# Service difficulty reports: N13881, cancelled Mar 21, 2013 A list on [N13881, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N13881-2013-03-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0100625](https://openairdocs.org/sdr/CALA0100625.md): Battery Pack · discharged · Jul 1, 2001 · N13881 · Doug DC981 · Emergency Lighting > INSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES IN OVERHEAD BATTERY PACK WERE REPLACED IAW MM 33-50-00 AND OPERATION CHECKED GOOD. - [SDR CALA0100102](https://openairdocs.org/sdr/CALA0100102.md): Battery Pack · inoperative · Feb 4, 2001 · N13881 · Doug DC981 · Emergency Lighting > INSPECTION FOUND EIGHT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACKS AT STA 427R AND 570R WERE REMOVED AND REPLACED IAW SRM 33-53-00. - [SDR CALA0001889](https://openairdocs.org/sdr/CALA0001889.md): Line · broken · Dec 12, 2000 · N13881 · Doug DC981 · Air Intake Anti/De-Ice System > THE FIRE DETECTOR LOOP AND MASTER CAUTION ILLUMINATED AND NR 1 ENGINE FIRE INDICATION CAME ON DURING CLIMB OUT OF BOS. QRH PROCEDURES WERE FOLLOWED AND ALL LIGHTS WENT OUT. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO - [SDR CALA0001000](https://openairdocs.org/sdr/CALA0001000.md): Skin · cracked · Jun 30, 2000 · N13881 · Doug DC981 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND A 1.8 INCH CRACK IN VERTICAL STABILIZER SKIN AT BASE OF STABILIZER, STA 1437, LT SIDE. A 4 INCH CRACK WAS FOUND IN VERTICAL STABILIZER SKIN AT BASE OF STABILIZER, STA 1437, RT SIDE. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5340 - [SDR CALA0000996](https://openairdocs.org/sdr/CALA0000996.md): Slide · will not test · Jun 29, 2000 · N13881 · Doug DC981 · Escape Slide > THE AFT TAILCONE SLIDE FAILED EMERGENCY SLIDE LIGHTS FUNCTIONAL TEST. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-00. - [SDR CALA0000995](https://openairdocs.org/sdr/CALA0000995.md): Skin · cracked · Jun 28, 2000 · N13881 · Doug DC981 · Fuselage Main, Plate/Skin > INSPECTION FOUND TWO 1 INCH CRACKS IN LT FUSELAGE EXTERIOR SKIN AT STA 1437 BETWEEN LONGERONS 3L AND 4L. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02973. - [SDR CALA0000994](https://openairdocs.org/sdr/CALA0000994.md): Floorbeam · corroded · Jun 28, 2000 · N13881 · Doug DC981 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM WEB AND FITTINGS CORRODED IN E/E COMPARTMENT AT LT SIDE, STA 160. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5310-04025. - [SDR CALA0000993](https://openairdocs.org/sdr/CALA0000993.md): Skin · cracked · Jun 28, 2000 · N13881 · Doug DC981 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1 INCH CRACK IN RT FUSELAGE EXTERIOR SKIN AT STA 1437 BETWEEN LONGERON 3R AND 4R. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02972. - [SDR CALA0000955](https://openairdocs.org/sdr/CALA0000955.md): Longeron · corroded · Jun 21, 2000 · N13881 · Doug DC981 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 22R CORRODED IN FORWARD BAGGAGE BIN AT STA 228. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18. - [SDR CALA0000954](https://openairdocs.org/sdr/CALA0000954.md): Shear Tie · cracked · Jun 21, 2000 · N13881 · Doug DC981 · Fuselage Main, Structure > INSPECTION FOUND A.5 INCH CRACK IN SKIN CLIP AT LT LAV WALL, STA 1309 BETWEEN LONGERONS 13L AND 14L. THE SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000943](https://openairdocs.org/sdr/CALA0000943.md): Shear Tie · cracked · Jun 20, 2000 · N13881 · Doug DC981 · Fuselage Main, Structure > INSPECTION FOUND A 1.5 INCH CRACK IN FRAME TO FUSELAGE SKIN CLIP AT STA 1307 BETWEEN STRINGER 15R AND 16R. A NEW SKIN CLIP WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0000941](https://openairdocs.org/sdr/CALA0000941.md): Skin · dented · Jun 20, 2000 · N13881 · Doug DC981 · Cargo/Baggage Doors > INSPECTION FOUND THE AFT CARGO DOOR EXTERNAL SKIN DENTED APPROXIMATELY 16 INCHES FROM AFT EDGE OF DOOR BETWEEN NR 1 AND 2 BEAMS. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 2. - [SDR CALA0000926](https://openairdocs.org/sdr/CALA0000926.md): Splice · cracked · Jun 19, 2000 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 3 INCH CRACK IN LONGERON 4L SPLICE AT STA 1193 - 1212. REPLACED WITH FABRICATED SPLICE IAW SRM 51-30-0. - [SDR CALA0000925](https://openairdocs.org/sdr/CALA0000925.md): Seat Track · corroded · Jun 19, 2000 · N13881 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AROUND FASTENER HOLES AT STA 1150 - 1174. THE CORRODED SECTION OF TRACK WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F. - [SDR CALA0000924](https://openairdocs.org/sdr/CALA0000924.md): Shear Tie · cracked · Jun 19, 2000 · N13881 · Doug DC981 · Fuselage Main, Structure > INSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE SKIN CLIP AT STA 1307 BETWEEN STRINGER 15L AND 16L. THE SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000912](https://openairdocs.org/sdr/CALA0000912.md): Splice · cracked · Jun 16, 2000 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND THREE.5 INCH CRACKS IN LONGERON SPLICE AT STA 1098 - 1117, LONGERON 1L TO 3L AND TWO.5 INCH CRACKS WERE FOUND IN LONGERON SPLICE AT STA 1193-1212, L1L. THE SPLICES WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0000899](https://openairdocs.org/sdr/CALA0000899.md): Seat Track · corroded · Jun 13, 2000 · N13881 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 229. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000340](https://openairdocs.org/sdr/CALA0000340.md): Light · inoperative · Mar 23, 2000 · N13881 · Doug DC981 · Emergency Lighting > INSPECTION FOUND THE L-1 DOOR EMERGENCY PORTABLE LIGHT ASSEMBLY INOPERATIVE. THE EMERGENCY PORTABLE LIGHT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9901439](https://openairdocs.org/sdr/CALA9901439.md): Strut · reqd service · Oct 31, 1999 · N13881 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. QRH PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT AT 100 PSI. THE STRUT WAS SERVICED IAW MM 32-21-02. THE GE - [SDR CALA9900940](https://openairdocs.org/sdr/CALA9900940.md): Uplock · broken · Aug 3, 1999 · N13881 · Doug DC981 · Landing Gear Retraction/Extension System > THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING EWR. THE LANDING GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO BOS WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND A BROKEN SPRING ON UPLOCK AND DOOR LATCH MECHANISM - [SDR CALA9802169](https://openairdocs.org/sdr/CALA9802169.md): Target · loose · Dec 10, 1998 · N13881 · Doug DC981 · Landing Gear Position and Warning > THE GEAR DOOR OPEN LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. WHEN THE GEAR WAS EXTENDED FOR LANDING, THE GEAR DOOR OPEN LIGHT REMAINED ON. THE GEAR WAS CYCLED AND THE LIGHT WENT OUT. MAINTENANCE FOUND THE DOOR PROXIMITY SWITCH TARGET DAMAGED/LOOSE. TH - [SDR CALA9801689](https://openairdocs.org/sdr/CALA9801689.md): Spring · broken · Sep 10, 1998 · N13881 · Doug DC981 · Landing Gear Retraction/Extension System > A LOUD SNAP SOUND WAS HEARD COMING FROM NOSE GEAR AREA WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. ALL THREE GREEN GEAR LIGHTS CAME ON AND THE GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. THE AIRCRAFT LANDED SAFELY WITH GEAR WORKING NORMALLY AND THE AIRCRAFT TAXIIE - [SDR CALA9801150](https://openairdocs.org/sdr/CALA9801150.md): Circuit Breaker · failed · Jun 23, 1998 · N13881 · Doug DC981 · Buffet/Galleys > A BURNING ELECTRICAL SMELL WAS DETECTED AT THE FORWARD FLIGHT ATTENDANT PANEL WHILE ON FINAL APPROACH. THERE WAS NO VISIBLE SMOKE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE CIRCUIT BREAKER PANELS IN COCKPIT BEHIND JUMPSEAT AND THE E AND E COMPARTMENT - [SDR CALA9800998](https://openairdocs.org/sdr/CALA9800998.md): Angle · corroded · Jun 9, 1998 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED. REPAIRED IAW SRM 53-05, FIGURE 63. - [SDR CALA9800046](https://openairdocs.org/sdr/CALA9800046.md): Turbine · failed · Jan 14, 1998 · N13881 · Doug DC981 · APU Core Engine > THE APU WAS STARTED AFTER LANDING IN EWR AND RAN NORMALLY FOR A WHILE AND THEN FLAMED OUT. THE APU WOULD NOT RESTART. MAINTENANCE FOUND AN UNCONTAINED TURBINE WHEEL SEPARATION. THE SHROUD DID NOT CONTAIN THE TURBINE WHEEL WHICH CAUSED DAMAGE TO THE APU FIREW - [SDR CALA9701381](https://openairdocs.org/sdr/CALA9701381.md): Fire Det Mod · inoperative · Sep 18, 1997 · N13881 · Doug DC981 · Fire Detection > THE AIRCRAFT HAD A HISTORY OF THE NR 1 ENGINE A-LOOP FIRE WARNING LIGHT ILLUMINATING IN FLIGHT. TWO A-LOOP CONNECTORS: P1-826 AND P1-827 WERE REPLACED. THE NR 1 ENGINE FIRE DETECTION MODULE WAS REMOVED AND REPLACED IAW MM 26-10-03. AN OPERATIONAL CHECK OF T - [SDR CALA9701299](https://openairdocs.org/sdr/CALA9701299.md): Strut · inoperative · Sep 2, 1997 · N13881 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM BOS. RECYLING PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WENT INTO GROUND MODE. THE GEAR REMAINED EXTENDED AND THE AIRCRAFT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG O - [SDR CALA9701255](https://openairdocs.org/sdr/CALA9701255.md): Bearing · failed · Aug 30, 1997 · N13881 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > A LOUD GRINDING NOISE CAME FROM THE NOSE WHEEL AREA UPON TOUCHDOWN ON LANDING AT BOS. MAINTENANCE FOUND THE LT NOSE WHEEL INNER BEARING HAD FAILED AND DAMAGED THE AXLE. THE LT AND RT NOSE WHEELS WERE REMOVED AND REPLACED. IN ADDITION, THE NOSE GEAR PISTON S - [SDR CALA9701162](https://openairdocs.org/sdr/CALA9701162.md): Hyd Line · ruptured · Aug 3, 1997 · N13881 · Doug DC981 · Hydraulic System, Main > THE RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO AFTER SELECTING FLAPS TO 15 DEGREES ON APPROACH. THE CHECKLIST PROCEDURES FOR LANDING WITH THE RIGHT HYDRAULIC SYSTEM INOPERATIVE WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINT - [SDR CALA9700861](https://openairdocs.org/sdr/CALA9700861.md): Bulb · failed · Jun 11, 1997 · N13881 · Doug DC981 · Landing Gear Position and Warning > WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH, THE GREEN LANDING GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE. THE CREW RELAMPED THE INDICATOR LIGHT DURING A GO-AROUND AND THE INDICATION WAS GOOD. MAINTENANCE FOUND BULB ON LEFT GREEN LANDING GEAR DOWN INDI - [SDR CALA9700631](https://openairdocs.org/sdr/CALA9700631.md): Defuel Valve · open · Apr 29, 1997 · N13881 · Doug DC981 · Fuel Storage > DURING CLIMB, CREW NOTICE FUEL LEAKING FROM RT WING. ALSO, HIGH FUEL USEAGE FROM RT ENGINE. AIRCRAFT THEN CAME OUT OF TRIM. RETURN TO EWR AND MAINTENANCE FOUND DEFUEL VALVE IN OPEN POSITION AS WELL AS FUELING PANEL DOOR. CYCLE FUEL VALVE AND OPS CHECK GOOD - [SDR CALA9700607](https://openairdocs.org/sdr/CALA9700607.md): Power Supply · inoperative · Apr 22, 1997 · N13881 · Doug DC981 · Emergency Lighting > EXTERIOR EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY. - [SDR CALA9700478](https://openairdocs.org/sdr/CALA9700478.md): Engine · failed · Apr 3, 1997 · N13881 · Doug DC981 · Engine (Turbine/Turboprop) > THE NR 1 ENGINE EPR WENT TO ZERO ACCOMPANIED BY A LOUD BANG AT 5,000 FEET WITH CLIMB POWER LEAVING EWR. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK AND O - [SDR CALA9601016](https://openairdocs.org/sdr/CALA9601016.md): Trans Rect · inoperative · Jul 14, 1996 · N13881 · Doug DC981 · DC Rectifier/Converter > AN ELECTRICAL ODOR WAS MOMENTARILY OBSERVED IN THE FORWARD GALLEY WHILE IN FLIGHT. UPON INVESTIGATION THE RIGHT DC TRANSFER RELAY WAS FOUND TRIPPED AND THE RIGHT DC LOAD METER READ ZERO. THE TRANSFER CIRCUIT BREAKER WAS NOT RESET AND THE ODOR WENT AWAY. THE - [SDR CALA9600829](https://openairdocs.org/sdr/CALA9600829.md): Intercostal · cracked · Jun 9, 1996 · N13881 · Doug DC981 · Passenger/Crew Doors > INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL. THE CRACK WAS LOCATED AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA9600830](https://openairdocs.org/sdr/CALA9600830.md): Frame · cracked · Jun 5, 1996 · N13881 · Doug DC981 · Fuselage Main, Frame > INSPECTION FOUND A 6 INCH CRACK IN CANTED BELT FRAME AT STA 1463, LONGERON 2L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01. - [SDR CALA9600837](https://openairdocs.org/sdr/CALA9600837.md): Floor Support · corroded · May 31, 1996 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT AT STA 718 CORRODED AROUND NUTPLATE. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2. - [SDR CALA9600836](https://openairdocs.org/sdr/CALA9600836.md): Floor Support · corroded · May 31, 1996 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY BETWEEN PANELS G AND H, STA 148 TO 200. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA9600835](https://openairdocs.org/sdr/CALA9600835.md): Angle · cracked · May 31, 1996 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF EXTERNAL ANGLE AT STA 984 TO 1003, LONGERON 20L. THE AREA WAS REPAIRED IAW ECRA 5310-03277 AND SRM 53-02. - [SDR CALA9600833](https://openairdocs.org/sdr/CALA9600833.md): Flr Support · corroded · May 31, 1996 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY PANEL F. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9600834](https://openairdocs.org/sdr/CALA9600834.md): Door Pan · dented · May 30, 1996 · N13881 · Doug DC981 · Service Doors > INSPECTION FOUND FORWARD SERVICE DOOR PAN DENTED AT BAYONET FITTING. A DOUBLER WAS FABRICATED AND INSTALLED AND DOOR STOP WAS REPLACED IAW SRM 53-05, FIGURE 42. - [SDR CALA9600831](https://openairdocs.org/sdr/CALA9600831.md): Support · cracked · May 30, 1996 · N13881 · Doug DC981 · Spoilers > INSPECTION FOUND A 1 INCH CRACK AT FORWARD ATTACH FASTENER OF RT GROUND SPOILER O/B CROSS BRACE SUPPORT. A CROSS BRACE WAS INSTALLED IAW ECRA 5710-01733. - [SDR CALA9600832](https://openairdocs.org/sdr/CALA9600832.md): Doubler · cracked · May 28, 1996 · N13881 · Doug DC981 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.1875 INCH CRACK IN DOUBLER AT NOSE WHEEL WELL LEFT AFT DOOR AFT HINGE CUTOUT, STA 100. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 62. - [SDR CAL960001](https://openairdocs.org/sdr/CAL960001.md): Duct · loose · Jan 1, 1996 · N13881 · Doug DC981 · Cabin Cooling System > FLT 1875 - THE CABIN PRESS BEGAN TO CLIMB SLOWLY WHILE AT CRUISE ALT FL 310 AND WAS ACCOMPANIED BY FLOW LIGHT COMING ON, WHILE EN ROUTE. SYS WAS SWITCHED TO STANDBY W/O REMEDY. WHILE DESCENDING TO 10,000 FT THE CABIN RATE OF CLIMB INCREASED AND THE 02 MASKS - [SDR CAL950937](https://openairdocs.org/sdr/CAL950937.md): Hyd Line · leaking · Oct 18, 1995 · N13881 · Doug DC981 · Hydraulic System, Main > FLT NR 0378 - BOS - THE RIGHT HYDRAULIC QUANTITY BEGAN TO DROP RAPAIDLY WHILE CLIMBING THROUGH 1700 FEET LEAVING EWR, BOUND FOR BOS. THE FLIGHT MANUAL PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS EXTENDED MANUALLY FOR AN UNEVENTFUL LANDING AT BOS. MAINT - [SDR CALA950591](https://openairdocs.org/sdr/CALA950591.md): Engine · failed · Jul 12, 1995 · N13881 · Doug DC981 · Engine (Turbine/Turboprop) > MCO - FLT 0554 - THE NR 2 ENGINE FAILED WITH A LOUD POP AND FLAME SEEN IN THE EXHAUST DURING TAKEOFF ROLL AT 60 KNOTS. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. THE SDR WILL REMAIN OP - [SDR CAL950591](https://openairdocs.org/sdr/CAL950591.md): Stator Support · failed · Jul 12, 1995 · N13881 · Doug DC981 · Compressor Bleed Control > FLT NR 0554 - MCO - THE NR 2 ENGNIE FAILED WITH A LOUD POP AND FLAME SEEN IN THE EXHAUST DURING TAKEOFF ROLL AT 60 KNOTS. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. TEARDOWN REVEALED - [SDR CAL950516](https://openairdocs.org/sdr/CAL950516.md): Eel Wiring · broken · Jun 22, 1995 · N13881 · Doug DC981 · Emergency Lighting > FLT NR 0323 - EWR - INSPECTION FOUND SEVERAL SECTIONS OF EMERGENCY AISLE PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING AT SEVERAL LOCATIONS. THE WIRING WAS SPLICED AND A NEW HARNESS WAS INSTALLED AT REAR ENTRY DOOR. OPERATION OF THE AISLE PATH LI - [SDR CAL950076](https://openairdocs.org/sdr/CAL950076.md): Eel Batteries · discharged · Jan 29, 1995 · N13881 · Doug DC981 · Emergency Lighting > FLT NR 0327 - EWR - THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS SECTION OF CABIN WOULD NOT ILLUMINATE WHEN TESTED DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. ( ## 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 = 'N13881' AND deregistration_id = 'N13881-2013-03-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N13881-2013-03-21/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.