# Service difficulty reports: N71314, cancelled Feb 19, 2004 A list on [N71314, cancelled Feb 19, 2004](https://openairdocs.org/deregistered/N71314-2004-02-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0300047](https://openairdocs.org/sdr/CALA0300047.md): Pressure Panel · cracked · Feb 14, 2003 · N71314 · Boeing 7373T0 · Fuselage Floor Panel > INSPECTION FOUND A.75 INCH CRACK IN BOTH THE LEFT HAND AND RIGHT HAND PRESSURE DECK AT STA 663.75. BOTH LOCATIONS WERE REPAIRED IAW SRM 53-60-51. - [SDR CALA0101018](https://openairdocs.org/sdr/CALA0101018.md): Web · corroded · Dec 2, 2001 · N71314 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO DOOR THRESHOLD SILL WEB CORRODED ON TOP AND UNDER SIDE. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0101012](https://openairdocs.org/sdr/CALA0101012.md): Frame · corroded · Nov 25, 2001 · N71314 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME CORRODED AT STA 794.3, STRINGER 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. - [SDR CALA0101011](https://openairdocs.org/sdr/CALA0101011.md): Angle · corroded · Nov 25, 2001 · N71314 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD L-ANGLE SUPPORT FOR SILL WEB CORRODED AT THRESHOLD OF AFT PIT, STA 704, STRINGER 25R. A NEW ANGLE WAS INSTALLED IAW BOEING DRAWING 69-43233 AND SRM 51-40-02. - [SDR CALA0101008](https://openairdocs.org/sdr/CALA0101008.md): Skin · cracked · Nov 21, 2001 · N71314 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND A 2" CRACK IN L/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01608. - [SDR CALA011007](https://openairdocs.org/sdr/CALA011007.md): Angle · corroded · Nov 20, 2001 · N71314 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT L-ANGLE SUPPORT FOR SILL WEB CORRODED AT AFT PIT THRESHOLD, STA 870, LONGERON 25L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00. - [SDR CALA011006](https://openairdocs.org/sdr/CALA011006.md): Frame · cracked · Nov 20, 2001 · N71314 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR FORWARD FRAME BETWEEN #3 & #4 STOP FITTINGS. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0101002](https://openairdocs.org/sdr/CALA0101002.md): Skin · gouged · Nov 14, 2001 · N71314 · Boeing 7373T0 · Trailing Edge Flaps > INSPECTION FOUND THE R/H O/B FOREFLAP L/E O/B EDGE WITH SEVERAL DEEP GOUGES IN SKIN. A REPAIR WAS INSTALLED IAW SRM 57-53-01. - [SDR CALA0100998](https://openairdocs.org/sdr/CALA0100998.md): Skin · cracked · Nov 9, 2001 · N71314 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1.3" CRACK IN KEEL BEAM SKIN AT STA 699, RBL 5 AND A 1/2" CRACK WAS FOUND IN KEEL BEAM SKIN AT STA 699, LBL 5. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-60-12. - [SDR CALA0100997](https://openairdocs.org/sdr/CALA0100997.md): Skin · cracked · Nov 9, 2001 · N71314 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 3.5" CRACK IN KEEL BEAM SKIN AT STA 674, RBL 5. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-12, FIGURE 202. - [SDR CALA9901131](https://openairdocs.org/sdr/CALA9901131.md): Bulkhead Web · cracked · Sep 5, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Bulkhead > INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD WEB CRACKED IN FOUR PLACES AT FASTENER HOLES AT STA 1016, STRINGER 6L-7L. ALSO, SEVERAL ELONGATED HOLES WERE FOUND. REPAIRED IAW ECRA 5310-03917. - [SDR CALA9901097](https://openairdocs.org/sdr/CALA9901097.md): Floorbeam · corroded · Aug 27, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND RT AND LT AFT LAV FLOORBEAM CORRODED ON NUT PLATE HOLES AT STA 1016, RBL 0 TO RBL 50 AND LBL 0 TO LBL 40. REPAIRED IAW ECRA 5310-03906. - [SDR CALA9901096](https://openairdocs.org/sdr/CALA9901096.md): Floorbeam · corroded · Aug 27, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 985.5 FROM LBL 18 TO R-2 DOOR JAMB. REPAIRED IAW ECRA 5310-03906. - [SDR CALA9901077](https://openairdocs.org/sdr/CALA9901077.md): Seat Track · corroded · Aug 22, 1999 · N71314 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 328-344. REPAIRED IAW SRM 53-00-52, FIGURE 202, SHEET 1. - [SDR CALA9901066](https://openairdocs.org/sdr/CALA9901066.md): Floorbeam · corroded · Aug 18, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 14 TO RBL 12. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA9901059](https://openairdocs.org/sdr/CALA9901059.md): Floorbeam · corroded · Aug 15, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND CORROSION ON FLOORBEAM WITH FASTENERS PULLED THROUGH AT STA 328, LBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA9901056](https://openairdocs.org/sdr/CALA9901056.md): Floorbeam · corroded · Aug 14, 1999 · N71314 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312 BETWEEN LBL 10 AND RBL 32. INSTALLED REPAIR IAW SRM 53-10-51, FIGURE 205. - [SDR CALA9800728](https://openairdocs.org/sdr/CALA9800728.md): Skin · wrinkled · Apr 30, 1998 · N71314 · Boeing 7373T0 · Trailing Edge Flaps > RIGHT WING O/B FOREFLAP HAS WRINKLED SKIN. REPLACED RIGHT WING O/B FOREFLAP PER MM 27-51-37. - [SDR CALA9800007](https://openairdocs.org/sdr/CALA9800007.md): Sensor · out of adjust · Jan 8, 1998 · N71314 · Boeing 7373T0 · Landing Gear Retraction/Extension System > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE GEAR HANDLE WOULD NOT GO PAST OFF POSITION. MAINTENANCE FOUND THE MAIN GEAR AIR SAFETY SENSOR OUT OF ADJUSTMENT. THE AIR SAFETY SENSOR WAS ADJUSTED/TESTED IAW MM 32-09-01 AND GEAR HANDLE OPERATI - [SDR CALA9600905](https://openairdocs.org/sdr/CALA9600905.md): Hyd Line · leaking · Jun 27, 1996 · N71314 · Boeing 7373T0 · Hydraulic System, Main > THE A-HYDRAULIC SYSTEM FLUID WAS LOST ON FINAL APPROACH TO EWR. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 BRAKE LINE LEAKING. THE BRAKE LINE WAS REMOVED AND REPLACED AND THE BRAKES WERE BLED, - [SDR CAL960334](https://openairdocs.org/sdr/CAL960334.md): Uplock Act · inoperative · Mar 18, 1996 · N71314 · Boeing 7373T0 · Landing Gear Retraction/Extension System > IAH - FLT 1703 - THE RT MLG GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A TOWER FLYBY VERIFIED THE RT GEAR WAS NOT EXTENDED. A MANUAL GEAR EXTENSION WAS PERFORMED WITH 3 GREEN LIGHTS INDICATED AND A SECOND TOWER FLYBY CONFIRME - [SDR CAL960111](https://openairdocs.org/sdr/CAL960111.md): Fan · inoperative · Feb 9, 1996 · N71314 · Boeing 7373T0 · Air Distribution Fan > FLT NR 1082 - CLE - A SMOKEY ODOR IN REAR OF CABIN WAS REPORTED TWICE DURING FLIGHT. THE AIR WAS CLEARED BOTH TIMES BY USING HIGH POSITION ON BOTH PACKS. MAINTENANCE RAN BOTH PACKS AND INSPECTED THE WATER SEPARATOR BAGS. MAINTENANCE WAS UNABLE TO REPRODUCE - [SDR CAL950868](https://openairdocs.org/sdr/CAL950868.md): Hyd Pump · inoperative · Sep 30, 1995 · N71314 · Boeing 7373T0 · Hydraulic Pump (Electric/Engine), Main > IAH - FLT 1769 - THE B-SYSTEM HYDRAULIC QUANTITY DECREASED TO JUST ABOVE ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE DRIVE ## 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 = 'N71314' AND deregistration_id = 'N71314-2004-02-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N71314-2004-02-19/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.