# Service difficulty reports: N14814, cancelled Oct 2, 2002 A list on [N14814, cancelled Oct 2, 2002](https://openairdocs.org/deregistered/N14814-2002-10-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0200032](https://openairdocs.org/sdr/CALA0200032.md): Skin · cracked · Jan 23, 2002 · N14814 · Doug DC982 · Engine Thrust Reverser > INSPECTION FOUND A 1" CRACK IN #1 ENGINE UPPER THRUST REVERSER OUTER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 7830-01000. - [SDR CALA0200031](https://openairdocs.org/sdr/CALA0200031.md): Skin · cracked · Jan 23, 2002 · N14814 · Doug DC982 · Engine Thrust Reverser > INSPECTION FOUND A 1" CRACK IN #2 ENGINE UPPER THRUST REVERSER OUTER SKIN. TWO DOUBLERS WERE INSTALLED IAW ECRA 7830-01000. - [SDR CALA0001780](https://openairdocs.org/sdr/CALA0001780.md): Intercostal · cracked · Nov 16, 2000 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND TWO.5 INCH CRACKS IN INTERCOSTAL IN MID CARGO COMPARTMENT AT STA 769 - 788, CENTERLINE. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001745](https://openairdocs.org/sdr/CALA0001745.md): Frame · corroded · Nov 13, 2000 · N14814 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND AFT SIDE OF BELT FRAME CORRODED IN AFT BAGGAGE BIN AT STA 1302, LONGERON 22L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A NEW SECTION WAS INSTALLED USING SPLICE ANGLES IAW SRM 53-03, FIGURE 2A. - [SDR CALA0001744](https://openairdocs.org/sdr/CALA0001744.md): Cargo Track · corroded · Nov 13, 2000 · N14814 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT STA 1212 - 1322. A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 51-30. - [SDR CALA0001723](https://openairdocs.org/sdr/CALA0001723.md): Floorbeam · corroded · Nov 10, 2000 · N14814 · Doug DC982 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE UNDER LT AFT LAV AT STA 1338. A REPAIR WAS INSTALLED IAW ECRA 5305-01051. - [SDR CALA0001705](https://openairdocs.org/sdr/CALA0001705.md): Pan · gouged · Nov 9, 2000 · N14814 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT BAGGAGE BIN DOOR STOP PAD FITTING ATTACH POINT SKIN GOUGED AT AFT LOWER LOCATION. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01540. - [SDR CALA0001703](https://openairdocs.org/sdr/CALA0001703.md): Web · corroded · Nov 8, 2000 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP AT LT SIDE FLOOR LINE CORRODED AT STA 190 - 237. A REPAIR WAS INSTALLED IAW ECRA 5310-04066. - [SDR CALA0001699](https://openairdocs.org/sdr/CALA0001699.md): Seat Track · corroded · Nov 7, 2000 · N14814 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT MID SEAT TRACK CORRODED AT STA 1030 - 1200. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA0001685](https://openairdocs.org/sdr/CALA0001685.md): Channel · corroded · Nov 3, 2000 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD Z-CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 53-05, FIGURE 63, SHEET 1. - [SDR CALA0001684](https://openairdocs.org/sdr/CALA0001684.md): Seat Track · corroded · Nov 3, 2000 · N14814 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1030 - 1132. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05. - [SDR CALA0001682](https://openairdocs.org/sdr/CALA0001682.md): Attach Angle · cracked · Nov 2, 2000 · N14814 · Doug DC982 · Vertical Stabilizer > INSPECTION FOUND A 1.125 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1463. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23. - [SDR CALA9900989](https://openairdocs.org/sdr/CALA9900989.md): Wire · loose · Aug 5, 1999 · N14814 · Doug DC982 · Landing Gear System Wiring > THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF FROM IAH. THE GEAR HANDLE WAS EXTENDED, BUT THE LIGHT REMAINED ON WITH THE GEAR DOOR OPEN LIGHT ILLUMINATING INTERMITTENTLY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED - [SDR CALA9900454](https://openairdocs.org/sdr/CALA9900454.md): Manifold · cracked · Apr 26, 1999 · N14814 · Doug DC982 · Engine Fuel Distribution > NUMBER 2 FUEL FLOW INDICATES HIGHER THAN NUMBER 1 ON TAKEOFF. AT CLIMB POWER NUMBER 2 FUEL FLOW IS 1000 POUNDS HIGHER AND AT CRUISE 500 POUNDS HIGHER. FUEL USED AND FUEL REMAINING VERIFY THE HIGHER FUEL FLOW. FOUND CRACKED FUEL MAINFOLD. REMOVED AND REPLAC - [SDR CALA9801903](https://openairdocs.org/sdr/CALA9801903.md): Beltframe · corroded · Oct 2, 1998 · N14814 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND BELTFRAME CORRODED AT STA 1322 BETWEEN LONGERON 29L AND 29R. THE CORROSION WAS REMOVED, FILLER AND DOUBLERS INSTALLED IAW SRM 53-03, FIGURE 2A. - [SDR CALA9801902](https://openairdocs.org/sdr/CALA9801902.md): Fitting · worn · Oct 1, 1998 · N14814 · Doug DC982 · Landing Gear Actuator > INSPECTION FOUND RT MLG RETRACT ACTUATOR UPPER ATTACH COKE BOTTLE FITTING WORN. A NEW COKE BOTTLE FITTING AND BUSHINGS WERE INSTALLED IAW MM 57-40-02. - [SDR CALA9801901](https://openairdocs.org/sdr/CALA9801901.md): Beltframe · corroded · Oct 1, 1998 · N14814 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND BELTFRAME WEB CORRODED AT STA 1338 BETWEEN LONGERONS 25 AND 26. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4. - [SDR CALA9801895](https://openairdocs.org/sdr/CALA9801895.md): Beam · cracked · Oct 1, 1998 · N14814 · Doug DC982 · Service Doors > INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. THE DOOR BEAM WAS REPLACED IAW WORK CARD 99-5240-1-0002. - [SDR CALA9801894](https://openairdocs.org/sdr/CALA9801894.md): Skin · cracked · Sep 30, 1998 · N14814 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.375 INCH CRACK IN FUSELAGE SKIN AT STA 1418, LONGERON 2R. REPAIRED IAW SRM 53-04, FIGURE 40. - [SDR CALA9801416](https://openairdocs.org/sdr/CALA9801416.md): B Nut · leaking · Aug 7, 1998 · N14814 · Doug DC982 · Hydraulic System, Main > THE RT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO 1.5 QUARTS ON CLIMB-OUT OF DCA EN ROUTE TO EWR. THE RIGHT PUMP AND AUX PUMP WERE TURNED OFF. THE GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED AT EWR WITH GEAR DOORS OPEN. THE RIGHT GEAR DOOR SUSTAINED - [SDR CALA9800100](https://openairdocs.org/sdr/CALA9800100.md): Wire · broken · Jan 24, 1998 · N14814 · Doug DC982 · Landing Gear System Wiring > THE NLG INDICATED RED UNSAFE WHEN GEAR WAS EXTENDED, BUT THE COCKPIT INDICATOR PIN SHOWED DOWN AND LOCKED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN WIRE ON NLG DOWNLOCK SENSOR. THE WIR - [SDR CALA9601910](https://openairdocs.org/sdr/CALA9601910.md): Fuel Contl Unit · malfunctioned · Dec 29, 1996 · N14814 · Doug DC982 · APU Engine Fuel and Control > THE APU AUTO SHUT DOWN INFLIGHT AND THE HIGH OIL TEMP LIGHT ILLUMINATED. ALSO, THE NR 2 FIRE BOTTLE LOW AGENT LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 FIRE BOTTLE APU SQUIB BLOWN. THE APU WAS PLACARDED INOPERAT - [SDR CALA9601574](https://openairdocs.org/sdr/CALA9601574.md): Threshold · corroded · Oct 17, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT AFT SERVICE DOOR THRESHOLD WEB AT AFT LOWER CORNER CORRODED. THE CORRODED WEB SECTION WAS REMOVED. A NEW WEB REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-03 AND 53-01, FIGURE 2. - [SDR CALA9601573](https://openairdocs.org/sdr/CALA9601573.md): Support · corroded · Oct 8, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 218 TO 238, LBL 14. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-18-1, FIGURE 11. - [SDR CALA9601572](https://openairdocs.org/sdr/CALA9601572.md): Support · corroded · Oct 8, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150 TO 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND 51-30-1. - [SDR CALA9601571](https://openairdocs.org/sdr/CALA9601571.md): Support · corroded · Oct 8, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150-200, LBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-14-1. - [SDR CALA9601570](https://openairdocs.org/sdr/CALA9601570.md): Support · corroded · Oct 8, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 160 TO 200, LBL 44. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND SRM 51-30-2. - [SDR CALA9601566](https://openairdocs.org/sdr/CALA9601566.md): Support · corroded · Oct 8, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200-204, LBL 56. THE FLOORBOARD SUPPORT WAS REMOVED AND A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. - [SDR CALA9601577](https://openairdocs.org/sdr/CALA9601577.md): Support · corroded · Oct 7, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT F.S. 1155, LBL 18 - 40. THE FLOOR SUPPORT WAS REMOVED AND A SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA9601576](https://openairdocs.org/sdr/CALA9601576.md): Support · corroded · Oct 7, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT FORWARD BULKHEAD OF MID CARGO COMPARTMENT, STA 541, STRINGER 29L TO 28L. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A REPLACEMENT FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-24-0, FIGURE 9A, SHEET - [SDR CALA9601575](https://openairdocs.org/sdr/CALA9601575.md): Brace · cracked · Oct 7, 1996 · N14814 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND A 1.5 INCH CRACK IN LT MLG DOOR CENTER BRACE. THE CENTER BRACE WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED AND THE BRACE WAS REINSTALLED IAW SRM 51-30-1. - [SDR CALA9601569](https://openairdocs.org/sdr/CALA9601569.md): Support · corroded · Oct 7, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 168 FROM RBL 10 TO RBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND SRM 51-10-2. - [SDR CALA9601568](https://openairdocs.org/sdr/CALA9601568.md): Support · corroded · Oct 7, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, RBL 10 TO RBL 44. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-3. - [SDR CALA9601567](https://openairdocs.org/sdr/CALA9601567.md): Support · corroded · Oct 7, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, LBL 7 TO RBL 5. THE CORRODED SECTION WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND SRM 51-30-2. - [SDR CALA9601578](https://openairdocs.org/sdr/CALA9601578.md): Support · corroded · Oct 6, 1996 · N14814 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 221, LBL 3. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-2. - [SDR CALA9601565](https://openairdocs.org/sdr/CALA9601565.md): Skin · cracked · Oct 5, 1996 · N14814 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1.5 INCH CRACK AND DENT IN FUSELAGE SKIN AT STA 258 JUST BELOW STRINGER 21R. THE DENT WAS REWORKED AND THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21, VIEW I. - [SDR CALA9601140](https://openairdocs.org/sdr/CALA9601140.md): Hyd Line · leaking · Aug 8, 1996 · N14814 · Doug DC982 · Hydraulic System, Main > THE RT HYDRAULIC SYSTEM QUANTITY BEGAN TO DECREASE DURING CLIMB. THE R/H HYDRAULIC QUANTITY CONTINUED TO DROP SLOWLY WHILE AT CRUISE. THE TRANSFER PUMP, RT HYDRAULIC PUMP AND AUX PUMP WERE TURNED OFF. THE PUMPS WERE RETURNED TO NORMAL ON APPROACH WITH THE R - [SDR CAL960059](https://openairdocs.org/sdr/CAL960059.md): Fire Det Module · inoperative · Jan 20, 1996 · N14814 · Doug DC982 · Fire Detection > FLT NR 421 - IAH - THE NR 1 ENGINE LOOP 'B' FIRE DETECTOR LIGHT AND MASTER CAUTION LIGHT ILLUMINATED DURING CLIMB-OUT AT 18,000 FEET. THE NR 1 ENGINE LOOP SWITCH WAS MOVED TO LOOP 'A' AND TEST WAS NORMAL. THE NR 1 ENGINE FIRE DETECTION MODULE WAS REMOVED AND - [SDR CAL950649](https://openairdocs.org/sdr/CAL950649.md): Fuel Pump · leaking · Aug 8, 1995 · N14814 · Doug DC982 · Engine Fuel Pump > DFW - FLT 0140 - THE NR 1 FUEL QUANTITY DECREASED FROM 6500 TO 1350 WITHIN 15 MINUTES WHILE ENROUTE FROM LAS TO IAH. THE CROSSFEED PROCEDURE WAS USED AND THE NR 2 FUEL QUANTITY DECREASED FASTER THAN FUEL QTY DISPLAYS COULD INDICATE. THE AIRCRAFT WAS DIVERTED ## 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 = 'N14814' AND deregistration_id = 'N14814-2002-10-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14814-2002-10-02/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.