N887GA

Part: CLAMP — DISCONNECTED (COOLING DUCT) · airframe 55,432 hrs · 36,657 cycles

FLOW LIGHT ILLUMINATED AND CABIN ALTITUDE BEGAN TO CLIMB AT MAX RATE WITH OUTFLOW VALVE FULLY CLOSED. EMERGENCY DECLARED. EXECUTED QRH PROCEDURE AND FOUND COOLING TURBINE DUCT TO WATER SEPERATOR V CLAMP DISCONNECTED. RECONNECTED CLAMP.

Part: FUEL CONTROL — FAULTY (NR 2 ENGINE) · airframe 52,401 hrs · 36,038 cycles

RIGHT ENG WAS SURGING WHILE CLIMBING TO FL 330. ALL ENG INDICATIONS WERE FLUCTUATING, FF +- 200 N1 UP TO 10 EPR 1.90 2.02. VIDEO WAS EMAILED TO MTC CONTROL SHOWING FLUCTUATIONS. THROTTLES WERE STATIONARY DURING FLUCTUATIONS. LT ENG WAS FLUCTUATING TOO, BUT NOT AS SEVERE AS THE RT ENG. ENGS STABILIZED AFTER LEVEL OFF & ENG ANTI-ICE TURNED ON. FLIGHT ATTENDANT REPORTED NO COMPRESSOR STALL NOISES FROM THE BACK OF THE PLANE. FOUND NR 2 ENG FUEL CONTROL BELLOWS REQUIRE SERVICE. CHECKED MOISTURE TRAP & SERVICED BELLOWS IAW AMM 73-00-00-01.

Part: STRUT — LEAKING (NLG)

AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. WHEN THE MLG DID NOT RETRACT, THERE WERE SEVERAL CONFIGURATION WARNINGS. FLAP WARNING, STABILIZER WARNING & STALL INDICATION FAILURE. THE CREW DID THE QRH PROCEDURE FOR GEAR HANDLE LOCKED DOWN AFTER TAKEOFF ON PAGE 32.6 OF THE QRH. THEY DID THE ELEC GND SHIFT FAILURE PROCEDURE & THE AUTO SPOILER FAIL PROCEDURE AS DIRECTED BY THE QRH. ALSO DID THE STALL INDICATION FAILURE & FALSE STALL WARNING ON PAGE 85.4 OF THE QRH. THEY LOST THE FLIGHT DIRECTOR, THE AUTOPILOT DID NOT WORK & THE ACFT DID NOT PRESSURIZE. THEY TOOK OFF AT 1715 UTC, THEY ASKED THE TOWER CONTROLLER TO STOP THEIR CLIMB TO RUN THE CHECKLIST & PROCEDURES. THEY DID CLIMB TO 5000 FEET AND THEY WERE HANDED OFF TO THE DEPARTURE FREQUENCY. THE ACFT WAS NOT OVERWEIGHT FOR THE LANDING BACK. ACFT HANDLED & OPERATED NORMALLY AFTER LANDING & THEY TAXIED BACK TO A GATE. OUND NLG BOTTOMED OUT & GLAND NUT LEAKING FLUID. REPACKED STRUT & SERVICED IAW TASK CARD 32-047-003 & 32-047-004 REF LOG PAGE 635108. PREFORMED GEAR SWING IAW MM 32-30-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

L1 DOOR EMER EXIT LIGHT INOPERATIVE. REPLACED BATTERIES FOR L1 DOOR EMER EXIT LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: AUTOPILOT SYS — DISENGAGED · airframe 51,927 hrs · 35,799 cycles

IN FLIGHT, AIRCRAFT BANKED HARD TO THE LEFT WITH AUTOPILOT ENGAGED, THEN HARD TO THE RIGHT, FLIGHT DIRECTERS DISENGAGED AND AUTOPILOT DISENGAGED, PERFORMED RTS ON DFGC 1 & 2, GO-REPORTED FROM BOTH. OK FOR CONTINUED SERVICE IAW MM 22-01-05.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,802 hrs · 35,727 cycles

THREE TAIL SECTION EMER LIGHTS ABOVE SLIDE ARE INOPERATIVE, STATION 1539L. R & R EMER LIGHT BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN)

TAIL COMPARTMENT EMER LIGHTS VERY DIM. REPLACED BATTERIES IN POWER SUPPLIES. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: BATTERY — DISCHARGED (CABIN)

ROWS 27 - 29 EMER LIGHTS VERY DIM. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: PLATE — CORRODED (COCKPIT)

ON CAPTAIN'S FWD WINDSHIELD OTBD VERTICAL RETAINER PLATE CORROSION PRESENT ON TOP. R & R CAPTAIN'S WINDOW AFT RETAINER IAW MM 56-10-01-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,849 hrs · 35,215 cycles

REF LOG PAGE 606701 RT LONGERON 20 CRACK EXTENDS 1/8 " BEYOND FASTENER HOLE. STOP DRILLED CRACK WITH REFERENCE TO ENGINEERING TELEPHONE REQUEST FOR EA 20-2015-071 REVISION. SEE LP FOR HFEC VERIFICATION THAT CRACK TERMINATED.

Part: LIGHT — INOPERATIVE (TAIL CONE) · airframe 50,289 hrs · 34,922 cycles

AFT TAIL CONE SLIDE EMER LIGHT ASSEMBLY INOPERATIVE. R & R AFT TAIL CONE SLIDE EMER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (TAIL CONE) · airframe 50,289 hrs · 34,922 cycles

AFT TAIL CONE SLIDE EMER LIGHT ASSEMBLY INOPERATIVE. R & R AFT TAIL CONE SLIDE EMER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (TAIL CONE) · airframe 50,289 hrs · 34,922 cycles

TAIL CONE RELEASE HANDLE EMER LIGHT INOPERATIVE. R & R EMER LIGHT BATTERY PACK B5-28 IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,240 hrs · 34,897 cycles

EXIT IDENTIFIER LIGHT AT AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERIES IN LIGHT ASSEMBLY AT AFT ENTRY DOOR IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (TAIL CONE) · airframe 50,162 hrs · 34,861 cycles

EMERGENCY TAIL CONE EXIT IDENTIFIER LIGHT DIM. REPLACED LT BATTERY IN EMER TAIL CONE EXIT IDENTIFIER LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN LT CUSP WEB CORRODED OUT OF THE LIMITS STATION 484 - 541. REMOVED DAMAGED CUSP MEMBRANE, TRIMMED OUT DAMAGE FROM MEMBRANE. FABRICATED FILLERS, HIGH DOUBLERS, DOUBLER & INSTALLED REPAIRS PARTS IAW SRM53-05 FIGURE 131 A-17.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CUSP WEB CORRODED BETWEEN STATIONS 503 & 617. REMOVED & CUT OUT DAMAGE ON CUSP WEB. FABRICATED MULTIPLE FILLERS, DOUBLERS, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 53-05 FIGURE 131A-8.

Part: SKIN — CORRODED (FUSELAGE)

LEFT EXTERNAL SKIN CORRODED UNDER RUB STRIP STATION 769 TO 826. BLEND REPAIR IN LIMITS EXCEPT AT STATION 790. FABRICATED FILLER, DOUBLER & INSTALLED IAW SRM 53-04 FIGURE 57. DOUBLER MEASURES 8" X 8".

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT AFT CABIN CUSP WEB CORRODED IN NUMEROUS AREAS FROM STATION 1036 TO 1130. CUT OUT DAMAGED AREAS, FABRICATED FILLERS, DOUBLERS, LOCATED, DRILLED & INSTALLED IAW SRM 53-05 FIGURE 131A-7.

Part: FAIRING — DAMAGED (VERTICAL STAB)

VERTICAL STAB LE FAIRING AT SPAR CAP HAS ONE EACH ELONGATED HOLE, 2 ROWS ABOVE STATION ZFS 52.267 LT SIDE 6TH ROW FROM BOTTOM. REMOVED DAMAGE FOR BUSHING REPAIR, HFEC INSPECTED NO CRACKS NOTED IAW SRM 55-03 PARA 27. FABRICATED BUSHING & INSTALLED BUSHING IAW SRM 55-03 PARA 27 FIGURE 29.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK CORRODED OUT OF LIMITS STATION 237. REMOVED DAMAGED SEAT TRACK. LOCATED, DRILLED & INSTALLED A REPLACEMENT SEAT TRACK IAW SRM 51-10-4, 51-30-5 & 51-30-1.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN RT CUSP WEB CORRODED BETWEEN STATIONS 275 & 313. CUT OUT DAMAGED SECTION OF CUSP WEB, RECEIVED NEW WEB SECTION. FABRICATED RING DOUBLER, LOCATED, DRILLED & INSTALLED REPLACEMENT WEB SECTION & REPAIR PARTS IAW SRM 53-05 FIGURE 131A-13.

Part: CUSP WEB — CORRODED (FUSELAGE)

PASSENGER CABIN CUSP WEB STATION 1160 UNDER L2 DOOR AFT GRIT BAR FITTING CORRODED. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 51-90-4 FIG 4.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

FORWARD CABIN UPPER EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN UPPER EMERGENCY FLASHLIGHT BATTERY PACK IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

AFT ATTENDANT`S JUMP SEAT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R EA BATTERIES & OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MAINTENANCE R & R THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECK WAS NORMAL. THE ACFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO PIT FRAME AT STATION 1099 CORRODED AT LONGERON 29R 3029L ATTACH POINT. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SPAR — DAMAGED (LT HORIZ STAB)

LEFT HORIZONTAL STABILIZER L/E SPAR AT STATION XHS107 UPPER HOLE ELONGATED. REMOVED DAMAGE AND FREEZE PLUG HOLE.

Part: SPAR — DAMAGED (LT HORIZ STAB)

LEFT HORIZONTAL STABILIZER L/E SPAR AT STATION XHS154 UPPER HOLE ELONGATED. REMOVED DAMAGE AND FREEZE PLUG HOLE.

Part: SEAT TRACK — GOUGED (FUSELAGE)

PASSENGER CABIN SEAT TRACK GOUGED AT STA 965 LBL 72. REMOVED DAMAGE, FABRICATED AND INSTALLED.

Part: SKIN — CHAFED (TE FLAP VANE)

RIGHT WING I/B FLAP O/B VANE HAS 2 EA CHAFES ON UPPER SKIN AT I/B END. CUT OUT DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED REPAIR PARTS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE)

BIRD STRIKE DURING LANDING, DENT ON RT FWD SIDE OF FUSELAGE APPROX 3 O`CLOCK POSITION. DENT IS 28" X 19" X S 3/4" DEEP WITH PULLED RIVETS IN SECOND FRAME, BENT AND CRACKED. CUT OUT DAMAGED SKIN AND FRAMES, HFEC INSPECTED AREA NO CRACKS NOTED. FABRICATED SKIN, FILLERS, DOUBLERS AND STRAPS. RECEIVED REPLACEMENT FRAMES, LOCATED DRILLED AND INSTALLED FRAMES, SKIN AND REPAIR PARTS IAW AAR EA14718 AND MD80 SRM 53-04 FIG 62.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE POWER SUPPLY BATTERY PACK, OPS CHECK ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: DOUBLER — CRACKED (LT WING)

LT WING UPPER BEAVER TAIL DOUBLER ABOVE MLG AREA IS CRACKED FROM FASTENER TO EDGE (O/B SIDE). REPAIRED WO 2003754 N/R 657955 PER MD80 SRM 57-03 FIG 34, PAGE 143.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING SMELL FROM ROW 24 THROUGH THE AFT GALLEY. SMELL STRONGEST AT ROW 24 AND AFT GALLEY. OVERHEAD PANELS FROM ROW 22-27 FELT VERY HOT, WHILE SURROUNDING AREAS WERE ICE COLD. MAINTENANCE DEPARTMENT PERSONNEL GAINED ACCESS TO ALL BALLAST FROM ROW 18 BACK, INSPECTED ALL BALLAST AND WIRING, NO DEFECTS NOTED WITH BALLAST OR WIRING, REF AMM 33-21-03. RAN BOTH PACKS TO VERIFY OPERATION AND POSSIBLE SOURCE OF SMELL, NO DEFECTS NOTED, BOTH PACKS OPS CHECK GOOD. NO SMELLS NOTED REF AMM 21-00-00. LOADED UP BOTH ENGINE GENERATORS, NO DEFECTS NOTED WITH MAIN POWER SYSTEMS, REF AMM 24-20-00. INSPECTED A/C AND FOUND NO DEFECTS OR POSSIBLE SOURCES OF ELECTRICAL SMELL. AIRCRAFT RETURNED TO SERVICE.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, CORROSION CUSP FOUND AT STA 60 TO 67 RT. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, CORROSION ON CUSP STA 522-541 RIGHT. ADDRESSED AS REQUIRED.

Part: SKIN — CRACKED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND FUSELAGE SKIN CRACKED AT STA 1380, LONG 13R - 14R. REPAIRED PER AARD 53-30-00-02. ADDRESSED AS REQUIRED.

Part: BEAM — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND BEAM ABOVE MID CARGO DOOR OPENING CORRODED TOP SIDE STA 636 TO 693. REPAIRED PER SRM 51-30-05. ADDRESSED AS REQUIRED.

Part: SKIN — CRACKED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CRACK IN FUSELAGE SKIN STA 1380, BETWEEN L13 - L14 LT. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CORROSION ON CUSP BETWEEN STA 256-275 RT. ADDRESSED AS REQUIRED.

Part: FITTING — CRACKED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND 6EA DOOR STRAP FITTINGS CRACK (4 TIE DOWN ON FWD EDGE AND THE TOP AND 4TH FROM THE TOP ONE ON AFT EDGE). ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CORROSION ON LT CUSP, STA 526-537. REPAIRED PER ESO 80559, DATED 11/10/0/ & 11/13/09. ADDRESSED AS REQUIRED.

Part: SKIN — DAMAGED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, STATIC DISCHARGE BURN IN FUSELAGE SKIN STA 503, LONGERON 2 RIGHT. ADDRESSED AS REQUIRED.

Part: LONGERON — CRACKED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND LONGERON L-9R CRACKED AT STA 1271. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CORROSION IN CEILING MEMBRANE ON FWD SIDE OF CABIN FLOORBEAM STA 148, APPROX 10 INCHES RIGHT OF AIRCRAFT CENTER LINE. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CORROSION ON CUSP STA 845 TO 864 RT. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND CORROSION ON RT CUSP STA 886 TO 905. ADDRESSED AS REQUIRED.

Part: SPACER — CORRODED (THRESHOLD)

AFTER REMOVAL OF THRESHOLD, FOUND CORRODED SPACER AT LWR FRAME OF AFT CARGO DOOR CUTOUT OTBD SURFACE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: MANIFOLD — LEAKING (13TH STAGE BLEED)

FLIGHT CREW PERSONNEL REPORTED ON THE INITIAL CLIMBOUT OF FLIGHT 883-3 FROM PIE, THE FIRE DETECTOR HANDLE AND LOOP "A" ILLUMINATED ON THE LT ENGINE. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL PERFORMED A VISUAL INSPECTION OF THE LT ENGINE AND DETERMINED THE 13TH STAGE BLEED MANIFOLD LEAKING HOT BLEED AIR INTO THE ENGINE NACELLE. THE LT ENGINE WAS REPLACED IAW ALL AMM PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: FIRE LOOP — FAILED (LT NACELLE)

FLIGHT CREW PERSONNEL REPORTED ON THE INITIAL CLIMBOUT OF FLIGHT 883-1 FROM PIE, THE FIRE DETECTOR HANDLE AND LOOP "B" ILLUMINATED ON THE LEFT ENGINE. THE AIRCRAFT RETURNED TO ST. PETERSBURG, FL AND LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL PERFORMED A VISUAL INSPECTION OF THE LT ENGINE FIRE DETECTION "B" SYSTEM AND DETERMINED A FIRE LOOP DETECTOR WAS DEFECTIVE. THE "B" LOOP WAS DEFERRED IAW ALLEGIANT AIR MEL PROCEDURES AND THE AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S)

Part: BATTERY — FAILED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A)

Part: BATTERY — FAILED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A)

Part: BATTERY PACK — DISCHARGED (CABIN)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS, AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: PITOT LINE — DISCONNECTED

FLIGHT 707 SFB/DSM. THE FLIGHT CREW REPORTED THE LOSS OF CAPT'S ALTIMETER, MACH/AIRSPEED INDICATOR, EPR BUGS AND AUTO THROTTLE. 'NO MODE DISPLAY ON THRUST RATING PANEL. THE FLIGHT RETURNED WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPORT THAT THE PITOT LINE WAS FOUND DISCONNECTED FROM THE CADC NR 1 AT THE QUICK DISCONNECT. ATTACHED PITOT LINE TO NR 1 CADC PER AMM34-16-01. A SATISFACTORY OPERATIONAL CHECK OF CADC NR 1 WAS ACCOMPLISHED PER AMM 34-16-00. A SATISFACTORY AUTO PILOT RTS CHECK PER AMM22-01-05 WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: DISPLAY — UNKNOWN (COCKPIT)

FLIGHT 715 SFB/LAN - THE FLIGHT CREW REPORTED; DURING TAKEOFF ROLL "F/S FAIL" INTERMITTENTLY APPEARED ON BOTH PRIMARY FLIGHT DISPLAYS. REJECTED TAKEOFF AT 100 KTS. UPON CLEARING THE RUNWAY THE SYSTEM INDICATION RETURNED TO NORMAL. SFB MAINTENANCE REPORT THAT DFGC NR 2 FAILED A RETURN-TO-SERVICE TEST. THEY PERFORMED A LOGIC RESET ON DFGC NR 2 AND THE SYSTEM PASSED THE RETURN-TO-SERVICE TEST. THE AIRPLANE HAS RETURNED TO SERVICE.