# Service difficulty reports: N703AA, cancelled Jul 9, 2013 A list on [N703AA, cancelled Jul 9, 2013](https://openairdocs.org/deregistered/N703AA-2013-07-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 20001127SH016](https://openairdocs.org/sdr/20001127SH016.md): Cylinder · cracked · Nov 6, 2000 · N703AA · Boeing 727223 · Main Landing Gear Attach Section > SUBJECT PART RECEIVED WITH SEVERE CRACK INDICATION EXTENDING ALL THE WAY THROUGH THE AFT TRUNNION SPUD AREA. (X) - [SDR AALA991694](https://openairdocs.org/sdr/AALA991694.md): Controller · malfunctioned · Nov 10, 1999 · N703AA · Boeing 727223 · Detection System > CUN - FLT 0940 - EN ROUTE TO MIA, NR 3 ENGINE FIRE DETECTION SYSTEM INOPERATIVE. AIRCRAFT LANDED CUN WITHOUT INCIDENT. REPLACED NR 3 ENGINE FIRE DETECTOR MODULE CONTROL. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA991594](https://openairdocs.org/sdr/AALA991594.md): Light · inoperative · Oct 24, 1999 · N703AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR VENTRAL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR VENTRAL EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA990813](https://openairdocs.org/sdr/AALA990813.md): Bulkhead Web · cracked · Jun 2, 1999 · N703AA · Boeing 727223 · Fuselage Main, Bulkhead > TUL - APPROX 1 INCH CRACK IN STATION 870 BULKHEAD WEB AT APU LOAD CONTROL VALVE CUTOUT. STOP DRILLED CRACK AND INSTALLED REPAIR AS PER SRM 53-10-2 PAGE 261C. (M) - [SDR AALA990812](https://openairdocs.org/sdr/AALA990812.md): Bulkhead Angle · cracked · Jun 2, 1999 · N703AA · Boeing 727223 · Fuselage Main, Bulkhead > TUL - FOUND STATION 870 BULKHEAD TO KEELBEAM ATTACH ANGLE CRACKED RIGHT W/W. REPLACED CRACKED ANGLE WITH NEW. (M) - [SDR AALA990815](https://openairdocs.org/sdr/AALA990815.md): Frame · cracked · May 28, 1999 · N703AA · Boeing 727223 · Cargo/Baggage Doors > TUL - CRACK IN FORWARD FRAME WEB NR 2 CARGO DOOR FRAME FROM LOWER DOOR STOP TO TOOLING HOLE. NO STOP DRILL REQUIRED. INSTALLED DOUBLER REPAIR PER S/B 727-53-A0199 DATED AUG 5, 1993 PER CARD 5295 PG A4. (M) - [SDR AALA990814](https://openairdocs.org/sdr/AALA990814.md): Keel Beam · cracked · May 28, 1999 · N703AA · Boeing 727223 · Fuselage Main, Keel > TUL - FOUND LEFT KEEL BEAM CHORD CRACKED AT FORWARD FASTENER HOLE AT STATION 871 INSIDE KEEL BEAM, CRACK ENDED AT HOLE. INSTALLED DOUBLER REPAIR PER REV 1, S/B 727-53-0208, DATED FEB 29/96. (M) - [SDR AALA990810](https://openairdocs.org/sdr/AALA990810.md): Skin · corroded · May 27, 1999 · N703AA · Boeing 727223 · Wing, Plate/Skin > TUL - FOUND CORROSION ON CENTER TANK SKIN ABOVE LEFT AFT PLENUM. REMOVED CORROSION AND INSTALLED DOUBLER/TRIPLER REPAIR PER SRM 57-30-3. (M) - [SDR AALA99081](https://openairdocs.org/sdr/AALA99081.md): Skin · gouged · May 27, 1999 · N703AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - FUSELAGE SKIN GOUGED STRINGER 8R STATION 610, RED 'M' AREA. CUTOUT DAMAGED AREA OF SKIN. INSALLED DOUBLER PER SRM 53-30-3. (M) - [SDR AALA980524](https://openairdocs.org/sdr/AALA980524.md): Light · defective · Mar 18, 1998 · N703AA · Boeing 727223 · Emergency Lighting > DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTING EXIT SIGN IN FIRST CLASS INOPERATIVE. REPLACED THREE EMERGENCY EXIT FLOOR LIGHT SEGMENTS UNDER EXIT SIGN IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980089](https://openairdocs.org/sdr/AALA980089.md): Stringer · cracked · Jan 12, 1998 · N703AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - LEFT FUSELAGE STR 24L CRACKED AND FUSELAGE SKIN DENTED FROM STA 475 TO STA 478. INSTALLED STRINGER REPAIR PER SRM 53-10-3. INSTALLED FUSELAGE SKIN DOUBLER PER SRM 53-30-3. TST: 46,539 HOURS. CYCLES: 24,289. (X) - [SDR AALA960965](https://openairdocs.org/sdr/AALA960965.md): Skin · corroded · Jun 25, 1996 · N703AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - CORROSION ON FUSELAGE SKIN BELOW STR 28L, ST 480 - STA 500. REPAIRED PER SRM 53-30-3, FIGURE 3A, PAGE 14. TST: 42,362 HOURS. CYCLES, 22,280. (X) - [SDR AALA960964](https://openairdocs.org/sdr/AALA960964.md): Skin · cracked · Jun 25, 1996 · N703AA · Boeing 727223 · Fuselage Main, Plate/Skin > TUL - UPPER POST BETWEEN CAPTAIN'S SLIDING WINDOW AND WINDSHIELD IS CRACKED (VERIFIED BY DYE PENETRANT CHECK) EXTERNAL SKIN. STOPPED DRILLED CRACK. HFEC SHOWS NO CRACKING PAST STOP DRILL HOLE. DRILLED HOLES IN DOUBLER AND INSTALLED DOUBLER IAW SRM 53-30-3, - [SDR AALA960963](https://openairdocs.org/sdr/AALA960963.md): Stringer · corroded · Jun 25, 1996 · N703AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > FOUND CORROSION ON STRINGER 29R. CUT AND SPLICED NEW SECTION OF STRINGER PER SRM 53-10-3 PG 11A-11E. (M) - [SDR AALA960962](https://openairdocs.org/sdr/AALA960962.md): Stringer · corroded · Jun 25, 1996 · N703AA · Boeing 727223 · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 28L JUST AFT OF STA 480. REPAIRED PER SRM 53-10-3, FIGURE 1, PAGE 4. TST: 42,362 HOURS. CYCLES, 22,280. (X) - [SDR AALA960045](https://openairdocs.org/sdr/AALA960045.md): Fuel Pump · defective · Jan 11, 1996 · N703AA · Boeing 727223 · Engine Fuel Pump > MEX - FLT 2087 - DURING DESCENT INTO MEX, FUEL HEAT APPLIED PER PROCEDURES. UPON LEVEL OFF WHEN POWER LEVERS INCREASED, NOTED NR 3 ENGINE HAD EXPERIENCED FLAME-OUT. ATTEMPTED NR 3 ENGINE RESTART. ACCOMPLISHED ENGINE SHUT-DOWN PROCEDURE AND AIRCRAFT PROCEEDE - [SDR AALA950724](https://openairdocs.org/sdr/AALA950724.md): Accessory Unit · defective · Apr 21, 1995 · N703AA · Boeing 727223 · Landing Gear Retraction/Extension System > DFW - FLT 0636 - AFTER TAKEOFF HOU, UNABLE TO RAISE LANDING GEAR HANDLE. DEPRESSED LANDING GEAR OVERRIDE TRIGGER AND LANDING GEAR HANDLE MOVED TO UP POSITION AND LANDING GEAR RETRACTED. AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. REPLACED LANDING G - [SDR AALA950238](https://openairdocs.org/sdr/AALA950238.md): Air Distr · smoking · Feb 8, 1995 · N703AA · Boeing 727223 · Air Distribution System > SJC-CCS - FLT 2141 - DURING CRUISE PASSENGERS AND FLIGHT ATTENDANTS REPORTED SMELLING SMOKE IN MID SECTION OF ACFT. SMELL DISSIPATED, PRECAUTIONARY TESTED AFT BODY OVERHEAT CIRCUIT. LANDED CCS WITHOUT INCIDENT. COULD NOT DUPLICATE ON GROUND, SYSTEM GROUND C ## 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 = 'N703AA' AND deregistration_id = 'N703AA-2013-07-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N703AA-2013-07-09/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.