# N661HA: 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)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 47796
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 29, 2002
- Last registry action: June 21, 2005
- Mode S code: A8B8A0
- 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/N661HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=661HA
- Page: https://openairdocs.org/deregistered/N661HA-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 (47)

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

- [SDR HALA0100056](https://openairdocs.org/sdr/HALA0100056), Feb 23, 2001: GCU. FAILED. FLT 184 - HNL - AIRCRAFT X-TIE LOCKOUT LIGHT CAME ON IN FLIGHT. IT CAUSED A DOUBLE GENERATOR FAILURE, RESET GENERATORS IN FILGHT. APU WAS RESTARTED SUCCESSFULLY
- [SDR HALA0000240](https://openairdocs.org/sdr/HALA0000240), Jul 26, 2000: ACM. FAILED. OGG - FLT 112 - SMOKE AND VERY STRONG BURNING SMELL IN CABIN WITH NR 1 LEFT AC PACK ON. OK TO CONTINUE PER MEL 21-1 DMI NR 13681 TRANSCRIBED TO HAL M443 AND MPC
- [SDR HALA9900195](https://openairdocs.org/sdr/HALA9900195), Sep 24, 1999: COTTER KEY. OUT OF POSITION. FLT 113 - HNL - ON APPROACH TO LIH, WHEN GEAR HANDLE PLACED DOWN, BOTH MAINS CAME DOWN. NOSE GEAR DID NOT COME DOWN. FOLLOWED SOP. RETURNED HNL. GEAR CAME DOWN 
- [SDR HALA9900194](https://openairdocs.org/sdr/HALA9900194), Jul 2, 1999: WINDOW. CRACKED. MAE - CABIN WINDOW NR 26 LEFT INTERNAL DOUBLER TOP FORWARD EDGE IS CRACKED AT STATION 693 LONGERON 12L. REPAIRED WINDOW RING PAN IAW EA 9-5310-19-A0458 AND SRM 
- [SDR HALA9900193](https://openairdocs.org/sdr/HALA9900193), Jul 1, 1999: SPLICE. CRACKED. MAE - FUSELAGE SKIN PRODUCTION SPLICE IS CRACKED JUST BELOW LONGERON 17R BETWEEN FS 1247 AND FS 1258. TRIM OUT OF PRODUCTION SPLICE BETWEEN LONGERON 17R AND 16R
- [SDR HALA9900192](https://openairdocs.org/sdr/HALA9900192), Jun 30, 1999: PANEL. CORRODED. MAE - LEFT WING TE FLAP LOWER SIDE AT PANEL 1523A, SKIN AND RIB ARE CORRODED. REMOVED AND REPLACED RIB, ANGLE, AND SKIN IAW SRM 51-30-2 AND 51-30-5. (M)
- [SDR HALA9900191](https://openairdocs.org/sdr/HALA9900191), Jun 30, 1999: LONGERON. CRACKED. AFT CARGO LONGERON 26L IS CRACKED AT STATION 964. REMOVED AND INSTALLED REPAIR TO LONGERON 26L IAW SRM 51-30-2 AND 51-30-5 AND EA 9-5314-19-A0469. (M)
- [SDR HALA9900190](https://openairdocs.org/sdr/HALA9900190), Jun 30, 1999: SKIN. CORRODED. MAE - RT WING T/E FLAP INBOARD END OUTER SKIN HAS CORROSION ON ENTIRE AREA AFT OF MOVEABLE VANE. REMOVED SKIN AND DOUBLER AND REPLACED IAW 51-30-2 AND 51-10-4 A
- [SDR HALA9900119](https://openairdocs.org/sdr/HALA9900119), May 22, 1999: SWITCH. FAILED. HNL - FLT 106 - FLIGHT ATTENDANTS REPORT HAZE AND UNUSUAL ODOR IN CABIN AND SMOKE ALARM ACTIVATION. REPLACED APU OIL PRESSURE SEQUENCE SWITCH, OPS CHECK OK. (M)
- [SDR HALA9800346](https://openairdocs.org/sdr/HALA9800346), Oct 14, 1998: BATTERY. DISCHARGED. HNL - FLT 106 - EMERGENCY LIGHTS OVERHEAD, INOP ROWS 6-10. REMOVED AND REPLACED BATTERY, OPS CHECK GOOD. (M)
- [SDR HALA980340](https://openairdocs.org/sdr/HALA980340), Oct 11, 1998: BATTERY. DISCHARGED. HNL - FLT 102 - (LOG PAGE NR A 154589) - OVERHEAD EMERGENCY LIGHTS ROWS 6-11 INOPERABLE. REPLACED BATTERY, OPS CHECK OK. (X)
- [SDR HALA9800264](https://openairdocs.org/sdr/HALA9800264), Jul 23, 1998: BATTERY. DISCHARGED. HNL - LOG PAGE NR A143926 - EMERGENCY LIGHTS CEILING BATH ABOVE ROW 10 HAS A WEAK BATTERY. REPLACED BATTERY, OPS CHECK GOOD. (X)
- [SDR HALA9800129](https://openairdocs.org/sdr/HALA9800129), May 21, 1998: SENSOR TARGET. WORN. HNL - FLT 61 - (LOG PAGE A140341). ON CLIMB-OUT WITH HYDRAULIC PUMP ON HIGH, RT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON. IT STAYED ON APPROXIMATELY 3
- [SDR HALA9800123](https://openairdocs.org/sdr/HALA9800123), Apr 22, 1998: CONTROL CABLE. BINDING. ITO - FLT 122 - (LOG PAGE A140193). LEFT ENGINE STUCK IN IDLE. NO RESPONSE FROM THROTTLES. FOUND POWER CABLE ON QUADRANT, ENGINE SIDE BINDING. RE-SECURED POWER 
- [SDR HALA9800071](https://openairdocs.org/sdr/HALA9800071), Mar 24, 1998: BATTERIES. DISCHARGED. HNL - FLT 512 - EMERGENCY LIGHT CEILING ROW 6-12 DOES NOT COME ON DURING PREFLIGHT TEST. REPLACED BATTERY FOR EMERGENCY LIGHTS FOR ROW 6-12, OPS CHECK OK. (M)
- [SDR HALA9800053](https://openairdocs.org/sdr/HALA9800053), Feb 24, 1998: CHAFE STRIPS. FAILED. HNL - FLT 177 - LOG PAGE NR A137992 - FLUTTER/VIBRATION AND RUMBLE FELT AT .75 MACH AND ABOVE. (FEELS AERODYNAMICALLY GENERATED). REMOVED AND REPLACED TWO CHAFE
- [SDR HALA9800047](https://openairdocs.org/sdr/HALA9800047), Feb 16, 1998: BATTERIES. DISCHARGED. HNL - LOG PAGE NR A136850 - CAPTAIN'S OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES AND THE OPERATIONAL CHECK WAS OK. (X)
- [SDR HALA970036](https://openairdocs.org/sdr/HALA970036), Nov 5, 1997: FITTING. CORRODED. DURING C-CHECK INSPECTION, FOUND FITTING P/N 3932805-501 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED FITTING IAW SRM 53-04 FIG 43 SHEET 3. (M)
- [SDR HALA9700314](https://openairdocs.org/sdr/HALA9700314), Nov 5, 1997: LONGERON. CORRODED. LONGERON 30 CORRODED BEYOND LIMITS BETWEEN MLG WELLS. FABRICATED AND INSTALLED LONGERON PER SRM 53-04 FIGURE 43. (M)
- [SDR HALA9700313](https://openairdocs.org/sdr/HALA9700313), Nov 5, 1997: FITTING. CORRODED. FITTING P/N 3932805-501 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED FITTING IAW SRM 53-04 FIG 43 SHEET 3. (M)
- [SDR HALA9700310](https://openairdocs.org/sdr/HALA9700310), Nov 5, 1997: FRAME. CORRODED. FOUND CORROSION AT BASE OF TAILCONE FRAME, APPROX 28 INCHES LEFT AND RIGHT OF 6 O'CLOCK POSITION. REMOVED DAMAGED FRAMES, INSTALLED NEW FRAMES PER SRM 51-30-0 A
- [SDR HALA9700309](https://openairdocs.org/sdr/HALA9700309), Nov 5, 1997: LONGERON. CORRODED. LOWER FUSELAGE CORROSION ON LONGERON 28R FS 733-753. REMOVED DAMAGED SECTION, ACCOMPLISHED SPLICE REPAIR PER SRM 51-30-05 AND 53-02. (M)
- [SDR HALA9700308](https://openairdocs.org/sdr/HALA9700308), Nov 5, 1997: LONGERON. CORRODED. LONGERON 30 BETWEEN FS 870-889 IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03 FIG 2A - 7005 
- [SDR HALA9700307](https://openairdocs.org/sdr/HALA9700307), Nov 5, 1997: DOUBLER. CRACKED. INTERNAL TITANIUM DOUBLER BETWEEN FS 654 AND 699 LONGERON 25L TO 25R IS CRCKED AT LONGERON 25R. GAINED ACCESS, TRIMMED OUT DAMAGE. VERIFIED DAMAGE CONTAINMENT B
- [SDR HALA9700304](https://openairdocs.org/sdr/HALA9700304), Nov 5, 1997: FRAME. CRACKED. FOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF CAPTAINS WINDSHIELD, APPROX FS 83 BY 9. FABRICATED AND INSTALLED TWO DOUBLERS FROM 7075-T6 .090 INCH PE
- [SDR HALA9700303](https://openairdocs.org/sdr/HALA9700303), Nov 5, 1997: FRAME. CRACKED. CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF F/O WINDSHIELD, APPROX FS 83 BY 9.0. STOP DRILLED CRACK, FABRICATED AND INSTALLED TWO ANGLE REPAIR PER SRM 53
- [SDR HALA9700302](https://openairdocs.org/sdr/HALA9700302), Nov 5, 1997: TRUNNION. CORRODED. RIGHT MLG TRUNNION FITTING HAS CORROSION ON OUTBOARD WING MOUNT FLANGE. REPLACED TRUNNION FITTING AND BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-
- [SDR HALA9700301](https://openairdocs.org/sdr/HALA9700301), Nov 5, 1997: TRUNNION. CORRODED. LEFT MLG TRUNNION IS CORRODED. REPLACED TRUNNION, BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-040 TREATED AND PRIMED. (M)
- [SDR HALA9700298](https://openairdocs.org/sdr/HALA9700298), Nov 5, 1997: STRINGER. CORRODED. FOUND CORROSION ON LOWER AFT LEG, STRINGER 11, XCW 58.5 TO XRS 91, RT. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STRAPS PER SRM 57-08 METHOD 2. TREATE
- [SDR HALA9700252](https://openairdocs.org/sdr/HALA9700252), Nov 5, 1997: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER AFT LEG, STRINGER 11, XCW 58.5 TO XRS 91, RT. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STRIPS PER
- [SDR HALA9700251](https://openairdocs.org/sdr/HALA9700251), Nov 5, 1997: SPAR CAP. CORRODED. DURING C-CHECK INSPECTION, FOUND CORROSION ON FORWARD SPAR LOWER CHORD, XCW 58.5 TO XRS 61.0, LT. REPAIRED BY BLENDOUT, HFEC INSPECTED WITH NO NEGATIVE FINDINGS
- [SDR HALA9700250](https://openairdocs.org/sdr/HALA9700250), Nov 5, 1997: T-CAP. CORRODED. DURING C-CHECK INSPECTION, FOUND CORROSION ON T-CAP HORIZONTALLY LEG STATION 58.5 RIGHT FWD TO AFT SPAR. BLENDED OUT DAMAGE, HFEC INSPECTED WITH NO DEFECTS NOTE
- [SDR HALA9700249](https://openairdocs.org/sdr/HALA9700249), Nov 5, 1997: TRUNNION. CORRODED. DURING C-CHECK INSPECTION, FOUND LEFT MLG TRUNNION IS CORRODED. REPLACED TRUNNION, BUSHED HOLES IN MATING STRUCTURE PER SABRE TECH EA DC9-57-040, TREATED AND PR
- [SDR HALA9700248](https://openairdocs.org/sdr/HALA9700248), Nov 5, 1997: TRUNNION. CORRODED. DURING C-CHECK INSPECTION, FOUND RT MLG TRUNNION FITTING HAS CORROSION ON OUTBOARD WING MOUNT FLANGE. REPLACED TRUNNION FITTING AND BUSHED HOLES IN MATING STRUC
- [SDR HALA9700247](https://openairdocs.org/sdr/HALA9700247), Nov 5, 1997: BULKHEAD CLIP. CRACKED. DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD (RT SIDE) OUT BOARD LOWER CLIP CRACKED AT LONGERON 14. REMOVED DAMAGED MATERIAL, VERIFIED DAMAGE CONTAINM
- [SDR HALA9700246](https://openairdocs.org/sdr/HALA9700246), Nov 5, 1997: FRAME. CRACKED. DURING C-CHECK INSPECTION, FOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FWD OF F/O WINDSHIELD, APPROX FS 83 BY 9. STOP DRILLED CRACKED, FABRICATED AND INSTALLE
- [SDR HALA9700245](https://openairdocs.org/sdr/HALA9700245), Nov 5, 1997: FRAME. CRACKED. DURING C-CHECK INSPECTION, FOUND CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FWD OF CAPTAINS WINDSHIELD, APPROX FS 83 BY 9. FABRICATED AND INSTALLED TWO DOUBLERS FR
- [SDR HALA9700242](https://openairdocs.org/sdr/HALA9700242), Nov 5, 1997: DOUBLER. CRACKED. DURING C-CHECK INSPECTION, FOUND INTERNAL TITANIUM DOUBLER BETWEEN FS 654 AND 699 LONGERON 25L TO 25R IS CRACKED AT LONGERON 25R. GAINED ACCESS, TRIMMED OUT DAM
- [SDR HALA9700241](https://openairdocs.org/sdr/HALA9700241), Nov 5, 1997: LONGERON. CORRODED. DURING C-CHECK INSPECTION, FOUND LONGERON 30 BETWEEN FS 870-889 IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED REPAIR SECTION AND SP
- [SDR HALA9700240](https://openairdocs.org/sdr/HALA9700240), Nov 5, 1997: LONGERON. CORRODED. DURING C-CHECK INSPECTION, FOUND LOWER FUSELAGE, CORROSION ON LONGERON 28R FS 733-753. REMOVED DAMAGED SECTION, ACCOMPLISHED SPLICE REPAIR PER SRM 51-30-05 AND 
- [SDR HALA9700239](https://openairdocs.org/sdr/HALA9700239), Nov 5, 1997: FRAME. CORRODED. DURING C-CHECK INSPECTION, FOUND CORROSION AT BASE OF TAIL CONE FRAME, APPROX 28 INCHES LEFT RIGHT OF 6 O'CLOCK POSITION. REMOVED DAMAGED FRAMES, INSTALLED NEW 
- [SDR HALA9700237](https://openairdocs.org/sdr/HALA9700237), Nov 5, 1997: STRUCTURE. CORRODED. DURING C-CHECK INSPECTION, FOUND AFT FUSELAGE AREA CORRODED BETWEEN 1260 AND 1292 CANTED FRAMES BETWEEN LONGERONS 10R AND 13R. REMOVED ALL CORROSION AND RESTORE
- [SDR HALA9700235](https://openairdocs.org/sdr/HALA9700235), Nov 5, 1997: LONGERON. CORRODED. DURING C-CHECK INSPECTION, FOUND LONGERON 29R CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED LONGERON. (M)
- [SDR HALA9700234](https://openairdocs.org/sdr/HALA9700234), Nov 5, 1997: LONGERON. CORRODED. DURING C-CHECK INSPECTION, FOUND LONGERON 30 CORRODED BEYOND LIMITS BETWEEN MLG WELLS. FABRICATED AND INSTALLED LONGERON PER SRM 53-04 FIGURE 43. (M)
- [SDR HALA97126](https://openairdocs.org/sdr/HALA97126), Jun 17, 1997: NLG. BIRD STRIKE. HNL - DURING LANDING POSSIBLE BIRD STRIKE IN VICINITY OF NOSE AREA UNDERCARRIAGE. CHECKED CONDITION AND SECURITY OF NOSE GEAR AREA. ALSO, CHECKED NR 1 AND NR 2 
- [SDR HALA97112](https://openairdocs.org/sdr/HALA97112), May 28, 1997: SHUTOFF VALVE. FAILED. HNL - FLT 522 - FROM LOG PAGE 122617: ACFT HAS NOTICEABLE WOBBLE ABOVE 290 KNOTS CL/DESCENT/CRUISE WITHOUT AP YAW DAMPER OR RUDDER POWER. DUE TO NOTICEABLE AC W
- [SDR HALA9737](https://openairdocs.org/sdr/HALA9737), May 10, 1997: BEARING. WORN. HNL - FLT 524 - FROM LOG PAGE 124685: AT AIRSPEEDS GREATER THAN 300 KIAS, THE ACFT HAS A RUMBLE AND WOBBLE THAT IS MORE PRONOUNCED AT WEIGHTS LESS THAN 95,000 P

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