N762AT, cancelled Nov 30, 2010

Service difficulty reports · 65

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 = 'N762AT' AND deregistration_id = 'N762AT-2010-11-30'
  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 EE4Y10351Floorbeam · corrodedDURING INSP, LOWER FUSELAGE AFT CARGO COMPARTMENT STA 1130 FLOORBEAM UPPER CHORD CORRODED.Aug 18, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Floor BeamSDR EE4Y1010347Skin · dentedRIGHT WING OTBD AILERON, LOWER SURFACE WITH DENT AND BULGED SKIN.Aug 17, 2010 · N762AT · Boeing 7272B7 · AileronsSDR EE4Y1010346Stringer · cracked(EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010345Stringer · crackedEMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010344Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010343Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010342Stringer · crackedEMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010341Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010329Keelbeam · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FROM 950D TO STA 1000, KEEL BEAM LT CORRODED.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, KeelSDR EE4Y1010328Cover · corrodedLOWER FUSELAGE, RAM AIR DOOR INLET AREA, VERTICAL FIXED COVER WITH CORROSION.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, StructureSDR EE4Y1010327Floor Support · corrodedMAIN CARGO CABIN FLOOR SUPPORT CHANNEL CORRODED AT BS 1145, LBL 12.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR EE4Y1010326Keelbeam · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 989, KEEL BEAM RT WITH CORROSION.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, KeelSDR EE4Y1010325Skin Panel · crackedLOWER FUSELAGE SKIN WITH CRACK AT BS 243, WL 178, LT SIDE.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHLA200800132Oil Filter · bypassingNR 3 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT PRESS TO TEST CAUSED LIGHT TO BE BRIGHTER SHUT DOWN ENGINE IN ACCORDANCE WITH ABNORMAL PROCEDURES RESOLUTION: REMOVED AND REPLACED NR 3 MAIN OIL FILTER PER MM CH 79-00 OPS CHECK NORMAL. A/C WAS GROUNDED.Nov 19, 2008 · N762AT · Boeing 7272B7 · Turbine Engine Oil SystemSDR DHL2008F00001Tab · delaminatedA 3 X 1 INCH DELAMINATION ON RT WING O/B AILERON BALANCE TAB AT TRAILING EDGE. AILERON BALANCE TAB WAS REMOVED AND REPLACED IAW BOEING 727 MAINTENANCE MANUAL 27-10-41. OPERATION CHECK NORMAL. (A)Jun 27, 2008 · N762AT · Boeing 7272B7 · Aileron TabsSDR DHLA200800007Battery · inoperativeFLT 152, EMERGENCY EXIT LIGHTS DON'T WORK. REMOVED AND REPLACED BATTERIES IN FWD AND AFT EMERGENCY EXIT LIGHTS, OPS CHECK GOOD IAW B727 MM 33-50-71, P/N 37067-001 4 EACH. ACFT GROUNDED.Jan 19, 2008 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHLA200800005Light · dislodgedFLT 577, EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR FELL OFF DURING TAKEOFF ROLL. REINSTALLED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR. OPS CK. GOOD PER MM 33-50-01. ACFT GROUNDED.Jan 18, 2008 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHLA200700080Switch · malfunctionedAPPROXIMATLY 35 MIN, AFTER TAKEOFF NR 3 ENG OIL PRESSURE/BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE ACCOMPLISHED, DETERMINED THAT BYPASS MODE WAS RESPONSIBLE AND ENGINE WAS SHUT DOWN AT 0835Z. PRESSURE AND QUANTITY WAS NORMAL PRIOR TO SHUT DOWN. WINDMILL Dec 8, 2007 · N762AT · Boeing 7272B7 · Engine Oil Indicating SystemSDR DHLA200700050Fitting · failedUPON FLAP RETRACTION FROM FLAPS 2 TO 0, SYSTEM A HYD QTY WENT TO 0. FOUND FITTING BLOWN OUT ON NR 7 SLAT SHUTTLE VALVE. REPLACED NR 7 SLAT ACTUATOR SHUTTLE VALVE PER M/M 27-81-71. SERVICED HYDRAULICS TO FULL PER 12-12-0. OPS CHECKS NORMAL.Oct 3, 2007 · N762AT · Boeing 7272B7 · Leading Edge Slat ActuatorSDR DHL2007762502Support Angle · crackedFOUND CRACK IN LT AFT AIR STAIRS TORQUE BOX ON UPPER WEB SUPPORT ANGLE, APPROX BS 1253. MADE TWO EACH CUT OUTS FOR ACCESS, 4 BY 4 AT UPPER WEB IAW B727 SRM 51-10-1. REMOVED CRACKED SUPPORT ANGLE IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE USING 7075TMar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2007762501Torque Box · gougedLEFT AFT AIR STAIRS TORQUE BOX LIGHTING HOLE GOUGED BS 1320. ROUTED OUT GOUGED AREA, MATERIAL LOSS .008 IAW B727 SRM 53-30-1 FIG 1. FAB REPAIR DOUBLER 4" BY 2.5" BY .050, 7075T6 IAW B727 SRM 53-10-2 FIG 6 AND 51-40-1, FIG 1. TREATED ALODINE AND PRIMED IAW BMar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Main, StructureSDR DHL2006762511Seat Track · corrodedFOUND CABIN SEAT TRACK HAS CORROSION AT BS 650 LBL 45. REMOVED CORROSION AT MAIN CABIN SEAT TRACK BS 650 LBL 45, CORROSION IS OUT OF LIMITS IAW B727 SRM 51-10-1 AND 53-10-1 FIG 4. REMOVED SEAT TRACK FROM BS 620-710 LBL 45 IAW B727 SRM 51-30-2. FAB NEW SEAT Jul 12, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762512Seat Track · corrodedFOUND CABIN SEAT TRACK RBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 - RBL 24 STA 480-690 IAW B727 SRM 51-30-2. REMOVED SEAT TRACK AT RBL 24 STA 480-660 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK OF BAC1520-792 DIM 17.5' PO NR 9003095 IAW Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762510Seat Track · corrodedCABIN SEAT TRACK LBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 TO LBL 45 FOR ACCESS IAW SRM 51-30-2, BS 480-690 SEAT TRACK CORROSION FOUND OUT OF LIMIT IAW SRM 51-10-1 & SRM 53-10-1 FIG. 4. REMOVED SEAT TRACK LBL24 BS 480-690 IAW SRM 51-30-Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762508Mount · crackedNR 5 LE FLAP INBD ACTUATOR MOUNT BRACKET IS CRACKED BY THE LWR CORNER. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW B727 SRM 51-30-2. FAB NEW I/B MOUNT WEB IAW DWG NR 65-16263. TREATED AND PRIMED WEB MOUNT AND WORKING AREA IAW B727 SRM 51-10-2. INSTALLED I/Jul 6, 2006 · N762AT · Boeing 7272B7 · Wing, Attach FittingsSDR DHL2006762515Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION AT BS 480-620 RBL 45" BALL MAT AREA. REMOVED CABIN FLOORBOARDS RBL 24-RBL 65 FOR ACCESS IAW B727 SRM 51-30-2. REMOVED SEAT TRACK RBL 45 STA 480-620 FOR REPAIR, CORROSION WAS FOUND OUT OF LIMITS IAW B727 SRM 51-30-2 AND SRM 53-1Jun 30, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762501Frame · crackedNR 6 SLAT AT ACT ROD END ATTACHMENT WS 515 HAS BOTH I/B & O/B FRAMES CRACKED FWD. REMOVED I/B & O/B NR 6 SLAT FRAMES AT WS 515 IAW B727 SRM 51-30-2, FAB NEW I/B & O/B FRAMES FROM 20024-0 .040 PO 9003230 DIM. FOR BOTH FRAMES 6 X 16 INCHES IAW B727 SRM 57-50-2Jun 30, 2006 · N762AT · Boeing 7272B7 · Leading Edge DevicesSDR DHL2006762514Wedge · dentedRT O/B AILERON WEDGE UPPER SURFACE IS DENTED 2 PLACES. REMOVED RT O/B AILERON WEDGE AS PER B727 SRM 51-30-2. INSTALLED REPAIRED WEDGE VENDOR ORDER NR 500080771 P/N 65-21725-19 AT RT O/B AILERON AS PER B727 SRM 51-30-2Jun 29, 2006 · N762AT · Boeing 7272B7 · AileronsSDR DHL2006762513Firewall · damagedNR 2 VERT FIREWALL HAS HOLE WORN THROUGH DOUBLER 6:30 POSITION AT T/E STA 1352. REMOVED EXISTING REPAIR AT NR 2 VERT FIREWALL 6:30 POSITION IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .050 PO NR 900342 DIM 11 3/4" BY 2 1/2" IAW B727 SRM 5Jun 29, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, BulkheadSDR DHL2006762509Skin · delaminatedLT WING, INBD FLAP TE IS DELAMINATED ON OUTBD TE WBL 243. REMOVED PREVIOUS REPAIR AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPAIR SKIN APPROX 6 1/2" BY 4 AND EXTERNAL DOUBLER APPROX 3" BY 4" FROM 7075T6 .016 PO NR 9003142. CLEANED, PREPPED, APPLIEJun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762506Skin · wornLT WING INBD FLAP, FORE FLAP L/E HAS WEAR SPOT ON SKIN WBL 114. REMOVED DAMAGED DOUBLER L/WING I/B FORE FLAP L/E WBL 114 AS PER B727 SRM 51-30-2. FABRICATED NEW DOUBLER 7" BY 8" 2024T3 .063 PO NR 9003310 AS PER B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUJun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762507Skin · crackedREF NR 072657 DISCREPANCY, RT WING T/E UPPER SURFACE AT NR 13 SPOILER CTR HINGE HAS SKIN CRACKED. REMOVED FASTENERS ON RT T/E UPPER NR 13 SPOILER IAW SRM 51-30-2, CUT OUT DAMAGE SECTION .7500 INCH X ,2500 AT RT WING T/E UPPER SURFACE NR 13 SPOILER HINGE SKIN Jun 29, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHL2006762504Skin · delaminatedRIGHT O/B MID FLAP WBL 348-358 HAS UPPER T/E DELAMINATED. CUT OUT DELAMINATED AREA R/W O/B MID FLAP UPPER SKIN APPROX 3.25 X 22 INCHES IAW SRM 51-40-20 PARA 6 & 7. FABBED ONE SKIN REPLACEMENT APPROX .75 X 22 INCHES AND ONE SPLICE PLATE 3 X 3.25 INCHES USING Jun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762525Web · crackedAT RT SIDE OF AFT AIRSTAIR WELL CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. CUT OUT DAMAGED SECTION 11/8X1 AT RT SIDE OF AFT AIRSTAIR WELL TORQUE BOX WEB LIGHTENING HOLE STA 1237 IAW B727 SRM 51-40-2. FABRICATED DOUBLERS 7075T-6 .040Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762522Torque Box · crackedAT LT SIDE OF AFTSTAIR WELL, CRACK EMANATING FROM UPPER LIGHTENING HOLE IN TORQUE BOX AT BS 1263. REMOVED EXISTING DOUBLER AT LT SIDEWALL AFT AIRSTAIR WEB BS 1263 IAW SRM 51-30-2. FAB. NEW REPAIR DOUBLER FROM 7075T6 .040 PO NR 9003137 APPROX. DIM. 3 INCH X 3 IJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762521Structure · crackedAT LT SIDE OF AFT AIRSTAIR WELL 2 CRACKS EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. REMOVED EXISTING DOUBLER AT LT SIDE AFT AIRSTAR WEB BS 1237 IAW B727 SRM 51-30-2. FAB NEW DOUBLER FROM 7075T6 .040 PO NR 9003137 DIM.3" BY 3" IAW B727 SRMJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, StructureSDR DHL2006762517Web · crackedAFT AIRSTAIR DOOR SIDEWALL CRACKED AT LT ROLLER ON LOWER END OF STAIRS. REMOVED EXISTING REPAIR DOUBLER AT AFT AIRSTAIR SIDEWALL WEB LT ROLLER IAW B727 SRM 51-30-2. FAB NEW DOUBLER FROM 7075T5 .040 PO NR 9003137 APPROX 3"BY 3" IAW B727 SRM 51-40-2 FIG 1 AND Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762516Torque Box · crackedAT LT SIDE OF AIRSTAIR WELL CRACK EMANATING FROM UPPER LIGHTENING HOLE TORQUE BOX AT BS 1303. REMOVED PREVIOUS REPAIR DOUBLER AT LT SIDE AFT AIRSTAIR SIDEWALL WEB BS 1303 IAW B727 SRM 51-30-2. FAB NEW REPAIR DOUBLER FROM 7075T6 .040 PO NR 9003134 APPROX 3" BJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762500Web · crackedAT RIGHT SIDE OF AFT AIRSTAIR WELL, CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1225. REMOVED INTERIOR ACCESS PANEL AT RT SIDE OF AFT AIRSTAIRS STA 1183-1237 TORQUE BOX WEB AREA FOR ACCESS AS PER B727 SRM 51-30-2. CUTOUT DAMAGE .5 X .5 INCJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762520Angle · crackedRIGHT INBD MID FLAP REAR LWR CHORD ANGLE CRACKED WBL 105. REMOVED SEAL RETAINER AND LWR CHORD ANGLE SECTION AND LOWER SKIN IAW B727 SRM 51-30-2. FAB NEW LOWER CHORD AT RIGHT INBD MID FLAP WBL 105 FROM P/N BAC1517-1367 PO NR 501953 IAW B727 SRM 51-50-2 FIG 5 Jun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762518Angle · crackedLEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOW CRACKS 2 WBL 105. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD IAW B727 SRM 51-30-2. FAB NEW MID FLAP LWR CHORD ANLGE FROM P/N BAC1503-100046 PO NR 627846 APPRJun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762503Hinge · crackedL1 DOOR CUTOUT, UPPER HINGE HAS EVIDENCE CRACK. NDT CONFIRMED CRACK IS ABOUT 1 INCH LONG, MARKED END OF CRACK 727 NDT PART 6, 51-00-00 FIG 23. OPENED AREA INTERIOR PANELS AT LT STA 259 FOR ACCESS. CUTOUT DAMAGED SECTION 1.75 X 1.5 INCH AT L1 DOOR UPPER HINGJun 27, 2006 · N762AT · Boeing 7272B7 · Fuselage, Door HingeSDR DHL2006762502Skin · dentedEXT FUS BS 1055 BELOW STR 20R HAS DENT. DENT AT BS 1055 BELOW STR 20R IS OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUTOUT DAMAGE AREA DIM 2" BY 2 3/4" AND 2" BY .750 IAW B727 SRM 53-30-3 FIG 5. REMOVED FASTENERS FOR SKIN REPAIR IAW B727 SRM 51-30-2. FAB REJun 26, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006762523Skin Panel · delaminatedL/WING TE UPPER PANEL DELAMINATED AT LWBL 88 BS 889 IN/SQ WITH NO CRACKS EVIDENT IN OUTER SKIN. CUT OUT DELAMINATED AREA ON UPPER SKIN OF L/WING TE PANEL APPROX 10" DIA. FABRICATED DOUBLER 14" DIA FROM .016" 7075T6 PO# 526029 AND BONDED. REMOVED SECTION OF Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHL2006762505Mount · crackedNR 5 KRUGER FLAP ACTUATOR MOUNT W.S. 230 OB LOWER CORNER IS CRACKED. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW SRM 51-30-2 . FAB NEW OB ACTUATOR MOUNT WEB IAW MFG DWG NR 65-16263, TREATED AND PRIMED WEB MOUNT AND WORKING AREA IAW SRM 51-10-2, INSTALLED NEW Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Attach FittingsSDR DHL2006762001Brake · malfunctionedLEFT BRAKE IS SOFT AND REQUIRES TWICE AS MUCH PRESSURE TO STOP AIRCRAFT AS RIGHT BRAKE. INSPECTED ALL BRAKES , NO DEFECTS NOTED. TAXIED AIRCRAFT, TESTED BRAKES, NO DEFECTS NOTED. WORK DONE IAW B-727 MM 32-40-00 AND JRH 5.2.Jan 26, 2006 · N762AT · Boeing 7272B7 · Landing Gear Brake SystemSDR DHL2005762004Battery · inoperativeEMERGENCY EXIT LIGHT IN GALLEY WON`T TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW M/M 33-50-101, OPS CK NORMAL P/N MISC062.Oct 28, 2005 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHL2005762003Oil Cooler · leakingAT 10,000FT, THE CREW OBSERVED THE NR 3 ENGINE PARAMETERS FLUCTUATING,FOLLOWED SPECIAL PROCEDURES SHUT DOWN THE ENGINE,DECLARED AN EMERGENCY AND DIVERTED BACK TO PHOENIX. AFTER TAKE OFF, NR 3 ENGINE PARAMETERS BEGAN FLUCTUATING. PERFORMED ABNORMAL PROCEDURE PMay 3, 2005 · N762AT · Boeing 7272B7 · Engine Oil CoolerSDR DHL2005762002Light · looseEMERGENCY EXIT LIGHTS AT FRONT ENTRY DOOR NEEDS TO BE REMOUNTED. INSTALLED EMERGENCY LIGHT AT FWD ENTRY DOOR AND OPS CHECKS SERVICEABLE IAW MM 33-50-01.Apr 23, 2005 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHL2005762001Brake Assy · malfunctionedLEFT BRAKE STICKS AND CHATTERS WHEN TAXIING. BLEED NR 2 BRAKE IAW MM 32-41-00. TAXIED A/C, OPS CKS GOOD. OK TO CONTINUE.Jan 20, 2005 · N762AT · Boeing 7272B7 · Brake
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