N407DA, cancelled Jan 31, 2001

Service difficulty reports · 51

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 = 'N407DA' AND deregistration_id = 'N407DA-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 DL72S002028Engine · bird strikeDURING TAKEOFF, A/C SUFFERED BIRD STRIKE, FODDING OUT NR 1 ENGINE. REPLACED ENGINE.Oct 16, 2000 · N407DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S001699Light · inoperativeON L/O, FOUND L-2 OVER DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.Sep 3, 2000 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S001169Battery · dischargedAFT CABIN DOOR OVERHEAD EMERG LIGHT INOP. C/W REPLACED BATTERIES, OPS NOW OK.Jun 16, 2000 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S000300Engine · failedRIGHT ENGINE OIL PRESS HIGH WITH NR 3 OIL BYPASS LIGHT. ENGINE SUBSEQUENTLY FAILED. REPLACED ENGINE.Feb 13, 2000 · N407DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S992706Bracket · crackedA 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21.Dec 10, 1999 · N407DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S992688Light · inoperativeFLIGHT DECK EMERGENCY PORTABLE EXIT IDENTIFIER LIGHT WOULD NOT TEST. REPLACED BATTERY PACK, OP CKS GOOD.Dec 9, 1999 · N407DA · Boeing 727232 · Flight Compartment LightingSDR DL72S991433Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE JOINT. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAJun 23, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991178Csd · required serviceCSD LOW PRESSURE LIGHT FLICKERED AND THEN STAYED ON, LOST MAIN AC NR 2. FOUND CSD LOW. SERVICED CSD, RAN ENG AND NO LEAKS NOTED.May 25, 1999 · N407DA · Boeing 727232 · Alternator-Generator DriveSDR DL72S991124Web · crackedTPA LTR CHK B-2, LT VERT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0 PG 828, LT VERT TORQUE BOX WEB LWR LIGHTENING HOLE .375 INCH CRACK AT UPPER END AND A .625 INCH CRACK ON LWR END STA 1226. REPAIRED PER MM May 20, 1999 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991122Frame · crackedFOUND AT B-2 LETTER CHECK, LT AFT ENTRYWAY DOOR FRAME HAS .375 INCH VISIBLE CRACK. REPAIRED PER SRM 53-10-9.May 20, 1999 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990588Skin · 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 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REMar 15, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990546Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 500 AND 520. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRMar 13, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990566Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 400 AND 420. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990565Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 TO 740 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 720 AND 720A. THE CRACKED AREA WAS ROUTED OUT AND REPAIRED PEMar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990562Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B727 SRM Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990348Pump · failedB-SYSTEM HYD WENT TO 0, FOLLOWED PROCEDURES. WHEN GEAR EXTENDED HYD PRESS WENT TO 1700 PSI. OPERATED BRAKE INTERCONNECT, USED PNEUMATIC BRAKES TO STOP. TOWED ACFT TO GATE FROM RUNWAY. FOUND NR 2 B-HYD PUMP LEAKING. REPLACED SAME AND FITTINGS, LEAK CKS OK.Feb 21, 1999 · N407DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72S982564Actuator · leakingAIRCRAFT LOST 'A SYSTEM HYDRAULICS WHILE TAXING TO THE GATE AFTER LANDING IN CVG. MTC FOUND THAT THE NUMBER 7 LEADING EDGE SLAT ACTUATOR HAD FAILED. REPLACED ACTUATOR AND BOTH HYDRAULIC PUMPS.Dec 15, 1998 · N407DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S982154Stringer · crackedS18 TAB ON THE RT WING VENT BOX AT WS 171.5 WAS FOUND CRACKED. ADDITIONAL DAMAGE INCURRED WHILE INSTALLING THE SRM REPAIR. REPAIRED PER ERA 332288-14.Oct 16, 1998 · N407DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S982151Stringer · crackedFUSE STR 29R WAS FOUND CRACKED AT FS 950E. REPAIRED PER ERA 332275-14.Oct 16, 1998 · N407DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S982150Stringer · crackedRT WING UPPER SURFACE S18 AT WS 304 WAS FOUND CRACKED, REQUIRING A 2.5 INCH CUTOUT. REPAIRED PER ERA 332341-14.Oct 16, 1998 · N407DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S982149Frame · crackedCRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED PER ERA 332283-14AD.Oct 16, 1998 · N407DA · Boeing 727232 · Wing SparSDR DL72S982139Skin · crackedFUSELAGE SKIN WAS FOUND WITH A TIME LIMITED EXT REPAIR DOUBLER FOR A CRACK IN THE SKIN AT FS 294.5, BELOW S15R. THE TIME LIMITED REPAIR WAS REMOVED AND ADDITIONAL DAMAGE FOUND. REPAIRED PER ERA 332347-14.Oct 14, 1998 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982094Skin · crackedFUSE SKIN HAD A TIME LIMITED REPAIR REMOVED AT FS294, S15R; AND ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332347-14.Oct 8, 1998 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982085Spar · damagedDURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO TOOLING DAMAGE. REPAIRED PER ERA 332359-14AD.Oct 8, 1998 · N407DA · Boeing 727232 · Wing SparSDR DL72S982063Frame · crackedA CRACK WAS FOUND IN THE FS 784 RT FRAME INBD FLANGE. THE CRACK PROPAGATES FROM THE FIRST FASTENER HOLE ABOVE THE FLOOR LINE. REPAIRED PER ERA 300891-14AD, REV A.Oct 6, 1998 · N407DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S982112Track · corrodedCORROSION FOUND AT FWD ATTACH LUG FACES AND BORE AND TO MLG BEAM ATTACH HOLES. BUSH LUG HOLES AND INSTALLED SPLICE PLATE REPAIR FOR MLG BEAM ATTACH HOLES.Oct 1, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982318Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 18 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982316Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982315Angle · repairedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.Sep 30, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982053Rib · crackedINBOARD AFT CLOSE OUT RIB CRACKED AT LWR AFT CORNER. DAMAG REPAIRED PER MM 57-52-0 ON SHOP ORDER 582612.Sep 29, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981998Pin · corrodedBORE CORRODED LEFT AFT BTL PIN IS CORRODED. CLEANED CORROSION PER SRM 53-40-1 FIG 4 DAMAGE WITHIN LIMITS OK TO TREAT. TREATED BORE PER PS 900-2-4-1 NO O2.Sep 25, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S982218Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 21 AND 34 FR OM IB END OF FLAP. THE ANGLE WAS REPAIRED BY SPLICING IN A NE W SECTION OF ANGLEPER MM 57-52-0, FIG. 802.Sep 23, 1998 · N407DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S982060Support · wornITEM: NR 2 ENG FWD COWL SUPPORT RING IS WORN AT THE 9 O'CLOCK POS LOC ON FUSELAGE. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER PER M/M 53-11-0 PG 801. OK TO INSTALL. INSTALLED REPAIR PER M/M 53-11-0 PG 801.Sep 23, 1998 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981764Battery Pack · dischargedON L/O, AFT OVERWING ESCAPE LIGHT INOP. REPLACED BATTERY PACK.Aug 24, 1998 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S971562Control Mech · malfunctionedON APPROACH OUTBD FLAPS WOULD NOT EXTEND. MADE MISSED APPROACH. FLAPS EXTENDED NORMAL ON SECOND ATTEMP. FLAP OPERATIONAL TEST NORMAL ON GROUND AND VISUALLY INSPECTED NO DEFECT FOUND.Aug 8, 1997 · N407DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S970745Sequence Valve · damagedAFTER T/O DURING GEAR RETRACTION, SYS-A PRESSURE/QUANTITY WENT TO 0, A-SYSTEM PUMPS TURNED OFF 1 MIN LATER. CASTING DAMAGED ON LT GEAR DOOR SEQUENCE VALVE. REPLACED SAME.Apr 22, 1997 · N407DA · Boeing 727232 · Landing Gear Door Retract SectionSDR DL72S970292Skin · corrodedCORROSION REMOVED AROUND RADIO ALTIMETER ANTENNA CUTOUT BTWN FS 520 TO 540, STR 28L AND 29R. INTERNAL REPAIR WILL BE INSTALLED. ADDITIONAL DAMAGE WAS FOUND AT LETTER CHECK ON 041297. CUT OUT 2 IN BY 2.625 IN AT FS 540, STR 28L. A SEPARATE REPAIR WAS INSTALFeb 12, 1997 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S962654Power Supply · inoperativeLEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, OPS CHECKS GOOD.Dec 6, 1996 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S962437Bracket · crackedFOUND ON F1 LETTER CK, NR 1 SLAT ACTUATOR ATTACH BRACKETS CRACKED INBD AND OUTBD SIDES. REPAIRED PER MM 57-20-21.Nov 2, 1996 · N407DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S961425Swivel · leakingDURING CLIMB, A-HYD QTY WENT TO ZERO AND A PUMP LIGHT FLICKERED, RETURNED TO SHV. REPLACED CASE DRAIN FILTERS, NO METAL FOUND. FOUND THE NR 4 SLAT ACTUATOR SWIVEL LEAKING. REPLACED O-RING, REFILLED HYD SYS, RAN ENGINES AND B-PUMPS, OPERATED ALL FLT CONTROLSJun 12, 1996 · N407DA · Boeing 727232 · Hydraulic System, MainSDR DL72S961145Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECITON AREA SPECIFIED BY BOEING SERVICE BULLApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960876Skin · corrosionCORROSION DAMAGE WAS REMOVED FROM AROUND THE HOLE CUTOUT FOR THE RADIO ALTIMETER ANTENNA BETWEEN STATION 520 AND STATION 540, BETWEEN STRINGER 28 LEFT AND STRINGER 29 RIGHT. THE SKIN IS MACHINED CLAD 2024-T3 SHEET WITH A LOCAL THICKNESS OF 0.090 THICK. AN INApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960875Skin · corrosionCORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING STRINGER SPLICE AT BS 490 AND A NEW SPLICE BEING INSTALLED AT BS 510 PER B727 SRM. THE SKIN IS MANUFACTURED FROM MACHINED CLAD 2024-T3 WITH AApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960843Angle · crackedFOUND ON E-2 LETTER CHECK, LWR T-ANGLE CRACKED AT AFT HINGE FOR LWR FUS PANEL 3448R. REPAIRED PER M/M 53-30-1 PG 807.Apr 11, 1996 · N407DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960512Light · looseON PRE-FLIGHT, FOUND SECTION OF TRACK LIGHTING LOOSE WITH EXPOSED WIRING. REPAIRED WIRING SECURED TRACK, OPERATION NORMAL.Mar 4, 1996 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S960291Sensor · dirtyON GEAR RETRACTION, RED RT GEAR AND GREEN RT GEAR LIGHTS REMAINED ON. COMPLETED LDG GEAR RETRACTION MALFUNCTION CHECK LIST, BOTH LIGHTS REMAINED ON. ABOUT 40 SECONDS LATER, BOTH LIGHTS OUT. CHECKED AND CLEANED RIGHT MAIN LANDING GEAR DOWNLOCK, SENSOR OPERATFeb 6, 1996 · N407DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S960024Skin · crackedA SKIN CRACK, 1.75 INCH BY 2 INCH WAS DISCOVERED BETWEEN STRINGER 27R AND 28R, FS 481. THE PREVIOUS REPAIR ON THIS SECTION MEASURED 5.5 INCH BY 13 INCH. THE REPAIRS WERE INCORPORATED INTO ONE REPAIR AFTER REMOVAL OF PREVIOUS REPAIR. THIS ER/A SUPERCEDES ER/Dec 28, 1995 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954791Stringer · crackedFORWARD LOWER FUSELAGE BS-480 STRINGER 28R SKIN BULGING AND CRACKED. REPAIRED PER DL ERA 302938-14.Dec 20, 1995 · N407DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S954747Battery Pack · dischargedEMERGENCY LIGHT OUT LOWER RT OVERWING FAIRING. REPLACED EMERGENCY LIGHT BATTERY PACK. CKS NORMAL.Dec 19, 1995 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S954709Cooling Valve · failedDURING CLIMB AND LEVEL AT FL 240, WERE UNABLE TO MAINTAIN, CABIN SLOWEST RATE OF ASSENT WAS 700 FPM. DESCENDED AND RETURNED TO JFK. FOUND EQUIPMENT COOLING VALVE STUCK OPEN. REPLACED VALVE. RETURNED TO SERVICE.Dec 15, 1995 · N407DA · Boeing 727232 · Cabin Cooling System
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