N505DA, cancelled Mar 21, 2013

Service difficulty reports · 66

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 = 'N505DA' AND deregistration_id = 'N505DA-2013-03-21'
  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 DL72L011283Light · inoperativeON LAYOVER FOUND 4CD FASTEN SEAT BELT LIGHT INOP. C/A RELAMPED OPS CKS GOODAug 3, 2001 · N505DA · Boeing 727232 · Passenger Compartment LightingSDR DL72L011149Switch · out of adjAT 5 DEG FLAPS NR 3 L/E FLAP DID NOT EXTEND FULLY CYCLED. ACCORDING TO CHECKLIST BUT DID NOT EXTEND. ADJUSTED NR 3 L/E FLAP SWT RAN FLAPS TO 5 DEG AND BACK ALL IND NORMAL.Jul 11, 2001 · N505DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72L010335Battery · dischargedON L/O, FOUND 1L OVERHEAD EMERGENCY EXIT SIGN DIM. REPLACED EXIT SIGN BATTERIES, CKS OK.Feb 27, 2001 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L010309Web · crackedA 1 INCH CRACK IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1210 AND TWO CRACKS IN LT TORQUE BOX VERT WEB AT UPPER RIVET ROW STA 1235. REPAIR PER M/M 53-11-000-8.Feb 21, 2001 · N505DA · Boeing 727232 · Fuselage Main, StructureSDR DL72L001381Angle · crackedFOUND ON B1 LETTER CK, 1.5 INCH CRACK IN STA 870 WEB VERTICAL CHORD AT I/B END OF LT WHEEL WELL. REPAIRED PER B727 DRD 53-10-9D FIG 806.Jul 21, 2000 · N505DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L000352Actuator · leakingLOST B HYDRAULIC SYSTEM PRESS AND FLUID IN FLIGHT. MADE UNSCHEDULED LANDING. FOUND NUMBER 3 SPOILER ACTUATOR LEAKING. REPLACED NR 3 SPOILER ACTUATOR.Feb 21, 2000 · N505DA · Boeing 727232 · Drag Control ActuatorSDR DL72L992760Web · dentTHE NR 4 RIB OF THE VERTICAL STABILIZER HAS A DENT IN THE WEB THAT RESULTED IN A 1 INCH DIAMETER CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333924-14.Dec 16, 1999 · N505DA · Boeing 727232 · Vertical StabilizerSDR DL72L992782Rib · crackedAT HMV2 FOUND NR 3 SLAT RIBS CRACKED. REPAIR AT RIB MARKED NR 3, RIB MKD NR 10, RIB MKD NR 17. CORROSION - DYE CKD AS PER PS 900-6-3 AND NO CRACKS. FABRICATED DOUBLER PER MM 57-54-0 PG 807. INSTALLED DOUBLER PER SAME, DYE CHECKED RIB NR 17 PER PS 900-6-3 Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L992727Rib · crackAT HMV2, FOUND NR 4 SLAT RIB (MARKED) CRACKED. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. DYE CHECKED END OF CRACK PER FIG 504. CHEM TESTED PER PS 900-2-4-1 NR 2. REPAIRED RIB PER MM 57-54-0.Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L992671Rib · crackedAT HMV2, FOUND NR 8 SLAT RIB'S CRACKED, NR 4, 14 (MARKED). REMOVED I/B SLTRK AND STOP DRILLED CRACK PER MM 57-40-0 FIG 809, FABRICATED REPAIR PARTS PER MM 57-54-00 FIG 809.Dec 1, 1999 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L992783Skin · tornAT HMV2 ELEVATOR T/E CHIPPED/TORN LT ELEVATOR EXTREME O/B END. BUSHED AREA AND FOUND TO BE WITHIN LIMITS PER SRM 55-20-1 FIG 161, INSTALLED FASTENERS.Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L992670Skin · disbondedAT HMV2, FOUND RT ELEV T/E DISBONDED BETWEEN UPPER AND LWR SKIN SEVERAL AREA'S FROM I/B TO O/B AREA. REPAIRED PER MM 55-20-0 PG 801 NR 2.Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L992669Skin · delaminatedAT HMV2, FOUND LT ELEVATOR T/E DELAMINATED I/B AND O/B OF TAB. REPAIRED PER MM 55-20-0 PG 801 NR 2.Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L992668Skin · disbondedAT HMV2, FOUND RT ELEVATOR I/B TRAILING EDGE DISBONDED. REPAIRED PER MM 55-20-0 PG 801 NR 2.Nov 30, 1999 · N505DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L992667Stringer · crackedAT HMV2, FOUND STRINGER 5R CRACKED AT RIB NR 9 VERT STAB INTERIOR. DYE CHECKED AND FOUND CRACK EXTENDS TO EDGE OF MATERIAL. CHEM TREATED PER PS 900-2-4-1 NR 2, FABRICATED REPAIR PER MM 55-30-0 PG 803, AND INSTALLED PER SAME.Nov 30, 1999 · N505DA · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR DL72L992254Socket · failedPILOT REPORT, FIRST CLASS SECTION EMERGENCY TRACK LIGHTING INOP. FOUND BAD SOCKET AT 10DEF REPLACED FUSE AT FWD POWER SUPPLY PACK. SYSTEM OPS NORMAL DEFERED SOCKET AT 10DEF PER MEL 33-00-17B SOCKET DISCONECTED AND WIRE HARNESS SECURED. REPLACED SEAT MOUNTEDOct 10, 1999 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L991809Frame · crackedFUSELAGE C1 DOOR SURROUND FRAME, FS 560, WEB CRACK REPAIR. A INCH 2 CRACK WAS FOUND IN THE WEB OF THE FORWARD JAMB FRAME OF THE C1 DOOR OPENING. THE CRACK WAS LOCATED AT THE 2ND FROM THE TOP DOOR STOP. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER Aug 11, 1999 · N505DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991795Web · cracked1 INCH CRACK AT RIGHT TORQUE BOX VERTICAL WEB AT UPPER RIVET ROW STA 1223 (48 SEC). REPAIR PER MM 53-11-0.Aug 11, 1999 · N505DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991459Accessory Unit · inoperativeGEAR EXTENSION BUF UNSAFE GEAR WARNING WITH RT MAIN GEAR RED INDICATOR LIGHT ON WITHOUT THE GREEN DOWN AND SAFE LIGHT ON. REPLACED LANDING GEAR ACCESSORY UNIT.Jun 28, 1999 · N505DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72L991225Skin · crackedINTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 2 CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND REPAIRED WITH AN ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991224Skin · crackedINTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 3May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991223Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 47 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN May 31, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990764Battery · dischargedRT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY AT M957, OPS CHECKS GOOD.Apr 7, 1999 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L990318Frame · damagedFUSELAGE LT OVERWING EXIT CUTOUT FRAME FS 784, REPAIR FOR DISCREPANT FASTENER HOLES. WHILE ACCOMPLISHING INSPECTIONS OF THE LT OVERWING EXIT CUTOUT FRAME AT FS 784, SEVERAL FASTENER HOLES WERE FOUND OVERSIZED DAMAGED. THE MODIFICATION PER BAC S/B 727-53-0197Feb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L990317Frame · damagedFUSELAGE RT OVERWING EXIT CUTOUT FRAME FS 783.95, REPAIR FOR DAMAGED HOLES. UPON INSPECTION FOR TYPICAL CRACKS IN THE INNER CHORD OF THEFS 783.95 OVERWING EXIT CUTOUT FRAME, SEVERAL HOLES WERE FOUND MISDRILLED. THE PREVENTATIVE MODIFICATION PER BAC S/B 727-5Feb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L990316Frame · crackedFUSELAGE RT OVERWING EXIT FRAME, FS 761, FRAME CHORD REPAIR. THE FS 761 FRAME FOR THE RT OVERWING EXIT CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE INNER CHORD. THE FRAME WAS REPAIRED/MODIFIED PER BAC S/B 727-53-0197 WITH MODIFICATIONS REQUIRED DUE TO EXFeb 14, 1999 · N505DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L990275Support · corrodedWING MLG SUPPORT BEAM, LT AFT ATTACH LUG, REPAIR FOR CORRODED LUG. THE AFT ATTACH LUG OF THE LT MLG SUPPORT BEAM WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG HOLE BORE AND SPOTFACING THE SURFACE OF THE LUG. THE LUG WAS REPAIRED BY INSFeb 10, 1999 · N505DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L990184Skin · gougedA GOUGE WAS FOUND IN THE SKIN PANEL AT FS 500 BELOW THE STRINGER 26L LAP SPLICE. THE DAMAGE WAS TRIMMED OUT OF THE SKIN WITHOUT DAMAGING THE EXISTING LAP. THE CUTOUT WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366548-14.Jan 26, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990039Skin · crackedNR 7 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.Jan 7, 1999 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L982657Line · crackedCREW LOST B HYDRAULICS PRESSURE AND QUANTITY ON ARRIVAL TO PHL. FOUND BROKEN HYDRAULIC LINE IN HYD SERVICE BAY REF IPC-29- 14-00-06 ITEM 160. MPN-65-17849-61M. DPN-294201161. INSTALLED TEMP HYDRAULIC LINE, SERVICED HYD SYS TO FULL AND LEAK CHKS NORMAL. FWD Dec 30, 1998 · N505DA · Boeing 727232 · Hydraulic System, MainSDR DL72L982470Stop · looseWING NR 7 SLAT, DOWNSTOP FITTING, REPAIR FOR LOOSE BOLT. THE NR 7 SLAT DOWNSTOP FITTINGS WERE FOUND WITH LOOSE BOLTS. DURING INSPECTIONS PER S/B 727-57-171. THE STOP FITTINGS FOR THE SLAT WERE MODIFIED PER THE REQUIREMENTS OF THE S/B. THE MODIFICATION OF Nov 27, 1998 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L982374Battery Pack · dischargedRIGHT AFT EMERGECY OVERWING LIGHTS ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK.Nov 16, 1998 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L981187Mount · crackedNR 1 LE FLAP ACTUATOR MOUNT CRACKED UPPER O/B CORNER. REPAIR PER M/M 57-20-21.Jun 3, 1998 · N505DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L981186Skin · delaminated5 IN LENGTH DELAMINATION ON RT ELEVATOR TRAILING EDGE I/B END. REPAIR PER M/M 55-20-0.Jun 3, 1998 · N505DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L981185Web · cracked.1875 IN CRACK ON VERTICAL WEB LIGHTNING HOLE STA 1228 LT SIDE. ROUTE CRACK PER M/M 53-11-0.Jun 3, 1998 · N505DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981184Casting · cracked0/B ACTUATOR ATTACH CASTING BROKEN AT LOWER MOUNT BOLT NR 4 SPOILER. REPLACED CASTING PER M/M 57-42-0.Jun 3, 1998 · N505DA · Boeing 727232 · Drag Control ActuatorSDR DL72L980646Air Distribution · smokeAIR RETURN SMOKE IN AFT CABIN DURNING T/O CREW DUMPED FUEL TO 163,500 NORMAL LANDING AND STOP. RAN PACKS WITH APU AIR ALL PACKS OPERATED NORMAL. FLT CREW TAXI AND AND RAN ENGINES AT RUNUP AREA WITH MECHANIC, CHECKING PACKS WITH ENGINE AIR AT IDLE AND POWER.Mar 24, 1998 · N505DA · Boeing 727232 · Air Distribution SystemSDR DL72L980266Light · inoperativeL-2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.Jan 30, 1998 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L972116Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER I/B SIDE OF THE SECOND FROM THE I/B HINGE FITTING. THE CRACK IS APPROXIMATELY .25 LONG. THIS CRACK LENGTH IS WITHIN THE .250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED UNOct 13, 1997 · N505DA · Boeing 727232 · Elevator, Spar/RibSDR DL72L971429Battery Pack · dischargedAFT FLOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK M9027, ALL OPS NORMAL.Jul 21, 1997 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L970933Rear Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER INBD SIDE OF THE SECOND FROM INBD HINGE FITTING. THE CRACK IS APPROX .25 INCH LONG. THIS CRACK LENGTH IS WITHIN THE 0.250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED (TEMPMay 14, 1997 · N505DA · Boeing 727232 · Elevator, Spar/RibSDR DL72L961135Light · frayed wiresEMERGENCY LIGHTS OUT FROM ROWS 12 TO 19. FOUND FRAYED WIRES RUBBING AT ROW 17. REPLACED BULB SOCKET, FUSES IN M9026 AND M9027 POWER SUPPLIES, OP CKS NORMAL.May 12, 1996 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L960878Light · inoperativeFWD ENTRY OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.Apr 16, 1996 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L960833Slide · torn webbingON PREFLIGHT, FOUND RT AFT SERVICE DOOR EMERGENCY SLIDE WEBBING AT GIRT BAR TORN. REPLACED SLIDE.Mar 31, 1996 · N505DA · Boeing 727232 · Escape SlideSDR DL72L960622Compressor · stalledAPPLYING TAKEOFF POWER HAD EXPERIENCED COMPRESSOR STALLS ON NR 2 ENG, WIND WAS APPROX 320 AT 17 TO 20 KTS, DEPARTED 35L DFW. AFTER TAKEOFF COMPRESSOR STALLS RETURNED ON CLIMBOUT AT 190 KTS. REPLACED PRBC AND P AND D VLV, NO HELP. ACTVATED 6TH STAGE BLEED PMar 20, 1996 · N505DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72L960614Power Supply · inoperativeDURING EMERGENCY LIGHTING CHECK, MAINT FOUND TRACK LIGHTING BETWEEN ROWS 12 AND 19 INOP. REPLACED POWER SUPPLY, OPERATION NORMAL.Mar 19, 1996 · N505DA · Boeing 727232 · Emergency LightingSDR DL72L960500Angle · crackedFOUND ON D1 LETTER CK, NR 7 SLAT LOWER ANGLE CRACKED AT THE ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960499Angle · crackedFOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR SUPPORT BOX CRACKED INBD END. REPAIRED PER MM 57-20-21.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L960498Casting · crackedFOUND ON D1 LETTER CK, NR 2 SLAT ACTUATOR MOUNT CASTING/ANGLE CRACKED O/B UPPER EAR. REPAIRED PER MM 57-42-0.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L954319Eel Charger · malfunctionedON PREFLIGHT, EMERGENCY EXIT LIGHTING BATTERY CHARGER POPS CIRCUIT BREAKER. T/S SYS REPLACED BATT CHARGER C/B AND SPLICE SM17 WDM 33-51-02 PG 5, OPERATION NORMAL.Oct 29, 1995 · N505DA · Boeing 727232 · Emergency Lighting
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