Boeing 727-2D4

Service difficulty reports · 279

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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 = '7272D4'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA04553Bulkhead · crackedLEFT WING INBD L/E CAVITY, SUPPORT BRACKET CRACKED AT FWD FIXED L/E 3 INCH OTBD NR 1 FLAP INBD HINGE. REMOVED SUPPORT BRACKET ASSY REF: SRM 51-30-02. CRACKS FOUND .25 INCH AND 1 INCH LONG ON PARTS 65-17356-39 AND -87, OUT OF LIMITS. FABRICATED -39 AND -87 Oct 26, 2008 · N287FE · Boeing 7272D4 · Wing Miscellaneous StructureSDR 08FDEA04552Stringer Clip · corrodedAFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F, STR 27L WL 141. INSTALLED NEW STRINGER CLIP 65-12434-3 REF SRM 51-10-1 AND ARM 53-10-1. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 26, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04551Panel · crackedPANEL RACK, EDGE PANEL STA 1030 TO STA 1166 RBL 19 TO 28 AFT PLATE OB EDGE BROKEN AND CORRODED UPPER SURFACE BLENDED CORROSION ORG "T" .040, MATERIAL LOSS OF .005 AT DEEPEST POINT WITHIN LIMITS. REF SRM 53*-10-1 FIG 7 TOOL NR AAR20278 CAL DUE 12-11-08. REPAIOct 26, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04549Crease Beam · crackedR-1 DOOR CREASE BEAM WEB CRACKED AT FWD END OF CUT-OUT. REMOVED AND REPLACED RT CREASE BEAM WEB REF DWG 65-56153 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIROct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, StructureSDR 08FDEA04548Beam · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION ON FWD SHEAR DECK STA 382 RBL 46-55. REPAIRED FLOORBEAM REF EA 7-5310-123808 AND DWG SR27-53-034 REV F REPAIR 5. THIS IS CLASSIFIED AS A MAJOR REPAIR. (ORIGINAL MATERIAL THICKNESS .125, MATERIAL LOSS .027, ROct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04547Frame · damagedAFT PIT BS 1090 FRAME HAS DOUBLE DRILLED HOLE INBD OF TIEDOWN FITTING AT S27R. REPAIRED IAW SRM 51-40-3. FABRCATED BRACKET IAW DWG 69-44106 TREATED, PRIMED IAW SRM 51-10-2. THIS CLASSIFIED AS A MAJOR REPAIR.Oct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04546Frame · damagedAFT PIT BS 1130 FRAME UPPER CHORD HAS TRIPLE DRILLED HOLE INBD OF TIE DOWN FITTING AT S27R. CUTOUT DAMAGE, REMOVED FASTENERS FROM FRAME AT REPAIR AREA. FABRICATED REPAIR ANGLE & HEAT TREATED TO T6 CONDITION. TREATED, PRIMED, & INSTALLED FRAME REPAIR ANGLEOct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04545Frame · damagedAFT PIT BS 1130 FRAME UPPER CHORD HAS DOUBLE DRILLLED HOLE IB OF TIE DOWN FITTING AT S27L. REMOVED AND INSTALLED FLOOR SUPPORT BRACKET, TIE DOWN BRACKET, FLOOR SUPPORT REF 51-30-2. REPAIRED DAMAGED FRAME REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REF SRM 51-10Oct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04544Frame · wornFUSELAGE UPPER LOBE INTERIOR STRUCTURE, FRAME 1166 SCRATCHED RBL 68 AT STR R11- R12 BLENDED DAMAGE REF SRM 53-10-1 PG 1-2A, OUT OF LIMITS, HEAT TREATED NEW REPAIR. REMOVED DAMAGE REF SRM 51-40-3 PG 1-6. TREATED AND PRIMED REPAIR REF SRM 51-20-13 AND 51-20-2Oct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04539Panel · crackedPFM BOX SHROUD SEVERED ON ONE END AND CRACKED AT OTHER END, PANEL RACK, DOT 3 REPAIRED PFM BOX SHROUD REF SRM 51-40-9 PAR 3 AND 7. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 25, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04524Stringer Clip · crackedAFT PIT BS 1130 S27L STRINGER CLIP SPLIT REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED STR CLIP REF SRM 51-30-02, 51-10-2 AND BOEING DWG 69-44104. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 24, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04523Shear Tie · corrodedAFT PIT BS 1130 SHEAR TIE HAS CORROSION ON LOWER FLANGE BETWEEN S27L AND 28L. FABRICATED SHEAR TIE. REMOVED AND REPLACED SHEAR TIE REF DWG 69-20813, SRM 51-30, OLD SHEAR TIE WAS BLENDED OUT OF LIMITS. ORIG "T" .050', .042 INCH REMAINING .008' MAT LOSS. THOct 24, 2008 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting StructureSDR 08FDEA04527Web · crackedMED FWD LWR CORNER INTERIOR SURFACE OF THE LOWER DOOR WEB IS CRACKED. REMOVED LOWER PORTION OF INNER SKIN FOR ACCESS REF SRM51-30-2 PG 32. REMOVED LWR FWD STOP FITTING REF SRM 51-30-2 PG 8 HAD WEB NDT'ED, AND NO CRACK WAS FOUND, TOOL NR IN22-0043 WAS USED CAOct 24, 2008 · N287FE · Boeing 7272D4 · Passenger/Crew DoorsSDR 08FDEA04520Stringer Clip · corrodedFWD PIT (STA 740), STR 27L, END CLIP ON STRINGER CORRODED FABRICATED NEW STRINGER CLIP, TREATED AND PRIMED. REFERENCE BOEING DRAWING NR 69-45628/ITEM NR 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 24, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04498Attach Fitting · corrodedAFT LOWER CARGO PIT STA 950E STR 29L ATTACH FITTING CORRODED ON LEFT SIDE. REMOVED ATTACH FITTING REF SRM 51-30-2 PG 32, MATCH DRILLED NEW ATTACH FITTING REF SRM 51-30-5, INSTALLED NEW ATTACH FITTING REF SRM 51-30-2 PG 2-12 THIS IS CLASSIFIED AS A MAJOR REPOct 23, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04497Stringer Clip · corrodedFWD PIT BS 620 STR 27R STRINGER CLIP CORRODED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.Oct 23, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04483Frame · corrodedAFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODEDOct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04481Support Angle · crackedFUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN FWD SUPPORT ANGLE AT BS 1176 RBL 53-70 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED NEW ANGLE (CLASSIFIED AS A MINOR REPAIR) REF DWG 65-29548-11& 51-30-02.Oct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04480Pan · crackedFUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PANEL CRACKED AT STA 1183 RBL 70. REMOVED DAMAGED DITCHING PAN, FABRICATED AND HEAT TREATED NEW DITCHING PAN, INSTALLED NEW DITCHING PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29548-53 & SRM 51-30-02Oct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04479Angle · crackedPASSENGER CABIN, BULKHEAD 1183 DITCHING PAN, LBL 19 ATTACH BRACKET CRACKED. REPLACED ANGLE IAW SRM 51-30-02 & DWG 65-29-567. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04478Pan · crackedPASSENGER CABIN BULKHEAD 1183 DITCH PAN, LBL 28 CRACKED.Oct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04476Pan · corrodedFUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN CORRODED AT BS 1183 RBL 53. REMOVED PAN & FABRICATED NEW PAN HEAT TREATED, INSTALLED NEW PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29567 & SRM 51-40-02.Oct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04473Frame · wornCABIN BS 360 S4R FRAME INNER CHORD WORN. BLENDED AREA, FOUND OUT OF LIMITS IAW SRM 53-10-04. FABRICATED REPAIR PART IAW SRM 53-10-04, REMOVED DAMAGE AND INSTALLED FARICATED REPAIR PART IAW SRM 53-10-4. TREATED AND PRIMED. THIS IS CLASSIFIED AS A MAJOR REPAIROct 22, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04453Strap · crackedPNL RACK, FWD PIT SIDEWALL TO FLOOR STRAP NR 5 IS CRACKED REPLACED STRAP ORIGINAL THICKNESS .063 2024 T3 A24170 PO NR 1039696, TREATED AND PRIMED NEW STRAP REF DWG 65-67205 AND MM 51-20-151-7 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 21, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04452Strap · corrodedPNL RACK, FWD PIT SIDEWALL TO FLOOR RT NR 2 STRAP IS CORRODED, STRAP IS CRACKED, CORROSION FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 30 NOTE A. FABRICATED, TREATED, PRIMED, AND IDENTIFIED NEW STRAP REF DWG 65-67205, SRM 51-10-2, AND FED EX MM1805 SEC 11-0-2700Oct 21, 2008 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 08FDEA04451Frame · corrodedAFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODED. REPAIRED FRAME BY INSTALLING REPAIR ANGLE REF SRM 51-40-03. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 21, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 08FDEA04432Stringer Clip · crackedCABIN BS 950B S6L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP AND INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04444Stringer Clip · crackedINTERIOR UPPER FUSELAGE BS 680 STR 10R CRACKED LOWER FLANGE RADIUS, OB OF CLIP. NDT VERIFIED CRACK, SPLICE ANGLES REMOVED REF SRM 51-30-2, DRILLED NEW STRINGER CLIP REF SRM 51-30-5. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. APPLIED CIC TO INTERIOR AND REOct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04438Stringer Clip · crackedUPPER INTER FUSELAGE BS 600 STR 9R STRINGER CLIP OTBD LOWER RADIUS CRACKED. REMOVED STRINGER CLIP REF. SRM 51-30-02 P1, LOCATED AND DRILLED FASTENERS HOLES REF SRM 51-30-05 P1 INSTALLED STRINGER CLIP 65-45313-14 A45966 REF SRM 51-30-02 P1, APPLIED CORROSION IOct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04437Stringer Clip · crackedINTERIOR UPPER FUSELAGE BS 640 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED CRACKED STRINGER CLIP REF: SRM 51-30-02 P1. LOCATED AND DRILLED FASRENER HOLES IN CLIP REF SRM 51-30-05, INSTALLED STRINGER CLIP REF SRM 51-30-02 P1. APPLIED CORROSION INHIBIOct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04436Stringer Clip · crackedINTERIOR UPPER FUSELAGE BS 660 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED STRINGER CLIP, CLEANED AND FOUND NO CRACKS. REINSTALLED STRINGER CLIP REF SRM 51-30-02 THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04435Stringer Clip · crackedINTERIOR UPPER FUSELAGE BS 480 STR 10R STRINGER CLIP OB RADIUS CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES AND INSTALLED STRINGER CLIP REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04434Stringer Clip · crackedINTERIOR UPPER FUSELAGE BS 680 STR 10R STRINGER CLIP CRACKED. REMOVED STRINGER CLIP REF SRM51-30-2, DRILLED NEW CLIP REF SRM 51-30-5. INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIROct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04433Stringer Clip · crackedCABIN BS 950B S7L STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 & 51-30-5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04431Stringer Clip · crackedCABIN BS 950B S5L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES TO NEW CLIP AND INSTALLED REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA04430Stringer Clip · crackedCABIN BS 950B S4L STRINGER CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP REF 51-30-02, LOCATED AND DRILLED FASTENER HOLES REF SRM 51-30-05, INSTALLED STRINGER CLIP 65-45313Y2/A23841 REF SRM 51-30-02 P1, APPLIED CORROSION INHIBITING COMPOUND REF SRM 51-10-02 P14Oct 20, 2008 · N287FE · Boeing 7272D4 · Fuselage Main, Attach FittingsSDR 08FDEA02901Warning System · malfunctionedINFLIGHT, LOWER AFT BODY OVERHEAT LT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND DETERMINED THAT THE LEAK IS BETWEEN NR 3 BLEED VLV AND PACK VALVE. HAD TO DESCEND TO FL250 TO CONTROL CABIN ALTITUDE AT 10000 FT. RAN ENGINES AT H/P. NO OVERHEAT LIGHT CHECKEJul 15, 2008 · N287FE · Boeing 7272D4 · Overheat DetectionSDR 06FDEA04176Door · stiffDOORS LIGHT ILUMINATED WITH LANDING GEAR DOWN, NOSE GEAR LIGHT ILLUMINATED ON S/O PANEL. FLIGHT-GO-AROUND, RAN QRH LANDED UNEVENTFULLY. OBSERVED NG DOORS DROPPING 1 INCH, FOUND EXCESSIVE AMOUNT OF RUBBER BUILD UP ON FWD EDGE OF BOTH NG FWD FRAMES, CAUSING BODec 5, 2006 · N287FE · Boeing 7272D4 · Landing Gear Position and WarningSDR 06FDEA03767Indicator · intermittentOTBD FLAP GAUGE SHOWED ASYMMETRY WHEN RETRACTING FLAPS FOR 15 DEGREE TO 5 DEGREE. RIGHT NEEDLE STAYED AT FLAPS 15, LEFT NEEDLE MOVED TO 5 DEGREE AND STOPPED. ON TOUCHDOWN, FLAPS TRACKED NORMALLY TO FLAPS 25. T/S AND FOUND OUTBOARD FLAP INDICATOR INTERMITTEOct 23, 2006 · N287FE · Boeing 7272D4 · Trailing Flap Position Indicating SystemSDR 06FDEA03747Indicator · malfunctionedOUTBOARD FLAP GAUGE SHOWED ASYMMETRY WHEN RETRACTING FLAPS FOR 15 DEGREE TO 5 DEGREE. RIGHT NEEDLE STAYED AT FLAPS 15, LEFT NEEDLE MOVED TO 5 DEGREE AND STOPPED. ON TOUCHDOWN FLAPS TRACKED NORMALLY TO FLAPS 25. T/S AND FOUND OUTBOARD FLAP INDICATOR INTERMITOct 20, 2006 · N287FE · Boeing 7272D4 · Trailing Flap Position Indicating SystemSDR 06FDEA2114Wire · damagedEMERGENCY EXIT LIGHT ABOVE L-1 ENTRY DOOR INOP. REPAIR GROUND WIRE W102B-090-20 IAW BSWPM 20-20-00. LIGHT OPS CHECK GOOD IAW FEDEX B727-200 MM 33-50-101-2. FOR REFERENCE SEE FEDEX SNRM N00970.May 31, 2006 · N287FE · Boeing 7272D4 · Light System WiringSDR 05FDEA03838Indicator · inoperativeCREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 INFO 16NOV05 18:20 MC1 R. PLEASE WORK IN CONJUNCTION WITH TSI: 77-10 7868.Nov 16, 2005 · N287FE · Boeing 7272D4 · Engine Pressure Ratio (EPR)SDR 05FDEA03313Uplock Switch · malfunctionedAMBER AIRSTAIR LIGHT ON S/O PANEL CAME ON IN FLIGHT. CHECKED A/C ON ARRIVAL, FOUND DOOR UP AND LOCKED. RAN DOOR SEVERAL TIMES. LIGHT STAYED ON ON FIRST TRY. ADJUSTED UPLOCK SWITCH ON LEFT AND RIGHT SIDE UPLOCK SWITCHES, PER AMM 52-62-001-5. OPS CHECK NORMOct 8, 2005 · N288FE · Boeing 7272D4 · Entrance StairsSDR 04FDEA03011Line · leakingWHILE DESCENDING ON GLIDESLOPE, ELEVATOR LOW PRESSURE LIGHT FLICKERED, CROSS CHECKED WITH HYDRAULIC PANEL AND NOTICED "A" SYSTEM AT ABOUT 1 QT. C/W QRH PROCEDURES. ENT BY: 448879 ADDED MPN BACH8A06NN0300T CPN 0109172 QTY 1 HOSE MSN 904416 ENT BY: 448879 Nov 2, 2004 · N287FE · Boeing 7272D4 · Hydraulic System, MainSDR 02FDEA00273Hydraulic Line · failedHYDRAULIC A SYSTEM FAILURE DURING GEAR RETRACT FLUID QTY DEPLETED TO ZERO, EXCEEDED HYD FLUID S/O VALVE LIMITATION. REMOVED AND REPLACED LINE, CHECKED ALL A-SYS. LEAK CHECK GOOD.Apr 23, 2002 · N287FE · Boeing 7272D4 · Hydraulic System, MainSDR 02FDEA00223Actuator · failed02-83 ON T/O FLAP RETRACTED FROM 5 DEG TO 2 DEG, #4 SLAT IND OUT. R&R #4 SLAT ACTUATOR PER MM 27-81-032-4. OK FOR SERVICE.Mar 29, 2002 · N288FE · Boeing 7272D4 · Leading Edge Slat Control SystemSDR 02FDEA00057Position Switch · faultyAFTER T/O AMBER LIGHT DID NOT EXTINGUISH ON RETRACTION TO FLAPS 2 DEG, S/O AUX PANEL SHOWED A RIGHT NR 5 L/E FLAP INTRANSIT LIGHT. RECYCLED WITH SAME RESULT. REMOVED AND REPLACED NR 5 L/E FLAP POS SWITCH DUE TO FLT CREW WRITE UP. REF MM 27-82-001-4.Jan 17, 2002 · N287FE · Boeing 7272D4 · Leading Edge Slat Position Indicating SystemSDR 01FDEA00802Warning Light · illuminated01-300 LWR AFT BODY HEAT LIGHT CAME ON. CK DUCTS IN AIR CONDITION COMP & AFT AIRSTAIR AREA. NO DEFECTS NOTED. OPS CK PER MM 26-14-00-1.Sep 6, 2001 · N287FE · Boeing 7272D4 · Overheat DetectionSDR 01FDEA00770Fitting · crackedMLG ACTUATOR SUPPORT FITTING COMMON TO 348.2 BULKHEAD CRACKED. REMOVED AND REPLACED FITTING PER MM 32-33-011-4 & SRM 51-30-2.Aug 27, 2001 · N288FE · Boeing 7272D4 · Landing Gear ActuatorSDR 01FDEA00767Shear Tie · corrodedCORROSION C53-113-01(1) ON FRAME BS 720 LBL 4 TO RBL 4 WL 149 AFT SIDE OF FRAME. REMOVED AND REPLACED SHEAR TIE 51-30-2, 51-31-000-2, 51-20-1, 51-20-021-7, 51-20-031-7.Aug 24, 2001 · N288FE · Boeing 7272D4 · Fuselage Main, Structure
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