N988Z, cancelled May 1, 2013

Service difficulty reports · 48

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 = 'N988Z' AND deregistration_id = 'N988Z-2013-05-01'
  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 ZW0A0104806Longeron · crackedCRACK IN LONGERON AT STATION 617 FRAME .5 INCH LONG. REPAIRED LONGERON IAW DAC REWORK DRAWING SR09530128 AND SRM 53-02.Jul 8, 2001 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9917415Door Frame · crackedDURING CHECK-C MAINT, FOUND A FORWARD LT PASSENGER DOOR STOP HOLE, FOURTH HOLE FROM THE TOP ON THE AFT SIDE AND FIFTH FROM THE BOTTOM, AFT SIDE. THE DOOR STOP HOLE HAD A .75 IN CRACK. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND INSTALLED DOUBLER PER EMLR 9Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9917402Longeron · crackedDURING CHECK-C MAINT, THE AFT END OF LONGERON 2L WAS CRACKED AT STA 1076. COMPLETED LONGERON SPLICE PER SRM 53-02, FIG 8.Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9917401Longeron · crackedDURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT STA 1076. REPAIRED LONGERON 2R AT STA 1076 PER SRM 53-02, FIG 8.Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9917403Angle · crackedDURING CHECK-C MAINT, THE FUSELAGE TO VERTICAL STAB ATTACH ANGLE WAS CRACKED .875 INCH LONG AT RT SIDE, STA 1121. CRACK IS BEYOND STOP DRILLED HOLES OF LOWER LEG CRACK. REPAIRED PER SRM 53-05, FIG 230. DOUBLER INSTALLED.Dec 23, 1999 · N988Z · Doug DC931 · Vertical StabilizerSDR TWAA9817302Angle · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM SUPPORT ANGLE CRACKED AT STA 680 LBL 43 IN. INSTALLED NEW FITTING (P/N 3916209-501N), USING TENSION HEAD HI-LOKS AND LIKE FASTENERS.Oct 26, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9817301Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT STA 208 TO 217, LONGERON 18L. REPLACED MEMBRANE PER SRM 53-05 FIG 55 SHEET 2 AND FASTENER SUB PER SRM 51-60-0 AND ARA 15704.Oct 26, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816804Angle · crackedDURING OP 16 MAINT CHECK, FOUND RT WING OTBD SPOILER, OTBD DOWN STOP ANGLE WAS CRACKED ON THE INBD SIDE. INSTALLED NEW TEE ANGLE, MFG 5918134-1, PER SRM 51-01, PG 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED FASTENERS PER SRM 51-30-0.Oct 16, 1998 · N988Z · Doug DC931 · SpoilersSDR TWAA9816405Former · corrodedDURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON THE FORMER CAP AT STA 897, LONGERON 27L TO 29L. REPLACED FORMER CAP PER STANDARD PROCESSES MANUAL 6-70-1.Oct 16, 1998 · N988Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9816503Membrane · puncturedDURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 947, RBL 50 IN, WAS PUNCTURED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 2 ROWS OF RIVETS ON 0.040 DOUBLER.Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816502Membrane · crackedDURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 958, LBL 50 IN, WAS CRACKED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 3 ROWS OF RIVETS ON 0.040 DOUBLER.Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816314Longeron · crackedDURING OP 16 MAINT CHECK, FOUND RT LAV STA 980 LONGERON 14R WITH 2 IN CRACK IN FORMER FOOT. REPAIRED PER MO72J14H, DRAWING J060119, AND ARA 15706.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9816313Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LT LAV STA 980 LONGERON 14L WITH 2 IN CRACK IN FORMER FOOT. REPLACED CRACKED FORMER WITH DAC P/N J060119-17 FORMER PER MO72J14 PHASE G, AND ARA 15706.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9816311Former · crackedDURING OP 16 MAINT CHECK, FOUND STA 996 FORMER RING FOOT CRACKED ABOVE AND BELOW LONGERON 19L. REMOVED AND REPLACED FORMER RING FOOT SECTION WITH NEW SECTION PART A5910163-79 PER SRM 51-31-0, AND TWA STANDARD PROCEDURES.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9816103Former · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT BOTTOM FWD SIDE OF FORMER RING BELOW CABIN FLOOR STA 658 LT. REPAIRED PER SRM 53-03, FIG 16. INSTALLED DOUBLER WITH HI-LOKS AS REQUIRED.Oct 5, 1998 · N988Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9816312Buklhead Web · crackedDURING OP 16 MAINT CHECK, FOUND AT RT FUSELAGE BULKHEAD WEB AT STA 965.091, PYLON FROM SPAR LOWER CAP, HIGH FREQ EDDY CURRENT INDICATED CRACK IN LOWER OTBD BOLT HOLE. REAMED HOLE SIZE TO .02807 AND ELIMINATED.Oct 1, 1998 · N988Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9815903Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND NR 4 CABIN CHAIR TRACK CORRODED AT STA 218 TO 237. CORRODED SECTION OF TRACK REMOVED AND NEW SECTION INSTALLED WITH EXISTING HARDWARE.Sep 30, 1998 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9815902Panel · corrodedDURING OP 16 MAINT CHECK, FOUND PANEL ABOVE O/B END OF LT AILERON, 8 IN TO 17 IN FROM O/B END, WAS CORRODED AND DELAMINATED. INSTALLED NEW CORE AND ALUM SKIN PER SRM 51-70-2 HOT BOND PROCEDURE PER SERVICEABLE TAG.Sep 30, 1998 · N988Z · Doug DC931 · Wing, Plate/SkinSDR TWAA9815802Pan · wornDURING OP 16 MAINT CHECK, FOUND PAN IN FWD ACCESSORY COMPT WITH INTERIM REPAIR INSTALLED PER ARA 11869 AND ARA 11870. REPLACED PAN AND REPAIRED PER ARA 15700, AND SRM 51-30-00 AND SRM 51-30-2.Sep 28, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9815801Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT, STA 218 TO 237, WAS CORRODED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01.Sep 25, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816006Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STA 813. CORROSION WAS APPROX 0.008 DEEP AND 3 IN BY 3 IN. REMOVED CORROSION AND REPAIRED WITH ALUM 2024-T3, 0.032 IN PER SRM 53-01, PAGE 9 FIG 2.Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9815312Stringer · corrodedDURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT BOTH SIDE FLANGES AT STA 200. REPLACED LONGERON MFG PART NR 5911406-13, USING FASTENERS PER SRM 51-30-0.Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9815311Floor · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 20 WAS CORRODED THROUGH AND HAD BROKEN SUPPORT CHANNELS. FABRICATED NEW FLOOR PANEL PER SRM 53-00-64, FIG 201 PAGE 201.Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Floor PanelSDR TWAA9815310Support · brokenDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 34 WITH BROKEN SUPPORT CHANNELS. REMOVED AND INSTALLED NEW SUPPORT CHANNELS.Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9815309Floor · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 19 WITH CORROSION AND SEVERAL BROKEN SUPPORT CHANNELS. REPLACED CABIN FLOOR PANEL SHEET/HAT SECTION PER SRM 53-00-14, PAGE 201.Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Floor PanelSDR TWAA9815308Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM WITH CORROSION, STA 237 TO 313. REPLACED SUPPORT ANGLE STA 237 TO 258. REMOVED CORROSION FROM STA 258 TO 313.Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9814708Seat Track · corrodedCHAIR TRACK GROUND BEYOND LIMITS TO REMOVE CORROSION AT STA 200 TO 237, RBL 23 IN. REMOVED CHAIR TRACK AND REPLACED WITH NEW TRACK. INSTALLED WITH FASTENERS PER SRM 51-30-0.Sep 11, 1998 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9814707Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED AT STA 200. REPLACED LONGERON USING FASTENERS PER SRM 51-30-0.Sep 11, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9814310Bulkhd Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND .75 INCH CRACK AT UPPER RIVET HOLE ON VERT STIFFENER, AFT SIDE OF BULKHEAD, BETWEEN LONG 3L AND 4L. REPLACED TIE CLIP, UPPER END OF STIFFENER, WITH FASTENERS PER SRM 51-30-0.Sep 2, 1998 · N988Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9814309Pan · crackedDURING OP 16 MAINT CHECK, FOUND LT FWD EMERGENCY EXIT DOOR PAN CRACKED, WITH INTERIM REPAIR INSTALLED. INSTALLED NEW PAN STOCK NR 63-3273.Sep 2, 1998 · N988Z · Doug DC931 · Emergency ExitsSDR TWAA9814308Rib · crackedDURING OP 16 MAINT CHECK, FOUND LT WING TE, I/B RIB CRACKED IN RADIUS BELOW BOLT HOLE, INSIDE FLAP AT O/B HINGE ARM. REPLACED I/B RIB PER SRM 57-50-3, PAGES 9 AND 10. IPC 27-50-01, FIG 2B PAGES 0 TO 7.Sep 2, 1998 · N988Z · Doug DC931 · Trailing Edge FlapsSDR TWAA9814307Rib · crackedDURING OP 16 MAINT CHECK, FOUND LT WING TE O/B RIB CRACKED AT TOP BOLT HOLE INSIDE FLAP AT O/B HINGE ARM. REPLACED O/B RIB PER SRM 57-50-3, PAGE 9 AND 10, IPC 27-50-01, FIG 2B PAGE 0 TO 7.Sep 2, 1998 · N988Z · Doug DC931 · Trailing Edge FlapsSDR TWAA9814306Skin · corrodedDURING OP 16 MAINT CHECK, FOUND SLIGHT BULGE IN SKIN WITH STRESSED FASTENERS AND BLIND FASTENERS INSTALLED AT STA 29L, JUST AFT OF ELECTRONIC COMPT DOOR. BLENDED DENT AREA AND INSTALLED .025 TITANIUM INTERNAL DOUBLER PER SRM 53.04, FIG 38 SHEET 28 PAGE 218H.Aug 27, 1998 · N988Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9812129Longeron · crackedDURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 680 WITH .750 INCH CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WORK CARD MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02. CHECK-C 1-8-98 STL.Jul 22, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9812128Longeron · crackedDURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 658 WITH .750 IN CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WORK SHEET MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02 AS REQUIRED. CHECK-C 1-8-98 STL.Jul 22, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9784001Lights · illuminatedSTL - FLT 583 - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED. OPERATIONAL CHECK OF EMERGENCY LIGHTS COMPLETED, NO DEFECTS NOTED. CHECK C - 10-30-96 - STL. (X)Jul 24, 1997 · N988Z · Doug DC931 · Emergency LightingSDR TWAA9727004Engine · failedDSM - FLT 382 - DURING CLIMB, NR 1 ENGINE, S/N 2161, OIL FILTER CLOG LIGHT ILLUMINATED. CHANGED ENGINE S/N 2161. (M)Feb 24, 1997 · N988Z · Doug DC931 · Engine (Turbine/Turboprop)SDR TWAA9613304Fitting · crackedSTL - DURING SPECIAL CHECK, FOUND END FITTING OF LONGERON 30 CRACKED, STATION 598. REPLACED FITTING PER SRM 51-00 AND TWA STANDARD PRACTICES. (M)Oct 26, 1996 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 96ZZZM1339Anti Retract Mec · out of adjustSTL - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED TO RETRACT, LANDING GEAR DID NOT RETRACT. FOUND ANTI-RETRACT LATCH OUT OF ADJUSTMENT. RIGGED ANTI-RETRACT MECHANISM. LANDING GEAR OPERATIONS THEN CHECKED NORMAL. (M)Aug 9, 1996 · N988Z · Doug DC931 · Landing Gear Retraction/Extension SystemSDR 96ZZZX307Duct · crackedSTL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED. REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND. OP-15 - 8-21-95 - STL.Jan 8, 1996 · N988Z · Doug DC931 · Pneumatic Distribution SystemSDR 95ZZZM680Fuel Tank · leakingATL - DURING CRUISE, FUEL SMELL DETECTED IN CABIN. FOUND FUEL LEAK FROM CENTER TANK IN RIGHT WHEEL WELL.Oct 18, 1995 · N988Z · Doug DC931 · Fuel StorageSDR 95ZZZX5144Downlock Switch · malfunctionedSTL - FLT 693 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED NOSE LANDING GEAR GREEN, LOCKED LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND GREEN LOCKED LIGHT ILLUMINATED. FOUND DEFECTIVE NOSE GEAR DOWNLOCK SWITCH, MFG PN H14-6. REPLACED NOSE GEAR DOWNSep 1, 1995 · N988Z · Doug DC931 · Landing Gear Position and WarningSDR 95ZZZX5146Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STA 945 TO STA 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, SRM 51-30-2, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 67,006 HOURS; 73,957 CYCLES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM532Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. TOTAL CYCLES 73,957.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM531Seat Track · corrodedSTL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4. TOTAL CYCLES 73,957.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZM456Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM455Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM447Seat Track · corrodedSTL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
Back to N988Z, cancelled May 1, 2013