# Service difficulty reports: N660HA, cancelled Jul 20, 2005 A list on [N660HA, cancelled Jul 20, 2005](https://openairdocs.org/deregistered/N660HA-2005-07-20.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HALA0000323](https://openairdocs.org/sdr/HALA0000323.md): Control Cable · broken · Oct 2, 2000 · N660HA · Doug DC951 · Aileron Control System > HNL - FLT 288 - AILERON INPUT CAUSES EXCESSIVE ROLL ON LANDING. FOUND FDR AILERON POSITION SENSOR CABLE BROKEN. REMOVED, REPLACED AND NULLED FDR AILERON SURFACE POS SENSOR. OPS CHECKED OK FOR SERVICE. (X) - [SDR HALA0000264](https://openairdocs.org/sdr/HALA0000264.md): Harness · damaged · Aug 18, 2000 · N660HA · Doug DC951 · Landing Gear Position and Warning > HNL - FLT 382 - NOSE GEAR UNSAFE LIGHT STAYS ON AFTER GEAR LEVER SELECTED UP. WILL EXTINGUISH WITH GEAR HANDLE DOWN, NORMAL INDICATIONS. REPLACED NLG UPLOCK SENSOR HARNESS. GEAR SWING CHECK OK. (M) - [SDR HALA0000250](https://openairdocs.org/sdr/HALA0000250.md): Hinge · broken · Aug 5, 2000 · N660HA · Doug DC951 · Trailing Edge Flaps > OGG - FLT 520 - AFTER LANDING AT OGG, RIGHT WING FLAP WAS NOT RETRACTED FULLY. FURTHER INSPECTION BY MECHANICS FOUND RT WING OUTBOARD FLAP HINGE BROKEN. REMOVED AND REPLACED RT WING OUTBOARD FORWARD FLAP IDLER HINGE HALF, PER MM 27-10-0, OPS AND SECURITY CHE - [SDR HALA0000232](https://openairdocs.org/sdr/HALA0000232.md): Fitting · cracked · Jul 13, 2000 · N660HA · Doug DC951 · Trailing Edge Flaps > FLT 183 - LIH - LEFT OUTBOARD FLAP SUPPORT CRACKED. REMOVED AND REPLACED FLAP HINGE FITTING IDLER ASSEMBLY. RIGGED AILERON BUS CABLES PER MM 27-10-0. RIGGED AILERON TRIM CABLES PER MM 27-10-0. INSPECTION CHECK OK PER MM 27-10-0. SECURED ALL ACCESS PANELS. - [SDR HALA0000206](https://openairdocs.org/sdr/HALA0000206.md): O-Ring · leaking · Jun 29, 2000 · N660HA · Doug DC951 · Fuel Controlling System > HNL - FLT 357 - FUEL SMELL NOTICED ON TAXI IN HNL. REPLACED ALL SEALS ON RIGHT ENGINE AND P/D VALVE. ENGINE RUN, NO LEAKS. OPS OK. REMOVED AND REPLACED H20 SEPARATOR COALESCER BAGS. OPS CHECK OK. LEAK CHECK GOOD. (M) - [SDR HALA9900109](https://openairdocs.org/sdr/HALA9900109.md): Control Box · malfunctioned · May 4, 1999 · N660HA · Doug DC951 · Brake Anti-Skid Section > HNL - FLT 388 - ANTI-SKID WOULD NOT ARM PRIOR TO TAKEOFF. CONDITION CLEARED AFTER ENGINE SHUTDOWN. REPLACED ANTI-SKID CONTROL BOX. BITE TEST OK. (M) - [SDR HALA9900104](https://openairdocs.org/sdr/HALA9900104.md): Pump · failed · Apr 29, 1999 · N660HA · Doug DC951 · Hydraulic Pump (Electric/Engine), Main > HNL - LEFT ENGINE HYD PUMP FAILED. REPLACED LEFT ENGINE HYD PUMP PER MM 29-20-5 ENGINE RUN. OPS AND SECURITY CHECK OK AND LEAK CHECK OK. (M) - [SDR HALA9900004](https://openairdocs.org/sdr/HALA9900004.md): Fcu · malfunctioned · Jan 5, 1999 · N660HA · Doug DC951 · Fuel Control/Turbine Engines > HNL - FLT 102 - POWER SURGE RIGHT ENGINE AT MID RANGE EPR SETTINGS, CLIMB POWER. EPR VARIED PLUS/MINUS.05. N1 PLUS/MINUS 2 PERCENT. NOT EVIDENT AT TAKEOFF POWER OR AT IDLE, A/C RETURNED TO HNL WHERE AN UNEVENTFUL LANDING WAS MADE. (M) - [SDR HALA9800369](https://openairdocs.org/sdr/HALA9800369.md): Valve · malfunctioned · Oct 26, 1998 · N660HA · Doug DC951 · Cabin Pressure Control System > ITO - FLT 182 - AT TOP OF DESCENT FROM FL 250, UNABLE TO MAINTAIN CABIN PRESSURIZATION WITH LESS THAN CRUISE POWER AND OUTFLOW VALVE FULLY CLOSED IN MANUAL. REMOVED AND REPLACED FLOW CONTROL VALVE ASSEMBLY. OPS CHECK, LEAK CHECK OK ON GROUND RUN. (M) - [SDR HALA9800325](https://openairdocs.org/sdr/HALA9800325.md): Press Controller · failed · Sep 15, 1998 · N660HA · Doug DC951 · Cabin Pressure Controller > ITO - FLT 102 - DEPLOYED CABIN OXYGEN MASK INFLIGHT. CABIN PRESSURE CONTROLLER IN FULL CLOSED POSITION. FERRIED A/C UNPRESSURIZED FROM ITO TO HNL, A/C MADE AN UNEVENTFUL LANDING IN HNL. REMOVED AND REPLACED BOTH ENG SEG SW AND PASSENGER OXYGEN REGUALTOR PER - [SDR HALA9800257](https://openairdocs.org/sdr/HALA9800257.md): Battery · discharged · Jul 22, 1998 · N660HA · Doug DC951 · Emergency Lighting > HNL - LOG PAGE NR A164796/A164794 - PER FLEET CAMPAIGN, OVERHEAD LIGHTS FROM ROWS 13 TO 17 AND AFT TAIL EMERGENCY LIGHTS FAILED CHECK. REPLACED BATTERY, OPS CHECK GOOD. (X) - [SDR HALA9800178](https://openairdocs.org/sdr/HALA9800178.md): Power Supply · failed · Jun 25, 1998 · N660HA · Doug DC951 · Emergency Lighting > HNL - FLT 103 - (LOG PAGE NR A144870) - BOTH FORWARD OVER-WING EXIT EMERGENCY LIGHTS DO NOT COME ON. REPLACED THE OVER-WING POWER SUPPLY AND THE OPERATIONAL CHECK WAS OK. (X) - [SDR HALA9800128](https://openairdocs.org/sdr/HALA9800128.md): Conduit · broken · May 17, 1998 · N660HA · Doug DC951 · Landing Gear Position and Warning > HNL - FLT 204 - (LOG PAGE A140278). AFTER GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON IN CRUISE. FOUND NOSE GEAR LOCK SENSOR CONDUIT BROKEN. REPLACED NOSE GEAR LOCK SENSOR CONDUIT, OK FOR SERVICE. (X) - [SDR HALA9800007](https://openairdocs.org/sdr/HALA9800007.md): Batteries · discharged · Jan 12, 1998 · N660HA · Doug DC951 · Emergency Lighting > HNL - FLT 106 - ONE FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS IN THE CABIN ARE VERY DIM. REPLACED EMERGENCY LIGHT BATTERIES. THE OPERATIONAL CHECK WAS GOOD. (M) - [SDR HALA9800017](https://openairdocs.org/sdr/HALA9800017.md): Skin · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE LEFT CANTED BULKHEAD FUSELAGE SKIN AT STATION 1337, LONGERON 25L. REPAIRED BY TRIMMING OUT THE CORRODED OVERLAPPING SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR SKIN FILLER, EXTERNAL REPAIR DO - [SDR HALA9800016](https://openairdocs.org/sdr/HALA9800016.md): Skin · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Wing, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT LOWER WING FORWARD SKIN AT XRS 362 BY BLENDING OUT THE CORROSION, FABRICATING AND INSTALLING REPAIR DOUBLERS WET WITH SEALANT. ACCOMPLISHED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHOR - [SDR HALA9800015](https://openairdocs.org/sdr/HALA9800015.md): Doubler · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Fuselage Miscellaneous Structure > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT REAR SPAR BULKHEAD DOUBLER AT STATION 1292.22, LONGERONS 16R AND 20R. REPAIRED BY TRIMMING OUT THE CORROSION, FABRICATING AND INSTALLING REPAIR DOUBLER SECTION, TITANIUM REPAIR SPLICES AND SHIMS WET - [SDR HALA9800014](https://openairdocs.org/sdr/HALA9800014.md): Skin · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Fuselage Main, Plate/Skin > DURNG C-CHECK INSPECTION, DISCOVERED CORROSION ON THE LEFT CANTED BULKHEAD FUSELAGE SKIN LAP SEAM AT STATION 1291 AND 1326 ALONG LONGERON 16L. REPAIRED BY TRIMMING OUT THE CORRODED OVERLAPPING SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR SKIN FILL - [SDR HALA9800013](https://openairdocs.org/sdr/HALA9800013.md): Chord · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Trailing Edge Flaps > DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT FLAP SPAR UPPER TEE CHORD AT XFLS 187.406. REPAIRED BY BLENDING OUT THE CORRODED AREA, HFEC INSPECTING, ROTO PEENING AND REINSTALLING FITTING REMOVED FOR ACCESS WITH 301 CRES SHIMS TO FILL VOID CREA - [SDR HALA9800012](https://openairdocs.org/sdr/HALA9800012.md): Skin · cracked · Dec 31, 1997 · N660HA · Doug DC951 · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED WRINKLES AND CRACKED SKIN ON THE LEFT SIDE OF THE FLT COMPARTMENT BETWEEN STATION 94 AND 120, APPROXIMATELY 12 INCHES BELOW THE PILOTS SLIDING WINDOW CUTOUT. REPAIRED BY TRIMMING OUT THE DAMAGED SKIN, HFEC INSPECTING, FAB - [SDR HALA9800011](https://openairdocs.org/sdr/HALA9800011.md): Spar · corroded · Dec 31, 1997 · N660HA · Doug DC951 · Trailing Edge Flaps > DURINC C-CHECK INSPECTION, DISCOVERED CORROSION ON THE LEFT FLAP FRONT SPAR LOWER CAP BETWEEN XFLS 299.601 AND 304.031. REPAIRED BY BLENDING OUT THE EXFOLIATION CORROSION, HFEC INSPECTING, ROTO PEENING, REINSTALLING FITTING REMOVED FOR ACCESS WITH 301 CRES SH - [SDR HALA9800010](https://openairdocs.org/sdr/HALA9800010.md): Skin · cracked · Dec 31, 1997 · N660HA · Doug DC951 · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, DISCOVERED CRACKED FUSELAGE SKIN AT STATION 1167, LONGERON 19L. REPAIRED BY TRIMMING OUT THE DAMAGE, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR FILLER AND EXTERNAL REPAIR DOUBLER WET WITH SEALANT. ACCOMPLISHED IAW EVERGREEN - [SDR HAL97125](https://openairdocs.org/sdr/HAL97125.md): Schrader Valve · leaking air · Jun 12, 1997 · N660HA · Doug DC951 · Nose/Tail Landing Gear Strut/Axle > HNL - FLT 158 - FROM LOG PAGE 128188: NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO HNL. REPLACED SCHRADER VALVE AND SEAL DUE LEAKING AIR. RE-SERIVCED NOSE STRUT PER MM. GEAR SWING MADE AND OPERATION OK. (X) ## 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 = 'N660HA' AND deregistration_id = 'N660HA-2005-07-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N660HA-2005-07-20/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.