N764AT, cancelled Jul 21, 2010
Service difficulty reports · 89
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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21' 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.
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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21' 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 DHL2006764510Angle · crackedLEFT WING LE WBL117.0 CHORD ANGLE CRACKED TO FWD END. REMOVED CHORD ANGLE AT LEFT WING LE WS117 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE MATERIAL USED 7075T6 .063 PO# 9003002 DIM. 46"X 2" IAW B727 SRM 57-20-2 FIG 1 AND MAT SUBSTUITION 51-20-1 FIG 2. LOCATSDR DHL2006764509Support Angle · crackedLEFT WING LE WBL117.0 LWR PANEL SUPPORT ANGLE SHOW CRACK BETWEEN FASTENER HOLES. NDT CONFIRM. REMOVED SUPPORT ANGLE AT LEFT WING LE WBL 117 LWR PANEL IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE SUPPORT MATERIAL USED 7075T6 .050 PO# 9002787 DIM 18"X 1 3/4" IASDR DHL2006764518Panel · delaminatedNR 5 SPOILER UPPER TE CORNER IB SURFACE DELAMINATED CUT OUT DELAM AREA APPROX 13.2500 INCHES X 4.2500 INCHES AND VACUUM BAGGED FOR MOISTURE REMOVAL SRM 51-40-20 FABED REPAIR SKIN APPROX 13.2500 INCHES X 4.25 INCHES AND DOUBLER APPROX 16.2500 INCHES X 5.7500 INSDR DHL2006764511Skin · dentedLT HORIZ STAB UPPER SURFACE AT STAB STA 170 DENTED. MEASURED DENT AT LT HORIZ STAB UPPER SURFACE STA 170 IAW B727 SRM 55-10-1 FIG 1. FOUND WITHIN LIMITS A=.500 Y=.012 A/Y=41. NDT HFEC SHOWS SKIN CRACK PER MANUAL PT6 51-00-00 FIG 4. REMOVED DAMAGED AREA IAWSDR DHL2006764513Skin · dentedL/S UPPER RUDDER T/E DENTED (RED DOT). REMOVED AT L/S UPPER TRL ANGLE AS REQ IAW B727 SRM 51-30-2. FAB`D NEW RUDDER TRL ANGLE MAT USED 2024T3 .032 PO NR 53081 DIM 54 1/2" BY 7" IAW B727 SRM 55-40-2 FIG 2 AND 51-30-5. TREATED AND PRIMED AREA AND PART IAW B7SDR DHL2006764500Skin · chafedLT FUSELAGE EXTERIOR SKIN CHAFED AT STA 720E STR 20L, MARKED. REMOVED FASTENERS FOR ACCESS AT LT FUSELAGE STA 720E STR 20L IAW B727 SRM 51-30-2, CUT OUT DAMAGE AREA DIM 2.5" X 2.25" IAW B727 SRM 53-30-3 FIG 14. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .080 SDR DHL2006764503Skin · crackedLT WING NR 4 SLAT OB GUIDE CUTOUT ON FIXED LE, CRACKED AT OB AFT CORNER, MARKED. REMOVED FASTENERS FOR ACCESS AT LT WING NR 4 SLAT OB GUIDE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. NDT INSPECTED ASDR DHL2006764501Skin · crackedLT WING FIXED LE CRACKED AT NR 4 SLAT OB TRACK CUTOUT, MARKED. REMOVED FASTENERS FOR ACCESS AT LT WING FIXED LE AT NR 4 SLAT OB TRACK CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1, NDT ACCOMPLISHED 727 HSDR DHL2006764504Structure · crackedLT WING FIXED LE UPPER SURFACE CRACKED AT NR 3 SLAT OB GUIDE (HOOK) CUTOUT AFT OB CORNER, MARKED. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1, NDT INSPECTED PER 727 PT6 51-00-00 FIG 23 CRACK ENDS IN STOP HOLE. SDR DHL2006764508Rib · crackedLT WING INSIDE NR 2 SLAT LE ACTUATOR POINT IB AND OB RIBS HAVE EVIDENCE OF CRACKS, MARKED. HFEC INSP PER 727 PT6 51-00-00 FIG 23 CONFIRMED BOTH RIBS CRACKED. REMOVED AND REPLACED RIB ASSY OB P/N 65-17310-4 PO# 619582 AND IB P/N 65-17310-4 PO# 619577 ON LH WISDR DHL2006764507Rib · crackedLT WING INSIDE NR 3 SLAT LE ACTUATOR ATTACH POINT RIB CRACKED, MARKED. REMOVED AND REPLACED INBOARD AND OUTBOARD ATTACH POINT ACTUATOR AT LT WING NR 3 SLAT LE PO NR 6195105 P/N 65-17294-14 AND PO NR 619578 P/N 65-17294-13 IAW B727 SRM 51-30-2.SDR DHL2006764505Stiffener · crackedLWR END OF VERTICAL STIFFENER CRACKED ON RT WING FIXED LE WSTA125. STOP DRILLED CRACK PER B727 SRM 51-10-1, HFEC STOP DRLL IAW B727 NDT MAN PT 6 51-00-00 FIG 23. FAB`D DOUBLER FROM 7075T6 .063 PO# 9002454 DIM. 25" BY 7" IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2SDR DHL2006764502Rib · crackedNR 6 SLAT IB ACTUATOR ROD END MOUNT RIB CRACKED. REMOVED AND REPLACED RIB AT NR 6 SLAT IB ACTUATOR ROD MOUNT PO NR 619549 P/N 65-17294-13 IAW B727 SRM 51-30-2.SDR DHL2006764514Rib · crackedFOUND CRACK INDICATION ON NR 7 SLAT I/B ACTUATOR ROD END MOUNT RIB. REMOVED AND REPLACED RIB ASSY P/N 65-17310-3 PO NR 619595 AND P/N 65-17310-4 PO NR 61956. CHANNEL P/N 65-17310-7 PO NR 619596 IAW B727 SRM 51-30-5 AT NR 7 SLAT IB AND OB ACTUATOR ROD END MOUSDR DHL2005764004Skin · dentedFUSELAGE SKIN DENTED ABOVE L-2 DOOR AT STR. 5L. - EVALUATED DENT BE OUT OF LIMITS IAW 53-30-1 FIG.1. OPENED CABIN LINING ABOVE L2 DOOR FOR ACCESS IAW B727 SRM 51-30-2. REMOVED PREVIOUS REPAIR FOR INCORPORATION IAW B727 SRM 51-30-2 CUTOUT DAMAGE AREA DIM 1 X 1 SDR DHL2005764003Skin · dentedRT. ELEVATOR LOWER SURFACE IS DENTED AT ELEVATOR STA 121. FOUND DENT OUT OF LIMITS. CUT OUT DAMAGE AREA IAW B727 SRM 55-20-1. FABRICATED DOUBLER REPAIR IAW B727 SRM 55-20-3. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 55-20-3 FIG.5SDR DHL2005764002Landing Gear · malfunctionedLEFT GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. PERFORMED GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR HANDLE UP OR OFF. ABNORMAL PROC RECYCLED GEAR AND LIGHT WENT OUT. CYCLED DOOR SEVERAL TIMES. INSP DOOR, NO DEFECTS NOTED. COULD NOT DUSDR DHL2008764525Tab · delaminatedWHILE AT C CHECK, RT ELEVATOR CONTROL TAB O/B AFT CORNER DELAMINATED. CLEANED AND PREPPED DELAMINATED CORNER ON RT ELEVATOR CONTROL TAB, CUT OUT DELAM AREA APPROX 2 1/2 INCHES BY 2 INCHES, FABRICATED FILLER APPROX 2 1/2 INCHES BY 2 INCHES AND DOUBLER 4 INCHESSDR DHL2005764001Control Box · malfunctionedLE FLAPS AMBER LIGHT CAME ON AFTER TAKEOFF WITH FLAPS 15. NR 1 LE DEVICE. NO INDICATION. C/W ABNORMAL PROCEDURE. ON APPROACH WHEN GEAR EXTENDED LIGHT NORMAL. REMOVED AND REPLACED L/E CONTROL BOX IAW MM 27.82.31. OPS CK SERVICEABLE.SDR DHL2005764500Skin · debondedRT INBOARD MID FLAP UPPER SKIN TO T/E WBL 200 PREVIOUS FIBERGLASS REPAIR BECOME DISBONDED (PEELING OFF). REMOVED TWO EACH PREVIOUS FIBERGLASS REPAIRS & CLEANED AREA FOR NEW REPAIR IAW B727 SRM 51-40-20 FIG 30. FABRICATED TWO EACH SKIN REPLACEMENTS APPROX 4 XSDR DHL2004764010Display · failedWX RADAR MADE GRINDING NOISE WX RADAR C/B THEN POPPED SMELLED ELECTRICAL SMOKE. REMOVED AND REPLACED TWAS DISPLAY (MFD 640) IAW MMS 34-20-02, OPS CK NORMAL PER CM 34-20-02-01.SDR DHL2004783013Brake Assy · sticksRIGHT BRAKE GRABS. BLED RIGHT SIDE BRAKES & INSPECTED. TAXIED AIRCRAFT, PER JRH 9.1 COULD NOT DUPLICATE. BRAKES CHECK GOOD IAW MM 32-41-0.SDR DHL2004764009Connector · mispinnedNR 3 LED WOULD NOT RETRACT ON DEPARTURE ACCOMPLISHED ABNORMAL PROCEDURE LED WOULD NOT RETRACT ON SECOND ATTEMPT, NR 3 SLAT. SWAPPED PINS 1 AND 3, 2 AND 4 ON NR 3 SLAT ACTUATOR IAW B727 MM 27-82-11 PAGE 101. OPS CKS GOOD.SDR DHL2004764008Indicator · malfunctionedRTO DUE TO SPEED CLACKER SOUNDING AT 80 KNOTS . WT = 169,000 IAS = 80 KNOTS OHT = 25 DEG. PA = 400. DEFERRED CLACKER IAW MEL 34-4-1 CAT B CONTROL NR 17604 C/W RTO INSP. IAW B727 MM 05-51-121. CAPTAINS MACH / AIRSPEED IND. REPLACED IAW MM CH 34-12-0 P.3. OSDR DHL2004764007Plate · shortedAT FL330 CREW SMELLED SMOKE OBSERVED SMOKE COMING FROM OVERHEAD PANEL AT YAW DAMPER SWITCHES. TURNED OFF LOWER YAW DAMPER AND OVERHEAD LIGHTS, SMOKE STOPPED. EMERGENCY LANDING AT ABQ. FOUND YAW DAMPER LIGHT PLATE SHORTED. REMOVED AND REPLACED LIGHT IAW B-7SDR DHL2004764006Fire Detector · malfunctionedLOWER CARGO FIRE DETECTOR DOES NOT TEST PROPERLY. RED ANNUNCIATOR ON S/O PANEL, NOR RED ANNUNCIATOR ON FWD GLARESHIELD DOES NOT ILLUMINATE. RESET CARGO FIRE DETECTOR, SYS OPS GOOD IAW MM 26-10-0.SDR DHL2004764005Smoke Detector · will not testCARGO FIRE DETECTOR WILL NOT TEST. FOUND FAULT LIGHT ON RESET SYSTEM CB'S, SYSTEM CHECKS NORMAL REF MM 26-11-0. NO COMPONENTS REPLACED.SDR DHL2004764004Spoiler · out of adjustA PULSATING HIGH FREQUENCY VIBRATION IS FELT THROUGH THE YOKES AND THRUST LEVERS. THE VIBRATION IS MORE INTENSE DURING CLIMB THAN IN CRUISE, AND IS MORE INTENSE IN CAPTAINS YOKE. SUSPECT THE VIBRATION IS ENGINE RELATED. ALL ENGINE GAUGES INDICATE NORMALLY. WITSDR DHL2004764002Fire Loop · malfunctionedNR 3 DETECTOR INOP LIGHT ILLUM IN FLIGHT, REWORKED/READJUSTED LOOP ELEMENT AWAY FROM NR 3 ENG COWL-LOWER IAW MM 26-14-00 NO FURTHER FAULTS NOTED OPS CK GOOD.SDR DHL2004764003Fire Loop · looseNR 3 DETECTOR INOPERATIVE LIGHT ILLUMINATED IN FLIGHT. FOUND LOOSE CLAMP ON FIRE LOOP, RE-SECURED AND RAN ENG. PER JRH 5.2. OPS CHECK GOOD ON GROUND.SDR DHL2004764001Battery · dischargedEMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR BATTERY IS DEAD. REMOVED AND REPLACED L1 ENTRY DOOR LIGHT ASSEMBLY. OPS SERVICEABLE IAW M/M 33-50-71.SDR 2002F00154Actuator · leakingFLT 8001 - DURING CRUISE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO, FOLLOWED BY NR 1 'A' SYSTEM PUMP LOW PRESSURE LIGHT. FLIGHT CREW FOLLOWED AOM PROCEDURE. AIRCRAFT LANDED AT MMUN WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM RESERVOIR WITH 1 GALLONSDR 20010207SG013Engine · failedATL - FLT 8027 - AT FL26.0 CRUISING, CREW HEARD LOUD NOISE FOLLOWED BY DETERIORATING EPR AND FUEL FLOW OF 2000 LBS ON NR 1 ENGINE. CREW SHUTDOWN THE NR 1 ENGINE AND DIVERTED TO MEM. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TWO ENGINE FERRIED TSDR 20000412AP002Control Valve · inoperativeEN ROUTE FROM MDW TO MCO, LEADING EDGE AMBER FLAP LIGHT ILLUMINATED WHEN FLAPS ARE AT 2 DEGREES. VERIFIED SLATS 2, 3, 6, 7 INTRANSIT AT FLT ENGINEERS FLAP/SLAT PANEL. RETURNED TO MDW WITHOUT FURTHER INCIDENT. REPLACED LEADING EDGE FLAP AND SLAT CONTROL VALVSDR 99ZZZM786Pulley · seizedDURING C-CHECK, FOUND THE AFT FLAP CABLE FRAYING AGAINST THE INBOARD FLAP PULLEY. THE INBOARD FLAP OUTBOARD CABLE PULLEY WAS FOUND WITH THE SWIVEL POINT CONTAMINATED WITH CIC COMPOUND AND DIRTY CAUSING TO SEIZE IN ONE POSITION. REPLACED FLAP CABLE AND BOTH ISDR 99ZZZM302Battery Charger · inoperativeDURING PREFLIGHT, FOUND THE FIRST TEN ROWS OF EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD BATTERY CHARGER PER MM 33-50. (M)SDR 95ZZZX5191Slide · leakingIND - RIGHT NR 1 SLIDE IS ZERO PSI. REPLACED R-1 DOOR SLIDE, OK FOR SERVICE.SDR 95ZZZX5192Fire Det Module · failedSTL - AFTER TAKEOFF WHEN ENGINE POWER WAS RETARDED TO CLIMB EPR, BOTH MASTER F/W LIGHTS ILLUMINATED AND F/W BELL ACTIVATED WITHOUT ANY FIRE. RETURNED TO STL. REMOVED AND REPLACED FIRE DETECTION AND WARNING MODULE. OPS CHECK AND F/W SYSTEM TESTS GOOD ON GROUSDR 95ZZZW326Slide · detachedIND - FLT NR 975 - FORWARD ENTRY DOOR CHUTE FELL OUT OF ITS CASE AFTER PUSH OUT. REINSTALLED FORWARD CHUTE INTO CASE, SECURED NOW AND CHECKED OK.
Back to N764AT, cancelled Jul 21, 2010