N764AT, cancelled Jul 21, 2010

Service difficulty reports · 89

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 = 'N764AT' AND deregistration_id = 'N764AT-2010-07-21'
  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 DHLA2000800117Cable Assy · noisyFLIGHT 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 Oct 16, 2008 · N764AT · Boeing 727264 · Landing Gear Door Retract SectionSDR DHLA200800114Accessory Unit · failedON 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 Oct 16, 2008 · N764AT · Boeing 727264 · Landing Gear Retraction/Extension SystemSDR DHL2008764532Spar · crackedWHILE 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.May 29, 2008 · N764AT · Boeing 727264 · Wing SparSDR DHL2008764531Spar · crackedWHILE 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.May 29, 2008 · N764AT · Boeing 727264 · Wing SparSDR DHL2008764533Attach Angle · crackedWHILE 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.May 29, 2008 · N764AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2008764530Rib · crackedWHILE 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.May 27, 2008 · N764AT · Boeing 727264 · Leading Edge DevicesSDR DHL2008764529Skin · bentWHILE AT C CHECK, L1 DOOR INNER SKIN BENT FWD LOWER CORNER. REPAIRED IAW B727 SRM 51-40-2 AND ASTAR EVA B52-00073 REV1.May 27, 2008 · N764AT · Boeing 727264 · Passenger/Crew DoorsSDR DHL2008764528Keelbeam · crackedWHILE 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.May 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, KeelSDR DHL2008764527Frame · dentedWHILE 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.May 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764526Stringer · corrodedWHILE 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 FRMay 27, 2008 · N764AT · Boeing 727264 · Fuselage Main, Longeron/StringerSDR DHL2008764524Skin · delaminatedWHILE 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-May 25, 2008 · N764AT · Boeing 727264 · Aileron TabsSDR DHL2008764523Hinge · crackedWHILE 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.May 25, 2008 · N764AT · Boeing 727264 · Cargo/Baggage DoorsSDR DHL2008764535Bulkhead · crackedCRACK 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.May 22, 2008 · N764AT · Boeing 727264 · Fuselage Main, BulkheadSDR DHL2008764522Mount Bracket · crackedNR 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.May 22, 2008 · N764AT · Boeing 727264 · Leading Edge Slat ActuatorSDR DHL2008764521Frame · dentedDENTS 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.May 22, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764520Bracket · crackedNR 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 ENGINEERINMay 22, 2008 · N764AT · Boeing 727264 · Leading Edge Slat ActuatorSDR DHL2008764519Skin · damagedSKIN 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 B72May 22, 2008 · N764AT · Boeing 727264 · Wing, Plate/SkinSDR DHL2008764518Flap · crackedLEFT 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/May 22, 2008 · N764AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2008764534Tab · bentLT 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.May 21, 2008 · N764AT · Boeing 727264 · Elevator, Tab StructureSDR DHL2008764517Seat Track · corrodedCORROSION 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 5May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764516Seat Track · corrodedCORROSION 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 53-1May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764515Rib · crackedNR 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.May 21, 2008 · N764AT · Boeing 727264 · Leading Edge DevicesSDR DHL2008764514Flap · crackedL/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.May 21, 2008 · N764AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2008765513Seat Track · corrodedCORRODED 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 1503-1001May 21, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764512Seat Track · corrodedCORRODED 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.May 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764511Seat Track · corrodedCORROSION 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 AMay 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764510Shear Web · dentedDENT 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 AMay 20, 2008 · N764AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2008764509Floorbeam · corrodedCORROSION 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. TMay 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, Floor BeamSDR DHL2008764507Frame · gougedWHILE 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 2-3715May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764506Frame · dentedWHILE 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.May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764505Frame · dentedWHILE 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.May 20, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764508Seat Track · corrodedCORROSION 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 May 20, 2008 · N764AT · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008764504Frame · dentedWHILE 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.May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764503Frame · dentedWHILE 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.May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764502Frame · dentedWHILE 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.May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764501Frame · dentedWHILE 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.May 19, 2008 · N764AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008764500Skin · crackedWHILE 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.May 19, 2008 · N764AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2006764003Light · inoperativeSECURITY CHECK COCKPIT EMERG EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERG EXIT LIGHT ASSY IAW B727 M/M 33-50-101. OPS CHECK GOOD.Dec 18, 2006 · N764AT · Boeing 727264 · Emergency LightingSDR DHL2006764007Skin · damagedREF. 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 53100140-001Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006764004Skin · damagedCREASE 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. Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006764006Web · damagedWEB 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.Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2006764005Skin · damagedSTRINGERS 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 423185Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006764002Battery · dischargedCOCKPIT 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.Jun 29, 2006 · N764AT · Boeing 727264 · Emergency LightingSDR DHL2006764001Light · looseEMERGENCY EXIT LIGHT IN COCKPIT LOOSE AND REMAINS ILLUMINATED IN FLIGHT. RESECURED COCKPIT EMERGENCY EXIT LIGHT PACK. OPS CHECK GOOD IAW MM 33-50-71.May 16, 2006 · N764AT · Boeing 727264 · Emergency LightingSDR DHL2006764517Tab · dentedDENT 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 TREATApr 16, 2006 · N764AT · Boeing 727264 · Aileron TabsSDR DHL2006764516Skin · dentedNR 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 51-30-5Apr 16, 2006 · N764AT · Boeing 727264 · AileronsSDR DHL2006764519Stiffener · crackedLT 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 .Apr 15, 2006 · N764AT · Boeing 727264 · Wing SparSDR DHL2006764506Attach Fitting · crackedL/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. Apr 6, 2006 · N764AT · Boeing 727264 · Wing, Attach FittingsSDR DHL2006764515Rib · crackedREF 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.Apr 5, 2006 · N764AT · Boeing 727264 · Wing, Rib/BulkheadSDR DHL2006764512Attach Bracket · crackedLT 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 65-1Apr 5, 2006 · N764AT · Boeing 727264 · Leading Edge Devices
Back to N764AT, cancelled Jul 21, 2010