# Service difficulty reports: N764AT, cancelled Jul 21, 2010

A list on [N764AT, cancelled Jul 21, 2010](https://openairdocs.org/deregistered/N764AT-2010-07-21.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 · 89 reports

- [SDR DHLA2000800117](https://openairdocs.org/sdr/DHLA2000800117.md): Cable Assy · noisy · Oct 16, 2008 · N764AT · Boeing 727264 · Landing Gear Door Retract Section
  > FLIGHT 935 - DURING CLIMBOUT HEARD LOUD NOISE SEEMING TO COME FROM NOSE GEAR AREA, MINUTES LATER RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ILLUM ON S/O PANEL. FELT VIBRATION. COMPLETED ABNORMAL PROCEDURE & RETURNED TO ILN. REPLACED BOTH NOSE GEAR
- [SDR DHLA200800114](https://openairdocs.org/sdr/DHLA200800114.md): Accessory Unit · failed · Oct 16, 2008 · N764AT · Boeing 727264 · Landing Gear Retraction/Extension System
  > ON CLIMBOUT AT 300KIAS PASSING FL200 RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED. FELT HEAVY VIBRATION PERFORMED ABNORMAL PROCEDURE AFTER SLOWING TO 260KTS LIGHT WENT OUT /VIBRATION REMAINED. MX INSTRUCTED, CYCLE GEAR UPON
- [SDR DHL2008764532](https://openairdocs.org/sdr/DHL2008764532.md): Spar · cracked · May 29, 2008 · N764AT · Boeing 727264 · Wing Spar
  > WHILE AT C CHECK, RT WING REAR SPAR J BEAM CRACKED WBL 126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00911-001.
- [SDR DHL2008764531](https://openairdocs.org/sdr/DHL2008764531.md): Spar · cracked · May 29, 2008 · N764AT · Boeing 727264 · Wing Spar
  > WHILE AT C CHECK, LT WING REAR SPAR J BEAM CRACKED INDICATION WBL126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00910-001 MATERIAL BAC 1506-860 7075T6 DIM 81 INCH BY 5 1/2 INCH PO NR 815922.
- [SDR DHL2008764533](https://openairdocs.org/sdr/DHL2008764533.md): Attach Angle · cracked · May 29, 2008 · N764AT · Boeing 727264 · Trailing Edge Flaps
  > WHILE AT C CHECK, LT O/B MID FLAP I/B LOWER END CAP AND ATTACHMENT ANGLE CRACKED. REPAIRED IAW B727 SRM 51-40-2, 51-20-1, 51-30-5 AND 57-50-2 FIG 6. REPAIR ANGLE MAT.7075 T6.071" PO NR 9006522 DIM 4 INCH BY 4 INCH AND 3 INCH BY 2 INCH.
- [SDR DHL2008764530](https://openairdocs.org/sdr/DHL2008764530.md): Rib · cracked · May 27, 2008 · N764AT · Boeing 727264 · Leading Edge Devices
  > WHILE AT C CHECK, NR 5 K-FLAP ACTUATOR SIDE MOUNTING RIBS I/B AND O/B CRACKED. REPAIRED RIBS IAW BOEING DWG 65-16269 REVC MATERIAL 2024T3.063" DIM 7" BY 6 1/8 INCH PO NR 9006773.
- [SDR DHL2008764529](https://openairdocs.org/sdr/DHL2008764529.md): Skin · bent · May 27, 2008 · N764AT · Boeing 727264 · Passenger/Crew Doors
  > WHILE AT C CHECK, L1 DOOR INNER SKIN BENT FWD LOWER CORNER. REPAIRED IAW B727 SRM 51-40-2 AND ASTAR EVA B52-00073 REV1.
- [SDR DHL2008764528](https://openairdocs.org/sdr/DHL2008764528.md): Keelbeam · cracked · May 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, Keel
  > WHILE AT C-CHECK, CRACK AT BS 874 RIGHT KEEL BEAM LWR CHORD IN APU BAY. REPAIRED IAW S/B 727 53-02-08 MATERIAL 4130 STEEL.071" PO 610176.
- [SDR DHL2008764527](https://openairdocs.org/sdr/DHL2008764527.md): Frame · dented · May 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C-CHECK, DENT AT MAIN FRAME BS 580 BETWEEN STR 16 AND 17R. REPAIRED IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, 7075T6.050 DIM 7.125" X 6.25" PO 9006742.
- [SDR DHL2008764526](https://openairdocs.org/sdr/DHL2008764526.md): Stringer · corroded · May 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, Longeron/Stringer
  > WHILE AT C-CHECK, PILLOWING AT FASTENERS AT RIGHT LWR FUSELAGE AT BS 350, 4 INCHES FWD OF NOSE JACK PAD. REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 2. MATERIAL USED P/N 95-24786-10 GUSSET / CHANNEL, REPAIR FOR 21R BAC 1496-138 DIM 11" PO 815987, CHANNEL SPLICE FR
- [SDR DHL2008764524](https://openairdocs.org/sdr/DHL2008764524.md): Skin · delaminated · May 25, 2008 · N764AT · Boeing 727264 · Aileron Tabs
  > WHILE AT C-CHECK, LT WING O/B AILERON TAB LWR I/B SURFACE DELAM WBL 492. CUT OUT DELAMINATED AREA 1 INCH DIA AND APPLIED POTTING COMPOUND. FABRICATED DOUBLER 3 INCH DIA FROM.010" 2024-T3 PO 9003621. BONDED DOUBLER, CLEANED PRIMED AND SEALED IAW B727 SRM 51-
- [SDR DHL2008764523](https://openairdocs.org/sdr/DHL2008764523.md): Hinge · cracked · May 25, 2008 · N764AT · Boeing 727264 · Cargo/Baggage Doors
  > WHILE AT C-CHECK, EXTERNAL FUSELAGE BS 650 MCD AFT HINGE SEGMENT HAS AFT 2 LOBES WITH SMALL CRACKS. REMOVED AND REPLACED MCD STA 650 AFT HINGE SEGMENT IAW AEI B727 M/M CH 52 PGS 17-20 P/N MS20001-16-7200 PO 9006913.
- [SDR DHL2008764535](https://openairdocs.org/sdr/DHL2008764535.md): Bulkhead · cracked · May 22, 2008 · N764AT · Boeing 727264 · Fuselage Main, Bulkhead
  > CRACK INDICATION AT BS 870 IN RT W/WELL AT APU LOAD CONTROL VALVE CUT-OUT. TRIMMED OUT CRACKED MATERIAL, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR AT BS 870 BULKHEAD PER B727 SRM 53-10-9 FIG 5, 51-10-6, 51-10-1, AND NDTM PT6, 51-00-00 FIG 23.
- [SDR DHL2008764522](https://openairdocs.org/sdr/DHL2008764522.md): Mount Bracket · cracked · May 22, 2008 · N764AT · Boeing 727264 · Leading Edge Slat Actuator
  > NR 1 K-FLAP ACTUATOR TRUNNION MOUNTING BRACKETS CRACK INDICATION WS 305. REMOVED NR 1 K-FLAP MOUNTING BRACKETS WS 305 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3.063", DIM 7.5" X 4" AND PO 9006027 IAW BOEING ENGINEERING DWG 65-16275.
- [SDR DHL2008764521](https://openairdocs.org/sdr/DHL2008764521.md): Frame · dented · May 22, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > DENTS ON MAIN CABIN FRAME BS 640 BETWEEN STR 16 AND 17R. CUT OUT DAMAGED AREA AT FRAME BS 640 BETWEEN STR 16 & 17 RT APPROX 7/8" X 1", FAB DOUBLER REPAIR WITH 7075-T6.050", DIM 7" X 5" AND PO 9006742 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1.
- [SDR DHL2008764520](https://openairdocs.org/sdr/DHL2008764520.md): Bracket · cracked · May 22, 2008 · N764AT · Boeing 727264 · Leading Edge Slat Actuator
  > NR 2 K-FLAP ACTUATOR, TRUNNION MOUNTING BRACKETS CRACK INDICATION (WS 235 APPROX). REMOVED NR 2 K-FLAP TRUNNION MOUNTING BRACKETS FROM ACTUATOR WS 235 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3.063" DIM 9" X 6.5 AND PO 9006773 IAW BOEING ENGINEERIN
- [SDR DHL2008764519](https://openairdocs.org/sdr/DHL2008764519.md): Skin · damaged · May 22, 2008 · N764AT · Boeing 727264 · Wing, Plate/Skin
  > SKIN DAMAGE ON LT WING T/E AT NR 2 SPOILER NR 3 HINGE CUTOUT. ROUTER OUT SKIN AT LT WING T/E NR 2 SPOILER NR 3 HINGE CUTOUT FOUND OUT OF LIMITS IAW B727 SRM 51-10-1 AND 57-20-1 FIG 2. FAB DOUBLER REPAIR WITH 7075-T6. DIMENSION: 4" X 7" AND PO 9006522 IAW B72
- [SDR DHL2008764518](https://openairdocs.org/sdr/DHL2008764518.md): Flap · cracked · May 22, 2008 · N764AT · Boeing 727264 · Trailing Edge Flaps
  > LEFT INBOARD FORE FLAP CRACK INDICATIONS AT L/E FWD OF SEQUENCE CAR ATTACH POINTS (FITTING) WBL 124/203. STOP DRILLED AT THE END OF CRACKS AT LEFT INBOARD FORE FLAP L/E WBL 124/203 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR WITH 2024-T3.050" AND PO 9006457 I/
- [SDR DHL2008764534](https://openairdocs.org/sdr/DHL2008764534.md): Tab · bent · May 21, 2008 · N764AT · Boeing 727264 · Elevator, Tab Structure
  > LT ELEV TAB INBD CORNER DAMAGED, REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED BY BONDING IAW B727 SRM 51-40-20 PGS 12 THROUGH 62 AND SRM 51-80 FIG 2. NO FURTHER ACTION REQUIRED.
- [SDR DHL2008764517](https://openairdocs.org/sdr/DHL2008764517.md): Seat Track · corroded · May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 24. REMOVED SEAT TRACK FROM MAIN CABIN BS 1110-1137 LBL 24 FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3 AND SRM 51-30-2. FAB NEW SEAT TRACK WITH BAC1520-792-7178-T6 DIM, 2'3" AND PO 9003797 IAW B727 SRM 5
- [SDR DHL2008764516](https://openairdocs.org/sdr/DHL2008764516.md): Seat Track · corroded · May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 45. REMOVED CORRODED SEAT TRACK FROM BS1110 TO 1137 LBL 45 FOUND OUT OF LIMITS IAW B727 SRM 51-30-2 ZND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM. 2'3" AND P.O. 6295113 IAW B727 SRM 53-1
- [SDR DHL2008764515](https://openairdocs.org/sdr/DHL2008764515.md): Rib · cracked · May 21, 2008 · N764AT · Boeing 727264 · Leading Edge Devices
  > NR 6 K-FLAP ACTUATOR SUPPORT SIDE I/B AND O/B RIBS CRACKED WS 304. REMOVED INBOARD AND OUTBOARD RIBS AND FAB NEW RIBS WITH 2024-T3-.063 INCH DIM 7 1/2 INCH BY 4 INCH AND PO 9006773 IAW BOEING ENGINEER DWG NR 65-16275.
- [SDR DHL2008764514](https://openairdocs.org/sdr/DHL2008764514.md): Flap · cracked · May 21, 2008 · N764AT · Boeing 727264 · Trailing Edge Flaps
  > L/WING I/B MIDFLAP T/E CHORD CRACKED AT I/B CABLE DRUM, 2 PLACES. REMOVED DAMAGED AREA AT T/E CHORD ABOUT 51 INCHES. FABRICATED NEW SECTION WITH P/N 604754 7075-T6 DIM 51 INCH AND PO 815986 IAW B727 SRM 57-50-2 FIG 5 AND 51-40-1 FIG 1.
- [SDR DHL2008765513](https://openairdocs.org/sdr/DHL2008765513.md): Seat Track · corroded · May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK RBL 45 BS 1110-1135. SEAT TRACK AT RBL 45 BS 950 TO 1183 CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6 DIM 15'7 INCH AND PO 9006864 AND TWO ANGLES FOR SPLICES WITH BAC 1503-1001
- [SDR DHL2008764512](https://openairdocs.org/sdr/DHL2008764512.md): Seat Track · corroded · May 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK RBL 24 BS 1110-1135. SEAT TRACK CORRODED FROM RBL 24 FROM BS 1070 TO 1136 IAW B727 SRM 51-30-2 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM 5'6" AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1.
- [SDR DHL2008764511](https://openairdocs.org/sdr/DHL2008764511.md): Seat Track · corroded · May 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON MAIN CABIN SEAT TRACK BS 480-600 LBL 45. SEAT TRACK CORRODED OUT OF LIMITS STA 480-590 IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6511 DIM 9'2 INCH PO 9006020 IAW B727 SRM 53-10-2 FIG 1 A
- [SDR DHL2008764510](https://openairdocs.org/sdr/DHL2008764510.md): Shear Web · dented · May 20, 2008 · N764AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > DENT AND PUNCTURE HOLE ON MAIN CABIN SHEAR WEB BS 1140 RBL 24. CUT OUT DAMAGED AREA AT SHEAR WEB RBL 24 BS 1140 (2 EACH) 3/4 INCH BY 3/4 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 51-40-2 FIG 1. FAB DOUBLER REPAIR WITH 7075-T6.071 INCH SIZE: 9 INCH BY 7 INCH A
- [SDR DHL2008764509](https://openairdocs.org/sdr/DHL2008764509.md): Floorbeam · corroded · May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, Floor Beam
  > CORROSION ON BS 1110 FLOORBEAM LBL 24 - LBL 45. CORROSION ON FLOORBEAM LBL 24-LBL 45 BS 111O FOUND OUT OF LIMITS AT LBL 33 IAW B727 SRM 51-10-6 AND 53-10-1 FIG 5. CUT OUT DAMAGED AREA, FAB ONE FILLER WITH 7075-T6.125 INCH DIM 2 INCH BY 1 INCH PO 7371263. T
- [SDR DHL2008764507](https://openairdocs.org/sdr/DHL2008764507.md): Frame · gouged · May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 097896, 4 EACH TOOLING MARKS/GOUGES ON MAIN CABIN FRAME BS 700 BETWEEN S7-8L. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-O PO NR 9006027 HEAT TREATED FROM 7075-O TO 7075-T6 IAW FAS ENGINEERING REPORT NR 2-3715
- [SDR DHL2008764506](https://openairdocs.org/sdr/DHL2008764506.md): Frame · dented · May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 098177, DENT ON MAIN CABIN FRAME BS 600 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6.050 INCH DIMENSION 7 INCH BY 5 1/4 INCH PO NR 9006153.
- [SDR DHL2008764505](https://openairdocs.org/sdr/DHL2008764505.md): Frame · dented · May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 098175, DENT ON MAIN CABIN FRAME BS 540 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6.050 INCH DIM 7 1/8 INCH BY 6 INCH PO NR 9006742.
- [SDR DHL2008764508](https://openairdocs.org/sdr/DHL2008764508.md): Seat Track · corroded · May 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON MAIN CABIN SEAT TRACK BS 480-620 RBL 45. SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178T6 DIM 12'6 3/8 INCH AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1 AND VENTURA AEROSPACE
- [SDR DHL2008764504](https://openairdocs.org/sdr/DHL2008764504.md): Frame · dented · May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 098180, DENT AT MAIN CABIN FRAME BS 680 BETWEEN STR 16 AND 17R. FABRICATED REPAIR IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL 7075-T6.050 INCH DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.
- [SDR DHL2008764503](https://openairdocs.org/sdr/DHL2008764503.md): Frame · dented · May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R098179, DENT AT MAIN CABIN FRAME BS 660 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 DOUBLER MATERIAL 7075-T6.050 DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742.
- [SDR DHL2008764502](https://openairdocs.org/sdr/DHL2008764502.md): Frame · dented · May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 098174, DENT AT MAIN CABIN FRAME AT BS 520 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MAT, 7075-T6.050" DIM 5 1/8 INCH BY 8 1/4 INCH PO NR 9006742.
- [SDR DHL2008764501](https://openairdocs.org/sdr/DHL2008764501.md): Frame · dented · May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, Frame
  > WHILE AT C CHECK REF N/R 098173, DENT AT RT MAIN CABIN FRAME BS 480 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL DOUBLER 7075-T6.050 INCH DIM 7 1/4 INCH BY 5 3/4 INCH PO NR 9006742.
- [SDR DHL2008764500](https://openairdocs.org/sdr/DHL2008764500.md): Skin · cracked · May 19, 2008 · N764AT · Boeing 727264 · Trailing Edge Flaps
  > WHILE AT C CHECK REF N/R 097599, RT I/B AFT FLAP LOWER SKIN WBL 203 CRACKED AT MOUNTING FITTING. REPAIRED IAW B727 SRM 57-50-4 FIG 11, SPLICE 2024T3.050 DIM 5.5 INCH BY 11 INCH PO NR 9006742. FABBED FILLER 2024T3.040 DIM 9 INCH BY 14 INCH PO NR 9006587.
- [SDR DHL2006764003](https://openairdocs.org/sdr/DHL2006764003.md): Light · inoperative · Dec 18, 2006 · N764AT · Boeing 727264 · Emergency Lighting
  > SECURITY CHECK COCKPIT EMERG EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERG EXIT LIGHT ASSY IAW B727 M/M 33-50-101. OPS CHECK GOOD.
- [SDR DHL2006764007](https://openairdocs.org/sdr/DHL2006764007.md): Skin · damaged · Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/Skin
  > REF. ASTAR LOG PAGE 098862 ITEM 1P. BELT LOADER STRUCK A/C AFT OF FWD BELLY LEFT 17 INCH GASH. C/W ASTAR JC EA53100140-001-B REPAIR SKIN (FS680-690). ACCOMPLISHED ASTAR JC EA53100140-001-B WO 600017273 REPAIR SKIN (FS680-690) EXT. B727 AND DWG NR 53100140-001
- [SDR DHL2006764004](https://openairdocs.org/sdr/DHL2006764004.md): Skin · damaged · Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/Skin
  > CREASE IN SKIN STA 660 STR 26R-27R IAW ITEM 1P LP 098862. CUTOUT DAMAGE AREA DIM. 3 INCH X 1 INCH, FAB. DOUBLER MAT. USED 2024T3.063 PO NR 9003898 DIM. 11.3750 INCH X 9.7500 INCH. FAB TRIPLER MAT USED 2024T3.071 PO NR 9003866 DIM. 12.1250 INCH X 10 INCH.
- [SDR DHL2006764006](https://openairdocs.org/sdr/DHL2006764006.md): Web · damaged · Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > WEB DAMAGED BELOW STR 27R BETWEEN STA 680-700 REF. ITEM 1P LP 098862. REMOVED DAMAGED WEB, FABRICATED PO NR 900245 DIM. 18.1250 INCH X 7.1250 INCH, INSTALLED, PRIMED AND TREATED IAW SRM 51-30-2 & 51-10-2 AT STA 680-700 BELOW STR 27R.
- [SDR DHL2006764005](https://openairdocs.org/sdr/DHL2006764005.md): Skin · damaged · Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/Skin
  > STRINGERS 28R AND 27R DAMAGED BETWEEN STA 680-700. REF. ITEM 1P LP 098862. CUTOUT DAMAGED SECTIONS STR 27R 26.5 INCH AND STR 28R 7.5 INCH. FAB. NEW FROM BAC1498-144. SPLICE FROM BAC1498-132 STR 27R 12INCH AND STR 28R 22.5 INCH PO INCH 623185 AND PO INCH 423185
- [SDR DHL2006764002](https://openairdocs.org/sdr/DHL2006764002.md): Battery · discharged · Jun 29, 2006 · N764AT · Boeing 727264 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUM. DURING SBY PWR CHECK. R&R EMERGENCY EXIT LIGHT BATTERIES 2 EACH P/N38931-002. INSTALLED, OPS CHECK SERVICEABLE PER B-727 M/M 33-50-00.
- [SDR DHL2006764001](https://openairdocs.org/sdr/DHL2006764001.md): Light · loose · May 16, 2006 · N764AT · Boeing 727264 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT LOOSE AND REMAINS ILLUMINATED IN FLIGHT. RESECURED COCKPIT EMERGENCY EXIT LIGHT PACK. OPS CHECK GOOD IAW MM 33-50-71.
- [SDR DHL2006764517](https://openairdocs.org/sdr/DHL2006764517.md): Tab · dented · Apr 16, 2006 · N764AT · Boeing 727264 · Aileron Tabs
  > DENT ON R/WING OB AILERON TAB UPPER SURFACE. CUT OUT DENTED AREA ON RT OB AILERON TAB APPROX 1 INCH DIA FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3.7500 INCHES X 4 INCHES FROM 2024-T3.010 PO NR 9912184CLEANED, PREPPED PRIMED, BONDED CLEANED TREAT
- [SDR DHL2006764516](https://openairdocs.org/sdr/DHL2006764516.md): Skin · dented · Apr 16, 2006 · N764AT · Boeing 727264 · Ailerons
  > NR 016062 LT WING IB AILERON UPPER SKIN HAS NUMEROUS DENTS. REMOVED AND REINSTALLED LH IB AILERON AND TAB IAW MM 27-10-01 AND MM 27-10-11. FABRICATED NEW SKIN USING MAT 2024T3.040 PO NR 9003189 DIM 41.2500 X 22.2500 INCH IAW SRM 57-50-2 FIG7 AND SRM 51-30-5
- [SDR DHL2006764519](https://openairdocs.org/sdr/DHL2006764519.md): Stiffener · cracked · Apr 15, 2006 · N764AT · Boeing 727264 · Wing Spar
  > LT WING FRONT SPAR VERTICAL STIFFENER AT WS 90 SHOWS CRACK FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 HFEC AT ANGLE MARKED END OF CRACK NDT MAN PART6 51-00-00 FIG23 STOP DRILLED.250 END OF CRACK IAW SRM51-10-1 FAB REPAIR MAT USED 7075 T6.
- [SDR DHL2006764506](https://openairdocs.org/sdr/DHL2006764506.md): Attach Fitting · cracked · Apr 6, 2006 · N764AT · Boeing 727264 · Wing, Attach Fittings
  > L/WING INSIDE NR 4 SLAT LE ACTUATOR ATTACH POINT FOUND CRACK ON INNER SKIN AT WS 410. CUTOUT AREA AT L/WING INSIDE NR 4 SLAT LE ON INNER SKIN AT WS 410 DIM 10.5"X 5.250" IAW B727 SRM 57-30-4 FIG 3. FABRICATED FILLER MAT USED 2024T3.040 PO# 9002787 AND DIM.
- [SDR DHL2006764515](https://openairdocs.org/sdr/DHL2006764515.md): Rib · cracked · Apr 5, 2006 · N764AT · Boeing 727264 · Wing, Rib/Bulkhead
  > REF ASTAR N/R 015815 DISCREPANCY: NR 6 SLAT OB ACT ROD END MOUNT RIB CRACKED REMOVED AND REPLACED RIB NR 6 SLAT OB ACT ROD END MOUNT PO NR 619549 P/N 65-17294-14 IAW B727 SRM 51-30-2.
- [SDR DHL2006764512](https://openairdocs.org/sdr/DHL2006764512.md): Attach Bracket · cracked · Apr 5, 2006 · N764AT · Boeing 727264 · Leading Edge Devices
  > LT WING INSIDE NR 4 SLAT LE ACTUATOR ATTACHED POINT IB AND OB RIB CRACKED. REMOVED RIBS AT LT WING NR 4 SLAT IB AND OB ACTUATOR ATTACHED POINT AND 1 CHANNEL IAW B727 SRM 51-30-5. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2. INSTALED RIBS P/N 65-1

Next page: https://openairdocs.org/deregistered/N764AT-2010-07-21/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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N764AT-2010-07-21/reports

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