N517DA, cancelled Dec 19, 2002

Service difficulty reports · 67

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 = 'N517DA' AND deregistration_id = 'N517DA-2002-12-19'
  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 DL72S020528Skin · crackedFUSELAGE / SKIN / STRG. 4L / FS 360-480 / SKIN LAP SPLICE : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 & 480 REVEALED CRACK INDICATIONS IN THE LOWER FASTENER ROW OF THE May 8, 2002 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S020527Skin · crackedFUSELAGE / SKIN / STRG. 4L / FS 1030-1110 / SKIN LAP JOINT: CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 1030 & 110 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED A TOTAL OFMay 8, 2002 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S020426Angle · crackedA .375 INCH CRACK AT LWR SLAT COVE SKIN ATTACH ANGLE BELOW NR 6 SLAT TAI DUCT. REPAIRED PER M/M 57-54-000-8.Apr 11, 2002 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S020051Battery Pack · dischargedMCO- AFT F/A FLASHLIGHT INOP. REPLACED BATTERY PACK AND TAMPER STRAP.Jan 15, 2002 · N517DA · Boeing 727232 · Emergency EquipmentSDR DL72S011531Web · crackedCRACK AT UPPER FASTNER VERTICAL WEB L/H SIDE STA 1223 REPAIRED PER M/M 57-11-000-8Sep 14, 2001 · N517DA · Boeing 727232 · Fuselage Structure (General)SDR DL72S011044Light · inoperativeAFT LEFT EXTERIOR EMERGENCY LIGHT INOP WHILE TESTING, DURING LAYOVER CHECK. REPLACED LIGHT RACK.Jun 22, 2001 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S010189Web · crackedA .375 INCH CRACK AT UPPER LIGHTENING HOLE RT LOWER TORQUE BOX, VERTICAL WEB AFT OF STA 1223 IN 48 SECTION. REPAIR PER MM 53-11-000-8.Feb 1, 2001 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S002285Skin · crackedFUSELAGE / SKIN / FS 360-380 / STRG. 4R / SKIN LAP SPLICE : CRACK REPAIR. LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP SPLICE INDICATED A CRACK. INTERNAL MFEC INSPECTION OF THE SKIN LAP CONFIRMED A SINGLE CRACKED FASTENER HOLE IN THE LOWER FASTENER ROWNov 22, 2000 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000835Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 REVEALED A CRACK INDICATION IN THE LOWER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION OF THE ENTIRE LAP CONFIRMED A SINGLE CRACKED FASTENER HOLE BETWEEN FS 640 & 660. THE DAMAGED SECApr 25, 2000 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S992632Angle · crackedFOUND ON D1 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B STOP PAD. REPAIRED PER MM 57-54-0.Dec 1, 1999 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S992187Light · inopEMERGENCY AISLE LT AT ROW 31 INOP. REPLACED LT ASSY, OPS NML.Oct 1, 1999 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S992007Bleed Valve · malfunctionedAFTER TAKEOFF, (NORMAL POWER) THE ENG 2 APU BLEED HIGH TEMP LIGHT ILLUMINATED. THE NR 2 THROTTLE WAS RETARDED AND THE LIGHT WENT OUT. DISCUSSED WITH ATL/MCC AND FLIGHT RETURNED TO SLC. LIGHT TESTED GOOD. REPLACED NR 2 ENG BLEED VALVE CB, CKS GOOD.Sep 9, 1999 · N517DA · Boeing 727232 · Compressor Bleed ValveSDR DL72S991760Overheat Loop · out of positionAT APPROX 100 FEET AFE, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. REPLACED FIRE/OVERHEAT DETECTION MODULE. REPLACED KEEL BEAM LOOP M367 REPOSITIONED LOOP M 365 NEAR RT PURGE SHUTOFF VALVE. RAN ALL 3 ENGS AT T/O EPR. AT T/O EPR AFT BODY OVERHEAT CHKS NAug 6, 1999 · N517DA · Boeing 727232 · Overheat DetectionSDR DL72S990188Light · inopEMERGENCY PATH LIGHT OUT ROW 26DEF. REPAIRED EMERGENCY PATH LIGHTS ROW 26DEF.Jan 29, 1999 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S982557Wire · damagedEMERGENCY LIGHTS IN F/C AND ENTRY DOOR AREAS INOP. FOUND WIRES TO 1L DOOR EXIT LIGHT PINCHED BEHIND SIDEWALL AREA. REPAIRED AND REPLACED BATT AND RACK DUE BLOWN FUSES.Dec 12, 1998 · N517DA · Boeing 727232 · Light System WiringSDR DL72S982487Angle · corrodedFOUND CORROSION ON HEAVYWEIGHT HUSH-KIT MOD ON RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE IN EXCEEDANCE OF MFG MINIMUM ALLOWABLE TOLERANCES. REPLACED RT CHORD ANGLE WITH NEW MFG PART.Dec 1, 1998 · N517DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S981992Power Supply · inoperativeDURING L/O, FOUND FLOOR TRACK LIGHTS FROM SEAT 27-36 INOP. REPLACED EMERGENCY LIGHTS PWR SUPPLY DAL (P/N 337701962) (S/N 0474) OFF, (S/N 1881) ON.Sep 26, 1998 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S981967Angle · crackedNR 6 L/E FLAP ACT ATTACH ANGLE CRACKED O/B LOWER RADIUS. REPAIRED PER MM 57-20-21 PG 811.Sep 22, 1998 · N517DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981406Door · not closedAIRCRAFT WOULD NOT PRESSURIZE IN CLIMB. AIRCRAFT AIR TURN BACK TO ATL. FOUND R-1 DOOR NOT FULLY STOWED IN FUSELAGE. INSPECTED DOOR AND CHECKED FOR PROPER OPERATION, CLOSED DOOR. CHKS OK.Jul 5, 1998 · N517DA · Boeing 727232 · Service DoorsSDR DL72S980505Skin · crackedTHE FUSELAGE SKIN AND UNDERLYING DOUBLER AND BEAR STRAP WERE FOUND WITH A 3.5 INCH CRACK IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER AND TRIPLER PER ER/A 364131-14, REV A.Feb 27, 1998 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S980486Web · crackedWHILE BUYING BACK N/R 52 FOUND LT TORQUE BOX VERTICAL WEB UPPER LIGHTENING HOLE STA 1243 CRACKED AT PREVIOUS ROUT OUT. REPAIRED PER M/M 53-11-0 PG 828.Feb 26, 1998 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980480Angle · crackedFOUND DURING B-2 LETTER CHECK, NR 2 SLAT COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.Feb 26, 1998 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S980479Bracket · crackedFOUND DURING B-2 LETTER CHECK, NR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.Feb 26, 1998 · N517DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971712Actuator · leakingLOST A-SYSTEM HYDRAULIC ON FLAP RETRACTION. FOUND RT MAIN GEAR DOOR ACTUATOR HOUSING CRACKED. REPLACED RT GEAR DOOR ACT, LEAK CKS OK.Aug 31, 1997 · N517DA · Boeing 727232 · Landing Gear Door ActuatorSDR DL72S971483Skin · crackedTHE LT AND RT SKINS OF THE VERTICAL STABILIZER WERE FOUND CRACKED AT THE FRONT SPAR JUST ABOVE THE FUSLEAGE CREASE. ON THE LT SIDE, A TOTAL OF FOUR FASTENER HOLES HAVE CRACKS EMANATING FROM THEM. TWO ARE IN THE TYPICAL LOCATION OF THE SRM 55-30-3, FIGURE 7 RJul 25, 1997 · N517DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S971620Chord · crackedNR 3 MIDFLAP WAS FOUND TO HAVE A CRACKED AFT LOWER CHORD. THIS FLAP CHORD WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0.Jul 15, 1997 · N517DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971362Skin · loose fastenersFASTENERS PULLING THROUGH UPPER SKIN. SPLICED SKIN PER SRM 57-50-5, RT AILERON.Jul 11, 1997 · N517DA · Boeing 727232 · AileronsSDR DL72S971242Fitting · corrosionTHE DRAG BRACE FITTING WAS FOUND CORRODED ON THE FACE OF A SMALL LUG. THE CORROSION WAS LOCALLY BLENDED TO A MAX DEPTH OF 0.030. THE LUG BORE WAS OVERSIZED TO 2.858. THIS REPAIR WAS AUTHORIZED BY FAA/ DER FORM 8110-3, DER DESIGNATION NM-2256, DTD 6-20-97.Jun 20, 1997 · N517DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S980478Web · crackedFOUND ON B2 LETTER CK, .25 INCH CRACK AT LT TORQUE BOX VERTICAL WEB UPPER LIGHTENING HOLE STA 1223. REPAIRED PER MM 53-11-0.Feb 26, 1997 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S962562Battery Pack · dischargedLEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD.Nov 21, 1996 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S962141Stringer · crackedFOUND DURING A-1 LETTER CHECK, .75 INCH CRACK STR 18A LEFT 8 INCHES AFT BS 940 FRAME ATTACH. REPAIRED PER M/M 53-12-0.Sep 19, 1996 · N517DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S962140Bracket · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LWR I/B RADIUS. REPAIRED PER M/M 57-20-21 PAR 12.Sep 19, 1996 · N517DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960429Angle · crackedNR 3 L/E SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.Feb 23, 1996 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960428Angle · crackedNR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.Feb 23, 1996 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960427Angle · corrodedCORROSION AT UPSTOP ANGLE FWD OF FWD HINGE ACCESS PNL 3348L. REPAIRED BEAM PER M/M 53-30-1.Feb 23, 1996 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960312Retract Mech · lack of lubeRT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF. INSPECTED, LUBRICATED RT MAIN GEAR. JACKED A/C CYCLED GEAR SEVERAL TIMES, OPERATION NORMAL.Feb 10, 1996 · N517DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S960255Wire · brokenON CLIMBOUT, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON, WING ANTI-ICE NOT ON, BUT DUCT TEMP SHOWED 200 DEGREES. FOUND STRUT WING ANTI-ICE VALVE STUCK OPEN. REMOVED AND REPLACED RELAY R32 AND FOUND BROKEN WIRES IN CANNON PLUG ON STRUT VALVE. REMOVED AND REPLAFeb 1, 1996 · N517DA · Boeing 727232 · Overheat DetectionSDR DL72S960219Skin · crackedNR 4 KRUEGER FLAP HAS TWO 1 INCH CRACKS AT O/B CUTOUT FOR LWR LIP ATTACH FITTING. REPAIRED PER SRM 57-50-3.Jan 28, 1996 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960256Access Door · corrodedCORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR ON THE LT SIDE. THE CORROSION WAS CUT OUT AND STRUCTURAL INTEGRITY WAS RETURNED PER AN INTERNAL AND EXTERNAL DOUBLER REPAIR PER DL ERA 303056-14.Jan 22, 1996 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960278Stringer · crackedSTRINGER 8 ON LT SIDE OF VERT STAB AT FIN STA 180.6 IS CRACKED. FABRICATED REPAIR ANGLE IAW MM 55-30-0 PG 803.Jan 20, 1996 · N517DA · Boeing 727232 · Vertical StabilizerSDR DL72S960231Stringer · corrosionHMV ATL, CORROSION STA 1090 TO 1110. BULGED BETWEEN STRINGER AND SKIN APPROX 6 INCHES FWD OF 1090 TO 4 INCHES AFT OF 1110. REPAIRED DAMAGE PER SRM 53-12-0 FIG 807.Jan 19, 1996 · N517DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S960227Galley Track · corrosionATL HMV, STA 380 TO 440 CENTER RT GALLEY TRACK HAS CORROSION IN AND ON LEGS OF TRACK. REMOVED TRACKS FROM STA 380 TO 440. INSTALLED NEW TRACK PER MM 53-20-11.Jan 19, 1996 · N517DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S960187Skin · crackedFROM HMV ATL, THE LOWER SKIN ON THE LT HORIZ STAB IS GOUGED AND CRACKED I/B END. ACCOMPLISHED REPAIRS PER SRM 55-10-3 FIG 3.Jan 19, 1996 · N517DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72S960152Bracket · crackedFROM HMV ATL, NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET CRACKED. INSTALLED REPAIR PER MM 57-20-21 PG 811.Jan 19, 1996 · N517DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S954463Angle · crackedSKIN ATTACHING ANGLE CRACKED 31 INCHES FROM OUTBOARD END. REPAIRED AS PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jul 27, 1995 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954462Angle · crackedCOVE PANEL ATTACHING ANGLE CRACKED UNDER UPSTOPS. REPAIRED AS PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jul 27, 1995 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953177Skin · crackedFOUND DURING F-1 LETTER CHECK - NR 4 L/E FLAP CRACKED OUTBD HINGE CUTOUT. REPAIRED PER MM 57-53-0 PG 802.Jul 24, 1995 · N517DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953075Eel Battery Pack · dischargedDURING LAY OVER, FOUND FWD DOOR ESCAPE SLIDE LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL.Jul 14, 1995 · N517DA · Boeing 727232 · Emergency LightingSDR DL72S952391Trunnion · pittedRIGHT MLG FWD TRUNNION ATTACH FITTING BUSHING IS PITTED. REPAIRED PER M/M 57-43-0.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952389Fitting · pittedRIGHT MLG SIDE BRACE AFT BEARING FITTING IS PITTED. REF MM REPAIR 57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
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