > HNL - INFORMATION FROM LOG PAGE 146503 - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 2-7 INOPERATIVE AND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 17-21 ARE DIM. (X) - [SDR HAL95137](https://openairdocs.org/sdr/HAL95137.md): Battery Pack · discharged · Oct 17, 1995 · N420EA · Doug DC951 · Emergency Lighting > HNL - INFORMATION FROM LOG PAGE 143713-2. BOTH AFT OVERWING EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (X) - [SDR HALA95129](https://openairdocs.org/sdr/HALA95129.md): Eyebolt · broken · Oct 1, 1995 · N420EA · Doug DC951 · Leading Edge Slat Control System > FLT NR 561 - ON INITIAL SLAT EXTENSION IN FLIGHT AIRCRAFT ROLLED TO THE LEFT. NO SLAT EXTENDED LIGHT ON. RETRACTED SLATS AND AIRCRAFT RETURNED TO NORMAL TRIM. ALL SUBSEQUENT SLAT EXTENSIONS CAUSED THE AIRCRAFT TO ROLL LEFT, THEN SLAT EXTEND LIGHT COMES ON. - [SDR HAL95068](https://openairdocs.org/sdr/HAL95068.md): Eel Battery · discharged · Jun 5, 1995 · N420EA · Doug DC951 · Emergency Lighting > HNL - EMERGENCY CEILING LIGHTS ROWS 18-21 ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (X) - [SDR HAL95067](https://openairdocs.org/sdr/HAL95067.md): Fitting · cracked · May 23, 1995 · N420EA · Doug DC951 · Vertical Stabilizer, Spar/Rib > SBA - THE UPPER LEFT RUDDER HINGE AT THE REAR SPAR OF THE VERTICAL STABILIZER HAS SURFACE CORROSION AND FITTING IS CRACKED AT THE OUTBOARD SIDE OF THE FASTENER HOLE. REPLACED RUDDER HINGE 'A' ARM IAW MM 27-20-1. (W) - [SDR HAL95066](https://openairdocs.org/sdr/HAL95066.md): Le Cap · corroded · May 23, 1995 · N420EA · Doug DC951 · Trailing Edge Flaps > SBA - THE LEFT WING OUTBOARD LEADING EDGE CAP IS EXFOLIATED ON FLAP AT THE BASE OF FOREFLAP MOUNTS IN 3 LOCATIONS. REMOVED THE DAMAGED CAP AND SENT OUT FOR OVERHAUL. INSTALLED THE OVERHAULED CAP PER SRM 51-30-01. (W) - [SDR HAL95065](https://openairdocs.org/sdr/HAL95065.md): Fitting · cracked · May 21, 1995 · N420EA · Doug DC951 · Fuselage Miscellaneous Structure > LEFT REAR SPAR TO TRAPEZOIDAL PANEL ATTACH FITTING CRACKED AT THE LOWER INBOARD BOLT HOLE. THE CRACK WAS DETECTED DURING AN ULTRA-SONIC INSPECTION. REMOVED AND REPLACED THE REAR SPAR TRAPEZOIDAL FITTING AT LEFT FUSELAGE STATION 794, PER SRM 51-30-02. (W) - [SDR HAL95064](https://openairdocs.org/sdr/HAL95064.md): Angle · cracked · May 21, 1995 · N420EA · Doug DC951 · Fuselage Miscellaneous Structure > THE LEFT DORSAL FIN ATTACH ANGLE HAS A CONDITION 2 CRACK IN THE VERTICAL LEG REF EO 53-92-32-91 FIG 1. REMOVED THE LEADING EDGE PANEL, REMOVED AND REPLACED THE DORSAL FIN ATTACH ANGLE WITH A NEW ATTACH ANGLE. REINSTALLED THE LEADING EDGE PANEL PER SRM 51-30- - [SDR HAL95022](https://openairdocs.org/sdr/HAL95022.md): Adi · failed · Feb 18, 1995 · N420EA · Doug DC951 · Attitude Gyro and Indicating System > FLT NR 172 - HNL - CAPTAINS ADI GYRO FLAG ON ADI STUCK ON 12 DEGREES NOSE-UP. MADE AIR TURN BACK TO HNL. REMOVED AND REPLACED THE CAPTAINS ADI AND THE GROUND OPERATIONAL CHECK WAS OK. (W) - [SDR HAL95003](https://openairdocs.org/sdr/HAL95003.md): Skin · cracked · Jan 3, 1995 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > HNL - ITEM FROM FORM 46 NR 138536 DURING SERVICE CHECK. LEFT FUSELAGE SKIN CRACKED APPROXIMATELY.6250 INCH AT STA 1209 APPROXIMATELY 9 INCHES ABOVE LEFT ENGINE PYLON. (X) - [SDR HAL95002](https://openairdocs.org/sdr/HAL95002.md): Skin · cracked · Jan 3, 1995 · N420EA · Doug DC951 · Fuselage Main, Plate/Skin > HNL - ITEM FROM FORM 46 NR 138535 DURING SERVICE CHECK. RIGHT FUSELAGE SKIN CRACKED APPROXIMATELY.75 INCH AT STA 1209 APPROXIMATELY 13 INCHES ABOVE RIGHT ENGINE PYLON. REPAIRED MADE PER HAL AIRCRAFT REPAIR AUTHORIZATION FORM M105 FILE NR 71035. (CUT-OUT DA ## 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 = 'N420EA' AND deregistration_id = 'N420EA-2006-05-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N420EA-2006-05-16/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.