# Service difficulty reports: N148AA, cancelled Jun 12, 2002

A list on [N148AA, cancelled Jun 12, 2002](https://openairdocs.org/deregistered/N148AA-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 HALA0000281](https://openairdocs.org/sdr/HALA0000281.md): Module · inoperative · Sep 4, 2000 · N148AA · Doug DC1010 · Emergency Lighting
  > HNL - FLT 27 - EMERGENCY LIGHTING ON LEFT SIDE, LIGHT UP DURING CRUISE. RESET CIRCUIT BREAKER AND RECYCLED EMERGENCY LIGHT SWITCH. NO CHANGE. REPLACED MODULE AM1-13, OPS CHECK OK. (M)
- [SDR HALA9900103](https://openairdocs.org/sdr/HALA9900103.md): Tire · failed · Apr 22, 1999 · N148AA · Doug DC1010 · Tire
  > SEA - AIRCRAFT ARRIVED SEATTLE LEFT NOSE GEAR TIRE BLOWN. FOUND WHEEL BEARING SEIZED TO AXLE SLEEVE. REMOVED BEARING RACE INSPECTED SLEEVE. DAMAGE WITHIN LIMITS PER 32-42-01. AIRCRAFT CYCLE LIMITED TO 10 CYCLES. (M)
- [SDR HALA9900045](https://openairdocs.org/sdr/HALA9900045.md): Control Cable · out of position · Feb 9, 1999 · N148AA · Doug DC1010 · Power Lever
  > HNL - FLT 25 - (LOG PAGE NR 2344159). NR 3 THROTTLE LEVER FROZEN. REPOSITIONED NR 3 THROTTLE PUSH/PULL CABLE. ROD END BINDING AT THROTTLE IDLER CRANK. INSPECTED FOR CONDITION AND SECURITY. OPS CHECK OK. (X)
- [SDR HALA9800125](https://openairdocs.org/sdr/HALA9800125.md): Rccb · failed · May 15, 1998 · N148AA · Doug DC1010 · DC Generating System
  > HNL - FLT 465 - (LOG PAGE NR 4205729). MULTIPLE INDICATIONS OF POSSIBLE RCCB FAILURE. MANIFOLD FAIL LIGHTS 1 AND 2 DO NOT TEST. CABIN STANDBY PRESSURE DOES NOT TEST. NO AMPERAGE DRAWN ON AUXILIARY PITOT HEAT. NO PRESSURE INDICATION ON NR 2 PNEN DUCT PRESSU
- [SDR HALA9800091](https://openairdocs.org/sdr/HALA9800091.md): Controller · failed · Apr 8, 1998 · N148AA · Doug DC1010 · Pneumatic Distribution System
  > FLT 25 - LOS - NR 1 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB. PERFORMED ABNORMAL PROCEDURE. SUPPLY SELECTOR AND PACK OFF. LIGHT DIDN'T GO OUT WITH SYSTEM UNPRESSURIZED AND PNEU TEMPERATURE BELOW 120 DEGREES. LEFT SYSTEM UNPRESSURIZED AND DEACTIVATED FA
- [SDR HALA9700170](https://openairdocs.org/sdr/HALA9700170.md): Batteries · discharged · Sep 2, 1997 · N148AA · Doug DC1010 · Emergency Lighting
  > HNL - DURING WALK AROUND FOUND EMERGENCY LIGHTS DIM IN THE CABIN. REPLACED THE EMERGENCY BATTERIES IN EACH CABIN. THE OPERATIONAL CHECK WAS OK. (M)
- [SDR HALA97110](https://openairdocs.org/sdr/HALA97110.md): Generator · failed · May 12, 1997 · N148AA · Doug DC1010 · AC Generator-Alternator
  > FLT 465 - HNL - AIR RETURN, AFTER T/O WHILE CLIMBING THROUGH 16,000 FT THE NR 3 GEN DROPPED OFF LINE, RESET GEN CONTROL SWITCH. VOLTS RETURNED TO 118 AND FREQ 401. PULLED GALLEY OVEN C/B'S NR 5 AND NR 6. PUT GEN NR 3 ON LINE AND PARALLED GEN'S. LATER IN FL
- [SDR HALA96152](https://openairdocs.org/sdr/HALA96152.md): Wire · disconnected · Nov 2, 1996 · N148AA · Doug DC1010 · Light System Wiring
  > FLT 1038 - HNL - L-3 DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY AND RECONNECTED WIRES TO L-3 DOOR. THE OPERATIONAL CHECK WAS OK. (M)
- [SDR HAL960079](https://openairdocs.org/sdr/HAL960079.md): Skin · corroded · Oct 8, 1996 · N148AA · Doug DC1010 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN BULGED AND CRACKED FROM CORROSION AT STATION 1661 BETWEEN LONGERON 43L AND 44L. REMOVED CORROSION SRM 51-21-01. INSTALLED DOUBLERS PER SRM 53-20-00 VOL 1. (M)
- [SDR HAL960087](https://openairdocs.org/sdr/HAL960087.md): False Spar Cap · corroded · Oct 7, 1996 · N148AA · Doug DC1010 · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION ON LEFT WING FUSELAGE SPAR UPPER CAP AT STATION XW=320 TO XW=224. REMOVED AND REPLACED EIGHT FOOT SECTION OF FALSE SPAR PER AARD 51-01-00-05, 51-35-01 VOL 2 AND ESO 7349 DATED 10-4-96. (M)
- [SDR HALA960084](https://openairdocs.org/sdr/HALA960084.md): False Spar · corroded · Oct 5, 1996 · N148AA · Doug DC1010 · Wing Miscellaneous Structure
  > CORROSION ON AFT SIDE OF FALSE SPAR JUST OUTBOARD OF NR 1 SPOILER ACT. REMOVED AND REPLACED 8 FOOT SECTION OF FALSE SPAR PER AARD 51-01-00-05 AND ESO 7349 DATED 10-4-96. (M)
- [SDR HAL960083](https://openairdocs.org/sdr/HAL960083.md): Longeron · corroded · Oct 4, 1996 · N148AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 52 BETWEEN STATION 1059 AND 1079. SPLICED NEW SECTION AT LONGERON FROM STATION 1072-1079 AS PER AARD 51-10-00-05. (M)
- [SDR HAL960082](https://openairdocs.org/sdr/HAL960082.md): Longeron · corroded · Oct 4, 1996 · N148AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 52 BETWEEN STATION 1039-1059 HAS SURFACE CORROSION. SPLICED NEW SECTION AT LONGERON FROM STATION 1053-1059 AS PER AARD 51-01-00-05 AND SRM 51-21-01. (M)
- [SDR HAL960081](https://openairdocs.org/sdr/HAL960081.md): Skin · corroded · Oct 4, 1996 · N148AA · Doug DC1010 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN, BELLY BETWEEN LANDING GEAR. FABRICATED AND INSTALLED DOUBLER FROM LONGERON 50R TO 50L AND FROM STATION 1461 TO 1531 IAW ESO 7349 DATED 9-23-96. (M)
- [SDR HAL960080](https://openairdocs.org/sdr/HAL960080.md): Door Jamb · cracked · Oct 4, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > CRACK IN AFT DOOR JAMB WEB AT NR 8 ACCESS HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM VOL 1 53-50-00 PAGE 69. (M)
- [SDR HAL960076](https://openairdocs.org/sdr/HAL960076.md): Frame Strap · corroded · Oct 2, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > CORROSION ON THE UPPER EAR OF THE FUSELAGE FRAME STRAP ABOVE R2 DOOR. REMOVED CORROSION AND INSTALLED A STRAP OVER THE AREA PER ESO 7349 DATED 10-1-96. (M)
- [SDR HAL960078](https://openairdocs.org/sdr/HAL960078.md): Frame · corroded · Oct 1, 1996 · N148AA · Doug DC1010 · Fuselage Main, Frame
  > WEB AT FRAME 979 HAS CORROSION BETWEEN LAYERS OF FRAME 6 INCHES ABOVE THE BELLY AND CRACKED 2 PLACES AT STRINGER 50L. INSTALLED REPLACEMENT WEB AT STATION 979 LEFT SIDE PER ESO 7349 DATED 9-27-96 AND SRM VOL NR 51-21-01 AND SRM VOL NR 51-31-01. (M)
- [SDR HAL960075](https://openairdocs.org/sdr/HAL960075.md): Longeron · corroded · Oct 1, 1996 · N148AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > HEAVY CORROSION ON STRINGER R43 STATION 1099 TO STATION 1119. CUT OUT DAMAGE, INSTALLED STRINGER REPAIR PER AARD 51-10-00-1 SRM 53-10-00. (M)
- [SDR HAL960074](https://openairdocs.org/sdr/HAL960074.md): Intercostal · corroded · Oct 1, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON INTERCOSTAL AT L 43R STATION 1099 TO STATION 1119. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-1. (M)
- [SDR HAL960073](https://openairdocs.org/sdr/HAL960073.md): Support · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LOCATED IN FRONT OF LAV NR 6 IS CORRODED. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-01-00-05, PAGE 1 AND 2. (M)
- [SDR HAL960072](https://openairdocs.org/sdr/HAL960072.md): Support · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT FORWARD OF COFFEE BAR CORRODED. REMOVED AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-01-00-05, PAGE 1 AND 2. (M)
- [SDR HAL960071](https://openairdocs.org/sdr/HAL960071.md): Support · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > INBOARD FLOOR SUPPORT FOR COFFEE BAR CORRODED. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-10-00-05, PAGE 1 AND 2. (M)
- [SDR HAL960069](https://openairdocs.org/sdr/HAL960069.md): Roller Tray · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > NR 4 ROLLER TRAY HAS HEAVY CORROSION BOTTOM SIDE AT STATION 859 TO 879. REPLACED ROLLER TRAY FROM STATION 879 TO 795 PER SRM 51-01-00-05. (M)
- [SDR HAL960068](https://openairdocs.org/sdr/HAL960068.md): Roller Tray · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION ON OUTBOARD LIP OF NR 4 RIGHT ROLLER TRAY BETWEEN FRAME STATION 815 AND 825. REPLACED ROLLER TRAY FROM STATION 879 TO 795 PER SRM 51-01-00-05. (M)
- [SDR HAL960066](https://openairdocs.org/sdr/HAL960066.md): Support · corroded · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR BOARD SUPPORT FORWARD CARGO COMPARTMENT INBOARD NR 1 ROLLER TRAY. REPLACED FLOOR BOARD SUPPORT PER SRM 51-10-00. (M)
- [SDR HAL960065](https://openairdocs.org/sdr/HAL960065.md): Shear Tie · broken · Sep 30, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > SHEAR TIE CORRODED, BROKEN OFF BETWEEN STRINGER 52 AND 51R. INSTALLED SHEAR TIE CLIP REPAIR PER SRM 53-30-00, FIG 10. (M)
- [SDR HAL960064](https://openairdocs.org/sdr/HAL960064.md): Longeron · cracked · Sep 26, 1996 · N148AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > CRACK IN LONGERON NR 33 RIGHT AT STATION 550. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-00 PAGE 1-5. (M)
- [SDR HAL960063](https://openairdocs.org/sdr/HAL960063.md): Stringer · corroded · Sep 24, 1996 · N148AA · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > HEAVY CORROSION ON STRINGER 52 FROM STATION 999 TO STATION 1019. SPLICED IN NEW SECTION OF STRINGER FROM STATION 989 TO 1101 PER SRM 51-10-00. (M)
- [SDR HAL960061](https://openairdocs.org/sdr/HAL960061.md): Shear Tie · corroded · Sep 19, 1996 · N148AA · Doug DC1010 · Fuselage Miscellaneous Structure
  > SHEAR TIE HEAVY CORROSION AT STATION 899 BETWEEN STRINGER 52L AND 51L. INSTALLED NEW SHEAR TIE SECTION BETWEEN STRINGER 52L AND 51L PER SRM VOL 1 53-30-00 AND 53-30-00-10. (M)
- [SDR HALA96127](https://openairdocs.org/sdr/HALA96127.md): Gear Indication · malfunctioned · Aug 26, 1996 · N148AA · Doug DC1010 · Landing Gear Position and Warning
  > FLT NR 11 - HNL - WITH GEAR HANDLE DOWN ON APPROACH, ALL THREE GEAR LIGHTS WERE RED. RECYCLED GEAR, SAME THING HAPPENED. THIRD TIME, GEAR LIGHTS WERE ALL GREEN. HYDRAULIC PRESSURE WAS 3000 PSI EACH TIME. INSPECTED ALL THREE LANDING GEAR PROX SENSORS FOR CO
- [SDR HAL9655](https://openairdocs.org/sdr/HAL9655.md): Prox Box · malfunctioned · May 5, 1996 · N148AA · Doug DC1010 · Landing Gear Position and Warning
  > HNL - FLT 921 - LANDING GEAR INDICATED THREE RED ON FINAL. CYCLED GEAR TWICE AND GOT THREE GREEN AFTER GO-AROUND. REPLACED PROXIMITY SWITCH CONTROL BOX. BITE CHECK GOOD. (X)
- [SDR HALA9634](https://openairdocs.org/sdr/HALA9634.md): Tire · blown · Apr 1, 1996 · N148AA · Doug DC1010 · Tire
  > HNL - FLT NR 921 - RIGHT SIDE MAIN GEAR TIRE BLOWN ON TAKEOFF AS REPORTED BY ANOTHER AIRCRAFT. FOUND NR 8 TIRE BLOWN, RIGHT FLAP L/E DENTED AND SPOILER CONTROL ACCESS PANEL DAMAGED. REPLACED NR 7 AND NR 8 TIRES. INSTALLED TEMPORARY REPAIR ON SPOILER ACCESS
- [SDR HAL95149](https://openairdocs.org/sdr/HAL95149.md): Battery Pack · discharged · Nov 10, 1995 · N148AA · Doug DC1010 · Emergency Lighting
  > HNL - INFORMATION FROM LOG PAGE 3590898 - ON PRE-FLIGHT, FOUND FORWARD POWER SUPPLY OF EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY SUPPLY PACK, OPERATIONAL CHECK 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 = 'N148AA' AND deregistration_id = 'N148AA-2002-06-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N148AA-2002-06-12/reports

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