# Service difficulty reports: N19072, cancelled Oct 23, 2002 A list on [N19072, cancelled Oct 23, 2002](https://openairdocs.org/deregistered/N19072-2002-10-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9901363](https://openairdocs.org/sdr/CALA9901363.md): Support · cracked · Oct 8, 1999 · N19072 · Doug DC1030 · Nacelle/Pylon Structure > PYLON NUMBER ONE SUPPORT PANELS 437DR/437ML CRACKED (0.5). REPLACED SUPPORT PER SRM 51-31-01. - [SDR CALA9901362](https://openairdocs.org/sdr/CALA9901362.md): Angle · cracked · Oct 8, 1999 · N19072 · Doug DC1030 · Wing Miscellaneous Structure > RIGHT WING OUTBOARD FLAP OUTBOARD FAIRING RIGHT SIDE ANGLE IS CRACKED (0.5). REPLACED ANGLE PER SRM 51-33-01. - [SDR CALA9901361](https://openairdocs.org/sdr/CALA9901361.md): Skin · cracked · Oct 8, 1999 · N19072 · Doug DC1030 · Wing, Plate/Skin > LEFT WING LEADING EDGE INTERNAL SKIN CRACKED (4) AT STA XORS562. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-00 AND DWG ARB 3954. - [SDR CALA9901336](https://openairdocs.org/sdr/CALA9901336.md): Skin · cracked · Oct 6, 1999 · N19072 · Doug DC1030 · Landing Gear Doors > INSPECTION FOUND A 2.5 INCH CRACK IN LT FORWARD NLG DOOR SKIN. THE AREA WAS REPAIRED IAW SRM 52-00-01. - [SDR CALA9901119](https://openairdocs.org/sdr/CALA9901119.md): Wire · damaged · Sep 1, 1999 · N19072 · Doug DC1030 · Light System Wiring > INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEATS 29AB TO 35AB. MAINTENANCE REPAIRED DAMAGED WIRES AT SEAT 32AB IAW WDM 33-53-03 AND OPERATION CHECKED GOOD. - [SDR CALA9900761](https://openairdocs.org/sdr/CALA9900761.md): Battery · discharged · Jun 30, 1999 · N19072 · Doug DC1030 · Emergency Lighting > THE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK AND CHARGER AT DOOR 3L WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-01, PAGE 201. - [SDR CALA9900710](https://openairdocs.org/sdr/CALA9900710.md): Fuel Line · broken · Jun 18, 1999 · N19072 · Doug DC1030 · Engine Fuel Distribution > THE NR 3 ENGINE FLAMED OUT DUE TO LOSS OF FUEL FLOW WHILE EN ROUTE FROM GUM TO HNL. ALL OTHER ENGINE PARAMETERS WERE IN NORMAL RANGE AT TIME OF FAILURE. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE EDU - [SDR CALA9900206](https://openairdocs.org/sdr/CALA9900206.md): Slide · low pressure · Mar 3, 1999 · N19072 · Doug DC1030 · Escape Slide > THE R-3 DOOR EMERGENCY SLIDE LOW PRESSURE INDICATOR LIGHT WAS FOUND ILLUMINATED DURING A PRE-DEPARTURE CHECK. THE R-3 DOOR EMERGENCY SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-02, PAGE 201-208. - [SDR CALA9802086](https://openairdocs.org/sdr/CALA9802086.md): Battery Pack · discharged · Nov 20, 1998 · N19072 · Doug DC1030 · Emergency Lighting > INSPECTION FOUND FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9801601](https://openairdocs.org/sdr/CALA9801601.md): Skin · cracked · Aug 31, 1998 · N19072 · Doug DC1030 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND A 1 CRACK IN SKIN OF RT HORIZONTAL STABILIZER LEADING EDGE ON SECOND SECTION NEAR THE LOWER EXTERNAL CORNER. THE AREA WAS REPAIRED IAW ECRA 5513-01001. - [SDR CALA9801559](https://openairdocs.org/sdr/CALA9801559.md): Skin · cracked · Aug 26, 1998 · N19072 · Doug DC1030 · Wing, Plate/Skin > INSPECTION FOUND A 1.5 CRACK IN LT WING LEADING EDGE SKIN AT STA XORS 683. THE SKIN WAS REPAIRED IAW SRM 57-10-00, FIGURE 49 AND FIGURE 68, SHEET 10. - [SDR CALA9801173](https://openairdocs.org/sdr/CALA9801173.md): Hyd Line · ruptured · Jun 27, 1998 · N19072 · Doug DC1030 · Hydraulic System, Main > THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG TRIM CYLINDER HYDRAULIC LINE RUPTURED. THE HYDRAULIC LINE WAS REMOV - [SDR CALA9800653](https://openairdocs.org/sdr/CALA9800653.md): Frame · broken · Apr 8, 1998 · N19072 · Doug DC1030 · Fuselage Main, Frame > THE AIRCRAFT LOST NR 3 HYDRAULIC SYSTEM FLUID WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED THE LT MLG SUPPORT FRAME ASSEMBLY WAS BROKEN. *S/D* FAILURE OF THE SUPPORT FRAME ASSEMBLY RESULTED IN - [SDR CALA9701340](https://openairdocs.org/sdr/CALA9701340.md): Intercostal · corroded · Aug 20, 1997 · N19072 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 1964 TO 1973, LONGERON 47L TO 48L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-35-01. - [SDR CALA9701339](https://openairdocs.org/sdr/CALA9701339.md): Doubler · corroded · Jul 31, 1997 · N19072 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FINGER DOUBLER CORRODED BETWEEN STA 1700 AND 1720, LONGERON 51. THE FINGER DOUBLER WAS REMOVED, A NEW FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-33-01 AND 53-00-01. - [SDR CALA9601875](https://openairdocs.org/sdr/CALA9601875.md): Hyd Pump · cracked · Dec 24, 1996 · N19072 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main > THE A/C LOST NR 2 SYSTEM HYDRAULIC FLUID WHILE ENROUTE FROM HNL TO GUM. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF BOTH LT AND RT PUMP PRESSURE LOW LIGHTS. THE NR 2 HYD QTY LOSS CHECKLIST WAS PERFORMED, FUEL WAS DUMPED, AND THE A/C WAS RETURNED TO HNL W - [SDR CALA9601859](https://openairdocs.org/sdr/CALA9601859.md): Decoder · failed · Dec 20, 1996 · N19072 · Doug DC1030 · Data Transmission Auto Call > THE SECOND OFFICER WAS NOTIFIED THAT THE READING LIGHTS IN MIDDLE SECTION OF COACH WERE INOPERATIVE WHILE IN FLIGHT. THE CIRCUIT BREAKER FOR THE READING LIGHTS WAS OUT. IT WAS RESET AND BEGAN FUNCTIONING. A BURNING SMELL AND SMOKE WERE THEN OBSERVED. THE - [SDR CAL960277](https://openairdocs.org/sdr/CAL960277.md): Hyd Pump · leaking · Feb 29, 1996 · N19072 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main > FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAULIC QUANTITY. BOTH PUMPS WERE SHUTOFF AND TEMP WAS NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. BOTH NR 2 ENGINE HYDRAULIC PUMPS WERE RE - [SDR CAL960276](https://openairdocs.org/sdr/CAL960276.md): Hyd Pump · leaking · Feb 29, 1996 · N19072 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main > FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAULIC QUANTITY. BOTH PUMPS WERE SHUTOFF AND TEMP WAS NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. BOTH NR 2 ENGINE HYDRAULIC PUMPS WERE RE ## 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 = 'N19072' AND deregistration_id = 'N19072-2002-10-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N19072-2002-10-23/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.