# Service difficulty reports: N73243, cancelled Feb 2, 1999 A list on [N73243, cancelled Feb 2, 1999](https://openairdocs.org/deregistered/N73243-1999-02-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9701698](https://openairdocs.org/sdr/CALA9701698.md): Skin · corroded · Nov 26, 1997 · N73243 · Boeing 7372C0 · Fuselage Main, Plate/Skin > INSPECTION FOUND CORROSION IN SKIN LAP AT STA 400, LONGERON 24L. A DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 16. - [SDR CALA9701615](https://openairdocs.org/sdr/CALA9701615.md): Frame · cracked · Nov 13, 1997 · N73243 · Boeing 7372C0 · Service Doors > INSPECTION FOUND A 2 INCH CRACK IN LOWER FORWARD FRAME OF R-1 DOOR AND AN 8 INCH CRACK WAS FOUND IN LOWER AFT FRAME OF R-1 DOOR. THE R-1 WAS REMOVED AND REPLACED AND RIGGED IAW MM 52-41-0. LEAK AND OPERATIONAL CHECKS WERE GOOD. - [SDR CALA9701613](https://openairdocs.org/sdr/CALA9701613.md): Battery Pack · discharged · Nov 12, 1997 · N73243 · Boeing 7372C0 · Emergency Lighting > INSPECTION FOUND LEFT SIDE EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. - [SDR CALA9601726](https://openairdocs.org/sdr/CALA9601726.md): Web · cracked · Nov 5, 1996 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A CRACK IN LT MLG WHEEL WELL UPPER PRESSURE WEB AT LT FORWARD CORNER JUST AFT OF STA 664. LENGTH OF CRACK NOT IDENTIFIED. THE WEB WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND 53-10-2, FIGURE 3. - [SDR CALA9601728](https://openairdocs.org/sdr/CALA9601728.md): Skin · creased · Oct 31, 1996 · N73243 · Boeing 7372C0 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN CREASED AND OIL CANNED. THE DAMAGED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-3 FIGURE 6, 52-30-3 AND 51-10-6. - [SDR CALA9601727](https://openairdocs.org/sdr/CALA9601727.md): Support · corroded · Oct 31, 1996 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 887, RBL 60. THE CORRODED AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND 53-10-2. - [SDR CALA9601341](https://openairdocs.org/sdr/CALA9601341.md): Air Data Comp · contaminated · Sep 27, 1996 · N73243 · Boeing 7372C0 · Air Data Computer > THE ACFT EXPERIENCED INTERMITTENT ROLL OF NO MORE THAN 10 DEGREES UNCOMMANDED WITH BOTH AUTOPILOT A ANDB SELECTED WHILE EN ROUTE. PITCH MODE FUNCTIONED NORMALLY. MAINTENANCE PERFORMED A GROUND TEST OF BOTH AUTOPILOT SYSTEMS. THE A-SYSTEM WAS TOTALLY INOPERA - [SDR CALA9600745](https://openairdocs.org/sdr/CALA9600745.md): Engine · oil leak · Jun 3, 1996 · N73243 · Boeing 7372C0 · Turbine Engine Oil System > THE NR 2 ENGINE OIL PRESSURE AND QUANTITY DROPPED ON TAKEOFF. THE DROP IN PRESSURE AND QUANTITY WAS ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGI - [SDR CAL960383](https://openairdocs.org/sdr/CAL960383.md): Battery Pack · discharged · Mar 21, 1996 · N73243 · Boeing 7372C0 · Emergency Lighting > FLT NR 1626 - CLE - INSPECTION FOUND BOTH THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT RIGHT WING EMERGENCY EXIT INOPERATIVE. THE CHARGER AND BATTERY PACK WERE REMOVED AND THE CONNECTIONS TO BOTH WERE CLEANED. EXTERIOR SOCKET WAS RELAMPED AND OPERATION OF T - [SDR CAL960154](https://openairdocs.org/sdr/CAL960154.md): Firewall · cracked · Feb 9, 1996 · N73243 · Boeing 7372C0 · Nacelle/Pylon, Bulkhead/Firewall > IAH - INSPECTION FOUND THE NR 2 ENGINE PYLON FIREWALL PAN HAD A 2.5 INCH CRACK THROUGH FOUR FASTENERS AT NAC STATION 144. A DOUBLER WAS INSTALLED IAW ECRA 5450-01139. A DIP WAS ISSUED TO REINSPECT THE AREA AT LPV CHECKS AND PERMANENTLY REPAIR PAN AT NEXT 1/4 - [SDR CAL960110](https://openairdocs.org/sdr/CAL960110.md): Turb Blade · broke · Feb 8, 1996 · N73243 · Boeing 7372C0 · Turbine Section > FLT NR 1930 - IAH - THE NR 2 ENGINE SHUDDERED AND THEN BEGAN TO LOSE POWER DURING CLIMB-OUT OF IAH. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION - [SDR CAL951137](https://openairdocs.org/sdr/CAL951137.md): Doubler · corroded · Dec 1, 1995 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > GSO - INSPECTION FOUND DOUBLER CORRODED AT STA 323, STR 27L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02337. (X) - [SDR CAL951136](https://openairdocs.org/sdr/CAL951136.md): Angle · corroded · Dec 1, 1995 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > GSO - INSPECTION FOUND T-ANGLE CORRODED AT STA 323, S27L TO S27R. A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-2. (X) - [SDR CAL951135](https://openairdocs.org/sdr/CAL951135.md): Angle · corroded · Dec 1, 1995 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > GSO - INSPECTION FOUND T-ANGLE CORRODED AT STA 323 - STA 328, RT SIDE. A NEW T-ANGLE, SPLICES, AND DOUBLER WERE INSTALLED IAW ECRA 5330-02337. (X) - [SDR CAL951134](https://openairdocs.org/sdr/CAL951134.md): Skin · corroded · Dec 1, 1995 · N73243 · Boeing 7372C0 · Fuselage Main, Plate/Skin > GSO - INSPECTION FOUND RT FUSELAGE SKIN PANEL CORRODED AT STA 290. THE SKIN PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) - [SDR CAL951132](https://openairdocs.org/sdr/CAL951132.md): Panel · cracked · Nov 28, 1995 · N73243 · Boeing 7372C0 · Fuselage Miscellaneous Structure > GSO - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEELWELL CEILING PRESSURE PANEL AT STA 277, RT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5310-03186. (X) - [SDR CAL950849](https://openairdocs.org/sdr/CAL950849.md): Hyd Pump · inoperative · Sep 21, 1995 · N73243 · Boeing 7372C0 · Hydraulic Pump (Electric/Engine), Main > FLT NR 1746 - GSO - THE HYDRAULIC QUANTITY INDICATOR GAUGE DECREASED SLOWLY TO ZERO WITH NO OTHER INDICATIONS WHILE ON APPROACH TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE HYDRAULI - [SDR CAL950745](https://openairdocs.org/sdr/CAL950745.md): Hyd Pump · leaking · Aug 22, 1995 · N73243 · Boeing 7372C0 · Hydraulic Pump (Electric/Engine), Main > GSO - FLT 1275 - THE A-SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO DURING CLIMB-OUT OF GSO. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM LOW PRESSURE LIGHTS. A MANUAL GEAR AND FLAP EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS RETU - [SDR CAL950129](https://openairdocs.org/sdr/CAL950129.md): Fire Warning · activated · Feb 13, 1995 · N73243 · Boeing 7372C0 · Fire Detection > EWR - FLT 1452 - WHEN THE APU WAS STARTED ON APPROACH, THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. THE APU WAS SHUTDOWN, THE APU FIRE BOTTLE WAS DISCHARGED AND THE FIRE WARNING CEASED. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FI ## 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 = 'N73243' AND deregistration_id = 'N73243-1999-02-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N73243-1999-02-02/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.