N408DA, cancelled Jan 31, 2001

Service difficulty reports · 59

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 = 'N408DA' AND deregistration_id = 'N408DA-2001-01-31'
  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 DL72S002196Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 1009 AND 1183 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION CONFIRMED 8 CRACKS. THE ENTIRE SKIN LAP JOINT WAS CUTOUT BETWEEN FS 1009 AND 1120. THE JOINT WNov 8, 2000 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002112Battery Pack · dischargedR-2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED OVERHEAD LIGHT BATTERY PACK ON R-2 DOOR.Oct 25, 2000 · N408DA · Boeing 727232 · Emergency LightingSDR DL72S001223Skin · crackedFOUND ON C2 CHECK, FUSELAGE SKIN CRACKED LOWER INBD CORNER OF L-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.Jun 28, 2000 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S001033Line · rupturedTOTAL LOSS OF B HYDRAULIC SYS. HYDRAULIC QTY WAS ZERO, PRESS WAS FLUCTUATING. FLIGHT CREW ADVISES LOSS BEGAN 50 MILES FROM ATL. NO CONFIGURATION CHANGE. FOUND PRESS LINE ON B SYS ELEC PUMP RUPTURED. REPLACED LINE.May 25, 2000 · N408DA · Boeing 727232 · Hydraulic System, MainSDR DL72S992805Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 480 & 680 CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS. THE ENDec 21, 1999 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S992804Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 360 & 480 CONFIRMED A TOTAL OF 4 CRACKS IN ALONG THE SKIN LENDec 21, 1999 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S992803Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPECTION OF THE 4R LAP SPLICE BETWEEN FS 680 & 740 CONFIRMED 7 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE PANDec 21, 1999 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982299Power Supply · inopFIRST CLASS EMERGENCY LIGHTS INOP. REPLACED BATTERY PWR SUPPLY, NOW CKS GOOD.Nov 8, 1998 · N408DA · Boeing 727232 · Emergency LightingSDR DL72S981942Stiffener · damagedWING UPPER SURFACE J STIFFENER REPAIR (STR 17 RT AT WS 300). REPAIR PER ER/A 332215-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981941Clip · crackedFS 400 FRAME CLIP BETWEEN STR 17 AND 18 WAS FOUND CRACKED. REPAIRED PER ER/A 332224-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981940Stringer Tab · crackedSTRINGER 18 TAB ON THE RT WING VENT BOX WAS FOUND CRACKED. REPAIR PER ER/A 332222-14.Sep 16, 1998 · N408DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S981939Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN, SIMILAR TO S/B 727-53-0172. STRINGER 18A LOWER FLANGE WAS FOUND WITH A CRACK. REPAIR PER ERA 332141-14.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981938Chord · gougedTHE C-2 DOOR STA 990 INBOARD CHORD WAS FOUND WITH A GOUGE AT STRINGER 26R. THE GOUGE WAS LOCATED ON THE OUTER CORNER OF THE INTERSECTION OF THE 2 LEGS OF THE L-SHAPED CHORD. REPAIRED PER ER/A 332209-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981919Ball Nut · rustedAT HMV, LANDING GEAR CHECK OUT THE NOSE GEAR EMERGENCY EXTENSION FAILED TO OPERATE DUE TO THE BALL NUT AND SCREW ASSY BEING RUSTED AND FROZEN UP. REF IPC 32-31-00-06 ITEM 185 (P/N 10-60744-1). THE ASSY WAS REPLACED AND THE CHECK OUT COMPLETED SATISFACTORY.Sep 15, 1998 · N408DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S981918Rib · crackedUPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. REPAIRED PER ERA 332223-14.Sep 15, 1998 · N408DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S981875Duct · bentDOGHOUSE AFT LIP, ON AIRINTAKE DUCT 360 DEGREES AREA, BENT AND DISTORTED. HEAVY ACCUMULATION OF SEALER. REMOVED DAMAGE DOUBLER, BEGAN DRILLING NEW DOUBLER. COMPLETED FABRICATION OF NEW DOUBLER PER SRM 54-10-3 FIG 13 D. OK TO INSTALL DOUBLER. INSTALLED REPSep 10, 1998 · N408DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S982067Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER WAS FOUND CRACKED IN 2 PLACES, 32 AND 37 FROM IB END. THE ANGLE WAS REPAIRED PER 727MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Aug 26, 1998 · N408DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982062Skin · cracked.5 INCH LONG CRACK IN COVE SKIN -31 FROM I/B END OF FLAP, REPAIRED ON SHOP ORDER 553647 PER MM5 7-52-0 FIG 809.Aug 24, 1998 · N408DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982061Spar · crackedCRACK AFT SPAR RAIL 19 FROM I/B END OF FLAP. REPAIRED ON SHOP ORDER 553647 PER MM 57-52-0 FIG 802.Aug 24, 1998 · N408DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981903Stringer · crackedSTRINGER CRACKED VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 180.6 STA 9L. CRACK RUNS FROM HOLE TO EDGE OF PART. NO STOP DRILL REQUIRED. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. IK INSTALL. BEGAN INSTALL OF REPAIR PER M/M 55-30-0 FIG 803. FINISAug 23, 1998 · N408DA · Boeing 727232 · Vertical StabilizerSDR DL72S981902Stringer · crackedSTRINGER CRACKED. VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 157.2 STR 8L. CRACK RAN FROM CTR OF HOLE TO EDGE OF STRINGER. FABRICATED REPAIR ANGLE PER MM 55-30-0 FIG 803 OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 FIG 803.Aug 23, 1998 · N408DA · Boeing 727232 · Vertical StabilizerSDR DL72S981809Cowl · wornFOUND AT HMV, STA 1352 FWD COWLING RING WORN THROUGH AT 6 O'CLOCK POSITION. ROUTED OUT DAMAGE MANFCT BDLER PER MM 53-11-0 PG 801 AND INSTALLED PER SRM 53-11-0 PG 801.Aug 23, 1998 · N408DA · Boeing 727232 · Engine Cowling SystemSDR DL72S981286Batteries · dischargedON L/O, FOUND 2L DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES.Jun 17, 1998 · N408DA · Boeing 727232 · Emergency LightingSDR DL72S980965Stringer · crackedFOUND AT A2 LETTER CHECK, VERTICAL STAB STRINGER 6L CRACKED AT BOLT HOLE FIN STA 157.2. REPAIRED PER M/M 55-30-0.May 6, 1998 · N408DA · Boeing 727232 · Vertical StabilizerSDR DL72S971984Flap · crackedA .75 INCH CRACK IN NR 4 L/E FLAP AT OUTBOARD LIP HINGE CUTOUT. REPAIRED PER ERA NR 362925-14 AND M/M 57-53-0.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971982Fitting · crackedFOUND DURING A1 LETTER CHECK, 1 INCH CRACK NR 8 SLAT ACT INBD ATTACH FITTING OUTBD SIDE. REPAIRED PER M/M 57-20-21.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971981Frame · crackedFOUND ON A1 LETTER CK, .5 IN CRACK FWD FRAME AT LOWER STOP CASTING R-1 DOOR. REPAIRED PER MM 52-12-0 AND ERA.Oct 6, 1997 · N408DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S971980Rib · crackedFOUND ON A1 LETTER CK, 2 IN VISIBLE CRACK NR 1 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-20-21.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971365Actuator · failedSYS-A HYD QTY WENT TO 0 AND BOTH LOW PRESS LIGHTS CAME ON WITH EXTENSION OF FLAPS ON TAXI OUT. FOUND NUMBER 4 SLAT ACTUATOR LEAKING. REPLACED ACTUATOR.Jul 11, 1997 · N408DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S962607Skin · crackedFOUND A GOUGE IN THE LOWER FUSELAGE SKIN JUST AFT OF THE L-1 DOOR. REPAIRED PER DAL EO 4-60829-3 AND ER/A 30446-14, REV A.Nov 21, 1996 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S962529Support · crackedFOUND CRACK ON THE NR 1 SLAT ACTUATOR SUPPORT STRUCTURE. REPLACED CRACKED WEB IAW DAL ER/A 304444-14AD.Nov 14, 1996 · N408DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S962587Chord · corrodedAT MID VISIT, THE NLG LT LWR CHORD WAS FOUND TO BE CORRODED. CORROSION WAS REMOVED AND REPAIR ACCOMPLISHED PER SRM 53-10-4.Nov 13, 1996 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S962588Bulkhead Support · wornAT MID VISIT, THE VERT SUPPORT BEAMS FOR AFT C1 BIN BULKHEAD WERE FOUND TO BE WORN. THEY WERE REPAIRED PER SRM 53-10-9.Nov 12, 1996 · N408DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S962017Megaphone · inoperativeFWD MEGAPHONE BATTERY LOW. REPLACED MEGAPHONE, TESTS GOOD.Aug 31, 1996 · N408DA · Boeing 727232 · Emergency EquipmentSDR DL72S971363Skin · crackedSKIN CRACKED AT FAIRING NUMBER 5 SLAT.Aug 16, 1996 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960367Bell Crank · wornPILOT REPORTS, AT 230 KTS A LOUD VIBRATION WAS HEARD FROM THE F/O WINDOW AREA DURING CLIMBOUT AND AT 220 KTS DURING DECEL THE VIBRATION STOPPED. REPLACED THE RIGHT HAND OUTBOARD AILERON TRIM TAB BELL CRANK, WHICH WAS FOUND TO HAVE OBLONGED MOUNT HOLES. RIG CFeb 18, 1996 · N408DA · Boeing 727232 · Aileron Control SystemSDR DL72S960218Skin · crackedLOWER L/E SKIN CRACKED AND WORN AT FENCE ATTACH HOLE. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 LE SLAT.Jan 28, 1996 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960217Skin · crackedOUTER SKIN CRACKED AT FENCE ATTACH HOLE AND GROOVED AT REMAINING ATTACH HOLES. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jan 28, 1996 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960216Rib · crackedRIB WAS FOUND TO BE CRACKED ON INSPECTION. RIB WAS REPAIRED PER M/M 57-54-00. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jan 28, 1996 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960143Light · inoperativeON INSPECTION, LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPN CKS NORMAL.Jan 21, 1996 · N408DA · Boeing 727232 · Emergency LightingSDR DL72S961602Transverse Beam · crackedTHERE IS A .5 INCH CRACK IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129.Jan 17, 1996 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960110Angle · crackedFOUND ON E2 LETTER CHECK, KEEL BEAM VERT STIFFENER CRACKED .5 INCH FWD INBD RT W/W. TIME LIMITED REPAIR PER SRM 53-10-9.Jan 16, 1996 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960105Blkhd Web · crackedFOUND ON E2 LETTER CHECK, STA 870 BULKHEAD WEB CRACKED 3 INCHES AT APU LOAD CONTROL VALVE CUTOUT, LWR END IN RT W/W. REPAIR PER SRM 53-10-9, TIME LIMITED INST.Jan 16, 1996 · N408DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960104Angle · crackedFOUND DURING E-2 LETTER CHECK, .375 INCH CRACK NR 4 L/E SLAT COVE SKIN LWR ATTACH ANGLE AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.Jan 16, 1996 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960054Skin · dentedDURING SHOP INSPECTION, AILERON PANEL UPPER SKIN WAS FOUND DENTED. SPLICED UPPER SKIN PER SRM 57-53-5 FIG 3.Jan 9, 1996 · N408DA · Boeing 727232 · AileronsSDR DL72S960480Wire Harness · burnedA/C LOST N-1 INDICATION, FUEL HEAT LIGHT AND START VALVE LIGHT 'ON'. F/F STUCK ON 4800 PPH, ENGINE SHUTDOWN. FOUND WIRE HARNESS MELTED IN FWD PYLON SPLICED IN NEW ENG WIRING AT PLUGS D374J, D356J, D350J, D386P AND D362J, PERFORMED CK OUT PER PFHB AND CKS GOOJan 1, 1996 · N408DA · Boeing 727232 · Engine Indicating System WiringSDR DL72S954761Tube · wornPIREP LOSS OF ALL HYD B-QUANTITY IN-FLIGHT. FOUND HYD LINE IN LEFT BODY FAIRING AREA LEAKING. REF IPC 29-14-0-6, ITEM 155, AND ITEM 160. HOLE IN LINE DUE TO CHAFING.Dec 23, 1995 · N408DA · Boeing 727232 · Hydraulic System, MainSDR DL72S954583Skin · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH L/E SKIN CRACKED AT OUTBOARD END. REPAIRED PER SRM 57-30.Nov 30, 1995 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954549Rib · crackedDURING SHOP INSPECTION, NR 6 L/E RIB WAS FOUND WITH L/E SUPPORT RIBS NRS 3, 4, 7, 8, 10 AND 12 CRACKED. REPAIRED PER MM 57-54-0.Nov 28, 1995 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954499Rib · crackedDURING ROUTINE SHOP INSPECTION A CRACK WAS FOUND IN THE 16TH RIB AND A DOUBLER WAS INSTALLED USING MM 57-54-0 FOR NR 6 L/E SLAT.Nov 27, 1995 · N408DA · Boeing 727232 · Leading Edge Devices
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