Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA02224Attach Bracket · crackedNR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET REF, FED EX J/C 76C07500 AND BOEING DWG 65-21795 AND SRM 51-30-2 PG 4&5.Jun 20, 2007 · N286FE · Boeing 727233 · Wing, Attach FittingsSDR 07FDEA02222Floorbeam · crackedFWD ENTRY FLOOR SUPPORT UPPER FLANGE CRACKED BS 310, LBL32. REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 53-30-2.Jun 20, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02221Stringer · misrepairedFOUND ON AGING A/C INSP EXISTING REPAIR AT STR S-27R FROM BS 610 TO BS 630 DOES NOT CONFORM TO CURRENT SRM 53-10-3 FIG 1. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON STR 27R, BS 610 TO BS 630, REF SRM 53-10-3 PG 3. INSTALLED STRINGER SPLICE REPAIR HAT CHJun 20, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA02215Keelbeam · corrodedAFT PIT STR 29L, KEEL BEAM CHORD CORRODED STA 950F-970 REMOVED A MAXIMUM OF .032" OF CORROSION ON KEEL BEAM BETWEEN STA 950F AND 970 AND IS OUT OF LIMITS. SPOT FACED HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP. INSTALLATION OF REPAIR PARTJun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, KeelSDR 07FDEA02214Keelbeam · corrodedAFT PIT STR 29L KEEL BEAM CHORD CORRODED STA. 970-990 REMOVED A MAXIMUM OF .048" CORROSION ON KEEL BEAM BETWEEN STA 970 AND 990 AND IS OUT OF LIMITS. SPOT FACED FASTENER HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP AND INSALLATION OF REPAIJun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, KeelSDR 07FDEA02213Keelbeam · corrodedAFT PIT STR 29L/KEEL BEAM CHORD CORRODED BETWEEN STA 950D - 950E REMOVED CORROSION, FABRICATED REPAIR STRAP, SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED FILLER WASHER AND INSTALLED REPAIR PARTS. REF FED EX STANDARD REWORK DRAWING, LT AND RT KEELJun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, KeelSDR 07FDEA02212Keelbeam · corrodedAFT PIT STA 950E-950F STR 29L KEEL BEAM CORRODED REMOVED CORROSION, REMOVED .052" MAXIMUM DEPTH ON KEEL BEAM BETWEEN STA 950E AND 950F IS OUT OF LIMITS. SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED REPAIR STRAP, FABRICATED FILLER WASHER AND INSTALLEJun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, KeelSDR 07FDEA02211Channel · corrodedAFT PIT ANTENNA DOUBLER CORRODED AT STA 1030-1050 BETWEEN STR 29R-30. REMOVED NR 3 VHF ANTENNA AND DOUBLERS REF SRM 51-30-02. REMOVED HAT CHANNEL. REMOVED CORROSION FROM DOUBLERS. ORIGINAL THICKNESS .196" REMOVED .002 REMAINING .194" WITHIN LIMITS REF SRM Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02210Skin · crackedLOWER EXTERNAL SKIN IS CRACKED AT BS 1082, RBL 4. R EMOVED SURROUNDING STRUCTURE TO ACCESS DAMAGE. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL, NO DEFECTS. INSTALLED DOUBLER AND FILLER WHERE DAMAGE WAS REMOVED. INSTALLED SURROUNDING STRUCTURE REF SRM 51-3Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02209Door · corrodedLEFT AFT EMERGENCY EXIT HATCH INTERIOR STRUCTURE ATTACH ANGLE AT FWD LWR CORNER OF WINDOW FRAME CORRODED REMOVED OLD ANGLE AT FWD CORNER OF WINDOW FRAME AND FABRICATED AND INSTALLED A NEW ANGLE USING 7075-T-6 .071". ORIGINAL THICKNESS WAS .071" CALIPER GAUGE Jun 19, 2007 · N286FE · Boeing 727233 · Emergency ExitsSDR 07FDEA02206Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED STA 950E BETWEEN STR 28-29L. REMOVED CORRODED SHEAR TIE AND REPAIRED PER SRM 53-10-4 FIG 15.Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 07FDEA02205Floorbeam · misrepairedAGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX DWG SR27-53-034 AT BS 680 LBL 3'' TO 23''. REMOVED OLD REPAIR, FABRICATED NEW PARTS AND INSTALLED REF SRM 51-10-1 AND FED EX DWG SR27-53-034.Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02204Floorbeam · misrepairedON AGING AC INSPECTION FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT FED EX SR27-53-034 AT BS STA 720D, LBL27"-43" FLOORBEAM. REMOVED OLD REPAIR, FABRICATED 2 NEW ANGLES, HEAT TREATED, CAD PLATED, PRIMED AND PAINTED. INSTALLED 2 NEW ANGLES AND FILLERS AT Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02200Floorbeam · corrodedCABIN FLOOR SUPPORT WEB AT STA 804 RBL 45 IS CRACKED OUT FASTENER HOLE. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT WEB STA 804, RBL 5, SRM 51-30-2, DWG 65-16279.Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02199Stringer Clip · corrodedAFT PIT STA 950E STR 29L STRINGER CLIP/FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE REF SRM 51-30-2.Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02196Stringer · corrodedLOWER FUSELAGE STA 1082 STR 30 HAS CORROSION ON LOWER SURFACE OF STRINGER AT CUT OUT FOR SKIN. REMOVED DAMAGED SECTION OF OF STRINGER 30, AT STA 1082 AND REPAIRED REF SRM 53-10-30 FIG 1.Jun 19, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA02133Skin · misrepairedAGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20, AT RT WING OB AFT FLAP T/E 8" TO 22" FROM OB END. REMOVED PREVIOUS REPAIR AND REPAIRED AFT FLAP REF SRM 51-40-20 PAR 7, 14, 15, 18, 21, 22. PRIMED AND PAINTED REPAIR REF MM 51-201Jun 14, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02132Skin · misrepairedON AGING A/C INSP, FOUND FWD RT CORNER OF AIR STAIR CUTOUT DID NOT CONFORM TO FED EX DWG SR27-53-024. REMOVED OLD DOUBLER, HFEC INSP TO VERIFY CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER REF, FED EX DWG 27-53-024.Jun 14, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02120Floorbeam · corrodedCABIN BS 620, FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE, LBL 37 TO LBL 42 REMOVED CORROSION, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS =.135, REMOVED .013". FLAP PEENED BLENDED AREA. TREATED AND PRIMED AND APPLIED CORROSION INHIBITOR. REF SRM 51-10-2Jun 13, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02119Floorbeam · corrodedCABIN BS 620 FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE FROM LBL 3 TO LBL22 REMOVED CORROSION, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS= .135". REMOVED .017" FLAP PEENED BLENDED AREA, TREATED AND PRIMED AND APPLIED CORROSION INHIBITOR. REF SRM 51-10-6,Jun 13, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02096Web · gougedAGING A/C INSP. FOUND REPAIR LOCATED AT BS 620 FWD LOWER CARGO DOOR AFT FRAME FWD SURFACE UPPER CORNER, HAS ADDITIONAL DAMAGE ON AFT SIDE. REMOVED EXISTING REPAIR REF SRM 51-30-2. BLENDED DAMAGE AREA, ORG. THICKNESS .071, AFTER BLENDING, THICKNESS .064" TOJun 9, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02095Tab · dentedLWR RUDDER TAB LT SIDE HAS SPOT OF SURFACE DAMAGE, 14" UP FROM BOTTOM AND 8" FWD FROM BACK EDGE. REPAIRED DAMAGE TO LOWER RUDDER TAB LT SIDE REF SRM 51-40-9 PARA 3D. APPLIED CONDUCTIVE COATING REF MM 51-20-051-7. APPLIED PRIMER AND PAINT REF MM 51-20-151-7Jun 8, 2007 · N286FE · Boeing 727233 · Rudder Tab Control SystemSDR 07FDEA02085Skin · damagedRT LOWER FUSE STA 380-387 STR 23R, 3 LIGHTNING STRIKES. REMOVED LIGHTNING STRUCK RIVETS, HFEC FOUND CRACKS AROUND RIVET HOLES AND SKIN. REMOVED DAMAGE, SECOND TIME HFEC FOUND NO CRACKS. FAB`D DOUBLER, DRILLED AND INSTALLED, PRIMED AND PAINTED IN REF TO SRM Jun 7, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR CA070608007Bypass Valve · failed(CAN) ON ARRIVAL, THE IB FLAPS FAILED TO EXTEND WHEN LANDING, CONFIGURATION SELECTED. THE CREW ELECTED TO DIVERT. THE AIRCRAFT COMPLETED A NORMAL LANDING. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND INSPECTED THE SYSTEM FOR LEAKS AND ANOMALIES. THE FLAJun 4, 2007 · Boeing 727233 · Hydraulic Power SystemSDR 07FDEA02051Skin · delaminatedRT INBD FOREFLAP T/E IS DELAMINATED 36" FROM INBD END. REPAIRED DELAMINATION REF SRM 51-40-21 PG 1 AND 2, TAP TEST GOOD.Jun 2, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02040Skin · misrepairedON AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX STD REWORK DWG SR27-53-024. REMOVED OLD DOUBLER SRM 51-30-2, HFEC VERIFY OF CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER PER DWG SR27-53-024, TREATED AND PRIMED DOUBLER REF MM 51-20-151-7. INSJun 1, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA01847Skin · delaminatedFOUND REPAIR LOCATED AT RT O/B FOREFLAP LWR SURFACE I/B END ON AGING A/C INSP. EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20. REPAIRED RT O/B FOREFLAP AREA REF SRM 51-40-20 PARA 14-20, 21, 22.May 18, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA01818Line · failedAFTER TOUCHDOWN AMD SPOILER DEPLOYMENT, EXPERIENCED LOSS OF "A" HYDRAULIC SYSTEM QUANTITY AND PRESSURE. FOUND BLOWN FLEX LINE ON LT ELEVATOR PCU. PART IS IN STOCK AT SAV. REMOVED AND REPLACED I/B FLEX LINE PER MM27-30-081-4. SERVICED "A" HYD SYS TO FULL PEMay 15, 2007 · N273FE · Boeing 727233 · Hydraulic System, MainSDR 07FDEA01782Rib · crackedCOMPLY WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND (94-07-08) MAIN FRAME -RIB REPAIR EO 7-5710-7-2308. COMPLIED WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND AD 94-07-08)MAIN FRAME-RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2.May 14, 2007 · N221FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA01781Rib · crackedRT WINGS, RIB AT BL 70-5 FASTENER INSP DURING "B" CHECK CRACK INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1R. REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57-10/0313.May 14, 2007 · N221FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA01780Rib · crackedLT WINGS, RIB UPPER CORD AT BL 70-5 FASTENER INSP. DURING "B" CHECK, CRACKED INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1L . REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57-10/May 14, 2007 · N221FE · Boeing 727233 · Leading Edge DevicesSDR 07FDEA01766Rib · damagedCOMPLY WITH E.A. 7-5710-110741-WING (AD 90-06-09:94- 87-08;98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 7-5710-110741 WING (AD90-06-09-94-0 7-08, 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 5710-110741 WMay 12, 2007 · N221FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA01733Electrical Sys · contaminatedAT ROTATION, ESSENTIAL POWER FAIL LIGHT CAME ON MOMENTARILY THEN WENT OUT WITH NR 1 GENERATOR FAIL. UNABLE TO BRING NR 1 BUSSSM20ACD200A2 ON LINE. LOST THE FOLLOWING: CAPT'S INST LIGHTS, PITCH TRIM, ASYM FLAPS, NR 1 EPR WITH PACKS TRIPPED, NR 1 OIL TEMP WEMay 9, 2007 · N282FE · Boeing 727233 · AC Power Distribution SystemSDR 07FDEA01674Throttle Cable · shearedNR 1 THROTTLE BINDS 2/3 THROUGH TRAVEL. FOUND NR 1 THROTTLE CABLE BROKEN IN BELLY. LOOSE CABLE COILED IN AVIONICS BAY. FOUND THROTTLE CABLE (T1B) BROKEN AT STA 673, REMOVED FWD AND AFT CARGO CEILING PANELS FOR ACCESS TO CABLE RUN "K" FROM STA 450 TO 980. Apr 29, 2007 · N267FE · Boeing 727233 · Power LeverSDR 07FDEA01527Rib · crackedCOMPLY WITH EA 7-5710-102033 WINGS (AD 90-06-09 AND AD 94-07-08) MAIN FRAME - RIB REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-102033 (AD90-06-09 AND AD 94-07-08) RIB REPAIR EO 7-5710-7-2308 PART 2.Apr 18, 2007 · N223FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA01524Web · crackedWEB AT STA 760-780 RBL65-70.5 IS CRACKED STR 17R 3 " CRACK FABRICATED WEB ON TRAVELER T7/671242 AND SRM 51-10-1. INSTALLED ON NR S00009.Apr 18, 2007 · N223FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA01521Wire · damagedFERRY FLIGHT AFTER RAISING GEAR HANDLE UP HAD UNSAFE NOSE GEAR RED LIGHT. CYCLED GEAR IAW QRH UNSAFE NOSE GEAR LIGHT REILLUMINATED. ALL DOORS INDICATED SAFE. CONTINUED FLIGHT WITH GEAR HANDLE UP. TROUBLESHOT SYSTEM IAW WDM 32-64-01 FOUND BAD SPLICE IN WIREApr 17, 2007 · N223FE · Boeing 727233 · Landing Gear System WiringSDR CA070413002Cylinder · failed(CAN) THE CREW OBSERVED AN A SYSTEM DEPLETION CONDITION AFTER EXTENDING THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NOSE LANDING GEAR SYSTEM TRANSFER CYLINDER HAD FAILED. THE CYLINDER HAD FAILED AT THE LAST END CAP THREApr 9, 2007 · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 07FDEA01346Arm · failedFORWARD ENTRY DOOR OPENED UPON TOUCHDOWN. AFTER FURTHER INSP FOUND THE UPPER GUIDE ARM WORN CAUSING THE DOOR OPEN LOCK NOT TO WORK AND DOOR HARD TO CLOSED. REMOVED AND REPLACED THE UPPER GUIDE ARM IAW 727 M/M 52-11-001-5. OPS CHECK GOOD OF THE DOOR OPERATIOApr 4, 2007 · N220FE · Boeing 727233 · Passenger/Crew DoorsSDR 07FDEA01223Relay · failedFIRE WARNING MASTER LIGHTS ILLUMINATED, INTERMITTENTLY, WITH AUDIO BELL. NO OTHER INDICATIONS. REMOVED AND REPLACED R97 RELAY AND M438, REF WIRING DIAGRAM MANUAL 49-41-01 PAGE 3. NEEDS OPS CHECKS. REF MM 26-15-000, OP CHECK APE FIRE SYSTEM. CHECKS OK.Mar 31, 2007 · N283FE · Boeing 727233 · Smoke DetectionSDR 07FDEA01137Drive Unit · leakingDESCENDING THROUGH 10,000 EN ROUTE TO KTPA, EXPERIENCED HYDRAULIC SYSTEM "A" LOSS O QUANTITY FOLLOWED BY BOTH PUMP LIGHTS ILLUMINATED. SYSTEM "A" FLUID SHUTOFF SWITCHES WERE CLOSED FOR 20 MINUTES. REMOVED AND REPLACED FLAP POWER UNIT HYD MOTOR PER M/M 27-51Mar 27, 2007 · N285FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 07FDEA01003Actuator · leakingSHORT FINAL, LOSS OF A SYSTEM, LANDED STRAIGHT AHEAD. TOWED IN. AFTER T/S FOUND NR 2 L/E FLAP ACTUATOR LEAKING. CANCELED FIRST PART. REMOVED AND REPLACED NR 2 LE FLAP ACT IAW M/M 27-81-022-4. SERVICED HYD SYSTEM PER 12-12-000-2.Mar 18, 2007 · N274FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 07FDEA00910Door · unsecureAFTER TAKEOFF IN IAD CABIN ALTITUDE WENT ABOVE 10,00 0' RAN QRH PROCEDURES CABIN ALTITUDE WENT TO 11,500' WENT ON O2 RETURNED TO IAD. NOTICE FORWARD ENTRY DOOR WAS NOT SEATED PROPERLY OPEN AND SECURED DOOR SEVERAL TIMES, PERFORMED FORWARD ENTRY DOOR INSPECTMar 15, 2007 · N269FE · Boeing 727233 · Passenger/Crew DoorsSDR 07FDEA00631Hydraulic System · dischargedHYD "A" SYSTEM DEPLETED W/FLAPS SELECTED TO 2 ON APPROACH ON 27 MEM. NR 2 "A" PUMP LIGHTS ON FOR 2-3 MINS, FLUID SHUTOFF SWITCHES OF 2-3 MINS.Mar 3, 2007 · N218FE · Boeing 727233 · Hydraulic System, MainSDR PCSA21820071Uplock · crackedFLIGHT 8714 WHILE ON TAXI FROM THE GATE AT SAP THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED AND WARNING HORN SOUNDED. THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOOT THE INDICATION PFeb 18, 2007 · N994AJ · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 07FDEA00523Accessory Unit · failedDURING GEAR RETRACTION, AN AUDIO HORN SOUNDS WITH A CORRESPONDING RED GEAR LIGHTS AND RED DOOR LIGHT. NOTE: RED DOOR LIGHT EXTINGUISHES AFTER AN APPROPRIATE TIME. BEFORE TAKEOFF, AIRCREW CYCLED FLAPS TO 30 DEGREES AND BACK TO 15 DEGREES. TRIED SAME SEQUFeb 18, 2007 · N284FE · Boeing 727233 · Landing Gear Position and WarningSDR 07FDEA00519Module · faultyON TAKEOFF WHEN GEAR RETRACTED, RED DOOR AND ALL RED GEAR LIGHTS WITH GEAR WARNING HORN. DOORS LIGHT EVENTUALLY GO OUT, BUT RED GEAR LIGHTS AND AURAL HORN STAYS ON. TROUBLESHOT SYSTEM REF MM 32-61-001-1. REPLACED LGAU MODULE REF MM 32-09-121-4. LANDING GEAFeb 17, 2007 · N284FE · Boeing 727233 · Landing Gear Position and WarningSDR 07FDEA00439Hinge Pin · damagedMAIN CARGO DOOR HINGE PIN HAS A .2 INCH GAP BETWEEN THE RETENTION NUT AND WASHER ON THE AFT END OF THE HINGE (PIN CRACKED/BROKEN). INSTALLED NEW HINGE PIN UPON DOOR INSTALL REF MM 52-34-009-4-1 PAGE 1, MM 52-34-009- 5 PAGE 1, NASI SUP FXV-727-MM14 CLASSIFIEFeb 9, 2007 · N284FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA00431Sill · corrodedFOUND MAIN DECK 1R DR CUTOUT LWR SILL CREASE BEAM SCUFF PLATE IB SUPPORT UPPER FLANGE IS CORRODED. BLENDED CORROSION, HFEC, NO DEFECTS NOTED. ALODINED AND PRIMED, REF EA NR 7-5310-106989, PART 1.Feb 9, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00388Web · tool damageMAIN CARGO DOOR UPPER AFT CORNER WEB BS.590-640 HAS MULTIPLE TOOLING MARKS ON INNER SURFACE REMOVED GILL LINER AND PARTIALLY REMOVED INNER SKIN WEB FOR ACCESS. REMOVED REPAIR DOUBLER REF SRM 51-30-2, CUT OUT DAMAGE AREA REF. 51-10-1 HFEC CUT OUT, IAW B727 NDTFeb 8, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
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