N7640U, cancelled Mar 14, 2007

Service difficulty reports · 65

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 = 'N7640U' AND deregistration_id = 'N7640U-2007-03-14'
  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 C7WA200600007Control Box · false indicationNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED SHUTDOWN ENGINE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL BOX OPS CHECK GOOD IAW MM. (K)Mar 22, 2006 · N7640U · Boeing 727222 · Fire DetectionSDR C7WA200600008Clamp · looseNR 1 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED IN FLIGHT. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. INSPECTED ENGINE FOR LEAKS AND DAMAGE. TIGHTENED CLAMPS ON BLEED AIR DUCTS AND REPOSITIONED FIRE LOOP IN PYLON. RAN ENGINE OPERATIONAL CHECKMar 22, 2006 · N7640U · Boeing 727222 · Engine Bleed Air SystemSDR C7WA200600003Engine · fodIN FLIGHT, AT FL 28.0, NR 2 ENGINE COMPRESSOR STALLED. ENGINE WAS IN STABLE OPERATION, NO BLEED AT 1.80 EPR. EPR DROPPED TO 1.4 EGT RUNS 80 TO 100 HOTTER THAN ENGINES 1 AND 3 IN ALL PARAMETERS OF FLIGHT. INSPECTION ON NR 2 ENGINE REVEALED HEAVY FOD DAMAGE. Feb 22, 2006 · N7640U · Boeing 727222 · Engine (Turbine/Turboprop)SDR C7WA200500110Overheat Loop · groundedLOWER AFT BODY OVERHEAT LIGHT ON. COMPLETED EMERGENCY PROCEDURE, FOUND IT TO BE NR 2 ENGINE. INSPECTED NUMBER 2 ENGINE FOUND LOOP TOUCHING BLEED AIR DUCT. REPOSITIONED LOOP OPERATIONAL CHECKS GOOD PER MM 26-14-0. (M)Jul 23, 2005 · N7640U · Boeing 727222 · Overheat DetectionSDR C7WA200300077Connector · dirtyAIR RETURN, UPON FLAP RETRACTION ON CLIMB-OUT, NR 1 SLAT FAILED TO RETRACT. CLEANED CONNECTOR IAW 20-80-01, OPS CHECKED FLAPS AND SLATS PER MM 27-80-0. ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE. (M)Jan 15, 2005 · N7640U · Boeing 727222 · Leading Edge Slat Control SystemSDR C7WA200400041Transmitter · frozenEXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM.Sep 7, 2004 · N7640U · Boeing 727222 · Trailing Flap Position Indicating SystemSDR C7WA2004000AASwitch · inoperativeENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. REMOVED AND REPLACED NAug 25, 2004 · N7640U · Boeing 727222 · Engine Start Valves/ControlsSDR 2004F00172Accessory Unit · faultyON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIATE CHECKLIST FOR UNSAFE GEAR. RECYCLED GEAR SECOND TIME AND ALL INDICATIONS WERE NORMAL. AIRCRAFFeb 4, 2004 · N7640U · Boeing 727222 · Landing Gear Retraction/Extension SystemSDR 2004F00167Duct · crackedON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT. AIRCRAFT LANDED ICT WITHOUT INCIDENT. REMOVED AND REPLCED NR 3 ENGINE 13 STAGE SADDLE DUCT. GROUND OPERATIONAL CHECK NORMAL. (M)Feb 2, 2004 · N7640U · Boeing 727222 · Engine Bleed Air SystemSDR 2004F00110Generator · failedDURING TAKEOFF FROM BNA, AIRCRAFT LOST NR 3 GENERATOR, EPR WENT TO 1.6 AND OIL PRESSURE FELL TO REDLINE. PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. DURING GROUND RUN OF ENGINES, FOUND NDec 11, 2003 · N7640U · Boeing 727222 · AC Generation SystemSDR 2004F00072Hinge · crackedAT B-CHECK, FOUND AFT SECTION OF MAIN CARGO DOOR HINGE CRACKED AT AFT END AIRFRAME SIDE. REMOVED CRACKED SECTION OF MAIN CARGO DOOR HINGE. FABRICATE, TREAT, PRIME AND INSTALLED NEW HINGE SEGMENT. MAIN CARGO DOOR OPERATIONAL CHECKED NORMAL. (M)Sep 30, 2003 · N7640U · Boeing 727222 · Cargo/Baggage DoorsSDR 2004F00057Angle · crackedAT B-CHECK, FOUND NR 2 SPOILER ACTUATOR IB MOUNT BRACKET CRACKED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR IB MOUNT BRACKET. RIGG AND LEAK CHECKED NORMAL. (M)Sep 30, 2003 · N7640U · Boeing 727222 · Wing, Attach FittingsSDR RYN2004F00027Module · failedAFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCEDURES. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYSep 16, 2003 · N7640U · Boeing 727222 · Hydraulic System, MainSDR 2003F00420Floor Support · dentedAT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 17. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 17 STATION 950F PLUS 2 INCHES. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00419Frame · crackedAT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 660, STRINGER 23R/24R. FABRICATE REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 660 STRINGER 23R AND 24R. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00417Frame · crackedAT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 680, STRINGER 23R/24R. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 680 STRINGER 23R THROUGH 24R. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00413Floor Support · dentedAT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 13. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED REPAIR AT AFT CARGO FLOOR SUPPORT RBL 13 STATION 950F. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00412Floor Support · dentedAT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 9. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 9 STATION 950F. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00410Access Panel · crackedAT C-CHECK, FOUND CRACK ON RIGHT WING, NR 6 SLAT LOWER ACCESS PANEL NR 6589. FABRICATED NEW PANEL. ALODINED, PRIMED AND INSTALLED NEW ACCESS PANEL AT RIGHT LOWER NR 6 SLAT. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Wing, Plate/SkinSDR 2003F00409Bracket · brokenAT C-CHECK, FOUND NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BRACKET BROKEN. REPLACD NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BOLT BRACKET. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00405Frame · crackedAT C-CHECK, FOUND DENT ON FORWARD CARGO FRAME AT BS 720A, STRINGER 24L. FABRICATED REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 720A STRINGER 24L. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00404Frame · crackedAT C-CHECK, FOUND DENTS ON FORWARD CARGO FRAME AT BS 700, STRINGER 24L/25L. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 700 STRINGER 24L AND 25L. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00403Floor Support · dentedAT C-CHECK, FOUND DENT ON AFT CARGO COMPARTMENT FLOOR SUPPORT, STATION 950E, LBL 10. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED PARTS ON AFT CARGO FLOOR SUPPORT LBL 10 STATION 950E. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00401Panel · crackedAT C-CHECK, FOUND CRACK ON RIGHT WING, OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD ATTACH BRACKET. FABRICATED BRACKET. TREATED, PRIMED AND INSTALLED BRACKET ON RIGHT WING OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Wing, Plate/SkinSDR 2003F00397Floorbeam · crackedAT C-CHECK, FOUND CRACK ON AFT CARGO FLOORBEAM AT STATION 950B, BL 0. FABRICATE NEW ANGLE. TREATED, PRIMED AND INSTALLED NEW ANGLE AT STATION 950B BL 0. (M)Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Floor BeamSDR 2003F00418Stringer Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER CLIP AT STAITON 540, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 540 STRINGER 5R. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00416Frame · crackedAT C-CHECK, OFUND CRACK ON LOWER LEFT PANEL MOUNT FRAME AT LOWER END, BS 720. FABRICATE REPAIR ANGLE. ALODINED, PRIMED AND INSTALLED NEW ANGLE AT LOWER LEFT PANEL MOUTN FRAME STATION 720. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00415Skin · crackedAT C-CHECK, FOUND CRACK ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. FABRICATE DOUBLER REPAIR. ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/SkinSDR 2003F00414Fairing · crackedAT C-CHECK, FOUND CRACK ON LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. CUT OUT CRACKED SECTION AND INSTALLED DOUBLER AT LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00402Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER FRAME ATTACH CLIP AT STATION 570, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 560 STRINGER 5R. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00400Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720, STRINGER 3L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720 STRINGER 3L. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00399Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720C, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720C STRINGER 5R. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00398Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720A, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 720A STRINGER 5L. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00422Stringer Clip · crackedAT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720E, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720E, STRINGER 5L. (M)Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 2003F00421Duct · crackedAT C-CHECK, FOUND CRACK ON HEATING AND AIR CONDITIONING DUCT AT BS 720E/D, STRINGER 12/13. STOP DRILLED CRACKS. FABRICATED DOUBLER. ALODINED, PRIMED AND INSTALLED DOUBLER AT FUSELAGE HEATING AND AIR CONDITIONING DUCT, RIGHT SIDE OF CABIN, BETWEEN STATION 72Mar 13, 2003 · N7640U · Boeing 727222 · Air Distribution SystemSDR 2003F00441Frame · crackedAT C-CHECK, FOUND INDICATION OF CRACK AT TERMINAL HOLE FITTING, BS 870. STOP DRILLED CRACK AT SECOND FASTENER ROW, SECOND FASTENER DOWN FROM STRINGER 9R ON BS 870 TERMINAL FITTING. FABRICATED AN EXTERNAL DOUBLER REPAIR. TREATED AND PRIMED DOUBLER AND AREA OMar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00440Skin · crackedAT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN CRACKED. STOPPED DRILLED CRACKS ON RIGHT FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER ON RIGHT FORWARD GALLEY DOOR LOWER AFT,Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/SkinSDR 2003F00439Frame · crackedAT C-CHECK, FOUND TIE FRAME TO FUSELAGE CRACKED AT STATION 680, STRINGER 17L. FABRICATED ANGLE REPAIR. ALODINED, PRIMED AND INSTALLED ANGEL REPAIR ON BS 680, STRINGER 17L, LOWER SILL BEAM TIE FRAME. (M)Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00429Skin · crackedAT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT LOWER FORWARD CORNER SKIN CRACKED. STOP DRILLED CRACK ON RIGHT FORWARD GALLEY DOOR CUTOUT, FORWARD, LOWER CORNER SKIN. FABRICATED DOUBLER AND TRIPLER. TREATED, PRIMED AND INSTALLED DOUBLER AND TRIPLER ON FORWARD Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/SkinSDR 2003F00493Skin · crackedAT C-CHECK, FOUND CRACK ON LEADING EDGE WING SKIN AT NR 5 OUTBOARD SLAT TRACK. STOP DRILLED CRACK. FABRICATED DOUBLER. ALODINED AND PRIMED AREA REPAIR DOUBLER. INSTALLED AT RIGHT WING NR 5 OUTBOARD SLAT TRAKC LEADING EDGE CUT OUT. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Wing, Plate/SkinSDR 2003F00458Skin · crackedAT C-CHECK, FOUND CRACK AT RT WING LEADING EDGE ABOVE NR 5 INBOARD SLAT TRACK LEADING EDGE CUTOUT UPPER RADIUS. STOP DRILLED CRACK AT RIGHT WING LEADING EDGE NR 5 SLAT TRACK CUT OUT, AT WING STATION 383. FABRICATED REPARI DOUBLER. ALODINED, PRIMED AND INSTAMar 10, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00457Panel · crackedAT C-CHECK, FOUND CRACK AT LEFT ELEVATOR BALANCE BAY PANEL 9720. ROUTED CRACKED AREA ON LT ELEVATOR BALANCE PANEL NR 9720. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Elevator, Plate/SkinSDR 2003F00449Retainer · crackedAT C-CHECK, FOUND CRACK AT RIGHT WING NR 5 SLAT OUTBOARD SEAL RETAINER. REMOVED AND REPLACED RIGHT WING NR 5 SLAT, OUTBOARD HOOK SEAL, UPPER LEADING EDGE WING, OUTBOARD SEAL RETAINER TRIM. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00448Plate · crackedAT C-CHECK, FOUND CRACK AT NR 6 SLAT LOWER BACKSIDE ACTUATOR ROD END ACCESS CUTOUT SUPPORT PLATE. REMOVED DAMAGED PLATE FROM RIGHT WING NR 6 SLATE LOWER BACKSIDE SLAT ACTUATOR ROD END ACCESS CUT OUT. FABRICATED PLATE. TREATED AND PRIMED PART AND AREA. INSTMar 10, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00436Retainer · crackedAT C-CHECK, FOUND CRACK AT NR 5 SLAT, INBOARD HOOK SEAL CUTOUT, OUTBOARD SEAL RETAINER. REMOVED AND REPLACED NR 5 SLAT INBOARD HOOK SEAL, UPPER LEADING EDGE, OUTBOARD SEAL RETAINER TRIM. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00435Bracket · crackedAT C-CHECK, FOUND CRACK AT NR 6 SLATE ACTUATOR SUPPORT BRACKET. ACCOMPLISHED AN HFEC INSPECTION ON RIGHT WING NR 6 SLAT ACTUATOR OUTBOARD MOUNT BRACKET. NO CRACKS NOTED. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge DevicesSDR 2003F00430Angle · crackedAT C-CHECK, FOUND STRUCTURE CRACKED, NOSE WHEEL WELL AT BS 294.5, LBL 12 RT, WL 177. STOP DRILLED CRACKS. FABRICATED FORMED ANGLE REPAIRS AND STRAPS. TREATED, PRIMED AND INSTALLED ANGLES AND STRAPS IN NOSE WHEEL WELL RIGHT SUPPORT AT STATION 294.5. (M)Mar 10, 2003 · N7640U · Boeing 727222 · Wing Miscellaneous StructureSDR 2003F00433Skin · burnedAT C-CHECK, FOUND STATIC DISCHARGE BURN, RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. CUT OUT DAMAGED AREA ON RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. FABRICATED DOUBLERS AND FILLER. TREATED AND PRIMED PARTS. INSTALLED REPAIR PARTS. (M)Mar 9, 2003 · N7640U · Boeing 727222 · Elevator, Plate/SkinSDR 2003F00427Frame · crackedAT C-CHECK, FOUND TIE FRAME CRACKED AT BS 480, STRINGER 17L. FABRICATED REPAIR ANGLES. TREATED AND PRIMED FABRICATED REPAIR ANGLES. INSTALLED AT STATION 480, STRINGER 17L. (M)Mar 9, 2003 · N7640U · Boeing 727222 · Fuselage Main, FrameSDR 2003F00446Bracket · crackedAT C-CHECK, FOUND CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET, OUTBOARD OF NR 2 SPOILER ACTUATOR. REMOVED AND REPLACED BRACKET ON LEFT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET AT NR 2 SPOILER, OUTBOARD OF ACTUATOR. (M)Mar 8, 2003 · N7640U · Boeing 727222 · Wing Miscellaneous Structure
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