N406DA, cancelled Feb 16, 2001

Service difficulty reports · 60

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 = 'N406DA' AND deregistration_id = 'N406DA-2001-02-16'
  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 DL72S002085Battery Pack · inoperativeFOUND THE BATTERY PACK INOP AT THE AFT CARGO DOOR EMERGENCY LIGHTS. CHANGED BATTERY PACK, EMERGENCY LIGHTS ARE OK.Oct 22, 2000 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S001796Transmitter · inoperativeOUTBOARD FLAP INDICATIONS SPLIT AT 15 DEG CAUSING A LOCKOUT. ALT FLAP EXTEND USED. INDICATORS BOUNCE BETWEEN SPLIT AND EQUAL SETTINGS. NO ROLL TENDENCIES WERE FELT WHEN FLAPS WERE EXTENDED. REPLACED LEFT OUTBOARD FLAP TRANSMITTER PER M/M. FLAP IND AND OPESep 17, 2000 · N406DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S001765Angle · crackedFOUND ON C1 LETTER CK, 1.25 INCH CRACK IN THE RT FS 870 KEEL BEAM I/B ATTACH ANGLE. STOP DRILLED CRACK PER B727 DRD 53-10-9D FIG 806D.Sep 11, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001710Bracket · broken2L GIRT BAR ATTACH FITTING TO FLOOR SPRING BROKEN, BAR WILL NOT ENGAGE. REPLACED BROKEN BRACKET.Sep 6, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001706Battery · dischargedAFT I/B EMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY.Sep 5, 2000 · N406DA · Boeing 727232 · Emergency EquipmentSDR DL72S001566Battery · leakingL1 OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY DUE TO WEAK BATTERIES LEAKING INTO LIGHT ASSY.Aug 15, 2000 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S001039Light · inoperativeAFT AIRSTAIRS EMERGENCY LIGHT FAILED TO TEST. REPLACED LIGHT ASSY.May 26, 2000 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S000571Battery · inoperativeLEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. LIGHT OPN CKS GOOD.Mar 24, 2000 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S000273Bulkhead · crackedFS 870 WEB CRACKED RT MLG W/W AT APU LOAD CONTROL VALVE. CUT OUT 1.5 INCH AT 6:00 POS. INSTALLED TIME LIMITED REPAIR PER SRM 53-10-9D FIG 806D.Feb 7, 2000 · N406DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S000272Angle · crackedA 2 INCH CRACK IN TORQUE BOX SHELF ANGLE FWD SIDE OF STA 1263. REPLACED ANGLE PER SRM 53-10-10D FIGURE 803D.Feb 7, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S992251Battery · dischargedAFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED BATTERY'S, OPS NOW OK.Oct 10, 1999 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S992130Battery · dischargedAFT AIRSTAIR EMERGENCY EXIT LIGHT INOP ON L/O CHECK. REPLACED BATTERYS (P/N 334101877), OPER NOW NORMAL.Sep 23, 1999 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S991960Battery Pack · dischargedRT AFT 2 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M957 AND M956, OPS CHKS GOOD.Sep 3, 1999 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S991935Insulation · splitON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-0Aug 2, 1999 · N406DA · Boeing 727232 · Electrical Power System WiringSDR DL72S991487Web · crackedTPA LTR CHK B1, .375 INCH CRACK TORQUE BOX VERT WEB STA 1226. REPAIRED PER MM 53-11-0.Jul 1, 1999 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991485Frame · crackedFOUND AT B-1 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.Jul 1, 1999 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990747Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 11 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT OVER THE LENGTH OF THE PANEL Apr 1, 1999 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990746Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 25 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND RApr 1, 1999 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982437Skin · damagedLWR SKIN OF THE LT HORIZONTAL STAB HAS A PRE-EXISTING EXTERNAL T/L REPAIR. NEED PERMANENT REPAIR INSTRUCTIONS. REPAIRED PER ERA 332447-14.Nov 25, 1998 · N406DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72S982282Rib · crackedDURING SHOP INSPECTION, A REPAIR DOUBLER AT THE I/B AFT RIB WAS FOUND TO BE CRACKED. THE DOUBLER WAS REMOVED AND THE RIB WAS REPAIRED PER MM 57-52-0 FIG 808.Nov 6, 1998 · N406DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S982567Spar · crackedNR 2 MID FLAP, CRACK AFT SPAR RAIL 33 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 615732.Nov 5, 1998 · N406DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982301Flap Track · corrodedINBOARD FLAP INBOARD TRACK TYP CORROSION AT FWD LUG AND MLG BEAM ATTACH HOLES: AD 90-07-05. INSTALL OVERSIZED BUSHINGS IN FWD LUG HOLES, OVERSIZE MLG BEAM ATTACH HOLES AND PROCEED WITH SPLICE PLATE REPAIR PER BAC SB 727-57-0178.Nov 5, 1998 · N406DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982404Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 19 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Nov 4, 1998 · N406DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982369Skin · crackedSKIN CRACKED APPROX 1.5 ON LWR SURFACE OF RT ELEV FWD AND I/B OF TAB CONTROL ROD. DYE CHECKED AND STOP DRILLED CRACKS, FABRICATED REPAIR PART PER SRM 55-20-3 FIG 5. OK TO INSTALL. INSTALLED DOUBLER, FASTENERS AND DOUBLE WEIGH 63G PER SRM 55-20-3 FIG 5.Nov 3, 1998 · N406DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S982363Angle · damagedNR 4 SLAT, ANGLE CRACKED IN CORNER. DYE CHECKED PER PS 900-6-3. NO CRACK FOUND. BURNISHED AREA, TREATED AND PAINTED PER PS 900-2 NR 5.Nov 3, 1998 · N406DA · Boeing 727232 · Leading Edge DevicesSDR DL72S982440Skin · corrodedA SKIN BULGE AND TWO CRACKED FASTENER HOLES WERE DISCOVERED AT BS 681, 8 INCHES ABOVE STRINGER 14R. UPON FURTHER INSPECTION CORROSION WAS FOUND ON THE I/B SIDE OF THE WINDOW BELT SKIN PANEL. REPAIRED PER ERA 332473-14.Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982439Frame · damagedLOWER LOBE FRAMES IN THE AFT B/B AT BS 1030 WERE FOUND DENTED BETWEEN S26R AND 27R. MISDRILLED HOLES WERE DONE DURING ACCOMPLISHMENT OF SRM REPAIR. REPAIRED PER ERA 332463-14AD.Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S982438Shear Tie · damagedSHEAR TIES AT BS 580 AND 620, S14R WERE DAMAGED DUE TO REWORK OF THE SKIN LAP JOINT. REPAIRED PER ERA 332452-14.Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980928Battery Pack · dischargedON INSP, FOUND AFT EMERGENCY EXIT SIGN NO TEST. REPLACED BATTERY PACK.Apr 30, 1998 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S980623Angle · crackedNR 7 SLAT ACT O/B ATTACH ANGLE CRACKED AT UPPER LOBE. REPAIRED PER MM 57-42-0.Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S980622Web · crackedNR 8 SLAT ACT I/B AND O/B ATTACH ANGLE CRACKED AT WEB. REPAIRED PER MM 57-20-21.Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980621Angle · crackedFOUND ON A1 LETTER CK, NR 8 SLAT LOWER ATTACH ANGLE CRACKED AT THE INBD STOP PAD. REPAIRED PER MM 57-54-0.Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980620Stiffener · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK IN LOWER END OF L/E SPAR STIFFENER NR 2 SLAT O/B TRACK, INBD STIFFENER. REPAIRED PER MM 57-20-21.Mar 20, 1998 · N406DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S972567Roller · bindingAFTER TAKEOFF, THE LEFT FORWARD ENTRY DOOR DID NOT SEAL PROPERLY. DAYLIGHT COULD BE SEEN THROUGH THE DOOR SEAL. FOUND DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, FOUND CAMPLATE ROLLER BINDING. REPLACED ROLLER, FOUND UPPER DOOR GUIDE HINGE GUIDE ARM OUT OF ADDec 8, 1997 · N406DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S972081Fuel Control · failedAPPROX 40 MINS INTO FLIGHT AT FL330 THE NR 1 ENG INVOLUNTARILY WENT TO FULL POWER. THE THROTTLE DID NOT MOVE. PHYSICAL MOVEMENT OF THE THROTTLE PRODUCED NO ENGINE RESPONSE. PARAMETERS AT SHUTDOWN AS FOLLOWS OIL PRESSURE POSITIVE 45 EPR 2.4 N1-102 EGT-600C Oct 17, 1997 · N406DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR DL72S970340Spar · crackedDURING THE CURRENT SHOP VISIT AND INSPECTION PER SI 4-58705-12AD, THE UPPER CHORD WAS FOUND COMPLETELY FRACTURED. THE SPAR WEB WAS NOT DAMAGED. HOWEVER, THE FRACTURE OF THE UPPER CHORD APPARENTLY CAUSED A CRACK IN THE SKIN BETWEEN TWO FASTENER HOLES. MAINTEFeb 12, 1997 · N406DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S970201Compressor Case · damagedON TAKEOFF AT 1,000 FEET, NR 1 ENGINE FIRE LIGHT ILLUMINATED AND FIRE BELL OCCURRED. ALL ENGINE INDICATIONS ON TAKEOFF AND FIRE LIGHT WERE NORMAL AND APPROX EQUAL. ALL EMERGENCY CHECK LISTS COMPLETED AND RETURNED TO LAND, ENGINE WAS THEN SHUT DOWN ON FINAL. Feb 1, 1997 · N406DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72S970179Fitting · crackedTHE LT INBOARD STR 3A TENSION TIE FITTING WAS FOUND CRACKED. THE TENSION TIE BOLT HAS BEEN REPLACED IN ACCORDANCE WITH S/B 727-53-0178 WHICH IS REQUIRED BY A.D. 90-06-09. THE FITTING WAS REPLACED PER S/B 727-53-0095.Jan 3, 1997 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S970043Angle · wornFOUND THE LWR LIP OF FWD COWL SUPPORT ANGLE WORN AT THE NR 2 ENG FIREWALL. THE DAMAGE WAS REMOVED AND A NEW FRAME DRILLED AND INSTALLED PER SRM 53-11-0, PG 801.Dec 24, 1996 · N406DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S962101Battery Pack · dischargedRT AFT SLIDE EMERG LITE INOP C/A RPLD BATT PACK AT RACK M957 OPS CHKS GOODSep 11, 1996 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S961986Light · inoperativeON LAYOVER, FOUND LEFT FWD ENTRY DOOR EMERGENCY LIGHT NOT TESTING. REPLACED LIGHT ASSEMBLY (P/N 334701743) AND BATTERIES. LIGHT NOW TESTS OK.Aug 27, 1996 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S961414Torque Box · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF THE AD 94-07-08 WHICH REQUIRES INSPECTION PER SB 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDMay 21, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961293Transverse Beam · crackedCRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA IS SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B.May 21, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961224Skin · crackedA .5 INCH CRACK FROM FASTENER RT ELEVATOR LOWER SKIN JUST INBD OF 3RD FROM OUTBD HINGE. REPAIRED PER SRM 55-20-3.May 20, 1996 · N406DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S961223Skin · crackedA .5 INCH CRACK IN FUSELAGE SKIN AT LWR INBD CORNER OF R-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.May 20, 1996 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S961222Tq Box Web · crackedTORQUE BOX VERTICAL WEB CRACKED 1 INCH AT FASTENER, UPPER ROW OF RIVETS STA 1233 LT LOWER TORQUE BOX. REPAIRED PER M/M 53-11-0 FIG 819.May 20, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961221Door Frame · cracked1 INCH CRACK AT RT AFT SERVICE DOOR FWD FRAME ON FUSE, EXTENDING FROM UPPER STOP PAD CASTING. REPAIRED PER MM 53-13-0.May 20, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960643Bulb · failedEMERGENCY TRACK LIGHTING UNDER SEAT 31D IS OUT. RELAMPED BULB, CKS NORMAL.Mar 23, 1996 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S960175Rib · crackedDURING INSPECTION, NR 8 LE SLAT WAS FOUND WITH INTERNAL RIB NR 3 AND NR 2 CRACKED. REPAIRED PER MM 57-54-0.Nov 21, 1995 · N406DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954060Angle · crackedNR 6 L/E SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER SRM 57-54-0. FOUND AT LETTER CHECK.Oct 19, 1995 · N406DA · Boeing 727232 · Leading Edge Devices
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