N629BR

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 39,944 hrs · 36,348 cycles

A/SKID OTBD CAUTION MSG. EMERGENCY DECLARED. DIVERTED. (FLT 7439) CLOSED DEFERRED A/SKID OUTBOARD CHANNEL PER MEL.

Part: SHUTOFF VALVE — FAILED (RT ENGINE) · airframe 39,649 hrs · 36,034 cycles

AFTER TAKEOFF, SWAPPED BLEEDS FROM THE APU TO THE ENGINES AND THE NR 2 PACK SHUTOFF. THEN GOT A NR 1 PACK HIGH PRESSURE. LEVELED THE PLANE AT 10000, AND THE CABIN ALTITUDE BEGAN TO CLIMB. DECLARED THE EMERGENCY AND RAN THE QRH. A NORMAL LANDING WAS ACCOMPLISHED. REMOVED AND REPLACED THE RIGHT ENGINE PRSOV, OPS CHECKED AND LEAK CHECKED GOOD IAW AMM. PERFORMED OPS CHECK FOR PRESSURIZED THE AIRCRAFT IAW AMM. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (MLG) · airframe 39,315 hrs · 35,672 cycles

WOW INPUT CAUTION MESSAGE DURING FINAL, WITH GEAR DOWN, FLAPS 30. COMPLIED WITH QRH. ABORTED APPROACH. LANDED WITHOUT INCIDENT. SECURED THE SAFETY CONNECTOR PLUG ON THE LT MAIN LANDING GEAR S10 IAW AMM. PERFORMED AN EXTENSIVE OPS CHECK OF THE SYSTEM, WITH FLAPS IN MULTIPLE POSITIONS. FAULT NO LONGER EXISTED AND OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 39,133 hrs · 35,475 cycles

FLOOR SUPPORT, BS 559 TO 559+16 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR PANEL — CORRODED (BS 499-559) · airframe 39,133 hrs · 35,475 cycles

RIGHT SIDE PRESSURE FLOOR PANEL HAS CORROSION BS 499 TO 559. BLENDED IAW REO.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 39,133 hrs · 35,475 cycles

BS 559 FLOORBEAM STRAP HAS CORROSION, BETWEEN RBL 27 AND RBL 42. REMOVED AND REPLACED THE STRAP IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 39,133 hrs · 35,475 cycles

FLOOR SUPPORT LEFT SIDE, BS 424 TO 409.128 CORRODED. REPAIRED IAW REO.

Part: SKIN — CORRODED (BS 559) · airframe 39,133 hrs · 35,475 cycles

EXTERIOR LOWER SKIN, BS 599+112, STRINGER 27 CORRODED RT AND LT SIDES. REPAIRED THE SKIN IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-563) · airframe 39,133 hrs · 35,475 cycles

FLOOR SUPPORT CORRODED AT LBL 43, BS 559+96 - 563. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.

Part: FRAME — CORRODED (BS 605) · airframe 39,133 hrs · 35,475 cycles

FRAME AT BS 605 WAS FOUND CORRODED BETWEEN STRINGERS 25L & 26R. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: DOOR SILL — CORRODED (BS 536-620) · airframe 39,133 hrs · 35,475 cycles

CARGO DOOR SILL CORRODED AT LBL 43, BETWEEN BS 563 & 620. REPLACED THE DOOR SILL IAW REO.

Part: FRAME — CORRODED (BS 574) · airframe 39,133 hrs · 35,475 cycles

FRAME AT BS 574 WAS FOUND CORRODED BETWEEN STRINGERS 26L & 26R. REPAIRED THE FRAME IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 39,133 hrs · 35,475 cycles

FWD SIDE OF THE AFT PRESSURE BULKHEAD WAS GOUGED. REPAIRED THE BS 621 BULKHEAD, RBL 27.5, RBL 18, LBL 18, AND LBL 27.5 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 569-619) · airframe 39,133 hrs · 35,475 cycles

CARGO FLOOR SUPPORT CORRODED AT LBL 27, BS 569 - 619. REPLACED THE FLOOR SUPPORT IAW SRM AND REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,133 hrs · 35,475 cycles

AFT FUSELAGE, LOWER SKIN AROUND THE CARGO DOOR HAD CORROSION. REMOVED THE CORROSION TO A SMOOTH CONTOUR IAW SRM.

Part: SKIN — DENTED (BS 682-700) · airframe 39,133 hrs · 35,475 cycles

EXTERNAL LEFT, AFT LOWER FUSELAGE SKIN BETWEEN BS 682 AND 700 HAD TWO INWARD DENTS AND TWO PROTRUDING DENTS. REPAIRED THE SKIN IAW REO.

Part: SKIN — DENTED (BS 630-700) · airframe 39,133 hrs · 35,475 cycles

EXTERIOR RIGHT LOWER FUSELAGE SKIN BETWEEN BS 630 AND 700 HAD 11 PROTRUDING DENTS. REPAIRED THE SKIN IAW REO

Part: SKIN — GOUGED (PAX DOOR) · airframe 39,133 hrs · 35,475 cycles

PAX DOOR EXTERNAL SKIN WAS FOUND GOUGED ON THE FWD SIDE OF THE EXTERNAL HANDLE. REPAIRED THE DOOR SKIN IAW REO.

Part: SKIN — DENTED (BS 280) · airframe 39,133 hrs · 35,475 cycles

A DENT WAS FOUND APPROXIMATELY 18 INCHES FORWARD OF BS 280 ON THE LOWER LEFT FUSELAGE SKIN. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 605 & 621) · airframe 39,133 hrs · 35,475 cycles

TWO DENTS ON THE RT LOWER FUSELAGE SKIN AFT OF BS 605 AND BETWEEN STRINGERS 24R - 25R AND FWD OF BS 621, BETWEEN STRINGERS 23R - 24R. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 605-621) · airframe 39,133 hrs · 35,475 cycles

ONE DENT WAS FOUND ON THE LT LOWER FUSELAGE SKIN BETWEEN BS 605 - 621, STRINGERS 22L - 23L. REPAIRED THE SKIN IAW REO.

Part: FRAME — CORRODED (BS 319) · airframe 35,898 hrs · 31,973 cycles

FRAME AT BS 319 CORRODED BETWEEN STRINGERS 26 AND 27L. COMPLIED WITH EA. PERFORMED PRESSURIZATION LEAK CHECK IAW AMM. CHECKED GOOD, NO LEAKS NOTED.

Part: ANGLE — CORRODED (BS 394) · airframe 35,898 hrs · 31,973 cycles

ANGLE CORRODED FWD SIDE OF FRAME AT FS 394 BETWEEN STR 25L AND 25R. COMPLIED WITH EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 35,898 hrs · 31,973 cycles

CHAFE DAMAGE FOUND ON LT INBD FLAP VANE, ON OTBD L/E SKIN. REPLACED NEW, IAW SRM.

Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 35,898 hrs · 31,973 cycles

PASSENGER DOOR LOWER SILL, VERTICAL FACE AND CAP ANGLE HAS CORROSION. R & R PAX DOOR LOWER SILL VERTICAL ANGLE, PN: 601R31527-219 AND CAP ANGLE PN: 601R51527-205 IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 35,898 hrs · 31,973 cycles

PAX DOOR PANEL 832BL HAS CORROSION. INSTALLED PANEL 832BL IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 35,898 hrs · 31,973 cycles

PAX DOOR PANEL 832ER HAS CORROSION. REPLACED PANEL 832ER IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 35,898 hrs · 31,973 cycles

PAX DOOR PANEL 832EL HAS CORROSION. REPLACED PANEL 832EL IAW SRM.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 35,898 hrs · 31,973 cycles

PANEL 599BB IS CHAFED. REPLACED PANEL 599BB WITH FACTORY NEW PART IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 35,898 hrs · 31,973 cycles

PAX DOOR PANEL 832BR HAS CORROSION. PAX DOOR ACCESS PANEL 832BR REPLACED WITH A NEW PANEL, IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,236 hrs · 30,274 cycles

FS 280 FLOORBEAM HAS LOWER FLANGE CRACKED LBL 12 - 13.5 AND OTBD, LBL 9. REPAIRED THE FLOORBEAM IAW EA.

Part: SEAT TRACK — GOUGED (BS 364-400) · airframe 34,236 hrs · 30,274 cycles

SEAT TRACK LBL 9 FROM BS 364-400 GOUGED. REMOVED DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 34,236 hrs · 30,274 cycles

FS 280, FWD FLOORBEAM ANGLE IS CORRODED FROM RBL 9 TO LBL 9. R & R THE FLOORBEAM ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 34,236 hrs · 30,274 cycles

SEAT TRACK AT RBL 9 FROM BS 364 - 400 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.

Part: PLATE — CORRODED (EMERGENCY EXIT) · airframe 34,236 hrs · 30,274 cycles

FOUND CORROSION ON RT FWD EMERGENCY EXIT DOOR LOWER SILL COVER PLATE ASSY, REPLACED COVER PLATE ASSY IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,236 hrs · 30,274 cycles

FS 280 TO RBL 9, FLOORBEAM ANGLE WAS FOUND CRACKED. R & R THE ANGLE IAW SRM.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 34,236 hrs · 30,274 cycles

PASSENGER DOOR BOTTOM PLATE SILL CORRODED. REMOVED BLISTERED AND FLAKING PAINT FROM PASSENGER DOOR BOTTOM PLATE SILL IAW SRM, NO DAMAGE NOTED.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,236 hrs · 30,274 cycles

FLOORBOARD 232BRF DELAMINATED. REPAIRED IAW EA.

Part: WARNING LIGHT — FALSE ACTIVATION (CABIN PRESSURE) · airframe 32,962 hrs · 29,043 cycles

RETURNED TO DEPARTURE FOR PRESSURIZATION ISSUES AND SERVICE DOOR CAUTION. INSPECTED ALL DOOR SEALS-NO ISSUES. PERFORMED OPS CHECK OF THE PRESSURIZATION SYSTEM. NO FAULTS FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,807 hrs · 28,885 cycles

EMERGENCY LIGHT OUT IN THE CABIN. CHANGED ALL FOUR BATTERY PACKS.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 32,715 hrs · 28,786 cycles

F/O EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY PACK FOR THE F/O EMEGENCY FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,618 hrs · 28,677 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,423 hrs · 28,468 cycles

RT SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,349 hrs · 28,394 cycles

EXIT LIGHT ROW 8A IS INOPERATIVE. R & R NR 2 EMERGENCY LIGHTING BATTERY PACK IAW AMM, PN ON: 2013-1A, PN OFF: AD-2013-1A, SN ON: 112163, SN OFF: 69898. (2014NM060066)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,265 hrs · 28,308 cycles

NR 7 EMERGENCY LIGHT ON THE EXTERIOR LT SIDE OF THE FUSELAGE INOPERATIVE. R & R NR 7 EMERGENCY LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 32,197 hrs · 28,241 cycles

LEFT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IAW AMM.

Part: PANEL — CHAFED (UNKNOWN) · airframe 32,176 hrs · 28,222 cycles

PANEL 599BB CHAFED . C-CHECK, BLENDED CHAFE ON PANEL 599BB IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650FB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650FB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 540AB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 540AB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 640EB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 640EB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650EB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650EB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650BB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650BB ON WING PLANK IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,176 hrs · 28,222 cycles

LUGS CHAFED ON THE PAX DOOR HINGE, PAX DOOR SIDE. C-CHECK, BLENDED CHAFE LUGS ON PAX DOOR HINGE, DOOR SIDE, IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 540EB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 540EB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550GB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550GB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 640CB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 640CB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER, PANEL 610BB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 610BB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 540DB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 540DB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 540FB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 540FB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 540CB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 540CB ON WING PLANK IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,176 hrs · 28,222 cycles

ONE LUG CHAFED ON THE PAX DOOR HINGE, FUSELAGE SIDE, C-CHECK, BLENDED CHAFE ON PAX DOOR, FUSELAGE SIDE, IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550BB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550BB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650CB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650CB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650GB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650GB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 640FB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 640FB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650DB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650DB ON WING PLANK IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550DB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550DB ON WING PLANK IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,176 hrs · 28,222 cycles

TOP AFT SIDE OF PAX DOOR HINGE HAS CHAFE FUSELAGE SIDE, C-CHECK BLENDED CHAFE ON TOP AFT SIDE OF PAX DOOR HINGE FUSELAGE SIDE IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,176 hrs · 28,222 cycles

FUEL ACCESS PANEL ON RT LOWER WING PLANK UNDER PANEL 650AB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 650AB ON WING PLANK IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 32,176 hrs · 28,222 cycles

MAIN AVIONICS BAY FRAME AT BS 333 FOUND CORRODED. C-CHECK, REMOVED AND INSTALLED NEW FRAME SECTION AT BS 333 BETWEEN STRINGERS 23L AND 23R IAW SRM AND AMM.

Part: FILLER — CHAFED (RT MLG DOOR) · airframe 32,176 hrs · 28,222 cycles

RT MLG DOOR HAS CHAFED FILLER ON LOWER FWD CORNER. C-CHECK, REPAIRED IAW SRM AND REO.

Part: FILLER — CHAFED (LT MLG DOOR) · airframe 32,176 hrs · 28,222 cycles

LEFT MLG DOOR HAS CHAFED FILLER ON LOWER FWD CORNER. C-CHECK, REPAIRED IAW REO AND SRM.

Part: LEVER — CHAFED (PAX DOOR) · airframe 32,176 hrs · 28,222 cycles

PAX DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED PAX DOOR FWD PULL-IN LEVER IAW REO.

Part: FRAME — CORRODED (BS 319) · airframe 32,176 hrs · 28,222 cycles

MAIN AVIONICS BAY, BS 319 FRAME CORRODED. C-CHECK, BLENDED OUT CORROSION IAW EA.

Part: FRAME — CORRODED (BS 349) · airframe 32,176 hrs · 28,222 cycles

MAIN AVIONICS BAY FRAME BS 349 CORRODED AT FRAME. C-CHECK, COMPLIED WITH PERMANENT REPAIR OF MAIN AVIONICS BAY FRAME IAW EA.

Part: FLOOR PANEL — CRACKED (LAVATORY) · airframe 32,176 hrs · 28,222 cycles

LAVATORY FLOOR PANEL CRACKED. C-CHECK, REPAIRED FLOOR PANEL IAW EA.

Part: POST — CRACKED (BS 409) · airframe 32,176 hrs · 28,222 cycles

BS 409 +128, VERT POST AT BL 0 IS CRACKED ON RT SIDE. C-CHECK, R,& R RT VERTICAL POST IAW REO.

Part: FRAME — CRACKED (BS 193) · airframe 32,176 hrs · 28,222 cycles

CRACK INSIDE RT TRU DOOR AT FLOOR WEB AND BS 193 OTBD FRAME. C-CHECK, TRIMMED AWAY CRACKED SECTION AND INSTALLED -1 DOUBLER ON RT TRU DOOR AT FLOOR WEB AND FRAME IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,176 hrs · 28,222 cycles

LEFT INBD FLAP VANE, MID CAP HAS CHAFE. C-CHECK, REPAIRED LT INBD FLAP VANE MID CAP IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,176 hrs · 28,222 cycles

LEFT INBD FLAP VANE, OTBD CAP HAS CHAFE. C-CHECK, REPAIRED LT INBD FLAP VANE OTBD CAP IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,176 hrs · 28,222 cycles

RIGHT INBD FLAP VANE, INBD CAP HAS CHAFE. C-CHECK, REPAIRED RT INBD FLAP VANE INBD CAP IAW REO.

Part: SKIN — CRACKED (LT WING) · airframe 32,176 hrs · 28,222 cycles

POSSIBLE CRACK ON LT LOWER WING PLANK IN THE AREA OF THE REAR SPAR AT WS 148.019. C-CHECK, LT LOWER WING PLANK IN THE AREA OT THE REAR SPAR AT WS 148.019, REPAIRED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,176 hrs · 28,222 cycles

RIGHT INBD FLAP VANE, MID CAP HAS CHAFE. C-CHECK, R & R RT INB FLAP VANE, MID CAP IAW SRM AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,176 hrs · 28,222 cycles

LEFT INBD FLAP VANE, INBD CAP HAS CHAFE. C-CHECK, REPAIRED LT INBD FLAP VANE INBD CAP IAW REO.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 31,133 hrs · 27,151 cycles

LIGHTS IN EMERGENCY EXIT SIGN BURNED OUT. FLT#4647 RELAMPED.

Part: HANDLE — OBSTRUCTED (DOOR) · airframe 31,021 hrs · 27,040 cycles

UNABLE TO OPEN FORWARD DOOR. FLT#4571 CLEANED OUT SMALL AMOUNTS OF DEBRIS ON THE DOOR HANDLE LOCK PLUNGER. .

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 30,569 hrs · 26,594 cycles

LEFT SIDE OVERWING EMERGENCY EXIT LIGHT IS BURNED OUT. RELAMPED.

Part: CONNECTOR — DAMAGED (CABIN PRESSURE) · airframe 30,126 hrs · 26,134 cycles

REMOVED CABIN PRESSURE CONTROL PANEL ON OVERHEAD IN COCKPIT. FOUND EVIDENCE OF BURNING AT ELECTRICAL CONNECTOR. (SERVICE) REPLACED CONNECTOR P1HH AND REPINNED BURNT PINS NR 1, 2, 31, 20. REPLACED CABIN PRESSURE SELECTOR PANEL IAW AMM. P/N: D38999/26WD354N, P/N: 2119764-6 S/N: 112-C0634 P/N OFF: 2119764-5, S/N OFF: 46-B0185.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,352 hrs · 25,354 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4809) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,965 hrs · 24,963 cycles

LAST CABIN CEILING EMERGENCY LIGHT IS OUT. (FLT 4649) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,873 hrs · 24,883 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 4850) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,777 hrs · 24,774 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,704 hrs · 24,706 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4514) RELAMPED EMERGENCY LIGHTS.

Part: SKIN — CHAFED (RT AILERON) · airframe 28,590 hrs · 24,595 cycles

RIGHT AILERON UPPER SKIN LEADING EDGE SHROUD IS CHAFED. (C-CHECK) REPLACED RIGHT AILERON UPPER SKIN LEADING EDGE SHROUD.

Part: VANE CAP — CHAFED (TE FLAP) · airframe 28,590 hrs · 24,595 cycles

LEFT INBOARD FLAP CENTER LEADING EDGE VANE CAP IS CHAFED. (C-CHECK) REPLACED LEFT INBOARD FLAP CENTER LEADING EDGE VANE CAP.

Part: VANE CAP — CHAFED (TE FLAP) · airframe 28,590 hrs · 24,595 cycles

RIGHT INBOARD FLAP CENTER LEADING EDGE VANE CAP IS CHAFED. (C-CHECK) REPLACED RIGHT INBOARD FLAP CENTER LEADING EDGE VANE CAP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,590 hrs · 24,595 cycles

(C-CHECK) FS 621.0 BULKHEAD WEB IS CRACKED AT LBL 36.20 6 INCHES ABOVE FLOOR. REPAIRED FS 621.0 BULKHEAD WEB AT LBL 36.20.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,500 hrs · 24,506 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4457) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,413 hrs · 24,419 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4644) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,311 hrs · 24,328 cycles

OVERHEAD EMERGENCY LIGHT IS OUT AT ROW 5. (FLT 4446) RELAMPED EMERGENCY LIGHT.

Part: RIB — CORRODED (RT WING) · airframe 28,263 hrs · 24,286 cycles

RIGHT WING OUTBOARD LEADING EDGE HAS CORROSION ON THE INBOARD RIB. (SERVICE) REPLACED INBOARD RIB ON RIGHT WING OUTBOARD LEADING EDGE IN REFERENCE TO SRM.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 28,113 hrs · 24,151 cycles

AFTER ROTATION AND LIFT OFF CYCLED THE GEAR LEVER AND HAD A NOSE GEAR DISAGREE. (FLT 7316) ADJUSTED PROX SENSOR PS14GA AND PERFORMED FUNTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,882 hrs · 23,931 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4506) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,811 hrs · 23,862 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4712) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,434 hrs · 23,522 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4681) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,336 hrs · 23,439 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4568) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,300 hrs · 23,407 cycles

RIGHT FORWARD EXTERNAL EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — LOOSE (CABIN) · airframe 27,285 hrs · 23,393 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4275) TIGHTENED BULB IN SOCKET.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,032 hrs · 21,314 cycles

BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,032 hrs · 21,314 cycles

FS 559.00 LT CAP ANGLE CRACKED AT LBL 18.00. REPAIR CW IAW REO 601R-53-41-260 AND 601R-53-41-609.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,032 hrs · 21,314 cycles

FS 559.00 RT WEB CRACKED. WEB IS STOP DRILLED WITH TEMP REPAIR INSTALLED. REPAIR CW IAW REO 601R-53-41-260 AND 601R-53-41-609.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,032 hrs · 21,314 cycles

FS 559.00 RT CAP ANGLE CRACKED AT LBL 18.00. REPAIR CW IAW REO 601R-53-41-260 AND 601R-53-41-609.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 25,032 hrs · 21,314 cycles

FOUND CRACK IN PAX DOOR FRAME SUPPORT STRUCTURE NEAR SUPPORT WHEEL. REMOVED DAMAGE AND REPAIRED IAW REO 601R-52-11-402.

Part: SENSING ELEMENT — FAILED (RT PYLON) · airframe 23,081 hrs · 19,680 cycles

ON CLIMBOUT FROM LGA RECEIVED RIGHT 14TH STAGE DUCT WARNING MSG. FOLLOWED QRH CONTINUED FLIGHT, WARNING MSG REAPPEARED WOULD NOT GO OUT. EMERGENCY DECLARED, A/C DIVERTED TO JAX, LANDED SAFELY. REMOVED AND REPLACED RIGHT 14TH STAGE PYLON SENSING ELEMENT.

Part: WARNING SYSTEM — ACTIVATED (FUEL SYSTEM) · airframe 22,987 hrs · 19,599 cycles

ON CLIMBOUT FROM JAX RECEIVED FUEL IMBALANCE MSG FOLLOWED BY 0 FUEL INDICATION ON RIGHT SIDE TANK. EMERGENCY DECLARED, A/C RETURNED TO JAX LANDED SAFELY. DEFERRED PER MEL 28-41-01-1.

Part: PCU — FAULTY (SPOILER SYSTEM) · airframe 20,673 hrs · 17,729 cycles

FLIGHT 5661 - ON TAKEOFF ROLL RECEIVED TAKEOFF CONFIG SPOILER WARNING. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT FLIGHT SPOILER O/B PCU.

Part: PROXIMITY SENSOR — DIRTY (SPOILER) · airframe 20,673 hrs · 17,727 cycles

FLIGHT 5155 - ON TAKEOFF RECEIVED TAKEOFF CONFIG SPOILER WARNING. ABORTED TAKEOFF. INSPECTED AND CLEANED GROUND SPOILER PROX SENSORS. PERFORMED OPS CHECK OF SPOILER SYSTEM, ALL CHECKS GOOD.

Part: CONTROL UNIT — FAULTY (E&E BAY) · airframe 20,663 hrs · 17,719 cycles

FLIGHT 5653 - RECEIVED CONFIG SPOILERS WARNING MESSAGE. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. REPLACED LEFT SECU. NO FURTHER DEFECTS.

Part: CONTROL UNIT — FAULTY (E&E BAY) · airframe 20,663 hrs · 17,719 cycles

FLIGHT 5653 - RECEIVED CONFIG SPOILERS WARNING MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. REPLACED RIGHT SECU. NO FURTHER DEFECTS.

Part: THROTTLE SWITCH — FAULTY (COCKPIT) · airframe 20,463 hrs · 17,555 cycles

FLIGHT 5384 - ABORTED TAKEOFF BELOW 80 KTS FOR SPOILER CONFIG MESSAGE WITH POWER LEVERS ADVANCED. REMOVED AND REPLACED ACSU (THROTTLE POSITION INDICATOR).

Part: PSEU — MALFUNCTIONED (E&E BAY) · airframe 20,463 hrs · 17,555 cycles

FLIGHT 5384 - ABORTED TAKEOFF BELOW 80 KTS FOR SPOILER CONFIG MESSAGE WITH POWER LEVERS ADVANCED. REMOVED AND REPLACED PSEU.

Part: SPOILER SYS — MALFUNCTIONED · airframe 20,280 hrs · 17,408 cycles

FLIGHT 5592 - ON T/O ROLL RECEIVED WARNING CONFIG SPOILERS MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED RESET OF SECU'S NR 1 AND NR 2, OPS CHECK GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,282 hrs · 17,410 cycles

FLIGHT 5592 - AFTER T/O FLAPS FAIL MESSAGE. FOLLOWED QRH AND RETURNED TO BNA AND LANDED SAFELY. FOUND SKEW DETECTION SYSTEM TO BE CAUSE OF FLAP FAIL. DEFERRED THE SKEW DETECTION SYSTEM PER MEL 27-51-03-1. FLAP SYSTEM OPS CHECK GOOD.

Part: RELAY — FAILED (WOW) · airframe 19,046 hrs · 16,403 cycles

FLIGHT 5405 - NR 2 ENGINE THROTTLE BINDING ON TAKEOFF, ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT WOW RELAY (2K2KE).

Part: FLEX DRIVE — BENT (T/E FLAP) · airframe 18,802 hrs · 16,207 cycles

FLIGHT 5257 - FLAP FAIL MESSAGE RECEIVED AT START-UP. REPLACED LEFT NR 5 FLEX DRIVE. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS.

Part: CONTROL UNIT — FAULTY (E&E BAY) · airframe 18,802 hrs · 16,207 cycles

FLIGHT 5257 - FLAP FAIL MESSAGE RECEIVED AT START-UP. REPLACED FECU. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS.

Part: RACK — DIRTY (GALLEY) · airframe 18,542 hrs · 16,004 cycles

FLIGHT 5008 - EN ROUTE RSW-CMH CREW REPORTED THE PRESENCE OF STRONG ELECTRICAL SMOKE SMELL IN THE COCKPIT, FLIGHT DIVERTED TO MCO. REPLACED THE COFFEEMAKER RACK.

Part: IDG — FAILED (LT ENGINE) · airframe 18,302 hrs · 15,824 cycles

FLIGHT 5620 - DURING TAKEOFF ROLL RECEIVED A NR 1 IDG CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE NR 1 IDG.

Part: STRUT — UNDERSERVICED (NLG) · airframe 18,207 hrs · 15,745 cycles

FLIGHT 5151 - GEAR DISAGREE MESSAGE AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR WOULD NOT FULLY EXTEND. SERVICED NOSE STRUT. NO FURTHER DEFECTS.

Part: FITTING — CRACKED (RT MLG) · airframe 18,113 hrs · 15,680 cycles

DURING ULTRA-SONIC INSPECTION OF RIGHT MAIN GEAR, MAIN FITTING FOUND CRACKED. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR.

Part: DUCT — FAILED (14TH STAGE)

EVENT SUMMARY ON 01/06 STATED ENGINE SHUTDOWN DUE TO QRH 1H 14TH STAGE BLEED DUCT FAIL. INSP LT 14 STAGE BLEED AIR SYSTEM. FOUND PYLON TO FUSELAGE TEFLON INSERT STUCK TO ONE SIDE. RESET INSERT TO PROPER LOCATION AND OPS CHK GOOD. NO FURTHER DEFECTS, REF 36-21-00.

Part: TIRE — FAILED (MLG)

BLOWN TIRE ON TAKEOFF. PAX DEPLANED ON TAXIWAY. MX CHANGED TIRE. THEN CHANGED AGAIN, DUE TO SKYDROL CONTAMINATION.

Part: DOOR — STUCK (PAX)

PAX DOOR WILL NOT OPEN. MX NO DEFECTS WERE NOTED. OPS CHECK GOOD.

Part: GEARBOX — SEIZED (RT ENGINE) · airframe 14,283 hrs · 12,071 cycles

DURING FLIGHT THE CREW REPORTED THE RIGHT HAND ENGINE THROTTLE LEVER LOCKED UP. THE FLIGHT LANDED UNEVENTFULLY. THE THROTTLE GEARBOX ASSEMBLY WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

DURING FINAL NR 1 HYDRAULIC SYSTEM LOST ALL FLUID. AIRCRAFT LANDED SAFELY AND PASSENGERS DEPLANED NORMALLY. THE NR 1 HYDRAULIC PRESSURE SERVICE LINE HAD A HOLE IN IT AND WAS REPLACED. A SATISFACTORY LEAK CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,510 hrs · 11,423 cycles

DURING INSPECTION A SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A SECTION OF EMERGENCY TRACK LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,342 hrs · 11,276 cycles

DURING MAINTENANCE INSPECTION THE FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,229 hrs · 11,187 cycles

DURING MAINTENANCE INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: CONTACTOR — CONTAMINATED (CABIN)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING NEAR THE PASSENGER ENTRY DOOR WAS INOPERATIVE. MAINTENANCE PERSONNEL FOUND THAT THE AREA WAS WET FROM RAIN. DRIED THE AREA, CLEANED THE CONTACTS AND RECONNECTED. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH

During climb of the flight from IAD to BNA, the crew experienced uncommanded nose down pitch trim. The crew performed the QRH procedures and returned to IAD and landed without further incident. Maintenance personnel removed the first officer's yoke pitch trim switch. An operational check was satisfactory and the aircraft was returned to service.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY FLOOR TRACK LIGHTS AT ROLL 10/CD WERE FOUND TO BE INOPERATIVE DURING INSPECTION. MAINTENANCE PERSONNEL SECURED AN ELECTRICAL CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAILED (NACELLE)

(CAN) AIRCRAFT DEPARTED WASHINGTON DULLES INTERNATIONAL AIRPORT ON FLIGHT 7187, THE FLIGHT CREW DETECTED A SEVERE VIBRATION AND RESULTANT ENGINE SHUTDOWN WITHOUT PILOT'S INPUT. THE AIRCRAFT RETURNED TO THE ORIGINATING AIRPORT AND DECLARED AN EMERGENCY. ENGINE CHANGED WAS INITIATED AND THE AIRCRAFT RETURNED TO SERVICE - GEARBOX SUSPECTED. AWAITING TEARDOWN REPORT. ENGINE INSTALLED (TSN 0.0; CSN 0)

Part: WINDOW — BROKEN (COCKPIT)

FLT 6655 - ORD-FAR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO F/O'S SIDE WINDOW SHATTERED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLACED WINDOW, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)

Part: TRANSDUCER — FAILED (LEFT)

FLT 6723 - IAD-SAV - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BRAKE WARNIGN LIGHT ILLUMINATED AND BRAKE PSI INDICATION WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 54656, MEL 32-40. MAINTENANCE CLOSED DMI 54656 ON 11-23-98 BY REMOVING AND REPLACING PRESSURE TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAL — FAILED (LT ENGINE)

IAD/BNA - FLT 6700 - DURING TAKEOFF ON 11-18-98 AT 0820 HOURS, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT TAXIED TO THE GATE. TROUBLESHOT THE DISCREPANCY AND OPENED A DMI AGAINST THE LEFT ACM SYSTEM, DMI NR 54655. DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAINTENANCE CLOSED DMI 54655 ON 11-21-98 BY REMOVING AND REPLACING LT ENGINE NR 3 CARBON SEAL. OPS CHECK OK. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. (X)

Part: SEAL — FAILED (LT ENGINE)

FLT 6700 - IAD-BNA - DURING TAKEOFF, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. A/C DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT TAXIED TO THE GATE WHERE MAINTENANCE WAS NOTIFIED. MAINTENANCE T/S THE DISCREPANCY AND OPENED A DMI AGAINST THE LEFT ACM SYSTEM DMI NR 54655, DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAINTENANCE CLOSED DMI 54655, DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAINTENANCE CLOSED DMI 54655 ON 11-21-98 BY REMOVING AND REPLACING LEFT ENGINE NR 3 CARBON SEAL, OPS CHECK OK. AIRCRAFT WAS RELEASED FOR RETURN TO SERV

Part: CONNECTOR — CONTAMINATED (RT PACK)

FLT 6632 - ORD-CRW - DURING CRUISE, EXPERIENCED A RT PACK 'HI PSI' INDICATION ILLUMINATION. AIRCRAFT RETUREND TO ORD WHERE MAINTENANCE WAS DISPATCHED TO TROUBLESHOOT THE SYSTEM DISCREPANCY. MAINTENANCE CLEANED THE CANNON PUG FOR THE RIGHT PACK ACM AND CHECKED THE PRESSURE SWITCH TO THE RIGHT PACK IAW MM PROCEDURES FOUND IN 21-51-10. MAINTENANCE THEN CONDUCTED AN OPERATIONAL CHECK WITH NO FURTHER DEFICIENCIES NOTED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M)

Part: BPSU — FAILED (TE FLAP)

FLT 6654 - SGE-ORD - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP FAIL MESSAGE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BPSU. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)

Part: ROLLERS — LACK OF LUBE (PASSENGER DOOR)

FLT 6645 - AVP-ORD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING BY DIVERTING TO PIT DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LUBED UPPER ROLLER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)

Part: SENSOR — FAILED (RT WING)

FLT 6647 - AVP-ORD - DURING CRUISE, EXPERIENCED A RIGHT WING ANTI ICE FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAFT CONTACTED MAINTENANCE CONTROL AND DISPATCH, DECISION TO DIVERT TO PIT WAS MADE. DUE TO ICING IN ORD. UPON ARRIVAL AT PIT THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPATCHED. MAINTENANCE WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPATCHED. MAINTENANCE TROUBLESHOT THE DISCREPANCY. REMOVED AND REPLACED ALL 21 WING TEMPERATURE SENSORS. PERFORMED NUMEROUS GROUND CHECKS AND SIGNED OFF THE DISCREPANCY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M)

Part: WARNING LIGHT — ACTIVATED (TE FLAP)

FLT 6764 - PWM-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS THE FLAP FAULT WARNING LIGHT ILLUMINATED. FLAPS STUCK AT ZERO. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKER. MAINTENANCE ALSO OPENED RIGHT 1021 TO WATCH FLAPS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETRN TO SERVICE. (M)

Part: ACTUATOR — FAILED (T/E FLAPS)

IAD/BNA - FLT 6700 - DURING LANDING AT 1,000 HRS ON 8-16-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS, AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLACED LT OUTBOARD/INBOARD FLAP ACTUATOR. MAINTENANCE PERFORMED OPS CHECK, OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X)