# Service difficulty reports: N144AA, cancelled May 16, 2002 A list on [N144AA, cancelled May 16, 2002](https://openairdocs.org/deregistered/N144AA-2002-05-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AALA991255](https://openairdocs.org/sdr/AALA991255.md): Probe · defective · Aug 23, 1999 · N144AA · Doug DC1030 · Fuel Quantity Sensor > LAX - FLT 123 - EN ROUTE DFW-HNL - NUMBER 2 FUEL TANK QTY GAUGE INDICATED 5000 LBS LESS THAN TANKS 1 AND 3. FUEL WAS TRANSFERRED AND TANKS BALANCED. CONTINUED FLIGHT UNTIL FUEL GAUGES INDICATED APPROXIMATELY 5000 LBS FUEL LESS THAN PLANNED USAGE. DIVERTED T - [SDR AALA990953](https://openairdocs.org/sdr/AALA990953.md): Filter · defective · Jun 25, 1999 · N144AA · Doug DC1030 · Turbine Engine Oil System > HNL - FLT 72 - DURING CLIMB-OUT, NR 2 ENGINE STRAINER CLOG LIGHT ILLUMINATED INTERMITTENTLY AND THEY STAYED ON. FLIGHT CREW ACCOMPLISHED SHUT DOWN PROCEDURES CHECKLIST AND RETURNED AND LANDED HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE OI - [SDR AALA990642](https://openairdocs.org/sdr/AALA990642.md): Packing · leaking · Apr 29, 1999 · N144AA · Doug DC1030 · Fuel Storage > HNL - FLT 72 - AFTER TAKEOFF HNL, A FLUID LEAK WAS REPROTED COMING FROM THE LEFT WING. FLIGHT AIR INTERRUPTED AND RETURNED HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND FUEL LEAKING FROM UPPER WING 5TH PANEL FROM WING TIP. REPLACE - [SDR AALA990160](https://openairdocs.org/sdr/AALA990160.md): Apu · defective · Feb 5, 1999 · N144AA · Doug DC1030 · APU Core Engine > DFW - FLT 102 - DURING TAKEOFF AND CLIMB, FUME SMELL IN CABIN WAS NOTICED BY CREW AND PASSENGERS AND DISSIPATED. ODOR RETURNED DURING DESCENT AND LASTED THROUGH ENGINE SHUTDOWN. MAINTENANCE FOUND APU TO BE CAUSE OF ODOR. REMOVED AND REPLACED APU, CHANGE COA - [SDR AALA990100](https://openairdocs.org/sdr/AALA990100.md): Skin · corroded · Jan 14, 1999 · N144AA · Doug DC1030 · Fuselage Main, Plate/Skin > TUL - FOUND CORROSION 12 INCHES FORWARD OF AFT BULKHEAD INSIDE RIGHT W/W ON SKIN PLATE BELOW STRINGER 32R. REPAIRED WITH DOUBLERS PER ESO 7349, DATED 1-7-99. (M) - [SDR AALA990075](https://openairdocs.org/sdr/AALA990075.md): Longeron · corroded · Jan 14, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON LONGERON 31R UNDER HAT SECTION. REPAIRED PER SRM VOL 1 53-10-00. (M) - [SDR AALA990067](https://openairdocs.org/sdr/AALA990067.md): Stringer · corroded · Jan 14, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION AT STRINGER 30 AT FUSELAGE RT ABOVE WING SURFACE STATION 1401 TO STATION 1441. REMOVED CORROSION IN STRINGER 30 AND INSTALLED SPLICE REPAIR PER SRM 53-10-60 VOL 1. (M) - [SDR AALA990066](https://openairdocs.org/sdr/AALA990066.md): Longeron · corroded · Jan 14, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON LONGERON 32R UNDER HAT SECTION. REPAIRED PER ESO 7349 DATED 01-14-99. (M) - [SDR AALA990047](https://openairdocs.org/sdr/AALA990047.md): Stringer · corroded · Jan 8, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 51L. REPLACED STRINGER END PER AARD 51-01-00-05. (M) - [SDR AALA990045](https://openairdocs.org/sdr/AALA990045.md): Stringer · corroded · Jan 8, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON L52 STATION 1964-1975. REPLACED STRINGER END PER AARD 51-01-00-05. (M) - [SDR AALA990044](https://openairdocs.org/sdr/AALA990044.md): Cap · corroded · Jan 8, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - FOUND STRINGER 50R END CAP CORRODED AT AFT HOLE IN SPLICE. REPLACED STRINGER END CAP PER AARD 51-01-00-05. (M) - [SDR AALA990022](https://openairdocs.org/sdr/AALA990022.md): Angle · corroded · Jan 8, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON LEFT ATTACH ANGLE OUTBOARD NR 1 ROLLER TRAY STATION 1014-1099. REMOVED AND REPLACED SIDE WALL TO ROLLER TRAY Z-ANGLE STATION 959 TO 1099 PER SRM 53-60-01. (M) - [SDR AALA990083](https://openairdocs.org/sdr/AALA990083.md): Longeron · corroded · Jan 6, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON LONGERON 52 FORWARD OF STATION 1156 FORWARD TO STATION 1148. REMOVED PART, TREATED, PRIMED AND PAINTED AND INSTALLED NEW PART AND FASTENERS PER AARD 51-10-00-1 PAGE 1. (M) - [SDR AALA990082](https://openairdocs.org/sdr/AALA990082.md): Stringer · corroded · Jan 6, 1999 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION AT STRINGER 51R. INSTALLED NEW STRINGER FROM STATION 1059-1079 AND SPLICES PER SRM 53-10 VOL 1 P-T PLUS P PER SRM 51-21-01. (M) - [SDR AALA990007](https://openairdocs.org/sdr/AALA990007.md): Support · corroded · Jan 5, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - FOUND GALLEY SUPPORT CORRODED. REMOVED AND REPLACED GALLEY SUPPORT AARD 51-10-00-1. (M) - [SDR AALA990006](https://openairdocs.org/sdr/AALA990006.md): Support · corroded · Jan 5, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - GALLEY SUPPORT CORRODED. REMOVED AND REPLACED GALLEY SUPPORT AARD 51-10-00-1. (M) - [SDR AALA990005](https://openairdocs.org/sdr/AALA990005.md): Support · corroded · Jan 5, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - FLOOR SUPPORT CORRODED NR 2 GALLEY SUPPORT. FABRICATED FLOOR SUPPORT PER AARD 51-10-00-1. (M) - [SDR AALA990009](https://openairdocs.org/sdr/AALA990009.md): Plug · corroded · Jan 4, 1999 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - LAV TIE DOWN TRACK PLUG CORRODED IN NR 1 SEAT TRACK. INSTALLED NEW LAV TRACK PLUG PER SRM 57-21-01. (M) - [SDR AALA990013](https://openairdocs.org/sdr/AALA990013.md): Trunnion · corroded · Dec 30, 1998 · N144AA · Doug DC1030 · Main Landing Gear Attach Section > TUL - FOUND CORROSION IN AFT LUG OF FORWARD TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.072 DIAMETER. INSTALLED OVERSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) - [SDR AALA990012](https://openairdocs.org/sdr/AALA990012.md): Trunnion · corroded · Dec 30, 1998 · N144AA · Doug DC1030 · Main Landing Gear Attach Section > TUL - FOUND CORROSION IN FORWARD LUG OF FORWARD OF FORWARD TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.0675 DIA. INSTALLED OVERSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) - [SDR AALA990010](https://openairdocs.org/sdr/AALA990010.md): Trunnion · corroded · Dec 30, 1998 · N144AA · Doug DC1030 · Main Landing Gear Attach Section > TUL - CORROSION IN AFT LUG OF AFT RT MLG TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.054 INCH. INSTALLED OVERSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) - [SDR AALA990008](https://openairdocs.org/sdr/AALA990008.md): Channel · corroded · Dec 28, 1998 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON CHANNEL AROUND LAV TIE DOWN HOLES. REPLACED LAV SUPPORT CHANNEL PER AARD 51-10-00-01. (M) - [SDR AALA981211](https://openairdocs.org/sdr/AALA981211.md): Valve · failed · Jun 19, 1998 · N144AA · Doug DC1030 · Landing Gear Retraction/Extension System > HNL - FLT 102 - AFTER TAKEOFF HNL, RT MAIN GEAR DOOR WOULD NOT CLOSE. RECYCLED GEAR DOOR, REMAINED OPEN. RETURNED HNL AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980011](https://openairdocs.org/sdr/AALA980011.md): Trunnion · corroded · Jan 26, 1998 · N144AA · Doug DC1030 · Main Landing Gear Attach Section > TUL - FOUND CORROSION IN FORWARD LUG OF AFT TURNNION. REMOVED CORROSION BY BORING LUG TO 4.125 DIAMETER. INSTALLED OVERSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) - [SDR AALA990046](https://openairdocs.org/sdr/AALA990046.md): Longeron · corroded · Jan 8, 1998 · N144AA · Doug DC1030 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND 1975. REMOVED CORROSION ON LONGER 51R PER SRM 51-21-01. REPLACED STRINGER 651R END CAP PER AARD 51-01-00-05. TREATED PAINTED AND PRIMED PER SRM 51-21-01 VOL 2. (M) - [SDR AALA972108](https://openairdocs.org/sdr/AALA972108.md): Wire · loose · Nov 6, 1997 · N144AA · Doug DC1030 · Light System Wiring > ORD - FLT 72 - EN ROUTE HNL/ORD DURING CRUISE, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE IN FIRST CLASS CABIN ILLUMINATED. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPAIRED WIRING AT TERMINAL BURNDY BLOCK A53-22 TO 7X7A AT AMI-8 CONTROL MODULE. S - [SDR AALA972110](https://openairdocs.org/sdr/AALA972110.md): Multiplexer · defective · Oct 31, 1997 · N144AA · Doug DC1030 · Emergency Lighting > DFW - FLT 102 - EN ROUTE HNL/DFW, DURING CRUISE, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE IN FIRST CLASS CABIN ILLUMINATED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FIRST CLASS SEAT MULTIPLEXER SET. SYSTEM GROUND CHECKED NORMAL OPERATION - [SDR AALA972109](https://openairdocs.org/sdr/AALA972109.md): Lights · malfunctioned · Oct 31, 1997 · N144AA · Doug DC1030 · Emergency Lighting > ORD - FLT 2248 - EN ROUTE DFW/ORD DURING CRUISE, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE IN MID AND FIRST CLASS CABINS ILLUMINATED. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. SYSTEM GROUND CHECKED NORMAL OPERATION. UNABLE TO DUPLICATE PROBLEM AND - [SDR AALA970884](https://openairdocs.org/sdr/AALA970884.md): Support · corroded · Apr 25, 1997 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - CORROSION ON CASTING SUPPORT FWD END OF FWD CARGO LOWER JAMB BELOW RT ROLLER TRAY AT STA 874 TO STA 888, LONGERON 43R. AFTER CORROSION BLEND-OUT, INSTALLED SPLICE ANGLE. REPLACED SPLICE DOUBLER PER ESO 7349 DATED 4-24-97. TST: 91,786 HRS. CYCLES, 18 - [SDR AALA970764](https://openairdocs.org/sdr/AALA970764.md): Roller Track · corroded · Apr 18, 1997 · N144AA · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > TUL - RIGHT ROLLER TRACK OUTBOARD FLANGE HAS DEEP CORROSION FORWARD CARGO AFT LOWER DOOR JAM AREA STA 999 AND LONGERON 43R. INSTALLED NEW SECTION OF ROLLER TRACK PER SRM 53-20-00, FIG 7. TST: 91,786.20 HOURS. CYCLES: 18,348. (X) - [SDR AALA970741](https://openairdocs.org/sdr/AALA970741.md): Door Frame · corroded · Apr 16, 1997 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - DURING C-CHECK, FOUND CORROSION AT L3 DOOR INSIDE NR 7 DOOR STOP ATTACH HOLES IN AFT DOOR FRAME STA 1305 AND CORROSION INSIDE NR 4 AND NR 5 DOOR STOP ATTACH HOLES IN FWD DOOR FRAME STA 1256. REAMED HOLES TO REMOVE CORROSION, TREATED, PRIMED, SRM 51-21-0 - [SDR AALA970733](https://openairdocs.org/sdr/AALA970733.md): Jamb · damaged · Apr 11, 1997 · N144AA · Doug DC1030 · Fuselage Miscellaneous Structure > TUL - DURING C-CHECK, FOUND TEMPORARY DOUBLER INSTALL ON BOTTOM OF AFT DOOR JAM BOX PANEL AT L3 DOOR. STA 1302 TO STA 1318. REMOVED EXISITNG DOUBLER AND INSTALLED NEW DOUBLER PER VOL I, SRM 53-50-00, FIG 19. TST: 91,786.20 HOURS. CYCLES: 18,348. (X) - [SDR AALA961242](https://openairdocs.org/sdr/AALA961242.md): Switch Cover · broken · Aug 19, 1996 · N144AA · Doug DC1030 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT ARMING SWITCH AT THE L1 DOOR REEL HAS BROKEN SPRING. REPLACED SWITCH COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA961063](https://openairdocs.org/sdr/AALA961063.md): Wire · loose · Jul 11, 1996 · N144AA · Doug DC1030 · Light System Wiring > DFW - DURING OVERNIGHT CHECK, FOUND WIRE PULLED OFF OF PLUG FOR THE R4 DOORWAY LIGHTING FORWARD BOTTOM EMERGENCY EXIT FLOOR PATH LIGHT. REPAIRED EMERGENCY EXIT FLOOR PATH WIRES TO PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (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 = 'N144AA' AND deregistration_id = 'N144AA-2002-05-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N144AA-2002-05-16/reports --- 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.