N975EV

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,792 hrs · 19,852 cycles

F/A FLASHLIGHT INOPERATIVE. REPAIRED IAW AMM 25-61-02, OPS CHECKED GOOD, OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,792 hrs · 19,852 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. REPAIRED IAW AMM 25-61-02. OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,629 hrs · 19,681 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED BULB AND INSTALLED A NEW BULB IAW AMM 33-51-20. OPS CHECKED GOOD.

Part: RELAY — UNSERVICEABLE (PAX DOOR ASSIST) · airframe 21,016 hrs · 18,989 cycles

F/A REPORTED, OPENING PASSENGER DOOR, DOOR AUTOMATICALLY CLOSED ON ITS OWN. RESISTANCE IS FELT. DOOR KEPT CLOSING ON ITS OWN WHILE PASSENGER WERE EXITING AIRPLANE. PULLED CIRCUIT BREAKER 1F1 TO STOP DOOR FROM CLOSING. CIRCUIT BREAKER LEFT OPEN. R & R JB-2 RELAY K1MB IAW AMM 24-01-02 AND IAW ESPM 20-22-00. OPS CHECKED GOOD.

Part: BLEED VALVE — FAILED (LT ENGINE) · airframe 20,752 hrs · 18,713 cycles

ENROUTE RECEIVED LT 14TH DUCT WARNING MESSAGE. QRH PROCEDURE DID NOT EXTINGUISH. ACFT DIVERTED, EMERGENCY DECLARED. R & R LT 14TH STAGE BLEED AIR SHUTOFF VALVE IAW AMM 36-12-01. LEAK AND OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,088 hrs · 17,959 cycles

EXTERNAL EMERGENCY LIGHT NR 5 INOPERATIVE. RELAMPED EXTERNAL EMERGENCY LIGHT NR 5. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: DOOR — BINDING (SERVICE) · airframe 19,430 hrs · 17,232 cycles

CATERING PERSONNEL UNABLE TO OPEN "SERVICE DOOR" FROM OUTSIDE. ADJUSTED SERVICE DOOR TO WITHIN LIMITS IAW AMM 52-41-00. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,300 hrs · 17,089 cycles

NR2 AND 8 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED NR 2 AND 8 EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-21. OPS CHECK GOOD.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 19,284 hrs · 17,070 cycles

2 EA CLIPS CRACKED AT RBL 9 AND 280 FRAME. REMOVED DAMAGED CLIPS IAW 51-42-06 AND INSTALLED IAW SRM 51-40-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,284 hrs · 17,070 cycles

PAX DOOR FLOOR SILL CORRODED IN SEVERAL PLACES. (MARKED) REMOVED CORRODED FLOOR SILL AND PAX DOOR FITTINGS (2 EA) IAW SRM 51-42-00. DRILLED AND DEBURRED NEW FLOOR SILL ANGLE IAW SRM 51-40-11. INSTALL NEW FLOOR SILL ANGLE IAW SRM 51-42-00. INSTALLED NEW FLOOR SILL ANGLE IAW SRM 51-42-00. INSTALL (2) PAX DOOR FITTING (1EA) JUMPER WIRE AND APPLY CORROSION INHIBITING COMPOUND. INSTALL PAX SWITCH IN DOOR SILL CB 80054 5/11/11 (HF) INSTALLED FWD & AFT HANDRAIL FTGS/JUMPER AMM 52-11-00-400-802 AND PS9MB SWITCH IAW 52-70-04-400-803. PROX SWITCH REQUIRES OPS CHECK WHEN POWER IS AVAILABLE 52-70-04-710-803. OPS CHECK SATISFACTORY IAW AMM 52-70-04-710-803. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 19,284 hrs · 17,070 cycles

2 EA CLIPS CRACKED AT LBL9 AND 280 FRAME. R & R INBD AND OTBD 280 CLIPS ON LBL9 IAW SRM 51-42-21. THIS IS A MINOR REPAIR. (CLOSED)

Part: SILL — CORRODED (FUSELAGE) · airframe 19,287 hrs · 17,074 cycles

FLOOR SILL CORROSION JUST FWD OF SERVICE DOOR CUTOUT FWD EDGE. DEEP PILLOWING CORROSION AROUND NUTPLATE REPLACE INTERCOSTAL. FS 310.00-319.70, RBL44, GF 88021 05/06/11 (LT) REMOVED 2 EA SILL ANGLES UPPER & LOWER AT FS 310.00-319.70, RBL44 IAW SRM 51-42-06. THIS IS A MINOR REPAIR. FOUND CORROSION ON UPPER ANGLE. REMOVED CORROSION FROM UPPER ANGLE BY HAND USING SCOTCH BRITE PAD IAW SRM 51-21-06 TREATED PRIMED & PAINTED IAW SRM 51-21-11, 51-25-06 & 51-25-16. THIS IS A MINOR REPAIR. CORROSION ON LOWER ANGLE/SILL OUT OF LIMITS ANGLE NEEDS TO BE REPLACED. DRILLED UP NEW FLOOR SILL FROM OLD SILL, SEALED RIVETED TO UPPER ANGLE OK TO INSTALL. INSTALLED ON ACFT IAW SRM 51-42-13 & 51-42-06. THIS IS A MINOR REPAIR. UPPER ANGLE NEEDS TO BE REINSTALLED. RIVETS UPPER ANGLE TO LOWER FLOOR SILL & INSTALLED 2 NUTPLATES REINSTALLED IAW SRM 51-42-06. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,284 hrs · 17,070 cycles

PASSENGER SEAT TRACK HAS CORROSION AT ROW 1 AT RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,284 hrs · 17,070 cycles

PASSENGER SEAT TRACK HAS CORROSION AT ROW 1 AT LBL9. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: DRAG BRACE — CRACKED (PAX DOOR) · airframe 19,284 hrs · 17,070 cycles

PAX DOOR AFT RISER PANEL, AFT DRAG BRACE IS CRACKED. R & R IAW SRM 51-42-06

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,662 hrs · 16,346 cycles

F/O'S FLASHLIGHT INOP. R & R F/O'S FLASHLIGHT IAW AMM 25-61-01. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED. (CLOSED)

Part: LIGHT — DAMAGED (CABIN) · airframe 18,328 hrs · 15,962 cycles

WARDROBE CLOSET FLOOR LEVEL EMERGENCY FLOOD LIGHT BASE DAMAGED. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. (CLOSED)

Part: PLACARD — DETERIORATED (SERVICE DOOR) · airframe 17,430 hrs · 14,951 cycles

ASD "OPEN" AND "EXIT" PLACARDS ARE DETERIORATED. REMOVED AND REPLACED ASD "OPEN" AND "EXIT" IAW AMM 11-30-00.

Part: TRANSMITTER — INTERMITTENT (TE FLAPS) · airframe 17,063 hrs · 14,509 cycles

STALL FAIL CAUTION MSG IN FLIGHT NO OVERWEIGHT LANDING OCCURED ON RETURN. (EMERGENCY DECLARED AS A PRECAUTION) R & R RT FLAP POSITION TRANSMITTER REF AMM 27-55-01. OPS CK GOOD. OPS CK STALL PROTECTION, OPS CK GOOD REF AMM 27-35-01.

Part: ACM — CONTAMINATED · airframe 17,003 hrs · 14,440 cycles

SMOKE IN COCKPIT IN CABIN MOMENTARILY AT 100 KNOTS DISSIPATED UPON TEMP REDUCTIOIN ON PACKS NO FURTHER SMOKE OBSERVED. EXCESSIVE DEICE FLUID USED. OPERATED PACKS 1 AND 2 IAW AMM 21-00-00. NO DEFECTS NOTED.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 16,370 hrs · 13,733 cycles

FLT 5122. INFLIGHT LT REVERSE UNLOCK MSG. DURING CRUISE FLIGHT, LEFT ENGINE REVERSE UNLOCK CAUTION MESSAGE APPEARED. [EMERGENCY DECLARED AND HAD EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION -- ENROUTE TO CVG A/C DIVERTED TO TRI DUE TO MTC] ( THRUST REVERSER SYSTEMS )

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,634 hrs · 12,982 cycles

JOB 8759921 OPERATION 328 / EMERGENCY LIGHT DOES NOT WORK ON LT CABIN WINDSCREEN.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 15,616 hrs · 12,962 cycles

FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT RBL 18 I/B SIDE, WL 59.10 APPROX. .3" IN LENGTH, 60% FSH. FAILED NDT INSPECTION. INSTALLED NEW SERVICEABLE RETURN SIDE OF THE PRESSURE AND RETURN MANIFOLD SERVICE POST LINE P/N 601R75286-9 IAW 20-22-00-910-802. INSTALLED 2EA BONDING JUMPER TO THE TUBE ASSY IAW 51-80-00-400-803. C/W RESISTANCE CHECK IAW 51-80-00-760-802.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,616 hrs · 12,962 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED .2" LONG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,616 hrs · 12,962 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT O/B SIDE LBL 9 CRACKED .2" LONG. REMOVED CRACKED FS 484 FLOOR SUPPORT ANGLE AT O/B LBL 9. LOCATED NEW SERVICEABLE ANGLE. INSTALLED 4 EA RIVET THROUGH INTERCOSTAL IAW SRM 51-42-06. FOUR EA FASTENERS THROUGH FLOORBEAM REQUIRE INSTALL. INSTALLED 4 FASTENERS THRU FLOORBEAM IAW REO 601R-53-41-949. C/W EO EC/TC REO 601R-53-41-949 REV 0 REO 601R-53-41-949 REV D DATED 5/20/09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,616 hrs · 12,962 cycles

OVERWING EMER EXIT SIGN IN CEILING HAS (1) BURNED OUT BULB ON FWD SIDE AND (6) BURNED OUT BLBS ON AFT SIDE. REMOVED AND REPLACED LAMP IAW AMM 33-51-00-710-801.

Part: ANGLE — CRACKED (BS 621-625 S14R) · airframe 15,616 hrs · 12,962 cycles

RT 621-625 OBLIQUE ANGLE IS CRACKED AT STRINGER 14 APPROX 1 INCH L. REMOVED CRACKED RH OBLIQUE ANGLE AT F.S. 621-625 STR 14. INSTALLED NEW OBLIQUE ANGLE IAW SRM 51-42-06

Part: ANGLE — CRACKED (BS 621-625 S14L) · airframe 15,616 hrs · 12,962 cycles

LT 621-625 OBLIQUE ANGLE IS CRACKED APPROX 1½ INCHES L AT STRINGER 14L. REMOVED CRACKED LH OBLIQUE ANGLE AT F.S. 621-625 STR 14L. INSTALLED NEW OBLIQUE ANGLE IAW SRM 51-42-06

Part: CONTROLLER — MALFUNCTIONED (ADG DEPLOY) · airframe 15,053 hrs · 12,418 cycles

AT FL230, SMOKE NOTICED COMING FROM ADG AUTO DEPLOY PANEL. EMERGENCY DECLARED. AIR DRIVEN GENERATOR ADG AUTO DEPLOY SYSTEM. REMOVED AND REPLACED ADG AUTO DEPLOY CONTROL IAW AMM 24-23-15 RAN AND OPS CHECKED GOOD. NO SMOKE, CHECKED GOOD.

Part: FLAP — FAILED (WING) · airframe 14,094 hrs · 11,592 cycles

FLAP FAIL AT 0 DEG. EMERGENCY DECLARED. FLT 4317 DEL 236 MINS.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 13,956 hrs · 11,487 cycles

FLAP FAIL AT ZERO. EMERGENCY DECLARED - EN ROUTE TO SCE, A/C DIVERTED TO MDT DUE TO MTC. FLT 9951 DEL 109 MINS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,884 hrs · 11,428 cycles

FLAPS FAIL ZERO DEGREE AT 210 KNOTS >12000 FT, EMERGENCY DECLARED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,884 hrs · 11,428 cycles

FLAPS FAIL AT 0 WHEN DEPLOYED AT 200 KNOTS AT 2000'. TOWER DISPATCHED EMERGENCY EQUIPMENT AS A PRECAUTION. FLT 4809 CX.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,538 hrs · 10,306 cycles

LINTEL SUPPORT FITTING P/N 601R35050-109 CRACKED ON AFT PRESSUE BULKHEAD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,532 hrs · 10,299 cycles

AFT PRESSURE BULKHEAD CRACKED AT ANGLE, AREA IS MARKED. IN REFERENCE TO TASKCARD AWL 53-61-153. [06-14-07] BEGAN REO 601R-53-61-1230. REMOVED ANGLE FORWARD OF STA 621. REMOVED AFT INTERCOSTAL AT STA 621. REMOVED FORWARD LINTEL FITTING AT STA 621.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 12,532 hrs · 10,299 cycles

EMERGENCY ESCAPE HATCH OUTER HANDLE CORRODED SEE EC/TC 600-52-0157 FOR ALL WORK ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (BS 340) · airframe 12,532 hrs · 10,299 cycles

ASD THRESHOLD, FLOOR PANEL SUPPORT AT FS 340 IS CORRODED.

Part: BRACE — CRACKED (BS 280) · airframe 12,532 hrs · 10,299 cycles

ANGLE BRACE IS CRACKED AT FS 280.0 RBL 9.0 ON THE OUTSIDE.

Part: BRACE — CRACKED (BS 280) · airframe 12,532 hrs · 10,299 cycles

FOUND ANGLE BRACE IS CRACKED AT FS 280.0 LBL 9.0 ON THE INSIDE.

Part: ATTACH ANGLE — UNKNOWN (BS 559) · airframe 12,532 hrs · 10,299 cycles

PRESSURE FLOOR AFT PRESSURE BULKHEAD FS 559.0 RBL 9 SUPPORT O/B ATTACH ANGLE IS CRACKED WHERE IT ATTACHES TO FRAME 559.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 12,532 hrs · 10,299 cycles

ASD THRESHOLD, FLOOR PANEL SUPPORT AT FS 319.7 IS CORRODED.

Part: STRINGER — CORRODED (BS 654-682) · airframe 12,532 hrs · 10,299 cycles

SUSPECT CORROSION ON STRINGERS FROM WL97.50 TO FLOOR, BETWEEN FS 654.5 TO FS 682.

Part: WARNING SYSTEM — ACTIVATED (EXTINGUISH SYS) · airframe 12,240 hrs · 10,080 cycles

CARGO BOTTLE LOW MSG ILLUMINATED ON DEPARTURE. RETURNED TO GPT. EMERGENCY DECLARED. FLT 4546 DEL 200 MINS. CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,382 hrs · 9,445 cycles

LT EXT EMERGENCY LIGHT BEHIND EMERGENCY EXIT DOOR INOP.

Part: ODOR — DETECTED (COCKPIT) · airframe 10,625 hrs · 8,867 cycles

FUEL SMELL IN COCKPIT FROM AC.

Part: ODOR — DETECTED (CABIN) · airframe 10,625 hrs · 8,867 cycles

PACKS EMIT FUEL SMELL AS HEAT IS APPLIED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,401 hrs · 8,692 cycles

FOUND EMERGENCY FLOOR LIGHTS INOP FROM ROW 6CD TO 8CD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 10,339 hrs · 8,638 cycles

EMERG EXIT LIGHT NEXT TO RT OVERWING EMERG AND FLOOR TRACK LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,206 hrs · 8,527 cycles

AFT CABIN, CEILING EMERGENCY LIGHT IS INOP.

Part: PLACARD — DETERIORATED (CABIN) · airframe 9,527 hrs · 7,995 cycles

PAX DOOR EXIT PLACARD DETERIOTATED.

Part: LAMP — BURNED OUT (CABIN)

DURING A HANGAR INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING APPROACH FROM ATL-FWA, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE FLAPS AT ZERO AND CONDUCTED A GO AROUND UPON DESCENT INTO FWA. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED IN FWA WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE FLAPS SYSTEM WITH NO DEFECTS FOUND AND RESET THE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BPSU — MALFUNCTIONED (TE FLAPS)

DURING CLIMBOUT, AT APPROXIMATELY 10,000 FT, THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE FLIGHT CONTROL PAGE WAS CHECKED AND THE FLAPS WERE HIGHLIGHTED AMBER ZERO ON THE SCHEMATIC DIAGRAM. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT PERFORMED A ZERO FLAPS LANDING WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT BPSU AND RIGGED THE FLAPS AND PERFORMED A TORQUE CHECK IAW AMM 27-50-00. THE FLAPS WERE CYCLED WITH NO DEFECTS NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — BINDING (PASSENGER DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS BINDING. MAINTENANCE OPERATED THE PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LOOP — OUT OF POSITION (LT PYLON)

FLT 4578 - DURING CRUISE FROM ATL-BTR, AT APPROXIMATELY 26,000 FEET, THE CREW RECEIVED AN INTERMITTENT LEFT 14TH STATE DUCT MASTER WARNING WHICH BECAME CONSTANT. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY . THE AIRCRAFT DIVERTED TO MGM AND LANDED SAFELY. MAINTENANCE FOUND THE 14TH STAGE PYLON LOOP TOUCHING THE FRAME AND THE PYLON LOOP WAS REPOSITIONED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)