N305FA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,546 hrs · 34,412 cycles

EMERGENCY LIGHT OUT IN CEILING PANEL.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,473 hrs · 34,382 cycles

AFT AIRSTAIR LIGHT MISSING, FOUND LIGHT DAMAGE.

Part: PA SYSTEM — MALFUNCTIONED (COCKPIT)

FLIGHT DECK PA VOLUME LOW AND HAS STATIC.

Part: STRUCTURE — DAMAGED (LT WING SLAT)

DURING WALK AROUND INSPECTION, BIRD STRIKE WAS FOUND AT LT WING NR 4 SLAT DAMAGED. R & R NR 4 SLAT ASSY IAW AMM 27-80-01.

Part: TRIM SYSTEM — INOPERATIVE

ALTERNATE TRIM INOPERATIVE AND STALL WARNING INDICATION LIGHT ON IN FLIGHT. ACFT DIVERTED.

Part: WARNING LIGHT — ILLUMINATED

ALTERNATE TRIM INFORMATION AND STALL WARNING INDICATION LIGHT ON IN FLIGHT. ACFT WAS DIVERTED.

Part: WARNING MESSAGE — FALSE ACTIVATION

TAKEOFF WARNING OUT OF SLAT DISAGREEMENT LIGHT ON, RESET COULD NOT DUPLICATE.

Part: BUTTON — INOPERATIVE (INTERPHONE) · airframe 60,381 hrs · 34,337 cycles

AFT L2 INTERPHONE, CREW TO CREW BUTTON DOES NOT WORK, ON DONG OR LIGHT.

Part: PA SYSTEM — UNKNOWN · airframe 60,134 hrs · 342,919 cycles

INFLIGHT PA IS BARELY AUDIBLE. PERFORMED OPS CHECK OF PA SYS. NO DISCREPANCIES NOTED. SYS RETURNED TO SERVICE AMM 23-30-00.

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 60,646 hrs · 34,168 cycles

AFT CABIN SMOKE ALARMS ACTIVATED IMMEDIATELY AFTER TAKEOFF, ACRID ODOR OBSERVED ON FLIGHT DECK AND IN CABIN, F/A NOTIFIED FLIGHT DECK OF SMOKE. EMERGENCY RETURN TO AIRFIELD .

Part: UNKNOWN — SMOKE (COCKPIT AND CABI) · airframe 60,046 hrs · 34,168 cycles

SMOKE IN COCKPIT CABIN RIGHT AFTER TAKEOFF. OPEN

Part: ADI — FAILED · airframe 60,012 hrs · 34,156 cycles

CAPTAIN ADI INDICATOR TUMBLED ENROUTE. QRL DID NOT SOLVE ISSUE.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 59,999 hrs · 34,152 cycles

RIGHT PACK UNABLE TO MAINTAIN CABIN. DESCENDED TO 13,000 FROM 24,000: POWER SETTING : 1.3 EPR ALTITUDE 13,000 FT CABIN ALTITUDE: 9,100 FT. PACK SUPPLY: 24 PSI SUPPLY TEMP FULL COLD AUTO AND MANUAL 65-74 CONTROLLER FULLY CLOSED: AUTO/MANUAL FLOW LIGHT ON BOTH CONTROLLERS 1 AND 2.

Part: WARNING LIGHT — ILLUMINATED · airframe 41,434 hrs · 21,388 cycles

ART INOPERATIVE ANNUNCIATOR CAME ON WITH FLAPS/SLATS EXTENDED-RECYCLED FLAPS/SLATS AND CAME ON AGAIN: PERFORMED SYS MX BITE TEST. FOUND NO FAULTS ON GROUND AFTER SPEAKING WITH CREW, FAULT SEEMS TO BE INTERMITTENT.

Part: CONNECTOR — DIRTY (ANTI SKID SYS) · airframe 59,808 hrs · 34,050 cycles

DURNING TAXI OUT LT INBD, RT INBD, LT OTBD, RT OTBD, ANTI-SKID LIGHTS CAME ON. FOUND CONNECTOR PLUG AT ANTI-SKID DUAL VALVE DIRTY. CLEANED CONNECTOR PLUG, AND OPS CHECK NORMAL.

Part: AIRSTAIR — INOPERATIVE · airframe 59,785 hrs · 34,042 cycles

AFT AIRSTAIR CAT WALK WILL NOT STAY IN UP POSITION.

Part: DOOR — DAMAGED (COCKPIT) · airframe 59,561 hrs · 33,902 cycles

DURING TAKE OFF JUST PRIOR TO ROTATION, FLIGHT DECK DOOR FLEW OPEN AND JAMMED OPEN. TESTED DOOR LOCK MECHANISM, OPS CHECKED GOOD IAW AMM 52-50-01. WHEN DOOR FLEW OPEN IT JUMPED THE STOPS. SECURED HARDWARE TO STOPS IAW AMM 20-30-01. ACFT RETURNED TO SERVICE.

Part: STOP — DAMAGED (COCKPIT DOOR) · airframe 59,561 hrs · 33,902 cycles

DURING TAKEOFF, JUST PRIOR TO ROTATION, FLIGHT DECK DOOR FLEW OPEN AND JAMMED OPEN. TESTED DOOR LOCK MECHANISM OPS CHECKED GOOD IAW CMM 52-50-01. WHEN DOOR FLEW OPEN, IT JAMMED THE STOPS. SECURED HARWARE TO STOPS IAW CMM 20-30-01.

Part: PLACARD — DEFECTIVE (CABIN) · airframe 59,507 hrs · 33,870 cycles

SELF ILLUMINATING EXIT SIGNS FAIL TEST AT COCKPIT DOOR AND MID AISLE POSITIONS (2 EA). R & R SELF ILLUMINATING EXIT SIGNS AT COCKPIT DOOR AND MID AISLE IAW MM 11-00-01. FUNCTIONAL TESTED SELF ILLUMINATING EXITS SIGNS IAW MM 33-53-01.

Part: WEB — CORRODED (BS 1211) · corrosion level 2 · airframe 59,507 hrs · 33,870 cycles

CORROSIONS AT AFT CARGO DOOR CUT OUT AT TORQUE BOX WEB AT BS 1211 UNDER TIE DOWN TRACK. BLENDED OUT CORROSION, AFTERWARD, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-10. REMOVE DAMAGED SECTION OF THE WEB IAW SRM 51-70-4, FABRICATED REPAIR WEB SECTION AND REPAIR SPLICE IAW SRM 51-10-2 AND 51-10-4 INSTALLED FABRICATED REPAIR PARTS PARTS IAW SRM 51-70-4.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,507 hrs · 33,870 cycles

CORROSION ON CARGO TIE DOWN TRACK ANGLES AT FS 1212 AT RBL 23 IN AFT CARGO COMPARTMENT. EVALUATED THE CORROSION ON CARGO TIE DOWN TRACK ANGLES, CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED ANGLES IAW SRM 53-30-05. FABRICATED REPAIR ANGLES IAW SRM 53-05. LOCATED, DRILLED AND TREATED REPAIR ANGLES IAW SRM 53-05 AND 51-10-3. INSTALLED REPAIR ANGLES IAW SRM 53-05 AND 51-30-5.

Part: SKIN — CORRODED (BS 229-279) · corrosion level 3 · airframe 58,896 hrs · 33,516 cycles

PULLING RIVETS AND SKIN BULGING AT FORWARD LAVATORY SERVICE PANEL BOTTOM FORWARD CORNER FROM BS 237 TO 256 LONGERONS 19-21L. REMOVED FORWARD LAVATORY SERVICE PAN AND AFTER FURTHER EVALUATON CORROSION WAS DISCOVERED WIDE SPREAD BETWEEN INNER AND OUTER SKIN DOULBLER. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. DAMAGE WAS FOUND TO BE OUTSIDE OF THE REPAIRABLE LIMITS WITHIN THE SRM. REQUESTED AND RECEIVED ENGINEERING SUPPORT FOR A REPAIR SCHEME. RECEIVED FUSELAGE SKIN REPAIR FROM FLIGHT VEHICLE CONSULTING INC, DRAWING FVC 53-12367. THE REPAIR NOW INCOMPASSED FS 229 TO 279 AND L 18L TO L 22L. REMOVED ALL CORROSION IN AND AROUND THE AFFECTED AREA. FABRICATED INNER AND OUTER REPAIR DOUBLERS FROM INSTRUCTION ON DWG FVC 53-12367-1. LOCATED AND INSTALLED ALL REPAIR PARTS IAW FVC DWG 53-12367.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,715 hrs · 33,426 cycles

OVERHEAD CEILING EMERGENCY LIGHTS OUT IN ROW 21 AND 26.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,715 hrs · 33,426 cycles

OVERHEAD CEILING EMERGENCY LIGHTS OUT IN ROWS 21 AND 26.

Part: BUTTON — DIRTY (F/A PANEL) · airframe 58,548 hrs · 33,350 cycles

PILOT CALL BUTTON ON F/A PANEL AT L1 DOES NOT WORK. THERE IS NO CHIME "ATTND CALLING" LIGHT DOES NOT WORK. CLEANED ATTENDANT TO PILOT CALL BUTTON AT L1 DOOR IAW SWPM 20-00-09. OPS CHECK GOOD IAW MM 33-23-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE SERVICE CHECK, MX DISCOVERED THE EMERGENCY CABIN OVERHEAD CEILING LIGHTS IN ROWS 21L, 23L, 23R, 28L, 29L, AND 29R INOPERATIVE. MX R & R BATTERIES AT LOCATION 909R AND 1057, OPS CHECKED GOOD IAW AMM 33-53-00.

Part: UNKNOWN — MULTIPLE FAIL · airframe 58,420 hrs · 33,295 cycles

REF SDR : LOST PRIMARY TRIM AFTER DEPARTURE, PRIMARY LONGITUDINAL TRIM BRAKE C/B POPPED, RESET, POPPED AGAIN, ALT LONG TRIM WORKED NORMAL. STALL INDICATION FAILURE WENT OFF AND ON THROUGH FLIGHT, AUTO SLOT FAIL" CAUTION ILLUMINATED RANDOMLY.

Part: HANDSET — INOPERATIVE (PA/INTERPHONE) · airframe 58,367 hrs · 33,258 cycles

L1 HANDSET INOPERATIVE, PA INTERPHONE FLIGHT DECK.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (LEFT) · airframe 58,315 hrs · 33,222 cycles

DURING CLIMBOUT, AUTOTHROTTLE DISENGAGED, LT THROTTLE WAS 2 HANDLE WIDTHS AHEAD OF RT, TRIED TO MATCH EPR RT ENGINE N1 & N2 DIFFERED BY OVER 20 PERCENT SIDE TO SIDE

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 57,708 hrs · 32,904 cycles

ON DEPARTURE NOTICED RED " NOSE" GEAR LIGHT ON AFTER GEAR RETRACTION, QRH PROCEDURE, CYCLED GEAR, NOSE GEAR LIGHT ON WITH LOUD AIR NOISE, NOSE INDICATOR PIN ON CONSOLE RETRACTED. AC ACCOMPLISHED AN UN SCHEDULED LANDING IN AIRPORT OF FLIGHT ORIGINATION. ISSUED A SPECIAL FERRY PERMIT FOR REPAIRS.

Part: DOOR — OUT OF ADJUST (MLG) · airframe 57,708 hrs · 32,904 cycles

AFTER TAKEOFF, RED NOSE GEAR UNSAFE ANNUNCIATOR ILLUMINATED UPON GEAR RETRACTION. QRH PROCEDURE FOLLOWED NO CHANGE RETURNED TO DEPARTURE. UPON ACFT ARRIVAL THE ACFT WAS PLACED ON JACKS AND A FUNTIONAL CHECK REVEALED THAT THE LANDING GEAR DOORS WERE OUT OF ADJUSTMENT. MX AT ASCENT MRO ACCOMPLISHED NLG DOORS/LINKAGED ADJUSTMENT IAW AMM 32-22-01. REPLACED NLG GROUND INTERLOCK SWITCH IAW AMM 32-60-05. ACCOMPLISHED TRIPLE GEAR SWING, CYCLED SEVERAL TIMES AND ALL INDICATIONS ON RETRACION ARE NORMAL. REF AMM 32-60-05.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 57,708 hrs · 32,904 cycles

ON DEPARTURE NOTICED RED " NOSE" GEAR LIGHT ON AFTER GEAR RETRACTION, QRH PROCEDURE, CYCLED GEAR, NOSE GEAR LIGHT ON WITH LOUD AIR NOISE, NOSE INDICATOR PIN ON CONSOLE RETRACTED. AC ACCOMPLISHED AN UN SCHEDULED LANDING IN AIRPORT OF FLIGHT ORIGINATION. MOC ISSUED A SPECIAL FERRY PERMIT (ASCENT) FOR REPAIRS.

Part: GYRO — FAILED (DIRECTIONAL) · airframe 57,627 hrs · 32,862 cycles

PRIOR TO DEPARTURE, CABIN FILLED WITH SMOKE, EVACUATED. CAPTAIN'S HEADING FLAG IN VIEW. CONDUCTED A SCAN FOR HOT SPOTS USING THERMAL IMAGING, NO HOT SPOTS OBSERVED. MX PERFORMED INSPECTION OF ALL READILY ACCESSIBLE AREAS. ACCOMPLISHED RTS OF ALL SYS IAW AMM 22-01-05 ALL SYS ARE OPERATING NORMAL. R & R DIRECTIONAL GYRO IAW AMM 34-21-04 PERFORMED RTS IAW AMM 22-01-05, OPS CHECKED GOOD. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. NO FURTHER REPORTS OF SMOKE IN CABIN REPORTED.

Part: PANEL — MISINSTALLED (COCKPIT) · airframe 20,151 hrs · 9,416 cycles

ABORTED TAKEOFF. DURING TAKEOFF ROLL, FLIGHT CREW REPORTED AIRCRAFT WOULD NOT STEER TO LT. TAKEOFF REJECTED AT APPROXIMATELY 60 KNOTS. FOUND LOWER SIDEWALL PANEL IN FLIGHT DECK, RT SIDE BETWEEN STA 178 AND 254, IMPROPERLY INSTALLED AND INTERFERRING WITH FIRST OFFICER'S RT RUDDER PEDAL. REINSTALLED PANEL PROPERLY PER MM 25-11-21. RUDDER PEDALS MOVED FREELY THROUGH FULL TRAVEL WITH NO INTERFERENCE. PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION. NO DISCREPANCIES FOUND.

Part: INTERCOSTAL — CORRODED (STA. 747-767) · corrosion level 2 · airframe 18,239 hrs · 8,278 cycles

DURING C-6 CHECK, INSPECTION REPORTED INTERCOSTAL AT STR. 26-R BETWEEN STA.747-767 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DRAWING 69-16500, ITEM 4, AND SRM 51-40-02.

Part: SKIN — DAMAGED (LOWER FUSELAGE)

LGA - FLT 417 - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED BELT LOADER STRUCK AIRCRAFT AFT OF FORWARD CARGO DOOR, SECTION 43, FS 500, BETWEEN STRINGER 23R AND 25R, CREATING A VERTICAL HOLE IN THE FUSELAGE SKIN APPROXIMATELY 12 TO 14 INCHES LONG. MAINTENANCE INSTALLED TEMPORARY DOUBLER AND FERRIED AIRCRAFT TO DEN. REPAIRED DAMAGED AREA PER EA 53-737-078B AND EA 53-737-079. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - PRIOR TO DEPARTURE, MAINTENANCE REPORTED EMERGENCY FLOOR PROXIMITY PATH LIGHTING INOPERATIVE AT ROWS 6 THROUGH 11. MAINTENANCE REPAIRED FAULTY GROUND WIRE PER EA 25-737-064. (M)

Part: BATTERY — DISCHARGED (ESCAPE SLIDE)

DEN - DURING C-3 CHECK INSPECTION, REPORTED AFT ENTRY DOOR ESCAPE SLIDE BATTERY FAILED BATTERY CHECK. MAINTENANCE REPLACED AFT ENTRY DOOR ESCAPE SLIDE. (M)

Part: BATTERY — DISCHARGED (L2 DOOR SLIDE)

DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOTLAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X)

Part: BATTERY — DISCHARGED (L1 DOOR SLIDE)

DEN - DURING C-CHECK, INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X)