N997Z, cancelled Aug 24, 2001

Service difficulty reports · 52

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 = 'N997Z' AND deregistration_id = 'N997Z-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 TWAA0000502Actuator · wornCREW WAS UNABLE TO EXTEND THE NOSE LANDING GEAR DURING APPROACH TO MLI WAS NECESSARY TO USE MANUAL NOSE GEAR EXTENSION. FOUND PROBLEM WAS THE NOSE LANDING GEAR BUNGEE CYLINDER. MAINTENANCE FERRIED THE AIRCRAFT TO STL FOR REPLACEMENT. CHECK-C 8-28-99 STL.Jan 7, 2000 · N997Z · Doug DC932 · Landing Gear ActuatorSDR TWAA9911803Longeron · crackedDURING CHECK-C MAINT, LONGERON 2R WAS FOUND CRACKED AT END CAP STA 1076, A ONE INCH CRACK. REPAIRED PER SRM 53-02, FIG 8 AND 18.Aug 27, 1999 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9911802Longeron · crackedDURING CHECK-C MAINT, LONGERON 2L WAS FOUND CRACKED AT THE END CAP STA 1076, ONE INCH LONG. REPAIRED PER SRM 53-02, FIG 8 AND 18.Aug 27, 1999 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807202Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN BENEATH DOOR THRESHOLD HAD CORROSION AT STATION 916 TO 945, L29R TO L27R. REPAIRED AS PER ARA 15272 AND STD PRACTICES. (M)Apr 14, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9806914Bulkhead Angle · crackedDURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE TO BULKHEAD ATTACH ANGLE CRACKED BETWEEN LONG 15L AND 16L. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C, AND TWA STD PRACTICE. (M)Apr 3, 1998 · N997Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9806913Rib · wornMCI - DURING OP 15 MAINTENANCE CHECK, FOUND HOLE WORN THROUGH FLAP RIBS AT RT WING INBOARD AND OUTBOARD FLEX JOINT BOTTOM SIDE. REPLACED END RIBS PER SRM 51-01 AND TWA STD PRACTICE. (M)Apr 3, 1998 · N997Z · Doug DC932 · Trailing Edge FlapsSDR TWAA9806904Support · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN CHAIR AND FLOORBEAM SUPPORT CRACKED AT STATION 680, LBL 22 IN. REPLACED PART PER SRM 51-01-01 AND STANDARD PRACTICES. (M)Mar 31, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807105Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, LONGERONS 13 AND 14L. REPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X)Mar 30, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9806903Intercostal · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FS 1043 LBL 10.5 INCH INTERCOSTAL CRACKED ON LWR FLANGE, LEFT SIDE OF TAIL SKID CASTING. REPAIRED AND REINSTALLED PER SRM 53-01, FIG 2 PAGE 10. (M)Mar 30, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807304Spar Cap · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND STATION XRS 164 INSIDE TANK FWD FACE OF LOWER SPAR CAP, VERTICAL LEG WITH CRACK EXTENDING INTO LOWER RADIUS, BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG J060165 AND STD PROCEMar 27, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9807302Bulkhead Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE TO BULKHEAD ATTACH ANGLE CRACKED BETWEEN RT STRINGER 13 AND 14, ON FUSELAGE SIDE OF BULKHEAD STATION 965. REPLACED ANGLE PER SRM 51-01, PATE 1 ITEMC AND TWA STD PRACTICES. (M)Mar 27, 1998 · N997Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9807301Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND UPPER TE PANEL FORWARD OF RT WING AILERON UPPER SURFACE, OUTBOARD AREA HAD SEVERAL FASTENER HEADS STRESSED AND ALL SKIN PILLOWING. REPLACED TE SKIN PANEL, NEW PANEL INSTALLED PER SRM 51-01. (M)Mar 27, 1998 · N997Z · Doug DC932 · AileronsSDR TWAA9807207Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK AT APPROX STATION 964, LONGERON 22L, CORROSION ON DOUBLER INBOARD SIDE AND PELLED RIVETS AREA ON OUTER SKIN. REPLACED DOUBLER PER SRM 51-01, PG 1 ITEM C. (M)Mar 27, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806915Spar Cap · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT WING STATION XRS 164 INSIDE TANK, FWD FACE OF LOWER SPAR CAP, VERTICAL LEG HAD CRACK EXTENDING INTO LOWER RADIUS BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG JO60165 ANDMar 27, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9806906Skin · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR INNER SKIN CRACKED AT LOWER FWD CORNER OF DOOR. REPAIRED PER SRM 53-01, PAGE 8, AND STD PRACTICE. (M)Mar 27, 1998 · N997Z · Doug DC932 · Passenger/Crew DoorsSDR TWAA9806905Casting · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND TAIL SKID CASTING CRACKED AT STATION 1038, LBL 4 INCH, BOTTOM OF FORMER RING. REPLACED CASTING PER SRM 51-01, ITEM 1 PAGE C, AND STANDARD MAINTENANCE PRACTICE. (M)Mar 27, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806811Rivets · failedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 26L WITH A RIVET POPPED AT FS 354. REMOVED AND REPLACED RIVETS AS REQUIRED PER SRM 51-30-02. (M)Mar 27, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807204Spar Cap · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK. REPAIRED PER DAC DWG J060271 AND STANDARD PRACTICES. (M)Mar 23, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9806809Window Frame · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN WINDOW 23L HAD WINDOW TO FRAME TIE CRACKED. REPLACED WITH NEW FRAME PER SRM 51-10-1, PAGE 1 ITEM C. (M)Mar 23, 1998 · N997Z · Doug DC932 · Passenger Compartment WindowsSDR TWAA9805003Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 23L, STATION 945 TO 950. REMOVED CORROSION PER SRM 51-10-03. INSTALLED NEW PART PER SRM 51-01 PAGE 1 ITEM C. (M)Mar 23, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806104Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 23L CORRODED, STATION 945 TO 950. REMOVED CORROSION PER SRM 51-10-03. INSTALLED NEW PART PER SRM 51-01, PG 1 ITEM C. (M)Mar 22, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9809406Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TRAILING EDGE INBD FLAP REAR SPAR, INBD FLAP CASTING MOUNT HOLE LOWER INBD HOLE, WITH CRACK EXTENDING INTO RADIUS ON FWD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STA XRS 111.510 TO XRS 195.210, Mar 19, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9807303Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE INBOARD FLAP REAR SPAR INBOARD FLAP CASTING MOUNT HOLE, LOWER INBOARD HOLE, WITH CRACK EXTENDING INTO RADIUS FORWARD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STATION XRS 111.510 TO XRS 195.21Mar 19, 1998 · N997Z · Doug DC932 · Trailing Edge FlapsSDR TWAA9806922Longeron · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND LONGERON 14R AT STATION 1076 WITH CRACKED FORMER. REPAIRED FRAME PER SRM 53-03, FIG 4, AND STANDARD PRACTICES. (M)Mar 19, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807206Angle · crackedDURING OP 15 MAINTENANCE CHECK, FOUND AT RT STATION 980, FORMER RING TO FUSELAGE ATTACH ANGLE CRACKED AT 2 PLACES JUST BELOW LONGERON 15R. FORMER FOOT FORMED AND HEAT TREATED TO 7075 PER SRM 51-102A. INSTALLED NEW FORMER FOOT SECTION PER SRM 51-01, PAGE 1 ITMar 17, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807203Skin · dentedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN BEYOND LIMITS AT FS 503 BETWEEN L27 AND L38R, 5.5 INCH BY 2.5 INCH BY .175. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807104Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON TO CANTED KEEL FORMER TIE CRACKED AT STA 637, APPROX 15 LBL. REPLACED TIE PER SRM 51-01, PAGE 1 ITEM C. SEALED REPAIR PER SRM 51-20-0. (X)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807103Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, BETWEEN LONGERON 13 AND 14 RT SIDE. REPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9806912Doubler · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 26L AT STATION 902 'FINGER DOUBLER'. REPLACED FINGER DOUBLER PER SRM 51-01, PAGE 1 ITEM C. REMOVED CORROSION PER SRM 51-10-3. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806910Floor · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 560 AND 579, APPROX 58 INCH RBL, UNDER AFT END OF FLOOR PANEL 37. REPAIRED PER SRM 53-01, FIG 4. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Floor PanelSDR TWAA9806909Floor · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 579 AND 598, APPROX 58 INCH RBL, UNDER FWD END OF FLOOR PANEL 43. REPAIRED PER SRM 53-01, FIG 4. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Floor PanelSDR TWAA9806908Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 13R CRACKED AT STATION 1076. REPLACED LONGERON PER SRM 51-03, PAGE 1 ITEM C. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806907Longeron · crackedDURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 27R CRACKED AT STATION 541. REMOVED AND REPLACED WITH NEW PART PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9809405Casting · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND 718 CASTING CRACKED BEYOND PREVIOUS REPAIR ON AFT SIDE OF CASTING, RT SIDE OF ACFT. REMOVED AND REPLACED CASTING PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD MAINT PRACTICES. (X)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806921Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT CUSP ANGLE CRACKED AT STATION 996, 58.5 LBL, APPROX 4 INCH LONG. MANUFACTURED NEW TIE PLATE AND INSTALLED PER SRM 51-01, PAGE 1, AND TWA STANDARD PRACTICE. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806815Bulkhead Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND L ANGLE ON AFT PRESSURE BULKHEAD CRACKED AT S996, BELOW CUSP ANGLE LBL 58.5. REPLACED L ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9806814Former · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FORMER RING AT STATION 1076, LONGERON 15R, CRACKED. REPLACED PER SRM 53-03, FIG 4, AND STD PRACTICES. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806813Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 6L CRACKED AT STATION 639. INSTALLED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806812Skin · dentedDURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENT AT FS 980, S5R, .75 INCH BY .068. REPAIRED DENT PER SRM 53-04, PAGE 218K, FIG 38. SEALED REPAIR PER SRM 51-20. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807205Former · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON TO CANTED KEEL FORMER TIE CRACKED AT STATION 637, APPROX 15 IN RBL. REPLACED TIE PER SRM 51-01, PAGE 1 ITEM C. SEALED REPAIR PER SRM 51-20-0. (M)Mar 11, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806810Skin · crackedDURING OP15 MAINTENANCE CHECK, FOUND AFT CABIN FUSELAGE SKIN TO FORMER RING CRACKED AT STATION 945, BETWEEN L14 AND 15R. REPLACED PART PER SRM 51-01 PAGE 1 ITEM C. (M)Mar 11, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9803306Seat Track · corrodedMCI - DURING MAJOR MAINTENANCE CHECK, NR 4 CABIN CHAIR TRACK CORROSION WAS OUT OF LIMITS AFTER CLEAN UP. REPLACED FLOOR TRACK FROM STATION 200 TO 266 PER SRM 51-01 PAGE 1 ITEM C AND STANDARD PROCEDURES. (M)Mar 2, 1998 · N997Z · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9809403Jamb · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT FORWARD SERVICE DOOR JAMB PAN DAMAGED AT BAYONET PICK-UP BRACKET ON CENTER AFT EDGE OF DOOR. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 42. (X)Feb 18, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807201Skin · dentedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 503, BETWEEN L26R AND L26R, 3 INCH BY 2 INCH BY .145 DEEP. REPAIRED PER SRM 53.04, FIG 38 SHEET 22. (M)Feb 18, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807102Firewall Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK FOUND ON NR 2 PYLON AFT FIREWALL A ONE INCH CRACK IN UPPER FLANGE, AT OTBD END APPROX 40 INCHES AFT OF AFT ENGINE MOUNT. REPAIRED CRACKED ANGLE UPPER FLANGE ON AFT FIREWALL PER SRM 53-01. (X)Feb 18, 1998 · N997Z · Doug DC932 · Nacelle/Pylon, Bulkhead/FirewallSDR TWAA9806911Floorbeam · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FLOORBEAM CRACKED AT STATION 617, APPROX 58.6 RBL. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C AND SRM 51-30-0. (M)Feb 18, 1998 · N997Z · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9809512Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND 3 INCH BY 3 INCH BY .150 INCH DEEP DENT AT STA 490, BETWEEN LONGERON 24 AND LONGERON 25R. REPAIRED SKIN BETWEEN S24R AND 25R AT STA 490 PER SRM 53-04-12B, SHEET 2 PAGE 25. ACFT TT: 70,084 HOURS. ACFT TC: 84,015.Aug 4, 1997 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9575T-Cap · corrodedMCI - DURING OP-15, FOUND CORROSION IN HORIZONTAL LEG AT T-CAP BETWEEN STRINGERS 12 AND 13. REMOVED CORROSION AND INSTALLED CLIPS PER SERVICE BULLETIN 57-98. (M)Aug 22, 1995 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM639Spar · crackedMCI - DURING OP-15, FOUND CRACK IN LOWER REAR SPAR HORIZONTAL LEG OF RIGHT WING TANK, FROM HOLE IN AFT ROW TO RADIUS. REMOVED CRACK PER STANDARD PRACTICES AND SRM 51-10-1, REPAIRED PER ARA 9184. (M)Aug 22, 1995 · N997Z · Doug DC932 · Wing SparSDR 95ZZZM637Skin · corrodedMCI - DURING OP-15, FOUND CORROSION IN RIGHT WING TANK AROUND FASTENER IN STRINGER 11, BETWEEN STRINGERS 69 AND 91.0. REMOVED CORROSION PER SRM 51-10-3, REPAIRED PER ATA 9183 AND STANDARD PRACTICES.Aug 22, 1995 · N997Z · Doug DC932 · Wing, Plate/Skin
Back to N997Z, cancelled Aug 24, 2001