# Service difficulty reports: N765AT, cancelled Aug 6, 2010

A list on [N765AT, cancelled Aug 6, 2010](https://openairdocs.org/deregistered/N765AT-2010-08-06.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 · 93 reports

- [SDR DHLA200900034](https://openairdocs.org/sdr/DHLA200900034.md): Battery Pack · malfunctioned · Jun 7, 2009 · N765AT · Boeing 727264 · Emergency Lighting
  > DEFECT DESCRIPTION; ENTRY WAY EMERGENCY EXIT LIGHT FLICKERS AND IS DIM WHEN STDY BATTERY CHECK IS DONE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIES IAW B727 M/M 33-50-01. OPS CK NORMAL, P/N-55-2713-1 2EA.
- [SDR DHLA20087651016](https://openairdocs.org/sdr/DHLA20087651016.md): Casting · cracked · Oct 16, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > UPON VISUAL INSPECTION FOUND THE NR 6 K-FLAP CENTER HINGE CASTING OUTBOARD SIDE AT THE ATTACH POINT FOR THE ACTUATOR ROD END CRACKED APPROX 2 INCHES IN LENGTH. K-FLAP IS TO BE CHANGED. REMOVED PART NUMBER IS 65-16227-18 SERIAL NUMBER BN1869. UNKNOWN IS THE
- [SDR DHL2008F00000](https://openairdocs.org/sdr/DHL2008F00000.md): Pin · damaged · Jul 2, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > SMALL DAMAGE ON NR (6) L/E SLAT AT IB GUIDE PIN EXISTING DOUBLER. DAMAGE WAS BLENDED SMOOTH LESS THAN 1 INCH X.100 MATERIAL LOSS, WORK ACCOMPLISHED IAW SRM 57-50-01. (K)
- [SDR DHLA200800041](https://openairdocs.org/sdr/DHLA200800041.md): Fire Warning · malfunctioned · Apr 22, 2008 · N765AT · Boeing 72764 · Fire Detection
  > FLT NR 1489 FIRE WARNING BELL ONLY AT CRUISE FL 330 COMPLETED ABNORMAL PROCEDURES ALL SYSTEMS TESTED NORMAL. PERFORMED SYSTEM CK OF FIRE DETECTION SYSTEM OPS NORMAL IAW MM 26-11-0. AIRCRAFT WAS GROUNDED.
- [SDR DHLA200800039](https://openairdocs.org/sdr/DHLA200800039.md): Trim Switch · broken · Apr 9, 2008 · N765AT · Boeing 727200 · Elevator Tab Control System
  > FLT 589, WHEN THRUST LEVERS ADVANCED FOR TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. FLAPS 15 SPEED BRAKES STOWED TRIM SET AT 6.6. FOUND UPPER STAB. TRIM SWITCH (S532) RETURN MECHANISM BROKEN. R&R SWITCH IAW MM 31-26-24 & WDM 27-43-01. TESTED TAKE-OFF WARNING I
- [SDR DHL2008765033](https://openairdocs.org/sdr/DHL2008765033.md): Rib · cracked · Feb 1, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, NR 2 SLAT INBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED INNER SKIN PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED DAMAGE INBOARD RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5 AND 51-40-1. TREATED AND PRIMED HOLES AND AREA IAW
- [SDR DHL2008765020](https://openairdocs.org/sdr/DHL2008765020.md): Skin · dented · Feb 1, 2008 · N765AT · Boeing 727264 · Horizontal Stabilizer, Plate/Skin
  > DURING C CHECK, 2 EACH PROTRUDING DENTS ON RIGHT HORIZONTAL STABILIZER UPPER SURFACE 3" INBOARD OF PCU PANEL. REWORKED TO ORIGINAL CONTOUR IAW SRM 51-40-1, 2 EACH DENTS. C/W HFEC IAW NDTM PT 6 51-00-00 FIG 23, CRACK INDICATION. REMOVED DAMAGED DRILLED HOLE
- [SDR DHL2008765015](https://openairdocs.org/sdr/DHL2008765015.md): Structure · cracked · Feb 1, 2008 · N765AT · Boeing 727264 · Trailing Edge Flaps
  > DURING C CHECK, LEFT INBOARD MID FLAP LOWER TRAILING EDGE WBL 102 AT PUSH-ROD IS CRACKED, INBOARD. REMOVED INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW SECTION DIMENSION 57.5" LONG IAW SRM 53-30-5 AND 57-50-2 FIG
- [SDR DHL2008765010](https://openairdocs.org/sdr/DHL2008765010.md): Frame · gouged · Jan 29, 2008 · N765AT · Boeing 727264 · Fuselage Main, Frame
  > DURING C CHECK, FUSELAGE FRAME GOUGED AT BS 480 BELOW STRINGER 17L. BLENDED AREA AT BS 480 BELOW STRINGER 17L, ORIGINAL MATERIAL 0.150", MATERIAL REMAINING WAS APPROXIMATE 40% OF THICKNESS LEAVING 60% FOUND TO BE WITHIN LIMITS IAW EO NR OE-N765AT-1-25-08. TR
- [SDR DHL2008765009](https://openairdocs.org/sdr/DHL2008765009.md): Frame · damaged · Jan 29, 2008 · N765AT · Boeing 727264 · Fuselage Main, Frame
  > DURING C CHECK, 2 MISDRILLED HOLES IN FUSELAGE FRAME STRINGER 18L BS 480. REMOVED AND REINSTALLED HINGE ASSEMBLY AT FRAME, STRINGER 18 BS 480 IAW STC DRAWING 727021025-1, DRILLED THROUGH THE TWO HOLES AND INSTALLED MS20426AD6-6 RIVET FLUSH IAW DRAWING NR 7270
- [SDR DHL2008765001](https://openairdocs.org/sdr/DHL2008765001.md): Skin · misrepaired · Jan 29, 2008 · N765AT · Boeing 727264 · Fuselage Main, Plate/Skin
  > DURING C CHECK, EXISTING REPAIR HAS BLIND RIVETS INSTALLED IN DOUBLER SHOULD BE SOLID FASTENERS PER SRM AT BS 1185 STRINGER 17L. REMOVED EXISTING REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 26 AND 53-30-2 FIG 3. ZERO TIMING OF
- [SDR DHL2008765024](https://openairdocs.org/sdr/DHL2008765024.md): Skin · cracked · Jan 27, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, NR 4 SLAT UPPER SKIN CRACKED AT INBOARD HOOK MOUNT SCREW WS 390. STRIPPED AREA IAW B727 MM 51-20-1, C/S HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. CRACKS TERMINATE IN STOP DRILL HOLES. FABRICATED REPAIR PLATE MATERIAL USED 7075-T6 0.125" PO NR
- [SDR DHL2008765022](https://openairdocs.org/sdr/DHL2008765022.md): Beam · damaged · Jan 27, 2008 · N765AT · Boeing 727264 · Wing Main, Frame Structure
  > DURING C CHECK, REJECTED NR 105146 BECAUSE ORIGINAL FABRICATED 'J' BEAM WAS DAMAGED UPON INSTALLATION. RT WING TRAILING EDGE UPPER 'J' BEAM IS CRACKED AT WBL 118. REMOVED TRAILING EDGE PANEL FOR ACCESS AT RT WING IAW SRM 51-30-2. REMOVED 'J' BEAM AT RT SIDE
- [SDR DHL2008765016](https://openairdocs.org/sdr/DHL2008765016.md): Beam · cracked · Jan 25, 2008 · N765AT · Boeing 727264 · Wing Main, Frame Structure
  > DURING C CHECK, LT WING UPPER TRAILING EDGE PANEL SUPPORT 'J' BEAM WBL 124 IS CRACKED IN CUT OUT FORWARD OF NR 7 SPOILER ACTUATOR. REMOVED TRAILING EDGE UPPER PANEL FROM LT WING FOR ACCESS IAW SRM 51-30-2. REMOVED CRACKED 'J' BEAM IAW SRM 51-30-2. FABRICATE
- [SDR DHL2008765034](https://openairdocs.org/sdr/DHL2008765034.md): Bulkhead · corroded · Jan 23, 2008 · N765AT · Boeing 727264 · Fuselage Main, Bulkhead
  > DURING C CHECK, BS 227.8 BULKHEAD FORWARD LOWER WEB AND STIFFENER IS CORRODED. REMOVED STIFFENERS AND ATTACHED PARTS IN AREA FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION IAW SRM 51-40-4 FIG 1 AND 53-10-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-
- [SDR DHL2008765014](https://openairdocs.org/sdr/DHL2008765014.md): Structure · cracked · Jan 21, 2008 · N765AT · Boeing 727264 · Trailing Edge Flaps
  > DURING C CHECK: DISCREPANCY - RIGHT WING INBOARD FLAP, MID FLAP AFT IS CRACKED ON BOTH INBOARD AND OUTBOARD SIDE WBL 90.69 AND WBL 104.0. REMOVED NR 5 AND 6 TEAR DROP FAIRINGS AND RIGHT INBOARD MID FLAP LOWER SKIN TO GAIN ACCESS IAW SRM 51-30-2. REMOVED CRAC
- [SDR DHL2008765012](https://openairdocs.org/sdr/DHL2008765012.md): Stringer · corroded · Jan 21, 2008 · N765AT · Boeing 727264 · Fuselage Main, Longeron/Stringer
  > DURING C CHECK: DISCREPANCY - RT WHEEL WELL STRINGER 18A IS CORRODED AT WBL 70 ON FORWARD SIDE OF BS 880. REMOVED STRINGER 18A IAW SRM 51-30-2. FABRICATED STRINGER 18A IAW SRM 53-10-2 FIG 4, 51-10-3 AND 51-30-5. TREATED AND PRIMED PART AND AREA IAW SRM 51-1
- [SDR DHL2008765011](https://openairdocs.org/sdr/DHL2008765011.md): Support · cracked · Jan 21, 2008 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > DURING C CHECK, RIGHT WHEEL WELL SUPPORT STRUCTURE HAS CRACK AT BS 880 RBL 26. REMOVED SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 51-30-2. FABRICATED NEW SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 53-10-2 FIG 4 AND 51-10-3.
- [SDR DHL2008765003](https://openairdocs.org/sdr/DHL2008765003.md): Torque Box · cracked · Jan 21, 2008 · N765AT · Boeing 727264 · Fuselage Main, Structure
  > DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 5 O'CLOCK POSITION RIGHT SIDE BS 1265 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE DIMENSION 1" BY.75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6 AND 51
- [SDR DHL2008765021](https://openairdocs.org/sdr/DHL2008765021.md): Hinge · cracked · Jan 20, 2008 · N765AT · Boeing 727264 · Fuselage, Door Hinge
  > DURING C CHECK, MCD AFT HINGE SECTION IS CRACKED AT BS 612 STRINGER 4L. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR BS 612 STRINGER 4L IAW MM FIG 5201B REV E. FABRICATED HINGE SECTION IAW MM FIG 5201B REV E. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10
- [SDR DHL2008765032](https://openairdocs.org/sdr/DHL2008765032.md): Rib · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, NR 2 SLAT OUTBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 2 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLED ACCESS PAN
- [SDR DHL2008765030](https://openairdocs.org/sdr/DHL2008765030.md): Rib · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, CRACK INDICATION ON NR 4 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 4 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLE
- [SDR DHL2008765025](https://openairdocs.org/sdr/DHL2008765025.md): Skin · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, CRACKED ON NR 3 SLAT UPPER SURFACE AT INBOARD SLAT HOOK MOUNT SCREW WS 520. REMOVED HOOK FROM AREA IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR AT NR 3
- [SDR DHL2008765005](https://openairdocs.org/sdr/DHL2008765005.md): Torque Box · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Fuselage Main, Structure
  > DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 6 O'CLOCK POSITION RIGHT SIDE BS 1240 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLES 6 O'CLOCK POSITION BS 1240 RT IAW SRM 51-40-2 FIG 1, DIMENSION 1.25" BY.5". FABRICATED DOUBLER R
- [SDR DHL2008765004](https://openairdocs.org/sdr/DHL2008765004.md): Torque Box · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Fuselage Main, Structure
  > DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 12 O'CLOCK POSITION RIGHT SIDE OF STAIRWELL BS 1243 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE BS 1243 RIGHT DIMENSION 1.5" BY.5" IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR AT AFT
- [SDR DHL2008765002](https://openairdocs.org/sdr/DHL2008765002.md): Web · cracked · Jan 19, 2008 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > DURING C CHECK, CUT OUT DAMAGED AREA AFT STAIRWELL LIGHTENING HOLE 10 O'CLOCK POSITION DIMENSION CUT OUT 1.5" BY.75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR AT AFT STAIRWELL LIGHTNING HOLES 10 O'CLOCK POSITION IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1
- [SDR DHL2008765006](https://openairdocs.org/sdr/DHL2008765006.md): Cover · gouged · Jan 18, 2008 · N765AT · Boeing 727264 · Ailerons
  > DURING C CHECK, RT INBOARD AILERON UPPER INBOARD HINGE COVER HAS DEEP GOUGE. REMOVED COVER IAW SRM 51-30-2. FABRICATED NEW COVER IAW SRM 57-50-2 FIGURE 7 AND 51-20-1. TREATED AND PRIMED NEW COVER IAW SRM 51-10-2. INSTALLED NEW COVER AT RT WING INBOARD AIL
- [SDR DHL2008765031](https://openairdocs.org/sdr/DHL2008765031.md): Rib · cracked · Jan 17, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, CRACK INDICATION ON PREVIOUS REPAIR OF NR 3 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED NR 3 SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED CRACKED RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB IAW SRM 51-3
- [SDR DHL2008765018](https://openairdocs.org/sdr/DHL2008765018.md): Structure · gouged · Jan 16, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, RIGHT WING NR 6 SLAT TRAILING EDGE GOUGED AT HOOK FITTINGS WS 150 APPROXIMATE. REMOVED HOOK FITTING FROM ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIGURE 10. TREATED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTA
- [SDR DHL2008765017](https://openairdocs.org/sdr/DHL2008765017.md): Skin · cracked · Jan 16, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DRILLED 3 EACH CRACKED PLACES AROUND RIVETS AT INBOARD END WS 150 (DIAMETER 0.190") IAW SRM 51-10-1 AND 57-50-3 FIGURE 12. HFEC C/W AROUND ST
- [SDR DHL2008765026](https://openairdocs.org/sdr/DHL2008765026.md): Skin · cracked · Jan 15, 2008 · N765AT · Boeing 727264 · Spoilers
  > DURING C CHECK, NR 2 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. REMOVED ON LT WING TRAILING EDGE SKIN SECTION AT NR 2 SPOILER DIMENSION 36" BY 2.5" IAW SRM 51-30-2. FABRICATED NEW SKIN SECTION IAW SRM 57-30-2 FIG 4 AND 51-20-1. TREATED AND
- [SDR DHL2008765013](https://openairdocs.org/sdr/DHL2008765013.md): Skin · gouged · Jan 15, 2008 · N765AT · Boeing 727264 · Trailing Edge Flaps
  > DURING C CHECK, LT OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR IS GOUGED 2 PLACES. REMOVED OLD DOUBLER REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR IAW SRM 57-50-2 FIG 4. TREATED AND PRIMED NEW DOUBLER IAW SRM 51-10-2. INSTALLED NEW DOUBLER IA
- [SDR DHL2008765007](https://openairdocs.org/sdr/DHL2008765007.md): Skin · dented · Jan 15, 2008 · N765AT · Boeing 727264 · Leading Edge Devices
  > DURING C CHECK, RT WING WS 760 NR 8 SLAT UPPER SURFACE HAS A DENT AROUND FASTENER. EVALUATED AND FOUND DENT OUT OF LIMITS IAW SRM 57-50-1 FIG 2 DUE TO DENT BEING ON FASTENER. CUT OUT DAMAGED AREA DIMENSION 1.75" BY 1.125" IAW SRM 57-50-3 FIG 1. FABRICATED D
- [SDR DHL2008765008](https://openairdocs.org/sdr/DHL2008765008.md): Intercostal · cracked · Jan 12, 2008 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > DURING C CHECK, AFT CARGO COMPARTMENT BS 950A + 19" INTERCOSTAL LBL 5" HAS FASTENERS POPPED AND METAL CRACKED. REMOVED INTERCOSTAL AT AFT CARGO PIT IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW SRM 53-10-2 FIG 5 AND 51-20-1. LOCATED AND DRILLED NEW INTERC
- [SDR DHL2008765027](https://openairdocs.org/sdr/DHL2008765027.md): Skin · cracked · Jan 11, 2008 · N765AT · Boeing 727264 · Spoilers
  > DURING C CHECK, NR 3 SPOILER NR 3 HINGE CUT OUT ON LT WING TRAILING EDGE IS CRACKED. STOP DRILLED CRACK 0.250 IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR IAW SRM 51-20-1, 51-30-5 AND 57-30-4 FIG 10. ALODINED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INST
- [SDR DHL2008765029](https://openairdocs.org/sdr/DHL2008765029.md): Skin · cracked · Jan 9, 2008 · N765AT · Boeing 727264 · Spoilers
  > DURING C CHECK, NR 4 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250 INCH AND FABRICATED REPAIR DOUBLER IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT CONFIRMED STOP DRILL END STOP CRACK IAW NDT MM CH 51-00-00 PART 6 FI
- [SDR DHL2008765028](https://openairdocs.org/sdr/DHL2008765028.md): Skin · cracked · Jan 9, 2008 · N765AT · Boeing 727264 · Spoilers
  > DURING C CHECK, NR 4 SPOILER NR 3 HINGE CUT OUT ON LEFT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250" IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT STOP DRILL CONFIRMED END OF CRACK IAW NDT MM CH 51-00-00 PART 6. FABRICATED REPAIR DOUBLER IAW SRM
- [SDR DHL2008765019](https://openairdocs.org/sdr/DHL2008765019.md): Stringer · cracked · Jan 9, 2008 · N765AT · Boeing 727264 · Vertical Stabilizer, Spar/Rib
  > DURING C CHECK, VERTICAL STABILIZER NR 8 STRINGER CRACKED FIN STATION 133. REMOVED PREVIOUS REPAIR FROM AREA IAW SRM 51-30-2. FABRICATED 2 EACH REPAIR ANGLES IAW SRM 55-30-5 FIGURE 1 AND 55-30-2 FIGURE 2. HFEC VERIFIED CRACK TERMINATES IN FASTENER HOLE IAW
- [SDR DHL2007765001](https://openairdocs.org/sdr/DHL2007765001.md): Web · cracked · Nov 24, 2007 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > A-8 CHECK REF N/R 054239 AFT AIRSTAIR AREA LT TORQUE BOX AT STA 1263 LWR LIGHTING HOLE SKIN HAS 1 INCH CRACK AT 11:00 POSITION. CUT OUT DAMAGED AREA AT AFT AIRSTAIRS AREA LT TORQUE BOX STA 1263 LWR LIGHTING HOLE SKIN DIMENSION 3/4" BY 1/4" IAW B727 SRM 51-40-
- [SDR DHLA200700046](https://openairdocs.org/sdr/DHLA200700046.md): Light · dislodged · Sep 26, 2007 · N765AT · Boeing 727264 · Emergency Lighting
  > FOUND UPPER EMERG EXIT LIGHT DISLODGED. RE INSTALLED UPPER EMERGENCY EXIT LIGHT PER MM 33-50-00.
- [SDR DHLA200700041](https://openairdocs.org/sdr/DHLA200700041.md): Light · loose · Aug 31, 2007 · N765AT · Boeing 727264 · Emergency Lighting
  > EMERGENCY LIGHT ILLUMINATED ON TAKEOFF. FOUND COCKPIT EMERGENCY LIGHT ASSY LOOSE. RESECURED IN PLACE PERFORMED GROUND TEST IAW M/M33-50-01,TEST OK
- [SDR DHL2006765004](https://openairdocs.org/sdr/DHL2006765004.md): Brake Assy · noisy · Nov 1, 2006 · N765AT · Boeing 727264 · Landing Gear Brake System
  > LEFT BRAKE MAKES NOISE WHEN DEPRESSED AND AIRCRAFT SHAKES. BLED LEFT MLG BRAKES PER B727 MM CH 32-41-00. OPS AND LEAK CHECK GOOD.
- [SDR DHL2006765003](https://openairdocs.org/sdr/DHL2006765003.md): Indicator · failed · Sep 22, 2006 · N765AT · Boeing 727264 · Engine Oil Pressure
  > NR 3 OIL PRESSURE WENT TO 100 PSI ON T/O ROLL. ABORTED T/O AT 10 KTS. REMOVED AND REPLACED NR 3 OIL PRESSURE IND IAW MM 79-32-00. OPS CHECK GOOD IAW JRH 5.2.
- [SDR DHL2006765002](https://openairdocs.org/sdr/DHL2006765002.md): Engine · malfunctioned · Jun 27, 2006 · N765AT · Boeing 727264 · Engine (Turbine/Turboprop)
  > ON ENG START - START WAS NORMAL. ENG ACCELERATED TO 30 PERCENT N1, 520 EGT 52 PERCENT N2. GRD PERSONNEL REPORTED ENG SMOKING & ENG FLAMED-OUT. ENG FAILURE CHECKLIST COMPLETE. FLOW CHART COMPLETE. INSP INLET & EXHAUST - NO DAMAGE NOTED. OPENED COWLING & I
- [SDR DHL2006765001](https://openairdocs.org/sdr/DHL2006765001.md): Accessory Unit · warning light · Apr 12, 2006 · N765AT · Boeing 727264 · Landing Gear Position and Warning
  > RT MAIN (RED) GEAR LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHED AFTER GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED RT GEAR RED KORRY LIGHT ASSY. REPLACED LANDING GEAR ACCY UNIT IAW MM 32-09-21. JACKED A/C AND SWUNG GEAR. OPS NORMAL AT THIS TIME.
- [SDR DHL2005765511](https://openairdocs.org/sdr/DHL2005765511.md): Stringer · cracked · Dec 15, 2005 · N765AT · Boeing 727264 · Fuselage Main, Longeron/Stringer
  > FOUND FWD PIT STRINGER CRACKED STA 675 S-29L. CUT OUT CRACKED SECTION OF STRINGER AT STA 675 STR 29L. FABRICATED AND INSTALLED REPAIR STRINGER SECTION 20-5/8" FROM BAC1498-132 AND 5" FROM BAC1498-144 IAW B727 SRM 53-10-3 FIG 1.
- [SDR DHL2005765502](https://openairdocs.org/sdr/DHL2005765502.md): Channel · corroded · Dec 15, 2005 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FLOOR SUPPORT CHANNEL IS CRACKED BEYOND STOP DRILL HOLES (6" FWD OF STA 950F, RBL 4). REMOVED FLOOR SUPPORT IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL 5'8" FROM BAC1500-6199 IAW B727 SRM 51-30-2, 51-10-2.
- [SDR DHL2005765507](https://openairdocs.org/sdr/DHL2005765507.md): Hinge Fitting · corroded · Dec 12, 2005 · N765AT · Boeing 727264 · Elevator Structure
  > FOUND LEFT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1.
- [SDR DHL2005765506](https://openairdocs.org/sdr/DHL2005765506.md): Floor Support · corroded · Dec 12, 2005 · N765AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE PIT CORROSION ON FLOOR SUPPORT CHANNEL, LWR SIDE, BETWEEN STA 1030 AND 1050 RBL 12. REMOVED SECTION OF FLOOR SUPPORT STA 1030 - 1082. FABRICATED AND INSTALLED (3) REPAIR SPLICES 10.50" BY 1" BY 1" FROM BAC1490-2583, 10.50 BY.085" BY.085" FROM A
- [SDR DHL2005765508](https://openairdocs.org/sdr/DHL2005765508.md): Hinge Fitting · corroded · Dec 12, 2005 · N765AT · Boeing 727264 · Elevator Structure
  > RT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1.

Next page: https://openairdocs.org/deregistered/N765AT-2010-08-06/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 = 'N765AT' AND deregistration_id = 'N765AT-2010-08-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N765AT-2010-08-06/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.