N27190

Part: CONTROL UNIT — INOPERATIVE (ZONE 300) · airframe 42,738 hrs · 29,463 cycles

PITCH TRIM INOPERATIVE MESSAGE AT V1. REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT. OPS/INDICATION CHECK SAT.

Part: SKIN — CRACKED (ZONE 100) · airframe 42,459 hrs · 29,205 cycles

FF1 RH SKIN CRACKED AT FR 4 AND EDGE OF SKIN AT NLG CUTOUT. REPAIR DOUBLER ON RH FWD FUSE I SKIN, AT FR 4 AND ON LOWER EDGE.

Part: SKIN — CRACKED (ZONE 200) · airframe 42,459 hrs · 29,205 cycles

EXTERNAL REAR FUSELAGE SKIN, DENT FOUND 8 INCHES AFT FRAME 77, BTW STR 14L-15L. REPAIR DOUBLER ON LH REAR FUSE II SKIN, BTW FR 77-80 AND BTW STR 13L-16L

Part: FITTING — CRACKED (ZONE 800) · airframe 42,459 hrs · 29,205 cycles

ON BAGGAGE DOOR LIFTING AND LOWERING MECHANISM, FWD AND AFT SUPPORTS FOUND WITH CRACKS. BAGGAGE DOOR LIFTING AND LOWERING MECHANISM REMOVED FOR ACCESS. ON BAGGAGE DOOR LIFTING AND LOWERING MECHANISM FWD SUPPORT ANGLE REMOVED FOR REPLACEMENT. ON BAGGE DOOR LIFTING AND LOWERING MECHANISM, AFT SUPPORT (2) REMOVED FOR REPLACEMENT. ALL PARTS REMOVED WERE REPLACED WITH NEW PARTS. BAGGAGE DOOR LIFTING AND LOWERING MCHANISM INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 42,459 hrs · 29,205 cycles

CF1, SHEAR CLIP ON FR15 BTW STR 15R-16R FOUND CRACKED. CF1, ON EXTERNAL SKIN AT FR 15 BTW STR 15R-16R REMOVED AND REPLACED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CENTER FUSELAGE IV. LH SILL CORRODED BTW FRAME 60-61. CENTER FUSELAGE IV, LH SILL CORRODED BTW FRAME 60-61 BLENDED OUT OF LIMIT. CENTER FUSELAGE IV, LH SILL AT FR 60-61 REMOVED AND REPLACED

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

RH SIDEWALL SEAT TRACK BTW FR29-30 BLENDED OUT OF LIMITS. R/H SIDE WALL SEAT TRACK BTW FR29-30 REMOVED AND REPLACED.

Part: WEB — CRACKED (ZONE 600) · airframe 42,459 hrs · 29,205 cycles

RH AFT MLG WEB CRACKED. RH AFT MLG WEB REPLACED.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

LH FLOOR SAT TRACKS BTW FR31-32 FLENDED OUT OF LIMITS. L/H FLOOR SEAT TRACK BTW FR30-31 AND FR41-32 REOVED AND REPLACED.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CF1, CENTER CROSSBEAM AT FR20 FOUND CORRODED. CF1 CENTER CROSSBEAM AT FR20 BLENDED AND FOUND OUT OF LIMIT. CF1 CENTER CROSSBEAM AT FR20 INSTALLED

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

RIGHT SIDE SILL BTW FR 22-24 FOUND CORRODED. CF1, RH SIDE SILL BTW FR 22-24 BLENDED OUT OF LIMIT. SILL REMOVED AND REPLACED.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL FOUND CORRODED. CF1, SERVICE DOOR CUT OUT, ENTRANCE CHANNEL BLENDED OUT OF LIMIT. CF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL REMOVED FOR REPLACEMENT. CF1, SERVICE DOOR CUT-OUT, ENTRANCE CHANNEL REPLACED.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 CORRODED OUT OF LIMITS CENTER FUSELAGE IV, CENTER GUSSET BTW FR59-61 REPLACED.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CENTER FUSELAGE IV, RH GUSSET BTW FRAME 59-61 CORRODED. R/H GUSSET BLENDED OUT OF LIMITS. TH GUSSET BTW FR59-61 REMOVED FOR REPLACEMENT. CENTER FUSELAGE IV, R/H GUSSET BTW FR 59-61 REPLACED.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

CENTER GUSSET BTW FR18-24 FOUND CORRODED. CF1 CENTER GUSSET BTW FR18-24 BLENDED AND FOUND OUT OF LIMITS. CF1, CENTER GUSSET BTW FR18-24 REMOVED. CENTER GUSSET BTW FR18-24 REPLACED.

Part: ANGLE — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

RIGHT INBD FLAP INBD TIP, ONE ANGLE IS CORRODED. RT INBD FLAP INBD TIP, ONE ANGLE BLENDED OUT OF LIMITS. RH INBD FLAP INBD TIPO, ANGLE REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,459 hrs · 29,205 cycles

SHEAR CLIP ON FR16 BTW STR15R-16R FOUND CRACKED. REMOVED AND REPLACED CF1 SHEAR CLIP ON FR16 BTW STR15R-16R.

Part: BRACKET — CRACKED (ZONE 200) · airframe 42,459 hrs · 29,205 cycles

AFTER GUSSET REMOVAL, ANGLE BRACKET FOUND CRACKED BTW FR 20-21 ON CENTER BEAM HAT SECTION AT FR 20-21 ANGLE REMOVED FOR REPLACEMENT. ANGLE BRACKET REPLACED WITH MADE REPAIR PART INLAY FABRICATED. INSTALLED. FLUORESCENT PENETRANT INSPECTION CARRIED OUT ON LOCALLY FABRICATED PART. NO CRACK INDICATION FOUND.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 42,459 hrs · 29,205 cycles

FR30 BTW STR15-16 SHEAR CLIP CRACKED FR30 BTW STR15-16 SHEAR CLIP REMOVED, FR30 BTW STR15-16 SHEAR CLIP REPLACED

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 42,459 hrs · 29,205 cycles

RH SILL BTW FR 41-48 FOUND CORRODED. CF3, RH SILL BTW FR 41-48 IS OUT OF LIMIT. CF3, RH SILL BTW FR 41-48 REMOVED AND INSTALLED.

Part: ENGINE — FAULTED (NR 1) · airframe 41,584 hrs · 28,391 cycles

ENG 1 SHUTDOWN IN FLIGHT. REMOVED AND REPLACED #1 ENGINE. OPS AND LEAK CHECK SAT.

Part: CONTROL UNIT — INOPERATIVE (BRAKE SYS) · airframe 40,875 hrs · 27,759 cycles

BRAKE OUTBOARD INOPERATIVE EICAS MESSAGE. BRAKES NOT ENGAGING 100% ON LANDING ROLL. LEFT INBOARD BRAKE TEMP IN YELLOW. FOUND NO BRAKE RELATED CMC MESSAGES. REMOVED ALL 4 HUB CAPS AND INSPECTED TRANSDUCERS, FOUND NO VIABLE FAULT, REINSTALLED HUB CAPS. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS AND LEAK CHECK SAT.

Part: STOP FITTING — MISSING (ZONE 800) · airframe 40,811 hrs · 27,707 cycles

MCD FWD TOP STOP MISSING, WITH SHIMS FELL OUT. FWD TOP STOP FOUND TO BE IN SERVICEABLE CONDITION. FOUND AFT MIDDLE STOP TO BE MISSING INSTEAD. INSTALLED AND ADJUSTED AFT MIDDLE STOP. PERFORMED PRESSURIZATION TEST. LEAK CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,864 hrs · 26,886 cycles

LAV SMOKE WARNING ON EICAS IN FLIGHT. INSPECTED AND PERFORMED OPS CHECK OF LAV LIGHTS AND BALLAST. OPS CHECK SAT, NO SINGS OF BURNING/DAMAGE. PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYSTEM. OPS CHECK SAT. UNABLE TO DUPLICATE FAULT AT THIS TIME. NO FAULTS FOUND. PERFORMED HIGH ENG RUNS. NO DEFECTS NOTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,859 hrs · 26,861 cycles

WHEN IN VISABLR MOISTURE ELECTRICAL SMELL THROUGHOUT CABIN IN COCKPIT CENTER FLOOR BOARD FELT WARM. FOUND EVIDENCE OF DE-ICING FLUID RESIDUE. CLEANED UP FLUID. NO ADDITIONAL DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,406 hrs · 26,433 cycles

EMERGENCY LIGHT LAMP ABOVE SERVICE DOOR INOPERATIVE. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM. LIGHT OPS CHECK GOOD.

Part: ACTUATOR — LEAKING (TE FLAPS) · airframe 39,265 hrs · 26,293 cycles

FLAP FAIL ON EICAS AFTER FLAPS RETRACTED. RETRACTING THE FLAPS FROM 9 TO 0 AND IMMEDIATELY RECEIVED FAIL AND THE INDICATION DASHED OUT AND KEPT THE AIRCRAFT BELOW 250 KNOTS. CREW REPORTED NO HARD OR OVERWEIGHT LANDING "REPLACED FPDU. REPLACED FECU. PERFORMED ZERO RIGGING ON BOTH L/H AND R/H FLAPS, OPS CHECK SAT. R/R FPDU OPS C/K FAIL. FECU FAIL MESSAGE ON CMC. R/R FECU DID NOT FIX . FLAP LOW SPEED AND FLAP FAIL MESAGES SHOW ON EICAS. R/R FECU.  OPS CHECK REVEALED NO ""FLAP LOW SPEED"" MESSAGE BUT ""FLAP FAIL"" MESSAGE ON EICAS REMAINS. FURTHER GVI ON R/H FLAP MECHANICAL SYSTEM REVEALED THE FFS SECTION 1 WAS UNDER SEVERE TENSION AT 45 DEGREES.  REMOVED FFS SECTION 1. REPLACED R/H FFS SECTION 1.  OPS CHECK SAT. INSPECTED R/H FFS SECTION 1 INSTALLATION, OPS CHECK SAT PERFORM THE FLAP ZERO RIG. PERFORMED THE FLAP ZERO RIGGING.OPS CHECK SAT. INSP THE FLAP ZERO RIGGING. OPS CHECK SAT. PERFORMED BOTH L/H AND R/H FLAP ZERO DEGREE RIGGING, OPS CHECK SAT. INSPECTED  BOTH L/H AND R/H FLAP ZERO DEGREE RIGGING, OPS CHECK SAT. R/H INBD FLAP ROOT ACTUATOR LEAKING. REPLACED R/H INBD FLAP ROOT ACTUATOR AND ANGLE GEAR BOX AND C/W BOTH L/H AND R/H ZERO RIGGING. C/W INSTALLATION INSPECTION OF R/H INBD FLAP ROOT ACTUATOR AND GEAR BOX OPS CHECK GOOD AND C/W RIGGING INSP. PERFORMED R/H INBD FLAP ACTUATOR OPS CHECK, OPS CHECK SAT. INSPECTED  R/H INBD FLAP ACTUATOR OPS CHECK, OPS CHECK SAT. FLAP MOTOR DRIVE UNIT NOT WORKING PROPERLY. R/R FPDU.  OPS CHECK AND FOLLOW ON REQUIRED. PERFORMED OPS CHECK ON FPDU AND PERFORMED ZERO RIGGING ON BOTH L/H AND R/H FLAPS, OPS/RIGGING CHECK SAT. INSPECTED OPS CHECK OF FPDU AND PERFORMED ZERO RIGGING ON BOTH L/H AND R/H, OPS/RIGGING CHECK SAT.

Part: NONE — NONE · airframe 37,650 hrs · 24,839 cycles

FOUND COCKPIT STEP EMERGENCY EXIT LIGHT INOPERATIVE. FOUND HARNESS FOR COCKPIT STEP EMERGENCY LIGHT DISCONNECTED. RECONNECTED HARNESS. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE · airframe 37,495 hrs · 24,695 cycles

BOTH FWD WTF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS #1 AND #2. OPS CHECK SAT FOR #1. OPS CHECK FAILED FOR #2. PART BAD FROM STOCK. REMOVED AND REPLACED #2. OPS CHECK SAT.

Part: NONE — NONE · airframe 37,487 hrs · 24,688 cycles

AT REAR FUSE II EXT, SUSPECTED CRACKS (7X) FOUND ON RH SIDE SKIN BTW FR 77-FR80 AND BTW STR 3R-9R. AFTER INVESTIGATION 7 SUSPECTED CRACKS CONFIRMED. FRAME 77 BTW STR 3R-4R TWO CRACKS TOO CLOSED REPAIRED WITH DOUBLER. (X5) BUSHING LOCALLY FABRICATED )MADE REPAIR PARTS). BUSHING REPAIR (5X) INSTALLED ON RH SKIN BEWTEEN FR 77-FR80 AND BTW STR 3R-9R. REPRODUCTION ON FUSELAGE RH OUTER SKIN AT FR 77-80 BTW STR 3R-9R

Part: NONE — NONE · airframe 37,487 hrs · 24,688 cycles

AT REAR FUSE EXT, DAMAGE FOUND ON BELLY SKIN BTW FR73-74 AND BTW STR 19L-19R. RH REAR FUSELAGE #1 SKIN BTW FR72-76 AND BTW STR 16R TO 20L REMOVED AND SPLICED. NEW SKIN SECTION LOCALLY FABRICATED. RH REAR FUSELAGE #1 SKIN BTW FR77 - FR 76 AND BTW STR 16R-20L REPAIRED WITH MADE REPAIR PART FOR SKIN SECTION AND SPLICE DOUBLER AND INSTALLED WITH SOLID RIVERS AND HI-LOK.

Part: NONE — NONE · airframe 37,487 hrs · 24,688 cycles

CIRCULAR DOUBLER AT FWD BULKHEAD TO BE REMOVED FOR REPAIR MAPPING. DOUBLER AT FWD BULKHEAD REMOVED FOR INVESTIGATION. CIRCULAR DOUBLER AT FWD BULKHEAD REPLACED WITH MADE REPAIR PART, LOCALLY FABRICATED.

Part: NONE — NONE · corrosion level 2 · airframe 37,487 hrs · 24,688 cycles

AT CFII, CORROSION FOUND ON LOWER STR 21R BTW FR50-51 IN U/FLOOR AREA. LOWER STR 21R BTW FR50-51 IN UNDERFLOOR AREA FOUND BADLY CORRODED. LOWER STR 21R BTW FR 50-51 IN UNDERFLOOR AREA REPLACED.

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM) · airframe 37,246 hrs · 24,483 cycles

PITCH TRIM BACKUP INOPERATIVE ON EICAS IN FLIGHT. R&R HSCU. ADJUSTMENT TEST CARRIED OUT. REPLACED HAS. OPS CHECK SAT.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 37,246 hrs · 24,483 cycles

PITCH TRIM BACKUP INOPERATIVE ON EICAS IN FLIGHT. R&R HSCU. ADJUSTMENT TEST CARRIED OUT. REPLACED HAS. OPS CHECK SAT.

Part: ARMREST — CRACKED (SEAT) · airframe 36,992 hrs · 24,266 cycles

FOUND CRACK IN PAX SEAT ARMREST AT 3A, 4A, 5A, 6A, 7A, 9A, 10A. RR PAX SEAT 3A, 4A, 5A, 6A, 7A, 9A, 10A.

Part: ANTI-ICE VALVE — CRACKED (NR 2 ENGINE) · airframe 36,819 hrs · 24,101 cycles

ENG A/I FAIL, NO ICE ON, AND BLEED 1 LOW TEMP MESSAGES IN FLIGHT (E2 E/I FAIL WITH NO ICE A/I ON MESSAGES ON CLIMB FROM FL220 TO FL270. BLEED 1 LOW TEMP CAME ON AT 3000 FEET ON APPROACH WITH N1 AT 70% AND N2 80-85%. PERFORMED A/I ADJUSTMENT TEST. OPS CHECK SAT. INSPECTED FAN AIR VALVE FILTER. FOUND FILTER TO BE CLEAN AT THIS TIME. PERFORMED GVI OF ENGINE #2 A/I VALVE AND FOUND A SECTION OF THE VALVE CRACKED. #2 ENGINE A/I VALVE REQUIRES REPLACEMENT. FOUND RESISTOR RO534 BROKEN, NOTE THIS RESISTOR TIES TO THE PRECOOLER TEMP INDICATION FOR #1 BLEED TEMP. R&R RESISTOR RO534. OPS CHECK SAT. REPLACED #2 ENGINE AI VALVE. OPS CHECK SAT AT THIS TIME. LOTO REMOVED AND STOWED.

Part: NONE — NONE · airframe 37,487 hrs · 24,688 cycles

AT CF I EXT, DENT FOUND ON LH SIDE SKIN BTW FR 19 - FR 20 AND BTW STR 11L-12L. AT CFI EXT, BTW FR 19-20 BTW STR 11L-12L, SKIN REPAIRED

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,027 hrs · 23,349 cycles

EMERGENCY LIGHTS AT MAIN DOOR, MAIN ENTRANCE CEILING PANEL, COCK PIT FLOOR, GALLEY ISLE CEILING PANEL AND FWD WING-TO-FUSE, AND EMERGENCY EXIT SIGNS AT COCKPIT BULKHEAD, COCKPIT STEP, AND GALLEY CENTER AISLE CEILING INOP (8 LIGHTS TOTAL). R&R #1 EMERGENCY LIGHT BATTERY PACK. OPS CHECK SAT

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,016 hrs · 23,339 cycles

LH FWD OF WING EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R LH FWD OF WING EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,016 hrs · 23,339 cycles

SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 34,491 hrs · 21,968 cycles

AIRCRAFT UNCOMMANDED LEFT ROLL TWICE DURING DESCENT, WITH & WITHOUT AP ON. INADVERTENT SPOILER OPEN QRH PERFORMED, NO ROLL ISSUES AFTER CB F13, F14 & F21 WERE PULLED. PERFORMED FIM 27-63-00-810-802-A. FOUND TO BE IN TRANSITORY CONDITION. NO FURTHER DEFECTS NOTED OR CMC MESSAGES.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 34,490 hrs · 21,967 cycles

HYD 2 LOW QTY ON EICAS. R&R HYD PUMP. OPS CHECK SAT. LEAK CHECK GOOD.

Part: CONNECTOR — DAMAGED (NLG DOWNLOCK) · airframe 34,409 hrs · 21,881 cycles

FAILED OCF, LANDING GEAR DISAGREEMENT, ALL GEAR WOULD NOT RETRACT. TROUBLESHOT PROXIMITY SWITCHES AND HARNESS. FOUND NLG DOWN LOCK A CONNECTOR P4661 WITH PUSHED PIN. RE-SEATED PIN IN CANNON PLUG. PERFORMED PROXIMITY SWITCH FUNCTIONAL CHECK. OPS CHECK GOOD. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 34,408 hrs · 21,879 cycles

UPON REMOVAL OF FLOOR GUSSET, FOUND THE CENTER OMEGA BEAM HAS MULTIPLE AREAS OF CORROSION FR 59-61. FABRICATED AND INSTALLED OMEGA BEAM REPAIR DOUBLERS ON CENTER OMEGA BEAM AT FR59 AND FR61.

Part: YOKE — DAMAGED (RT PYLON) · airframe 34,408 hrs · 21,879 cycles

RT PYLON FWD YOKE UPPER FLANGE FASTENER HOLE SHOWS DAMAGE INDICATIONS BY THE HFEC ROTATIVE DRIVE INSPECTION METHOD. COMPLETED INSTALLATION OF FASTENER AT RIGHT PYLON FWD YOKE UPPER FLANGE.

Part: STRUCTURE — DAMAGED (FRAME 61) · airframe 34,408 hrs · 21,879 cycles

LEFT SIDEWALL OF THE INTERNAL STRUCTURE HAS ELONGATED HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 05L - 06L WHILE PICKING UP THE RIVET HOLES FOR REPAIR. REPAIRED LEFT SIDEWALL INTERNAL STRUCTURE ELONGATED HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 05L-06L BY CUT OUR, FILLER AND "L" ANGLE DOUBLER FABRICATION AND INSTALLATION

Part: SIDEWALL PANEL — DAMAGED (FRAME 61) · airframe 34,408 hrs · 21,879 cycles

LEFT SIDEWALL OF THE INTERNAL STRUCTURE HAS HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 11L-12L IN A REPAIR DOUBLER AND THE EDGE OF THE SHEAR CLIP. REMOVED, FABRICATED, AND REPLACED EXISTING REPAIR DOUBLER, PLUGGED HOLE AND BLENDED SLIGHT EDGE DAMAGE ON SHEAR CLIP AT LEFT SIDEWALL OF THE INTERNAL STRUCTURE ON FRAME 61 STRINGER 11L-12L

Part: PANEL — DAMAGED (STAB) · airframe 34,408 hrs · 21,879 cycles

UPON REMOVAL OF EROSION TAPE FOUND COMPOSITE DAMAGE ON PANEL 333DL. REPAIRED COMPOSITE DAMAGE AND RESTORED SURFACE PROTECTION ON PANEL 333DL.

Part: SHEAR TIE — DAMAGED (FRAME 68) · airframe 34,408 hrs · 21,879 cycles

CRACKED/BROKEN SHEAR CLIP AT FRM 68 STRINGERS 05R - 06R. REMOVED AND REPLACED CRACKED / BROKEN SHEAR CLIP AT FRM 68 STRINGERS 05R - 06R

Part: SKIN — CORRODED (FRAMES 18-19) · airframe 34,408 hrs · 21,879 cycles

UNDERFLOOR AREA SKIN HAS CORROSION AS MARKED BETWEEN FRAME 18-19 STRINGERS 21L-21R. REPAIRED UNDERFLOOR AREA SKIN CORROSION BETWEEN FRAME 18-19 STRINGERS 21L-21R BY BLEND OUT AND CUT OUT, FILLER AND DOUBLER FABRICATION AND INSTALLATION

Part: SHEAR TIE — CORRODED (FRAME 62) · airframe 34,408 hrs · 21,879 cycles

SHEAR CLIP CORRODED FR62 STR 20-19R. REMOVED AND REPLACED SHEAR CLIP BETWEEN FR62 STR 20-19R

Part: SHEAR TIE — CORRODED (FRAME 62) · airframe 34,408 hrs · 21,879 cycles

SHEAR CLIP CORRODED FR62 STR 21-20R. REMOVED AND REPLACED SHEAR CLIP BETWEEN FR62 STR 21-20R

Part: SLEEVE — BROKEN (NR 2 ACM) · airframe 34,185 hrs · 21,674 cycles

CABIN PRESSURIZATION RISING 2800' PER MINUTE WHILE CRUISING AT 17K. FOUND A BROKEN SLEEVE CONNECTING TO THE #2 ACM. R&R SLEEVE.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 33,441 hrs · 21,002 cycles

PITCH TRIM MAIN INOP WARNING CAME ON BETWEEN 10000 AND 14000 FEET. AUTOPILOT ON. REMOVED HORIZONTAL STAB ACTUATOR. INSTALLED HORIZONTAL STAB ACTUATOR. PERFORMED OPS CHECK. OPS CHECK SAT.

Part: ROLLER — BINDING (NLG DOOR) · airframe 33,369 hrs · 20,932 cycles

NOSE L/G DOOR DIDN`T RETRACT ON GEAR UP COMMAND,RAN QRH NOSE GEAR DOOR RETRACTED. FOUND UPLOCK ROLLER TO NOT MOVE FREELY. REMOVED, CLEANED AND REINSTALLED. OPS CHECK SAT

Part: SKIN — CORRODED (FRAMES 65-68) · airframe 30,083 hrs · 18,195 cycles

REAR FUSELAGE BETWEEN FRAMES 65 - 68 AND STRINGERS 21R-21R CORRODED UNDER BOTH AFT RADIO ALTIMETER ANTENNAS. AFT RADIO ANTENNA BASES WERE REPLACED IAW SRM 51-40-02. SKIN UNDER RADIO ANTENNA BASE WAS REPAIRED IAW ETD2017-145-018880.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 30,083 hrs · 18,195 cycles

CARGO DOOR SURROUND STRUCTURE LOWER BEAM CORRODED AT FRAME 66. LOWER BEAM AND ANGLE REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 52-59) · airframe 30,083 hrs · 18,195 cycles

BETWEEN FRAMES 52 AND 59 LT OTBD FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: ANGLE — CRACKED (CABIN) · airframe 30,083 hrs · 18,195 cycles

LEFT OUTBOARD OMEGA BEAM ANGLES CRACKED. THE ANGLES WERE REPLACED IAW SRM 53-23-02 AND ETD2017-145-017058A.

Part: PLATE — DAMAGED (FRAME 31) · airframe 30,083 hrs · 18,195 cycles

AT THE JUNCTION OF FRAME 31 AND RT FLOORBEAM, THE FLOOR SUPPORT PLATE WAS FOUND DAMAGED. THE FLOORBEAM SUPPORT PLATE WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 30,083 hrs · 18,195 cycles

FLOOR SUPPORT BETWEEN FRAMES 24 AND 25 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FRAME 15) · airframe 30,083 hrs · 18,195 cycles

ON PAX DOOR SURROUND AT FRAME 15 BETWEEN STRINGERS 15-16L REINFORCEMENT ANGLE FOUND CRACKED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 47-53) · airframe 30,083 hrs · 18,195 cycles

BETWEEN FRAMES 47 AND 53 LT FLOOR SUPPORT NR 6 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW 51-40-02.

Part: ANGLE — CORRODED (FRAMES 49-50) · airframe 30,083 hrs · 18,195 cycles

BETWEEN FRAMES 49 AND 50 CLOSING ANGLE CORRODED. CORROSION REMOVED IAW SRM 51-10-03.

Part: FLOORBEAM — CORRODED (FRAME 59) · airframe 30,083 hrs · 18,195 cycles

FLOORBEAM CORRODED AROUND ANCHOR NUT AT FRAME 59. REPAIRED THE FLOORBEAM. DOUBLER INSTALLED IAW SRM 53-24-10 PARA 3. HFEC INSPECTION PERFORMED ON REPAIRED AREA WITH NO FAULTS FOUND.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 30,083 hrs · 18,195 cycles

FLOOR SUPPORTCORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 30,083 hrs · 18,195 cycles

BETWEEN FRAME 59 AND 61 RT OUTBOARD FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

LT OMEGA BEAM FOUND CORRODED BETWEEN FRAME 23-23. LT OMEGA BEAM REPAIRED AS PER SRM 53-21-10 ITEM 7 FIG 206. SHEET 2, HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT FOUND.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

CF3 BETWEEN FRAME 35 AND 41. RT SILL 3 CORRODED. SILL REPLACED AS PER SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

RT SILL 5 BETWEEN FR 48 AND FR 52 CORRODED. RT SILL 5 REPLACED AS PER SRM 51-40-02.

Part: RIB — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

CARGO DOOR SURROUND STRUCTURE FWD FLOOR SIDE PLATE AT FRAME 65 CORRODED. RIB REPLACED AS PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

LT OMEGA BEAM FOUND CORRODED BETWEEN FRAME 23-23. LT OMEGA BEAM REPAIRED AS PER SRM 53-21-10 ITEM 7 FIG 206. SHEET 2, HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT FOUND.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

CF3 BETWEEN FRAME 35 AND 41. RT SILL 3 CORRODED. SILL REPLACED AS PER SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,097 hrs · 18,204 cycles

RT SILL 4 BETWEEN FR 41 AND FR 48 CORRODED. RT SILL 4 REPLACED AS PER SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,904 hrs · 17,333 cycles

EMERGENCY LIGHTS REPORTED INOPERATIVE. MX CHARGED EMERGENCY LIGHT BATTERIES AND OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,109 hrs · 16,719 cycles

DURING ROUTINE MAINTENANCE, THE FORWARD CENTER OVERHEAD EMERGENCY SIGN WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AND OPS CHECKS WERE GOOD.

Part: SKIN — DENTED (FRAMES 73-74) · airframe 27,606 hrs · 16,365 cycles

A DENT WAS DISCOVERED BEHIND THE CARGO DOOR BETWEEN FRAMES 73-74 STRINGERS 12L-13L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-31-01 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — FAILED (APU) · airframe 24,456 hrs · 14,223 cycles

PILOT REPORTED AN APU GENERATOR FAIL MESSAGE WITH STRONG ELECTRICAL ODOR. FOUND APU STARTER/GENERATOR INOPERATIVE.

Part: WIRE HARNESS — SHORTED (APU) · airframe 24,456 hrs · 14,223 cycles

SUP: ORIGINAL REPORT SDR PILOT REPORTED AN APU GENERATOR FAIL MESSAGE WITH STRONG ELECTRICAL ODOR. MAINTENANCE R & R APU ELECTRICAL HARNESS ASSY, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 23,042 hrs · 13,323 cycles

THE CREW REPORTED THE ACFT FILLED WITH SMOKE AT APPROXIMATELY 12000 FT, ALONG WITH LAVATORY SMOKE ALARM. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 22,876 hrs · 13,221 cycles

THE CREW REPORTED SMOKE IN CABIN, AIR RETURN. REPORTED SMOKE CLEARED ON APPROACH. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS OF BLEED AIR SYSTEM IAW 36-00-00. NO SMOKE IN CABIN OR COCKPIT NOTED.

Part: WIRE — CHAFED (FIRE LOOP) · airframe 22,018 hrs · 12,666 cycles

CREW REPORTED AN NR 2 ENGINE FIRE DETECT FAIL MESSAGE IN FLIGHT ON EICAS. MX REPAIRED CHAFED WIRE TO FIRE LOOP CONNECTOR. OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 19,048 hrs · 10,713 cycles

FUEL LEAK AFTER TAKEOFF. R & R LT WING OTBD FLAPPER VALVE. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 18,402 hrs · 10,287 cycles

DURING C-CHECK. CARGO DOOR LOWER CUT OUT CORRRODED. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,684 hrs · 9,787 cycles

DURING SCHEDULED MX INSPECTION, 12A EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX RESET AND PERFORMED. OPS CHECKED SUCCESSFULLY IAW AMM 33-50-00. ACFT WAS APPROVED FOR RETURN SERVICE.

Part: CARBON SEAL — LEAKING (ACCESSORY GB) · airframe 17,684 hrs · 9,787 cycles

CREW REPORTED ON DESCENT ENGINE NR 1 SHOWED LOW OIL PRESSURE AND 3 QUARTS OF OIL INFLIGHT. SHUT ENGINE DOWN DUE TO CONDITION. SHOWED 2 QUARTS OF OIL ON GROUND. MX FOUND 1 ENGINE ATS AGB CARBON SEAL LEAKING AND CASE DAMAGED. R & R NR 1 ENGINE AGB IAW MM 72-63-10 WITH OPS AND LEAK CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — VIBRATION (NR 1) · airframe 16,477 hrs · 9,134 cycles

EWR FLT 4683 THE CREW REPORTED A ENGINE NR 1 HP VIBRATION AMBER INDICATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT NR 1 ENGINE VIB INDICATION PER RRFIM 77-41-00-810-802. VIBES WERE WITHIN LIMITS. THE ENGINE WAS PLACED ON DMI FOR REPLACEMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,296 hrs · 8,471 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHT STRIP AT THE GALLEY TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (FIRE DETECTION) · airframe 15,076 hrs · 8,351 cycles

NR 1 ENGINE FIRE DETECTOR FAIL AND E1 & E2 SHORT DISPATCH BEFORE TAKEOFF. ABORTED TAKEOFF. PERFORMED OPERATIONAL TEST OF NR 1 AND NR 2 ENGINES AND RESET E1 AND E2 FADECS. OPS CHECKED GOOD. NR 2- E1 FIRE DETECTOR FAIL ON TAKEOFF. ABORT TAKEOFF. INSPECTED E1 FIRE LOOP. FOUND LOOSE CONNECTIONS. RE-SECURED BOTH CONNECTIONS AND OPS CHECKED GOOD. NR 3- E1 FIRE DETECT FAIL. REMOVED AND REPLACED E1 FIRE CONTROL MODULE. OPS CHECK GOOD. PERFORMED TEST FLIGHT AND TEST FLIGHT WAS SATIFACTORY.

Part: ANTI-ICE VALVE — FAULTY (NR 2 ENGINE) · airframe 14,884 hrs · 8,190 cycles

CREW REPORTED AN ENGINE 2 ANTI-ICE FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL PROCEDURES. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE ANTI-ICE VALVE AND NR 2 ENGINE ANTI-ICE PRESSURE TRANSDUCER. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 14,429 hrs · 7,856 cycles

OKC - FLIGHT 4934, THE CREW RETURNED TO OKC FOR LAV SMOKE IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT, AND IAH MAINTENANCE PERFORMED ENGINE RUNS, AND BLEED SYSTEMS OPERATIONAL CHECKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,435 hrs · 7,300 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — CRACKED (ZONE 700) · airframe 11,878 hrs · 6,446 cycles

IAH - FLIGHT 2553, DURING PREFLIGHT INSPECTION THE CREW REPORTED TAHT THE RIGHT MAIN LANDING GEAR AUX DOOR WAS CRACKED. MAINTENANCE REMOVED THE AUX DOOR, AND PLACED THE AIRCRAFT IN CDL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 2/28/2010, THE IAH MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR AUX DOOR, OPERATIONALLY TESTED WITH NO DEFECTS, CLEARED THE CDL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 11,361 hrs · 6,169 cycles

IAH - FLIGHT 2633, THE CREW REPORTED A RUDDER 1-2 INOP MESSAGE ON EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 & NR 2 RUDDER PRESSURE SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 11,361 hrs · 6,169 cycles

IAH - FLIGHT 2633, THE CREW REPORTED A RUDDER 1-2 INOP MESSAGE ON EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 & NR 2 RUDDER PRESSURE SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (AC PACK) · airframe 10,982 hrs · 5,951 cycles

IAH - FLIGHT 2172 - THE CREW REPORTED, RECEIVED A PACK ONE VALVE CLOSED MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PACK DUCT TEMPERATURE SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 10,920 hrs · 5,918 cycles

IAH - FLIGHT 2160, DURING CLIMB THE CREW REPORTED A BLEED ONE OVERTEMP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE FAN AIR VALVE FILTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TAT PROBE — INOPERATIVE (NR 1) · airframe 9,209 hrs · 4,985 cycles

IAH - FLIGHT 2951, THE CREW REPORTED A TAT 1 HEAT INOP IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE TAT PROBE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FILTER — DIRTY (OUTFLOW VALVE) · airframe 8,857 hrs · 4,804 cycles

IAH - FLIGHT 2579, THE CREW REPORTED THAT THE PRESSURIZATION FLUCTUATED IN MANUAL AND AUTO MODES. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE OUTFLOW VALVE AIR FILTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (ZONE 600) · airframe 8,488 hrs · 4,597 cycles

SHV DURING C-CHECK RT LOWER AILERON SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT LOWER AILERON SHROUD IAW EC5750-01315(E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 8,488 hrs · 4,597 cycles

SHV DURING C-CHECK LT OMEGA BEAM FRM 20 SIDE WALL CORRODED. MX REPAIRED LT OMEGA BEAM FRM 20 SIDE WALL IAW SRM 53-10-00. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — DIRTY (SMOKE DETECTOR) · airframe 7,275 hrs · 3,921 cycles

FLT 0032 - ONT - FLIGHT CREW REPORTED LAV SMOKE DETECTION WILL NOT TEST DURING PREFLIGHT CHECK. MX PERSONNEL CLEANED SMOKE DETECTOR SENSOR OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: FLAPPER VALVE — WORN (RT WING) · airframe 7,102 hrs · 3,825 cycles

FLT 220 - ABQ - FLIGHT CREW REPORTED FUEL LEAKING FROM RIGHT WING / OVERWEIGHT LANDING TOUCH DOWN 46,600, 100FPM. THE CREW RETURNED TO BLOCK AND DECLARED AN EMERGENCY AND LANDED SAFELY WITHOUT INCIDENT. MX REMOVED AND REPLACED RT WING MOST OUTBOARD FLAPPER VLV, OPERATIONALLY CHECKED SATISFACTORY. OVERWEIGHT LANDING IS PERMITTED AT SINK RATE INCODE IAW EMB 145 EC0550-01004.

Part: VALVE — LEAKING (RT WING) · airframe 7,046 hrs · 3,796 cycles

FLT 220 - ONT - FLIGHT CREW REPORTED FUEL LEAKING OUT OF RIGHT WING. MX REMOVED AND REPLACED RT OUTBOARD WING VENT VALVE. OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 4,279 hrs · 2,336 cycles

IAH - DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — OUT OF ADJUST (PAX DOOR) · airframe 4,124 hrs · 2,232 cycles

CLE FLIGHT 2327 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE WITH LARGE GAP AT THE TOP OF THE DOOR. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AFT MAIN CABIN DOOR ROLLER SUPPORT. OPERATIONAL CHECKS WERE GOOD.