N496DA, cancelled Feb 16, 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 = 'N496DA' AND deregistration_id = 'N496DA-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 DL72K001196Battery Pack · dischargedLT AFT BODY FAIRING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK PER M/M. OPS CHK NML.Jun 21, 2000 · N496DA · Boeing 727232 · Emergency LightingSDR DL72K001176Spar · crackedTHE WING CENTER SECTION REAR SPAR WEB WAS FOUND WITH 2 SMALL .25 INCH CRACKS JUST BELOW THE UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF BAC S/B 727-57A0182 AND AD 97-25-15 AND WERE LOCATED AT RBL 5 AND LBL 15. THE CRACKS WERE ROUTED OUT OF THE WEB AND REPAIJun 18, 2000 · N496DA · Boeing 727232 · Wing SparSDR DL72K992232Battery · inoperativeAISLE EMERGENCY LIGHT OUT AT OVERWING EXIT. REPLACED BATTERIES.Oct 7, 1999 · N496DA · Boeing 727232 · Emergency LightingSDR DL72S991239Angle · wornCOWL STRIKER ANGLE WORN LOWER FWD EDGE OF NR 2 ENGINE CUTOUT 5:30 POSITION. REPAIRED PER M/M 53-11-0 PAGE 801.Jun 2, 1999 · N496DA · Boeing 727232 · Engine Cowling SystemSDR DL72S991238Angle · crackedFOUND ON C2 LETTER CK, CRACK AT LOWER BOLT HOLE OF NR 2 SPOILER O/B SPAR ATTACH ANGLE. REPAIRED PER MM 57-42-0.Jun 2, 1999 · N496DA · Boeing 727232 · SpoilersSDR DL72S991096Skin · crackedINTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 360 AND 380. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUMay 17, 1999 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991095Skin · crackedINTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBMay 17, 1999 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990354Frame · crackedSTA 620 FRAME UPPER FLANGE AT RBL 8 HAS CRACK IN RADIUS. CRACK TRIMMED OUT AND REPAIR DOUBLER INSTALLED PER ERA 332727-14. ACTION TAKEN, ERA 332727-14.Feb 5, 1999 · N496DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990243Skin · crackedDURING INSP PER SI 4-74176-12 ON S4R, LAP JOINT CRACK INDICATIONS WERE NOTED FROM BS 481 TO BS 681 APPROX 19 CRACK INDICATIONS WERE NOTED BY HFEC INSP. LAP JOINT CUT OUT AND REPAIRED PER ERA 332726-14.Feb 5, 1999 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990230Rib · crackedMULTIPLE CRACKS FOUND IN THE WING RIB UPPER CHORD AT BS 760 AT R/LBL 70.85 DURING INSPECTIONS PER SI 4-58560-12AD. ALL CRACKS FOUND WERE TYPICAL OF PER SB727-57-0112, R5. ALSO, TOOLING DAMAGE WAS DONE DURING REPAIR INSTALLATION. REPAIRED PER ERA 332730-14ADFeb 4, 1999 · N496DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S982598Spring · brokenIN-FLT RUDDERS BECAME SUPER SENSITIVE, LITTLE OR NO PRESSURE ON RUDDER PEDALS. A/C WANTED TO ROLL LT WITH UPPER 'B' OFF. A/C RESPONSE WAS CLOSE TO NORMAL. FOUND LT SPRING ON RUDDER FEEL/CENTERING UNIT BROKEN.Dec 22, 1998 · N496DA · Boeing 727232 · Rudder Control SystemSDR DL72S982215Frame · crackedA .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME FWD END APPROX 6 BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9 FIG 11.Oct 26, 1998 · N496DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S982214Bracket · crackedFOUND ON C-1 LETTER CK, NR 1 SLAT I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.Oct 26, 1998 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981888Fire Loop · failedENG NR 2 FIRE WARNING CAME ON DURING CLIMB-OUT SHORTLY AFTER T/O, LIGHT STAYED ON AFTER GOING OUT INITIALLY. FOLLOWING THROTTLE BEING REDUCED TO IDLE. SHUT DOWN ENG. BOTH BOTTLES DISCHARGED. REPLACED FIREWALL LOOP, CKS OK. NO FIRE.Sep 11, 1998 · N496DA · Boeing 727232 · Fire DetectionSDR DL72S981345Battery Pack · dischargedAFT AIRSTAIR EMER LIGHT INOP. REPLACED BATT PACK AND LIGHT RACK, OPS OK.Jun 26, 1998 · N496DA · Boeing 727232 · Emergency LightingSDR DL72S971702Angle · crackedFOUND DURING B-1 LETTER CHECK, .25 IN CRACK NR 8 SLAT COVE SKIN ATTACH ANGLE BELOW O/B STOP PAD. REPAIRED PER M/M 57-54-0.Aug 29, 1997 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971701Bracket · crackedFOUND DURING B-1 LETTER CHECK, 2 IN VISIBLE CRACK NR 8 SLAT ACTUATOR ATTACH BRACKET. REPAIRED PER M/M 57-20-21.Aug 29, 1997 · N496DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971700Stiffener · crackedFOUND DURING B-1 LETTER CHECK, INBD VERTICAL STIFFENER CRACKED NR 6 SLAT O/B TRACK BOX. REPAIRED PER M/M 57-20-21.Aug 29, 1997 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971626Megaphone · inoperativeFIRST CLASS MEGAPHONE INOP. REPLACED MEGAPHONE.Aug 20, 1997 · N496DA · Boeing 727232 · Emergency EquipmentSDR DL72S971375Power Supply · inoperativeEMERG EXIT SIGN LIGHTS DON'T ILLUMINATE OVER LT WING EXITS IN TEST. REPLACED PWR SUPPLY RACK AND BATTERY PACK.Jul 13, 1997 · N496DA · Boeing 727232 · Emergency LightingSDR DL72S970178Bulkhead Web · crackedTHE B.S. 1183 BULKHEAD WEB WAS FOUND TO BE CRACKED AT RBL 24. THE CRACK WAS .25 INCH LONG EMANATING FROM A FASTENER HOLE AT WL 178. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY BACO S/B 727-53-171, REV. 2. A REPAIR DOUBLER WAS INSTALLED Jan 28, 1997 · N496DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S970122Window Post · crackedTHE F-N WINDOW POST ON THE RT SIDE OF THE AIRCRAFT WAS FOUND CRACKED DURING A X-RAY INSPECTION PER SI 4-35207-12AD (OPN 8706). THE CRACK IS LOCATED JUST ABOVE THE FIRST ROW OF FASTENERS ABOVE THE LOWER SKIN SPLICE. REV A - UPON NDT INSPECTION, THE CRACK LOCAJan 19, 1997 · N496DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S962779Battery Pack · dischargedRIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND BATTERY RACK FOR RIGHT AFT OVERWING EMERGENCY EXIT LIGHT, LIGHT OPERATES NORMALLY.Dec 27, 1996 · N496DA · Boeing 727232 · Emergency LightingSDR DL72S961497Stiffener · crackedA 1.5 INCH CRACK WING FRONT SPAR VERTICAL STIFFENER AT NR 3 SLAT INBD TRACK CUTOUT. REPLACED SPAR STIFFENER PER M/M 57-20-21.Jun 20, 1996 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961496Web · crackedONE CRACK 48 SECTION TORQUE BOX WEB AT UPPER EDGE STA 1223 LT. REPAIRED PER M/M 53-11-0.Jun 20, 1996 · N496DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960440Switch · defectiveWITH NR 1 AND NR 2 ENGINES RUNNING, STARTED NR 3 ENG AND THEN NR 2 FLAMED OUT. RESET FUEL SHUTOFF VALVE CIRCUIT BREAKER AND STARTED ENG, CONTRACT MTC CKD FUEL S/O VLV OPERATION. CKD ENG FOR FUEL LEAKS. CKD INTAKE/EXHAUST. ALL OK. STARTED ENG SEVERAL TIMESFeb 27, 1996 · N496DA · Boeing 727232 · Engine CrankingSDR DL72S960157Dnlock Switch · failedON GEAR EXTENSION RECEIVED RED NOSE GEAR LIGHT, VISUALLY VERIFIED DOWN AND LOCKED. REPLACED NOSE GEAR DOWNLOCK SWITCH AND NOSE GEAR POSITION SWITCH. ALSO, AS PRECAUTION REPLACED LANDING GEAR ACCESORY UNIT AND OPERATION NORMAL.Jan 17, 1996 · N496DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S960026Stringer · crackedTHE VENT STRINGER 13 ON THE LT WING WAS FOUND WITH A CRACK IN THE STRINGER TO RIB ATTACH TAB AT WING STATION 656.5. DUE TO THE EXTENT OF THE CRACK, THE STOP DRILL REPAIR CALLED OUT IN EO 4-60350-3AD COULD NOT BE ACCOMPLISHED. THE DAMAGED TAB WAS REMOVED AND Dec 22, 1995 · N496DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S960025Skin · crackedTHE FUSELAGE SKIN AT THE RT AFT SERVICE DOOR CUTOUT, LOWER AFT CORNER WAS CUT OUT TO REMOVE DAMAGE AROUND EXISTING NUTPLATE HOLE. THE RESULTANT CUT OUT IS APPROX 2.3 UP/DOWN AND 2.1 FWD/AFT. THE CUT OUT IS THROUGH THE SKIN AND BONDED DOUBLER ONLY. INSTALLEDDec 22, 1995 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960020Frames · crackedTHE LT FS 784 OVERWING EXIT FRAME WAS FOUND WITH A CRACK 1.1 INCH LONG. IT BEGAN AT A FASTENER HOLE ON THE INBD FLANGE AT WL 215 AND RAN HORIZONTALLY FWD AND THROUGH THE BEND RADIUS JUST INTO THE WEB. THIS CRACK IS OUTSIDE THE TYPICAL CRACK AREA AS DEFINED IDec 21, 1995 · N496DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S960022Frame · oversized holesDURING ACCOMPLISHMENT OF EO4-61904-3AD, SEVERAL HOLES IN THE INB'D FRAME FLANGE AT FS 760.95 LT AND RT WERE OVERSIZED BEYOND LIMITS. THE OVERSIZED HOLES WERE REWORKED AND OVERSIZED FASTENERS WERE INSTALLED PER BACO TWX DAL-ATL-95-1340RR DTD 11 DEC 95, DL ERA Dec 12, 1995 · N496DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S954711Stringer · crackedFROM ATL HMV: REF OPN 8602AD HFEC INSP. RT WING OUTER UPPER STRINGER TO RIB INSP. CRACK IND. W.S. 686.50 AFT VENT BOX FWD TAB. CORRECTION: STOP DRILLED CRACK AND INSTALLED REPAIR PER MM 57-13-0, FIG 804.Dec 11, 1995 · N496DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S954699Te Skin · separatingAT HMV, TRAILING EDGE OF LEFT ELEVATOR SEPARATED IN SEVERAL PLACES. REPAIRED PER MM 55-20-0 PG 801.Dec 8, 1995 · N496DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S960376Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND IN SCATTERED LOCATIONS FROM STA 680 TO 720, BETWEEN S-26L AND 26R. ALSO, THERE WERE THREE EXISTING REPAIR DOUBLERS ON THE LOWER SKIN IN THE SAME AREA. IN ACCORDANCE WITH BAC/O S/B 727-53A203, RV 2, THE EXISTING EXTERNALDec 1, 1995 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954807Floorbeam · corrodedAT HMV, CORROSION ON FS 344 FLOORBEAM UPPER CAP LBL 35R BL 25 C53-224-01.05. REPAIRED PER SRM 53-10-8 FIG 10.Nov 29, 1995 · N496DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954666Bracket · crackedBRACKET CRACKED: NR 1 LE FLAP ACTUATOR INBOARD BRACKET ON FRONT SPAR IS CRACKED IN LOWER FORWARD RADIUS. REMOVED BRACKET. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER MM 57-20-21, PG 811.Nov 29, 1995 · N496DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S954659Inlet Skin · damagedNR 2 ENGINE INLET EXT SKIN RIGHT SIDE TEMPORARY REPAIR DOUBLER AT LWR AFT CUTOUT FOR PANEL 9516. MANUFACTURED NEW DOUBLER PER M/M 54-30-0. INSTALLED REPAIR PER M/M 54-30-0.Nov 27, 1995 · N496DA · Boeing 727232 · Engine Cowling SystemSDR DL72S954622Stringer · damagedFROM ATL/HMV - STR 29L HAS TOOLING DAMAGE AT STA 1000. CORRECTION: FORMED REPAIR DOUBLER AND BEGAN DRILLING DOUBLER. ROUTED OUT DAMAGE, FABRICATED FILLER PER M/M 53-12-0, FIG. 806. OK TO INSTALL REPAIR. INSTALLED DOUBLER PER M/M 53-12-0.Nov 27, 1995 · N496DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S954698Angle · damagedUPON HMV, FOUND NR 2 ENG PYLON CIRCUMFERENTIAL ANGLE FOR MOUNTING SURFACE OF FWD COWL HAS TEMPORARY REPAIR INSTALLED. FABRICATED AND INSTALLED NEW ANGLE PER MM 53-11-0.Nov 23, 1995 · N496DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S954658Inlet Skin · damagedTIME LIMITED REPAIR INSTALLED AT NR 2 ENGINE INLET DUCT HOUSING RT SKIN AT LOWER AFT CORNER OF ACCESS PLATE 9516 CUTOUT REF NR 86 PER M/M 54-30-0 PG 802. REPAIRED PER M/M 54-30-0 REF NR 861.Nov 22, 1995 · N496DA · Boeing 727232 · Engine Cowling SystemSDR DL72S953982Door · crackedA FIVE INCH CRACK WAS FOUND IN THE R-1 DOOR. THE CRACK EXTENDED FROM THE UPPER AFT CORNER DOWN THE AFT FRAME. REPAIR INCLUDED DOOR REPLACEMENT.Oct 12, 1995 · N496DA · Boeing 727232 · Service DoorsSDR DL72S960540Skin · crackedUPON SHOP INSPECTION, FOUND OUTER SKIN AND FRAME CRACKED AT UPPER FORWARD CORNER. REPAIRED SKIN PER SRM 52-00-3, FIG 4 AND REPAIRED FRAME PER MM 52-12-0, FIG 805, FOR R-1 SERVICE DOOR.Oct 10, 1995 · N496DA · Boeing 727232 · Galley DoorsSDR DL72S953035Angle · crackedNR 7 SLAT COVE SKIN ANGLE DOUBLER CRACKED AT I/B STOP PAD. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.Jul 11, 1995 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953034Angle · crackedNR 7 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.Jul 11, 1995 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952464Fan · shortedDURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN AND FLIGHT DECK. ODOR STOPPED AFTER SECURING GASPER FAN. GASPER FAN WAS FOUND SHORTED. REPLACED FAN, OPERATION NORMAL.Jun 2, 1995 · N496DA · Boeing 727232 · Air Distribution FanSDR DL72S951685Skin · wornDURING INSPECTION, LEFT WING AILERON WAS FOUND WITH WEAR DAMAGE TO THE LOWER SKIN. REPAIRED PER SRM 57-51-0.Apr 25, 1995 · N496DA · Boeing 727232 · AileronsSDR DL72S951684Skin · wornDURING SHOP INSPECTION, LEFT WING AILERON WAS FOUND WITH DAMAGE TO UPPER SKIN. SPLICED IN NEW SECTION OF SKIN PER SRM 57-50-1.Apr 25, 1995 · N496DA · Boeing 727232 · AileronsSDR DL72S951621Fitting · corrodedNR 3 MID FLAP I/B CARRIAGE FITTING UPPER THRUST BEARING RETAINER BOLT AND HOLES HAVE CORROSION. FOUND AT SHOP INSPECTION. REAM HOLES TO .312 AND INSTALLED BUSHING.Apr 20, 1995 · N496DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950997Bearing Mount · corrodedLT MLG FWD TRUNNION BEARING MOUNT CORRODED ON INBD FACES AND ALL FOUR BORES.Mar 10, 1995 · N496DA · Boeing 727232 · Main Landing Gear Attach SectionSDR DL72S950525Skin · damagedDURING SHOP INSPECTION THE LEFT WING NR 1 FORE FLAP WAS FOUND WITH THE LEADING EDGE SKIN DAMAGED AT 7 INCHES TO 12 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 57-50-4.Feb 6, 1995 · N496DA · Boeing 727232 · Trailing Edge Flaps
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