# N660HA: Mcdonnell Douglas DC-9-51, registration cancelled 2005-07-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 20, 2005 - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-51](https://openairdocs.org/model/mcdonnell-douglas-dc-9-51) (registry code 3022051) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 48122 - Year built: 0 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 2, 1997 - Certificate issued: July 9, 2002 - Last registry action: June 21, 2005 - Mode S code: A8B4E9 - Owner when cancelled: [Ram Air Sales Inc](https://openairdocs.org/faa-owner/RAM%20AIR%20SALES%20INC) - Location: [Miami Springs, FL](https://openairdocs.org/faa-place/FL/Miami%20Springs) - Owner type: Corporation - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N660HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=660HA - Page: https://openairdocs.org/deregistered/N660HA-2005-07-20 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-51: https://openairdocs.org/model/mcdonnell-douglas-dc-9-51.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HALA0000323](https://openairdocs.org/sdr/HALA0000323), Oct 2, 2000: CONTROL CABLE. BROKEN. HNL - FLT 288 - AILERON INPUT CAUSES EXCESSIVE ROLL ON LANDING. FOUND FDR AILERON POSITION SENSOR CABLE BROKEN. REMOVED, REPLACED AND NULLED FDR AILERON SURFACE - [SDR HALA0000264](https://openairdocs.org/sdr/HALA0000264), Aug 18, 2000: HARNESS. DAMAGED. 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 SEN - [SDR HALA0000250](https://openairdocs.org/sdr/HALA0000250), Aug 5, 2000: HINGE. BROKEN. 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 - [SDR HALA0000232](https://openairdocs.org/sdr/HALA0000232), Jul 13, 2000: FITTING. CRACKED. 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 AIL - [SDR HALA0000206](https://openairdocs.org/sdr/HALA0000206), Jun 29, 2000: O-RING. LEAKING. 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 SEPA - [SDR HALA9900109](https://openairdocs.org/sdr/HALA9900109), May 4, 1999: CONTROL BOX. MALFUNCTIONED. 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), Apr 29, 1999: PUMP. FAILED. 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), Jan 5, 1999: FCU. MALFUNCTIONED. 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 POWE - [SDR HALA9800369](https://openairdocs.org/sdr/HALA9800369), Oct 26, 1998: VALVE. MALFUNCTIONED. 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. REM - [SDR HALA9800325](https://openairdocs.org/sdr/HALA9800325), Sep 15, 1998: PRESS CONTROLLER. FAILED. 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 U - [SDR HALA9800257](https://openairdocs.org/sdr/HALA9800257), Jul 22, 1998: BATTERY. DISCHARGED. 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 CHE - [SDR HALA9800178](https://openairdocs.org/sdr/HALA9800178), Jun 25, 1998: POWER SUPPLY. FAILED. 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 CHE - [SDR HALA9800128](https://openairdocs.org/sdr/HALA9800128), May 17, 1998: CONDUIT. BROKEN. 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 NO - [SDR HALA9800007](https://openairdocs.org/sdr/HALA9800007), Jan 12, 1998: BATTERIES. DISCHARGED. 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. - [SDR HALA9800017](https://openairdocs.org/sdr/HALA9800017), Dec 31, 1997: SKIN. CORRODED. DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE LEFT CANTED BULKHEAD FUSELAGE SKIN AT STATION 1337, LONGERON 25L. REPAIRED BY TRIMMING OUT THE CORRODED O - [SDR HALA9800016](https://openairdocs.org/sdr/HALA9800016), Dec 31, 1997: SKIN. CORRODED. 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 - [SDR HALA9800015](https://openairdocs.org/sdr/HALA9800015), Dec 31, 1997: DOUBLER. CORRODED. 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 - [SDR HALA9800014](https://openairdocs.org/sdr/HALA9800014), Dec 31, 1997: SKIN. CORRODED. 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 TRIMM - [SDR HALA9800013](https://openairdocs.org/sdr/HALA9800013), Dec 31, 1997: CHORD. CORRODED. 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 INSPECT - [SDR HALA9800012](https://openairdocs.org/sdr/HALA9800012), Dec 31, 1997: SKIN. CRACKED. 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 BELO - [SDR HALA9800011](https://openairdocs.org/sdr/HALA9800011), Dec 31, 1997: SPAR. CORRODED. 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 - [SDR HALA9800010](https://openairdocs.org/sdr/HALA9800010), Dec 31, 1997: SKIN. CRACKED. DURING C-CHECK INSPECTION, DISCOVERED CRACKED FUSELAGE SKIN AT STATION 1167, LONGERON 19L. REPAIRED BY TRIMMING OUT THE DAMAGE, HFEC INSPECTING, FABRICATING AND - [SDR HAL97125](https://openairdocs.org/sdr/HAL97125), Jun 12, 1997: SCHRADER VALVE. LEAKING AIR. 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 ## Other aircraft with N660HA - [Registered now](https://openairdocs.org/aircraft/N660HA): Bell Helicopter Textron 206L-1, S/N 45219, built 1979 --- 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.