N514DA, cancelled Apr 23, 2015

Service difficulty reports · 64

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 = 'N514DA' AND deregistration_id = 'N514DA-2015-04-23'
  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 DL72L010946Skin · crackedDURING AD 99-04-22 INSPECTIONS OF THE LAP SPLICE LOWER FASTENER ROWS, TWO NONCONSECUTIVE BAYS WERE FOUND WITH CRACK INDICATIONS. THE CRACKS WERE REMOVED AND THE SKIN REPAIRED PER B727 SRM 53-30-3 FIG 5, AS MANDATED BY FAA LETTER 99-120S-171, DTD 3-4-99.Jun 8, 2001 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L010863Stiffener · crackedBOTH L/E SPAR STIFFENERS CRACKED AT NR 2 SLAT I/B TRACK. REPAIR PER M/M 57-20-021-8.May 29, 2001 · N514DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L010862Stringer · corrodedFOUND CORROSION STR 27L AT STA 1050 REF NRC 68. REPAIR PER SRM 53-10-3.May 29, 2001 · N514DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L010226Swivel · leakingAT PUSH BACK HYD A QTY WAS 4.1 GAL, DURNING CRUISE HYD A QTY DROPPED TO 1.2 GAL. ACCOMPLISHED A SYS HYD LEAK/LOSS CK LIST AND RETURNED TO SALT LAKE. LEAK STOPPED WHEN BOTH A PUMP SHUT OFF. FOUND B-NUT AT SWIVEL JOINT LEAKING FOR NR 3 LEADING EDGE SLAT, INBDFeb 8, 2001 · N514DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72L010173Actuator · leakingSYSTEM A HYDRAULIC FLUID DECREASED BELOW 1 GALLON. TURNED OFF A-SYSTEM PUMPS AND COMPLIED WITH POM PROCEDURES FOR HYDRAULIC SYSTEM EMERGENCY. CRANKED GEAR AND FLAPS DOWN AND PERFORMED UNEVENTFUL LANDING AT 160000 LBS, RATE OF DESCENT AT TOUCHDOWN WAS 4Jan 30, 2001 · N514DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L002116Spar · crackedROUTINE INSPECTIONS OF THE LT ELEVATOR REAR SPAR REVEALED A .25 INCH LONG TYPICAL CRACK EMANATING FROM A TAB HINGE BRACKET. THE CRACK IS TYPICAL OF AD 96-06-05 AND BAC S/B 727-55-0089. THE CRACK WAS STOP DRILLED ON A TEMPORARY BASIS PER THE REQUIREMEOct 26, 2000 · N514DA · Boeing 727232 · Elevator, Spar/RibSDR DL72L001661Battery · inoperativeON L/O, FOUND EMERGENCY LIGHT AT L-1 DOOR INOP. REPLACED BATTERIES, OPERATION NORMAL.Aug 28, 2000 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L001348Mount · crackedWHILE ACCOMPLISHING HFEC BOLT HOLE INSPECTIONS ON THE NR 3 PYLON FWD ENGINE MOUNT SUPPORT FITTING PER BAC S/B 727- 54A0010 AND AD 97-05-08, HOLE WAS FOUND WITH A CRACK INDICATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND ADDTIONAL .0312 INSURANCE CUJul 17, 2000 · N514DA · Boeing 727232 · Engine Mount SectionSDR DL72L001263Battery Pack · inoperativeON LAYOVER, FOUND PORTABLE EMERGENCY EXIT LIGHTS INOP ABOVE CABIN ENTRY DOORS AND EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED BATTERIES, OPERATIONAL TEST NORMAL.Jul 4, 2000 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L001209Battery Pack · dischargedRT CARGO DOOR AND LT CENTER EXTERIOR EMERGENCY LIGHTS INOP. FOUND ON SERVICE CHECK. REPLACED BATTERY PACK CKS OK.Jun 26, 2000 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L000754Switch · stuckDURING CLIMBOUT FROM PHX, PRESSURIZATION WAS UNCONTROLLABLE IN ALL MODES. FOUND EQUIPMENT ACCESS DOOR OPEN WITH NO INDICATION IN COCKPIT. DOOR SWITCH STICKING. CLEANED SAME.Apr 19, 2000 · N514DA · Boeing 727232 · Door Warning SystemSDR DL72L000565Engine · malfunctionedNR 2 ENG FIRE BELL SOUNDED AND COULD NOT BE SILENCED. FLT CREW FOLLOWED POM WHICH LED TO ENGINE NR 2 SHUT DOWN. FOUND NR 2 ENGINE FIREWALL LOOP DAMAGED. REPLACED SAME.Mar 23, 2000 · N514DA · Boeing 727232 · Detection SystemSDR DL72L000542Skin · damagedFATIGUE CRACK FOUND IN THE VERTICAL STABILIZER SKIN AT STRINGER 10R AND THE FUSELAGE CREASE LINE. DAMAGE IS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER IS INSTALLED PER ER/A 334183-14.Mar 16, 2000 · N514DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L000544Frame · corrodedTHE BS 1166 FRAME WAS FOUND CORRODED BETWEEN STR 26L AND STR 27L AT THE SKIN ATTACH FLANGE. THE DAMAGE WAS TRIMMED OUT AND A REPAIR DOUBLER INSTALLED ER/A 334178-14 REV A.Mar 15, 2000 · N514DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L000543Spar · damagedDURING ACCOMPLISHMENT OF S/B 727-57A0182 MODIFICATION SEVERAL FASTENERS HOLES WERE OVERSIZED THROUGH ALL LAYERS OF THE REPAIR. MODIFICATION IS TO THE WING CENTER SECTION REAR SPAR WEB. ER/A 334197-14AD REV A.Mar 15, 2000 · N514DA · Boeing 727232 · Wing SparSDR DL72L000524Door Frame · damagedCRACK IN STA 560 FRAME AT A FASTENER HOLE AT WL 191 AND RBL 62 BETWEEN THE NR 1 AND NR 2 DOOR STOP FITTINGS. THE HOLES WERE OVERSIZED AND BUSHINGS INSTALLED TO CORRECT THE PROBLEM. ER/A 334156-14 REV A.Mar 15, 2000 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L000541Skin · corrodedSKIN FOUND CORRODED AROUND THE LOWER LAVATORY SERVICE PANEL. THE PANEL IS LOCATED BETWEEN STA 1166 AND 1183 BETWEEN STRINGERS 23L AND 25L. THE DAMAGED SKIN WILL BE CUT OUT AND A NEW SECTION OF SKIN SPLICED IN. ER/A 334175-14 REV A.Mar 14, 2000 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000540Stringer · corrodedSTRINGER 29R WAS FOUND WITH CORROSION REQUIRING A SPLICE FROM STA 950D+10 TO STA 950E+10. ER/A 334163-14.Mar 2, 2000 · N514DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L992544badRIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY, CKS GOOD.Nov 17, 1999 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L991401Connector · shortedCONTINUOUS FIRE WARNING ON NR 3 ENGINE. UNABLE TO SILENCE FIRE WARN. BOTH EXTINGUISHER BOTTLES DISCHARGED WITH NO HELP. NR 3 ENGINE SHUT DOWN. RECEIVED WARNING APPROX 50 MIN INTO FLIGHT. ENG WINDMILLED FOR APPROX 5 MIN AFTER SHUTDOWN. FOUND LWR FIRJun 20, 1999 · N514DA · Boeing 727232 · Fire DetectionSDR DL72L990161Chord · crackedTHE I/B UPPER CHORD OF THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A 1 INCH TYPICAL CRACK AT FS 1273. THE DAMAGED SECTION OF CHORD WAS REMOVED AND A NEW SECTION SPLICED PER BAC S/B 727-53-0129. THE REPAIR WAS DOCUMENTED PER ER/A 366542-14AD.Jan 23, 1999 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L990154Stiffener · crackedCHK D-1, O/B SPAR STIFFENER CRACKED, NR 6 L/E SLAT O/B TRACK BOX. REPLACED PER MM 57-20-21.Jan 22, 1999 · N514DA · Boeing 727232 · Leading Edge DevicesSDR DL72L981319Web · crackedFOUND ON C2 LETTER CK, .375 INCH CRACK ON LIGHTENING HOLE, LT LOWER TORQUE BOX WEB AT STA 1228. REPAIRED PER MM 53-11-0.Jun 22, 1998 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981072Battery Pack · dischargedAT DEPARTURE CHECK, FOUND THAT THE LT OVERWING EXIT EMER LIGHT FAILED THE STDBY PWR CHECK. REMOVED AND REPLACED BATTERY PACK AND PWR SUPPLY RACK.May 19, 1998 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L980563Battery · dischargedBOTH F/C DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.Mar 11, 1998 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L972597Actuator · leakingPILOT REPORTED, CLIMBING THROUGH 18,000 FT 'A' SYS QTY DECREASED TO ZERO. ALL PROCEDURES ACCOMPLISHED PER CHECKLIST. BOTH 'A' SYSTEM LOW PRESS LIGHTS WERE BLINKING AS PRESS WAS DROPPING. MAINTENANCE FOUND NR 4 L/E FLAP ACTUATOR LEAKING AT SWIVEL END. REPLADec 10, 1997 · N514DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L972489Light · corrodedLT AFT ENTRY DOOR SLIDE LIGHT INOP ON LAYOVER CHECK. REPLACED REFLECTOR ASSY DUE TO CORRODED CENTER ELECTRODE.Nov 28, 1997 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L972335Skin · corrodedTHE FUSELAGE SKIN AT STA 600 AND STR 28L WAS FOUND CORRODED AND WAS CUTOUT IN A 3.5 X 9 AREA. A PREVIOUSLY REPAIRED CUTOUT WAS INCORPORATED INTO THE REPAIR. THE CORROSION CUTOUTS WERE REPAIRED WITH A DOUBLER AND TRIPLER. INSTALLED PER ER/A 363146-14.Nov 11, 1997 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L972312Skin · corrodedTHE FUSELAGE SKIN AT STA 950 AND STRG 30 WAS FOUND CORRODED AND THE DAMAGE REMOVED BY CUTOUT. THE CUTOUT WAS REPAIR WITH A DOUBLER AND TRIPLER INSTALLED PER ER/A 363138-14, REV A.Nov 7, 1997 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L971640Light · inoperativeRT CTR OVRWING EMERG LIGHT INOP. REPLACED BATT PACK AT M956, OPS CHKS GOOD.Aug 21, 1997 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L970647Light · inoperativeCENTER AILSE EMERG LIGHT INOP. REPLACED CHARGER BASE, OP CK NORMAL PER MM.Apr 10, 1997 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L962435Battery · dischargedL-2 AND AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED BATTERIES, CHECKS OK.Nov 1, 1996 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L962076Battery Pack · dischargedOVERWING EXIT EMER LIGHT INOP // REPLACED BATT PACK M956 OPS CK GOODSep 8, 1996 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L960971Light · brokenIRREGULAR EMERGENCY EXIT LIGHT ON LOWER SIDEWALL AT ROW 20A IS MISSING. INSTALLED LIGHT ASSY. CKS NORMAL.Apr 23, 1996 · N514DA · Boeing 727232 · Emergency LightingSDR DL72L960615Angle · crackedTHE NR 4 SPOILER ACTUATOR ATTACH FITTING WAS REPLACED DUE TO A CRACK FOUND IN THE O/B FITTING. ALL WORK DONE PER SRM 57-50-6.Mar 20, 1996 · N514DA · Boeing 727232 · Drag Control ActuatorSDR DL72L960434Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN, DOUBLER AND TRIPLER WERE FOUND CRACKED IN THE UPPER FWD CORNER OF THE R-1 DOOR CUTOUT. THE CRACK IS 0.5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. IN ACCORDANCE WITH FAA 8110-3 FORM, A TIME-LIMITED RFeb 23, 1996 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L960417Skin · crackedA 1.5 INCH CRACK AT MAIN ENTRY DOOR CUTOUT, OUTER SKIN AT UPPER HINGE CUTOUT. FOUND AT A-2 LTR CHECK. REPAIRED PER MM 53-30-0 PG 11.Feb 22, 1996 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L954439Panel · delaminatedFOUND NR 2 SPOILER PANEL DELAMINATED. REPLACED PANEL, ROUTED TO SHOP FOR REPAIRS.Nov 19, 1995 · N514DA · Boeing 727232 · SpoilersSDR DL72L953130Web · crackedFOUND DURING A-1 LETTER CHECK, .3125 INCH CRACK AT LIGHTNING HOLE LT SIDE TOP 2ND HOLE FROM FWD SIDE AFT STAIRWELL WEB. REPAIRED PER SRM 53-11-0 828.Jul 20, 1995 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L950326Switch · faultyDURING CLIMB THROUGH 12,000 FEET ELEVATOR FEEL DIFF, PRESSURE LIGHT ILLUMINATED. PERFORMED PROCEDURES IAW POM, FOUND NO OTHER DISCREPANCIES. AFTER ONE HOUR AT CRUISE, LIGHT EXTINGUISHED FOR 5 MINUTES THEN ILLUMINATED, THEN LIGHT EXTINGUISHED IN DESCENT. LANJan 22, 1995 · N514DA · Boeing 727232 · Elevator Control SystemSDR DL72L950479Track · corrodedDURING INSPECTION AT HMV, THE LEFT SIDE INBD TRACK FOR THE INBD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE FWD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBD AND OUTBD SIDES OF THE TRACK. THE HOLES WERE REPAIRED Jan 19, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L950167Le Rib · crackedDURING HMV, FOUND RIB INSIDE NR 3 L/E SLAT CRACKED. REPAIRED PER SRM 57-50-3 FIG 9.Jan 13, 1995 · N514DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950369Skin · corrosionBELLY SKIN AT STR 28R, STA 990 FOUND CORRODED. A 2.5 INCH BY 2.5 INCH SECTION WAS CUT OUT TO REMOVE CORROSION. A 0.040 INCH TI-6AL-4V DOUBLER, AND A 0.063 INCH TI-6AL-4V TRIPLER WILL BE INSTALLED OVER CUTOUT.Jan 12, 1995 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L950206Le Skin · wornAT HMV SHOP INSPECTION, THE RIGHT WING NR 4 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO THE LEADING EDGE SKIN AT 86 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 5750-4.Jan 8, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L950205Le Skin · wornAT HMV, SHOP INSPECTION THE RIGHT WING NR 4 FORE FLAP HAS FOUND WITH WEAR DAMAGE ON THE LEADING EDGE SKIN AT 29 INCHES FROM THE OUTBOARD END OF FLAP. REPAIRED DAMAGE PER SRM 57-50-4.Jan 8, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L950125Frame · crackedDURING HMV, FOUND FRAME 804.5 BETWEEN L/A O/W EXIT OPENINGS STR 14 FRAME CHORD CRACKED. REPAIRED PER SRM 53-10-4 FIG 17.Jan 7, 1995 · N514DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L950168Web · crackedDURING HMV, FOUND WEB CRACKED INSIDE LT WING L/E O/B OF NR 2 SLAT ACTUATOR. REPAIRED PER M/M 57-54-0.Jan 6, 1995 · N514DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L950165Skin · dentedAT HMV, FOUND DENT IN FUSELAGE SKIN BETWEEN STA 450-460 AND STR 17R AND 18R. ROUTED OUT DAMAGE PER SRM 53-30-3.Jan 5, 1995 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L950264Angle · crackedDURING HMV, NR 5 SLAT CLOSEOUT ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-54-0.Jan 4, 1995 · N514DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950192Rib · crackedDURING HMV, FOUND NR 7 L/E SLAT ACT ATTACH RIBS CRACKED AT LWR FWD RADIUS. FABRICATED PART AND REPAIRED PER M/M 57-54-0.Jan 4, 1995 · N514DA · Boeing 727232 · Leading Edge Devices
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