Boeing 727-264

Service difficulty reports · 617

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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 aircraft_model_key = '727264'
  ORDER BY difficulty_date DESC"

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SDR K11A2012102529002Seat Track · corrodedMAIN DECK STA 380 TO STA 460 RBL 46 SEAT TRACK HAS CORROSION (NR 49057).Sep 14, 2012 · N729 · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2012100829001Seat Track · corrodedCORROSION ON SEAT TRACK AROUND NUT PLATE, 1X1 INCH (NR 49051).Sep 9, 2012 · N729CK · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR DHLA200900034Battery Pack · malfunctionedDEFECT 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.Jun 7, 2009 · N765AT · Boeing 727264 · Emergency LightingSDR DHLA200800118Circuit Breaker · trippedDURING THE CLIMB-OUT OF KILN, EMERGENCY EXIT CONTROL RT C/B POPPED. COCKPIT EMERGENCY EXIT LIGHTS OPERATE NORMAL.Oct 29, 2008 · N763AT · Boeing 727264 · Light System WiringSDR 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 DHLA20087651016Casting · crackedUPON 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 Oct 16, 2008 · N765AT · Boeing 727264 · Leading Edge DevicesSDR 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 DHL2008F00000Pin · damagedSMALL 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)Jul 2, 2008 · N765AT · Boeing 727264 · Leading Edge DevicesSDR 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 DHL2008763530Floorbeam · corrodedEXFOLIATION 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.Mar 24, 2008 · N763AT · Boeing 727264 · Fuselage Main, Floor BeamSDR DHL2008763529Rib · crackedNR 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.Mar 19, 2008 · N763AT · Boeing 727264 · Leading Edge DevicesSDR DHL2008763523Frame · dentedFRAME 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.Mar 16, 2008 · N763AT · Boeing 727264 · Fuselage Main, FrameSDR DHL2008763511Hinge · crackedMCD 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.Mar 16, 2008 · N763AT · Boeing 727264 · Fuselage, Door HingeSDR DHL2008763509Skin · chafedRT 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.Mar 16, 2008 · N763AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2008763528Support Fitting · crackedNR 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, ASSEMMar 14, 2008 · N763AT · Boeing 727264 · Leading Edge Slat ActuatorSDR DHL2008763527Support Fitting · crackedNR 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 90056Mar 14, 2008 · N763AT · Boeing 727264 · Leading Edge Slat Actuator
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