N405DA

Service difficulty reports not matched to an aircraft · 40

They name N405DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N405DA' AND registry_match IS NULL
  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 DL72S002459Engine · fireAFTER TAKE-OFF, NR 1 EGT GAGE IN YELLOW BAND, SHORTLY AFTER THAT, NR 1 FIRE HANDLE ILLUMINATED W/BELL. NR 1 THROTTLE BECAME DIFFICULT TO MOVE. COMPLIED WITH CHECK LIST AND NR 1 ENGINE WAS SHUT DOWN. LT FIRE BOTTLE DISCHARGED TO NR 1 ENG. DIFFICULT TO MOVE SDec 15, 2000 · N405DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S002220Spring · failedF/O QUICK DON O2 MASK HAS SPRUNG SPRING. REPLACED O2 MASK ASSY, OPS CHECK AND LEAK CHECK OK.Nov 13, 2000 · N405DA · Boeing 727232 · Crew Oxygen SystemSDR DL72S000841Web · crackedFOUND AT C-2 LETTER CHECK, .25 INCH CRACK AT LT TORQUE BOX VERT WEB LWR LIGHTENING HOLE STA 1323. REPAIRED PER M/M 53-11-0.Apr 28, 2000 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000840Skin · crackedA .375 INCH CRACK IN FUSE SKIN AFT OF L-3 WINDOW. INSTALLED DOUBLER PER SRM 53-30-3 F8. C-2 LETTER CHECK TPA.Apr 28, 2000 · N405DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000839Skin · crackedA .375 INCH CRACK IN FUSE SKIN AT LWR I/B CORNER OF L-4 WINDOW. INSTALLED DOUBLER PER SRM 53-30-3 F 8. C-2 TPA LETTER CHECK.Apr 28, 2000 · N405DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S992125Stiffener · crackedI/B SPAR STIFFENER CRACKED NR 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21 P 813.Sep 22, 1999 · N405DA · Boeing 727232 · Leading Edge DevicesSDR DL72S991988Light · damagedR1 DOOR EMERGENCY EXIT LIGHT DAMAGED. REPLACED EMERGENCY LIGHT ASSY.Sep 7, 1999 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S991357Skin · crackedLFEC INSPECTIONS PER SI 4-74176-12AD, REV J ON S26L LAP JOINT FROM BS 481-681 YIELDED SEVERAL CRACK INDICATIONS. ACCOMPLISHMENT OF THE HFEC CONFIRMED 4 CRACKS IN THE LOWER LAP ROW IN THE OVERLAPPED (LWR) SKIN. REPAIRED PER ERA 367594-14AD, REV A.Jun 14, 1999 · N405DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990332Web · crackedRT INBOARD VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1248 AND 1236. REPAIRED PER MM 53-11-0.Feb 18, 1999 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990176Battery Pack · dischargedFOUND ON PREFLIGHT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.Jan 27, 1999 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S981730Chord · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE TWO FWD MOST FASTENER HOLES AND TRAVELS DOWN. REPAIRED PER ERA 332062-14AD.Aug 21, 1998 · N405DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981724Rib · crackedUPPER CHORD OF THE LT WING RIB AT WS 171.5 WAS FOUND W/CRACKS. THE CRACKS WERE LOCATED EMANATING FROM FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER WING STRINGERS 17 AND 20. REPAIRED PER ERA 332081-14.Aug 21, 1998 · N405DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S981705Chord · crackedUPPER CHORD ANGLE OF THE RT WING AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS WERE LOCATED AT FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STRINGERS 16 AND 19. ALSO, THE S18 TAB WAS CRACKED. REPAIRED PER ERA 332040-14.Aug 19, 1998 · N405DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981676Rib · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. THE CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE 2 FWD MOST FASTENER HOLES AND TRAVELS DOWN, THRU THE ENTIRE THICKNESS OF THE HAug 14, 1998 · N405DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S981630Fitting · corrodedLEFT WING FWD WING FITTING BORE HAS CORROSION AND SCORING, FOUND WHEN BUSHING REMOVED. REMOVED BTL PIN ON R/C 59, OPN 5508AD AND REMOVED FWD BUSHING PER M/M 57-41-11. FOUND CORROSION TO BE WITHIN .15 OF INNER EDGE OF TERMINAL FITTING AT 10 AND 11 O'CLOCK POSAug 1, 1998 · N405DA · Boeing 727232 · Wing, Fuselage Attach FittingsSDR DL72S981798Spar · damagedAFT SPAR RAIL CRACKED 37 INCHES FROM I/B END OF FLAP. REPAIRED ON SO 529555 PER MM 57-52-0 FIG 802.Jul 24, 1998 · N405DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981653Rib · crackedDURING SHOP INSPECTION, THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED AT LOWER AFT CORNER. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER.Jul 24, 1998 · N405DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982006Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.Jul 23, 1998 · N405DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982005Angle · repairedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 30 INCHES FROM O/B END OF FLAP. THE CRACK WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0 FIG 802.Jul 23, 1998 · N405DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982004Skin · crackedDURING SHOP INSPECTION, THE AFT LOWER COVE SKIN WAS FOUND CRACKED IN THE CORNERS OF THE CUTOUT FOR I/B DRIVE ROD. THE CRACKS WERE ROUTED OUT AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.Jul 23, 1998 · N405DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981669Rib · crackedAT HMV FOUND, RIBS CRACKED I/B AND O/B OF GUIDE TRACK NR 6 SLAT I/B GUIDE TRACK. REMOVED ARM, FABRICATED DOUBLER MM 57-54-00 PG 813A, INSTALLED DOUBLER PER SAME.Jul 23, 1998 · N405DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981608Bulkhead Web · crackedSTA 1303 INSIDE OF VERT LOWER LT CORNER OF BULKHEAD WEB CRACKED. REMOVED EXISTING FASTENERS, STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. REPAIRED PER SRM 53-10-4 FIG 17.Jul 22, 1998 · N405DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S981607Bulkhead Web · crackedSTA 1303 INSIDE OF VERT RT SIDE CTR OF BULKHEAD WEB CRACKED AT CUTOUT FOR STR. REMOVED SECTION OF ANTI-ICE DUCT FOR ACCESS, REMOVED HORT SUPPORT BRACE FOR ACCESS, REMOVED EXISTING FASTENER AND DOUBLER. STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SJul 22, 1998 · N405DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S981025Fitting · crackedFOUND AT A2 LETTER CH, 1.5 INCH CRACK LT INBD TENSION TIE BOLT CASTING. REPLACED FIITING PER DRAWING 65-17509 REV M AND COLD WORK AND SPOT FACE PER DRAWING 65-16350.May 12, 1998 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980773Battery · dischargedAFT AIRSTAIR EMER LIGHT INOP. REPL BATT, OPS CK OK.Apr 8, 1998 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S972460Light · inoperativeL1 DOOR EXIT SIGN EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.Nov 24, 1997 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S972459Battery Charger · inoperativeE-PATH LIGHT INOP ROWS 12 TO 19. REPLACED BATTERY CHARGER.Nov 24, 1997 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S972126Bulb · failed1R DOOR EXT EMER LIGHT AND C2 AFT LIGHT INOP. REPLACED BULBS.Oct 21, 1997 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S970891Battery · dischargedAFT AIRSTAIRS EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS GOOD.May 10, 1997 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S970488Web · crackedFOUR EACH CRACKS IN LT AND RT LOWER TORQUE BOXES AT VERTICAL WEB AT LIGHTENING HOLES STA 1238 RT, STA 1228 LT, STA 1248 LT. ALL CRACKS .25 INCH. ROUTED PER M/M 53-11-0-NR 15.Mar 14, 1997 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S970487Angle · crackedFOUND ON F2 LETTER CHECK, NR 8 SLAT CRACKED AT THE LOWER COVE SKIN ATTACH ANGLE AT THE OUTBOARD STOP. REPAIRED PER MM 57-54-0.Mar 14, 1997 · N405DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961650Light · crackedR1 DOOR SLIDE LIGHT INOP. REPLACED REFLECTOR LIGHT ASSEM.Jul 6, 1996 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S961268Light · inoperativeL-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP CKS GOOD.May 23, 1996 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S960233Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BELLY SKIN ABOVE THE RAM AIR INLET. THE DAMAGE CUTOUT MEASURES 12 INCHES FWD AND AFT BY 10 INCHES INBD AND OUTBD AT FS 720C. IN ACCORDANCE WITH 8110-3 DATED 1/26/96, AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLEDJan 26, 1996 · N405DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960268Skin · dentedDURING INSPECTION, C-3 CARGO DOOR OUTER SKIN WAS FOUND WITH THREE DENTS BEYOND ALLOWBLE LIMITS. REPAIRED SKIN PER SRM 52-30-1 FIG 9.Jan 24, 1996 · N405DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S960177Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.Jan 23, 1996 · N405DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960176Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.Jan 23, 1996 · N405DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954750Solenoid · failedIRR - ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION. PUT GEAR HANDLE BACK DOWN. DIVERTED TO DEN DUE TO GEAR HANDLE. CORRECTIVE ACTION - REPLACED LANDING GEAR HANDLE LATCH LEVER SOLENOID PER DELTA M/M 32-31-16. CYCLED GEAR SEVERAL TIMES, ALLDec 21, 1995 · N405DA · Boeing 727232 · Landing Gear SelectorSDR DL72S953143Angle · cracked1.0 CRACK IN ANGLE OF FWD BEAM OF THE RT TORQUE BOX, FS 1263. REPAIRED PER DL ERA 301959-14.Jun 22, 1995 · N405DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S952738Stiffener · crackedFOUND DURING E-1 LETTER CHECK, WING SPAR STIFFENER AT NR 6 LE SLAT I/B TRACK O/B SIDE HAS 1 INCH CRACK FROM BOTTOM. REPAIRED PER M/M 57-20-21.Jun 21, 1995 · N405DA · Boeing 727232 · Wing Miscellaneous Structure
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