# N122AA: 1972 Mcdonnell Douglas DC-10-10, registration cancelled 2002-06-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 12, 2002
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-10-10](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10) (registry code 3022110)
- Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46522
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 1972
- Certificate issued: June 25, 2001
- Last registry action: June 25, 2001
- Mode S code: A05B21
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N122AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=122AA
- Page: https://openairdocs.org/deregistered/N122AA-2002-06-12

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-10-10: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10.md

## Service difficulty reports (41)

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

- [SDR HALA0000327](https://openairdocs.org/sdr/HALA0000327), Oct 3, 2000: FIRE LOOP. CHAFED. HNL - FLT 09 - DURING CRUISE, ENGINE NR 1 FIRE LOOP 'B' LIGHT FLICKERED ON AND OFF. ABNORMAL PROCEDURE COMPLETED. REF: WRITE-UP NR 55. FOUND WIRES CHAFING, REPL
- [SDR HALA0000289](https://openairdocs.org/sdr/HALA0000289), Sep 12, 2000: CONTROLLER. FAILED. HNL - FLT 481 - MISSED APPROACH/GO-AROUND, RIGHT MLG LIGHT DELAY COMING ON AFTER GEAR WAS EXTENDED APPROX 1 MINUTE. REPLACED GROUND PROXIMITY CONTROLLER. (M)
- [SDR HALA0000131](https://openairdocs.org/sdr/HALA0000131), Apr 21, 2000: VALVE. LEAKING. FLT 932 - HNL - AIR RETURN, ON CLIMB-OUT, NR 2 HYD LEAK, (2 GAL REMAINING). REMOVED AND REPLACED 2-1 NON-REVERSIBLE PUMP SHUTOFF VALVE PER MM 27-26-03. OPS/LEAK
- [SDR HALA0000108](https://openairdocs.org/sdr/HALA0000108), Apr 3, 2000: GENERATOR. MALFUNCTIONED. LAX - FLT 10 - NR 3 GEN WOULD NOT PARALLEL VOLTS AND FREQS OK. REPLACED GCU AND LOAD CONT, GEN STILL WOULD NOT PARALLEL. PLACARDED NR 3 GEN PARALLELING SYSTEM I
- [SDR HALA9900234](https://openairdocs.org/sdr/HALA9900234), Nov 20, 1999: GCU. MALFUNCTIONED. NR 2 AC BUS TIE ISOL LIGHT CAME ON IN FLIGHT PERFORMED PROCEDURES IN FCOM, LIGHT REMAINED ON. REMOVED AND REPLACED NR 2 GCU AND BCU. GROUND RUN CHECK OK. (M)
- [SDR HALA9900130](https://openairdocs.org/sdr/HALA9900130), May 22, 1999: BOLT. BROKEN. TUL - FLT 4101 - FUEL LEAK LEFT WING NR 1 ENGINE PYLON AREA. FOUND NR 1 PYLON FOOTSTOOL LOWER INBOARD, OUTBOARD BOLT BROKEN, NR 4. REPLACED BOLT PER AD96-06-08 
- [SDR HALA9900077](https://openairdocs.org/sdr/HALA9900077), Mar 12, 1999: FRAME. CORRODED. TUL - DURING CHECK FOUND FUSELAGE FRAME CORRODED AT THE FORWARD LAVATORY SERVICE PANEL 9 INCHES BY 2 INCHES AT FORWARD E/E STATION 410. DEPTH IS .063. FRAME SPL
- [SDR HALA9900073](https://openairdocs.org/sdr/HALA9900073), Mar 10, 1999: PANEL. CORRODED. DURING C-21 CHECK, FOUND AREA OF CORROSION ON OUTER WING PANEL .5 INCH BY .5 INCH WITH DEPTH OF .070 AT STATION XORS 399. FOUND BY VISUAL INSPECTION. INSPECTION
- [SDR HALA9900072](https://openairdocs.org/sdr/HALA9900072), Mar 5, 1999: STRUCTURE. CORRODED. TUL - FOUND CORROSION ON FRAME STATION 564 IN TWO PLACES FORWARD OF AC EXHAUST DUCT. CORROSION ON 1/B TEE OF CHORD STATION 561 TO 565. SKIN CORROSION STATION 57
- [SDR HALA9900086](https://openairdocs.org/sdr/HALA9900086), Mar 2, 1999: STRINGER. CORRODED. TUL - DURING C-1 CHECK, FOUND CORROSION ON STRINGER NEAR FORWARD FITTINGS. INSTALLED REPAIR DOUBLER PER 53-40-00 FIGURE 20 AND ESC 7349, DATED 3/17/99. (M)
- [SDR HALA9900085](https://openairdocs.org/sdr/HALA9900085), Mar 2, 1999: STRINGER. CORRODED. TUL - FOUND CORROSION ON STRINGER 48 LEFT. REPLACED STRINGER SECTION FROM STATION 1099 TO 1139 PER 51-01-00-05 CARD. (M)
- [SDR HALA9900084](https://openairdocs.org/sdr/HALA9900084), Mar 2, 1999: SUPPORT. CORRODED. TUL - FOUND CORROSION AT LAV SUPPORT TO BULKHEAD TEE AFT OF SEAT TRACK NR 1. REPLACED LAV SUPPORT PER AARD 51-10-00-10. (M)
- [SDR HALA9900083](https://openairdocs.org/sdr/HALA9900083), Mar 2, 1999: SPLICE. CRACKED. TUL - FOUND LEFT LONGERON 16 TO 22 SPLICE CRACKED INSIDE NR 1 FUEL TANK WING STATION XORS 372. INSTALLED AND SECURED SERVICEABLE LONG 16 TO 22 IAW AARD 51-01-00
- [SDR HALA9900046](https://openairdocs.org/sdr/HALA9900046), Feb 10, 1999: SPRING. FAILED. SEA - FLT 11 - ON TAKEOFF ROLL LANDING GEAR UNSAFE LIGHT CAME ON. ABORTED TAKEOFF. REPLACED LANDING GEAR HANDLE LOCK LEVER SPRING. (X)
- [SDR HALA9800416](https://openairdocs.org/sdr/HALA9800416), Dec 16, 1998: BULB. FAILED. FLT 1 - HNL - LEFT GEAR GREEN LIGHT DOES NOT ILLUMINATE WITH GEAR HANDLE DOWN. A/C DID A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C DID 
- [SDR HALA9800368](https://openairdocs.org/sdr/HALA9800368), Oct 27, 1998: CONTROLLER. MALFUNCTIONED. FLT 2 - HNL - ON PREFLIGHT, FOUND 'B' LOOP LIGHT ILLUMINATED FOR NR 1 FIRE DETECTION SYSTEM. REMOVED AND REPLACED CONTROLLER, SYSTEM OP CHECKS NORMAL. (M)
- [SDR HALA9800329](https://openairdocs.org/sdr/HALA9800329), Sep 20, 1998: INDICATOR. FAILED. FLT 9 - HNL - TCAS INOP IN FLIGHT AT THE SAME TIME GPWS CMPT FAIL AND WINDSHEAR INOP LIGHTS ILLUMINATED. BOTH RADAR SCREENS WENT BLANK WITH THESE WORDS APPEARIN
- [SDR HALA9800274](https://openairdocs.org/sdr/HALA9800274), Aug 7, 1998: ACM. FAILED. FLT 14 - ON TAXI ADVISED BY CABIN CREW OF SMOKE IN THE CABIN AREA ROWS 23 TO 35. FLT ENGINEER WENT BACK, DESCRIBED FOGGY OR HAZY. SOME FLT ATTENDANTS DESCRIBED 
- [SDR HALA9800272](https://openairdocs.org/sdr/HALA9800272), Aug 6, 1998: BRACKET. FAILED. LAX - FLT 9 - RIGHT NOSE GEAR DOOR DID NOT RETRACT. REMOVED AND REPLACED FORWARD RIGHT DRIVE LINK ASSY. (M)
- [SDR HAL960132](https://openairdocs.org/sdr/HAL960132), Dec 9, 1996: SKIN. CORRODED. DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND FASTENERS PULLED THROUGH SHOWING CORROSION UNDER SKIN AT LONGERON 43R AT FORWARD END OF FORWARD CARGO DOOR STATIO
- [SDR HAL960131](https://openairdocs.org/sdr/HAL960131), Dec 9, 1996: CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION ON SUPPORT CHANNEL UNDERNEATH NR 2 ROLLER TRAY AFT END IN THE LOWER GALLEY. INSTALLED NEW SUPPORT CHANNEL UNDER NR 2 ROLLER TRAY
- [SDR HAL960130](https://openairdocs.org/sdr/HAL960130), Dec 9, 1996: SPAR. CORROSION. DURING C-CHECK, FOUND CORROSION AROUND HI LOCK FASTENERS AT FRONT SPAR LOCATION LOWER SKIN AT RIGHT WING AT STATION XORS 376. REMOVED CORROSION AND INSTALLED DO
- [SDR HAL960129](https://openairdocs.org/sdr/HAL960129), Dec 9, 1996: LONGERON. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE LONGERON OUTBOARD OF THE LOWER LEG OF 51L AT STATION 1330 TO 1340. REPAIRED LONGERON PER SRM 53-10-00. TREATED AND PRIMED
- [SDR HAL960128](https://openairdocs.org/sdr/HAL960128), Dec 9, 1996: SHEAR TIE. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE FORWARD SIDE OF THE SHEAR TIE AT STATION 1207, STRINGER 51 AND 52L. REPAIRED SHEAR TIE PER SRM 53-30-00. TREATED AND PRIM
- [SDR HAL960127](https://openairdocs.org/sdr/HAL960127), Dec 5, 1996: ANGLE. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE FORWARD INBOARD SIDE OF THE FALSE SPAR ON THE LEFT WING AT STATION XORS 164 TO 171. INSTALL NEW REPAIR ANGLE WET, ALODINE
- [SDR HAL960125](https://openairdocs.org/sdr/HAL960125), Dec 4, 1996: PANEL. CORROSION. DURING C-CHECK, FOUND HEAVY INTERGRANNULAR CORROSION ON THE LOWER OUTBOARD CORNER OF THE LEFT MAIN GEAR WHEEL WELL SLANT PANEL. REPAIRED PER ENGINEERING INSTRUC
- [SDR HAL960124](https://openairdocs.org/sdr/HAL960124), Dec 4, 1996: SPLICE. CORRODED. SPLICE PLATE HAS CORROSION DAMAGE ON THE FALSE SPAR FORWARD SIDE JUST OUTBOARD OF NR 1 SPOILER ACTUATOR ON THE RIGHT WING TE AT STATION XORS 264. REPAIRED CORRO
- [SDR HAL960123](https://openairdocs.org/sdr/HAL960123), Dec 4, 1996: CLIP. CORRODED. DURING C-CHECK, FOUND THE PICK UP CLIP AT THE FALSE SPAR FORWARD OF THE INBOARD EDGE OF THE AILERON CLIP ON THE FORWARD SIDE OF THE FALSE SPAR ON TEH RIGHT WING
- [SDR HAL960122](https://openairdocs.org/sdr/HAL960122), Dec 4, 1996: BELTFRAME. CORRODED. DURING C-CHECK, FOUND CORROSION UNDER A PREVIOUSLY INSTALLED DOUBLER AT FORWARD CARGO COMPARTMENT FUSE STATION 939, STRINGER 51 LEFT AND RIGHT. REMOVED DAMAGED 
- [SDR HAL960121](https://openairdocs.org/sdr/HAL960121), Dec 4, 1996: STRINGER. CORRODED. DURING C-CHECK, FOUND CORROSIONI ON STRINGER 52 FROM STATION 814 TO 820 IN THE FORWARD CARGO COMPARTMENT. REMOVED CORRODED STRINGER AND REPLACED WITH ATTACHED S
- [SDR HAL960119](https://openairdocs.org/sdr/HAL960119), Dec 3, 1996: CHAIN DRV TRACK. CORRODED. DURING C-CHECK, FOUND THE INBOARD CHAIN DRIVE TRACK TRAY IN THE FORWARD CARGO COMPARTMENT CORRODED AT THE FORWARD END ON THE UNDERSIDE. REPLACED THE CHAIN DRIVE
- [SDR HAL960118](https://openairdocs.org/sdr/HAL960118), Dec 3, 1996: ANGLE. CORRODED. DURING C-CHECK, FOUND THE AFT CARGO WALL AND CEILING SUPPORT ANGLE HAS CORROSION AROUND SCREW HOLES. INSTALLED NEW ANGLE PER ESO 7349 AND AARD 53-01-00-05. (M)
- [SDR HAL960117](https://openairdocs.org/sdr/HAL960117), Nov 27, 1996: LONGERON. CORRODED. DURNG C-CHECK, FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND STATION 1975. INSTALLED LONGERON SPLICE REF SRM 53-10-00. ALL PARTS ALODINED, PRIMED AND
- [SDR HAL960116](https://openairdocs.org/sdr/HAL960116), Nov 26, 1996: ANGLE. CORRODED. DURING C-CHECK, FOUND THE CENTER CARGO FLOORBOARD SUPPORT WITH DEEP CORROSION ON THE AFT SIDE BETWEEN THE RIGHT TRAY AND THE RT FORWARD DRIVE CHAIN CHANNEL. INS
- [SDR HAL960115](https://openairdocs.org/sdr/HAL960115), Nov 25, 1996: ROLLER TRAY. CORRODED. DURING C-CHECK, FOUND THE LEFT TRAY IN THE CENTER CARGO FLOOR HAS CORROSION INSIDE AT SEVERAL AREAS. REMOVED DAMAGED TRAY AND INSTALLED NEW LEFT TRAY PER AARD 5
- [SDR HAL960114](https://openairdocs.org/sdr/HAL960114), Nov 25, 1996: LONGERON. CORROSION. DURING C-CHECK, FOUND CORROSION INSIDE AND ON TOP OF LONGERON 52 AND ON SPLICE PLATES AT FUSE STATION 937 AND 959. REMOVED DAMAGED LONGERON. SPLICE NEW SECTION 
- [SDR HAL960113](https://openairdocs.org/sdr/HAL960113), Nov 22, 1996: ANGLE. CORROSION. DURING C-CHECK, FOUND THE PICK UP ANGLE ON THE FORWARD SIDE OF THE FALSE SPAR AT THE OUTSIDE OF NR 1 SPOILER HINGE HAS A BRACKET WITH CORROSION DAMAGE, RT WING.
- [SDR HAL960112](https://openairdocs.org/sdr/HAL960112), Nov 20, 1996: FLOOR BEAM. CORRODED ANGLE. DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM ANGLE TOP FLANGE AT FUSE STATION 1841 BETWEEN LONGERON 46R AND LONGERON 45R. REPAIRED FRAME CAP ANGLE AT STATION 1
- [SDR HAL960111](https://openairdocs.org/sdr/HAL960111), Nov 18, 1996: DOUBLER. CORRODED. DURING C-CHECK, FOUND CORROSION ON SKIN DOUBLER BETWEEN FUSELAGE STATION 1851.85 AND 1868 AT LONGERON 52 LEFT. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLE
- [SDR HALA9676](https://openairdocs.org/sdr/HALA9676), Jun 12, 1996: FUSE HOLDER. ARCING. FLT NR 22 - SEA - NR 5 LAVATORY LIGHT FUSE ARCING IN FUSE HOLDER. POOR SOLDER CONNECTION. INSULATING TAPE FOUND SMOLDERING. FUSE REMOVED AND LAVATORY SECURED. R
- [SDR HALA9675](https://openairdocs.org/sdr/HALA9675), Jun 12, 1996: BALLAST. OVERHEATED. FLT NR 22 - SEA - FLUORESCENT LIGHT BALLAST FIRE AT SEAT 2A BEGAN TO SMOKE HEAVILY AT CRUISE. POWER REMOVED AND ASSOCIATED CIRCUIT BREAKERS PULLED, SMOKE DISSIP

## FAA accident and incident reports (5)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19960414011019I](https://openairdocs.org/incident/19960414011019I), Apr 14, 1996: Doug DC1010 (N122AA), Portland, OR. Narrative: hawaiian airlines, inc., flight 25, aborted takeoff when just prior to rotation, heard two loud booms and suspected compressor stall. Returned to…
- [Incident 19940809032789I](https://openairdocs.org/incident/19940809032789I), Aug 9, 1994: Doug DC1010 (N122AA), Hilo, HI, Minor damage. Loud pop heard 340 miles out. Landed normal. Outer window separated at FS1169 right side. Panel stabilizer.
- [Incident 19860804047349I](https://openairdocs.org/incident/19860804047349I), Aug 4, 1986: Doug DC1010 (N122AA), Dallas Fort Wor, TX, Minor damage. Nose of aircraft came up during landing, resulting in tail strike on runway. Very minor damage occurred.
- [Incident 19860703056069I](https://openairdocs.org/incident/19860703056069I), Jul 3, 1986: Doug DC1010 (N122AA), Chicago, IL, Minor damage. Pneumatic fail light came on, fire light lit, engine shutdown. Safe landing. Clamp on bleed air duct fell off.
- [Incident 19850405014649I](https://openairdocs.org/incident/19850405014649I), Apr 5, 1985: Doug DC1010 (N122AA), Detroit, MI, Minor damage. Struck by lightning, loss of first officer flight instruments. Crease in radome.

## Other aircraft with N122AA

- [Registered now](https://openairdocs.org/aircraft/N122AA): Robinson Helicopter R44 II, S/N 11228, built 2006

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