N508DA, cancelled Sep 16, 2003

Service difficulty reports · 68

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 = 'N508DA' AND deregistration_id = 'N508DA-2003-09-16'
  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 DL72L020038Skin · corrodedTHE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 1030 & 1050 AT STRINGER 28L. THE CORROSION WAS REMOVED WITH A 16 X 4 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH A DOUBLER PER ER/A 382438-14, REV A.Jan 11, 2002 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L020035Beam · crackedINSPECTION OF THE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER AD 94-07-08 AND BAC S/B 727-53-0129 REVEALED TYPICAL CRACKS IN THE FS 1263 AND 1273 HORIZONTAL BEAM CAPS. THE CRACKED MEMBERS WERE REMOVED AND NEW PARTS INSTALLED PER ER/A 382433-14AD.Jan 10, 2002 · N508DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L020031Skin · crackedFOUND ON B1 LETTER CHECK RT ELEVATOR LOWER SKIN IS CRACKED FWD OF TAB. REPAIRED PER B-727 DRD 55-20-3D FIG 4.Jan 10, 2002 · N508DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72L020032Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK I/B SIDE. REPLACED STIFFENER PER M/M.Jan 9, 2002 · N508DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L010922Angle · crackedFOUND ON A2 LETTER CK, .25 INCH CRACK NR 4 SLAT T/E CHORD AT O/B TRACK CUTOUT. REPAIRED PER MM 57-54-000-8.Jun 6, 2001 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002152Fitting · corrodedTHE VERTICAL STABILIZER TENSION TIE FITTING FORWARD AND AFT ATTACH BOLT HOLES WERE FOUND WITH CORROSION IN THE BORES. THE BORES WERE OVERSIZED AND BUSHED PER ERA 396341-14 AT HMV.Nov 2, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Attach FittingsSDR DL72L002114Beam · corrodedLT MLG BEAM LOWER FACE CORRODED AT LWR T/E PANEL BORES 2, 5, 6, 7, 8, 9, 11, 12, 14, 15, 28. ALL WORK ACCOMPLISHED PER ERA NR 396313-14, NO REVISION.Oct 26, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L002109Structure · damagedAFT END OF DOGHOUSE 6 O''CLOCK POSITION DOUBLER PEELED BACK ON BOTH SIDES OF INLET SKIN BUTT JOINT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE PENETRANT INSP AREA, NO CRACKS FOUND SRM 54-10-10-3D. CHEMICAL TREATED PER 900-2-4 NR 02. APPLIED EPOXY PRIMEOct 25, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72L002108Beam · corrodedLT MLG BEAM LWR T/E PNL BORES CORRODED. REAMED HOLES 34, 35, 36, 37 AND 18 TO .312 PER SRM 57-40D. REAMED HOLES 28 AND 39 TO .359 PER SRM 57-40D. REAMED HOLE 32 TO .312 PER SRM 57-40-D. BHEC INSP OF FASTENER FOR CRACKS AND CORROSION. NO ITEM. TURNED O/B Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L002107Beam · corrodedLT MLG BEAM HOLES BORES NR 2, 5, 6, 7, 8, 9, 11, 12, 14, 15 AND 28 SHOW CORROSION. REAMED HOLES 2, 5 6, 7, 8, 9, 11, 12, 14, 15 TO .312. HOLE 28 TO .359 PER SRM 57-40-D. BHEC INSP OF FASTENERS FOR CRACKS AND COROSION. NO ITEMS. TURNED O/B ON IN PROCESS Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L002094Fitting · crackedDURING INSPECTIONS REQUIRED BY AD 97-05-08 6 CRACKS WERE FOUND IN THE NR 1 FORWARD ENGINE PYLON AND ONE CRACK WAS FOUND IN THE NR 3 PYLON. ERA 396334-14AD OVERSIZES THE FASTENER HOLES TO REMOVE THE CRACK PER FEDEX AVIATION SERVICES S/B 2000-5410A01 AT HMV.Oct 24, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72L011138Angle · crackedDURING SHOP VISIT THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT.Oct 20, 2000 · N508DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L002061Skin · crackedCRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1070 AND FS 1090. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5 PER ERA 396320-14AD AT HMV.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002060Skin · crackedSKIN CRACKS WERE FOUND IN THE STR 4L LAP JOINT BETWEEN FS 1050 AND 1070. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396304-14AD.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002059Skin · crackedCRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1030 AND FS 1050. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396305-14AD.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002058Skin · crackedCRACKS WERE FOUND IN THE STR 26L LAP JOINT BETWEEN FS 600 AND FS 620. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396310-14AD SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002054Skin · crackedMULTIPLE CRACKS WERE FOUND BETWEEN FS 481 AND FS 681 IN THE STR 4R LAP JOINT. THE CRACKS WERE REMOVED AND REPAIRED PER ERA 396303-14 AT HMV.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002023Beam · corrodedLT MLG BEAM LWR T/E PANEL ATTACH BORES CORRODED. HOLES 35, 29, 27, 26, 25 REAMED TO .312 PER SRM 57-40D. 28 REAMED TO .359 PER SRM 57-40D. REAMED 10 8 TO .312 PER SRM 57-40D. BHEC INSPECT OF FASTENER HOLE FOR CRACKS AND CORROSION. NO ITEM, TURNED O/D ON Oct 16, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L010887Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED ON THE MID FLAP. THE CHORD ANGLE WAS REPAIRED PER 727 M/M 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.Oct 13, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L002095Skin · corrodedLOWER SECTION OF BONDED DOUBLER FOUND DISBONDED BELOW THE AFT LAV SERVICE PANEL CUTOUT. 396323-14 REV A.Oct 13, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L001972Beam · corrodedRT MLG SUPPORT BEAM BORES CORRODED. TASK: C57-581-01.01 FASTENER BORES CORRODED AT HOLES 3, 4, 5, 11, 12, 26, 27, 30, 31, 32, 36 & 38. REWORK HOLES PER DRD 57-40D. 3, 4, 5, 11, 26, 30, 31, 32, 36 REAMED TO 0.358. 27, 12, 13 REAMED TO 0.262. 38 REAMED TO 0Oct 11, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L002131Plate · corrodedAT HMV, THE VERT STAB TENSION TIE PLATE AFT CTR ATTACH POINTS WERE CORRODED AROUND FACE AND IN BORES. REMOVED CORR DYE PEN CK GOOD WITHIN LIMITS PER SRM 55-30-5D FIG 801D. REAMED HOLES TO .691 TI REM CIRR BHEC INSP NO ITEMS OPENED HOLES TO .737 BFEC INSP NO Oct 9, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L002020Rib · crackedAT HMV THE NR 11 RIB FLANGE OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE, FABRICATED REPAIR PARTS PER MM 57-54-0, REPAIRED PER MM 57-54-0.Oct 9, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002021Shim · shiftedAT HMV THE SHIMS WERE FOUND MIGRATING AT NR 12 SPOILER ACTUATOR LOWER ATTACH BOLT SHIMS. REPAIRED SHIMS AND C/W MM 57-54-0.Oct 8, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72L002052Stringer · crackedAT HMV, THE FIFTH STRINGER AFT OF FRONT SPAR STA 171.5 WAS FOUND TO BE CRACKED. REMOVED DAMAGE PER SRM 57-10-5D FIG 802D. PERFORMED HFEC PER SRM 57-10-5D FIG 802D, NO IND. TREATED AND PAINTED PER SRM 57-10-5D FIG 802D. FABRICATED REPAIR PARTS PER SRM 57-10Oct 6, 2000 · N508DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L002019Rib · crackedAT HMV THE NR 13 RIB OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE FOR FABRICATED DOUBLER. REPAIRED PER MM 57-54-0.Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002018Rib · crackedAT HMV NR 7 RIB OF SLAT FOUND TO BE CRACKED. REMOVED LWR AFT SPAR REPAIR DOUBLER IN AREA, FABRICATED REPAIR DOUBLER PER MM 57-54-0, ROUTED OUT DAMAGE, INSTALLED DOUBLER AND FILLER PER MM 57-54-0, REINSTALLED SPAR DOUBLER.Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002084Web · crackedAT HMV, THE WEB ON THE VERTICAL FIN WAS FOUND CRACKED. REMOVED FASTENERS AND BEGAN FABR DOUBLER PER SRM 53-10-4D FIG 802D. STOP DRILLED CRACKS, COMPLETED FABR OF DOUBLER, DYE CKED, INSTALLED DOUBLER PER SRM 53-10-4D FIG 802D.Oct 5, 2000 · N508DA · Boeing 727232 · Vertical StabilizerSDR DL72L002083Flange · bentAT HMV, THE AFT FLANGE OF THE NR 2 INLET WAS TORN/BENT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE CKED, NO FURTHER DAMAGE NOTED. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-10-3D FIG 801D.Oct 5, 2000 · N508DA · Boeing 727232 · Turbine Engine Air Inlet SectionSDR DL72L001982Cowling · wornAT HMV FOUND NR 2 ENG COWL RING WORN NR 2 FWD COWL, 5 O''CLOCK TO 7 O''CLOCK NO ED FOR RIVETS. REMOVED EXISTING REPAIR, FABD NEW REPAIR PER MM 53-11-0 PG 801, INSTALLED NEW COWL RING PER MM 53-11-0 PG 801, APPLIED TEFLON COATING PER PS 900-3-1, 04.Oct 5, 2000 · N508DA · Boeing 727232 · Engine Cowling SystemSDR DL72L001981Frame · crackedAT HMV FOUND FORMER CRACKED, STA 600, LBL 10. ROUTED OUT CRACK PER SRM 53-10-4D FIG 811D, FABD REPAIR, T/P PER SRM 51-40-3, INSTALLED PER SRM 51-40-3.Oct 5, 2000 · N508DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L001963Beam · corrodedAT HMV FOUND RT MLG SUPPORT BEAM BORES CORRODED. FASTENER BORES CORRODED AT HOLES, 17/18/19/22/23/24/39/40/41/42/43/44/45/46. REWORKED CORRODED HOLES PER DRD 57-40D FIG 803D, ALL HOLES ARE 0.312, BHEC INSP OF HOLES LISTED PER DRD 57-40D, SHOWS NO ITEMS.Oct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L001962Beam · corrodedAT HMV BHEC OF BEAM NR HOLE 25 ON RMLG SUPPORT BEAM SHOWS CORROSION IN HOLES. REWORK HOLE NR 25 PER DRD 57-40D FIG 803D, NR 25 0.358, BHEC INSP OF HOLE PER DRD 57-40 CKD OK, MECH AND TREATED BUSHINGS PER SRM 57-40D INSTALLED BUSHING PER SRM 57-40D PG 14, STEOOct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L001941Flap Track · corrodedDURING OVERHAUL AT BFGOODRICH, SEVERAL AREAS OF THE I/B FLAP, NR 4 I/B TRACK WERE FOUND WITH CORROSION/WEAR WHICH WERE BEYOND ALLOWABLE LIMITS. AFFECTED AREAS INCLUDE THE MLG BEAM ATTACH HOLES AND SPOTFACE, THE SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGOct 5, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L001940Flap Track · corrodedDURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS, AND WEAR AT THE FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, SPACER BLOCK ATTACH HOLES, AND CLIP ASSY ATTACH HOLES, AT THE MLG BOct 5, 2000 · N508DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L001980Bolt · looseAT HMV FOUND LW NR 4 SPOILER ACTUATOR MOUNT HAS LOOSE BOLTS ON BOTTOM OF WING SPAR TO MOUNT BOLTS. TIGHTENED NUT.Oct 4, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72L001965Actuator · looseAT HMV THE NR 3 SPOILER ACTUATOR WAS FOUND TO HAVE LOOSE MOUNT BOLTS ON BOTTOM ATTACHED TO REAR SPAR. REPAIRED PER MM 57-42-0.Oct 4, 2000 · N508DA · Boeing 727232 · Drag Control ActuatorSDR DL72L001945Mount · looseAT HMV FOUND NR 1 SPOILER MOUNT BOX ATTACHED TO REPAIR SPAR IS LOOSE AT BOTTOM BOLTS. REPAIRED PER MM 57-42-0.Oct 4, 2000 · N508DA · Boeing 727232 · SpoilersSDR DL72L992526Engine · unresponsiveNR 1 ENG THROTTLE DID NOT RESPOND TO CONTROL. RECONNECTED THROTTLE ROD LINKAGE, RAN ENG PER PFHB. OP CHECKS GOOD.Nov 15, 1999 · N508DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72L992410Stud · missingNR 1 ENG RAPID OIL LOSS, LOW OIL PRESS LT ILLUM AND QTY WENT TO ZERO. SHUTDOWN ENG PER POM. FOUND .25 INCH STUD MISSING FROM FRONT GEARBOX COVER. REINSTALLED STUD PER 727 M/M 72-61-02.Oct 31, 1999 · N508DA · Boeing 727232 · Turbine Engine Reduction GearSDR DL72L992180Batteries · dischargedBATTERIES WEAK IN FWD COACH CLASS CABIN OVERHEAD EMERGENCY LIGHT. REPLACED BATTERIES.Sep 30, 1999 · N508DA · Boeing 727232 · Emergency LightingSDR DL72L991253Wire · damagedON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION IN ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL24May 18, 1999 · N508DA · Boeing 727232 · Electrical Power System WiringSDR DL72L982003Floorbeam · corrodedFLOORBEAM CAP CORRODED STA 344 LBL 40 TO 48. REPAIRED PER 272 SRM 53-10-8.Sep 22, 1998 · N508DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72L981978Fitting · wornFITTING WORN ON LT AFT SERVICE DOOR AFT LOWER EDGE OF DOOR. C/W MM 52-14-0 FIG 805.Sep 22, 1998 · N508DA · Boeing 727232 · Service DoorsSDR DL72L981043Web · crackedFOUND AT E-1 LETTER CHECK, WEB CRACKED LT SIDE ABOVE LIGHTENING HOLE AFT STAIR AREA STA 1223. REPAIRED PER M/M53-11-0.May 15, 1998 · N508DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981042Angle · crackedFOUND ON E1 LETTER CK, 1 INCH CRACK INBD ATTACH CASTING NR 5 L/E SLAT ACTUATOR. REPLACED ANGLE.May 15, 1998 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L981041Angle · crackedFOUND ON E1 LETTER CK, 1.25 INCH CRACK INBD ATTACH CASTING FOR NR 4 L/E EDGE SLAT ACTUATOR. REPLACED ANGLE.May 15, 1998 · N508DA · Boeing 727232 · Leading Edge DevicesSDR DL72L981039Web · crackedFOUND AT E1 LETTER CHECK, WEB CRACKED RT SIDE FWD UPPER LIGHTENING HOLE REPAIRED PER M/M 53-11-0.May 15, 1998 · N508DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L980321Torque Tube · failedUPON T/O, AFTER GEAR RETRACTION (DOORS LIGHT REMAINED ILLUMINATED AND RT GEAR DOOR LIGHT ON S/O PNL WAS ON. ADDITIONALLY RT GEAR AND GREEN GEAR LIGHTS REMAINED ILL.VISUAL INSP CONFIRMED RMLG WAS DWN. ACCOMPLISHED POM WITH GEAR HANDLE UP POS THE LIGHTS REMAINFeb 5, 1998 · N508DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72L980216Light · inoperativeAFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.Jan 26, 1998 · N508DA · Boeing 727232 · Emergency Lighting
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