# Service difficulty reports: N14079, cancelled Jun 14, 2012 A list on [N14079, cancelled Jun 14, 2012](https://openairdocs.org/deregistered/N14079-2012-06-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0001683](https://openairdocs.org/sdr/CALA0001683.md): Skin · cracked · Nov 3, 2000 · N14079 · Doug DC1030 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND A 4 INCH CRACK IN RT HORIZONTAL STABILIZER UPPER AFT O/B SKIN. THE RT UPPER AFT O/B SKIN PANEL WAS REPAIRED IAW ECRA 5511-01035. - [SDR CALA0001681](https://openairdocs.org/sdr/CALA0001681.md): Fitting · corroded · Nov 1, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LAV E O/B SUPPORT BEAM CORRODED AT AFT ATTACHMENT FITTING, STA Y = 1831-1887, X = 31L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001657](https://openairdocs.org/sdr/CALA0001657.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LAV F I/B SUPPORT BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001656](https://openairdocs.org/sdr/CALA0001656.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LAV E I/B SUPPORT BEAM CORRODED AT STA. Y = 1831-1887, X = 5L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001655](https://openairdocs.org/sdr/CALA0001655.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND GALLEY G-2 SUPPORT BEAM CORRODED AROUND FORWARD ATTACHMENT BOLT HOLE AT STA Y = 392-412, X = 8R. A REPAIR WAS INSTALLED IAW GMM 10-900-01 AND 53-11-01. - [SDR CALA0001654](https://openairdocs.org/sdr/CALA0001654.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND GALLEY G-2 FLOOR SUPPORT CHANNEL SECTION CORRODED AT STA Y = 392-459, X = 40R. A NEW FLOOR SUPPORT CHANNEL SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001653](https://openairdocs.org/sdr/CALA0001653.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL SUPPORT BEAM AFT OF GALLEY G-1 CORRODED AT STA Y = 412-487, X = 24L. A NEW SECTION OF SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001652](https://openairdocs.org/sdr/CALA0001652.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND GALLEY G-6 O/B SUPPORT BEAM CORRODED AT FORWARD END. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001651](https://openairdocs.org/sdr/CALA0001651.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND GALLEY G-1 SUPPORT BEAM CORRODED AT STA Y = 392-422, X = 20L. A REPAIR WAS PERFORMED IAW GMM 10-900-01 AND SRM 53-11-1. - [SDR CALA0001650](https://openairdocs.org/sdr/CALA0001650.md): Floor Support · corroded · Oct 26, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LAV F O/B SUPPORT BEAM CORRODED AT Y = 1831-1887, X = 31R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-16-01. - [SDR CALA0001641](https://openairdocs.org/sdr/CALA0001641.md): Floor Support · corroded · Oct 24, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION AT BASE OF FLIGHT DECK STEP CORRODED AT STA Y = 392, X = 20L-20R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001640](https://openairdocs.org/sdr/CALA0001640.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP FORWARD OF GALLEY 6 AND 7 CORRODED AT STA Y = 1914, X = 17L-17R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001639](https://openairdocs.org/sdr/CALA0001639.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM FWD OF LAV H CORRODED AT STA Y = 1914, X = 44L-66L. A NEW SUPPORT SECTION WAS INSTALLED IAW SRM 53-16-01 AND GMM 10-900-01. - [SDR CALA0001628](https://openairdocs.org/sdr/CALA0001628.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP AFT OF LAVS E AND F AT STA Y = 1887, X = 5R-24R CORRODED. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001627](https://openairdocs.org/sdr/CALA0001627.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIPS AFT OF LAVS E & F AT STA Y = 1887, X = 28L-32L AND X = 38L-58L CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001626](https://openairdocs.org/sdr/CALA0001626.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING SECTIONS AFT OF LAVS E & F AT STA Y = 1887, X = 5L-24L AND X = 27R-53R CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001625](https://openairdocs.org/sdr/CALA0001625.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION CORRODED AT STA Y = 421, X = 24L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001624](https://openairdocs.org/sdr/CALA0001624.md): Floorbeam · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND GALLEY G3 LATERAL FLOORBEAM J SECTION CORRODED AT STA Y = 459, X = 18L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001623](https://openairdocs.org/sdr/CALA0001623.md): Floor Support · corroded · Oct 23, 2000 · N14079 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT LAVS E & F, STA Y = 1887, X = 38R-58R. A REPAIR WAS ACCOMPLISHED BY INSTALLING A NEW J SECTION IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001622](https://openairdocs.org/sdr/CALA0001622.md): Floorbeam · corroded · Oct 22, 2000 · N14079 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND LATERAL FLOORBEAM CORRODED AT STA Y = 459, X = 38R-41R. A SPLICE REPAIR WAS PERFORMED IAW SRM 53-30-00. - [SDR CALA0000146](https://openairdocs.org/sdr/CALA0000146.md): Fuse · failed · Feb 12, 2000 · N14079 · Doug DC1030 · Landing Gear Retraction/Extension System > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HNL. THE A/C WAS RETURNED TO HNL WHERE IT LANDED W/O INCIDENT. MX FOUND THE MLG INTERLOCK CYLINDER RETRACTED. RESET TRIM CYLINDER FUSE. INTERLOCK CYLINDER NOW IN PROPER POSITION IAW MM 32-31-06, PAGE 201 - [SDR CALA9901499](https://openairdocs.org/sdr/CALA9901499.md): Safety Wire · out of position · Nov 16, 1999 · N14079 · Doug DC1030 · Landing Gear Selector > CREW RECEIVED RED GEAR WARNING LIGHTS WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND GEAR WAS EXTENDED MANUALLY. ALL GEAR LIGHTS WERE GREEN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR CONTROL HANDLE WAS NOT MAKING CO - [SDR CALA9901480](https://openairdocs.org/sdr/CALA9901480.md): Angle · cracked · Nov 9, 1999 · N14079 · Doug DC1030 · Engine Cowling System > INSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT ANGLES WERE REPLACED IAW SRM 51-30-00. - [SDR CALA9901479](https://openairdocs.org/sdr/CALA9901479.md): Angle · cracked · Nov 9, 1999 · N14079 · Doug DC1030 · Wing Miscellaneous Structure > INSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9901478](https://openairdocs.org/sdr/CALA9901478.md): Skin · cracked · Nov 8, 1999 · N14079 · Doug DC1030 · Wing, Plate/Skin > INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CRACKED AT STA XORS 455 AND STA XORS 506. BOTH CRACKS WERE 1 LONG. REPAIRS WERE INSTALLED IAW DRAWING ARB2933-46, DRAWING ARB2933-10, SRM 57-10-00, FIGURE 49 AND 51-31-01. - [SDR CALA9901444](https://openairdocs.org/sdr/CALA9901444.md): Strip · cracked · Oct 28, 1999 · N14079 · Doug DC1030 · Leading Edge Devices > INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00. - [SDR CALA9901434](https://openairdocs.org/sdr/CALA9901434.md): Skin · cracked · Oct 25, 1999 · N14079 · Doug DC1030 · Wing, Plate/Skin > INSPECTION FOUND A 0.9 INCH CRACK IN RT WING LEADING EDGE SKIN AT XORS 783. A REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 68. - [SDR CALA9900509](https://openairdocs.org/sdr/CALA9900509.md): Rod · disconnected · May 10, 1999 · N14079 · Doug DC1030 · Emergency Exits > UNABLE TO ARM L3 DOOR AT DEPARTURE. FOUND ROD AT LOCKING MECHANISM OUT OF PLACE. REINSTALLED ROD AND TIGHTENED HARDWARE. - [SDR 98ZZZX4012](https://openairdocs.org/sdr/98ZZZX4012.md): Fan Frame · cracked · Sep 24, 1998 · N14079 · Doug DC1030 · Engine Thrust Reverser > THE NR 1 ENGINE REVERSER SEAL SUPPORT RING, LEFT, WAS FOUND CRACKED AT ALL FIVE FORWARD ATTACH POINTS. THE FLANGE SECTIONS HAD BROKEN COMPLETELY AWAY FROM THE TWO BOLT ATTACHMENTS IN AN ARC THE CRACK PASSING THROUGH THE TOP ROW OF TWO ATTACHMENT RIVETS OF A S - [SDR CALA9801671](https://openairdocs.org/sdr/CALA9801671.md): Hyd Line · punctured · Sep 9, 1998 · N14079 · Doug DC1030 · Hydraulic System, Main > THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN HYDRAULIC PRESSURE LINE TO LEFT HYDRAULIC PUMP AND THE RIGHT PUMP WAS LEAKING HYDRAULIC FLUID OUT DRAIN MAST. THE - [SDR CALA9801456](https://openairdocs.org/sdr/CALA9801456.md): Smoke Detector · inoperative · Aug 16, 1998 · N14079 · Doug DC1030 · Smoke Detection > THE AFT CARGO FIRE WARNING LIGHT AND SMOKE DETECTOR LIGHT ILLUMINATED WHILE ENROUTE. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE LIGHTS EXTINGUISHED. BOTH CARGO FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SJU WHERE IT LANDED WITHOUT INC ## 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 = 'N14079' AND deregistration_id = 'N14079-2012-06-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14079-2012-06-14/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.