Boeing 727-2B7

Service difficulty reports · 290

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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 = '7272B7'
  ORDER BY difficulty_date DESC"

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SDR DHL2006762514Wedge · dentedRT O/B AILERON WEDGE UPPER SURFACE IS DENTED 2 PLACES. REMOVED RT O/B AILERON WEDGE AS PER B727 SRM 51-30-2. INSTALLED REPAIRED WEDGE VENDOR ORDER NR 500080771 P/N 65-21725-19 AT RT O/B AILERON AS PER B727 SRM 51-30-2Jun 29, 2006 · N762AT · Boeing 7272B7 · AileronsSDR DHL2006762513Firewall · damagedNR 2 VERT FIREWALL HAS HOLE WORN THROUGH DOUBLER 6:30 POSITION AT T/E STA 1352. REMOVED EXISTING REPAIR AT NR 2 VERT FIREWALL 6:30 POSITION IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .050 PO NR 900342 DIM 11 3/4" BY 2 1/2" IAW B727 SRM 5Jun 29, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, BulkheadSDR DHL2006762509Skin · delaminatedLT WING, INBD FLAP TE IS DELAMINATED ON OUTBD TE WBL 243. REMOVED PREVIOUS REPAIR AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPAIR SKIN APPROX 6 1/2" BY 4 AND EXTERNAL DOUBLER APPROX 3" BY 4" FROM 7075T6 .016 PO NR 9003142. CLEANED, PREPPED, APPLIEJun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762506Skin · wornLT WING INBD FLAP, FORE FLAP L/E HAS WEAR SPOT ON SKIN WBL 114. REMOVED DAMAGED DOUBLER L/WING I/B FORE FLAP L/E WBL 114 AS PER B727 SRM 51-30-2. FABRICATED NEW DOUBLER 7" BY 8" 2024T3 .063 PO NR 9003310 AS PER B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUJun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762507Skin · crackedREF NR 072657 DISCREPANCY, RT WING T/E UPPER SURFACE AT NR 13 SPOILER CTR HINGE HAS SKIN CRACKED. REMOVED FASTENERS ON RT T/E UPPER NR 13 SPOILER IAW SRM 51-30-2, CUT OUT DAMAGE SECTION .7500 INCH X ,2500 AT RT WING T/E UPPER SURFACE NR 13 SPOILER HINGE SKIN Jun 29, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHL2006762504Skin · delaminatedRIGHT O/B MID FLAP WBL 348-358 HAS UPPER T/E DELAMINATED. CUT OUT DELAMINATED AREA R/W O/B MID FLAP UPPER SKIN APPROX 3.25 X 22 INCHES IAW SRM 51-40-20 PARA 6 & 7. FABBED ONE SKIN REPLACEMENT APPROX .75 X 22 INCHES AND ONE SPLICE PLATE 3 X 3.25 INCHES USING Jun 29, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762525Web · crackedAT RT SIDE OF AFT AIRSTAIR WELL CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. CUT OUT DAMAGED SECTION 11/8X1 AT RT SIDE OF AFT AIRSTAIR WELL TORQUE BOX WEB LIGHTENING HOLE STA 1237 IAW B727 SRM 51-40-2. FABRICATED DOUBLERS 7075T-6 .040Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762522Torque Box · crackedAT LT SIDE OF AFTSTAIR WELL, CRACK EMANATING FROM UPPER LIGHTENING HOLE IN TORQUE BOX AT BS 1263. REMOVED EXISTING DOUBLER AT LT SIDEWALL AFT AIRSTAIR WEB BS 1263 IAW SRM 51-30-2. FAB. NEW REPAIR DOUBLER FROM 7075T6 .040 PO NR 9003137 APPROX. DIM. 3 INCH X 3 IJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762521Structure · crackedAT LT SIDE OF AFT AIRSTAIR WELL 2 CRACKS EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. REMOVED EXISTING DOUBLER AT LT SIDE AFT AIRSTAR WEB BS 1237 IAW B727 SRM 51-30-2. FAB NEW DOUBLER FROM 7075T6 .040 PO NR 9003137 DIM.3" BY 3" IAW B727 SRMJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, StructureSDR DHL2006762517Web · crackedAFT AIRSTAIR DOOR SIDEWALL CRACKED AT LT ROLLER ON LOWER END OF STAIRS. REMOVED EXISTING REPAIR DOUBLER AT AFT AIRSTAIR SIDEWALL WEB LT ROLLER IAW B727 SRM 51-30-2. FAB NEW DOUBLER FROM 7075T5 .040 PO NR 9003137 APPROX 3"BY 3" IAW B727 SRM 51-40-2 FIG 1 AND Jun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762516Torque Box · crackedAT LT SIDE OF AIRSTAIR WELL CRACK EMANATING FROM UPPER LIGHTENING HOLE TORQUE BOX AT BS 1303. REMOVED PREVIOUS REPAIR DOUBLER AT LT SIDE AFT AIRSTAIR SIDEWALL WEB BS 1303 IAW B727 SRM 51-30-2. FAB NEW REPAIR DOUBLER FROM 7075T6 .040 PO NR 9003134 APPROX 3" BJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762500Web · crackedAT RIGHT SIDE OF AFT AIRSTAIR WELL, CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1225. REMOVED INTERIOR ACCESS PANEL AT RT SIDE OF AFT AIRSTAIRS STA 1183-1237 TORQUE BOX WEB AREA FOR ACCESS AS PER B727 SRM 51-30-2. CUTOUT DAMAGE .5 X .5 INCJun 28, 2006 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006762520Angle · crackedRIGHT INBD MID FLAP REAR LWR CHORD ANGLE CRACKED WBL 105. REMOVED SEAL RETAINER AND LWR CHORD ANGLE SECTION AND LOWER SKIN IAW B727 SRM 51-30-2. FAB NEW LOWER CHORD AT RIGHT INBD MID FLAP WBL 105 FROM P/N BAC1517-1367 PO NR 501953 IAW B727 SRM 51-50-2 FIG 5 Jun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762519Angle · crackedLEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOWS CRACK WBL 220. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD IAW B727 SRM 51-30-2. FABRICATED NEW MID FLAP LWR CHORD ANGLE FROM P/N BAC1503-100046 PO NR 627846Jun 27, 2006 · N762 · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762518Angle · crackedLEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOW CRACKS 2 WBL 105. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD IAW B727 SRM 51-30-2. FAB NEW MID FLAP LWR CHORD ANLGE FROM P/N BAC1503-100046 PO NR 627846 APPRJun 27, 2006 · N762AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006762503Hinge · crackedL1 DOOR CUTOUT, UPPER HINGE HAS EVIDENCE CRACK. NDT CONFIRMED CRACK IS ABOUT 1 INCH LONG, MARKED END OF CRACK 727 NDT PART 6, 51-00-00 FIG 23. OPENED AREA INTERIOR PANELS AT LT STA 259 FOR ACCESS. CUTOUT DAMAGED SECTION 1.75 X 1.5 INCH AT L1 DOOR UPPER HINGJun 27, 2006 · N762AT · Boeing 7272B7 · Fuselage, Door HingeSDR DHL2006762502Skin · dentedEXT FUS BS 1055 BELOW STR 20R HAS DENT. DENT AT BS 1055 BELOW STR 20R IS OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUTOUT DAMAGE AREA DIM 2" BY 2 3/4" AND 2" BY .750 IAW B727 SRM 53-30-3 FIG 5. REMOVED FASTENERS FOR SKIN REPAIR IAW B727 SRM 51-30-2. FAB REJun 26, 2006 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006762523Skin Panel · delaminatedL/WING TE UPPER PANEL DELAMINATED AT LWBL 88 BS 889 IN/SQ WITH NO CRACKS EVIDENT IN OUTER SKIN. CUT OUT DELAMINATED AREA ON UPPER SKIN OF L/WING TE PANEL APPROX 10" DIA. FABRICATED DOUBLER 14" DIA FROM .016" 7075T6 PO# 526029 AND BONDED. REMOVED SECTION OF Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHL2006762505Mount · crackedNR 5 KRUGER FLAP ACTUATOR MOUNT W.S. 230 OB LOWER CORNER IS CRACKED. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW SRM 51-30-2 . FAB NEW OB ACTUATOR MOUNT WEB IAW MFG DWG NR 65-16263, TREATED AND PRIMED WEB MOUNT AND WORKING AREA IAW SRM 51-10-2, INSTALLED NEW Jun 26, 2006 · N762AT · Boeing 7272B7 · Wing, Attach FittingsSDR DHL2006760002Pressure Valve · leakingRED GEAR DOOR LIGHT REMAINED ON AFTER T/O. PERFORMED AB PROC LIGHT WENT OUT. ALL INDICATIONS NORMAL. FOUND NOSE STRUT FLAT, HIGH PRESSURE VALVE ASSY LEAKING. REMOVED AND REPLACED VALVE ASSY PER M/M 32-21-01 AND SERVICE PER M/M 12-15-24. OPS GOOD. P/N MS2Jun 22, 2006 · N760AT · Boeing 7272B7 · Nose/Tail Landing Gear Strut/AxleSDR DHL2006770003Warning Switch · faultyAFTER T/O -R GEAR DOOR- AMBER LIGHT ON S/O PANEL ILLUMINATED. RED GEAR DOOR LIGHT ON FWD PANEL ILLUMINATED. F/O NOTED ASSYMETRIC YAW. COMPLETED ABNORMAL PROCEDURE PER AOM. LIGHTS REMAINED ILLUMINATED. PREVIOUS WRITE UP ON 6/13/06. REMOVED AND REPLACED RTJun 14, 2006 · N770AT · Boeing 7272B7 · Landing Gear Position and WarningSDR DHL2006770002Warning Switch · out of adjustDOOR WARNING LIGHT ILLUM RIGHT GEAR DOOR. CLEANED INSPECTED AND ADJUSTED CONTACTS FOR WARNING SWITCH IAW MM 32-62-11, PERFORMED OPS CK OF SYSTEM AND CKS OK ON GROUND.Jun 13, 2006 · N770AT · Boeing 7272B7 · Landing Gear Position and WarningSDR DHL2006760001Hinge · lack of lubeWHILE CLOSING THE FWD ENTRY DOOR THE HINGE JAMMED BETWEEN THE OPEN LOCK POSITION AND WHERE THE DOOR BEGINS TO PIVOT FOR CLOSING. TOOK SEVERAL ATTEMPTS TO GET THE DOOR CLOSED. LUBED DOOR HINGES, OPS CHECKS GOOD IAW B727MM 52-11-01.Mar 29, 2006 · N760AT · Boeing 7272B7 · Fuselage, Door HingeSDR DHL2006770001Connector · disconnectedRT GEAR DOOR ANNUNCIATOR LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION, S.O PANEL. RESEATED RT GEAR DOOR CONNECTOR PLUG CONNECTOR, SYSTEM OPS CHECK NORMAL IAW MM 32-62-08.Mar 17, 2006 · N770AT · Boeing 7272B7 · Landing Gear Position and WarningSDR DHL2006760510Rib · crackedL/WING NR 1 L/E SLAT ACTUATOR ROD END I/B ATTACH BRACKET SHOWS CRACK. REMOVED AND REPLACED RIB AND SUPPORT CHANNEL L/WING NR 1 L/E SLAT ACTUATOR ROD END I/B IAW B727SRM 51-30-2, 51-10-1.Mar 8, 2006 · N760AT · Boeing 7272B7 · Wing, Rib/BulkheadSDR DHL2006760503None · noneACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT HAND HORIZONTAL STABILIZER L/E SKIN AT L/E STA 30.0. INSTALLATION PERFORMED IAW 727 SRM 55-10-3 FIG 2. VERIFIED MATERIAL USED IS 7075-T6 0.063 THIS REPAIR IS CATEGORY A.Mar 7, 2006 · N760AT · Boeing 7272B7 · Standard Practices/StructuresSDR DHL2006760501Repair · noneACCOMPLISH IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT WING FIXED LEADING EDGE SKIN AT WS 207.0. ACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH REPAIR ON RIGHT WING FIXED LEADING EDGE SKIN AT WS 207.0. INSTALLATION PERFORMED IAW B-727 SRM 57-30-4 FIG 2. Mar 7, 2006 · N760AT · Boeing 7272B7 · Standard Practices/StructuresSDR DHL2006760513Skin · crackedRIGHT INBOARD MID FLAP LOWER T/E AT PUSH-ROD CUTOUT WBL 107 HAS BOTH CORNERS CRACKED. REMOVED DAMAGED AREA DIM 46.75 X 2.25 INCHES ON RIGHT INBOARD MID FLAP LOWER T/E AND FAB NEW PART MAT BAC 1517-1367-6511. EXTRUSION DIM 46.75 X 2.25 INCHES IAW B727SRM 57-5Mar 4, 2006 · N760AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006760512Web · crackedLEFT WING AT WBL 603.5 THRU ACCESS PANEL 8112 THE WEB IS CRACKED. CUT OUT DAMAGE 1 X 2 INCH IAW B727SRM 51-40-2 FIG 1. HFEC CUT OUT NO CRACKS NOTED IAW NDT MAN PART 6 51-00 FIG 23. REMOVED WEB IAW B727 SRM 51-30-2. FABBED DOUBLER FROM 2024 T3 .040 PO 90030Mar 4, 2006 · N760AT · Boeing 7272B7 · Wing Miscellaneous StructureSDR DHL2006760511Rib · crackedLEFT WING NR 3 L/E SLAT ACTUATOR ROD END OUTBOARD ATTACH SHOWS EVIDENCE OF CRACK. REMOVED AND REPLACED O/B RIB AT NR 3 L/E SLAT LEFT WING IAW B727 SRM 51-30-2.Mar 4, 2006 · N760AT · Boeing 7272B7 · Leading Edge DevicesSDR DHL2006760517Vertical Beam · crackedAFT CARGO COMPT STA 1183 VERTICAL BEAM AT RBL 8 IS CRACKED AT BOTTOM. STOP DRILLED CRACK AT AFT CARGO COMPT STA 1183 VERTICAL BEAM RBL 8 AS PER B727 SB 727-53-0175 REV3 01/25/1996 FIG 3 AND B727 SRM 51-10-1. INSTALLED REPAIR PARTS AT STA 1183 VERT BEAM RBL 8Mar 3, 2006 · N760AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2006760516Frame · corrodedAFT CARGO COMPT FRAME AT STA 1166 IS CORRODED WITH EXFOLIATION AND CRACKING BETWEEN STR 28L AND 28R ON AFT SIDE OF FRAME. CUTOUT FOR ACCESS STR 28RT STA 1158 TO 1166 DIM 8 INCHES IAW B727 SRM 51-10-1. REMOVED INTERCOSTAL FOR ACCESS STA 1148 TO 1166 RT IAW B7Mar 3, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006760515Frame · corrodedAFT CARGO COMPT FRAME AT STA 950B IS CORRODED AT WEB AND LOWER FLANGE BETWEEN STR 29L- 28L. CUT OUT DAMAGED AREA AT FRAME LWR FLANGE BS 950B STR 29L-28L DIM: 6.75 X 2 INCHES. FAB REPAIR DOUBLER FROM 7075 T6 .063 PO 9002695 DIM: 6.75 X 4.25 INCHES IAW B727 Mar 3, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006760514Frame · corrodedAFT CARGO COMPT FRAME AT STA 950B IS CORRODED AT WEB AND LOWER FLANGE BETWEEN STR 29L- 28L. CUT OUT DAMAGED AREA AT FRAME LWR FLANGE BS 950B STR 29L-28L DIM: 6.75 X 2 INCHES. FAB REPAIR DOUBLER FROM 7075 T6 .063 PO 9002695 DIM: 6.75 X 4.25 INCH IAW B727 SRMar 3, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006760530Nose Cowl · dentedNR 1 NOSE COWL L/E DENTED I/B SIDE. CUT OUT DAMAGED AREA, FABBED REPAIR DOUBLERS (4EA) FROM 2024 T3 /071 PO 550320 AND FILLER FROM 2024 T3 .063 PO 53125. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-30-2, 54-30-3 FIG 2, 54-30-2 FIG 1 AND 51-10-2. CUMar 2, 2006 · N760AT · Boeing 7272B7 · Engine Cowling SystemSDR DHL2006760529Rib · crackedLEFT WING NR 3 L/E SLAT ACTUATOR ROD END I/B ATTACH RIB CRACKED. REMOVED & REPLACED I/B RIB AT NR 3 L/E SLAT LEFT WING P/N 65-17297-13, PO 615063 IAW B727 SRM 51-30-2. THIS REPAIR IS A CATEGORY Q.Mar 1, 2006 · N760AT · Boeing 7272B7 · Wing, Rib/BulkheadSDR DHL2006760528Skin · delaminatedNR 1 SPOILER DELAMINATED AT I/B TRAILING EDGE. REMOVED SEAL CUT OUT DELAMINATED AREA APPROX 1.25 X 7.5 AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABBED REPAIR SKIN APPROX 7.5 X 4.25 & EXTERNAL DOUBLER APPROX 9 X 5.75 FROM 7075 T6 .025 PO 9002678. CLEANED, PRFeb 28, 2006 · N760AT · Boeing 7272B7 · SpoilersSDR DHL2006760527Frame · crackedCONTINUATION OF NR 029364 AFT CARGO COMP FRAME STA 1166 IS CORRODED WITH EXFOLIATION AND CRACKING BETWEEN STR 28L & 28R ON AFT SIDE OF FRAME. FABBED SPLICE REPAIR ON STR 28R STA 1158 & BCA1498-131 7075 T6 PO 5070593 DIM 10" IAW B727 SRM 53-10-3, TREATED & PRIFeb 21, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006760526Skin · dentedRIGHT SIDE FUSE HAS A DENT AT BS 1213 (RED DOT). CUT OUT DAMAGE AREA AT RT SIDE FUSE BS 1213 SIZE 3 X 3.25 INCH IAW B727 SRM 53-30-3 FIG 1. FABBED REPAIR DOUBLER RT SIDE FUSE BS 1213 SIZE 11.5 X 9 INCH MATERIAL USED 2024 T3 .063 PO 9003110 IAW B727 SRM 53-30Feb 20, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006760525Skin · dentedAFT AIRSTAIR EXTERIOR SKIN HAS NUMEROUS DENTS (MARKED RED). REMOVED STEPS TO SRN ACCESS IAW B727 SRM 51-30-2. REMOVED ORIGINAL SKIN IAW B727 SRM 51-30-2, FABBED NEW SKIN 11' X 42" 2024 T3 .040 PO 9003110 IAW B727 SRM 51-20-1 & 52-10-1 FIG 3. TREATED & PRIMEFeb 20, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006760524Spar · crackedRT ELEVATOR REAR SPAR HAS CRACK EXTENDING 0.125" FROM END OF SHEAR PLATE AT NR 4 HINGE BRACKET ELEV. STA 99.79 REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1.Feb 19, 2006 · N760AT · Boeing 7272B7 · Elevator, Spar/RibSDR DHL2006760523Spar · crackedRT ELEVATOR REAR SPAR HAS CRACK EXTENDING 0.125" FROM END OF SHEAR PLATE AT NR 4 HINGE BRACKET ELEV. STA 99.79 CORRECTIVE ACTION; REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1 THIS REPAIR IS A CATEGORY AFeb 19, 2006 · N760AT · Boeing 7272B7 · Elevator, Spar/RibSDR DHL2006760521Skin · crackedFOUND NR 5 SLAT IB FRAME AT ACTUATOR ROD END ATTACH IS CRACKED IN LOWER FWD RADIUS. REMOVED NR 5 SLAT I/B FRAME AT ACTUATOR ROD END IAW B727 SRM 51-30-2. REPLACED NR 5 SLAT I/B FRAME IAW B727 SRM 51-10-1 AND B727 SRM 51-30-2 P/N 65-17276-11. THIS REPAIR IS Feb 19, 2006 · N760AT · Boeing 7272B7 · Wing StructureSDR DHL2006760531Spar · crackedFOUND LT INBD MID-FLAP, REAR SPAR AT WBL 124, JUST BELOW INB AFT FLAP ACTUATION DRUM HAS CRACK. REMOVED DAMAGED AREA DIM.47" BY 2.25" ON L/H INBD MID FLAP LOWER, AND FAB NEW PART, MAT. BAC 1517-1367-6511, EXTRUSION, DIM 47" BY 2.25" IAW B727 SRM 57-50-1 AND IFeb 18, 2006 · N760AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006760532Spar · crackedLEFT INBOARD MID-FLAP, REAR SPAR AT WBL 124, JUST BELOW INBOARD AFT FLAP ACTUATION DRUM HAS CRACK. REMOVED DAMAGED AREA DIM 47 X 2.25 INCHES ON LEFT INBOARD MID FLAP LOWER, AND FAB NEW PART, MAT BAC 1517-1367-6511 EXTRUSIONDIM 47 X 2.25 INCHES IAW B727 SRM 57Feb 18, 2006 · N760AT · Boeing 7272B7 · Wing SparSDR DHL2006760520Skin · crackedFOUND NR 4 SLAT INBD HOOK CUTOUT IS CRACKED AT TOP OUTBD CORNER WING STA 390, NDT CONFIRMED). CUT OUT EXISTING FILLER STRIP TO ALLOW REPAIR FAB PLATE FROM P/N 301 1/2 HARD .025 PO #9002473 DIM 7" BY 5 1/4" FILLER FROM P/N 301 1/2 HARD .032 PO NR 9002473 DIM 7Feb 18, 2006 · N760AT · Boeing 7272B7 · Leading Edge DevicesSDR DHL2006760519Skin · crackedFOUND NR 3 SLAT OUTBD HOOK CUT OUT IS CRACKED AT TOP OUTBD CORNER WING STA 525. (NOT CONFIRMED). STOP DRILLED CRACK IAW B727 SRM 57-30-4 ACCOMPLISHED HFEC AROUND STOP HOLE NO CRACKS NOTED IAW NDT MAN PART 6 51-00-00 FIG 23. FABBED DOUBLER FROM .020 CRES 301 Feb 18, 2006 · N760AT · Boeing 7272B7 · Leading Edge DevicesSDR DHL2006760518Support Angle · crackedLEFT WING, NR 4 SPOILER ACTUATOR INBOARD SUPPORT ANGLE AT WS 460 APPROX HAS CRACK. INSPECTED NR 4 SPOILER I/B SUPPORT ANGLE USING HFEC AS GIVEN IN B727 NDTM, PART 6 SUB, 51-00-00 FIG 23, CRACK IS CONFIRMED. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2, PROCURFeb 18, 2006 · N760AT · Boeing 7272B7 · Wing Miscellaneous StructureSDR DHL2006762001Brake · malfunctionedLEFT BRAKE IS SOFT AND REQUIRES TWICE AS MUCH PRESSURE TO STOP AIRCRAFT AS RIGHT BRAKE. INSPECTED ALL BRAKES , NO DEFECTS NOTED. TAXIED AIRCRAFT, TESTED BRAKES, NO DEFECTS NOTED. WORK DONE IAW B-727 MM 32-40-00 AND JRH 5.2.Jan 26, 2006 · N762AT · Boeing 7272B7 · Landing Gear Brake SystemSDR DHL2005760006Switch · out of adjustWHEN PUTTING LANDING GEAR LEVER FROM UP TO OFF. IT CAUSED THE RT GEAR DOOR LIGHT TO ILLUMINATE ON S.O. PANEL. PERFORMED ABNORMAL PROCEDURE. LT GEAR HANDLE IN UP POSITION FOR LIGHT TO STAY OUT. CLEANED SWITCH PERFORMED ADJ AND TEST IAW MM REF 32-62-11 GRD OP CDec 8, 2005 · N760AT · Boeing 7272B7 · Landing Gear Position and Warning
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