# Service difficulty reports: N763AT, cancelled Jul 9, 2010

A list on [N763AT, cancelled Jul 9, 2010](https://openairdocs.org/deregistered/N763AT-2010-07-09.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 · 77 reports

- [SDR DHLA200800118](https://openairdocs.org/sdr/DHLA200800118.md): Circuit Breaker · tripped · Oct 29, 2008 · N763AT · Boeing 727264 · Light System Wiring
  > DURING THE CLIMB-OUT OF KILN, EMERGENCY EXIT CONTROL RT C/B POPPED. COCKPIT EMERGENCY EXIT LIGHTS OPERATE NORMAL.
- [SDR DHL2008763530](https://openairdocs.org/sdr/DHL2008763530.md): Floorbeam · corroded · Mar 24, 2008 · N763AT · Boeing 727264 · Fuselage Main, Floor Beam
  > EXFOLIATION FOUND ON FLT DECK FLOORBEAM UPPER CAP AT BS 266, BL 0. REMOVED AND REPLACED UPPER CHORD SECTION WITH P/N 65-17588-2, PO NR 8109233, PER B727 SRM 51-30-5, 51-30-2, AND BAC DWG 65-17588 REV D.
- [SDR DHL2008763529](https://openairdocs.org/sdr/DHL2008763529.md): Rib · cracked · Mar 19, 2008 · N763AT · Boeing 727264 · Leading Edge Devices
  > NR 5 L/E SLAT INB TRACK INTERIOR, O/B RIB IS CRACKED. REMOVED AND REPLACED RIB ASSY (I/B AND O/B) WITH P/N 65-17281-13, PO3 8109195, PER B727 SRM 51-30-2.
- [SDR DHL2008763523](https://openairdocs.org/sdr/DHL2008763523.md): Frame · dented · Mar 16, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME DAMAGED IN CARGO COMPT AT BS 347, ALONG STR 4L. CUT OUT DAMAGE, INSTALLED FRAME REPAIR PARTS, P/N AE727-2-360-11 AND AE727-2-360-12, PO NR 810972, PER B727 SRM 51-30-5, 51-30-2, AND AEI DWG AE727-2-360 REV G.
- [SDR DHL2008763511](https://openairdocs.org/sdr/DHL2008763511.md): Hinge · cracked · Mar 16, 2008 · N763AT · Boeing 727264 · Fuselage, Door Hinge
  > MCD AFT HINGE SEGMENT AFT LOBE CRACKED. REMOVED AND REPLACED HINGE SEGMENT WITH MS 20001-16-7200 MATERIAL PO NR 9002527 PER AEI B727-200 FREIGHTER MM CH 52 FIG 5201A AND SRM 51-30-5.
- [SDR DHL2008763509](https://openairdocs.org/sdr/DHL2008763509.md): Skin · chafed · Mar 16, 2008 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > RT I/B FORE FLAP I/B L/E CHAFED AT RWBL 73. DAMAGE BEYOND SERVICE LIMITS. REMOVED, FABRICATED, AND INSTALLED SKIN PANEL, 2024-T3.050 INCH BY 14 INCH BY 14.5 INCH, PONR 9006586, PER B727 SRM 57-50-2 FIG 3, 51-20-1, AND 51-30-2.
- [SDR DHL2008763528](https://openairdocs.org/sdr/DHL2008763528.md): Support Fitting · cracked · Mar 14, 2008 · N763AT · Boeing 727264 · Leading Edge Slat Actuator
  > NR 6 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5. REMOVED ACTUATOR SUPPORT MOUNT ASSY. FABRICATED SUPPORT WEBS FROM 2024-T3,.063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6,.125" BY 5" BY 2", (2 EA), PO NR 9005685, ASSEM
- [SDR DHL2008763527](https://openairdocs.org/sdr/DHL2008763527.md): Support Fitting · cracked · Mar 14, 2008 · N763AT · Boeing 727264 · Leading Edge Slat Actuator
  > NR 1 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5 AND 315.3. REMOVED ACTUATOR SUPPORT MOUNT ASSY, FABRICATED SUPPORT WEBS FROM 2024-T3,.063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6,.125" BY 5" BY 2", (2 EA), PO NR 90056
- [SDR DHL2008763518](https://openairdocs.org/sdr/DHL2008763518.md): Seat Track · corroded · Mar 14, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK CORRODED AT BS 480-600, RBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 209" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1.
- [SDR DHL2008763515](https://openairdocs.org/sdr/DHL2008763515.md): Seat Track · corroded · Mar 14, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED BS 520 TO 540, LBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH P/N 65-23637-53, PO NR 658565, 220 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.
- [SDR DHL2008763526](https://openairdocs.org/sdr/DHL2008763526.md): Seat Track · corroded · Mar 13, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED AT BS 990 TO 1130, LBL 45.75. REMOVED, FABRICATED SEAT TRACK SECTION FROM BAC1520-792, 297.875" LONG, PO NR 9006020, AND INSTALLED PER B727 SRM 53-10-5 FIG 1, 53-10-1 FIG 7, AND 51-30-2.
- [SDR DHL2008763508](https://openairdocs.org/sdr/DHL2008763508.md): Rib · cracked · Mar 13, 2008 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > PREVIOUS REPAIR ON L/WING O/B FORE FLAP UPPER SURFACE CHAFED, LWBL 400. REMOVED EXISTING REPAIR AND ASSOCIATED INTERNAL RIB. FABRICATED AND INSTALLED NEW REPAIR SKIN SECTION, 2024-T3.050 INCH BY 14.125 INCH BY 5.875 INCH, PO NR 9005554; AND SPLICE, 2024-T3
- [SDR DHL2008763517](https://openairdocs.org/sdr/DHL2008763517.md): Seat Track · corroded · Mar 12, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 1110-1130, LBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 297" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1 AT BS 958.5" TO BS 1139.
- [SDR DHL2008763510](https://openairdocs.org/sdr/DHL2008763510.md): Attach Angle · cracked · Mar 12, 2008 · N763AT · Boeing 727264 · Wing, Attach Fittings
  > R/WING L/E INTERIOR, CRACKED RIB ATTACH ANGLE AT RWS 125 (FRONT SPAR). FABRICATED AND INSTALLED REPAIR DOUBLER, 7075-T6.050 INCH BY 10.5 INCH BY 2.5 INCH, PO NR 9006153, AND FILLER, 7075-T6.040 INCH BY 3 INCH BY 2.5 INCH, PO NR 9006639, PER B727 SRM 51-40-3
- [SDR DHL2008763512](https://openairdocs.org/sdr/DHL2008763512.md): Support Angle · cracked · Mar 9, 2008 · N763AT · Boeing 727264 · Landing Gear Doors
  > RMLG BODY DOOR ACTUATOR HANGER SUPPORT ANGLE CRACKED AT BS 870. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE, 7075-T6.100 INCH BY 3.75 INCH BY 3.375 INCH, PO NR 9005773, PER B727 SRM 53-10-2 51-20-1 AND 51-30-5.
- [SDR DHL2008763516](https://openairdocs.org/sdr/DHL2008763516.md): Seat Track · corroded · Mar 8, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 560-600, LBL 25. REMOVED, FABRICATED FROM BAC1520-792, PO NR 9006020, 209" LONG, AND REPLACED SEAT TRACK SECTION PER B727 SRM 53-10-1 FIG 7 AND 53-10-5 FIG 1.
- [SDR DHL2008763514](https://openairdocs.org/sdr/DHL2008763514.md): Seat Track · corroded · Mar 8, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS 760 TO 850, RBL 25. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.
- [SDR DHL2008763513](https://openairdocs.org/sdr/DHL2008763513.md): Seat Track · corroded · Mar 7, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS 760 TO 850, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCHES LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2.
- [SDR DHL2008763525](https://openairdocs.org/sdr/DHL2008763525.md): Stringer Splice · corroded · Mar 4, 2008 · N763AT · Boeing 727264 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMP AT BS 1010, STR 29R SPLICE CORRODED O/B SIDE. REMOVED, FABRICATED NEW SPLICE FROM BAC1498-131, 15" LONG, PO NR 9005686, AND INSTALLED PER B727 SRM 53-10-2 FIG 9, 53-10-3 FIG 1, AND 51-30-2.
- [SDR DHL2008763522](https://openairdocs.org/sdr/DHL2008763522.md): Frame · dented · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 660, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.
- [SDR DHL2008763521](https://openairdocs.org/sdr/DHL2008763521.md): Frame · dented · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 640, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.
- [SDR DHL2008763520](https://openairdocs.org/sdr/DHL2008763520.md): Frame · gouged · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED IN CARGO COMPT AT BS 600, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.
- [SDR DHL2008763502](https://openairdocs.org/sdr/DHL2008763502.md): Seat Track · corroded · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC 1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.
- [SDR DHL2008763501](https://openairdocs.org/sdr/DHL2008763501.md): Seat Track · corroded · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 24. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.
- [SDR DHL2008763500](https://openairdocs.org/sdr/DHL2008763500.md): Seat Track · corroded · Mar 2, 2008 · N763AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 850-870, RBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2.
- [SDR DHL2008763524](https://openairdocs.org/sdr/DHL2008763524.md): Shear Tie · corroded · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Internal Mounting Structure
  > FRAME SHEAR TIE CORRODED AT BS 1130, BETWEEN STR 28R AND 29R, AFT SIDE. REMOVED, FABRICATED SHEAR TIE FROM 7075-T6,.050" BY 6" BY 2.5", PO NR 9006153, AND INSTALLED NEW SHEAR TIE PER B727 SRM 53-10-4 FIG 4, 53-10-2, AND 51-30-2.
- [SDR DHL2008763519](https://openairdocs.org/sdr/DHL2008763519.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME DENTED IN CARGO COMPT AT BS 580, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2.
- [SDR DHL2008763507](https://openairdocs.org/sdr/DHL2008763507.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED AND DENTED AT BS 560, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6,.063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2008763506](https://openairdocs.org/sdr/DHL2008763506.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED AND DENTED AT BS 540, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6,.063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2008763505](https://openairdocs.org/sdr/DHL2008763505.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED AND DENTED AT BS 520, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6,.063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2008763504](https://openairdocs.org/sdr/DHL2008763504.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED AND DENTED AT BS 500 ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6,.063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2008763503](https://openairdocs.org/sdr/DHL2008763503.md): Frame · dented · Mar 1, 2008 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > FRAME GOUGED AND DENTED AT BS 480, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6,.063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2007763002](https://openairdocs.org/sdr/DHL2007763002.md): Panel · delaminated · Dec 18, 2007 · N763AT · Boeing 727264 · Wing, Plate/Skin
  > 7 BY 5 INCH AREA OF DELAMINATION ON PANEL JUST O/B OF NR 1 SPOILER. DELAMINATION LOCATED JUST ABOVE JACKSCREW GEAR BOX, PANEL NR 8155.
- [SDR DHL2007763001](https://openairdocs.org/sdr/DHL2007763001.md): Web · cracked · Nov 10, 2007 · N763AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > A-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075-T6.025 X 2 INCH X 4 INCH IAW SRM 51-40-2 AND 53-10-2, PN 9003505 ALODINED AND PRIMED IAW SRM
- [SDR DHL2006763006](https://openairdocs.org/sdr/DHL2006763006.md): Relay · failed · Nov 26, 2006 · N763AT · Boeing 727264 · Emergency Lighting
  > EMERG LTS COME ON IN ARMED POS. REPLACED R-70 RELAY AND CHECK SERV PER B-727 M/M 33-50-101 P/N 9524-6508.
- [SDR DHL2006763005](https://openairdocs.org/sdr/DHL2006763005.md): Battery · discharged · Nov 26, 2006 · N763AT · Boeing 727264 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERIES P/N 37067-001 2 EA IAW B727 M/M 33-50-101. OPS CHECK SERVICEABLE.
- [SDR DHL2006763004](https://openairdocs.org/sdr/DHL2006763004.md): Coalescer Bag · dirty · Oct 31, 2006 · N763AT · Boeing 727264 · Humidity Control System
  > VERY STRONG ODOR, LIKE BURNING OIL COMING FROM PACKS DURING T/O AND CLIMB, GOES AWAY AFTER APPROX 20 MIN. REMOVED AND CLEANED BOTH WATER SEPARATOR COALESCER SOCKS. OPS CHECK GOOD. NO ODOR NOTED IAW AMM 21-55-51.
- [SDR DHL2006763003](https://openairdocs.org/sdr/DHL2006763003.md): Connector · damaged · Sep 7, 2006 · N763AT · Boeing 727264 · Landing Gear System Wiring
  > ON DEPARTURE LANDING GEAR WOULD NOT GO PAST OFF ABNORMAL PROCEDURES WAS PERFORMED HORN SOUNDED AT FLAPS 2 FLAPS WERE SELECTED BACK TO 5 AND GEAR HANDLE SELECTED DOWN AT CONNECTOR 1890B INTERMITTENT REPLACED PIN 35 AND 36 IAW SWPM 20-60-02 AND GEAR MODULE S
- [SDR DHL2006763002](https://openairdocs.org/sdr/DHL2006763002.md): Accessory Unit · failed · Sep 7, 2006 · N763AT · Boeing 727264 · Landing Gear Retraction/Extension System
  > ON DEP F/O WENT TO RAISE GEAR, GEAR HANDLE WOULD NOT GO PAST OFF. F/O PULLED LEVER LATCH TO RAISE GEAR. ON FLAP RETRACTION WARNING HORN SOUNDED ON FLAPS UP, COMPLIED WITH ABNORMAL PROCEDURES. REMOVED & REPLACED LANDING GEAR ACCESSORY BOX IAW B727 MM 32-09-1
- [SDR DHL2006763001](https://openairdocs.org/sdr/DHL2006763001.md): Accessory Unit · malfunctioned · Jun 6, 2006 · N763AT · Boeing 727264 · Landing Gear Position and Warning
  > RAISED GEAR, L GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED AB PROC, L & R GEAR UNSAFE LIGHT & DOOR LIGHT ILLUMINATED. RII REQUIRED. REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECK GOOD IAW 727 MM 32-09-121.
- [SDR DHL2006763505](https://openairdocs.org/sdr/DHL2006763505.md): Angle · gouged · Jan 25, 2006 · N763AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > FWD CARGO S-27R AT BS 560 HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION BS 568 - 547.2 S-27R. FABRICATED AND INSTALLED REPAIRS 3.150" X.090" X.800" FROM 7075-T6.090, 20.800" X 3.00" X 1.250" FROM BAC1498-131 AND 1.650" X.825" X 1.40" FROM 7075-T6.
- [SDR DHL2006763503](https://openairdocs.org/sdr/DHL2006763503.md): Cap · corroded · Jan 25, 2006 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > S/O 284007 N/R 031817 - FWD CARGO AFT DOOR OPENING FRAME CAP BS 620 S-26R HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION OF FRAME CAP. FABRICATED AND INSTLLED FRAME CAP REPAIRS 14" X 1" AND 22" X 1" FROM 60-9101 7075-T6 IAW B727 SRM 51-40-4 FIG. 1 AND 5
- [SDR DHL2006763517](https://openairdocs.org/sdr/DHL2006763517.md): Skin · punctured · Jan 23, 2006 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > S/O 284007 N/R 032223 - RT INBD FORE FLAP PUNCTURED APPROX 4 FEET FROM INBD END. CUT OUT PUNCTURED AREA 1" X 3". FABRICATED AND INSTALLED REPAIR DOUBLER 3 X 6" FROM 2024-T3.016" IAW SRM 51-40-20 FIG 8.
- [SDR DHL2006763510](https://openairdocs.org/sdr/DHL2006763510.md): Intercostal · corroded · Jan 22, 2006 · N763AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > S/O 284007 N/R 032047 - CORRODED SHEAR CLIP INTERCOSTAL, 6 INCHES FWD OF BS 990 OUTBD OF S-28R (BS 984). CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED INTERCOSTAL 7-1/4" X 4-3/8" X 5-5/8" X 2" FROM 7075-T6.050 IAW B727 SRM 53-10-4 FIG 11.
- [SDR DHL2006763515](https://openairdocs.org/sdr/DHL2006763515.md): Skin · chafed · Jan 21, 2006 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > S/O 284007 N/R 032201 - RT INBD T/E FORE FLAP L/E SKIN CHAFED BEYOND LIMITS AT WBL 72 AND 166, 1.5" AND 96" INBD END. REMOVED 2 EA L/E PANELS THAT WERE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PANELS 7" X 7-5/8" AND 15" X 15" FROM 2024-T3.040 IAW B727 BOE
- [SDR DHL2006763516](https://openairdocs.org/sdr/DHL2006763516.md): Skin · cracked · Jan 21, 2006 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > S/O 284007 N/R 032203 - RT INBD T/E FORE FLAP L/E SKIN CRACKED ON LOWER SURFACE 53.5" FROM INBD END WBL 124. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER 8" X 6.375 FROM 2024-T3.063" IAW SRM 57-50-4 FIG 1.
- [SDR DHL2006763501](https://openairdocs.org/sdr/DHL2006763501.md): Fitting · broken · Jan 21, 2006 · N763AT · Boeing 727264 · Ailerons
  > S/O 284007 N/R 031639 - LT OUTBD AILERON TAB HAS EXCESSIVE PLAY. OPEN LT OUTBD AILERON SKIN, FOUND INTERNAL TAB MOUNT FITTING BROKEN. REMOVED AND REPLACED FITTING, BALANCED IAW B727 SRM 51-80-4 AND 51-30-2.
- [SDR DHL2006763514](https://openairdocs.org/sdr/DHL2006763514.md): Skin · chafed · Jan 20, 2006 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > S/O 284007 N/R 032199 - LTOUTBD T/E FORE FLAP L/E SURFACE CHAFED BETWEEN IND AND CENTER HINGES WBL 367. TRIMMED OUT CHAFED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 6" X 4" FROM 2024-T3.063" IAW B727 SRM 57-50-4 FIG 1.
- [SDR DHL2006763518](https://openairdocs.org/sdr/DHL2006763518.md): Frame · cracked · Jan 19, 2006 · N763AT · Boeing 727264 · Fuselage Main, Frame
  > S/O 284007 N/R 032154 - CRACK ABOUT 10 INCHES LONG ON FRAME WEB AT BS 1352 RT LOWER SIDE FROM 4 O'CLOCK POSITION TO 5 O'CLOCK AFT SIDE OF WEB. CUT OUT CRACKED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR DOUBLER 27-7/8" X 3-3/8" AND FILLER FROM 7075-T6.071
- [SDR DHL2006763513](https://openairdocs.org/sdr/DHL2006763513.md): Nut Plate · missing · Jan 19, 2006 · N763AT · Boeing 727264 · Trailing Edge Flaps
  > S/O 284007 N/R 032195 - LT OUTBD FLAP OUTBD ATTACH FITTING ATTACH POINT HAS MISSING NUTPLATE. REMOVED EXISTING REPAIR DOUBLER, CUT OUT SKIN FOR ACCESS, REMOVED AND REPLACED NUTPLATE. FABRICATED AND INSTALLED REPAIR DOUBLER 10.25" X 4" FROM 2024-T3.063" IAW I

Next page: https://openairdocs.org/deregistered/N763AT-2010-07-09/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 = 'N763AT' AND deregistration_id = 'N763AT-2010-07-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N763AT-2010-07-09/reports

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