N786AT, cancelled Jul 5, 2011

Service difficulty reports · 44

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 = 'N786AT' AND deregistration_id = 'N786AT-2011-07-05'
  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 DHLA200800133Skin · damagedACFT SKIN DAMAGE 2 IN HOLE LOWER RT SIDE BELOW PITOT TUBE. ACFT DAMAGED BY CARGO CONTAINER. INSTALLED REPAIR IAW SRM 53-30-3 AT STA 212 RT STR 25R.Dec 4, 2008 · N786AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHLA200800029Light · defectiveFWD ENTRY L1 DOOR EMERGENCY LIGHT ASSY "ON" IN ARM POSITION, WOULD NOT TURN OFF. REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHT ASSY IAW MM 33-50-101. OPS CKS NORMAL PER MM 33-50-01. AIRCRAFT WAS GROUNDED.Mar 11, 2008 · N786AT · Boeing 727214 · Emergency LightingSDR DHLA200800020Light · inoperativeCOCKPIT EMERGENCY LIGHT ASSY INOP, BATTERIES OK. REMOVED AND REPLACED PER B727 MM 33-50-101 AND OPS CKS GOOD. AIRCRAFT WAS GROUNDED.Mar 3, 2008 · N786AT · Boeing 727214 · Emergency LightingSDR DHL2007786529Structure · crackedNR 1 SLAT ASSY CRACK WHERE SLAT ACTUATOR ATTACHES TO SLAT INTERNAL. REMOVED NR 1 SLAT ASSY TO FOM REPAIR IAW B727 M/M 27-81-11. REMOVED 2 RIBS INBD AND OUTBD FROM NR 1 SLAT ASSY IAW B727 SRM 51-30-2. LOCATED AND DRILLED RIBS IAW B727 SRM 51-30-2. INSTALLEDMar 30, 2007 · N786AT · Boeing 727214 · Leading Edge DevicesSDR DHL2007786505Rib · crackedNR 3 SLAT IB AND OB RIBS WS 515 AT ACT ATTACH ARE CRACKED IN THE AFT LOWER CORNERS. REMOVED AND REPLACED RIBS I/B AND O/B AT NR 3 SLAT WS 515 IAW B727 SRM 51-30-2.Mar 28, 2007 · N786AT · Boeing 727214 · Leading Edge DevicesSDR DHL2007786530Skin · gougedRIGHT WING INBD MID FLAP GOUGED 3 FROM INBD EDGE, WBL 73.597. CUTOUT DAMAGED AREA 1 BY 1.875. FABRICATED INTERNAL DOUBLER FROM 2024T3, .040, 7.75 BY 5.625 AND FILLER 2024T3, .040, 1 BY 1.875. TREATED, ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLMar 27, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786524Skin · dentedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR 112921, LT WING OB FORE FLAP ASSY HAS 1 DENT UPPER SKIN. CUT OUT DENT 1" DIA ON LT OB FORE FLAP UPPER SURFACE AND APPLIED POTTING COMPOUND. FABRICATED FILLER 4" DIA FROM .016 2024T3 PO NR 9004174. BOMar 27, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786523Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR NR 112916. LT OB FORE FLAP WAS FOUND TO HAVE A DEEP PUNTURE IN THE UPPER SURFACE WBL442. CUT OUT PUNTURE 1" DIA ON LT OB FORE FLAP UPPER SURFACE WBL442 AND APPLIED POTTING COMPOUND. FABRICATED DOUBLEMar 26, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786515Shear Tie · corrodedAFT CARGO COMPARTMENT BS 950F AND STR 28L, SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SHEAR TIE, SIZE 6” BY 1.50 IAW B727 SRM 53-10-4, FIG 13. FABRICATED DOUBLER REPAIR FROM 7075T6, .071, 8 BY 3.50 IAW B727 SRM 53-10-4, FIG 13. TMar 26, 2007 · N786AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007786528Frame · crackedEMPENNAGE INTERIOR BS 1303 WL 281, FRAME CENTER WEB AT SECOND UP RIGHT STRINGER CUTOUT IS CRACKED 1 INCH. STOP DRILLED CRACK IAW COTNEY AEROSPACE ED NR EAZ04E-1, REV IR, 8110-3 DATED 3/28/07. VISIONAL RE-INSPECTION REQUIRED AT INTERVALS NOT TO EXCEED 2400 FLMar 22, 2007 · N786AT · Boeing 727214 · Horizontal Stabilizer, Spar/RibSDR DHL2007786507Airstair · crackedFOUND CRACK AT LIGHTENING HOLE RT LWR TORQUE BOX STA 1329. STOP DRILLED .250 DIA HOLE AT LIGHTENING HOLE RT LWR TORQUE BOX STA 1329 IAW B727 SRM 51-40-2. HFEC FOR CRACK STOP VERIFIED IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED DOUBLER REPAIR AT LIGHTENINGMar 22, 2007 · N786AT · Boeing 727214 · Entrance StairsSDR DHL2007786506Skin · dentedFOUND TWO DENTS ON UPPER RUDDER LT T/E SKIN AT LOWER HINGE BS 1540. NO DENTS ALLOWED. FOUND OUT OF LIMITS IAW B727 SRM 55-40-1 FIG, 61. REMOVED LT T/E SKIN AT UPPER RUDDER BS 1540 IAW B727 SRM 51-30-2. FABBED LT T/E SKIN AT RUDDER BS 1540 MATERIAL USED 202Mar 22, 2007 · N786AT · Boeing 727214 · Rudder, Plate/SkinSDR DHL2007786520Skin · dentedDENT ON RT ELEVATOR LWR SKIN FWD OF NR 2 STATIC WICK, ELEV STA 209.96, 11" FWD OF T/E. EVALUATED DENT AND FOUND OUT OF LIMITS IAW B727 SRM 55-20-1, FIG 7. CUT OUT DAMAGED AREA 7" BY 0.50" AND FABRICATED REPAIR DOUBLER USING 2024T3, 0.032, 4" BY 2.0625 IAW B7Mar 21, 2007 · N786AT · Boeing 727214 · Elevator, Plate/SkinSDR DHL2007786516Skin · dentedLT ELEVATOR LWR T/E SKIN DENTED AT NR 1 TAB BOBWEIGHT CUTOUT, ELEV STA 99.79, FWD OF CONTROL TAB. EVALUATED TWO EACH DENTS, NR 1, A=.50" Y=.051" A/Y=9.80, NR 2, A=.50" Y=.052" A/Y=9.61, FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1, FIG 1. CUTOUT DAMAGE AREMar 21, 2007 · N786AT · Boeing 727214 · Elevator, Plate/SkinSDR DHL2007786514Skin · debondedRIGHT WING, INBD FOREFLAP, UPPER SKIN INBD EDGE SHOWS INCORRECT PREVIOUS REPAIR. NR 4 LE FLAP, LE STA 130.7. REMOVED INCORRECT PREVIOUS FIBERGLASS REPAIR APPROX 1.5 IAW B727 SRM 51-40-22 FIG 3 AND APPLIED POTTING COMPOUND. FAB DOUBLER 4" BY 5", .016, 2024T3Mar 21, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786513Rib · crackedRT ELEVATOR, FWD INBD RIB CRACKED AND MISSING RIVETS, ELEV STA 20. REMOVED ACCESS PANEL RT ELEVATOR LWR INBD IAW B727 SRM 51-30-2. REMOVED RIB IAW B727 SRM 51-30-2. FABRICATED NEW RIB FROM 7075T6, .040, 18.25 BY 2.50 IAW B727 SRM 55-20-2, FIG 2. TREATED ALMar 21, 2007 · N786AT · Boeing 727214 · Elevator, Spar/RibSDR DHL2007786531Skin · damagedREMOVE TEMP REPAIR AND INSTALL PERMANENT REPAIR AT FUSELAGE SKIN AT BS 620 BETWEEN STR 16L AND 17L. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2 AND SIE EO NR SIE–N786AT-3-27-07, DATED 04/02/07. FABRICATED REPAIR DOUBLER FROM 2024T3, .063, 28.25 BY 24 AND TRMar 20, 2007 · N786AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHL2007786518Shear Tie · corrodedAFT CARGO COMPARTMENT AT BS 985 AND STR 28R, SHEARTIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT BS 985 AND STR 28R SHEARTIE IAW B727 SRM 53-10-4, FIG 13. DIMENSION 5.25 BY 4 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEARTIE REPAIR FROM 70Mar 20, 2007 · N786AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007786511Shear Angle · corrodedAFT CARGO COMPARTMENT AT BS 990 AND STR 28L, SHEARTIE HAS CORROSION. REMOVED FLOOR SUPPORT LT STA 990 TO 950E. REMOVED Z ANGLE SUPPORT STA 990 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AFT CARGO COMPARTMENT SHEARTIE, DIMENSION 3 BY 6 IAW B727 SRM 53-10-4, Mar 20, 2007 · N786AT · Boeing 727214 · Fuselage Miscellaneous StructureSDR DHL2007786510Shear Tie · corrodedAFT CARGO COMPARTMENT AT BS 1148 AND STR 28L, SHEARTIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SHEARTIE, DIMENSION 4.50 BY 1.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEARTIE REPAIR FROM, FILLER 7075T6, .063, 1.1 BY 1 BY 4.75, DOUBLERMar 20, 2007 · N786AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007786Shear Tie · corrodedAFT CARGO COMPARTMENT AT BS 1148 AND STR 28L, SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SHEAR TIE, DIMENSION 4.50 BY 1.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR FROM, FILLER 7075T6, .063, 1.1 BY 1 BY 4.75, DOUBMar 20, 2007 · N786AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007786512Seat Track · gougedCUTOUT AREA OF SEAT TRACK GOUGED AND WORN AT LT BS 994, LBL 25. REMOVED FLOOR BOARDS AND SEAT TRACK AT STA 950 TO 1130 IAW B727 SRM 51-30-2. FABRICATED AND TRIMMED AS REQUIRED NEW SEAT TRACK SECTION, P/N BAC 1520-792 IAW B727 SRM 53-10-5, FIG 1. TREATED, PRMar 16, 2007 · N786AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007786509Seat Track · corrodedPITTING CORROSION IN LWR SECTION OF SEAT TRACK CUTOUT AT RT BS 486 TO 492.5, RBL 45. EVAL FOUND SEAT TRACK PITTING CORROSION BEYOND LIMITS. REMOVED SEAT TRACK FROM BS 480 TO 690 IAW B727 SRM 53-10-5, FIG 1. FABRICATED AND TRIMMED AS REQUIRED NEW SEAT TRACK Mar 16, 2007 · N786AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007786508Seat Track · gougedNUMEROUS DENTS AN GOUGES IN RT SEAT TRACK AT RT STA 1096-1103. MARKED IN RED. REMOVED SEAT TRACK AT RT RBL 45-STA 1050-1130 IAW B727 SRM 51-30-2. FABBED NEW SEAT TRACK SECTION MAT USED BAC 1520-792-792-7178T6511. PO NR 9003963, DIM 5 FT. 7" LONG IAW B727 SMar 16, 2007 · N786AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007786526Skin · delaminatedLEFT INBD AILERON OUTBD END LOWER SURFACE IS DELAMINATED, LT STAB STA 60.21. CUTOUT DELAMINATED AREA ON LT IB AILERON TAB LOWER SURFACE 4" BY 6". FABRICATED FILLER 4" BY 6" AND DOUBLER 5 1/2" BY 7" FROM .010" 2024T3 PO NR 9003621 IAW B727 SRM 57-50-2. BONDEMar 15, 2007 · N786AT · Boeing 727214 · AileronsSDR DHL2007786527Skin · delaminatedLEFT OUTBD AILERON TAB WBL 535 AND 567, T/E IS DEBONDED TWO PLACES. REMOVED LEFT OUTBD AILERON TAB IAW B727 M/M 27-10-41 AND WEIGH BEFORE REPAIR IS 3.9 LBS IAW B727 SRM 51-80-06, FIG 2. REMOVED DELAMINATION AREA 38.5" BY 5", CLEANED AND PREPPED REPAIR AREA IMar 15, 2007 · N786AT · Boeing 727214 · AileronsSDR DHL2007786525Shear Tie · corrodedAFT CARGO COMPARTMENT AT BS 970, BETWEEN STR 28R AND 29R, SHEAR TIE HAS CORROSION. REMOVED FLOOR SUPPORT AT STA.990 TO 950E FOR ACCESS IAW SRM 51-30-2. REMOVED INTERCOSTAL BETWEEN 970-950E FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT SHEAR TIE BSMar 15, 2007 · N786AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007786522Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF. ASTAR NR 080502. LT WING IB MID FLAP LOWER TE CHORD WBL100-134 HAS 5 CRACKS ON 3 CUTOUTS. REMOVED LT IB MID FLAP LOWER ACCESS PANEL FOR ACCESS IAW B727 SRM 51-30-2. FABRICATED REPAIR, MATERIAL USED ANGLE EXTMar 15, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786521Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES REF ASTAR NR 080528. RT WING IB MID FLAP LOWER CHORD AT WBL135 SHOWS CRACK. REMOVED R/WING IB MID FLAP LOWER PANEL AND LOWER AFT CHORD WBL135 AS REQ IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM BAC1503-100046 7075T6Mar 15, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786517Skin · debondedLEFT OUTBD FOREFLAP WBL 305, HAS T/E DISBONDING. CUT OUT DAMAGED AREA APPROX 2 BY 6 ON LT OUTBD FOREFLAP WBL 305 IAW B727 SRM 51-40-20. FABRICATED FILLER .016 BY 2 BY 6 AND DOUBLER, .016 3.50 BY 8.50 FROM 2024T3 IAW B727 SRM 53-10-4, FIG 13. BONDED FILLER AMar 15, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786502Skin · dentedRT HORIZ STAB LWR SURFACE HAS A DENT, STAB STA 144, 11 AFT OF L/E. CUT OUT DAMAGED AREA AT RT HORIZ STAB LWR, MEASUREMENTS, 1.25 BY 1.75 IAW B727 SRM 55-10-3. FABRICATED DOUBLER REPAIR FROM 2024T3, .080, 7.875 BY 5.375 IAW B727 SRM 55-10-3, FIG 3. TREATED AMar 15, 2007 · N786AT · Boeing 727214 · Horizontal Stabilizer, Plate/SkinSDR DHL2007786501Skin · damagedAFT AIR STAIRS OUTER SKIN HAS A CREASE FWD OF BS 1323-1342, RBL 17-24. CUT OUT DAMAGED AREA 2" BY 1.5" IAW B727 SRM 52-10-2 FIG 3. FAB DOUBLER 16" BY 6.375" BY .050, 7075T6 AND FILLER 2" BY .75'BY .040" IAW B727 SRM 52-10-1 AND 52-10-2. TREATED ALODINE AND Mar 14, 2007 · N786AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHL2007786519Hinge · crackedEXT FUSELAGE MCD HINGE AFT SEGMENT AFT MOST LOBE IS CRACKED. REMOVED HINGE AT EXT FUSE MCD AFT SEGMENT IAW AEI B727 FREIGHTER CHAPTER 52 FIG 5201 A REVF. FABRICATED AFT SEGMENT, MATERIAL MS20001-16-7200 PO NR 9002527 DIM 18" IAW B727 FREIGHTER CHAPTER 52 FIGMar 13, 2007 · N786AT · Boeing 727214 · Fuselage, Door HingeSDR DHL200786500Beam · corrodedHORIZONTAL WALKING BEAM AND CHORDS/HAVE HEAVY CORROSION ON LT SIDE BS 312 ON UPPER CHORD AREA, ALSO SOME CORROSION. REMOVED CORRODED VERTICAL ON LT WALKWAY BEAM AREA STA 312 IAW B727 SRM. CUT OUT CORRODED WEB SECTION AT STA 312 3" X 1.5" IAW B727 SRM 51-40-2Apr 19, 2006 · N786AT · Boeing 727214 · Fuselage Main, StructureSDR DHL2005786003Transmitter · failedNR 2 EPR GAUGE HAD NO INDICATION AS TAKEOFF THRUST APPLIED. TAKEOFF WAS REJECTED. ALL ENG INDICATIONS WERE NORMAL BEFORE LOSS OF EPR GAUGE. N1, N2, FUEL FLOW AND EGT FUNCTIONING NORMAL. DEFERRED NR 2 EPR PER MEL 77-1-1. CAT A. KPS CONTROL NR 23343 AT 0953.Nov 25, 2005 · N786AT · Boeing 727214 · Engine Pressure Ratio (EPR)SDR DHL2005786002Transmitter · malfunctionedDISC - NR 1 ENG OIL PRESSURE BELOW RED LINE DURING TAXI OUT. RAN ABNORMAL PROCEDURE, SHUT ENGINE DOWN. REMOVED AND REPLACED NR 1 ENG OIL PRESSURE TRANSMITTER IAW B727 MM 79-32-01. OPS CHECKS GOOD.Sep 3, 2005 · N786AT · Boeing 727214 · Engine Oil PressureSDR DHL2005786001Indicator · malfunctionedNOTED LOSS OF B-HYD SYSTEM QUANTITY AS WELL STANDBY QUANTITY PERFORMED ABNORMAL PROCEDURE AFTER LANDING STANDBY QUANTITY WENT TO FULL. FOUND B SYS QTY INDICATOR DEFECTIVE; FOUND STANDBY QTY FULL REMOVED AND REPLACED B-SYS QTY INDICATOR IAW M/M 29-33-0 SERVICApr 20, 2005 · N786AT · Boeing 727214 · Hydraulic Indicating SystemSDR 20010207SG015Turbine · failedMDW - FLT 7186 - DURING A REPOSITIONING FLIGHT, ENGINE NR 3 FAILED ON TAKEOFF, AIRCRAFT DIVERTED TO ORD WITHOUT FURTHER INCIDENT. CONTAINED TURBINE FAILURE, NO FUSELAGE DAMAGE, BUT TAILPIPE SUSTAINED AN .25 INCH HOLE AT ABOUT 2 INCHES FROM THE END. AIRCRAFT Nov 16, 2000 · N786AT · Boeing 727214 · Turbine SectionSDR 20001208AP011Drive Shaft · leakingPIE-IND - DURING CLIMB, THE A HYDRAULIC SYSTEM FAILED. AIRCRAFT DIVERTED TO MCO. THE RIGHT FLAP POWER DRIVE WAS LEAKING AT THE MATTING SURFACE. REPLACED THE POWER DRIVE, LEAK CHECKED AND FOUND OK. (M)Mar 11, 2000 · N786AT · Boeing 727214 · Trailing Edge Flap Control SystemSDR 20000412AP001Cable · looseLAS-IND - FLT 402 - LOUD POPPING UNDER FLOOR IN EMERGENCY WINDOW EXIT ROW, REPORTED BY FLIGHT ATTENDANTS AND PASSENGERS DURING DESCENT AND APPROACH. THE FLOOR IN CABIN AT ROW 19 MOVES AN INCH AND POPS DURING FLIGHT. FOUND LOW CABLE TENSION TO LEFT AND RIGHT Dec 6, 1999 · N786AT · Boeing 727214 · Landing Gear Retraction/Extension SystemSDR 99ZZZM268Turbine · failedMDW - ABORTED TAKEOFF, TAXIED BACK TO GATE. THE NR 2 ENGINE FAILED AND SOME DEBRIS WERE NOTED ON THE RUNWAY. THE NR 3 AND NR 4 TURBINE BLADES FAILED FOR UNKNOWN REASON. ENGINE WAS REPLACED AND TESTED OK. AIRCRAFT RETURNED TO SERVICE. CONTAINED DAMAGE, LIMFeb 8, 1999 · N786AT · Boeing 727214 · Turbine SectionSDR 98ZZZM467Battery · dischargedCEILING EGRESS LIGHT AT ROW 24 IS INOP. REMOVED AND REPLACED BATTERY, OPS CHECKED NORMAL. (M)May 20, 1998 · N786AT · Boeing 727214 · Emergency LightingSDR 98ZZZX1955Charger · failedEGRESS CEILING EXIT LIGHT INOPERABLE AT ROW 5A-F. REMOVED AND REPLACED BATTERY CHARGER.Apr 27, 1998 · N786AT · Boeing 727214 · Emergency LightingSDR 97ZZZX1967Battery · dischargedIND - DURING P/F, FOUND OVERHEAD EGRESS 'EXIT' SIGN BETWEEN L2 AND R2 DOORS FLICKERS WHEN ON. REMOVED AND REPLACED BATTERY PACK, LIGHT OPS CHKS NORMAL.Jan 26, 1997 · N786AT · Boeing 727214 · Emergency Lighting
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