N978Z, cancelled Aug 21, 2013

Service difficulty reports · 21

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 = 'N978Z' AND deregistration_id = 'N978Z-2013-08-21'
  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 TWAA0017202Bottle · dischargedTHE LEFT SIDE NUMBER 1 CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE SLIDE ASSEMBLY. CHECK-C 6-4-00 MCI.Nov 1, 2000 · N978Z · Doug DC931 · Escape SlideSDR TWAA0008713Floorbeam · corrodedDURING CHECK-C MAINT IN AFT CABIN AT STA 965 JUST UNDER I/B RIGHT LAV WALL AT LOWER SIDE OF FLOORBEAM, FOUND SUPPORT STRAP CORRODED. INSTALLED NEW SECTION OF 9912243-52 CHORD PER ARA 16725.May 24, 2000 · N978Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0008712Floorbeam · corrodedDURING CHECK-C MAINT IN AFT CABIN AT LOWER FWD SIDE OF CABIN FLOORBEAM, STA 965 RBL 32 IN, HAD HEAVY CORROSION. INSTALLED DOUBLER AND STRAPS PER ARA 16725.May 24, 2000 · N978Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0008711Skin · crackedAT CHECK-C MAINT CHECK, FOUND APPROX 2 INCH CRACK IN OUTER SKIN AT STA 108, BETWEEN LONGERON 27L AND 28L. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6. CRACK WAS CONTAINED AT DRAIN HOLE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01May 23, 2000 · N978Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0008309Airstair · bentDURING CC, FOUND IN THE AREA OF THE AFT STAIRS, FWD LOWER EDGE OF THE AIRSTAIR BENT AND HAS 2 CRACKS. LONGEST IS APPROXIMATELY ONE INCH. PERFORMED EDDY CURRENT FOR CRACK CONTAINMENT. STOP DRILLED AND INSTALLED AN EXTERNAL DOUBLER AS PER THE SRM 52-01 FIG 2.May 17, 2000 · N978Z · Doug DC931 · Entrance StairsSDR TWAA0008308Skin · crackedDURING CC, FOUND RT PYLON, UPPER SKIN CRACKED AT THE TOP OF THE PYLON ON THE WEDGE APPROXIMATELY 11 INCHES FROM THE FIXED COWL AFT EDGE, OUTBOARD EDGE OF THE SKIN. STOP DRILLED CRACKS, MADE DOUBLER SAME GUAGE THICKNESS AS SKIN AND INSTALLED WITH .125 INCH MS2May 17, 2000 · N978Z · Doug DC931 · Nacelle/Pylon, Plate/SkinSDR TWAA0007603Longeron · crackedDURING CHECK-C, MAINT FOUND LONGERON 5R AT STA 699, WAS CRACKED. INSTALLED NEW SECTION PER SRM 53-02, FIG 18.May 11, 2000 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9913702Bus Tie Unit · wornAFTER TAKEOFF, BOTH ENGINE GENERATORS TRIPPED OFF LINE. THE APU WAS RUNNING AND TOOK THE LOAD. THE RT GEN RESET BUT THE LT WOULD NOT. FLIGHT RETURNED TO STL. REPLACED THE BUS TIE UNIT AND RESET THE LH GEN CONTROL UNIT. CHECK-C 4-30-99 STL.Oct 5, 1999 · N978Z · Doug DC931 · AC Power Distribution SystemSDR TWAA9808501Power Supply · inoperativeSTL - FLT 281 - DURING PREFLIGHT CHECK, FOUND L1 AND R1 EMERGENCY EXIT LIGHTS AND EGRESS LIGHTS IN AREA OF ROW 7 INOP. REPLACED POWER SUPPLY MFG P/N 5822-2 AND FLOOR FLEX CABLE MFG P/N 5853-1 RESPECTIVELY. (M)May 27, 1998 · N978Z · Doug DC931 · Emergency LightingSDR TWAA9801701Longeron · crackedSTL - DURING OP16 MAINTENANCE CHECK, LONGERON 5L WAS FOUND WITH A .5 INCH CRACK AT STATION 737. REPAIRED PER SRM 53-02 FIG 18. (M)Feb 2, 1998 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9802903Longeron · crackedSTL - DURING OP 16 MAINTENANCE CHECK, THE LOWER ATTACH LEG OF LONGERON 12 RT STA 965 WAS FOUND CRACKED .25 INCH. SPLICED IN NEW LONGERON SECTION FROM STA 958 TO STA 972 RT SIDE OF FUSELAGE LONGERON 12 RT. LONGERON SPLICED IN PER SRM 53-02 FIG 18. ACFT TT: Jan 26, 1998 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9802906Longeron · crackedSTL - DURING OP 15 MAINTENCE CHECK, LONGERON 3L BELT RING WAS FOUND WITH A .25 INCH CRACK AT STA 160. REPLACED LONGERON FROM STA 148 END FITTING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X)Jan 24, 1998 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9802905Longeron · crackedSTL - DURING OP 15, A .25 INCH CRACK WAS FOUND AT STA 160 LONGERON 4L BELT RING. REPLACED LONGERON FROM STA 148 END FITTING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X)Jan 24, 1998 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9802904Longeron · crackedSTL - DURING OP 15 MAINTENANCE CHECK, A CRACK WAS FOUND AT STA 200 LONGERON 4L. REPLACED LONGERON FROM STA 148 END FITTING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X)Jan 24, 1998 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9711002Power Supply · inoperativeSTL - FLT 27 - DURING CRUISE, THE EMERGENCY EXIT FLOOR LIGHTS ILLUMINATED. REMOVED AND REPLACED THE POWER SUPPLY, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS INC. (M)Sep 7, 1997 · N978Z · Doug DC931 · Emergency LightingSDR TWAA9754002Connector · dirtyFLT 614 - STL - DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED IN LAST THREE ROWS OF COACH. REMOVED, CLEANED AND RECONNECTED BATTERY PACK CONNECTOR. OPERATIONAL CHECK NORMAL. (M)Apr 30, 1997 · N978Z · Doug DC931 · Emergency LightingSDR TWAA9725001Connector · moisture contamSTL - DURING CRUISE, AFT CABIN EMERGENCY EGRESS LIGHTS ILLUMINATED. CLEANED MOISTURE FROM TRACK AND LIGHT CONNECTOR. OPERATIONAL CHECK NORMAL. (M)Feb 19, 1997 · N978Z · Doug DC931 · Emergency LightingSDR 96ZZZM781Longeron · crackedDURING C-CHECK, FOUND .5 INCH CRACKS IN UPPER AND LOWER LEGS OF LONGERON 6L, STATION 688. REPAIRED PER SRM 53-02, FIGURE 2. (M)Mar 23, 1996 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM780Longeron · crackedDURING C-CHECK, FOUND .5 INCH CRACKS AT UPPER AND LOWER LEGS OF LONGERON 5L, STATION 699. REPAIRED PER SRM 53-02, FIGURE 2.Mar 23, 1996 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM653Uplimit Sw · broken wireSTL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR. FOUND BROKEN WIRE TO PIN 7 OF UPLIMIT SWITCH, MFG P/N H14-6. REPAIRED WIRE TO PIN 7 AND NOSE LANDING GEAR INDICATIONMar 14, 1996 · N978Z · Doug DC931 · Landing Gear Position and WarningSDR 96ZZZX1231Schrader Valve · iced upSTL - FLT 585 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG UNSAFE RED LIGHT REMAINED ILLUMINATED WITH INTERMITTENT WARNING HORN. CYCLED LANDING GEAR. FOUND ICE IN NLG STRUT SCHRADER VALVE, MFG PN B05076-2. REPLACED SCHRADER VALVE, SERVICED NOSE STRUFeb 3, 1996 · N978Z · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
Back to N978Z, cancelled Aug 21, 2013