N946UP

Part: FRAME — CORRODED (BS303 S10L-S9L) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, DURING INSPECTION OF SKIN CHANGE AREA FRAME AT BS 303 FOUND DAMAGED BETWEEN S10L AND S9L. CLEANED UP DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PART IAW SRM 51-40-4. INSTALLED REPAIR PART IAW SRM 51-40-4.

Part: HINGE FITTING — CRACKED (ENTRY DOOR) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C, DURING NDT OF ALL FASTENER HOLES COMMON TO SKIN CHANGE AT FWD ENTRY DOORWAY, CRACK FOUND IN FWD ENTRY DOOR UPPER HINGE LOWER FITTING. FITTING REPLACED IAW DRG 65-17684.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C 2 AREAS OF DELAM FOUND DURING SURFACE CORROSION REMOVAL ON LEFT I/B MIDFLAP AFT UPPER SKIN. NOTE THAT DURING REPAIR 2 AREAS OF DISBOND OCCURRED ON LOWER SURFACE. REPAIRS CARRIED OUT IAW SRM 51-40-20.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, VERTICAL FIN LEADING EDGE LOWER PANEL 9501, MATING STRAP HAS A CRACK IN THE OUTER SKIN. CRACK STOP DRILLED IAW SRM 51-10-01, REPAIR DOUBLER FABRICATED IAW SRM 51-20-01, FIG 7. REPAIR DOUBLER INSTALLED IAW SRM 51-30-02.

Part: FASTENER — CRACKED (SPAR) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, FOLLOWING HFEC INSPECTION AROUND FASTENER HOLES IN O/B FLANGES OF VERTICAL FIN FRONT SPAR FORGING, 2 CRACKS FOUND COMING FROM FASTENER HOLES ON LEFT SIDE. CRACKS STOP DRILLED IAW DRG 65-81528. REFERENCE SMRO EO 2003-041-001 FOR REWORK. REFERENCE UPS EO B727-5530-19081.

Part: SKIN — CRACKED (NR 4 KRUEGER) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, SMALL CRACK 1 INCH IN LENGHT ON TAI SKIN OF NR 4 KREUGER FLAP, JUST I/B OF ACTUATOR ROD END ATTACH POINT ON FLAP. RECTIFICATION CARRIED OUT IAW UPS EO B727-5750-3082.

Part: SUPPORT FITTING — CRACKED (SPOILER) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C NR 11 SPOILER SUPPORT FITTING IS CRACKED. FITTING REPLACED IAW UPS EO B727-5750-5182.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, NR 3 SLAT OUTER SKIN CRACKED ADJACENT TO I/B HOOK ATTACH POINT. HFEC INSP CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT CRACK CONFIRMED & END MARKED. REPAIR CARRIED OUT IAW SRM 51-10-1, 57-50-3 & 51-30-3.

Part: STRINGER — DAMAGED (B HYD SYS BAY) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, HOLE IN FLANGE OF STRINGER B-HYD SYS COMPARTMENT O/B OF HYD RESERVOIR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 2, DAMAGED REMOVED IAW SRM 51-10-06. CUT LINE TO BE NDT'D HFEC INSP CARRIED OUT AROUND CUT LINE ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00 -00 FIG 4 RESULT - NDF.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C NLG WHEEL WELL RT CEILING PRESSURE PANEL HAS A CRACK FROM OUTBOARD EDGE OF PANEL TO BOLT HOLE. PANEL REPAIRED IAW 2003-041-005. REFERENCE UPS ENGINEERING FILE NR 727-53-20125.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION AT LAP JOINT BS 820 TO BS 870, S-4R REPAIR CARRIED OUT IAW UPS EO B727-5330-0509.

Part: TAB — CONTAMINATED (ELEVATOR) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, FOLLOWING X-RAY INSPECTION OF RT ELEVATOR TAB, WATER INGRESS FOUND ON RT ELEVATOR TAB AT APPROX ELEV STA 95 TO ELEV STA 105. REPAIR CARRIED OUT IAW SRM 51-40-05.

Part: SKIN — DEBONDED (TE FLAPS) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, LEFT O/B AFT FLAP - DISBOND AT UPPER SURFACE 5 TO 20 INCHES FROM O/B END. REPAIR CARRIED OUT IAW SRM 51-40-20.

Part: SKIN — CRACKED (I/B MIDFLAP) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, LEFT I/B MIDFLAP LWR SURFACE 2 CRACKS AT FWD I/B & O/B CORNERS OF SKIN CUTOUT FOR I/B AFT FLAP ACTUATING ROD. CRACK STOP DRILLED TO .250 INCH IAW SRM 51-10-1. REPAIR CARRIED OUT IAW MRO EO 2003-041-002. UPS FILE NR 727-27-20007.

Part: SKIN — CRACKED (DOOR CUTOUT) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, EVIDENCE OF CRACK AROUND FASTENER AT MID GALLEY DOOR CUTOUT BS 640, S-8L. REPAIR CARRIED OUT IAW SMRO EO 2003-041-004. REFERENCE UPS EO B727- 5330-19065.

Part: PANEL — DEBONDED (NR 3 SPOILER) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C NR 3 SPOILER PANEL LOWER SURFACE DISBOND AT ACTUATOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-40-05.

Part: DOUBLER — CORRODED (BEAM) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, CORROSION ON DELTA BEAM LT WEB DOUBLER AT BS 740. REMOVED CORRODED DOUBLER IAW SRM 51-30-02. REMOVED CORROSION FOUND ON DELTA BEAM WEB & FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01 & 53-1 0-2. FABRICATED REPAIR PARTS IAW SRM 53-10-2. CARRIED OUT REPAIR IAW SRM 51-20-1 FIG 7.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, LIGHTNING STRIKE DAMAGE AT BS 590 S25R. FASTENER REMOVED AND AREA CLEANED IAW SRM 51-30-02. HFEC INSP CARRIED OUT ON DAMAGED AREA IAW B727 NDTM PT 6 FIG 4. RESULT CRACK FOUND AS MARKED ON A/C & ENDS OF CRACK MARKED. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 13.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C ENG NR 3 THRUST REV O/B FAIRING IS CRACKED NEAR FWD SUPPORT BRACKET UPPER EXISTING DOUBLER AT CRACK LOCATION REMOVED IAW SRM 51-30-02. CRACKS TOP DRILLED IAW SRM 78-30-01 0.025 HOLE. HFEC INSP CARRIED ON STOP DRILL IAW B727 NDTM PT 6 51-00-00 FIG 4 RESULT - CRACK CONTAINED. EXISTING DOUBLER RE-INSTALLED IAW SRM 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, FRAME CRACKED AT BS 1070 AND ATTACH POINT FOR AFT LWR CARGO DOOR. CRACKED FRAME AT BS 1070 REMOVED AND NEW FRAME INSTALLED IAW DRAWING NR65-18622.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, SKIN CRACKS FROM FASTENER HOLES BS 255 (AFT OF NR 3 RT WINDOW CUTOUT) BETWEEN S-10R AND S-9R. REPAIR CARRIED OUT IAW SRM 53-30-03, FIGURE 29.

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, ENG NR 3 THRUST REVERSER OUTER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE: C, SURFACE CORROSION ON ANGLE IN LT MLG WHEEL WELL AT BS 935 FWD OF 940 FITTING AT STR 19. REMOVED ANGLE IAW SRM 51-30-02. ANGLE FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. FABRICATED ANGLE IAW DRAWING 65-22419 & SRM 51-20-01 & 51-40-3. INSTALLED ANGLE IAW 51-30-03.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,500 hrs · 45,589 cycles

INSPECTION TYPE:C SKIN CRACK FOUND AT FWD CORNER CUTOUT OF FWD ENTRY DOOR S-7L. NOTE: WHEN NDT WAS CARRIED OUT IN REPAIR AREA, IT WAS FOUND THAT THERE WAS CORROSION BETWEEN THE SKIN AND BONDED DOUBLER IN THE AREA SURROUNDING THE FWD ENTRY DOOR SKIN PANEL P/N 65-18420-111. REPLACED IAW SHANNON MRO EO 2003-041-003. REFERENCE UPS EO B727-5330-19084.

Part: LATCH — OUT OF ADJUST (ENTRY DOOR)

INSPECTION TYPE:N/A, ENTRY DOOR HANDLE UNLATCHED ON LANDING FOUND DOOR ENTRYWAY PARTIALLY OPENED. ALSO ACFT SUFFICIENT TO MAINTAIN PRESSURIZATION IN AUTO/MAN. PERFORMED FWD ENTRY DOOR ADJ FOR SOFT UNLATCHING PER MM 52-11-00.

Part: STRINGER — CRACKED (STA 319)

INSPECTION TYPE:N/A STRINGER 20R CRACKED AT FRAME 294 FWD OF LAV WASTE CHUTE STRINGER REPAIRED AS PER SRM 53-10-03. STATION 319 TO 284.5 REPAIRED

Part: LAP JOINT — CORRODED (FUSELAGE)

INSPECTION TYPE:IN CORROSION AT CREW OXYGEN SERVICE PORT LAP SEAM, STRINGER 19R, STATION 360 TO 344 HAS CORROSION AT LAP SEAM. REMOVED FASTENERS HS 86801 10501 / REMOVED CORROSION HS 86801. VERIFIED REMOVAL OF CORROSION. REINSTALLED FASTENERS AS PER EO B727-533 0-15449-A AND EXTENDED CORRECTIVE ACTION FORM 05130.

Part: SMOKE DETECTOR — INOPERATIVE (CABIN)

MAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED AND DISPATCHED AIRCRAFT

Part: TRANSMITTER — INOPERATIVE (L1 DOOR)

INSPECTION TYPE:N/A, FWD L1 DOOR EMERGENCY BATTERY LIGHT DOES NOT TEST ON GROUND. REMOVED AND REPLACED TRANSMITTER, OPS CK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, ON EMERGENCY EXIT LIGHT TEST THE FOLLOWING LIGHTS FAILED MED EXIT MARKERS, RT GALLEY EXIT MARKER AND 2 GALLEY EXIT LOCATORS. REPLACED EMERGENCY EXIT BATTERIES PACKS, TESTED OK.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, ROW 2 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 2 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.

Part: PLATE — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, FWD L1 EMERGENCY EXIT ID AND PLATE IS INOPERATIVE DUE TO EMERGENCY LIGHT TEST INOP ON FWD L1 DOOR. REMOVED AND REPLACED BASE EXIT ID AND PLATE ON L1 DOOR.

Part: CONNECTOR — LOOSE (STICK SHAKER)

INSPECTION TYPE:N/A PILOT REPORT-STAB TRIM AND STICK SHAKER ON APPROACH CLEANED AND LUBED JACK SCREW. R/R CONNECTOR ON CAPT STICK SHAKER

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, CRACKED MAIN CARGO DOOR LATCH SUPPORT FITTING, BS 580 CRACK LOCATED A T-UPPER INBOARD FLANGE. INSTALLED SUPPORT FITTING REPAIR KIT IAW UPS EO B727-5310-0437I APPX 8.6 & 8.7.

Part: SPAR — CORRODED (CENTER FUEL CELL)

INSPECTION TYPE:C, OPEN AREA AT LOWER CHORD, AFT SPAR ON CENTER TANK OUTBOARD END, LEFT SIDE INSPECTION FOR SUSCEPTIBLE CORROSION. ACCOMPLISHED REPAIR OF WING CENTER SECTION REAR SPAR LOWER CHORD AT BBL 41.82 IAW UPS EO B727-5710-13234-A AND BOEING TELEX PRO-MIA-00-0 0052H.

Part: SPAR — CORRODED (CENTER FUEL CELL)

INSPECTION TYPE:C, CORROSION ON CENTER TANK, AFT SPAR, UPPER CHORD, OUTBOARD END, LEFT SIDE. ACCOMPLISHED WING CENTER SECTION REAR SPAR UPPER CHORD CORROSION REP AIR BETWEEN LBL 39.07 & LBL 70 IAW UPS EO B727-5710-13233-A, AVITAS EINGINEERING REPAIR ORDER AVHM-14R0-1 AND BOEING TELEX UPS-MIA 00-0001 4H.

Part: WEB — CRACKED (NLG WW)

INSPECTION TYPE:C, NOSE WHEEL WELL RIGHT SIDE VERTICAL WEB IS CRACKED AT BS 267, 5 INCHES DOWN FROM CEILING. STOP DRILLED CRACK AND INSTALLED WEB REPAIR IAW SRM 51-40-2 FIG 1.

Part: BULKHEAD — CRACKED (FUSELAGE)

INSPECTION TYPE:C, FORWARD PRESSURE BULKHEAD BS 178 FORWARD FACE BL 0 & WL 190 APPROXIMATELY HAS CRACK RUNNING FROM FASTENER. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR IAW UPS EO B727-5310-4290-B APPX B.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C, FUSELAGE SKIN BULGE AT STRINGER 10 LEFT BS 349 - 360. ACCOMPLISHED SKIN CORROSION REPAIR FROM STA 344 - 360, STR 10 - 9 LEFT IAW UPS EO B727-5330-13232A, BOEING TELEX UPS-MIA-00-00016H, AND AVI TAS ENGINEERING REPAIR ORDER AVHM-149RO-1.

Part: CONTROLLER — MALFUNCTIONED (MLG WW)

INSPECTION TYPE:N/A, WHEEL WELL FIRE INDICATION APPROX 6000 WITHIN 15 MILES OF SDF. ALSO, BELL CUTOUT DID NOT WORK PROPERLY, HAD TO HOLD BELL CUTOUT SWITCH IN. INSPECTED LOOPS, REMOVED AND REPLACED WHEEL WELL CONTROL UNIT. SYS OPS GOOD ON GROUND.

Part: BATTERY — INOPERATIVE (CABIN)

ALL EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED 7 EACH EMERGENCY EXIT LIGHT BATTERIES. REMOVED AND REPLACED REMOTE POWER ASSY. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A LH AFT OVERWG DOOR EMERG. LIGHT INOP REMOVED AND REPLACED BATT PACK OPS CHECK GOOD

Part: LIGHT — INTTERMITTENT (CABIN)

GREEN EXIT LIGHT AT FLOOR LEVEL AT FWD ENTRY DOOR BLINKS CONTINUOUSLY IN FLIGHT AND ON GROUND. RESET LIGHT ASSY, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT EXIT MARKER AT GALLEY DOOR FLOOR LEVEL FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

ROW 19 EMERGENCY LIGHT FAILED TEST. REPLACED BATTERY. OPS CHECKS GOOD.

Part: BATTER PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AFT OF LT FWD OVERWING EXIT WAS DIM. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF LT AFT OVERWING EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY PACK AT LT AFT OVERWING EXIT, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF FWD RT OVERWING EMERGENCY EXIT INOP, LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY AND BATTERY PACK, OPS CHECK GOOD. LIGHT ASSY (P/N 96-3-1032-2), BATTERY PACK (P/N 96-2-1015).

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AT FWD ENTRY ABOVE EMERGENCY FLASHLIGHTS WAS INOP. REPLACED BATT AND BULB, OP CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF RT AFT OVERWING EMERGENCY EXIT WAS DIM. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD.

Part: SWITCH — INOP (LT MLG DOOR)

INSPECTION TYPE:N/A, LEFT MAIN GEAR DOOR INDICATION UNSAFE FWD AND AFT. NO AIRFRAME VIBRATION NOTED. DEFERRED PER MEL 32-1. SWITCH AT FAULT INDICATION ONLY. REMOVED AND REPLACED LEFT MLG DOOR WARNING SWITCH IAW MM 32-62-11, OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A COCKPIT EMERG LIGHT DOES NOT FLASH DURING TEST EXIT LIGHT TESTED GOOD PER TC3000 AND MM

Part: BATTERY PACK — DISCHARGED (BAGGAGE COMPT)

INSPECTION TYPE:N/A, EMERGENCY LIGHT RIGHT SIDE JUST FWD OF AFT LOWER PIT DOOR INOP. REMOVED AND REPLACED LIGHT BATTERY PACK, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 19)

INSPECTION TYPE:N/A, EMERGENCY LIGHT ROW 19 LT SIDE INOP. REMOVED AND REPLACED BATTERY PACK AT SEAT ROW 19 LT SIDE. EMERGENCY LIGHT OPS CHECK GOOD.

Part: OXYGEN BOTTLE — EMPTY (COCKPIT)

INSPECTION TYPE:N/A, CREW O2 PRESSURE READS ZERO. *S/D* REMOVED AND REPLACED CREW O2 BOTTLE. NO LEAKS FOUND.

Part: FIRST AID KIT — MISSING (CABIN)

FWD FIRST AID KIT MISSING. REPLACED FIRST AID KIT.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD ENTRY EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD ENTRY EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEAT 19-A EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: RELAY — INOP (LT MLG WW)

IN DESCENT, WHEEL WELL FIRE WARNING ILLUMINATED. ACCOMPLISHED CHECKLIST ITEMS LIGHT EXTINGUISHED. INSPECTED W/W'S FOR EVIDENCE OF FIRE OVERHEAT AND PNEUMATIC LEAKS NO DEFECTS NOTED. INSPECTED FIRE LOOPS. NO EVIDENCE OF DAMAGE. REMOVED FIRE AND OVERHEAT ACCESSORY UNIT ASSY. FOUND ONE RELAY WITH BLACK PINS. REPLACED ACCESSORY UNIT W/W, FIRE TEST GOOD IAW MM 26-12-21. PART ON/OFF 65-24920-3 S/N ON 670604 S/N OFF 66807. SYSTEM CHECKS GOOD IAW.

Part: FIRE LOOP — SHORTED (NLG WW)

WHEEL WELL FIRE INDICATION 20 MILES FROM SDF. GEAR EXTENDED AND LIGHT WENT OUT IMMEDIATELY. NORMAL LANDING, TIRES OK. INSPECTED L AND R W/W FIRE LOOP, NO DEFECTS NOTED, TESTED W/W FIRE DETECTION SYSTEM PER MM 26-12-00 PAGE 501 SYSTEM CHECKS NORMAL. INSPECTED NOSE W/W FIRE LOOP AND REMOVED RUBBER CONTAMINANT FROM FWD LOOP CHECKS NORMAL.

Part: SWITCH — LEAKING (NR1 FUEL TANK)

INSPECTION TYPE:SI, NR 1 FUEL QUANTITY ROLLED BACK AT TAKEOFF FROM 10500 TO 5000 LBS. AIRCRAFT CONTROL WAS DEGRADED. ALTERNATE FUEL FEED ESTABLISHED TO COMPENSATE FOR INBALANCE. FUEL UPLIFT IN GALLONS DID NOT SHOW ANY DISCREPANCIES. IN FLIGHT EMERGENCY DECLARED. NRC 944172 GENERATED. *S/D* TROUBLESHOT FUEL QTY INDICATING SYSTEM FOR NR 1 TANK. FOUND ALL 4 FUEL PRESS SWITCHES ON LEFT L/E LEAKING FUEL. DAMAGED WIRING AT NR 1 TANK BOSSING PLUS CONNECTOR D578P FUEL SOAKED AND WIRE W436-512-22 DAMAGED AT SM17. REPAIRED IAW 28-41-02, 28-43-01 AND MM 28-41-02. NR 1 TANK FUEL QTY INDICATION SYSTEM FUNCTIONAL TESTS GOOD.

Part: SKIN — CORRODED (BS 1166)

INSPECTION TYPE:SI, PULLED FASTENERS BS 1166 STR 22 LT ON EXTERIOR SKIN CORROSION (C53-100-01.07-04). REMOVED AND REPAIRED DAMAGED AREA PER SRM 51-30-02, SRM 53-10-3 SRM 53-30-1, SRM 51-20-1, SRM 53-30-3, MM 51-20-21, SRM 51-30-5.

Part: STRAP — CORRODED (CARGO DOOR)

INSPECTION TYPE:SI, CORROSION (C53-111-01-03) ON AFT CARGO DOOR BEAR STRAP STA 1110 BETWEEN STR 23R-24R FWD AND AFT OF FRAME. REPAIRED BEAR STRAP PER ER 99-5506, SRM 51-10-7, 51-30-2, SRM 53-10-2, SRM 51-30-5.

Part: FRAME — CORRODED (CARGO DOOR)

INSPECTION TYPE:SI, WHILE WORKING FUSELAGE 117 CUSTOMER NR 943348 DISCOVERED AFT CARGO DOOR AFT FRAME TO BE CORRODED AND FRAME STRAP TO BE CRACKED AT FASTENER HOLE. REMOVED AND REPLACED FRAME PER ER 99-5506, SRM 51-30-2, SRM 51-10-2.

Part: SHEAR WEB — CORRODED (BS 1175)

INSPECTION TYPE:SI, CORROSION ON SHEAR WEB BS 1175 RBL 58 WL 208. MECHANICALLY REMOVED CORROSION FROM SHEAR WEB, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA ON SHEAR WEB PER SRM 51-30-2. PERFORMED WEB REPAIR PER SRM 51-40-2.

Part: CHORD — CORRODED (BS 298)

INSPECTION TYPE:SI, CORROSION ON LT NOSE WHEEL WELL MID CHORD BS 298 LBL 15 WL 169. REMOVED CORROSION FROM CHORD PER SRM 51-10-6. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED MID CHORD PER SRM 51-30-2. INSTALLED NEW MID CHORD PER SRM 51-30-5 AND 51-30-6.

Part: WEB — CORRODED (BS 560)

INSPECTION TYPE: SI, CORROSION (C53-224-01.05-01) ON WEB BS 560 WL 208 LBL 48-58. CORROSION REMOVAL OUT OF LIMITS IAW SRM 53-10-1. REPAIRED WEB FROM STA 510-590 WL 208 LBL 48-58 IAW BFG ER NR 99-5507 (UPS FILE 727-53-2130).

Part: BEAM — CORRODED (BS 592-596)

INSPECTION TYPE:SI, CORROSION (C53-111-01-2B) ON TRANSVERSE BEAM LOWER CHORD STA 592 TO 596 LBL 2 WL 199. REMOVED AND REPLACED TRANSVERSE BEAM AT BS 592 TO 596 LBL 2 WL 199 PER SRM 51-30-2.

Part: BEAM — CORRODED (BS 1110-1150)

INSPECTION TYPE:SI, AFT CARGO BAY TRANSVERSE BEAM BL 0 WL 200, CORROSION BETWEEN STA 1110 TO 1150 MARKED SDN C53-111-01.00-03. REMOVED AND REPLACED TRANSVERSE BEAM PER SRM 51-30-2.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK INSIDE REAR SPAR MAIN BOLT HOLE AND AROUND FWD LUG. REPLACED FLAP TRACK.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK AROUND FWD LUG. REPLACED FLAP TRACK.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 3 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE WITH SERVICEABLE UNIT.

Part: STIFFENER — CORRODED (BS 870)

INSPECTION TYPE:SI, CORROSION AND POPPED FASTENER ON BS 870, BL 0 STIFFENER WING CENTER SECTION. REMOVED AND REPLACED STIFFENER PER SRM 51-30-02.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 4 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE WITH SERVICEABLE UNIT.

Part: SKIN — CORRODED (BS 1040)

INSPECTION TYPE:SI, CORROSION, BULGING SKIN AND SHEARED FASTENER HEAD ON SKIN AT BS 1040 RBL 70, WL 208. REMOVED AND REPLACED SKIN FROM BS 1016 TO 1080, STR 14R-20R.

Part: BOLT — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, NR 6 FLAP TRACK AFT MOUNT BOLTS CORRODED. CLEANED AND TREATED BOLT HOLES AND REPLACED BOLTS.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI CORROSION ON NR 7 FLAP CARRIAGE AT SPINDLE FWD END. REPLACE FLAP CARRIAGE.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AT SPOILER BEAM MOUNT PAD. REMOVED AND REPLACED WITH NEW FLAP TRACK BEAM PER OHM 27-51-21 PG 502.

Part: INTERCOSTAL — CORRODED (BS 259-276)

INSPECTION TYPE:SI FLOOR SUPPORT UPPER CHORD CORRODED AT BS 259-276, LBL 8, WL 208. REPLACED INTERCOSTAL IAW SRM 51-30-2.

Part: RIB — CRACKED (WS 491)

INSPECTION TYPE:SI L/W FUEL TANK RIB UPPER CHORD AT WS 491, STR 15 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED RIB UPPER CHORD PER BAC DWG 65-16249.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:SI CORROSION IN SEVERAL PLACES ON FLOORBEAM BS 344, RBL 20 TO LBL 55, WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-8.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK AT REAR SPAR O/B MOUNT HOLE. REMOVED AND REPLACED FLAP TRACK IAW SRM 51-10-1, TO BE INSTALLED ON TC C57-581-04-3D.

Part: FRAME — CRACKED (BS 277)

INSPECTION TYPE:SI CRACK ON FRAME AT STA 277 ABOVE STR 16R. REPAIRED STA 277 FRAME AT STR 15R AND 16R IAW SRM 51-40-02.

Part: FITTING — CRACKED (RT ELEVATOR)

INSPECTION TYPE:SI RT ELEVATOR TAB CRANK O/B RIG PIN HOLE LUG IS CRACKED. REMOVED AND REPLACED FITTING IAW OVERHAUL MANUAL 55-20-01.

Part: STIFFENER — CRACKED (RT ELEVATOR)

INSPECTION TYPE:SI RT ELEVATOR T/E DOUBLER (STIFFENER) AT TAB ROD CUTOUT IS CRACKED. REMOVED AND REPLACED DOUBLER (STIFFENER) IAW SRM 51-30-2.

Part: STRINGER — CRACKED (LT WING)

INSPECTION TYPE:SI CRACKED TAB ON LEFT WING STRINGER 14. REPAIRED PER SRM 57-10-4 FIGURE 8, SHEET 2.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION ON NR 4 FLAP TRACK AT SPOILER BEAM ATTACH POINT. REPLACED TRACK PER MM 27-51-31.

Part: CHORD — CORRODED (BS 287)

INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) ON TOP CHORD OF F/E'S SEAT G-BEAM STA 287, LBL 9, RBL 11, WL 208 MARKED. REMOVED AND REPLACED CHORD ASSY AT STA 287, LBL 9, RBL 11, WL 208 PER SRM 51-30-2 AND 51-10-1.

Part: BEAM — CORRODED (LT SPOILER)

INSPECTION TYPE:SI CORROSION (C57-581-07.00-03) L/W SPOILER BEAM PAD, LOWER SURFACE WHERE NR 4 FLAP TRACK ATTACHES. REMOVED AND INSTALLED NEW SPOILER BEAM, FLAP TRACK ATTACHMENT PAD WORK DONE IAW SRM 51-30-5, 51-10-2, 51-30-2.

Part: FLOORBEAM — CORRODED (BS 380)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON BS 380 FLOORBEAM LBL 55 TO LBL 46 WL 208. CUT OUT DAMAGED FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8.

Part: FITTING — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 2 FLAP TRACK FWD ATTACH WING FITTING. REWORK OUT OF LIMITS PER BOEING DWG 65-32733. REPLACED WITH NEW ITEM.

Part: FITTING — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH WING FITTING. CORROSION OUT OF LIMITS PER BOEING DWG 65-32733, PART REPLACED WITH NEW ITEM PER SRM 51-30-02 AND DWG 65-17357.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 5 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE, INSTALLATION ON TC C57-581-04-4D.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 6 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE, INSTALLATION ON TC C57-581-04-4D.

Part: SKIN — CORRODED (BS 670)

INSPECTION TYPE:SI, RULLED FASTENER HEAD IN CROWN SKIN AT BS 670 RBL 28 WL 203. REMOVED FASTENER HEAD AND FOUND INTERNAL LAP CORROSION. CUT OUT CORROSION AND REPAIRED LAP PER EO B727-5330-0509Q PP 83.

Part: STIFFENER — CORRODED (BS 229)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON LONGITUDINAL STIFFENER TOP OF NOSE WHEEL WELL STN 229 LBL 20 WL 186. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-30-2 AND 53-10-1 PART REPLACED WITH USED ITEM PER SRM 51-30-5, SRM 51-30-2 PG 2/8 SRM 51-20-151 AND OHM 20-50-03.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C, FOUND .30 CRACK RADIATING FROM RIVET ON RIGHT WING TIP UPPER SKIN 18 INCHES AFT OF FORWARD EDGE, 6 INCHES O/B OF I/B EDGE. STOP DRILLED CRACK AND TRANSFERRED TO NON-ROUTINE CARD 943723.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, ON EMERGENCY EXIT LIGHT CK FOUND FWD RT OVERWING EXIT LIGHT OUT INSIDE CABIN, BOTH STAIRWELL LIGHTS OUT, BOTH LIGHTS OUT OVERWING UNDER OVERWING EXITS ON LEFT AND RIGHT SIDE OF AIRCRAFT AND LEFT REAR OUTSIDE LIGHT VERY DIM. FWD RIGHT OVERWING EXIT LIGHT REMOVED AND REPLACED, OPS CHECK GOOD. BOTH BATT PACKS REMOVED AND REPLACED, OPS CHECK GOOD. ALL BATTERIES REMOVED AND REPLACED, OPS CK GOOD. REMOVED AND REPLACED LEFT REAR OUTSIDE BATT, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 11 & 12)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP AT LT FWD EMERGENCY EXIT DOOR OVERWING LOWER ROW 11/12. REMOVED AND REPLACED 2 BATTERY PACKS FOR EMERGENCY EXIT DOORS, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

INSPECTION TYPE:N/A, LT AFT OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED LT AFT OVERWING BATTERY PACK, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, EMERG LIGHT BY COCKPIT DOOR INOP. REPLACED BATTERY PACK, OPS CK GOOD (P/N 96-2-1015).

Part: BATTERY PACK — DISCHARGED (ROW 11)

INSPECTION TYPE-N/A, EEL EXIT LIGHT LT CEILNG ROW 11. REPLACED BATT PACK, OPS CHK GOOD. (P/N 96-2-1024).

Part: BATT PACK — DISCHARGED (ROW 10)

INSPECTION TYPE-N/A, EMERG EXIT ROW LIGHTS INOP ROW 10 BOTH SIDES OVERWING. REMOVED AND REPLACED BATTERY PACKS, OPS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, MAIN ENTRY BY COCKPIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, RT FWD OVERWING DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED PACK, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT AREA LIGHT BY AFT LEFT LAV FAILED TEST. REPLACED BATTERY. CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, AFT CABIN EMER LIGHT EXIT MARKER INOP. REMOVED AND REPLACED THE AFT CABIN EXIT MARKER BATTERY PACK IAW BMM 33-50-81, OPS CK GOOD.

Part: LIGHT — INOP (RT WING)

INSPECTION TYPE-N/A, RT WING CENTER OVERWING ILLUMINATION EMERGENCY LIGHT IS NOT WORKING. REMOVED AND REPLACED THE CENTER RIGHT HAND OVERWING EXTERNAL RECEIVER AND PLATE ASSY IAW BMM 33-50-101, OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

INSPECTION TYPE-N/A, AISLE EEL INOP AT ROWS 13, 14, 15, 18 AND 6 ABC. ALSO, AFT ENTRY DOOR. REMOVED AND REPLACED BATT PACKS AS ABOVE, OPS CHECK GOOD.

Part: LIGHT — INOP (SEAT 11 L)

INSPECTION TYPE-N/A, EEL AT SEAT 11L IS INOP. INSTALLED EMERGENCY EXIT LIGHT, OPS CK OK (P/N 87-1001-71) (S/N 1018) ON, (S/N 1041) OFF.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS AT ROW 9 DOES NOT SHUT OFF WITH COCKPIT SWITCH. REPLACED EMERGENCY LIGHT, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, POSITION 9L, EMER EXIT LT INOP. REMOVED AND REPLACED BATTERY PACK, OPS OK (P/N 96-2-1015) TAG 185770 ON/OFF.

Part: LIGHT — INOPERATIVE (CABIN)

EMER EXIT LIGHT ON AFT OVERWING DOOR, RIGHT SIDE WILL NOT TEST. REPLACED EMER EXIT LIGHT ASSY CHECKS OK, PN ON 96-3-1032-2 SN ON 1033 PN OFF 96-3-1032-2 SN OFF 1012.

Part: BATTERY — DISCHARGED (CABIN)

ALL EMER EXIT LIGHTS INOP. REPLACED EMERG EXIT LIGHT BATTERY PACKS. ALL LIGHTS CHECK OK FOR SERVICE.

Part: OXY MASK — DEPLOYED (CABIN)

INSPECTION TYPE-N/A, ROW 19 O2 MASK DEPLOYED. REPLACED O2 MASK AS REQUIRED PER B727 PAX SUP 35-20-00.

Part: ANGLE — CORRODED (BS 915)

INSPECTION TYPE-C, CORROSION ON ANGLE AT BS 915, LBL 68, WL 190. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.

Part: BATTERY — DISCHARGED (CABIN)

LEFT FORWARD OVERWING EXIT MARKER, EMERGENCY LIGHTING BATTERY NEEDS REPLACEMENT PER TASK CARD 2403. PART ON REQ NR 482564. REMOVED AND REPLACED ROW LEFT EXIT MARKER BATTERY PACK. P/N ON AND OFF 96-21033. OPS NORMAL S/N ON TAG 00310263.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT RECEIVER BATTERIES NEED REPLACEMENT. ACCOMPLISHED TASK CARD 2403, EMERGENCY LIGHT RECEIVER BATTERIES REMOVED AND REPLACED BATTERIES, OPS CHECK NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHT RECEIVER BATTERIES NEED REPLACEMENT. ACCOMPLISHED TASK CARD 2403, EMERGENCY LIGHT RECEIVER BATTERIES REMOVED AND REPLACED BATTERIES. OPS CHECK NORMAL.

Part: OXY MASK — DEPLOYED (CABIN)

INSPECTION TYPE-N/A, PAX O2 INADVERTENTLY DEPLOYED. STOWED PAX O2 MASKS.

Part: OXY GENERATOR — ACTIVATED (CABIN)

INSPECTION TYPE-N/A, OXYGEN GEN ACTIVATED DURING DROP TEST AT SEAT 4-C. REPLACED O2 GEN PER MM 35-00-00.

Part: BATTERY — DISCHARGED (CABIN)

ROW 9 EMERGENCY FLOOR LIGHT DID NOT TEST. REMOVED AND REPLACED EMERG FLOOR LIGHT BATTERY, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD RT EMERG EXIT ID LIGHT DID NOT TEST. INSTALLED NEW BATTERY PACK IN FWD RT EMER EXIT IDENTIFIER LIGHT. TEST OK IAW UP TC 3000.

Part: BATTERY — LOOSE (CABIN)

FWD EMERGENCY EXIT MARKED DID NOT NOT TEST, RESEATED BATTERY. OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

MAIN ENTRY DOOR EMERG EXIT MARKER LIGHT DOES NOT TEST. INSTALLED NEW BATTERY BACK IN MAIN ENTRY DOOR EMERG EXIT MARKER LIGHT. TEST OK IAW TC 3000.

Part: BATTERY PACK — DISCHARGED (CABIN)

RT AFT OVERWING EMERG EXIT MARKER DID NOT TEST. INSTALLED NEW BATTERY PACK IN RT AFT OVERWING EMERG EXIT MARKER LIGHT. TEST OK IAW UPS TC 3000.

Part: BATTERY — DISCHARGED (CABIN)

AFT STAIRS EMERGENCY EXIT MARKER DID NOT TEST. REMOVED AND REPLACED EMERG EXIT MARKER BATTERY, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

GALLEY EMERGENCY EXIT ID DID NOT TEST. REMOVED AND REPLACED GALLEY EXIT ID LIGHT BATTERY, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EMERG EXIT MARKER COVER WING AFT DID NOT TEST. REMOVED AND REPLACED NEW BATTERY PACK IN LEFT AFT OVERWING EMERG EXIT MARKER LIGHT OPS CK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

LEFT GALLEY EMERGENCY CREW LIGHT DID NOT TEST. REMOVED AND REPLACED LEFT GALLEY AREA LIGHT BATTERY, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT FWD OVERWING EXIT MARKER DID NOT TEST. REPLACED BATTERY PACK 96-2-1033. NSN PERFORMED FUNCTIONAL CHECK. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

ROW 19 EMERGENCY FLOOR LIGHT DID NOT TEST. REMOVED AND REPLACED EMER 19 FLOOR LIGHT BATTERY, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD LFT EMERG EXIT ID LIGHT DID NOT TEST. INSTALLED NEW BATTERY PACK IN FWD LT EMER EXIT IDENTIFIER LIGHT, TEST OK IAW UPS TC 3000.

Part: POWER SUPPLY — FAILED (COCKPIT)

INSPECTION TYPE-N/A, AN ARCID SMELL WAS READILY IDENTIFIED IN COCKPIT DURING DESCENT, COULD NOT BE IDENTIFIED. REPLACED LT AND RT WATER SEPARATOR BAGS, NO HELP. DURING ENGINE RUN SMELL CONTINUED. FOUND SMOKEY SMELL EMANATING FROM AURAL WARNING BOX POWER SUPPLY. REMOVED AND REPLACED SAME, OP CK OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EXIT MARKER LIGHT BY FWD ENTRY DOOR, LOWER CORNER WILL NOT TEST. CLEANED CONTACTS, RETESTED EXIT MARKER LIGHTS AND LIGHT OPS CK'D GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EXIT IDENTIFIER NEXT TO VENTRAL STAIR DOOR 18 ABOVE FLOOR HAS NO STEADY GREEN LIGHT DURING TEST MODE. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY FLOOR LIGHT ROW NR 4 ABC WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ROW 6 ABC EMERGENCY FLOOR LIGHT HAS NO STEADY GREEN DURING TEST MODE. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, AREA LIGHT FORWARD WALL ABOVE FLASHLIGHTS DOES NOT HAVE STEADY GREEN LIGHT IN TEST MODE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ROW 15 ABC FLOOR LIGHT HAS NO STEADY GREEN DURING TEST MODE. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE-N/A, EXIT MARKER ON FACE OF DROP CEILING AT AFT OF A/C HAS NO STEADY GREEN LIGHT DURING TEST. PERFORMED FUNCTIONAL TEST OF SYSTEM, LIGHT OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ROW ABC FLOOR LIGHT HAS NO STEADY GREEN LIGHT DURING TEST MODE. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT LT SIDE UPPER AT AFT AIRSTAIRS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACKS, OPS CHECKS NORMAL.

Part: OXY GENERATOR — ACTIVATED (CABIN)

INSPECTION TYPE-N/A, 02 GENERATOR ACTIVATED DURING 02 DROP CHECK AT SEAT 6 DEF. REPLACED 02 GENERATOR.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT AT FWD ENTRY WON'T TEST. FLOOR AND CEILING REPLACED BOTH BATTERY PACKS, TEST OK.

Part: SIGN — MISSING (CABIN)

INSPECTION TYPE-N/A, EXIT IDENTIFIER AFT OF LT FWD EMER EXIT DOOR MISSING. INSTALLED SERVICEABLE LT FWD EMER EXIT DOOR INDENTIFER, OPS CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EXIT MARKER ABOVE FWD ENTRY DOOR DOES NOT TEST, BATTERY VOLTAGE LOW. INSTALLED SERVICEABLE BATTERY PACK, TEST OK.

Part: CONNECTOR — DIRTY (CABIN)

INSPECTION TYPE-N/A, EXIT IDENTIFIER FWD OF FWD ENTRY DOOR JUST ABOVE FLOOR LEVEL DOES NOT TEST. BATTERY VOLTAGE GOOD. CLEANED BATTERY/LIGHT ASSY CONNECTOR, TEST OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, RIGHT OVERWING EXIT LOCATION LIGHT FAILED TEST. REMOVED AND REPLACED RIGHT OVERWING EXIT LOCATION LIGHT BATTERY PACK, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, FWD EMERGENCY EXIT LIGHT FAILED TO TEST. REMOVED AND REPLACED FWD EXIT EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT FWD OVERWING EMER EXIT LIGHT INOP. SYS OPERATES NORMALLY THIS CLEARS M1277128. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERG LIGHT ASSY 6 AT ROW 11 HAS 1 LIGHT INOP (AFT BULB). RESEATED BATTERY PACK AND LIGHT BULB LT PACK, OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT SYSTEM FAILED TEST, BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AS DIRECTED BY UPS ENGINEERING AND ESTEL SYS REFERENCE TASK CARD 1300. FOLLOWING PART NUMBERS CHANGED: 96-2-1015 (25 EA), 96-2-1033 (4 EA), 96-2-1019 (2 EA) BALLASTS.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-IN, EMERGENCY LIGHT SYSTEM FAILED TEST, BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AS DIRECTED BY UPS A/C ENGINEERING. REMOVED AND REPLACED BATTERY PACKS AS DIRECTED BY UPS A/C ENGINEERING AND ESTEL SYSTEMS. REF TC 1300 25 EA 96-2-1015, 4 EA 96-2-1033, 2 EA 96-2- 1019 BALLASTS.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 6 EMER LIGHT BROKEN. REMOVED AND REPLACED THE ROW 6 EMERGENCY FLOOR PROXIMITY LIGHT PER M/M 33-50-71. SYSTEM OPS CHECKS NORMAL PER M/M 33-50-71.

Part: INDICATION — MALFUNCTIONED (NLG)

DID NOT HAVE GREEN NOSE GEAR INDICATIONS (NO RED LIGHTS). RECYCLED GEAR UP/DOWN SEQUENCE AND ALL LIGHTS NORMAL. JACKED ACFT AND CYCLED NLG 5 TIMES, COULD NOT DUPLICATE PROBLEM ON GROUND. AIRCRAFT OK TO CONTINUE SERVICE. ALL WORK DONE IAW B727 MM CHAPTERS 7 AND 32.

Part: FLOOR BEAM — CORRODED (FS 480)

INSPECTION TYPE-C, FLOOR BEAM CORRODED AT STA 480 FROM BL 0 TO RBL 48. CUT OUT DAMAGED AREA AT STA 480, FROM LBL 12 TO RBL 65 PER SRM 53-10-8, FAB'D AND INSTALLED UPPER CAP REPAIR PER SRM 53-10-8 FIG 5 AND SRM 51-30-2.

Part: SKIN — CRACKED (RT AFT EMER EXT)

INSPECTION TYPE-C, RT AFT EMERGENCY EXIT HAS TWO OPEN HOLES AND ONE HOLE IS CRACKED OUT TO THE EDGE OF SKIN. CUT OUT DAMAGE ON RT AFT EXIT DOOR PER SRM 52-40-2 FIG 1, FAB'D DOUBLER AND INSTALLED IAW SRM 52-40-11, 52-40-2 FIG 1 AND SRM 51-30-2.

Part: SPAR WEB — CRACKED (LT OUTBD AILERON)

INSPECTION TYPE-C, LT O/B AILERON SPAR WEB IS CRACKED AT O/B TAB ROD AREA THROUGH HOLE. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-2 FIG 1.

Part: FITTING — CORRODED (BS 870)

INSPECTION TYPE-C, RT FUSELAGE TERMINAL FITTING BS 870 HAS A 1 INCH CRACK EXTENDING BETWEEN TWO FASTENERS FWD, OUTER FLANGE, SIX INCHES ABOVE STR 13R. REMOVED AND REPLACED RT 870 TERMINAL FITTING PER BOEING DWG 65C-23231 AND UPS EO 727-5310-3056.

Part: STRINGER TIE — CRACKED (BS 990)

INSPECTION TYPE: C. STA 990 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 9700 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: SPAR — CRACKED (LT OUTBD AILERON)

INSPECTION TYPE-C, LT O/B AILERON SPAR UPPER CHORD IS CRACKED O/B OF NR 2 HINGE. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-10-1, 51-30-2 AND BOEING DWG 65-21723.

Part: STRINGER TIE — CRACKED (BS 990)

INSPECTION TYPE: C. STA 990 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 3R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1070)

INSPECTION TYPE: C. STA 1070 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1070)

INSPECTION TYPE: C. STA 1070 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1050)

INSPECTION TYPE: C. STA 1050 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1090)

INSPECTION TYPE: C. STA 1090 AT STR 5R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1050)

INSPECTION TYPE: C. STA 1050 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1090)

INSPECTION TYPE: C. STA 1090 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1050)

INSPECTION TYPE: C. STA 1050 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-1, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 990)

INSPECTION TYPE: C. STA 990 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1070)

INSPECTION TYPE: C. STA 1070 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 970)

INSPECTION TYPE: C. STA 970 AT STR 2R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 5L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 990)

INSPECTION TYPE: C. STA 990 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1050)

INSPECTION TYPE: C. STA 1050 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 990)

INSPECTION TYPE: C. STA 990 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE. FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (BS 1030)

INSPECTION TYPE: C. STA 1030 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: STRINGER TIE — CRACKED (FS 1010)

INSPECTION TYPE: C. STA 1010 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.

Part: FRAME — CORRODED (BS 760)

INSPECTION TYPE-C, RIGHT SIDE FRAME 760, FWD EDGE OF RT FWD EMERGENCY EXIT HAS TWO SMALL AREAS OF INTERGRANULAR CORROSION ON INNER FLANGE STRAP AT STRINGERS 16R AND 17R. REMOVED FASTENERS AND CORROSION PER SRM 51-30-2 AND 51-10-6, BLENDED AREA AND FINISHED PER DHC SK 946-750 AND SRM 51-10-2, INSTALLED FASTENERS PER SRM 57-30-2.

Part: EEL — MALFUNCTION (FLIGHT DECK)

PILOT REPORTED DURING TAKEOFF ROLL, ENCOUNTERED SEVERAL HARD BUMPS, EMERGENCY LIGHTS ILLUMINATED AND REMAINED ILLUMINATED IN ARMED POSITION. CHECKED OPERATION OF EMERGENCY LIGHTS AND FOUND OPERATION NORMAL AT PRESENT.

Part: EEL BATTERY — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT FAILS TEST. REPLACED BATTERIES, OPS CHECK OK.

Part: BLKHD FLANGE — CORRODED (BS 870)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON BOTTOM OF FWD FLANGE OF BEAM AT STA 870, LBL6-15, WL 207. REPAIRED FWD FLANGE OF 870 BULKHEAD UPPER CHORD PER UPS EO B727-5310-7012A.

Part: DOOR SILL — CORRODED (BS 520-550)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL (SHEAR WEB), LBL 47, STA 520-550 WL 208. INSTALLED REPAIR PER SRM 51-40-2.

Part: BALANCE PANEL — CORRODED (LT HORIZ STAB)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON LEFT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 55-10-1, 51-30-2, MM 51-20-21, 51-20-00, 27-30-21.

Part: BULLNOSE — CORRODED (NR 2 LE FLAP)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON NR 2 K FLAP BULLNOSE. REPLACED BULLNOSE PER SOHM 57-51-11 AND MM27-81-11.

Part: SKIN — DELAMINATED (RT ELEV TAB)

WHILE IN C CHECK, MAINTENANCE FOUND DELAMINATION ON RT ELEVATOR TAB, UPPER SURFACE. REPLACED TAB PER MM 27-30-00.

Part: MOP SILL — CORRODED (GALLEY DOOR)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MID GALLY DOOR MOP SILL STA 640-680, RBL 56, WL 208. REPLACED SILL PER SRM 53-10-1, 51-20-1, 51-10-2, 51-30-2, 51-20-4, MM 51-20-151.

Part: FRAME — CORRODED (BS 360)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION IN E/E COMPARTMENT, BS 360, FRAME AT APPROX LBL 35, STRINGER 24-25L. INSTALLED REPAIR PER SRM 53-10-1, 51-40-3.

Part: BALANCE PANEL — CORRODED (RT HORIZ STAB)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 51-30-2, 51-20-1, 55-20-2, 51-10-2, MM 27-30-21.

Part: SKIN — CORRODED (BS 1080)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON SKIN APPROX 1 INCH ABOVE STRINGER 10R, BS 1080, AFT CIRCUMFERENTIAL JOINT. INSTALLED REPAIR PER UPS EO B727-5330-1177K.

Part: DOOR SILL — CORRODED (BS 630)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL (SHEAR WEB), LBL 49, STA 630, WL 208. INSTALLED REPAIR PER SRM 51-40-2.

Part: COVE PANEL — CRACKED (NR 4 LE FLAP)

WHILE IN C CHECK, MAINTENANCE FOUND CRACK IN CUTOUT, NR 4 SLAT COVE PANEL, JUST O/B OF ACTUATOR ROD END. INSTALLED REPAIR PER SRM 51-30-2, 51-40-2.

Part: RIB — CORRODED (RT AILERON)

WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON RT ELEVATOR NOSE RIB AT ELEVATOR STA 191.58. REPLACED RIB PER SRM 51-30-2.

Part: STRINGER — CORRODED (BS 560-590)

WHILE IN C CHECK, MAINTENANCE FOUND CORROSSION ON STR 2R, STA 560-590. INSTALLED REPAIR PER SRM 51-20-4, 53-10-4, 53-10-3, MM 51-20-151.