N24633

Part: WARNING SYSTEM — FALSE ACTIVATION (MLG) · airframe 44,199 hrs · 23,175 cycles

AFTER T/O WHEN GEAR HANDLE PLACED IN UP MAIN GEAR DID NOT INDICATE UP NOSE GEAR INDICATED NORMAL. PERFORMED OPS CHECK OF MLG SYSTEM REF AMM 32-32-00, CYCLED MLG SEVERAL TIMES. NO DEFECTS NOTED AT THIS TIME. ALSO CHECKED UPLOCK SENSORS FOR PROPER ADJUSTMENT REF AMM 32-61-21. NO DEFECTS FOUND, A/C OK TO CONTINUE.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 43,264 hrs · 22,653 cycles

LT AFT LAV D AFT I/B MOUNT BLOCK CORRODED. REMOVED AND REPLACED I/B MOUNT BLOCK PER ECRA 2540-01746.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,264 hrs · 22,653 cycles

SUPPORT TASK - FLOOR SUPPORT CRACKED BETWEEN STA 344-360 BL 0. REMOVED AND REPLACED FLOOR SUPPORT REF SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,264 hrs · 22,653 cycles

SUPPORT TASK - FRAME AT STA 303 IS CRACKED AT STRINGER 16L CUTOUT. REPAIRED FRAME AT STA 303 PER EA 5310-04659.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

FRAME CRACKED AT STATION 597 BETWEEN STR 8 AND 9 LEFT. INSTALLED REPAIR PER ECRA 5311-01443 INITIATED DIP 092289 TO READ AS FOLLOWS, BEFORE THE ACCUMULATION OF 76,000 TOTAL AIRCRAFT FLIGHT CYCLES PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-01443 BEFORE THE ACCUMULATION OF 76,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER ECRA 5311-01443 PART 2.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 37,426 hrs · 19,547 cycles

VERTICAL STAB RIGHT INBOARD AFT LUG BOTH BUSHINGS HAVE CORROSION. REMOVED AND REPLACED CORRODED BUSHINGS REF BAC DWR 65-52274 AND SOPM 20-50-03.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 37,426 hrs · 19,547 cycles

VERTICAL STAB LEFT INBOARD AFT LUG BOTH BUSHINGS HAVE CORROSION. REMOVED AND REPLACED BOTH BUSHINGS REF BAC DWG 65-52274 AND SOPM 20-50-03.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

L-1 FORWARD ENTRY DOOR UPPER HINGE CUTOUT, 1/8 INCH CENTER HOLE HAS A CRACK INDICATION AT THE 3:00 O'CLOCK POSITION, INBOARD STRUCTURE. REPAIR WAS ACCOMPLISHED PER EC/RA 5331-01440.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

L-1 DOOR BEAR STRAP HAS A CRACK INDICATION AT HOLE BELOW UPPER DOOR HINGE CUTOUT. REPAIR WAS ACCOMPLISHED PER EC/RA 5331-01440.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

FUSELAGE CHEM-MILL POCKET HAS CRACK INDICATION AT STRINGER 4R STATION 867. REPAIR AND DOUBLER INSTALLATION WAS ACCOMPLISHED PER EC/RA 5331-01439 AND OPERATION 2 OF EA 5330-03455 REV A.

Part: ATTACH FITTING — WORN (HORIZ STAB) · airframe 37,426 hrs · 19,547 cycles

LEFT HORIZONTAL STABILIZER OUTBOARD ATTACH PLATES FOR ELEVATOR OUTBOARD HINGE FITTING NUMBER 6 ARE WORN. REPAIRED LEFT HORIZONTAL STABILIZER OUTBOARD ATTACH PLATES FOR ELEVATOR OUTBOARD HINGE FITTING PER ECRA 5552-01019.

Part: FRAME — CORRODED (BS 807 S27L) · airframe 37,426 hrs · 19,547 cycles

AFT CARGO COMP. BELTFRAME HAS CORROSION AT FWD LWR AREA STA BS 807 AND STRINGER S27L REPAIRED BELTFRAME SHEAR TIE IAW SRM 53-00-07 REPAIR 3 AT STA 807 STR 27L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

FRAME CRACKED AT STATION 400 BETWEEN STRINGER 8 AND 9 RIGHT. REPAIRED FRAME AT STATION 400, STRINGER 8R - 9R, PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,426 hrs · 19,547 cycles

FRAME CRACKED AT STATION 867 BETWEEN STRINGER 8 AND 9 LEFT. REPAIRED CRACKED FRAME PER EA 5310-04498, OP 2.

Part: FRAME — CRACKED (BS 727B S8-9L) · airframe 37,426 hrs · 19,547 cycles

FRAME CRACKED AT STATION 727B BETWEEN STRINGER 8 AND 9 LEFT. CUT OUT DAMAGED AREA FROM FRAME STA 727B BETWEEN STR 8 AND 9 LT INSTALLED REPAIR ANGLES PER EA5310-04498 OP2.

Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 37,426 hrs · 19,547 cycles

FRAME CRACKED AT STATION 380 BETWEEN STR 8 AND 9 RIGHT. CUT OUT DAMAGED AREA FROM FRAME AT STATION 380 BETWEEN STRINGERS 8 AND 9 RIGHT. INSTALLED REPAIR ANGLES PER EA5310-04498 OP2.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 35,930 hrs · 18,756 cycles

SMELLED SMOKE IN MID CABIN, HEARD GRINDING NOISE AT THE SAME TIME. TROUBLESHOT SYSTEM, REPLACED RECIRCULATION FAN. OPS CHECKED GOOD, REF M/M 21-21-22 PG 401. ROTABLE PARTS CHANGE WAS INDICATED - TT 0828156, S/N OFF 02329 FAN, AIR, DISTR OFF 03-2168-9-0001 2329 ON 03-2168-9-0001 3267.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 25,021 hrs · 13,042 cycles

INSPECTION FOUND A PUNCTURE IN THE RT ELEVATOR UPPER SKIN AT ELEVATOR STA 137.59. THE ELEVATOR SKIN WAS REPAIRED IAW ECRA 5520-01339.

Part: SKIN — CRACKED (LT WING) · airframe 25,022 hrs · 13,042 cycles

INSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER L/E SKIN AT NR 3 SLAT ACTUATOR. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-41-01.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 25,022 hrs · 13,042 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOORBOARD CHANNEL AT STA 537.45, BL 0 TO RBL 14. THE FLOORBOARD CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: WIRE — SHORTED (CABIN) · airframe 19,211 hrs · 9,889 cycles

THE EMERGENCY AISLE LIGHTING AT ROWS 5-9 LEFT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE FOUND SEAT 8 MOUNTED EMERGENCY LIGHT WIRING SHORTED. THE SHORTED SECTION OF WIRING WAS REPAIRED IAW WDM 33-51-41.

Part: FLOORBEAM — CORRODED (STA 986.5) · airframe 19,186 hrs · 9,872 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 4, LBL 30, AND RBL 38. A STRAP DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-51.