N980Z, cancelled Aug 24, 2001

Service difficulty reports · 38

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 = 'N980Z' AND deregistration_id = 'N980Z-2001-08-24'
  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 TWAA9915703Power Supply · wornTHE EGRESS LIGHTS ON LEFT SIDE OF CABIN, ROWS 15 TO 22, FLASHED DURING FLIGHT WITH THE SWITCH IN THE ARM POSITION. REPLACED THE POWER SUPPLY FOR ROWS 15 TO 22. CHECK-C 9-23-99 STL.Nov 17, 1999 · N980Z · Doug DC931 · Emergency LightingSDR TWAA9914202Connector · looseTHE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. RESEATED THE EGRESS POWER STRIP CONNECTOR THAT HAD BECOME LOOSE. CHECK-C 9-23-99 STL.Oct 17, 1999 · N980Z · Doug DC931 · Emergency LightingSDR TWAA9812707Frame · corrodedDURING OP 15 MAINT CHECK AT FWD AIRSTAIR, FOUND CORROSION ON DOOR CUTOUT INSIDE SURFACE AT CENTER AND AFT CORNER OF DOOR. REPLACED FRAME AND WEB WITH NEW PARTS, INSTALLED FASTENERS PER SRM 51-60-0, 51-30-02, AND SSRM 51-40-501.Aug 3, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812205Skin · damagedDURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B TOP SKIN PANEL WITH REPAIR. FABRICATED NEW PANEL PER DAC SRM 55-03, PG 23 AND 24. INSTALLED NEW PANEL PER DAC DWG 5910412-1.Jul 24, 1998 · N980Z · Doug DC931 · Elevator, Plate/SkinSDR TWAA9812204Skin · damagedDURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B T/E WITH STRIPPER DAMAGE. REMOVED AND REPLACED THE T/E PER DAC DWG 5910412-1.Jul 24, 1998 · N980Z · Doug DC931 · Elevator, Plate/SkinSDR TWAA9812202Skin · damagedDURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B LOWER SKIN PANEL WITH 2 REPAIRS. INSTALLED NEW LOWER PANEL, O/B END PER DAC DWG 5910412-1.Jul 24, 1998 · N980Z · Doug DC931 · Elevator, Plate/SkinSDR TWAA9812132Support · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT AT FS 200 TO 205, RBL 53. REMOVED CORRODED FLOOR SUPPORT FROM STA 160 TO 205. MADE NEW PART, INSTALLED WITH SAME TYPE AND SIZE FASTENERS PER SRM 53-11-1, PG 47 ITEM 10.Jul 23, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812213Skin · delaminatedDURING OP 15 MAINT CHECK, FOUND RT ELEVATOR O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED THE O/B TRAILING EDGE PER DWG 5910412-516.Jul 21, 1998 · N980Z · Doug DC931 · Elevator, Plate/SkinSDR TWAA9812125Skin · damagedDURING OP 15 MAINT CHECK, FOUND RT ELEVATOR LOWER O/B SKIN PANEL WITH 2 CREASES. REMOVED AND REPLACED LOWER O/B SKIN PANEL PER DWG 5910412-516.Jul 21, 1998 · N980Z · Doug DC931 · Elevator, Plate/SkinSDR TWAA9812135Support · damagedDURING OP 15 MAINT CHECK, FOUND CABIN FLOOR SUPPORT GROUND OUT OF LIMITS AT LBL 49, STA 180 TO 195. FABRICATED NEW FLOOR SUPPORT FROM 70757-6 EXT PER SRM 53-11-1, PAGE 47 ITEM 10.Jul 20, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812134Floor Track · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK NR 3, FS 200 TO 240. REMOVED CORRODED FLOOR TRACK AND REPLACED WITH NEW FROM STA 200 TO FACTORY SPLICE AT STA 267.Jul 20, 1998 · N980Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9812133Floor Track · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK NR 4, FS 200 TO 240. INSTALLED NEW TRACK STA 200 TO FACTORY SPLICE STA 267.Jul 20, 1998 · N980Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9812020Door Frame · misdrilledDURING OP 15 MAINT CHECK, FOUND .5 IN DIA HOLE AT FS 363.5, L29R, FORMER FOR DOOR FRAME CAP. REPAIRED PER ARA 92227.Jul 17, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812019Hinge · crackedDURING OP 15 MAINT CHECK, FOUND LT MLG STRUT DOOR HINGE, NR 5 HINGE LUG ON WING SIDE OF HINGE, CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED DOOR HINGE MFG (P/N 2924290-501) PER DWG 5910484. TORQUE FASTENERS PER SRM 51-30-1P PG 13. REAMED HOLES PER SRM 51Jul 16, 1998 · N980Z · Doug DC931 · Landing Gear DoorsSDR TWAA9812018Floorbeam · corrodedDURING OP 15 MAINT CHECK, FS 996, LBL 21 TO LBL 41, CORROSION REMOVED ON FLOORBEAM CAP WAS BEYOND LIMITS. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 20A.Jul 16, 1998 · N980Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9812014Support · crackedDURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT CAP, ATTACH TO FORMER, CRACKED AT FS 446 ABOVE LONGERON 28. REMOVED FLOOR SUPPORT, WELDED PER SHOP TAG NR 795242. REINSTALLED FLOOR SUPPORT.Jul 15, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812017Doubler · crackedDURING OP 15 MAINT CHECK, FOUND DOUBLER ABOVE LONGERON 16R AT STA 980 WAS CRACKED. REMOVED DAMAGED PART, FORMED NEW PART ONE GAUGE HEAVIER, PAINTED AND INSTALLED WITH FASTENERS LIKE REMOVED.Jul 14, 1998 · N980Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9812016Casting · crackedDURING OP 15 MAINT CHECK, FOUND 1 INCH CRACK ON RT WING T/E FLAP O/B HINGE CASTING, O/B UPPER ATTACH FLANGE. REPLACED CRACKED FRAME WITH PART NR 165489. INSTALLED FASTENERS PER SRM 51-30-2.Jul 14, 1998 · N980Z · Doug DC931 · Wing, Control Surface Attach FittingsSDR TWAA9812015Casting · crackedDURING OP 15 MAINT CHECK, FOUND CRACK ON RT WING T/E FLAP O/B HINGE CASTING, I/B UPPER ATTACH FRAME. REPLACED CRACKED FRAME WITH NEW FRAME AND INSTALLED FASTENERS PER SRM 51-30-2.Jul 14, 1998 · N980Z · Doug DC931 · Wing, Control Surface Attach FittingsSDR TWAA9812103Pan · damagedDURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 018 ON RT AFT EMERGENCY EXIT DOOR PAN. REPAIRED EMERG EXIT DOOR PAN PER SRM 52-05 CONFIG -7003.Jul 13, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9812101Skin · crackedDURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 016 ON ELECTRONIC COMPT ACCESS DOOR CUTOUT. REPAIRED PER ARA 9222.Jul 13, 1998 · N980Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9812013Frame · crackedDURING OP 15 MAINT CHECK, FOUND CRACK IN FORMER FOOT STA 945, BETWEEN L14L AND L15L. REMOVED AND DISCARDED FORMER FRAME, INSTALLED NEW TWA STOCK NR 16-0585 FRAME PER SRM 53-03, FIG 3.Jul 13, 1998 · N980Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9812012Skin · crackedDURING OP 15 MAINT CHECK, FOUND RT STAB L/E CRACKED 3 INCHES IN UPPER FLANGE OF L/E SECT AT XFS 40. FABRICATED DOUBLER AND INSTALLED PER SRM 55-01, PAGE 8.Jul 13, 1998 · N980Z · Doug DC931 · Horizontal Stabilizer, Plate/SkinSDR TWAA9812011Angle · crackedDURING OP 15 MAINT CHECK, FOUND LOWER ATTACH ANGLE AT FUSELAGE CRACKED 1.5 IN AT FWD END OF NR 1 PYLON. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE FROM 177PH STEEL, .040 IN. INSTALLED WITH MONEL RIVETS REF DWG 5923062.Jul 13, 1998 · N980Z · Doug DC931 · Nacelle/Pylon StructureSDR TWAA9812010Longeron · crackedDURING OP 15 MAINT CHECK, FOUND LONGERON 17R CRACKED AT STA 965. REPLACED CRACKED LONGERON PER SRM 53-02, PG 48 TO 53. INSTALLED RIVETS COMMON TO SKIN AND LONGERON PER SRM 51-30, PG 1 AND 6. USED MS 20615-M-4 AND AN960B4 WASHERS.Jul 13, 1998 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9812102Pan · damagedDURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 018 ON RT FWD EMERGENCY EXIT DOOR PAN. REPAIRED EMERGENCY EXIT DOOR PER SRM 52-05, PG 300, CONFIG 7003.Jul 8, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9811008Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT FLANGE OF LONGERON 4L CRACKED AT ATTACHMENT TO FORMER AT FS 200. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097 AD-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,1Jul 7, 1998 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9811007Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L WITH CRACKED FLANGES AT STA 160. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jul 7, 1998 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9811006Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT FS 200. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN AND LONGERON WITH NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jul 7, 1998 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9812402Skin · crackedDURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN CRACKED AT STA 389, LONGERON 28 AND 29R. REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR PER SRM 53-04, FIG 12B SHEET 3, AND ARA 9223 WHICH REMOVED SLOT 3 IN BY 1 IN IN AREA OF CRACK.Jun 29, 1998 · N980Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9810807Doubler · misinstalledMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO DOOR, AFT JAMB WITH DOUBLER INSTALLED USING BLIND FASTENERS. INSTALLED DOUBLER PER SRM 53-05, FIG 80. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jun 24, 1998 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9810718Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CLASS 3 REPAIR INSTALLED AT AFT END OF REAR CARGO DOOR CUT-OUT. INSTALLED CLASS 1 REPAIR PER SRM 53-05, FIG 80. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jun 24, 1998 · N980Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9712803Panel · crackedSTL - DURING MAINTENANCE, A CRACK WAS REPAIRED IN THE PRESSURE PANEL AT STATION 85 RIGHT TUNNEL OUTBOARD SIDE. (M)Oct 29, 1997 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 95ZZZW750Door Latch · out of adjustSTL - AFTER TAKEOFF RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION, AND LANDING GEAR DOOR OPENED DURING UPLATCH CHECK. FOUND DOOR LATCH MECHANISM, MFG P/N 5915169-5506, WOULD NOT ALWAYS ENGAGE DOOR ROLLERS. RIGGED DOOMay 20, 1995 · N980Z · Doug DC931 · Landing Gear Door Retract SectionSDR 95ZZZW740Fitting · crackedSTL - DURING OP-15, FOUND 12 INCH CRACK IN LEFT PORK CHOP FITTING HORIZONTAL LEG. REPLACED LEFT PORK CHOP FITTING PER DOUGLAS MM 20-10, 20-14, 20-16 AND PER TWA STANDARD PRACTICES. (W)May 2, 1995 · N980Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 95ZZZX2345Longeron · gougedSTL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STA 1000. REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02. AIRCRAFT TOTAL TIME: 62,133 HOURS; 75,010 CYCLES.Apr 12, 1995 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZW605Longeron · gougedSTL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STATION 1000. REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02.Apr 12, 1995 · N980Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZX851Downlock Switch · failedSTL - FLT 641 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR. REPLACED RIGHT MLG DOWNLOCK SWITCH, MFG PN H14-6. LANDING GEAR OPERATION AND POSITION AND WARNING SYSTEM CHECKED NORMAL. CHECK Feb 1, 1995 · N980Z · Doug DC931 · Landing Gear Position and Warning
Back to N980Z, cancelled Aug 24, 2001