N499DA, cancelled Aug 15, 2013

Service difficulty reports · 56

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 = 'N499DA' AND deregistration_id = 'N499DA-2013-08-15'
  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 DL72S001856Bulb · failedR-1 DOOR AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R-1 AFT EXTERIOR LIGHT, OPS CKS GOOD.Sep 21, 2000 · N499DA · Boeing 727232 · Exterior LightingSDR DL72S001068Coalescer Bag · dirtySMOKE SMELL IN COCKPIT AND CABIN. CHANGED COALESCER BAGS. CHECKED SYSTEM. SUSPECT FOREST FIRE.May 31, 2000 · N499DA · Boeing 727232 · Humidity Control SystemSDR DL72S000326Mount · crackedCRACKED HOLE WHILE ACCOMPLISHING REPETITIVE INSPECTIONS OF THE FWD ENGINE MOUNT BOLT HOLES ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICATION WAS FOUND IN ONE HOLE (REF HOLE F OF BAC S/B 727-54A0010). THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND Feb 17, 2000 · N499DA · Boeing 727232 · Engine Mount SectionSDR DL72S992376Angle · corrodedNR 2 ENG AFT MOUNT LOWER CHORD WAS CORRODED. REPLACED CHORD.Oct 27, 1999 · N499DA · Boeing 727232 · Engine Mount SectionSDR DL72S992375Angle · corrodedNR 2 ENG AFT MOUNT SUPPORT ANGLE LEFT HAND WAS CORRODED. REPLACED ANGLE.Oct 27, 1999 · N499DA · Boeing 727232 · Engine Mount SectionSDR DL72S992462Wire · 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 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SER- VICE LETTER 727-SLOct 25, 1999 · N499DA · Boeing 727232 · Electrical Power System WiringSDR DL72S990832Oil Filter · contaminatedNR 3 OIL FILTER BYPASS LIGHT CAME ON AT 17K FT. OIL PRESS TEMP AND QTY ARE GOOD POM PROCEDURES COMPLIED WITH. LIGHT REMAINED ON AND NR 3 ENGINE WAS SHUT DOWN IAW POM PROCEDURES. REMOVED FILTER, FOUND CARBON BUILDUP. INSTALLED NEW FILTER AND RAN ENG PER MM.Apr 13, 1999 · N499DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S990772Controller · failedDURING CLIMB-OUT, CABIN ALT BEGAN TO CLIMB AT 1000 FT, BOTH PACKS APPEARED TO OP. NORMAL CABIN CLIMBED TO AN ALT OF 12,000 AND DESCENT BEGAN. POM PREC FOLLOWED STBY AND DC HAD NEG EFFECT TO CLOSE OUTFLOW FURTHER CARGO V. CLOSED LIGHT ILLUMINATED ENTIRE TIMEApr 8, 1999 · N499DA · Boeing 727232 · Cabin Pressure ControllerSDR DL72S990568Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT ALONG ITS ENTIRE LENGTH AMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990541Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 36 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990540Skin · 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 CONFIRMED 69 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENTIRE LENGTH OF THE PAMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990411Oil Filter · dirtyNR 3 ENGINE OIL FILTER INDICATED BYPASS IN CRUISE FL280. PRECAUTIONARY, SHUTDOWN PROCEDURE ACCOMPLISHED. REPLACED OIL FILTER, LOP SWITCH, FILTER BYPASS SWITCH, DRAINED OIL RES, PERFORMED OIL BREATHER PRESS CK TEST 'Z' PER PFHB AND OPN OK. REPLACED OIL FILTEFeb 26, 1999 · N499DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S982454Filter · cloggedNR 3 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. THE LIGHT EXTINGUISHED AT 45 TO 50 PERCENT N1 ALL ON SHORT FINAL. LIGHT RE-ILLUMINATED AT IDLE. PER T/S CHART REPLACED FILTER, PERFORMED BREATHER PRESS CK, CKS GOOD. REPLACED FILTER, OK FOR SERVICE.Nov 29, 1998 · N499DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S981959Skin · crackedTHE R1 DOOR SURROUND SKIN ASSY WAS FOUND WITH A 2.25 INCH TYPICAL CRACK IN THE BEAR STRAP AT THE UPPER HINGE CUTOUT. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0136, REV 3. THE REPAIR WAS DOCUMENTED PER ER/A 365667-14. NOTE: THE BEAR STRAP HAD THE S/B 53-01Sep 18, 1998 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981049Bulb · failedEMERGENCY LIGHT OUT AT RIGHT WING ROOT FAIRING. RELAMPED.May 17, 1998 · N499DA · Boeing 727232 · Exterior LightingSDR DL72S980368Battery Pack · dischargedON LAYOVER CK, FOUND LT OVERWING EMERGENCY EXIT SIGN NOT ILLUMINATING. REPLACED BATTERY PACK.Feb 11, 1998 · N499DA · Boeing 727232 · Emergency LightingSDR DL72S980317Controller · malfunctionedAT FL 2500 WITH ONE PACK RUNNING, CABIN STARTED TO CLIMB, DIVERTED INTO DFW. MAINTENANCE IN PROGRESS. RT PACK ON PREVIOUS MCO. RT PACK REPLACED ACM. CKS GOOD. LT PACK REPLACED 35 DEGREE SENSOR AND 35 DEGREE CONTROLLER. PRESSURIZED A/C USING BOTH PACFeb 5, 1998 · N499DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S972713Web · crackedA 1 INCH CRACK IN LIGHTENING HOLE TORQUE BOX WEB RT SIDE STA 1223. REPAIRED PER MM 53-11-0 PG 828.Dec 23, 1997 · N499DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972250Light · inoperativeDURING SVC CHK AD9 FOUND L1 AND L2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSYS. OPS NML.Nov 4, 1997 · N499DA · Boeing 727232 · Emergency LightingSDR DL72S971715Relay · inoperativeEMERGENCY EXIT LTS AND EMERG PATH LTS CAME ON DURING CLIMB-OUT. COCKPIT SW IN ARMED POS AND CABIN SW IN NORM. REPLACED R70 CHARGING RELAY.Sep 1, 1997 · N499DA · Boeing 727232 · Emergency LightingSDR DL72S961018Tank Plate · leakingFUEL LEAK LEFT WING, IN-FLIGHT. REPORTED BY PASSENGER. DIVERTED ATL. FOUND FIFTH TANK PLATE FROM LT WING TIP LEAKING FUEL. SECURED TANK PLATE. NO LEAKS NOTED.Apr 29, 1996 · N499DA · Boeing 727232 · Fuel StorageSDR DL72S960634Angle · crackedDURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960631Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960630Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960629Angle · crackedFOUND DURING A-1 LETTER CHECK, .75 INCH CRACK NR 4 KRUEGER FLAP ACTUATOR MOUNT BOX AT UPPER I/B FWD CORNER. REPAIRED PER M/M 57-20-21.Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960178Cable · brokenLEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. REPLACED DOOR SLIDE PER M/M 25-60-15.Jan 23, 1996 · N499DA · Boeing 727232 · Escape SlideSDR DL72S953903Spar · crackedAFT SPAR CHORD WAS FOUND CRACKED 33, 54 AND 61 FROM IB END OF NR 3 MIDFLAP. THE DAMAGED SECTION WAS REPLACED AND SPLICED IN PER MM 57-50-00.Sep 25, 1995 · N499DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953636Angle · crackedNR 6 SLAT, .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A.Sep 7, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953669Rib · crackedNR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953633Rib · crackedDURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953602Skin · crackedDURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.Sep 3, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953586Stringer · crackedWING UPPER STRINGER TO RIB WS 686.5 STRINGER NR 5 IS CRACKED. STOP DRILLED CRACK PER M/M 57-13-0 PG 802. FABRICATED REPAIR PARTS AND INSTALLED PER M/M 57-13-00 PG 802.Aug 29, 1995 · N499DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S953666Attach Lug · brokenAT HMV, FWD ENTRY DOOR UPPER GATE STOP ROD ATTACH LUG FOUND BROKEN. REPAIRED PER 52-10-2 FIG 10.Aug 22, 1995 · N499DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S953578Act Attach · crackedNR 6 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.Aug 22, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953855Spar · crackedDURING SHOP INSPECTION, NR 2 MIDFLAP HAS A CRACKED AFT SPAR CHORD 22 FT AND 53 FROM I/B END OF FLAP AND A CRACK AT I/B ACTUATOR CUTOUT. SPLICED IN NEW SECTIONS OF AFT SPAR CHORD AND INSTALLED DOUBLERS, PER MM 57-52-00 PG 807.Aug 21, 1995 · N499DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953639Skin · crackedNR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0.Aug 21, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953577Act Attach · crackedNR 5 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LWR O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. CRACK WAS FOUND AT HMV.Aug 21, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953668Rib · crackedDURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953649Web · crackedDURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953637Skin · wornNR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953632Angle · crackedUPON HMV, FOUND .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953610Rib · crackedDURING HMV, FOUND NR 4 SLAT RIB CRACKED .5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953591Rib · crackedDURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814.Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953587Stringer · crackedLEFT WING UPPER STRINGER TO RIB WS 629 STRINGER NR 3 CRACKED. FABRICATED AND INSTALLED PARTS PER M/M 57-13-00 FIG 804. CRACK WAS FOUND AT HMV.Aug 20, 1995 · N499DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S953497Seat Track · corrodedSEAT TRACK AFT CABIN CORRODED RT SIDE OB TRACK STA 1090. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED CORROSION BETWEEN STA 1090 TO 1110 WITHIN LIMITS PER SRM 53-10-1 FIG 1. REMOVED PIGTAIL STA 1110 TO 1130, BEGAN REPLACEMAug 20, 1995 · N499DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S953496Seat Track · corrodedFWD CABIN SEAT TRACK, RT SIDE STA 400 OB, AND 470 OB, REMOVED CORR PER SRM 51-10-6. STA 470 WITHIN LIMITS PER SRM 53-10-1 FIG 3, STA 400 OUT OF LIMITS PER SRM 53-10-1 FIG 3. ALSO, FS 400 SHOWS EVIDENCE OF PREVIOUS CORROSION REMOVAL. PREPARED NEW SEAT TRACK Aug 20, 1995 · N499DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S953640Blkhd Bolts · wornDURING HMV, FOUND MOUNT BOLTS WORN FWD CARGO BULKHEAD AT FS 720D VERTICAL SUPPORT BEAMS ATTACH POINT AT STR 26L AND 26R. REPAIRED PER SRM 53-10-9 FIG 9.Aug 19, 1995 · N499DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953638Skin · crackedDURING HMV, FOUND NR 5 SLAT RIVET MISSING IN LWR T/E SKIN O/B OF O/B TRACK. SKIN WORN AT FENCE ATTACHMENT AND WORN THIN AT BOLT HOLE ON LWR T/E SKIN. REF NR CARD 1148, BURNISHED WORN AREA. DIE PENETRANT INSP SHOWS CRACK AT 3 FENCE ATTACH HOLES. FABRICATED Aug 19, 1995 · N499DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953658Fitting · looseTHE NR 2 SPOILER ACTUATOR SUPPORT FITTING LOWER TWO ATTACH BOLTS, AT REAR SPAR ARE VERY LOOSE IN MOUNT LUGS. REPAIRED PER MM 57-42-00 PG 804 STEP D.Aug 18, 1995 · N499DA · Boeing 727232 · Wing, Control Surface Attach FittingsSDR DL72S953550Actuator · looseITEM: SPOILER ACTUATOR SUPPORT FITTING LOOSE INBD LOWER BOLT AT NR 13 SPOILER. REPAIRED FITTING PER MM 57-42-0 REV D.Aug 18, 1995 · N499DA · Boeing 727232 · Drag Control Actuator
Back to N499DA, cancelled Aug 15, 2013