# Service difficulty reports: N8920E, cancelled Nov 19, 2013 A list on [N8920E, cancelled Nov 19, 2013](https://openairdocs.org/deregistered/N8920E-2013-11-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR NWAA09539927](https://openairdocs.org/sdr/NWAA09539927.md): Battery Pack · inoperative · Feb 20, 2009 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, BOTH OF THE AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD. (K) - [SDR NWAA082509927](https://openairdocs.org/sdr/NWAA082509927.md): Ground Wire · loose · Jun 4, 2008 · N8920E · Doug DC931 · Light System Wiring > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY FLOOD LIGHT FOR THE AFT EVACUATION SLIDE WAS NOT FUNCTIONAL. A GROUNDING POINT AT L2-110 WAS FOUND TO BE LOOSE. RE-SECURED GROUND AND OPERATIONAL CHECK WAS GOOD. (A) - [SDR NWAA08249927](https://openairdocs.org/sdr/NWAA08249927.md): Structure · leaking · May 29, 2008 · N8920E · Doug DC931 · Fuselage Main, Structure > AT FL 310 RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. BOTH ENGINE AND AIRFOIL ICE PROTECTION SYSTEMS OPERATING. COM PROCEDURES TO REGAIN CONTROL OF CABIN PRESSURE COMPLETED BUT CABIN STILL CONTINUED TO CLIMB AT AN INCREASING RATE. DECLARED AN EMERGENCY AND - [SDR NWAA082459927](https://openairdocs.org/sdr/NWAA082459927.md): Warning Light · illuminated · May 29, 2008 · N8920E · Doug DC931 · Cabin Cooling System > AT FL310 THE RED CABIN PRESS WARNING LIGHT ILLUMINATED. BOTH ENGINE & AIRFOIL ICE PROTECTION SYS OPERATING. ATTEMPT TO REGAIN CONTROL OF CABIN PRESSURE COMPLIED WITH, CABIN CONTINUED CLIMB. DECLARED EMERG & INITIATED EMERG DESCENT. CABIN PRESS FOLLOWED CO - [SDR NWAA081909927](https://openairdocs.org/sdr/NWAA081909927.md): Battery · discharged · May 2, 2008 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE CHECK MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING IN THE FIRST SIX ROWS OF COACH SEATS IN THE CABIN HAD FAILED. MAINTENANCE REPLACED THE APPLICABLE BATTERIES FOR THE EPSU. OPERATIONAL CHECK WAS GOOD. - [SDR NWAA080579927](https://openairdocs.org/sdr/NWAA080579927.md): Battery Pack · inoperative · Feb 12, 2008 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE CATWALK EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AND ALSO REPLACED A DAMAGED WIRE HARNESS FROM THE FLOODLIGHTS TO THE CATWALK LIGHTS. OP - [SDR 0501659927](https://openairdocs.org/sdr/0501659927.md): Door · not seated · Nov 30, 2005 · N8920E · Doug DC931 · Fuselage Main, Bulkhead > IN CRUISE FLIGHT AT FL270 AN AIR LEAK AT THE AFT PRESSURE BULKHEAD DOOR WAS REPORTED. THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED AS THE CABIN ALTITUDE REACHED 10,500 FEET. THE MASKS DID NOT DEPLOY. THE RED BORDER CHECKLIST AND DESCENT TO 11,000 FEET WE - [SDR 0301809927](https://openairdocs.org/sdr/0301809927.md): Slide · malfunctioned · Sep 18, 2003 · N8920E · Doug DC931 · Escape Slide > PER MAINTENANCE CONTROL ORDER 4721, AN OPERATIONAL CHECK OF THE TAIL CONE DEPLOYMENT WAS PERFORMED. FOUND SLIDE PACK DEPLOY STRAP DID NOT SNAP ON THE SLIDE ASSEMBLY AS DESIGNED. SLIDE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. - [SDR 0104369927](https://openairdocs.org/sdr/0104369927.md): Fitting · cracked · Jun 11, 2001 · N8920E · Doug DC931 · Fuselage Main, Attach Fittings > During Hck at the ATL Maintenance. The LHS MLG door hinge fitting AFT lug was found cracked. Material 7075-t6511, repaired per EA 99-181272 - [SDR 0103259927](https://openairdocs.org/sdr/0103259927.md): Skin · damaged · Jun 5, 2001 · N8920E · Doug DC931 · Fuselage Main, Plate/Skin > DURING AN H-CHECK AT ATLANTA THE FUSELAGE BELLY SKIN AT STA 332 AND BL 0 WAS DISCOVERED TO HAVE HOLES FOR FASTENERS COMMON TO SKIN AND SHEAR CLIP HAVE BEEN ELONGATED. THE SHEAR CLIP IS REPLACED AND THE SKIN IS REPAIRED BY TRIMMING OUT THE DAMAGE AND REINFORCI - [SDR 0105039927](https://openairdocs.org/sdr/0105039927.md): Longeron · cracked · Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, Structure > During an Hck in ATL, the longeron 26r end fitting was found cracked at station 598. Repaired per EA 99-181209. - [SDR 0104489927](https://openairdocs.org/sdr/0104489927.md): Fitting · cracked · Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, Structure > During H ck in ATL the longeron 26r end fitting was found cracked at sta 598. Repaired per EA. 99-181209. - [SDR 0103269927](https://openairdocs.org/sdr/0103269927.md): Keelbeam · gouged · Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, Keel > DURING AN H-CHECK AT ATLANTA BASE A DEEP GOUGE WAS FOUND IN THE KEEL FORMER AT STATION 737 (RT) JUST BELOW THE BRAKE CONTROL VALVE. THE GOUGE WAS AT THE TOP OF THE FORMER. THE REPAIR TO FORMER WAS ACCOMPLISHED PER EA 99-181256 LOG PAGE 1617459. - [SDR 0004299927](https://openairdocs.org/sdr/0004299927.md): Power Supply · inoperative · Nov 3, 2000 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, FOUND THE EMERGENCY LIGHTS IN THE AFT CABIN OVERHEAD INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY PACK. OPERATIONAL CHECK NORMAL. - [SDR 0000549927](https://openairdocs.org/sdr/0000549927.md): Angle · cracked · Jan 22, 2000 · N8920E · Doug DC931 · Fuselage Main, Frame > CRACK IN UPPER FASTENER OF LEFT VERTICAL ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-172131. - [SDR 9902919927](https://openairdocs.org/sdr/9902919927.md): Line · leaking · Jul 21, 1999 · N8920E · Doug DC931 · Hydraulic System, Main > LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED DURING APPROACH INTO DTW. PRESSURE FLUCTUATED BETWEEN 2399 AND 3000 PSI. FLIGHT CREW SHUT DOWN PUMPS AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES TO EXTEND GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTEN - [SDR 9810359927](https://openairdocs.org/sdr/9810359927.md): Roller · out of adjust · Nov 8, 1998 · N8920E · Doug DC931 · Landing Gear Door Retract Section > RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT GEAR DOOR ROLLER OUT OF RIG. RIGGED DOOR ROLLER. OPERATIONAL CHECK - [SDR 9709119927](https://openairdocs.org/sdr/9709119927.md): Fuse · blown · May 6, 1997 · N8920E · Doug DC931 · Emergency Lighting > DURING PERIODIC CHECK, FOUND RIGHT SERVICE DOOR AND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FUSE, OPERATIONAL CHECK NORMAL. - [SDR 9708329927](https://openairdocs.org/sdr/9708329927.md): Transformer · shorted out · Apr 13, 1997 · N8920E · Doug DC931 · Passenger Compartment Lighting > FLIGHT ATTENDANT REPORTED, SMOKE IN AFT CABIN WHILE SITTING AT GATE, NO PASSENGERS WERE ON BOARD. MAINTENANCE FOUND TRANSFORMER T1-2 FOR AFT MISCELLANEOUS CABIN AND LAVATORY OCCUPIED LIGHTS SHORTED OUT. REPLACED TRANSFORMER, OPERATIONAL CHECK NORMAL. - [SDR 9703979927](https://openairdocs.org/sdr/9703979927.md): Power Supply · inoperative · Feb 23, 1997 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND LEFT WING SCAN EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. - [SDR 9700879927](https://openairdocs.org/sdr/9700879927.md): Retract Mech · malfunctioned · Jan 18, 1997 · N8920E · Doug DC931 · Landing Gear Retraction/Extension System > AFTER DEPARTURE, THE LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE. GEAR EXTENDED AND FLIGHT RETURNED TO ATL FOR NORMAL LANDING. MAINTENANCE REPLACED THE LEFT UP AND DOWN LOCK SWITCHES, LEFT GEAR RETRACT ACTUATOR, - [SDR 9700889927](https://openairdocs.org/sdr/9700889927.md): Connector · failed · Jan 17, 1997 · N8920E · Doug DC931 · Landing Gear Position and Warning > AFTER TAKEOFF, THE LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE, RECYCLED GEAR. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. FOUND DOOR SWITCH CANNON PLUG BAD AND BROKEN WIRE TO UPLATCH SWITCH. REPLACED CA - [SDR 9701059927](https://openairdocs.org/sdr/9701059927.md): Evac Slide · low battery · Jan 15, 1997 · N8920E · Doug DC931 · Escape Slide > DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. - [SDR 9700659927](https://openairdocs.org/sdr/9700659927.md): Slide · low battery · Jan 14, 1997 · N8920E · Doug DC931 · Escape Slide > DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE BATTERY FAILED TEST. REPLACED SLIDE. - [SDR 9700309927](https://openairdocs.org/sdr/9700309927.md): Battery Pack · discharged · Jan 6, 1997 · N8920E · Doug DC931 · Emergency Lighting > DURING PERIODIC CHECK, EXTERIOR EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9625449927](https://openairdocs.org/sdr/9625449927.md): Batteries · discharged · Nov 25, 1996 · N8920E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9624679927](https://openairdocs.org/sdr/9624679927.md): Battery · discharged · Nov 14, 1996 · N8920E · Doug DC931 · Emergency Lighting > DURING FLIGHT, FOUND THAT THE RIGHT SIDE FLOOR EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FLASHING. REPLACED THE BATTERIES AND POWER SUPPLY AT THE AFT RIGHT EMERGENCY EXIT SIGN, CHECKED OK. - [SDR 9615809927](https://openairdocs.org/sdr/9615809927.md): Fuel Press Sw · failed · Jun 26, 1996 · N8920E · Doug DC931 · Fuel Pressure Indicating > WHILE APPLYING TAKEOFF POWER, THE LEFT ENGINE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AND FUEL DIFFERENTIAL PRESSURE SWITCH. RAN ENGINE TO TAKEOFF POWE - [SDR 9609729927](https://openairdocs.org/sdr/9609729927.md): Pressurization · malfunctioned · May 7, 1996 · N8920E · Doug DC931 · Cabin Pressure Control System > LOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET, CABIN PRESSURE WARNING LIGHT ILLUMINATED AND OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN. EMERGENCY DESCENT WAS MADE TO 24,000 FEET AND PRESSURE WAS REGAINED, DESCENDED TO 18,000 FEET AND CONTINUED TO - [SDR 9605949927](https://openairdocs.org/sdr/9605949927.md): Frame · worn · Mar 6, 1996 · N8920E · Doug DC931 · Fuselage Main, Frame > DURING LINE MAINTENANCE INSPECTION, FOUND FUSELAGE FRAMES WORN AT UPPER AND LOWER RIGHT AND LEFT TAIL CONE LATCH BAYONET HOLES. REPAIRED PER EA 99-109443 AND REPLACED LOWER FRAME SECTIONS. - [SDR 9520579927](https://openairdocs.org/sdr/9520579927.md): Hyd Shutoff Vlv · failed · Dec 17, 1995 · N8920E · Doug DC931 · Hydraulic System, Main > DURING APPROACH, THE AIRCRAFT LOST HYDRAULIC QUANTITY AND PRESSURE. ALSO, THE LANDING GEAR WOULD NOT EXTEND USING ALTERNATE HYDRAULIC PUMP. EXTENDED LANDING GEAR USING EMERGENCY EXTENSION LEVER. FOUND HYDRAULIC SOLENOID SHUTOFF VALVE DAMAGED. REPLACED THE - [SDR 9518719927](https://openairdocs.org/sdr/9518719927.md): Retract Cables · misrouted · Nov 15, 1995 · N8920E · Doug DC931 · Leading Edge Slat Control System > DURING APPROACH, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND AIRCRAFT CONTINUED TO GRR LANDING WITHOUT INCIDENT. FOUND RIGHT WING RETRACT CABLES MISROUTED A - [SDR 9515929927](https://openairdocs.org/sdr/9515929927.md): Rt Unit · malfunctioned · Oct 14, 1995 · N8920E · Doug DC931 · Weather Radar System > DURING CRUISE, RADAR WOULD NOT PAINT GROUND AND INDICATOR, ONLY SHOWED SOLID RED ARC OF 20 MILE RADIUS. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR RECEIVER TRANSMITTER AND OPERATIONAL CHECK GOOD. - [SDR 9505539927](https://openairdocs.org/sdr/9505539927.md): Release Mech · out of adjust · Apr 5, 1995 · N8920E · Doug DC931 · Aerodynamic Fairings > DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE, CHECKED OK. - [SDR 9503679927](https://openairdocs.org/sdr/9503679927.md): Door Mechanism · worn · Mar 8, 1995 · N8920E · Doug DC931 · Emergency Exits > DURING PERIODIC CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO LATCH THE FORWARD RIGHT OVERWING EMERGENCY EXIT HANDLE. REPLACED THE DOOR, CHECKED OK. - [SDR 9504079927](https://openairdocs.org/sdr/9504079927.md): Frame · cracked · Mar 7, 1995 · N8920E · Doug DC931 · Fuselage Main, Frame > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FS 756 BELTFRAME AT LONGERON 10L. REPAIRED PER XEA X9-53-47. - [SDR 9504069927](https://openairdocs.org/sdr/9504069927.md): Hinge · cracked · Mar 7, 1995 · N8920E · Doug DC931 · Spoilers > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN RIGHT OUTBOARD FLIGHT SPOILER INNER HINGE. REPLACED HINGE PER SRM 51-30-1. - [SDR 9501459927](https://openairdocs.org/sdr/9501459927.md): Floor Beam · corroded · Jan 19, 1995 · N8920E · Doug DC931 · Fuselage Main, Floor Beam > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN FLOOR BEAM FS 965, RBL 19-25. REPAIRED PER XEA X9-53-99. - [SDR 9501449927](https://openairdocs.org/sdr/9501449927.md): Fitting · cracked · Jan 18, 1995 · N8920E · Doug DC931 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN BELT FRAME ATTACH FITTING FS 658 ABOVE LONGERON 29L. REPLACED FITTING PER SRM 51-30-2. - [SDR 9501439927](https://openairdocs.org/sdr/9501439927.md): Fitting · cracked · Jan 18, 1995 · N8920E · Doug DC931 · Cargo/Baggage Doors > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN AFT CARGO DOOR FRAME END FITTING UPPER FORWARD CORNER. REPLACED FITTING PER SRM 51-30-5. - [SDR 9502459927](https://openairdocs.org/sdr/9502459927.md): Hinge · corroded · Jan 13, 1995 · N8920E · Doug DC931 · Trailing Edge Flaps > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN NR 3 FORWARD FLAP HINGE FASTENER BORES WS 251. REPAIRED PER XEA X9-27-11. - [SDR 9500849927](https://openairdocs.org/sdr/9500849927.md): Chord · corroded · Jan 12, 1995 · N8920E · Doug DC931 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION IN FS 110 LOWER CHORD ANGLE, NOSE WHEEL WELL RIGHT TUNNEL. REPAIRED PER EA X9-53-51. - [SDR 9500779927](https://openairdocs.org/sdr/9500779927.md): Frame · cracked · Jan 11, 1995 · N8920E · Doug DC931 · Fuselage Main, Frame > DURING PERIODIC CHECK, FOUND 12 INCH CRACK IN THE FS 1132 FRAME AT LONGERONS 17L - 19L. REPLACED LOWER FRAME PER DWG 9911877 AND SRM 51-30-2. - [SDR 9500519927](https://openairdocs.org/sdr/9500519927.md): Fitting · cracked · Jan 10, 1995 · N8920E · Doug DC931 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND RADIUS CRACK IN BELT FRAME ATTACH FITTING FS 676 ABOVE LONGERON 29L. REPLACED FITTING PER SRM 51-30-2. - [SDR 9500489927](https://openairdocs.org/sdr/9500489927.md): Spar Chord · cracked · Jan 7, 1995 · N8920E · Doug DC931 · Horizontal Stabilizer, Spar/Rib > DURING PERIODIC CHECK, FOUND CRACKS IN THE LEFT HORIZONTAL STABILIZER AFT SPAR UPPER 'T' CAP BETWEEN NR3 - NR4 HINGES AND LOWER 'T' CAP (OUTBOARD END). REPAIRED BOTH PER SRM 55-02. ## 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 = 'N8920E' AND deregistration_id = 'N8920E-2013-11-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8920E-2013-11-19/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.