# Service difficulty reports: N122AA, cancelled Jun 12, 2002

A list on [N122AA, cancelled Jun 12, 2002](https://openairdocs.org/deregistered/N122AA-2002-06-12.md).

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

- [SDR HALA0000327](https://openairdocs.org/sdr/HALA0000327.md): Fire Loop · chafed · Oct 3, 2000 · N122AA · Doug DC1010 · Smoke Detection
  > 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, REPLACED CORE LOOP WIRING, HARNESS. OPS CHECKED OK. (X)
- [SDR HALA0000289](https://openairdocs.org/sdr/HALA0000289.md): Controller · failed · Sep 12, 2000 · N122AA · Doug DC1010 · Ground Proximity System
  > 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.md): Valve · leaking · Apr 21, 2000 · N122AA · Doug DC1010 · Hydraulic System, Main
  > 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 CHECK OK. SERVICED HYD QTY. (M)
- [SDR HALA0000108](https://openairdocs.org/sdr/HALA0000108.md): Generator · malfunctioned · Apr 3, 2000 · N122AA · Doug DC1010 · AC Generation System
  > 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 INOPERATIVE. (M)
- [SDR HALA9900234](https://openairdocs.org/sdr/HALA9900234.md): Gcu · malfunctioned · Nov 20, 1999 · N122AA · Doug DC1010 · AC Generation System
  > 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.md): Bolt · broken · May 22, 1999 · N122AA · Doug DC1010 · Nacelle/Pylon Structure
  > 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 WITH (H11 TYPE) INCONEL PER AD. (M)
- [SDR HALA9900077](https://openairdocs.org/sdr/HALA9900077.md): Frame · corroded · Mar 12, 1999 · N122AA · Doug DC1010 · Fuselage Main, Frame
  > 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 SPLICED WITH FILLER PLATE INSTALLED PER ESO 7349, DATED 3/12/99. (M)
- [SDR HALA9900073](https://openairdocs.org/sdr/HALA9900073.md): Panel · corroded · Mar 10, 1999 · N122AA · Doug DC1010 · Wing, Plate/Skin
  > 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 WAS INTERNAL. BLENDED CORROSION AND REWORKED AREA IAW E50 7349, DATED 03/09/99. (M)
- [SDR HALA9900072](https://openairdocs.org/sdr/HALA9900072.md): Structure · corroded · Mar 5, 1999 · N122AA · Doug DC1010 · Fuselage Main, Structure
  > 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 575 AT EXHAUST DUCT (AC BAY) CORROSION ON FITTING INBOARD OF EXHAUST DUCT. INSTALLED REPAIR PER ESO
- [SDR HALA9900086](https://openairdocs.org/sdr/HALA9900086.md): Stringer · corroded · Mar 2, 1999 · N122AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · corroded · Mar 2, 1999 · N122AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > 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.md): Support · corroded · Mar 2, 1999 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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.md): Splice · cracked · Mar 2, 1999 · N122AA · Doug DC1010 · Wing Miscellaneous Structure
  > 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 51-01-00-05. (M)
- [SDR HALA9900046](https://openairdocs.org/sdr/HALA9900046.md): Spring · failed · Feb 10, 1999 · N122AA · Doug DC1010 · Landing Gear Selector
  > 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.md): Bulb · failed · Dec 16, 1998 · N122AA · Doug DC1010 · Landing Gear Position and Warning
  > 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 A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C MADE AN UNEVENTFUL LANDING A
- [SDR HALA9800368](https://openairdocs.org/sdr/HALA9800368.md): Controller · malfunctioned · Oct 27, 1998 · N122AA · Doug DC1010 · Fire Detection
  > 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.md): Indicator · failed · Sep 20, 1998 · N122AA · Doug DC1010 · Altimeter, Barometric/Encoder
  > 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 APPEARING, RADIO ALT NR 1 AND NR 2 ON DESCENT WHEN NR 1 RADIO ALT WAS TURNED ON AND TESTED TCAS APPEARED TO
- [SDR HALA9800274](https://openairdocs.org/sdr/HALA9800274.md): Acm · failed · Aug 7, 1998 · N122AA · Doug DC1010 · Cabin Cooling System
  > 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 SMELL OF ELECTRICAL, OTHERS AS LIKE A BURNED MATCH SMELL. RETURNED TO GATE. TURBINE INLET TEMP OB
- [SDR HALA9800272](https://openairdocs.org/sdr/HALA9800272.md): Bracket · failed · Aug 6, 1998 · N122AA · Doug DC1010 · Landing Gear Retraction/Extension System
  > 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.md): Skin · corroded · Dec 9, 1996 · N122AA · Doug DC1010 · Fuselage Main, Plate/Skin
  > 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 STATION 462 TO 474. REMOVED CORROSION AND INSTALLED CLASS 1 DOUBLER PER ESO 7349, DATED 12/5/96. (M)
- [SDR HAL960131](https://openairdocs.org/sdr/HAL960131.md): Channel · corroded · Dec 9, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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 PER SRM 51-20-00. (M)
- [SDR HAL960130](https://openairdocs.org/sdr/HAL960130.md): Spar · corrosion · Dec 9, 1996 · N122AA · Doug DC1010 · Wing Spar
  > 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 DOUBLER REPAIR PER ESO 7349, DATED 12/5/96. (M)
- [SDR HAL960129](https://openairdocs.org/sdr/HAL960129.md): Longeron · corroded · Dec 9, 1996 · N122AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > 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 PER SRM 51-21-01. (M)
- [SDR HAL960128](https://openairdocs.org/sdr/HAL960128.md): Shear Tie · corroded · Dec 9, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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 PRIMED AREA PER SRM 51-21-01. (M)
- [SDR HAL960127](https://openairdocs.org/sdr/HAL960127.md): Angle · corroded · Dec 5, 1996 · N122AA · Doug DC1010 · Wing Miscellaneous Structure
  > 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, ALODINED AND PRIMED PARTS AND INSTALLED HI LOCKS PER ESO 7349, DATED 12/5/96. (M)
- [SDR HAL960125](https://openairdocs.org/sdr/HAL960125.md): Panel · corrosion · Dec 4, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND HEAVY INTERGRANNULAR CORROSION ON THE LOWER OUTBOARD CORNER OF THE LEFT MAIN GEAR WHEEL WELL SLANT PANEL. REPAIRED PER ENGINEERING INSTRUCTIONS ON ESO 7349, DATED 12/4/96. (M)
- [SDR HAL960124](https://openairdocs.org/sdr/HAL960124.md): Splice · corroded · Dec 4, 1996 · N122AA · Doug DC1010 · Wing Miscellaneous Structure
  > 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 CORROSION DAMAGE RED SRM VOL 1, CHAPTER 51 STR GENERAL AND ESO 7349, REF DATED 12/3/96. (M)
- [SDR HAL960123](https://openairdocs.org/sdr/HAL960123.md): Clip · corroded · Dec 4, 1996 · N122AA · Doug DC1010 · Wing Miscellaneous Structure
  > 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 TRAILING EDGE HAS CORROSION DAMAGE. REPAIRED THE CORRODED AREA PER SRM VOL 1, CHAPTER 57-00-01, FI
- [SDR HAL960122](https://openairdocs.org/sdr/HAL960122.md): Beltframe · corroded · Dec 4, 1996 · N122AA · Doug DC1010 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND CORROSION UNDER A PREVIOUSLY INSTALLED DOUBLER AT FORWARD CARGO COMPARTMENT FUSE STATION 939, STRINGER 51 LEFT AND RIGHT. REMOVED DAMAGED SECTION OF BELT FRAME AND SPLICED IN NEW SECTION PER SRM 53-30-00, PAGE 15. (M)
- [SDR HAL960121](https://openairdocs.org/sdr/HAL960121.md): Stringer · corroded · Dec 4, 1996 · N122AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > 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 SPLICES PER AARD 51-01-00. (M)
- [SDR HAL960119](https://openairdocs.org/sdr/HAL960119.md): Chain Drv Track · corroded · Dec 3, 1996 · N122AA · Doug DC1010 · Cargo Compartments
  > 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 TRACK PER AARD 53-10-00-1. (M)
- [SDR HAL960118](https://openairdocs.org/sdr/HAL960118.md): Angle · corroded · Dec 3, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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.md): Longeron · corroded · Nov 27, 1996 · N122AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > 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 SEALED PER SRM 51-21-01. (M)
- [SDR HAL960116](https://openairdocs.org/sdr/HAL960116.md): Angle · corroded · Nov 26, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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. INSTALLED NEW FLOORBOARD SUPPORT ANGLE PER AARD 51-01-00-05. ALODINED AND PRIMED PER SRM 51-21-00-VOL
- [SDR HAL960115](https://openairdocs.org/sdr/HAL960115.md): Roller Tray · corroded · Nov 25, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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 51-01-00-05. (M)
- [SDR HAL960114](https://openairdocs.org/sdr/HAL960114.md): Longeron · corrosion · Nov 25, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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 IN PER MM REF SRM 53-10-00. (M)
- [SDR HAL960113](https://openairdocs.org/sdr/HAL960113.md): Angle · corrosion · Nov 22, 1996 · N122AA · Doug DC1010 · Wing Miscellaneous Structure
  > 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. INSTALLED NEW PICK UP ANGLE PER SRM 51-10-00-01. (M)
- [SDR HAL960112](https://openairdocs.org/sdr/HAL960112.md): Floor Beam · corroded angle · Nov 20, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > 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 1841 BETWEEN LONGERON 46R AND 45R REF SRM 53-30-00 FIG 8. ALODINED AND PRIMED RED SRM 51-21-01. (M
- [SDR HAL960111](https://openairdocs.org/sdr/HAL960111.md): Doubler · corroded · Nov 18, 1996 · N122AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON SKIN DOUBLER BETWEEN FUSELAGE STATION 1851.85 AND 1868 AT LONGERON 52 LEFT. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-10-00-01. (M)
- [SDR HALA9676](https://openairdocs.org/sdr/HALA9676.md): Fuse Holder · arcing · Jun 12, 1996 · N122AA · Doug DC1010 · Passenger Compartment Lighting
  > 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. RESOLDERED NR 5 LAV 1B LIGHT FUSE HOLDER. OPS CHECKED NORMAL. (M)
- [SDR HALA9675](https://openairdocs.org/sdr/HALA9675.md): Ballast · overheated · Jun 12, 1996 · N122AA · Doug DC1010 · Passenger Compartment Lighting
  > 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 DISSIPATED. REPLACED BOTH BALLAST ABOVE 2A. OPS CHECKED NORMAL. NO INDICATION OF FIRE. (M)

## 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 = 'N122AA' AND deregistration_id = 'N122AA-2002-06-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N122AA-2002-06-12/reports

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