N537UA

Part: COVER — UNSECURE (CABIN) · airframe 78,371 hrs · 28,408 cycles

THE EMERGENCY LIGHTS IN THE LAST 4 ROWS OF COACH ARE LIFTING UP OFF THE FLOOR. REPLACED EMER EXIT LIGHT COVER. OPERATIONS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 77,790 hrs · 28,186 cycles

EMERGENCY EXIT FLOOR STRIP LIGHTS LOOSE AT 26C. SPLICED IN NEW PIECE OF CABLE & SECURED COVER. OPERATIONS CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 77,411 hrs · 28,080 cycles

EMERGENCY EXIT LIGHT TRACK COVER CAME OFF WITH WIRE DAMAGED IN AFT CABIN. REPAIRED & CHECKED EMER EXIT LIGHT FOR CORRECT OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,979 hrs · 27,949 cycles

EMERGENCY LIGHTING DOES NOT TURN ON IN FRONT OF AFT FWD LAVATORY FLOOR. REPLACED EMER LIGHT LAMP STRIP. EMER LIGHT TEST FROM AFT ATTENDANT PANEL OK IAW AMM 33-51-00.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 74,177 hrs · 27,076 cycles

OIL LEAK ON NR 2 ENG. EVIDENCE OF OIL WETNESS FROM BREATHER OUTLET. CLEANED AREA, OIL CONSUMPTION IS NORMAL OK IAW AMM 79-00-95 PAGE 204, PARA F.

Part: ACM — SEIZED (AC BAY) · airframe 74,142 hrs · 27,067 cycles

FLIGHT CREW REPORTS SMOKE IN THE CABIN. AFTER FURTHER INSPECTION FOUND LT PACK ACM SEIZED, SENDING SMOKE INTO CABIN. REPLACED LT ACM IAW AMM 21-51-03. OPERATIONS CHECKED NORMAL. LT PACK CONTROLLER SHOWS NO FAULTS. OPERATED LT PACK WITH APU BLEED NO ODOR IN CABIN NOTICED.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 73,996 hrs · 27,021 cycles

WHEN PERFORMING THE REVERSE FLOW PROTECTION CHECK THE LT NR 1 ENG APPEARED TO HAVE A COMPRESSOR STALL & WENT SUB-IDLE & STAYED THERE WITH BOTH ENG BLEED VLVS OPEN. THE ISOLATION VLV OPEN & BOTH THROTTLES INITIALLY AT IDLE THE DUCT PRESS WAS NORMAL AROUND 15 PIS INCOMPLETE. R & R NR 1 ENG REVERSE FLOW CHECK CONTROLLER. OPERATIONS CHECKED GOOD ON ENG RUN IAW AMM 36-11-18 & JRH 2-5-1.

Part: SILL — CORRODED (FUSELAGE) · airframe 73,996 hrs · 27,021 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL AT BS 1400 FRONT SIDE. CORROSION AFT CARGO BAY DOOR CUT OUT LOWER SILL BS 1400 STRINGER 27R FOUND TO BE OUT OF LIMITS MATERIAL LOSS .013 INCHES, ORIGINAL THICKNESS .071 INCHES, REMAINING .058 INCHES IAW SRM 53-60-15 FIG 101 DETAIL VIII. REPAIRED LOWER SILL WEB IAW ECRA 5300-01908.

Part: SKIN — BENT (CARGO DOOR) · airframe 73,996 hrs · 27,021 cycles

AFT CARGO DOOR EXTERNAL SKIN IS BENT FWD & AFT CORNERS. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLERS ON FWD & AFT LOWER CORNERS IAW SRM 52-30-01 FIG 201 RPR 4, SKIN THICKNESS IS .063. FWD & AFT CORNERS REPAIRED IAW SRM 52-30-01 FG 201 REPAIR 4 & REQ REINSP AT 37500C WITH REPEAT INSP AT 3000C.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,996 hrs · 27,021 cycles

DENT ON FUSELAGE SKIN BS 1664 BETWEEN STRINGER 20R - 21R. INSTALLED REPAIR IAW SRM 53-00-01.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 73,414 hrs · 26,848 cycles

RT ENG PRI CONT STATUS MESSAGE DISPLAYED AFTER ENG START. MESSAGE READ RT ENG PRI CONT & P T 2 EEC

Part: BOLT — LOOSE (NR 1 IDG) · airframe 73,361 hrs · 26,831 cycles

OIL LEAKING FROM NR 1 ENG FAN COWL. SECURED BOLT ON NR 1 ENG IDG, BOLTS TWO EACH ARE LOCATED AT 4 O'CLOCK POSITION. ACCOMPLISHED ENG RUN, NO LEAKS NOTED. SERVICED NR 1 ENG IDG.

Part: SPRING — BROKEN (APU START SWITCH) · airframe 72,950 hrs · 26,702 cycles

RETURN SPRING IN APU START SWITCH IS BROKEN. REPLACED SWITCH SPRING FUNCTION & OPERATIONS CHECKED GOOD.

Part: SEAL — MIGRATED (TE FLAP) · airframe 72,222 hrs · 26,468 cycles

BULB SEAL BETWEEN INBD & OTBD FLAP RT WING MIGRATED BACKWARDS & PARTIALLY DETACHED. SECURED BULB SEAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 72,164 hrs · 26,449 cycles

NR 2 LT MED OVERHEAD EXIT LIGHT SECURED WITH TAPE. REPAIRED EXIT LIGHT.

Part: CAP — MISSING (CABIN) · airframe 72,164 hrs · 26,449 cycles

FLOOR EMERGENCY LIGHTING ENDCAP MISSING AT MID LAVATORY. REPLACED END CAP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,164 hrs · 26,449 cycles

FLOOR EMERGENCY LIGHTING COVER CRACKED & EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN SEAT ROWS 8 &12. REPAIRED EMERGENCY EXIT LIGHT & REPLACED COVER.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 72,125 hrs · 26,434 cycles

EMERGENCY EXIT SIGN DOOR 2L FELL OFF. SECURED EXIT SIGN.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 71,952 hrs · 26,380 cycles

EMERGENCY LIGHT DAMAGED NEAR DOOR 2L. SECURED COVER.

Part: INDICATOR — DAMAGED (OXYGEN BOTTLE) · airframe 71,893 hrs · 26,364 cycles

IN STOW BIN 1AB, O2 BOTTLE AND O2 BOTTLE NEXT TO AFT FWD LAV, HAVE INDICATION PRESSURE NEEDLES BENT OVER TO INDICATE FULL. REPLACED BOTH O2 BOTTLES.

Part: RETAINING CLIP — DAMAGED (CABIN) · airframe 71,609 hrs · 26,265 cycles

EXIT LIGHT LENS RETENTION CLIPS DAMAGED OVER DOOR 2L. REINSTALLED SIGN.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 71,598 hrs · 26,261 cycles

FLOORBEAM TEE CORRODED AT BS 1680 RBL 48. REPAIRED CORRODED TEE IAW ECRA 5360-01315. THIS IS A MAJOR CATEGORY `A` REPAIR.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 71,598 hrs · 26,261 cycles

RIGHT MAIN INBD FLAP UPPER SKIN GOUGED AT OTBD END 36" FROM T/E. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND INSTALLED BONDED DOUBLER REPAIR IAW REO G-16315, AND ECRA 5750-0455 8.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 71,598 hrs · 26,261 cycles

RIGHT INBD MAIN FLAP LOWER SURFACE HAS A DENT 3 INCHES WIDE BY 5 INCHES LONG BY .083" DEEP. FOUND WITHIN LIMITS IAW SRM 57-53-01. REPAIRED RT INBD MAIN FLAP LWR SURFACE IAW SRM 51-71-10 REPAIR 4, FIG 202, SHEET 3.

Part: WEB — CORRODED (BS 1680) · corrosion level 2 · airframe 71,598 hrs · 26,261 cycles

CABIN FLOOR WEB CORRODED AT BS 1680, RBL 4-47. REPAIRED AFT FLOOR WEB IAW ECRA 5330-04259.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 71,598 hrs · 26,261 cycles

MAIN CABIN FLOORBEAM BS 324 IS CORRODED NEAR RBL 60. INSTALLED SPLICE REPAIR IAW SRM 53-10-08, REPAIR 1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 71,598 hrs · 26,261 cycles

FLOORBEAM AT BS 365 HAS CORROSION FROM LBL 8 TO RT END OF BEAM, INSTALLED TEE REPAIR NR 3 IAW SRM 53-00-51. THIS IS A CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 71,598 hrs · 26,261 cycles

MAIN CABIN FLOORBEAM TEE FOUND CORRODED AT BS 1640 LBL10-RBL60. REPAIRED TEE IAW SRM 53-00-51 REPAIR NR 3 AND THIS IS A CATEGORY "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 71,160 hrs · 26,132 cycles

FLOOR SPONGY BETWEEN ROWS 9 AND 10. INSTALLED INTERM REPAIR PER AMM. LARGE AREA DELAMINATION. REPLACE PANEL BY NEXT C CHECK. DELAMINATION AREA EXTENDS BETWEEN CENTER AISLE ROWS 9-11.

Part: CAP — MISSING (EMERGENCY LIGHTS) · airframe 71,043 hrs · 26,095 cycles

EMERGENCY LIGHT END CAPS MISSING IN FIRST CLASS. REPLACED CAPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,633 hrs · 25,965 cycles

EMERGENCY LIGHT AT AFT LAV IS INOPERATIVE. REPLACED EMERGENCY LIGHT.

Part: DUCT — UNSECURE (CABIN AIR) · airframe 70,543 hrs · 25,938 cycles

CREW REPORTED A HUMMING NOISE IN AISLE AREA AT ROW 1. SECURED AIR DUCT OVERHEAD. NO DEFECTS NOTED.

Part: SWITCH — FAILED (EXTERNAL POWER) · airframe 70,461 hrs · 25,908 cycles

MAIN CABIN LIGHTING IS LOST WHEN GROUND POWER CABLE DISCONNECTED AND A-CON APU POWER. BITE CHECKED BPCU SYSTEMS, CHECKED OK. FOUND THAT OVERHEAD EXTERNAL POWER SWITCH HAD TO CYCLE SEVERAL TIMES IN ORDER FOR GROUND POWER TO COME ONLINE. REPLACED GROUND POWER SWITCH S12.

Part: FAN — FAILED (NR 1) · airframe 68,917 hrs · 25,357 cycles

AT TOP OF DESCENT, ACRID ODOR, LIKE BURNING GUNPOWDER IN THE COCKPIT AND CENTER TO AFT FUSELAGE. REPLACED NR 1 EQUIP COOLING FAN.

Part: LANDING GEAR — SMOKE (MAINS) · airframe 68,614 hrs · 25,259 cycles

SMOKE COMING FROM RT MAIN GEAR TIRES DURING WALKAROUND. INSPECTED RT MAIN GEAR AND BRAKE INSPECTION PER MM. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 67,585 hrs · 24,904 cycles

AT 2500' LOST CABIN PRESSURIZATION. MAINT TEXT: CREW VERBAL WAS HE HAD IT IN CABIN AUTO 1, PACK WAS OPERATING NORMAL. PNEU PRESSURE WAS GOOD ON BOTH ENGINE. HE WAS AT 500' PER MINUTE WITH NO MESSAGE. ACCOMPLISHED TEST OF THE PRESSURIZATION CONTROL SYSTEM PER MM, CKS GOOD.

Part: ACTUATOR — LEAKING (LT WING AILERONS) · airframe 67,108 hrs · 24,718 cycles

FOUND LEFT WING AILERON INBD ACTUATOR LEAKING FROM ROD END SEAL. REPLACED LEFT WING AILERON INBD ACTUATOR.

Part: CAP — MISSING (CABIN) · airframe 66,320 hrs · 24,443 cycles

EMERGENCY ESCAPE FLOOR LIGHT STRIP END CAPS MISSING 6B, 8C,1B AND 1L CLOSET AREA. REPLACED 3 END CAPS. CHECKS OKAY.

Part: STARTER — SHEARED (LT ENGINE) · airframe 65,926 hrs · 24,294 cycles

CREW REPORT: L ENG STARTER APPEARS TO HAVE SHEARED. SAMC TEXT: GRD CREW REPORTS SPARKS FROM UNDER ENG START VLV CONFIRMED OPENING BUT STARTER NOT TURNING. REPLACE STARTER AND START VLV PER MM. CO MECH REPLACED STARTER PER MM AND START VALVE PER MM. MOTOR OF ENG WAS NORMAL. COWLING SECURED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,812 hrs · 24,249 cycles

FUSELAGE SKIN REPAIR COMMON TO LOWER FWD CARGO DOOR CUTOUT BS 580 DENT-GOUGE HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH BUT COMPLIANCE TO 14 CFR 25.571 & 26.43(D) HAS NOT BEEN EVALUATED. A NEW FAA FORM 8100-9 SHOWING COMPLIANCE MUST BE ISSUED BEFORE 11AUG13. IF THE NEW 8100-9 FORM IS NOT ISSUED ON OR BEFORE 11AUG13 THE AIR WORTHINESS CERTIFICATE OF THIS AIRPLANE WITH THIS REPAIR US NO LONGER VALID. THE RECEIPT OF THE NEW 8100-9 IS BEING TRACKED BY DAT 11-145.

Part: AXLE — CHIPPED (NLG) · airframe 65,071 hrs · 23,978 cycles

RT NOSE TIRE OUTER AXLE BEARING SURFACE IS CHIPPED 1-16 WIDE BY 3-8 LONG. REPLACED NLG AXLE. REPLACED NR 1 AFT BRAKE ASSY. FOUND RT NOSE TIRE WITH BROKEN TREAD CORD. REPLACED NR 1 AFT MLG TIRE. REPLACED BOTH NOSE TIRES PER MM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 65,012 hrs · 23,957 cycles

F-O WINDSHIELD ARCING. REMOVED FO NR 1 WINDSHIELD. FOUND PRIMER LIFTING ON LOWER FRAME. CLEANED FRAME OF OLD PRIMER AND SEALANT. REAPPLIED FR PRIMER AND SEALANT PRIMER. CNTR WINDOW TRIM RMV'D FOR WINDOW 1R REPLACEMENT. ALSO 1R WINDOW SUN VISOR RAIL REMOVED FOR ACCESS TO WINDOW SENSORS. REPLACED REMOVED TRIM AND VISOR RAIL IN COCKPIT. REPLACED F/O FWD WINDOW PER MM. REPLACED MISSING PRIMER AND SEALANT. DURING WINDOW HEAT TEST FOUND WINDOW HEAT CONTROLLER M192 FAILED, WOULD NOT BITE TEST. REPLACED WINDOW HEAT CONTROL UNIT M192 PER MM, OPS CHECKS GOOD. CHK SEALANT AROUND FO WINDSHIELD IS CURED BEFORE DISPATCH. FOUND SEALANT CURED.

Part: WEDGE — DAMAGED (NR 5 LE SLAT) · airframe 64,820 hrs · 23,889 cycles

FLT CREW ON WALKAROUND REPORTS METAL PROTRUDING FROM LEFT WING UPPER WINGROOT. NR 5 L/E SLAT HAS 4 X 4 INCH TEAR TO SKIN PANEL ON UPPER SURFACE ADJACENT TO TRAILING EDGE WEDGE. REMOVED NR 5 L/E SLAT FOR REPAIR TO SHOP. REPLACED LEADING EDGE SLAT NR 5 PER MM. NO FAULTS NOTED.

Part: SEQUENCE VALVE — FAULTY (NLG DOOR) · airframe 64,494 hrs · 23,763 cycles

NOSE GEAR GREEN DOWN LIGHT OFF WITH GEAR HANDLE DOWN. EICAS MESSAGE 'GEAR DISAGREE' DISPLAYED. DOORS AMBER LIGHT OFF. GEAR LIGHT WAS ON. INDICATIONS WERE NORMAL AFTER ALT GEAR EXT. CREW DOESN'T BELIEVE DOORS LIGHT WAS ON PRIOR TO ALT EXTENSION. REPLACED NOSE GEAR OPERATED SEQUENCE VALVE. OPS CHECKED NLG NORMAL AND ALTERNATE EXTENSION & RETRACTION OK.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 63,219 hrs · 23,280 cycles

RIGHT ENGINE OIL FILTER EICAS, FLIGHT DIVERTED. NR 2 ENGINE HAS BEEN REMOVED AND IS BEING HELD. COVER WAS REINSTALLED WITH NO FILTER ELEMENT INSTALLED. REINSTALLED CONTAMINATED FILTER, FILTER IS FULL OF METAL. ENG HAS BEEN REPLACED.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 63,014 hrs · 23,206 cycles

FLOOR TRACK AT ROW 26-31 LIGHT INOP. TROUBLESHOT AND FOUND BAD LEAD ASSY WIRE. REPLACED ASSY WIRE, OPS CHECK GOOD. WORK WAS ACP ON NR 2227N00028.

Part: TEAR STRAP — DEBONDED (BS 620 S4-10R) · airframe 63,014 hrs · 23,206 cycles

SKIN PANEL TEAR STRAP AT FUSELAGE STA 620, BETWEEN STR 4R AND STR 10R DEBONDED. REPAIRED DEBONDED STRAP AT STA 620, STR 4R TO 10R IAW UAL JC 596970400. WORK WAS ACP ON TPA DURING SSR VISIT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 62,452 hrs · 22,989 cycles

FOUND BATTERY PACK FOR EGRESS LIGHTING NOT WORKING FWD OF AFT LAV DOOR. REPLACED EGRESS LIGHTING, BATTERY PACK. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,986 hrs · 22,829 cycles

4 RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,613 hrs · 22,688 cycles

ENCAPSULATED EEL LIGHT STRIP INOP AT FWD AFT LAV- LAV K. NEEDS LIGHT STRIP. REPLACED STRIP, CHECKS OKAY.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 61,451 hrs · 22,630 cycles

MED 1R SLIDE FELL OUT TO GATE GOURMET TRUCK STAND. SLIDE UNSECURE. REPLACED MED 1R SLIDE.

Part: RESERVOIR — DISCHARGED (R1 DOOR) · airframe 61,451 hrs · 22,630 cycles

MED 1R EMERGENCY ASSIST BOTTLE DISCHARGED. REPLACED MED 1R EMERGENCY POWER RESERVOIR.

Part: LAVATORY — FULL · airframe 61,208 hrs · 22,540 cycles

LAV ISSUE, FLT DIVERTED. LAVS HIGH BUT NOT OVERFLOWING. RESERVICED LAVS, ALL OPS CHECK NORMAL.

Part: STRUCTURE — DELAMINATED (THRUST REVERSER) · airframe 59,763 hrs · 21,998 cycles

NR 1 ENG RT INBOARD REVERSER UPPER BIFURCATION PANEL INNER SKIN IS DELAMINATED. REMOVED REVERSER. CONTINUED WORKING DOUBLER REPAIR. INSTALLED REV AFTER REPAIR, RIG & OPS CHECKS. ACCMP'D A INTERIM REPAIR CF0665 TO REPLACE WITHIN 300 FLIGHT HOURS.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

LOW PRESSURE. CHECKED FOR LEAKS. NO LEAKS FOUND. PRESSURE NEEDLE WAS ON HIGH SIDE OF GREEN BAND. RETURN TO SERVICE.

Part: PIN — BROKEN (CABIN) · airframe 58,094 hrs · 21,338 cycles

EEL ESCAPE LIGHTING ON FLOOR AT FWD AFT LAV IS INOP. LIGHT STRIP CONNECTOR PINS BROKEN. REPLACED EEL FLOOR LIGHTING STRIP AT AFT FWD LAV P/N 6024-3, OPS CHECKED GOOD.

Part: SEAL — LEAKING (APU COMPRESSOR) · airframe 56,864 hrs · 20,863 cycles

GENERATOR INDICATION AND APU EICAS MESSAGE. FLIGHT DIVERTED. FOUND FRONT LOAD COMPRESSOR SEAL LEAKING. REPLACED APU ASSY.

Part: WINDOW — OPEN (COCKPIT) · airframe 56,088 hrs · 20,589 cycles

1ST OFFICER'S WINDOW OPENED. RTFL. CHECK WINDOW OPERATION AND SEAL FOR DAMAGE AND WINDOW OPS NORMAL AND NO SEAL DEFECTS NOTED. CLOSED WINDOW.

Part: SENSOR — FAILED (R1 DOOR) · airframe 55,436 hrs · 20,355 cycles

GIRT-BAR ARM LT C/B TRIPPING, UNABLE TO ISOLATE FAULT. FOUND PROX SWITCH SW10216 FAILED. REPLACED PROX SWITCH SW10216.GIRT BAR LIGHT WORKS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,431 hrs · 20,352 cycles

LEFT EXTERNAL FUSELAGE STA 600-640, STR 15L - 17L, 3 EA DENTS, 2 EA OF WHICH ARE ON EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN & INSTALLED DOUBLER REPAIR.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 55,433 hrs · 20,353 cycles

NR 2 RT EXIT SIGN SLIDE LIGHT INOP. CAUSE, SHORT IN WIRING AT LIGHT SIGN ASSY AND POSSIBLE FAULTY PROX SENSOR ASSOCIATED WITH SYSTEM. REMOVED AND REPLACED DOOR SLIDE LT ASSY, AND DOOR GIRT BAR PROX SENSORS, OPS CHECK GOOD.

Part: FRAME — DENTED (BS 540 S25L) · airframe 55,431 hrs · 20,352 cycles

FWD PIT FRAME DENTED STA 540, STR 25L. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1520 S22-23R) · airframe 55,431 hrs · 20,352 cycles

AFT PIT STA 1520 BETWEEN S22-23R HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF INBOARD FLANGE. FABRICATED & INSTALLED J-ANGLE.

Part: FRAME — DAMAGED (BS 780 S28L/R) · airframe 55,431 hrs · 20,352 cycles

FWD PIT REPAIR ON FRAME STA 780 STR 28L AND STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 800-1420 S25L) · airframe 55,431 hrs · 20,352 cycles

FRAME AT BS 800-1420 LBL 5 - RBL 5 S25L REQUIRED REPAIR.

Part: FRAME — DAMAGED (BS 800 S28L/R) · airframe 55,431 hrs · 20,352 cycles

FWD PIT FRAME REPAIR AT STA 800, STR 28L TO STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 740 S28L/R) · airframe 55,431 hrs · 20,352 cycles

FWD PIT FRAME REPAIR AT STA 740 STR 28L TO STR 28R. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 760 S28L/R) · airframe 55,431 hrs · 20,352 cycles

FWD PIT FRAME AT STA 760 STR 28L TO STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 55,431 hrs · 20,352 cycles

LOW BOTTLE PRESSURE. *S/D* UNDER FILL AT TIME OF INSTALLATION. TECHNICIAN RETRAINED AND BOTTLE SERVICED.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 55,431 hrs · 20,352 cycles

DOOR 2L UPPER HINGE CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 55,431 hrs · 20,352 cycles

DOOR 2R UPPER HINGE CUTOUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED.

Part: STRUCTURE — GOUGED (R1 DOOR) · airframe 55,431 hrs · 20,352 cycles

DOOR 1R INTERIOR STRUCTURE IS GOUGED AT UPPER HINGE ARM AREA. ACCOMPLISHED MAJOR REPAIR.

Part: FITTING — CORRODED (BS 1720) · airframe 55,431 hrs · 20,352 cycles

MAIN CABIN RT SIDE BS 1720 BULKHEAD FITTING CORRODED AT RBL 47. ACCOMPLISHED MAJOR REPAIR.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 54,946 hrs · 20,176 cycles

DURING T/O ROLL BAD SMELL IN COCKPIT 30 SECONDS AFTER T/O POWER SET. CEASED AFTER 3 MINUTES.

Part: TRANSMITTER — FAILED (WEATHER RADAR) · airframe 53,104 hrs · 19,515 cycles

RTFL DUE TO LOSS OF WEATHER RADAR AND EN ROUTE THUNDERSTORMS. [08-07-07] ERRATIC WX RADAR RETURNS AT VARIOUS RANGES FROM 80, 40 AND 20 MI RANGES, FALSE RETURNS ARE DEPICTED AT AROUND THE 11'O'CLOCK AND 12'O-CLOCK, REPLACED WX RADAR TRANSMITTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,087 hrs · 19,507 cycles

LEFT WING EMERGENCY EXIT LIGHT INOP. REPLACED LAMP.

Part: DOOR FRAME — CRACKED (R2 DOORWAY) · airframe 51,165 hrs · 18,816 cycles

THE 2R MED FWD FRAME IS CRACKED. REPLACED WITH A NEW MAIN ENTRY CABIN DOOR. REMOVED DOOR SENT TO SHOP FOR EVALUATION. ROOT CAUSE OF CRACK IS STILL UNDER INVESTIGATION.

Part: SLIDE — LEAKING (PAX DOOR) · airframe 48,403 hrs · 17,817 cycles

SLIDE FAILED AIR RETENTION TEST DUE TO LEAKING SEAM. AT COMPONENT SHOP MAINTENANCE, SLIDE FAILED AIR RETENTION CHECK DUE TO SEAM LEAK. SLIDE WAS RETURNED TO OEM FOR INFLATABLE REPLACEMENT.

Part: WARNING LIGHT — ILLUMINATED (MACH SPEED TRIM) · airframe 48,340 hrs · 17,794 cycles

FLIGHT DIVERTED DUE TO MACH SPEED TRIM EICAS AND LIGHT ILLUMINATED. A NUISANCE FAULT TRIPPED THE AIR/GROUND FAULT BALLS ON THE LT AND RT STABILIZER/ELEVATOR ASYMMETRY MODULES (SAMS), WHICH GENERATED THE MACH TRIM EICAS MESSAGE AND CAUTION LIGHT. THE AIR-GRND FAULT BALLS WERE RESET ON BOTH SAMS PER MM 27-09-00, FIG 106. NO FURTHER FAULTS DETECTED AFTER BITE OPS CHECK WAS ACCOMPLISHED. NO FAULTED PARTS OR COMPONENTS WERE IDENTIFIED.

Part: ASPIRATOR — LEAKING (SLIDE)

ASPIRATOR FLAPPER VALVE LEAKS. LEAKAGE OF ASPIRATOR FLAPPER VALVE. ASPIRATOR WAS REPLACED.

Part: ASPIRATOR — CRUSHED (SLIDE/RAFT)

FOUND LOWER TUBE ASPIRATOR CRUSHED. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ASPIRATOR WAS OBSERVED DURING SHOP MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED.

Part: WIRE — DAMAGED (OVERHEAT LOOP) · airframe 45,725 hrs · 16,808 cycles

LANDED UNDER AMBER ALERT DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT. DETECTED A BROKEN SHIELD WIRE AT OIL FILTER SWITCH CONNECTOR. RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. SUPPLEMENTAL DATA UPDATE CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPS A & B WITH LOW RESISTANCE SHORT TO GROUND. REMOVED AND REPLACED OVERHEAT DETECTOR CORE LOOPS A & B. ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. REPAIRED SHIELD WIRE. REPLACED OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH.

Part: ACTUATOR — MALFUNCTIONED (FUEL TRANSFER) · airframe 45,248 hrs · 16,625 cycles

UNWANTED FUEL TRANSFER INDICATION. DEFECTIVE CROSS-FEED VALVE ACTUATOR.REPLACED CROSS-FEED VALVE.

Part: SLIDE — OVERSIZED (CABIN)

SLIDE TOO LARGE, AS MEASURED WITH TEMPLATE. SLIDE WAS PACKED INCORRECTLY AT OVERHAUL. WHEN SLIDE INSTALLATION WAS ATTEMPTED, IT WAS REJECTED DUE TO BEING OVERSIZE. SLIDE WAS NOT INSTALLED ON A/C. SLIDE WAS REPACKED PER AIR CRUISER CMM 25-66-01 AND MADE SERVICEABLE.

Part: SKIN — DENTED · airframe 36,902 hrs · 13,563 cycles

LEFT HAND EXTERIOR FUSELAGE SKIN BODY STATION 610, 8" BELOW 17L STRINGER IS DENTED. MAJOR REPAIR ACCOMPLISHED.REMOVED DAMAGE AND INSTALLED DOUBLER AND FILLER.

Part: SEAT TRACK — CRACKED · airframe 36,902 hrs · 13,563 cycles

LH OB SEAT TRACK CRACKED AT OB FASTENER HOLE STATION 1200. MAJOR REPAIR ACCOMPLISHED.SPLICED IN NEW SEAT TRACK SECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,902 hrs · 13,563 cycles

CABIN FLOOR SUPPORT ANGLE CORRODED AT STATION 736, RBL 68, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM ANGLE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 36,902 hrs · 13,563 cycles

CABIN CREASE BEAM WEB UPPER SURFACE CORRODED BODY STATION 982, LBL 71 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: CREASE BEAM — CORRODED · airframe 36,902 hrs · 13,563 cycles

MID CABIN CREASE BEAM HAS EXCESSIVE MATERIAL LOSS AT BODY STATION 1408 RBL71. MAJOR REPAIR ACCOMPLISHED.REPLACED CREASE BEAM.

Part: FRAME — DAMAGED · airframe 36,902 hrs · 13,563 cycles

FORWARD PIT CENTER LINE CIRCUMFERENTIAL FRAME STATION 800 HAS LOADER JACK-SCREW DAMAGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR ON FRAME.

Part: FRAME — DENTED · airframe 36,902 hrs · 13,563 cycles

AFT PIT FRAME AT STATION 1470 STRINGER 25L IS DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: FLANGE — WORN · airframe 36,902 hrs · 13,563 cycles

AFT PIT FRAME FLANGE AFT SIDE LIP WORN, 2 EACH AREAS FROM FASTENERS STA 1520 BETWEEN STRINGER 22R AND 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.L-ANGLE DOUBLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,902 hrs · 13,563 cycles

CABIN FLOORBEAM IS CORRODED AT STA 1640, RBL 50 TO RBL 60. MAJOR REPAIR ACCOMPLISHED. SPLICED IN A NEW FLOORBEAM CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,902 hrs · 13,563 cycles

CABIN FLOORBEAM CORRODED AT BODY STATION 345, RBL 36. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA CUT OUT RBL 34.5 - 37 FORWARD FLANGE ONLY. NESTED DOUBLE ANGLE AND STRAP APPLIED TO FLOORBEAM, RBL 31-41.

Part: FRAME — DAMAGED · airframe 36,902 hrs · 13,563 cycles

FORWARD PIT STATION 760 BEL0W FUSELAGE FRAME DAMAGED FROM LOADER JACKSCREW. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,902 hrs · 13,563 cycles

FORWARD PIT STATION 780 BELOW FUSELAGE FRAME UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FRAME — DAMAGED · airframe 36,902 hrs · 13,563 cycles

STATION 740 BEL0W FORWARD PIT FUSE FRAME HAS DAMAGE FROM TELESCOPING LOADER JACKSCREW. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND STRAP REPAIR.

Part: BEARING — FAILED (NLG) · airframe 36,540 hrs · 13,442 cycles

RIGHT NOSE WHEEL BEARING FAILED ON TAXI. SMOKE AND SMALL FLAME FROM WHEEL. RT NLG OUTBOARD BEARING FAILED. REPLACED NLG AXLE AND BOTH NLG WHEELS. PERFORMED NWS TEST.

Part: SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 35,555 hrs · 13,060 cycles

ELEV LT HYD PRESS STATUS MSG. REPLACED LEFT HYDRAULIC PRESSURE SWITCH S10002.

Part: MECHANISM — LACK OF LUBE (DOOR 4R)

RIGHT REAR GALLEY DOOR WOULD NOT ARM. *S/D* LUBED LINKAGE BETWEEN THE MODE SELECTOR LEVER AND GIRT BAR MECHANISM. ENGAGED SLIDE SEVERAL TIMES, TESTED OK EACH TIME.