Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  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 04FDEA00472Stringer Clip · damagedAFT CARGO BAY, MECHANICAL DAMAGE ON STRINGER CLIP, STR 25R, BS 1030. LOCATED & DRILLED HOLES ON NEW STRINGER CLIP AND REMOVED DAMAGE STRINGER CLIP AND INSTALLED NEW IAW SRM 51-30-2 AT BS 1030 25R STR.Feb 20, 2004 · N234FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA00471Stringer · corrodedCORROSION (C53-111-01, 3) AFT CARGO BAY, ON STR 25R, BS 1045. REMOVED CORROSION ON AFT CARGO BAY ON STR 25R BS 1045, 1 INCH X 2 INCHES. MAXIMUM MATERIAL LOST .040. ORIGINAL THICKNESS .071. OUT OF LIMITS. CUT OUT STRINGER FROM BS 1040 TO BS 1060. FABRICATEDFeb 20, 2004 · N234FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR P762004F00004Bracket · crackedLEFT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLES THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES AND CRACKED AND BENT.Feb 19, 2004 · N894AA · Boeing 727200 · Elevator Miscellaneous StructureSDR P762004F00001Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.Feb 19, 2004 · N894AA · Boeing 727200 · Elevator Miscellaneous StructureSDR 04FDEA00413Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED AT BS 1143 JUST 3 INCHES ABOVE STRINGER 12 LT.Feb 16, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00412Skin · gougedFUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232.Feb 16, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 2004F00077Wheel · fracturedPOSITION NR 3 OB WHEEL FLANGE SEPARATED FROM WHEEL, WHILE UNDER PRESSURE.Feb 16, 2004 · Boeing 727200 · Wheel/Ski/FloatSDR P9RA20040007Separator · dirtyAFTER TAKE OFF, THE AFT FLIGHT ATTENDANT REPORTED THE AFT CABIN WAS FILLING WITH SMOKE. RETURNED TO AIRPORT. PERFORMED TROUBLESHOOTING OF AIR CONDITIONING SYSTEM. FOUND DIRTY WATER SEPARATOR. CLEANED SAME. INSPECTED ALL INTERIOR PAX CABIN FOR EVIDENCE OF Feb 14, 2004 · N906PG · Boeing 727200 · Humidity Control SystemSDR 04FDEA00496Control Cable · out of positionAFTER LANDING, STABILIZER INOP IN BOTH CRUISE AND STAB MODE MANUAL HAND CRANK SHOWS NO RESISTANCE AS IF CABLE IS BROKEN. TROUBLESHOT TO STAB TRIM CABLES BEING OFF UPPER DRUM AND BOUND UP UNDERNEATH IT. REMOVED UPPER AND LOWER, LEFT AND RIGHT JACK SCREW ACCESFeb 12, 2004 · N244FE · Boeing 727200 · Stabilizer Control SystemSDR 04FDEA00393Generator · malfunctionedDURING CLIMBOUT LIGHTS FLICKERED ON & OFF, A/P CYCLED. ALL GEN LOADS VARIED FROM 18 KW TO 30 KW, SIMULTANEOUSLY APPROX 1/2 SEC IN DURATION. GEN VOLT STEADY; FREQUENCY SPIKED WITH GEN SPIKES. INITIALLY OCCURRED AT HIGH POWER SETTINGS. STABILIZED ON POWER REFeb 11, 2004 · N287FE · Boeing 727200 · AC Generation SystemSDR 04FDEA00376Cable · damagedRED DOORS WARNING LIGHT ILLUMINATED ON GEAR RETRACTION S/O'S PANEL. NOSE GEAR DOOR LIGHT ALSO ILLUMINATED AFTER FOLLOWING QRH PROCEDURES. THE LIGHTS REMAINED ILLUMINATED. RETURN TO MEM. REMOVED AND REPLACED BOTH DOOR CABLE, ADJ AND RIGGED NOSE GEAR FWD DOOFeb 9, 2004 · N480FE · Boeing 727200 · Landing Gear Door Retract SectionSDR 04FDEA00375Bulkhead · corrodedCORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRICATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2.Feb 9, 2004 · N237FE · Boeing 727200 · Fuselage Main, BulkheadSDR 04FDEA00374Beam · corrodedCORROSION, STA 760 BL 0 WL 148, DELTA BEAM LWR L-ANGLE HAS CORROSION. ACCESSED DELTA BEAM WEB. REMOVED L-ANGLE AND FOUND L-ANGLE OUT OF LIMITS. FABRICATED NEW L-ANGLE, INSTALLED ANGLE AND REINSTALLED ACCESSED DELTA BEAM WEB FASTENERS AND DME NR 2 ANTENNA CLFeb 9, 2004 · N288FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00373Stringer · corrodedCORROSION ON STR 24L BS 306. REMOVED DAMAGE ON STR 24L BS 306. DAMAGE FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-3.Feb 9, 2004 · N288FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA00379Warning Horn · false activationLOWER CARGO SMOKE WARNING BELL ACTIVATED TWICE AT ALTITUDE FOR 1-2 SECONDS. WARNING LIGHTS AND HORN WENT OUT IMMEDIATELY WITHOUT ACTIVATING THE DISCHARGE BUTTON. BEGAN IMMEDIATE DESCENT INTO YMX. WARNING CAME ON CONTINUOUS AT 500 FT, PUSH BOTTLE DISCHARGE BFeb 7, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA00378Tire · failedSHORTLY AFTER TAXI OUT FROM OAK RAMP, HEARD A VERY LOUD BANG AND AIRCRAFT SHUDDERED SLIGHTLY. BROUGHT THE AIRCRAFT TO A SLOW STOP. ENGINE INDICATIONS NORMAL. REQUESTED FEDEX MX INSPECTION. BLOWN NR 3 TIRE NOTED BY MX. TOWED BACK TO RAMP.Feb 7, 2004 · N481FE · Boeing 727200 · TireSDR 04FDEA00332Stringer · crackedVERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1.Feb 6, 2004 · N288FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 04FDEA00331Floorbeam · corrodedCORROSION ON FLOORBEAM AT FLOOR PANEL FASTENER HOLES BS 400 LBL 10 - RBL 10. REMOVED CORROSION IN A 1.0 X2.0 X .038 AREA. ORIG THICKNESS IS .125, TOP CHORD IS OUT OF LIMITS PER SRM 53-10-1. CUT-OUT DAMAGED UPPER CHORD PER SRM 53-10-8. FABRICATED CHORDFeb 6, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00330Floorbeam · corrodedCORROSION ON FLOORBEAM BS 360 LBL 17 - RBL 7 WL 208. FOUND CORROSION ON FLOORBEAM BS 360, LBL 17 TO RBL 17 WL 208 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.Feb 6, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00334Power Supply · inoperativeDOOR EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY IN EMERGENCY EXIT LIGHT PER 727-200 MM 33-50-121-2. OPS CHECK GOOD, AIRCRAFT OK TO CONTINUE.Feb 6, 2004 · N469FE · Boeing 727200 · Emergency LightingSDR 04FDEA00324Cylinder · crackedNOSE GEAR OUTER CYLINDER IS CRACKED INBOARD OF LEFT TRUNNION. C/W WITH W/C 32T2501 NOSE LANDING GEAR AND DRAG BRACE REMOVAL/INSTALL. COMPLIED WITH W/C 32T2501 REMOVED AND REPLACED NOSE LANDING GEAR ASSY AND DRAG BRACE.Feb 5, 2004 · N201FE · Boeing 727200 · Nose/Tail Landing GearSDR 04FDEA00313Motor · leakingDURING CLIMBOUT FROM EWR AT 25,000 FT CREW NOTICED A RAPID LOSS OF HYDRAULIC SYSTEM-A FLUID FOLLOWED PROPER CHECKLISTS AND RETURNED TO BASE. EVENTUALLY LOST ALL SYSTEM-A FLUID. FOUND HYDRAULIC FLUID POURING OUT OF CASE DRAIN OVERFLOW LINE FROM FLAP DRIVE MOTFeb 5, 2004 · N245FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 04FDEA00311Warning Light · illuminatedON DEPARTURE, AMBER AFT AIRSTAIR LIGHT ON F/E'S DOOR ANNUNCIATOR PANEL ILLUMINATED. COMPLIED WITH QRH. RETURN TO GTF.Feb 4, 2004 · N204FE · Boeing 727200 · Door Warning SystemSDR 04FDEA00305Fire Detector · false activationDURING CLIMBOUT FROM ONT A/C HAD FIRE WARNING WITH CORRESPONDING NR 4 MAIN CARGO LIGHT ILLUMINATED. PERFORMED QRH & RETURNED TO ONT. SMOKE LIGHT REMAINED ON UNTIL PULLING INTO THE ONT RAMP. VISUAL INSPECTION AFTER LANDING REVEALED NO INDICATION OF FIRE OR SFeb 3, 2004 · N236FE · Boeing 727200 · Fire DetectionSDR XNOA1175Proximity Switch · malfunctionedRIGHT GEAR LIGHT REMAINS ON AFTER GEAR-UP, FOLLOW AS PER FOM. REMOVED AND REPLACED RT MLG PROX SWITCH IAW B727 MM 32-61-21, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-111. PERFORMED OPERATIONAL GEAR SWING IAW B727 MM 7-11-0 Feb 3, 2004 · N76753 · Boeing 727200 · Landing Gear Position and WarningSDR 04FDEA00286Floorbeam · corrodedCORROSION ON FLOORBEAM AT FASTENER HOLES BS 344 LBL 59 - RBL 17 WL 208. REMOVED CORROSION AREAS 77 X 2 X .040 INCHES FROM ORIGINAL .100. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPALCED UPPER CHORD OF FLOORBEAM BS 344 LBL 65 TO RBL 65 PER SRM 51-30-Feb 2, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00285Skin · corrodedCORROSION IN FWD CARGO BAY, CORROSION ON INNER SURFACE OF SKIN STA 684 BETWEEN STR 27 LT AND 28 LT. FOUND CORROSION ON SKIN AT BS 684, STR 27L AND 28L TO BE .015 DEEP X 4 X 6 INCHES FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-30-3. CUT Feb 2, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00256Actuator · malfunctionedDURING FLAP RETRACTION FLAPS FROM 5 TO 2 DEGREE AMBER LIGHT. REMAINED ON AND NR 1 LED SHOWED INTRANSIT. COMPLIED WITH QRH AND RETURNED TO MEM. IN WORK, AFTER BLOCKING BACK INTO GATE, NR 1 LEADING EDGE FLAP WOULD RETRACT BUT WOULD CREEP BACK OPEN, WITH HYD SJan 31, 2004 · N223FE · Boeing 727200 · Leading Edge Slat ActuatorSDR 04FDEA00245Stringer · corrodedCORROSION FWD CARGO BAY BS 685 STR 26R WL 145 ON STRINGER. LOCATED CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 BLENDED CORRODED AREA (STR 26 RT) 4 INCHES LONG, BLEND OUT WAS OUT OF LIMITS. REPAIRED DAMAGED AREA, ALODINED & PRIMED IAW SRM 51-30-2, 5Jan 29, 2004 · N237FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA00246Floorbeam · corrodedCORROSION ON FLOORBEAM BS 380 LBL 8-55 WL 208. BLENDED CORROSION ON BS 380 FLOORBEAM PER SRM 51-10-1. FOUND LBL 8 OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED REPAIR PARTS PER SRM 53-10-8. APPLIED ALODINE AND PRIMER TO CUJan 29, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00247Wire · brokenRED NOSE GEAR UNSAFE LIGHT ON FOLLOWING GEAR RETRACTION; FOLLOWED RED TABS & RETURNED TO VLN FOR LANDING. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH & POSITION SWITCH. PERFORMED ADJUSMENT/TEST, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND PJan 29, 2004 · N223FE · Boeing 727200 · Landing Gear System WiringSDR 04FDEA00238Frame · corrodedN00260 CORROSION (C53-113-01(2)), AFT CARGO BAY, FRAME HAS CORROSION BY FASTENER COLLAR AT BS 1050 LBL 19 WL 150 (FASTENER COMMON TO FLOOR TO SIDEWALL SUPPORT AND FRAME) BLENDED CORROSION ON FRAME AT BS 1050 LBL 19 WL 150 IN AN AREA OF 3X1X.013 O.TJan 28, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00235Frame · dentedFWD CARGO BAY, FRAME DENTED STA 660 STR 24 LT. CUT OUT DENTED MATERIAL FROM FRAME AT BS 660, STR 24L AND PER SRM 51-40-3, 53-10-1, USING 7075-T6, .050 LOT #466242. CUT OUT WAS 1X1Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00241Beam · corrodedLEFT A/C BAY, DELTA BEAM LWR PLATE HAS CORROSION AT STA 800 LBL 6 WL 140. REMOVED CORROSION ON DELTA BEAM LWR PLATE AT BS 800, LBL 6, WL 140 IN A 2.500X1.00X.029 DEEP. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA 2.00X.500X.090. FABRICATED FILLER Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00240Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1110, RBL 22, WL 208. CUT OUT CORRODED SECTION OF FLOORBEAM'S TOP CHORD BS 1110 WL 208 RBL 8-23 AND INSTALLED REPAIR ANGLES, TEE CHORD AND STRAPS PER SRM 53-10-8.Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00239Angle · crackedANGLE CRACKED IN RT WHEEL WELL, FORWARD LOWER CORNER, AFT OF APU LOAD CONTROL VALVE. REMOVED ANGLE IN RT WHEEL WELL FWD LWR CORNER AFT OF APU LOAD CONTROL VALVE HOUSING. FABRICATED NEW ANGLE FROM BAC 1503-100058, 7075T6 LOT 509311. APPLIED PROTECTIVE TJan 28, 2004 · N237FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA00237Floorbeam · corrodedCORROSION ON FLOOR BEAM AT FLOOR PANEL FASTENER HOLE BS 440, LBL 7.75 - 10.75 (100 PERCENT MATERIAL LOSS). REMOVED DAMAGE AREA OF TOP FLANGE OF FLOORBEAM AT BS 440. FABRICATED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10-8.Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00236Frame · dentedFWD CARGO BAY, FRAME DENTED STA 680 STR 23 LT COMING CUT OUT DENTED MATERIAL 1 X 1 INCH FROM FRAME AT BS 680 STR 23L AND REPAIRED PER SRM 53-10-1, 51-40-3 USING 7075-T6 .050 LOT #466242.Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00234Frame · dentedFWD CARGO BAY, FRAME DENTED STA 700 STR 23L. REMOVED DENTED MATERIAL FROM FWD CARGO BAY, FRAME AT BS 700, STR 23L, 24L AND REPAIRED PER SRM 51-40-3 USING 7075-T6 .050 LOT 466242, CUT OUT WAS 1X1 INCH.Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00233Skin · damagedRT EXTERIOR FUSELAGE SKIN HAS CREASE AT BS 1143 STR 18R TO 3 INCHES BELOW STR 19R. DAMAGE ON EXTERNAL SKIN BS 1143 STR 18R TO 3" BELOW STR 19R A/Y RATION=76 AREA FOUND TO BE WITHIN LIMITS PER SRM 53-30-1 FIG 1 EXCEPT AT STR 19R. FOUND TO BE OUT OF LIMITS PERJan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00232Floorbeam · corrodedCORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208. REPAIR CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208 PER SRM 53-10-8Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA00228Smoke Detector · false activationFIRE BELL, LIGHT AND NR 4 MAIN SMOKE SENSOR SHORTLY AFTER TAKEOFF. NO ODORS OR FUMES DETECTED. SHORTLY AFTERWARD BOTH DUCT OVERHEAT LIGHTS CAME ON. S/O HAD AIR MIX VALVE AT 12 O'CLOCK, NR 1 PACK ONLY, 100 DEG F OUTPUT INDICATED. FIRE INDICATION WENT OUT WIJan 27, 2004 · N242FE · Boeing 727200 · Smoke DetectionSDR P9RA20040005Proximity Switch · out of adjustIN CRUISE FLIGHT PIE TO SYR, NOSE WHEEL GEAR DOOR EXTENDS IN LIGHT CHOP. FOUND LEFT NOSE WHEEL WELL DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SAME PER MM 32-62-11, OPS CHECKED NORMAL.Jan 25, 2004 · N919PG · Boeing 727200 · Door Warning SystemSDR DHL2004749002Control Unit · malfunctionedR2 WINDOW CRACKED. COMPLETED ABNORMAL PROCEDURE. REMOVED AND REPLACED RIGHT NR 2 WINDOW HEAT CONTROL UNIT. OPS CHECKED GOOD IAW 30-41-12. REPLACED R2 WINDOW, HEATING ELEMENT SHORTED OUT REPAIRED R2 WINDOW OPS CHECKED GOOD IAW 56-12-11.Jan 24, 2004 · N749DH · Boeing 727200 · Windshield/Door Rain/Ice RemovalSDR 04FDEA00212Shear Tie · corrodedCORROSION (C53-113-01, 2) AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950F BETWEEN STR 29 LT AND 30 LT. CORROSION ON FRAME SHEAR TIE AT BS 950F BETWEEN STR 29 AND 30L IS OUT OF LIMITS PER SRM 51-10-1. FABRICATED A NEW SHEAR TIE AND REPLACED IT PER SRMJan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00209Frame · crackedAFT CARGO BAY, FRAME CRACKED AT FASTENER HOLE BS 1050 RBL 20 WL 149 (FLOOR TO SIDEWALL SUPPORT ATTACH FASTENER HOLE). REPAIRED AFT CARGO BAY FRAME AT BS 1050, RBL 20, WL 149 IAW FED EX E.A. 7-5310-55217.Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00208Frame · dentedAFT CARGO BAY, FRAME IS DENTED AT BS 1070 BETWEEN STRINGER 25 RT AND 27 RT. REPAIRED AFT CARGO BAY FRAME AT BS 1070 STR 25-27R IAW FED EX E.A. 7-5310-55218.Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00210Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148. BLENDED CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148 PER SRM 51-10-1. BLEND AREA WAS 2X1INCHES, ORIGINAL THICKNESS WAS .063. 100 PERCENT MATERIAL WAS REMOVED. REMOVED DAMAGED SHEAR TIE, BS 500, STJan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00213Skin · dentedRT EXTERIOR FUSELAGE SKIN HAS A DENT AT BS 196 BELOW STR 19R 4 INCHES BELOW SKIN LAP. REMOVED DAMAGE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.Jan 23, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA00207Shear Tie · corrodedCORROSION IN AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950D BETWEEN STRINGER 29 LT AND 28 LT. REMOVED CORROSION ON SHEAR TIE AT BS 900D BETWEEN STR 29L AND 28L. FABRICATED SHEAR TIE. ALODINE, PRIMED AND INSTALLED SHEAR TIE AT BS 350D BETWEEN STR 29L Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, Structure
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