N945N, cancelled Aug 17, 2010

Service difficulty reports · 52

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N945N' AND deregistration_id = 'N945N-2010-08-17'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA1015699922Frame · damagedDURING GROUND OPERATIONS FORWARD NOSE LANDING GEAR FRAME DAMAGED AT BS 39 RBL 0 TO LBL 10.5. REPAIRED PER ERA 483286-14.Jul 2, 2010 · N945N · Doug DC932 · Fuselage Main, FrameSDR DALA1012339922Battery Pack · inoperativeDURING LINE CHECK MX FOUND CEILING EMERGENCY SIGNS AT ROW 12 AND 14 INOP. MX REPLACED BATTERY PACKS FOR POWER SUPPLY UNITS AT B5-33 AND B5-25. OPS CHECK OF LIGHTS NOW CHECK GOOD.Jun 4, 2010 · N945N · Doug DC932 · Emergency LightingSDR NWAA092909922Power Supply · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE LEFT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.Aug 12, 2009 · N945N · Doug DC932 · Emergency LightingSDR NWAA092479922Battery · misinstalledDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE GALLEY AND THE EXIT DOOR LIGHT WILL NOT ILLUMINATE. MAINTENANCE INSTALLED THE BATTERIES INTO THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jul 9, 2009 · N945N · Doug DC932 · Emergency LightingSDR NWAA082816743Hose · disconnectedFLT WAS PASSING THROUGH FL 280 WHEN THE RED "CABIN PRESS" LIGHT AND YELLOW "MASTER CAUTION" LIGHT BOTH ILLUMINATED. CREW SAW CABIN PRESSURIZATION WAS AT 10,500 FT AND CLIMBING. COM PROCEDURES WERE APPLIED BUT CABIN PRESSURE WAS NOT CONTROLLABLE. COCKPIT CREWJun 18, 2008 · N945N · Doug DC932 · Air Distribution SystemSDR 0601819922Unknown · malfunctionedAS THE AIRCRAFT WAS DESCENDING FROM FL250, CREW NOTICED RED -CABIN PRESS- LIGHT ILLUMINATED. CABIN VERTICAL AIRSPEED WAS CLIMBING IN EXCESS OF 1500 FPM BUT AN IMMEDIATE DESCENT TO 10,000 FT, SMOOTHLY PERFORMED BY F/O; ENABLED CREW TO KEEP CABIN AT NO HIGHER TAug 10, 2006 · N945N · Doug DC932 · Cabin Pressure Control SystemSDR 0201169922Acm · damagedCREW WAS UNABLE TO COOL THE CABIN DOWN WITH AIR CONDITIONING PRIOR TO DEPARTURE. THEN, DURING CLIMBOUT, CABIN DISPLAYED NONSTANDARD CLIMB PROFILE. VERY SLOW CLIMB TO ABOUT 17,000 FEET AND AS MAX DIFFERENTIAL WAS OBTAINED CABIN CONTINUED TO CLIMB AT 1000 FPM.Apr 15, 2002 · N945N · Doug DC932 · Cabin Cooling SystemSDR 0104979922Pan · crackedDuring M-ck in ATL, a crack was found at station 937 between longerons 26R and 27R. The crack was between marked holes "c" and "d" on the doorjamb pan. EA 99-181313Jul 27, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0104549922Spar · corrodedDuring an Mck in ATL, Corrosion was found in the left and right upper beaver tails. The Beaver tails were removed to accomplish corrosion removal. After the beaver tail removal it was noted that 11 fasteners common to the pylon spar were elongated. Repaired peJul 27, 2001 · N945N · Doug DC932 · Nacelle/Pylon, Main FrameSDR 0104529922Pan · crackedDuring Mck in ATL, A crack was found between 2 fasteners in the aft cargo doorjamb pan at sta 937, between longerons 26r and 27r. Material .050" 2024-t42 AL, and .090"2024-t42 AL. Repaired per EA 99-181313.Jul 27, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0103199922Skin · damagedDURING AN M-CHECK IN ATL, CORROSION WAS FOUND IN THE LEFT AND RIGHT UPPER BEAVER TAILS, P/N 5923937-501/502. THE BEAVER TAILS WERE REMOVED TO ACCOMPLISH CORROSION REMOVAL. AFTER THE BEAVER TAIL REMOVAL, IT WAS NOTED THAT 11 FASTENER HOLES COMMON TO THE PYLONJul 27, 2001 · N945N · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR 0104989922Skin · crackedDuring MCK in ATL, a 1/4" long crack was found in the fuselage skin at staion 1019, between longerons 14L and 15L. The crack emanated from one fastener hole common to the upper attach angle and was removed using 1" diameter cut out. This EA provides instructioJul 24, 2001 · N945N · Doug DC932 · Fuselage Main, Plate/SkinSDR 0104539922Skin · crackedDuring Mck in ATL a .25" crack was found in the fuselage skin at sta 1019, between longerons 14L and 15L. The crack emanated from one fastener hole common to the pylon upper attach angle and was removed using a 1" diameter cut out. Material .032 TI-6AI-4v. RepJul 24, 2001 · N945N · Doug DC932 · Fuselage Main, Plate/SkinSDR 0104999922Door Frame · crackedDuring an MCK in ATL, a .8" crack was found while accomplishing inspection of the lower aft corner of the forward cargo door doorjamb. This EA. 99-181281 provides repair of area. Material .050" 2014-t6 and .090" 2014-t6.Jul 19, 2001 · N945N · Doug DC932 · Fuselage Main, Plate/SkinSDR 0104569922Door Frame · crackedDURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-181281.Jul 19, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0104479922Door Frame · crackedDURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-181281.Jul 19, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0103139922Spar · damagedDURING AN M-CHECK SHOP VISIT AT ATL MAINTENANCE BASE WHILE REMOVING THE FRONT SPAR FOR REPLACEMENT, SEVERAL FASTENER HOLES ON THE UPPER AND LOWER SKIN ASSEMBLY WERE FOUND TO BE DAMAGED (TOOLING DAMAGE). REPAIR TO DAMAGED SKIN ASSEMBLY WAS ACCOMPLISHED PER SECJul 18, 2001 · N945N · Doug DC932 · Elevator, Spar/RibSDR 0103129922Door Frame · damagedDURING M-CHECK AT ATL AND WHILE ACCOMPLISHING A DOORJAMB PAN SPLICE REPAIR PER SRM 53-05, FIG 44, EIGHT .1875 INCH DIA HOLES WERE FOUND WITH SHORT ON-CENTER DISTANCE IN THE VERTICAL FLANGE OF FRAME STA 896 P/N 9958214-29 AS SHOWN IN FIGURE 1. THE FASTENER HOLJul 16, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0104969922Spar · corrodedDuring Mck in ATL, corrosion was found in the left and right beaver tails. The beaver tails were removed to accomplish corrosion removal. After the beaver tail removal, it was noted that 11 fastener holes common to the pylon front spar were elongated on each sJul 12, 2001 · N945N · Doug DC932 · Wing Miscellaneous StructureSDR 0103119922Frame · damagedDURING AN M1-CHECK IN ATL, STATION 579 FRAME REINFORCEMENT STRAPS 2800206-8 AND -9 WERE CUT FOR ACCESS AT LOCATION BETWEEN L-28 LT AND L-29 RT. ADDITIONAL DAMAGE WAS FOUND AT L-24 RT ON STRAP 2800206-8. THE EA 99-181344 (LOG PAGE 1640709) PROVIDES A SPLICE RJul 12, 2001 · N945N · Doug DC932 · Fuselage Main, FrameSDR 0105019922Intercostal · crackedDuring MCK in ATL, a crack was found in the outboard end of intercostal 9923484-9 at sta 180 and at X=-20. Repaired per EA 99-1813231.Jul 9, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0104449922Intercostal · crackedDuring M ck in ATL, A crack was found in the outboard end of the 923484-9 intercostal at station 180 at x=-20. Material 7075-t6 AL. Repaired per EA 99-181321.Jul 9, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0105009922Rib · crackedDuring Mck in ATL, the aft portion of the lower cap of the pylon closing rib was found cracked. The crack is .6" long and extends from a fasterner hole 3.7" forward from the aft end of the cap. Repaired per EA 99-181307.Jul 6, 2001 · N945N · Doug DC932 · Nacelle/Pylon, Main FrameSDR 0104409922Doubler · crackedDuring an Mck in ATL the production finger doubler along Longeron 18L was found with a cracked finger sta 850. Material .025" 2014-t6 AL. Repaired per EA 99-181280.Jul 5, 2001 · N945N · Doug DC932 · Fuselage Main, Plate/SkinSDR 0103189922Bulkhead · gougedDURING AN M-CHECK IN ATL, A GOUGE WAS FOUND IN THE STATION 604 BULKHEAD TEE AT LONGERON 27L. THE GOUGE WAS LOCATED IN THE AFT FACE OF THE WEB FLANGE AND WAS BLENDED OUT TO A MATERIAL THICKNESS OF 0.058 INCH.Jun 28, 2001 · N945N · Doug DC932 · Fuselage Main, BulkheadSDR 0001429922Battery · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Apr 18, 2000 · N945N · Doug DC932 · Emergency LightingSDR 9900029922Indicator · malfunctionedFLAPS WOULD NOT EXTEND BEYOND 25 DEGREES ON LANDING. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP POSITION INDICATOR, OPERATIONAL CHECK NORMAL.Jan 4, 1999 · N945N · Doug DC932 · Trailing Flap Position Indicating SystemSDR 9811019922Battery · dischargedDURING LINE CHECK, FOUND FIRST CLASS SECTION SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Dec 24, 1998 · N945N · Doug DC932 · Emergency LightingSDR 9810289922Air Dist · odorDURING CLIMBOUT AT FL29O, BOTH PILOTS AND A FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FLIGHT DECK. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL WIRING AND COMPONENTS, BOTH FORWARD AND MAIN ELECTRICAL COMPARTMENTS ANOct 17, 1998 · N945N · Doug DC932 · Air Distribution SystemSDR 9805969922Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Apr 6, 1998 · N945N · Doug DC932 · Emergency LightingSDR 9721089922Battery Pack · dischargedDURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS AND SIGNS INOPERATIVE. MAINTENANCE INSTALLED NEW BATTERY PACK, OPERATIONAL CHECK OK.Nov 10, 1997 · N945N · Doug DC932 · Emergency LightingSDR 9721029922Lights · miswiredDURING LINE CHECK, FOUND AFT AIRSTAIR SIDEWALL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REROUTED WIRING PER WIRING DIAGRAM, OPERATIONAL CHECK OK.Nov 9, 1997 · N945N · Doug DC932 · Emergency LightingSDR 9715559922Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND VENTRAL STAIR AND TAIL CONE DOME EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Aug 14, 1997 · N945N · Doug DC932 · Emergency LightingSDR 9711199922Aug Valve · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO YWG AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL.Jun 8, 1997 · N945N · Doug DC932 · Pneumatic Distribution SystemSDR 9710779922Clamp · looseTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LARGE AIR LEAK AT RIGHT AUGMENTATION VALVE INBOARD CLAMP. TIGHTENED CLAMP, LEAK AND OPERATIONAL CHECK NORMAL.Jun 3, 1997 · N945N · Doug DC932 · Pneumatic Distribution SystemSDR 9709349922Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.May 11, 1997 · N945N · Doug DC932 · Emergency LightingSDR 9706259922Fitting · crackedDURING L-CHECK, FOUND CRACK IN LEFT OUTBOARD SEAT TRACK SUPPORT FITTING FS 680. REPLACED FITTING PER SRM 51-30-5.Mar 21, 1997 · N945N · Doug DC932 · Fuselage Miscellaneous StructureSDR 9623749922Press Amplifier · malfunctionedLOSS OF CABIN PRESSURIZATION OCCURRED DURING FLIGHT AT 35,000 FEET. CABIN ALTITUDE REACHED 10,000 FEET WITH MASTER WARNING/CABIN PRESSURE ANNUNCIATOR LIGHTS ILLUMINATED. CAPTAIN DECLARED AN EMERGENCY AND SUCCESSFUL DESCENT WAS MADE TO 16,000 FEET. FLIGHT CONov 6, 1996 · N945N · Doug DC932 · Cabin Pressure Control SystemSDR 9623469922Relay · malfunctionedDURING DESCENT INTO EWR, THE LANDING GEAR WARNING CIRCUIT BREAKER TRIPPED. NO GREEN GEAR DOWNLOCK LIGHTS WERE ILLUMINATED AFTER GEAR WAS EXTENDED FOR LANDING. CREW VISUALLY CONFIRMED GEARS TO BE DOWN AND LOCKED THROUGH PERISCOPES. EMERGENCY EQUIPMENT WAS CANov 5, 1996 · N945N · Doug DC932 · Landing Gear Position and WarningSDR 9618769922Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Aug 29, 1996 · N945N · Doug DC932 · Emergency LightingSDR 9615549922Light Ballast · failedDURING LINE MAINTENANCE INSPECTION, FOUND EVIDENCE OF FIRE AT ROW 21DEF AT LOWER SIDEWALL LIGHT AFT BALLAST. DEFERRED LIGHT PER MEL 33-2, AWAITING PARTS FOR REPLACEMENT OF BALLAST ASSEMBLY.Jul 15, 1996 · N945N · Doug DC932 · Passenger Compartment LightingSDR 9613039922Uplatch Roller · out of adjustDURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND UPLATCH ROLLER ON LEFT GEAR NOT ENGAGED PROPERLY IN UPLATCH HOOK. RESHIMMED UPLATCH ROLLER FOR PROPJun 12, 1996 · N945N · Doug DC932 · Landing Gear Position and WarningSDR 9613029922Unsafe Light · illuminatedDURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. RECYCLED GEAR WITH NO CHANGE. FLIGHT RETURNED TO SMP AND LANDED WITHOUT INCIDENT. REPLACED GEAR UPLIMIT SWITCH, GEAR DOWN LIMIT SWITCH AND GEAR DOOR SWITCH, OJun 12, 1996 · N945N · Doug DC932 · Landing Gear Position and WarningSDR 9612309922Power Supply · inoperativeDURING PRE-FLIGHT CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. ALSO, REPAIRED WIRES THAT WERE FOUND TO BE SHORTED. OPERATIONAL CHECK NORMAL.Jun 4, 1996 · N945N · Doug DC932 · Emergency LightingSDR 9612019922Lights · inoperativeDURING PREFLIGHT CHECK, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. EMERGENCY LIGHTS WERE CHECKED PER MAINTENANCE MANUAL, NO PROBLEMS WERE FOUND.May 29, 1996 · N945N · Doug DC932 · Emergency LightingSDR 9519859922Fitting · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD FLIGHT SPOILER SUPPORT FITTING. REPLACED FITTING.Dec 6, 1995 · N945N · Doug DC932 · Wing, Control Surface Attach FittingsSDR 9518769922Battery Pack · dischargedDURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD.Nov 19, 1995 · N945N · Doug DC932 · Emergency LightingSDR 9514189922Latches · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LATCHES. ADJUSTED THE TAILCONE RELEASE SYSTEM AND CHECKED OK.Sep 8, 1995 · N945N · Doug DC932 · Aerodynamic FairingsSDR 9513949922Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 541 FLOOR SUPPORT FRAME BETWEEN LONGERON 29L TO 29R. REPAIRED FRAME PER EA 99-97124.Sep 1, 1995 · N945N · Doug DC932 · Fuselage Main, FrameSDR 9513939922Skin · cannedDURING H-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1076 TO 1087 BETWEEN LONGERONS 17L TO 18L. REPAIRED SKIN (P/N 5912870-501), PER EA 99-94921.Sep 1, 1995 · N945N · Doug DC932 · Fuselage Main, Plate/Skin
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