N504DA, cancelled Oct 30, 2003

Service difficulty reports · 53

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 = 'N504DA' AND deregistration_id = 'N504DA-2003-10-30'
  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 DL72L020420Battery · dischargedFOUND AFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK.Apr 8, 2002 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L020199Odor · detectedIN FLIGHT NOTICED A FAINT ELECTRICAL SMELL. AFTER LANDING NOTICED DRAIN MAST C/B POPPED. NO SMELL WHEN MTC ARRIVED. OPENED C/B PANELS IN C/P ALL OK. RAN PACKS WITH ENGINES AND APU, ALL OK. REMOVED SEVERAL OVERHEAD PANELS AND TURNED ON ALL C/P LIGHTING, ALFeb 18, 2002 · N504DA · Boeing 727232 · Air Distribution SystemSDR DL72L011847Transmitter · failedAFTER T/O RUDDER OSCILLATIONS FOLLOWED POM PROCEDURE. FOUND POSITION TRANSMITTER COIL OPEN REMOVED AND REPLACED POS XMTR PER MM ADJ/TEST OF YAW DAMP CHKS GOOD PER MM.Nov 23, 2001 · N504DA · Boeing 727232 · Autopilot SystemSDR DL72L011845Coupler · intermittentON TAKEOFF SLIGHT RUDDER OSCILLATIONS WITH HIGH WIND. AFTER TAKEOFF EXCESSIVE RUDDER MOVEMENT. FOLLOWED YAW DAMP INOP POM PROC. NO HELP. REMOVED AND REPLACED UPPER AND LOWER YAW DAMP COUPLERS PER M/M. SYSTEM TEST NORMAL.Nov 23, 2001 · N504DA · Boeing 727232 · Autopilot SystemSDR DL72L011217Stringer · corrodedSTRINGER 29L WAS FOUND BADLY CORRODED BETWEEN FS 950E AND FS 980.Jul 20, 2001 · N504DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L011148Fitting · corrodedFOUND DURING MV4 CORROSION VISIT NRC 54 CORROSION ON STR 27R END FITTING AT STA 740, OUTBD SIDE OF STR BEHIND RAM AIR DUCT.Jul 3, 2001 · N504DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L010836Beam · crackedINSPECTION OF THE RT TORQUE BOX STRUCTURE OF VENTRAL STAIRWAY OPENING REVEALED A 3 INCH CRACK IN THE UPPER HORIZONTAL BEAM AT FS 1263. THE CRACKED PART WAS REMOVED AND A NEW PART INSTALLED PER ER/A 380894-14AD. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129.May 23, 2001 · N504DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L010822Stiffener · crackedA 2 INCH CRACK AT WING L/E FRONT SPAR STIFFENER AT NR 6 SLAT O/B TRACK-O/B STIFFENER. REPAIR PER M/M 57-20-021-8.May 22, 2001 · N504DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L010239Shaft · shearedNR 3 ENG FAILED ON T/O ROLL. ABORTED AT 130 KIAS. REPLACED NR 3 ENG FUEL PUMP PER M/M. OPS CK AND LEAK CK ON IDLE RUN. ALSO TRIM ENG PER PFHB 4077 TEST Y. CK NML. RETORQUED FUEL PUMP QUAD RING PER M/M.Feb 10, 2001 · N504DA · Boeing 727232 · Engine Fuel PumpSDR DL72L002289Lens · crackedPASS. ST 21D EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED CA- RPLD LENSNov 23, 2000 · N504DA · Boeing 727* · Emergency LightingSDR DL72L002042Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT O/B ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.Oct 17, 2000 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002041Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT INBOARD ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.Oct 17, 2000 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002040Frame · crackedCHANNEL WORN/DAMAGED ALONG LWR FLANGE 5 O CLOCK TO 6 O CLOCK POSITION AT NR 2 ENG FWD COWL CUTOUT. REPAIRED PER MM 53-11-0 PG 801.Oct 17, 2000 · N504DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72L001635Light · inoperativeSEAT MOUNTED PROXIMITY LIGHTS INOP AT SEATS 16D AND 17D. RELAMPED AND REPLACED LENS AT 17D OPERATION NORMAL. FWD LIGHT AT 16D TO MCO AND PLACARD PER MEL.Aug 23, 2000 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L001356Battery Pack · inoperativeRIGHT WING CENTER OVERWING LIGHT INOP. REMOVED AND REPLACED RIGHT WING OVERWING BATTERY CHARGER.Jul 18, 2000 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L000358Battery · dischargedEMERGENCY LIGHT INOP AT CENTER AISLE NEAR AFT GALLEY. REMOVED AND REPLACED BATTERY PACK.Feb 22, 2000 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L992475Light · brokenEXIT LIGHT FORWARD OF R-1 DOOR IS UNSECURED/LOOSE. REPLACED SAME.Nov 10, 1999 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L992374Battery Pack · dischargedF/C SEAT MOUNTED EMERGENCY LIGHTS WON'T TEST. REPLACED RACK AND BATTERY PACK, CHECKS NORMAL.Oct 26, 1999 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L990970Start Valve · failedNR 1 START VALVE LIGHT ILLUMINATED IN FLIGHT. ENG SHUT DOWN PER PILOTS CK LIST. REPLACED START VALVE.May 3, 1999 · N504DA · Boeing 727232 · Engine Start Valves/ControlsSDR DL72L990701Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT FOR THE ENTIRE PANEL ANMar 27, 1999 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990177Skin · crackedI/B DRIVE ROD CUTOUT IN COVE SKIN IS CRACKED AT O/B AFT CORNER. REPAIRED PER M/M 57-52-0 FIG 809, ON SHOP ORDER 643487.Jan 8, 1999 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L982647Frame · corrodedCORROSION WAS FOUND ON THE BS 1166 FRAME AT THE SKIN CLIP BETWEEN S29R AND S30. DAMAGE RESULTED IN CUTOUT IN THE LWR 2.5 OF THE FRAME AS WELL AS THE BONDED FAIL SAFE STRAP. REPAIRED PER ERA 332608-14.Dec 29, 1998 · N504DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L982619Stringer · crackedUPPER CHORD ON THE RT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED FROM A FAST HOLE ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STR 17. REPAIRED PER ERA 332571-14.Dec 24, 1998 · N504DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L982618Stringer · crackedTHE UPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED PROPAGATING FROM A FAST. HOLE ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STR 16. REPAIRED PER ERA 332570-14.Dec 24, 1998 · N504DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L982617Track · corrodedINB'D FLAP INB'D TRACK, CORROSION AT MLG BEAM ATTACH PAD AND HOLES: AD 90-07-05 AND 90-06-09. THE SPOT-FACE DEPTH FOR THE MLG BEAM ATTACH HOLE HAS BEEN INCREASED TO REMOVE CORROSION. AUTHORIZED INCREASE DAMAGE REMOVAL WITHOUT ANY RE-INFORCING REPAIR.Dec 16, 1998 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L982519Frame · crackedDURING INSPECTION A CRACK WAS FOUND IN THE FRAME AT BS 380 WL 280; JUST ABOVE THE R1 DOOR CUTOUT. THE CRACK IS LOCATED ON THE INBD FLANGE OF THE PART AT A FASTENER HOLE. REPAIRED PER ERA 332549-14.Dec 9, 1998 · N504DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L990175Spar · crackedAFT SPAR RAIL LWR CHORD ANGLE CRACKED 2 PLACES 19 AND 23 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487.Dec 3, 1998 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L990174Spar · crackedAFT SPAR RAIL LWR CHORD ANGLE CRACKED 2 PLACES 32 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487.Dec 3, 1998 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L990173Spar · crackedAFT SPAR RAIL LWR CHORD ANGLE CRACKED 61 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487.Dec 3, 1998 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L982580Beam · corrodedL MLG SUPPORT BEAM HOLES CORRODED. REAMED HOLES. NDT-BHEC BEAM HOLES. TURNED BUSHINGS. TREATED BORES, INSTALLED BUSHINGS. ROTO PEEN HOLES SURFACES AS PER ERA 332561-14. TREATED AND PAINTED AREAS PER ERA 332561-14. SEALED EDGES OF BUSHINGS PER ERA 332561-Nov 30, 1998 · N504DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L982579Beam · corrodedLT MLG SUPPORT BEAM HOLES CORRODED. REAMED HOLES. BHEC INSP HOLES. TURNED AND TREATED BUSHINGS PER SRM 57-40. TREATED BORES. INSTALLED BUSHINGS. ROTO PEEN AREAS PER ERA 332561-14. TREATED AND PAINTED PER ERA 332561-14. SEALED ENDS OF BUSHINGS PER ERA 3Nov 30, 1998 · N504DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L982505Stringer · crackedITEM: OUTER WING UPPER STRINGER TO RIB WS 656.5 HAS A CRACK AT STRINGER 10 COMING FROM THE FASTENER HOLE. CRACK IS IN STRINGER. REPAIR INTO REFERENCED ON 8502AD ITEM 5. CRACK ORIGINATES IN FASTENER HOLE AND PROPAGATES TO EDGE OF STRINGER. DRILLED REPAIR DONov 30, 1998 · N504DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L981356Battery Pack · dischargedOVERWING EXIT EMERGENCY LIGHTS FAILED TO TEST DURING NR 3 SERVICE CHECK. REPLACED BATTERY PACK AND BASE, NOW CHECKS NML.Jun 28, 1998 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L981173Battery Pack · dischargedON L/O CK, LIGHTED EXIT SIGNS OVER LT O/W EXIT DID NOT ILLUMINATE. REPLACED BATTERY PACK.Jun 1, 1998 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L981172Battery · dischargedON L/O CK, AISLE EMERG LIGHT OVERHEAD ROW 13 DID NOT TEST. REPLACED BATTERY.Jun 1, 1998 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L981044Battery Pack · dischargedLEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK CHECKS GOOD.May 16, 1998 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L981001Skin · crackedA .5 INCH LONG CRACK WAS FOUND IN THE UPPER FWD CORNER OF THE R1 DOOR SKIN CUTOUT. THE CRACK WAS ROUTED OUT AND AN EXTERNAL ALUMINUM DOULBER INSTALLED PER ER/A 364704-14, REV A.May 6, 1998 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L980953Web · crackedFOUND ON A2 LETTER CK, 1.25 IN CRACK LT LOWER TORQUE BOX WEB AT THE UPPER ROW OF RIVETS STA 1235. REPAIRED PER MM 53-11-0.May 4, 1998 · N504DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L970447Skin · corrosionCORROSION WAS FOUND ON THE SKIN BELOW THE C2 DOOR BETWEEN STA 950F - 970 AT STR-28R. THE CORROSION WAS TRIMMED OUT LEAVING TWO CUT-OUTS MEASURING 3.6 INCHES BY 3 INCHES AND 4 INCES BY 2.6 INCHES. THE CUT-OUTS ARE 9 INCHES APART. REPAIRED PER DELTA ER/A 3048Mar 7, 1997 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L970446Frame · cut outIN ORDER TO FACILITATE A REPAIR ON STRINGER S-28R, FRAME 1130 ALONG WITH ITS FAIL SAFE ANGLE WAS CUT AT APPROXIMATELY RBL 12. THE ENTIRE OUTBOARD SECTION OF THE FRAME WAS THEN REMOVED AND RETAINED FOR A LATER RE-INSTALLATION. THE DAMAGE WILL BE REPAIRED PER Mar 7, 1997 · N504DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L970353Angle · crackedFOUND THE NR 3 MID FLAP ATTACH ANGLE FOR AFT SEAL, CRACKED IN 2 PLACES, APPROX 24 IN AND 36 IN FROM THE I/B END. REPAIRED PER MM 57-52-0, PG 807, FIG 802.Feb 20, 1997 · N504DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L962769Fuel Pump · sheared shaftNR 1 ENG FAILED ON T/O, ALL INDICATIONS NORMAL. FOUND FUEL PUMP SHAFT SHEARED. REPLACED PUMP, CHECKS NORMAL.Dec 25, 1996 · N504DA · Boeing 727232 · Engine Fuel PumpSDR DL72L961079Battery Pack · dischargedAFT RT CABIN EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED BATTERY PACK.May 5, 1996 · N504DA · Boeing 727232 · Emergency LightingSDR DL72L960636Actuator · failedAFTER TAKEOFF, AMBER LE FLAP LIGHT REMAINED ON AND NR 8 SLAT AMBER LIGHT ON S/O PNL. ON RETURN TO LAX LE FLAPS LIGHT STAYED ON, BUT ALL SLATS/FLAPS POS TEST SHOWS RETRACTED. RAN TEST USING TEST BOX 10M2425 PER M/M AND NR 8 SLAT ACTUATOR FAILED TEST. REPLACEMar 22, 1996 · N504DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L960238Prbc · failedON TAKEOFF, GOT COMPRESSOR STALL NR 2 ENGINE. INSPECTED INLET AND EXHAUST, ALL OK. RAN ENGINE TO TAKEOFF POWER, ALL CKS NORMAL, BUT ON DECEL GOT COMPRESSOR STALL AT 80 TO 85 N2. REPLACED PRBC, RAN ENGINE PER PFHB TEST-E AND ALL CKS GOOD.Jan 30, 1996 · N504DA · Boeing 727232 · Compressor Bleed ValveSDR DL72L960208Ribs · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH RIBS NR 12, 13, 14 AND 15 CRACKED. ACCOMPLISHED REPAIRS PER MM 57-54-0.Jan 19, 1996 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960210Angle · crackedLOWER FWD ANGLE CRACKED AT NR 13 RIB. REPAIRED PER MM 57-54-0 PG 807A. ALSO, WIND EROSION FWD OUTER SKIN. REPAIRED L/E WIND EROSION PER SRM 57-50-3 FIG 8 FOR L/E SLAT NR 6.Jan 18, 1996 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L961087Rib · crackedREPAIRED CRACKED RIB AS PER SRM 57-54-0 FIG 814.Jan 10, 1996 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L961620Skin · corrosionTHE SKIN AND STRINGER AT FS 480 TO 520 AND STR 26R WERE FOUND CORRODED. THE SKIN CORROSION REQUIRED A 3.25 BY 2.75 CUTOUT IN THE UPPER AND LOWER SKINS OF THE STR 26R LAP JOINT. THE STRINGER CORROSION REQUIRED A CUTOUT IN THE STRINGER FROM THE EXISTING FACTORDec 13, 1995 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L954688Web · crackedFOUND ON E2 LETTER CK, .2187 INCH CRACK IN 48 SECT TORQUE BOX WEB LIGHTENING HOLE RT FWD SIDE. REPAIRED PER MM 53-11-0.Dec 12, 1995 · N504DA · Boeing 727232 · Fuselage Miscellaneous Structure
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