# Service difficulty reports: N762AT, cancelled Nov 30, 2010

A list on [N762AT, cancelled Nov 30, 2010](https://openairdocs.org/deregistered/N762AT-2010-11-30.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 65 reports

- [SDR EE4Y10351](https://openairdocs.org/sdr/EE4Y10351.md): Floorbeam · corroded · Aug 18, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Floor Beam
  > DURING INSP, LOWER FUSELAGE AFT CARGO COMPARTMENT STA 1130 FLOORBEAM UPPER CHORD CORRODED.
- [SDR EE4Y1010347](https://openairdocs.org/sdr/EE4Y1010347.md): Skin · dented · Aug 17, 2010 · N762AT · Boeing 7272B7 · Ailerons
  > RIGHT WING OTBD AILERON, LOWER SURFACE WITH DENT AND BULGED SKIN.
- [SDR EE4Y1010346](https://openairdocs.org/sdr/EE4Y1010346.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > (EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.
- [SDR EE4Y1010345](https://openairdocs.org/sdr/EE4Y1010345.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.
- [SDR EE4Y1010344](https://openairdocs.org/sdr/EE4Y1010344.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.
- [SDR EE4Y1010343](https://openairdocs.org/sdr/EE4Y1010343.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.
- [SDR EE4Y1010342](https://openairdocs.org/sdr/EE4Y1010342.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.
- [SDR EE4Y1010341](https://openairdocs.org/sdr/EE4Y1010341.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.
- [SDR EE4Y1010329](https://openairdocs.org/sdr/EE4Y1010329.md): Keelbeam · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Keel
  > LOWER FUSELAGE AFT CARGO COMPARTMENT FROM 950D TO STA 1000, KEEL BEAM LT CORRODED.
- [SDR EE4Y1010328](https://openairdocs.org/sdr/EE4Y1010328.md): Cover · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Structure
  > LOWER FUSELAGE, RAM AIR DOOR INLET AREA, VERTICAL FIXED COVER WITH CORROSION.
- [SDR EE4Y1010327](https://openairdocs.org/sdr/EE4Y1010327.md): Floor Support · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > MAIN CARGO CABIN FLOOR SUPPORT CHANNEL CORRODED AT BS 1145, LBL 12.
- [SDR EE4Y1010326](https://openairdocs.org/sdr/EE4Y1010326.md): Keelbeam · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Keel
  > LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 989, KEEL BEAM RT WITH CORROSION.
- [SDR EE4Y1010325](https://openairdocs.org/sdr/EE4Y1010325.md): Skin Panel · cracked · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN WITH CRACK AT BS 243, WL 178, LT SIDE.
- [SDR DHLA200800132](https://openairdocs.org/sdr/DHLA200800132.md): Oil Filter · bypassing · Nov 19, 2008 · N762AT · Boeing 7272B7 · Turbine Engine Oil System
  > NR 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.
- [SDR DHL2008F00001](https://openairdocs.org/sdr/DHL2008F00001.md): Tab · delaminated · Jun 27, 2008 · N762AT · Boeing 7272B7 · Aileron Tabs
  > A 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)
- [SDR DHLA200800007](https://openairdocs.org/sdr/DHLA200800007.md): Battery · inoperative · Jan 19, 2008 · N762AT · Boeing 7272B7 · Emergency Lighting
  > FLT 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.
- [SDR DHLA200800005](https://openairdocs.org/sdr/DHLA200800005.md): Light · dislodged · Jan 18, 2008 · N762AT · Boeing 7272B7 · Emergency Lighting
  > FLT 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.
- [SDR DHLA200700080](https://openairdocs.org/sdr/DHLA200700080.md): Switch · malfunctioned · Dec 8, 2007 · N762AT · Boeing 7272B7 · Engine Oil Indicating System
  > APPROXIMATLY 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
- [SDR DHLA200700050](https://openairdocs.org/sdr/DHLA200700050.md): Fitting · failed · Oct 3, 2007 · N762AT · Boeing 7272B7 · Leading Edge Slat Actuator
  > UPON 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.
- [SDR DHL2007762502](https://openairdocs.org/sdr/DHL2007762502.md): Support Angle · cracked · Mar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > FOUND 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 7075T
- [SDR DHL2007762501](https://openairdocs.org/sdr/DHL2007762501.md): Torque Box · gouged · Mar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Main, Structure
  > LEFT 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 B
- [SDR DHL2006762511](https://openairdocs.org/sdr/DHL2006762511.md): Seat Track · corroded · Jul 12, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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
- [SDR DHL2006762512](https://openairdocs.org/sdr/DHL2006762512.md): Seat Track · corroded · Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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
- [SDR DHL2006762510](https://openairdocs.org/sdr/DHL2006762510.md): Seat Track · corroded · Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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-
- [SDR DHL2006762508](https://openairdocs.org/sdr/DHL2006762508.md): Mount · cracked · Jul 6, 2006 · N762AT · Boeing 7272B7 · Wing, Attach Fittings
  > NR 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/
- [SDR DHL2006762515](https://openairdocs.org/sdr/DHL2006762515.md): Seat Track · corroded · Jun 30, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 53-1
- [SDR DHL2006762501](https://openairdocs.org/sdr/DHL2006762501.md): Frame · cracked · Jun 30, 2006 · N762AT · Boeing 7272B7 · Leading Edge Devices
  > NR 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 57-50-2
- [SDR DHL2006762514](https://openairdocs.org/sdr/DHL2006762514.md): Wedge · dented · Jun 29, 2006 · N762AT · Boeing 7272B7 · Ailerons
  > RT 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 51-30-2
- [SDR DHL2006762513](https://openairdocs.org/sdr/DHL2006762513.md): Firewall · damaged · Jun 29, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, Bulkhead
  > NR 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 5
- [SDR DHL2006762509](https://openairdocs.org/sdr/DHL2006762509.md): Skin · delaminated · Jun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge Flaps
  > LT 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, APPLIE
- [SDR DHL2006762506](https://openairdocs.org/sdr/DHL2006762506.md): Skin · worn · Jun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge Flaps
  > LT 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 DOU
- [SDR DHL2006762507](https://openairdocs.org/sdr/DHL2006762507.md): Skin · cracked · Jun 29, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/Skin
  > REF 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
- [SDR DHL2006762504](https://openairdocs.org/sdr/DHL2006762504.md): Skin · delaminated · Jun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge Flaps
  > RIGHT 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
- [SDR DHL2006762525](https://openairdocs.org/sdr/DHL2006762525.md): Web · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AT 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-6.040
- [SDR DHL2006762522](https://openairdocs.org/sdr/DHL2006762522.md): Torque Box · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AT 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 I
- [SDR DHL2006762521](https://openairdocs.org/sdr/DHL2006762521.md): Structure · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, Structure
  > AT 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 SRM
- [SDR DHL2006762517](https://openairdocs.org/sdr/DHL2006762517.md): Web · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AFT 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
- [SDR DHL2006762516](https://openairdocs.org/sdr/DHL2006762516.md): Torque Box · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AT 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" B
- [SDR DHL2006762500](https://openairdocs.org/sdr/DHL2006762500.md): Web · cracked · Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AT 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 INC
- [SDR DHL2006762520](https://openairdocs.org/sdr/DHL2006762520.md): Angle · cracked · Jun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge Flaps
  > RIGHT 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
- [SDR DHL2006762518](https://openairdocs.org/sdr/DHL2006762518.md): Angle · cracked · Jun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge Flaps
  > LEFT 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 APPR
- [SDR DHL2006762503](https://openairdocs.org/sdr/DHL2006762503.md): Hinge · cracked · Jun 27, 2006 · N762AT · Boeing 7272B7 · Fuselage, Door Hinge
  > L1 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 HING
- [SDR DHL2006762502](https://openairdocs.org/sdr/DHL2006762502.md): Skin · dented · Jun 26, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > EXT 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 RE
- [SDR DHL2006762523](https://openairdocs.org/sdr/DHL2006762523.md): Skin Panel · delaminated · Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/Skin
  > L/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
- [SDR DHL2006762505](https://openairdocs.org/sdr/DHL2006762505.md): Mount · cracked · Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Attach Fittings
  > NR 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
- [SDR DHL2006762001](https://openairdocs.org/sdr/DHL2006762001.md): Brake · malfunctioned · Jan 26, 2006 · N762AT · Boeing 7272B7 · Landing Gear Brake System
  > LEFT 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.
- [SDR DHL2005762004](https://openairdocs.org/sdr/DHL2005762004.md): Battery · inoperative · Oct 28, 2005 · N762AT · Boeing 7272B7 · Emergency Lighting
  > EMERGENCY 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.
- [SDR DHL2005762003](https://openairdocs.org/sdr/DHL2005762003.md): Oil Cooler · leaking · May 3, 2005 · N762AT · Boeing 7272B7 · Engine Oil Cooler
  > AT 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 P
- [SDR DHL2005762002](https://openairdocs.org/sdr/DHL2005762002.md): Light · loose · Apr 23, 2005 · N762AT · Boeing 7272B7 · Emergency Lighting
  > EMERGENCY 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.
- [SDR DHL2005762001](https://openairdocs.org/sdr/DHL2005762001.md): Brake Assy · malfunctioned · Jan 20, 2005 · N762AT · Boeing 7272B7 · Brake
  > LEFT BRAKE STICKS AND CHATTERS WHEN TAXIING. BLEED NR 2 BRAKE IAW MM 32-41-00. TAXIED A/C, OPS CKS GOOD. OK TO CONTINUE.

Next page: https://openairdocs.org/deregistered/N762AT-2010-11-30/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N762AT-2010-11-30/reports

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