N503DA, cancelled Sep 26, 2016

Service difficulty reports · 49

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 = 'N503DA' AND deregistration_id = 'N503DA-2016-09-26'
  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 DL72L011292Valve · leakingSYSTEM A HYDRAULICS FAILURE AFTER GEAR RETRACTION. PRESSURE ZERO, FLUID ZERO. A SYSTEM PUMPS SHUT OFF IAW CHECKLIST APPROX 5 MIN. FOUND LOCK ASSY VALVE LEAKING IN RT MLG WW. REMOVED AND REPLACE R/H SIDE LOLOCK ASSY VALVE PER M/M JACKED A/C AND CYCLED GEAR. OAug 6, 2001 · N503DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72L010469Angle · crackedFOUND ON B2 LETTER CK FWD ANGLE CRACKED AT STA 910 ABOVE MLG UPLOCK IN THE LT MLG WW. REPAIRED PER MM 53-11-000-8.Mar 22, 2001 · N503DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L010085Battery · dischargedEMERGENCY EXIT SIGN OVER R2 DOOR INOP WITH BATTERY POWERED LIGHTS. REPLACED M1093 BATTERY PACK, OPS OK.Jan 17, 2001 · N503DA · Boeing 727232 · Emergency LightingSDR DL72L001638Beam · crackedTHE RT TORQUE BOX OF THE VENTRAL STAIRWAY WAS FOUND WITH A TYPICAL CRACK IN THE FS 1263 UPPER HORIZONTAL BEAM. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129. THE CRACKED PIECE OF STRUCTURE WAS REMOVED AND REPLACED WITH A NEW MEMBER PER THE REQUIREMENTS OF THEAug 23, 2000 · N503DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L001402Frame · damagedWHILE ACCOMPLISHING INSPECTIONS OF THE AFT ENTRY DOOR FRAMES ON THE FS 1183 BULKHEAD, AN ELONGATED FASTENER HOLE WAS FOUND IN THE RBL 17.8 FRAME CAP COMMON TO AN INTERCOSTAL AT WL 263. THE HOLE WAS REAMED TO A CLEAN AND ROUND CONDITION AND AN OVERSIZE FASTENEJul 24, 2000 · N503DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L001070Ballast · smokeWHILE BOARDING A/C NOTICIED WHITE SMOKE FROM OVER CEILING PANEL AT L-1 DOOR. C/MTC FOUND ENTRY BRIGHT C/B POPPED. INSPECTED LIGHT ASSEMBLY, FOUND BAD BALLAST. REPLACED SAME.May 31, 2000 · N503DA · Boeing 727232 · Passenger Compartment LightingSDR DL72L000189Skin · gougedTHIS AIRCRAFT RECEIVED GROUND DAMAGE TO THE FUSELAGE SKIN AT FS 990 AND STR 24R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334013-14.Jan 26, 2000 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000212Gimbal Fitting · gougedLT AND RT GIMBAL ATTACH FITTINGS WERE FOUND GOUGED IN THE FILLET RADIUS OF THE UPPER LUGS. ER/A 333979-14 REV A.Jan 19, 2000 · N503DA · Boeing 727232 · Horizontal Stabilizer, Attach FittingsSDR DL72L000240Spar · crackedLWR AFT SPAR CRACKED 19, 32 & 37 FROM I/B END. ALSO, CRACKED 37 & 43 FROM O/B END. THIS DAMAGE REPAIRED PER M/M 57-52-0 FIG 802.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000239Skin · crackedCOVE SKIN CRACKED 32 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000208Skin · crackedAPPROX .75 INCH LONG CRACK IN COVE SKIN, 32 FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 809.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000207Spar · crackedAFT SPAR DOUBLER CRACKED 21, 34 & 57S FROM I/B END DAMAGE LISTED ON N/R'S 016162, 016079 & 016080. REPAIRED PER CMM 57-52-0 FIG 802.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992531Slat · wornSKIN CRACKED AT FENCE ATTACH HOLES. REPAIRED PER M/M 57-54-0.Nov 16, 1999 · N503DA · Boeing 727232 · Drag Control SystemSDR DL72L991892Skin · crackedLFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 500 & 520. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXAug 23, 1999 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991855Bracket · crackedFOUND ON A1 LETTER CK, NR 2 SLAT ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-42-0.Aug 18, 1999 · N503DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L990905Skin · crackedFUSELAGE SKIN FS 481-681, STRINGER 26L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED MULTIPLE CRACKS Apr 24, 1999 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990338Valve · inopAT FL250 ALTITUDE WARNING HORN WENT OFF WITH CABIN ALT AT 12,000 FT. CREW WENT ON 02, OUTFLOW VALVE SHOWED CLOSED. CARGO VALVE CLOSED, LT PACK OFF, DUE TO PREVIOUS WRITE UP. FOUND LT PACK VALVE INOP AND LT ACM NOT TURNING. REPLACED LT PACK VALVE AND ACM CFeb 19, 1999 · N503DA · Boeing 727232 · Cabin Cooling SystemSDR DL72L981240Panel · holeFOUND ON F1 LETTER CHECK, HOLE .25 IN LOWER LT HORIZONTAL STAB ACCESS PANEL INBD OF ELEV PWR PACK. INSTALLED DOUBLER PER SRM 55-20-3.Jun 10, 1998 · N503DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72L980379Sill · corrodedTHE OUTBOARD CAP (EXTRUDED TEE) OF THE C2 DOOR SURROUND LOWER SILL WAS FOUND BADLY CORRODED ON THE OUTBD FLANGE. THE FLANGE WAS CUT AWAY TO REMOVE THE CORROSION. THE CUT FLANGE WAS REPAIRED WITH A SHEET METAL ANGLE REPAIR PER ER/A 363872-14, REV A.Feb 11, 1998 · N503DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L980376Stringer · corrodedSTRINGER 29R WAS FOUND CORRODED NEAR FS 950E+10. THE STRINGER WAS CUT AT FS 950D+10 AND THE AFT SECTION REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER ER/A 363710-14, REV B.Feb 11, 1998 · N503DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L980287Skin · corrodedCORROSION WAS FOUND IN THE SKIN AT FS 705, BL 0. BECAUSE OF THE CORROSION AND THE PRESENSE OF EXISTING REPAIRS IN THE AREA THE SKIN WAS SPLICED AT APPROX FS 715 FROM STR 26L TO 26R. THE NEW SECTION OF SKIN WAS SPLICED PER B727 SRM 53-30-3, EXCEPT THE SPLICE Jan 30, 1998 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L980021Spar · crackedFRONT SPAR CRACKED. REPAIRED SPAR PER SRM 51-40-3 (REF 57-50-2) ENG SIG.Jan 5, 1998 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L980020Skin · crackedCRACK IN LWR T/E SKIN AT ACTUATOR FITTING. REPAIRED SKIN PER SRM 57-50-3.Jan 5, 1998 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L972697Skin · corrodedTHE FUSELAGE SKIN A FS 705, BL 0 WAS FOUND WITH A SMALL AREA OF CORROSION. THE DAMAGE WAS REMOVED WITH A 1 DIA HOLE. THREE OTHER REPAIRS WERE IN THE GENERAL AREA OF THE CUTOUT. THEREFORE, THE SKIN WAS CUT AT FS 710 FROM S-26L TO S-26R AND A NEW SECTION OF SDec 19, 1997 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L972681Blkhd Stiffener · crackedA 2 INCH CRACK WAS FOUND IN THE RBL 36.83 STIFFENER AND A 1 INCH CRACK WAS FOUND IN THE LBL 36.83 STIFFENER AT WL 238 ON THE FS 1183 BULKHEAD. THE STIFFENERS WERE REPAIRED PER BOEING S/B 727-53-0192 AS DOCUMENTED IN ER/A 363498-14.Dec 18, 1997 · N503DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72L980218Frame · partFS FRAME 1352 FRAME WORN AT THE 6 O'CLOCK POSITION. FRAME WAS REPAIRED PER MM 53-11-0.Dec 8, 1997 · N503DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L980121Web · crackedAT MV-2/DFW, FOUND A CRACK AT A LIGHTENING HOLE AT FS 870 IN WEB AND DBLR. REPAIRS WHERE COMPLETED PER SRM 53-10-9 FIG 5. CRACK WAS LOCATED AT THE 5 O'CLOCK POSITION.Dec 8, 1997 · N503DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L972266Cowl · cracked1 1/2 CRACK EXTENDING FROM LOWER AFT CORNER OF EXISTING REPAIR DOUBLER RT SIDE OF #2 ENG NOSE COWL AFT OF NOSE RING REPLACED DOUBLER PER M/M 54-30-0Nov 5, 1997 · N503DA · Boeing 727232 · Engine Cowling SystemSDR DL72L972260Bracket · crackedFOUND DURING E-2 LETTER CHECK - NBR 8 SPOILER ACTUTOR MOUNT CASTING LWR ATTACH BRKT CRACKED REPAIRED PER M/M 57-20-22Nov 5, 1997 · N503DA · Boeing 727232 · Drag Control ActuatorSDR DL72L962446Battery Pack · dischargedOVERWING EMERGENCY LIGHT FAILS TO TEST. REPLACED BATTERY PACK RACK, CHECKS NORMAL.Nov 3, 1996 · N503DA · Boeing 727232 · Emergency LightingSDR DL72L960653Skin · damagedLAX REPORTED DAMAGE TO THE SKIN, STRINGERS AND FRAMES BETWEEN STA 340 TO STA 400 AND STR 22R TO S-24R. SEVERAL REPAIRS HAVE BEEN INSTALLED PER THE B727 SRM. DUE TO LIMITED ACCESS BLIND FASTENERS WILL BE INSTALLED IN SEVERAL LOCATIONS ON A TIME LIMITED BASIS,Mar 18, 1996 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L960418Mount Bracket · crackedFOUND DURING D-1 LETTER CHECK, .375 INCH CRACK AT NR 6 L/E FLAP ACTUATOR MOUNT BOX UPPER O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.Feb 22, 1996 · N503DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L960414Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 870 AND STR 9R. THE CUT OUT MEASURES 5 INCHES BY 3 INCHES, IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3A, A DOUBLER AND TRIPLER WERE INSTALLED.Feb 21, 1996 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L960059Slide · low pressureDURING INSPECTION, R-1 DOOR SLIDE PRESSURE FOUND LOW 500 LBS. REPLACED SLIDE.Jan 9, 1996 · N503DA · Boeing 727232 · Escape SlideSDR DL72L953289Skin · crackedUPON INSPECTION A CRACK WAS FOUND IN THE THERMAL ANTI-ICE SKIN BETWEEN THE RIBS O/B FROM THE ACTUATOR RIBS. REPAIRED PER M/M 57-54-0 FIG 803. FOUND DURING SHOP INSPECTION FOR NR 6 L/E SLAT.Aug 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953288Angle · crackedUPON INSPECTION A CRACK WAS FOUND ON THE LOWER ANGLE BETWEEN THE ACTUATOR RIBS. REPAIRED PER MM 57-54-0 FIG 812. FOUND DURING SHOP INSPECTION FOR NR 6 L/E SLAT.Aug 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953296Rib · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND CRACKED AT THE INBD RIB, INBD TRACK ARM IN RADIUS. ALSO, I/B ACTUATOR RIB CRACKED TOP FWD CORNER. REPAIRED PER MM 57-54-0 FIG 805 AND FIG 804.Jul 28, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953355Skin · corrodedDURING CV-2 INSPECTION, CORROSION WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 700 AND OUTBD OF STRINGER 28L. DAMAGE REMOVAL RESULTED IN A 2 BY 2 CUTOUT. DUE TO THE PROXIMITY TO AN EXISTING REPAIR, THE FACT THAT THE SKIN IS A SSI ITEM AND THE PROXIMITY TO Jul 21, 1995 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L953193Skin · corrodedFOUND ON CV2 CK. CORROSION ON SKIN LAP JOINT OUTBOARD OF STR 26R FROM STA 720C-STA 720F. REPAIR: REPAIRED PER ERA 302175-14.Jul 18, 1995 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L953182Firewall Panel · crackedFOUND ON CV2 CK, NR 2 ENG FIREWALL, NR 1 PANEL CRACKED .75 INCH, LT SIDE OF INLET, AND .50 INCH, RT SIDE OF INLET. REPAIR: REPAIRED PER SRM 54-10-3, FIG. 1.Jul 18, 1995 · N503DA · Boeing 727232 · Nacelle/Pylon, Bulkhead/FirewallSDR DL72L953198Angle · crackedFOUND ON CV2 CK, CRACK INBD OF ACTUATOR NR 5 SLAT. REPAIR: REMOVED SLAT PER OPN 7005, PEPAIRED PER MM 57-54-0, FIG 804.Jul 17, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L952504Turb Shear Pin · failedTHIS ENGINE WAS EXHIBITING HIGH EGT INDICATIONS AND SENT TO ATL FOR ENGINE TEST RUN ON WING. A NORMAL START WAS PERFORMED WITH START VALVE LIGHT EXTINGUISHING. THEN, 15 MINUTES AFTER START AND IDLE THE ENGINE FIRE WARNING LIGHT ILLUMINATED, JUST PRIOR TO REAJun 4, 1995 · N503DA · Boeing 727232 · Turbine SectionSDR DL72L952364Eel Battery Pack · dischargedRIGHT OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. REPLACED BATTERY, CHECKS GOOD.May 31, 1995 · N503DA · Boeing 727232 · Emergency LightingSDR DL72L950187Stiffiners · crackedDURING INSPECTION (L/C), THE RT TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS AT FS 1263. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4.Jan 6, 1995 · N503DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L950424Skin · crackedDURING SHOP ISNPECTION, LEFT WING NR 4 SLAT UPPER SKIN WAS WORN AT FENCE. ALSO, A TIME LIMITED REPAIR WAS FOUND ON LOWER SKIN AT FENCE AREA. REPAIRED PER MM 57-54-0 FIG 813 AND SRM 57-50-3 FIG 1.Jan 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950423Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH RIB NR 12 AND NR 18 CRACKED. REPAIRED PER MM 57-54-0.Jan 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950422Rib · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0.Jan 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950421Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH THE RIB CHORD CRACKED AT THE O/B END, AND WORN AT THE I/B TRACK. REPAIRED PER MM 57-54-0 FIG 812.Jan 5, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950420Skin · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKED LOWER SKIN AT INBD TRACK FAIRING. REPAIRED PER MM 57-54-0 FIG 15.Jan 5, 1995 · N503DA · Boeing 727232 · Leading Edge Devices
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