N8889Z, cancelled Nov 8, 2006
Service difficulty reports · 46
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 = 'N8889Z' AND deregistration_id = 'N8889Z-2006-11-08' 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.
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 = 'N8889Z' AND deregistration_id = 'N8889Z-2006-11-08' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL72S010919Light · shortedBURNING SMELL IN COCKPIT DURING CRUISE. FOUND WINDSHEAR ANNUNCIATOR LIGHT ASSEMBLIES SHORTED CAUSING BURNING SMELL IN COCKPIT. REPLACED LIGHT ASSY.SDR DL72S010881Mount · crackedINSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING HOLES PER AD 97-05-08 REVEALED A CRACK IN THE BORE OF HOLES A & B. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK INDICATIONS AND AN INSURANCE CUT ADDED. LARGER DIAMETER BOLTS WERE THEN INSTALLED. THE REPASDR DL72S010295Battery · dischargedAFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK.SDR DL72S010174Harness · burnedNR 2 ENGINE RT ISOLATION VALVE WIRING HARNESS BURNT IN TWO. REPAIRED WIRING. SYS OP CKS GOOD.SDR DL72S010078Control Unit · leakingDURING CRUISE B-SYSTEM HYD QTY DECREASED. FOUND UPPER RUDDER POWER CONTROL UNIT LEAKING. REPLACED UPPER RUDDER POWER CONTROL UNIT.SDR DL72S002244Spar · wornRUB MARKS ON FWD I/B LWR END OF AUX SPAR NEAR MLG W/W. REPAIR PER M/M 57-43-0.SDR DL72S000887Battery Pack · dischargedRT OVERWING EXIT SIGN 2 EACH INOP. REPLACED BATTERY PACK.SDR DL72S000775Clamp · leakingNR 3 ENG STRUT OVERHEAT LIGHT ILLUM AFTER T/O. LIGHT WENT OUT WITH THROTTLE AT IDLE. FOUND NR 3 ENG PRECOOLER INLET VALVE CLAMP LEAKING BADLY. REPLACED CLAMP, RAN ENG, NO PNEU LEAKS PER MM.SDR DL72S000310Skin · wornINSTALLED REPAIR PER B727 MM 57-54-0, FIG 813. SLAT WORN.SDR DL72S992088Bracket · crackedTHREE INCH CRACK IN NR 8 SLAT ACTUATOR I/B SUPPORT BRACKET. REPAIRED PER MM 51-20-21.SDR DL72S991956Light · inopL-2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L-2 EMERGENCY EXIT LIGHT ASSY CHECKS OK.SDR DL72S991949Battery Pack · dischargedRIGHT CENTER OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OP CKS GOOD.SDR DL72S990378B-Nut · looseCREW 02 WENT TO ZERO IN FLIGHT. TIGHTENED LOOSE B-NUT ON REGULATOR 3RD OFFICERS POSITION AND REPLACED O2 BOTTLE, LEAK CHECKS OK.SDR DL72S982453Battery Pack · dischargedR2 DOOR EMER EXIT LIGHT INOP. REPLACED BATTERY PACK.SDR DL72S982309Battery Pack · dischargedRT OVERWING EMEG EXIT SIGN INOP. REPLACED BATTERY PACK.SDR DL72S982308Battery Pack · dischargedRT EXTERIOR AND INTERIOR OVERWING EMER LIGHTS INOP. REPLACED BATTERY PACK.SDR DL72S981365Web · crackedA .25 INCH CRACK LIGHTENING HOLE STA 1230 LT ON AFT AIRSTAIR CUTOUT VERT WEB. REPAIRED PER M/M 53-11-0 PG 828.SDR DL72S980628Battery Pack · dischargedRT AFT OVERWING EMERG LIGHT OUT. REPLACED BATTERY IN M956 LOCATION OPN GD.SDR DL72S980254Battery Pack · dischargedRIGHT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CK'S GOOD.SDR DL72S972537Wire · looseLOOSE FLOORBOARD BY SEAT 27A WITH EXPOSED WIRES. SPARKS REPORTED BY PAX. FOUND VACUUM CLEANER RECP WITH WIRE PULLED LOOSE. INSTALLED TERMINAL ON RECP AND CK OK REF WDM25-11-01 PG 2 STA 950A +10.SDR DL72S972519Gusset · crackedFS 1273 TORQUE BOX STRUCTURE FOUND WITH A CRACK IN A GUSSET AND BEAM CHORD. THE CRACKED STRUCTURE WAS REPLACED PER THE GUIDELINES OF S/B 53-0129 TO COMPLY WITH AD 94-07-08. ER/A 363305-14AD WAS ISSUED TO DOCUMENT THE DAMAGE AND CONTROL THE REPAIR PROCESS.SDR DL72S972473Skin · crackedFOUND AT D-2 LETTER CHECK, .5 INCH CRACK I/B AFT CORNER OF PNEUMATIC GROUND CONNECTION DOOR. INSTALLED TIME LIMITED REPAIR DOUBLER PER M/M 53-30-0 AND ERA 363309-14.SDR DL72S972472Bracket · crackedNR 8 SLAT O/B ACTUATOR ATTACH BRACKET I/B WEB CRACKED. REPAIRED PER M/M 57-20-21 P 812.SDR DL72S972234Battery Pack · dischargedEMERGENCY EGRESS LIGHTS EXTERIOR AFT WING AND AFT CARGO DOOR RT SIDE INOP. REPLACED BATTERY PACK.SDR DL72S971856Generator · failedLOST ALL AIRCRAFT PWR AFTER T/O. DID NOT GET PWR BACK UNTIL ON THE GROUND WHEN NR 3 GEN TURNED OFF. FOUND 1 AND 2 GENERATORS OPERATING NORMALLY. WHEN NR 3 USED THE PWR STARTED TO FLUX. REPLACED NR 3 GEN, CSD, GCU, AND BPP.SDR DL72S970786Angle · corrodedSUPPORT ANGLE FOR PANEL 3348L IS CORRODED. CUT OUT CORRODED T, CLEANED OTHER CORROSION PER SRM 51-10-6 WITHIN LIMITS SRM 51-10-1 FIG 1, MADE REPLACEMENT ANGLE REF M/M 53-30-1 FIG 804. REPAIRED PER DAL M/M 53-30-1, FIG 804.SDR DL72S970785Support · corrodedCORROSION INSIDE HINGE SUPPORT STRUCTURE FOR PANEL 3448R. REMOVED CORROSION PER SRM 51-10-6. FOWARD CORROSION WITHIN SRM LIMITS 53-10-1 FIG 1. CUTOUT REAR CORROSION. CUTOUT ANGLE PER M/M 53-30-1 FIG 804, MADE NEW ANGLE, SPLICES AND DRILLED. REPAIRED ANGLESDR DL72S970772Stringer · damagedTIME LIMITED REPAIR ON STR 18A RT ABOVE UPLOCK ASSY. REMOVED TIME LIMITED REPAIR, CUT AND REMOVED SECTION OF STR 18A PER M/M 53-12-0 PG 819. FABRICATED REPAIR PER M/M 53-12-0 PG 819. INSTALLED REPAIR PER M/M 53-12-0 PG 819.SDR DL72S970771Rib · crackedNR 3 SLAT RIB NR 3 IS CRACKED IN 2 PLACES LWR FLANGE AT NUTPLATE AND UPPER FLANGE IN RADIUS. REPAIRED AND INSTALLED DOUBLER PER M/M 57-54-00, PG 813A AND SRM 57-50-3 PG 26.SDR DL72S970781Frame · damagedDURING ACCOMPLISHMENT OF M/M53-11-0 NR 12 PERMANENT REPAIR (REPAIR/MOD TO STA 910 AND 913 FRAME STUB BEAMS) MAINTENANCE DISCOVERED THAT INSTALLATION OF THE TIME LIMITED REPAIR DAMAGED THE EXISTING STUB FRAME. REPAIRED FRAME STUB PER M/M 53-11-00, FIG 813. RESDR DL72S970784Blkhd Stiffener · crackedCRACKS WERE FOUND IN THE VERT STIFF AT RBL 36.83 AND LBL 36.83 ON THE FWD SIDES OF THE BS 1183 BLKHD. THE CRACKS ARE APPROX 1.5 LONG AND ARE LOCATED AT APPROX WL 238 IN THE O/B RADIUS OF THE AFT CHORD. THIS AREA IS ADDRESSED BY S/B 727-53-0192 (EO 4-59821-3)SDR DL72S971277Angle · crackedLOWER CHORD ANGLE CRACKED AT 55 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIGURE 802.SDR DL72P961678Light · inoperativeEPL LIGHT AT SEAT 5C IS LOOSE FROM MOUNTING AND LIGHT INOP. REPLACED LIGHT ASSY AND CHECKS OK.SDR DL72P961627Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF CLAD 2024-T3 WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECSDR DL72P961225Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECSDR DL72P961105Stringer · crackedSTRINGER 18A RT CRACKED AT STA 940 SUPPORT FITTING AFT BOLT. REPAIRED PER MM 53-12-0.SDR DL72P961095Web · crackedA .625 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB AT LOWER LIGHTENING HOLE STA 1237. REPAIRED PER M/M 53-11-0 AND ERA DUE TO EFFECTIVITY.SDR DL72P961094Bracket · crackedAPPROX 2 INCH CRACK IN NR 1 SLAT I/B AND O/B ACTUATOR MOUNT BRACKET'S. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR DL72P961093Bracket · crackedNR 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR DL72P961091Angle · crackedFOUND DURING C-CHECK, .5 INCH CRACK IN NR 1 SLAT SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 51-54-0 AND ERA DUE TO EFFECTIVITY.SDR DL72P961090Aux Spar · chafedFOUND DURING C-CHECK, LT MLG STRUT DOOR CHAFING AUX SPAR I/B END MARKED, FWD OF NR 4 SCREWJACK. REPAIRED PER M/M 57-43-0 PG 802.SDR DL72P961089Frame · crackedFOUND DURING C-CHECK, AFT RT SVC DOOR FWD FRAME CRACKED AT LWR I/B END OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2.SDR DL72P960745Shim · misalignmentTHE LAMINATED SHIM INSTALLED ON THE RIGHT WING INBOARD TRAILING EDGE FLAP INBOARD TRACK WAS FOUND TO HAVE MIGRATED GREATER THAN THE .25 LIMIT SPECIFIED IN THE INSPECTION. IN COMPLIANCE WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED AND ATTACHMENTS RETOSDR DL72P950842Eel Rack · faultyDURING INSPECTION, ALL 3 RT WING EMERGENCY LIGHTS, AND CENTER CABIN OVERWING EMERGENCY EXIT LIGHT WERE INOP. REPLACED POWER SUPPLY, OPERATION NORMAL.SDR DL72P950726Eel Pack · dischargedDURING INSPECTION, RIGHT SIDE EMERGENCEY EXIT LIGHTS FAILED TO TEST. REPLACED BATTERY ASSEMBLY OPERATION NORMAL.SDR DL72P950447Skin · corrodedDURING INSPECTION, THE FUSELAGE SKIN AT F.S. 680-686 WAS FOUND CORRODED AT STR. 28L AND WAS CUT OUT. A PRE-EXISTING REPAIR DOUBLER SPANNING THE AREA FROM F.S. 688-720A AND STR. 28L-28R WAS REMOVED AND EXTENDED TO INCLUDE THE NEW CUTOUT NOTED ABOVE. BOTH OF T
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