N934UP

Part: LIGHT — DEFECTIVE (CABIN)

INSPECTION TYPE:PFLT EXIT LIGHTS STAY ON IN ARMED POSITION. REPLACED LIGHT ASSEMBLY

Part: FRAME — CRACKED (FUSELAGE BS913.5)

INSPECTION TYPE:C CRACK INDICATION AT FRAME, FUSELAGE BS913.5 RIGHT SIDE. CRACK CONFIRMED BY NDT INSP. PART 6 51-00-00 STOP DRILL CRACK AT FRAME AT BS 913.5 B727-51-10-01 INSTALLED KIT REPAIR AS PER EO B727- 5310-1896-B APPENDIX C AT FRAM FUSELAGE BS 913.5 RH SIDE KIT #65627 194-26.

Part: WEB — CRACKED (NLGWW BS259)

INSPECTION TYPE:C NOSE LANDING GEAR BAY LH SIDE AT BS 259 SIDE WALL HAS A CRACK INICATION. REMOVED ACCESS PANEL #3124 AND LOWER WEB TO GAIN ACCESS TO DAMAGE AREA, CUT OUT DAMAGE AREA APPROX 5"X1" AT NOSE LANDING GEAR BS259 AS PER B727 SRM51-40-2 ACCOMPLISHED NDT INSPECTION AT CUT OUT AREA INSTALL DOUBLER REPARI APPROX 8"X6"

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C, LEFT WW FRAME 930 HAS PREVIOUS REPAIR WITH STOP HOLE, BUT IS CONTINUING UPWARDS AFTER STOP HOLE FRAME BELOW FLOOR BS 930. PERFORMED HFEC INSP ON I/B FLANGE AS PER NDT MANUAL PART 6-51-00-01 FIG 4. CRACK AT 1/4 BOLTS HOLE APPROX .5 INCH DOWN FROM PRESSURE WEB, INSTALL DOUBLER REPAIR AS PER EO B727-5310-2611.

Part: BULKHEAD — CRACKED (RH W/W STA 870)

INSPECTION TYPE:C RIGHT WHEEL WELL STA 870 BULKHEAD CRACK AT APU VALVE CUT OUT RBL4.5 STOP DRILL CRACK ON RH W/W STA 870 AT APU VALVE CUT OUT RBL45 STOP DRILL 1/4" SIVE AND NDT INSPECTION ACCOMPISHED HFEC AS PER PART6-51- 00-00 FIG4 INSTALL 3 DOUBLER REPAIRS PART# 15-5PH. INSTALLED REPAIR AT RH W/W AT STA 870 RBL45 AS PER SRMB727-53-10-9 FIG #5.

Part: WEB — CRACKED (NLGWW BS266)

INSPECTION TYPE:C NOSE LANDING GEAR BAY RH SIDE WALL AT BS 266 HAS A CRACK INDICATION. REMOVED ACCESS PANEL #3125 AS PER SRMB727-51-30-2 CUT OUT DAMAGE AREA AS PER B727-51-40-2 APPROX 3.5"X1" ACCOMLPISHED NDT INSPECTION AND INSTALLED DOUBLER REPAIR AS PER B727-SRM51-40-2 FIG 1 APPROX SIZE 3"X1".

Part: BULKHEAD — CRACKED (FUSELAGE)

INSPECTION TYPE:C, RT WHEEL WELL FWD LOWER FRAME SHOWS CRACK DAMAGE AT BS 870 RBL 4.5. REMOVED FASTENERS AT DAMAGED AREA SRM 51-30-2, CUTOUT WEB DAMAGED AREA APPROX 1 X 1.5 INCH SRM 51-40-2 AT BS 870 RBL 4.5 HFEC INSP CUT OUT IAW M/M 51-00-00 PART 6 FIG 4. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 INSTALLED EXTRUDED REPAIR AT RT W/W LOWER FRAME RBL 4.5 AS PER B727 SRM-51-40-4 FIG 1.

Part: LANDING GEAR — FAULTY (NOSE)

INSPECTION TYPE:N/A NOSE GEAR DID NOT EXTEND ON FIRST TRY. RECYCLED & NOSEGEAR EXTENDED. JACKED AIRCRAFT, HEATED NOSE WHEEL AREA TO REMOVE ICE. GREASED TRUNI ON, OVERCENTER KNUCKLE, GEAR DOORS. CYCLED GEAR SEVERAL TIMES.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 44,709 hrs · 50,354 cycles

AIR TURN BACK ON DELIVERY FLIGHT FROM C CHECK AT SNN . CREW EXPERIENCED TOTAL LOSS OF B SYSTEM HYD PRESS . PRESS LINE FROM NR 1 B PUMP TO B SYS PRESS MODULE FOUND FRACTURED AT SLEEVE PRESS LINE CANIBALIZED FROM A/C N912UP TO REPLACE FRACTURED PIPE LINE. HYD SYS REPLENISHED , B PUMPS OPERATED AND SYS REPLENISHED AS NECESSARY. A/C RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (NR1 ENGINE T/R) · airframe 44,708 hrs · 50,352 cycles

INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED AS PER MM 78-30-00

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 44,708 hrs · 50,352 cycles

INSPECTION TYPE: C, LT WING, FIXED TE SUPPORT BRACKET CRACKED, AREA BELOW 37 SPOILER I/B HINGE. REPLACED BRACKET IAW SRM 51-30-02

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FWD ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL PER MM 33-50-01. A/C OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:D WHILE REPLACEING BS 740 LT FITTING SEVERAL HOLES ON FUSELAGE SKIN COMMON TO FITTING FOUND DAMAGED. CARRIED OUT SKIN SPLICE REPAIR IAW EO 98-27-002 ENGINEERING FILE NR 5330-2071.

Part: RIB — CORRODED (VERT STAB)

INSPECTION TYPE:D TENSION TIE RIB FWD AND AFT VERTICAL HOLES ARE PITTED. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NO 727-55-0374.

Part: BALANCE PANEL — CORRODED (LT HORIZ STAB)

INSPECTION TYPE-D, CORROSION ON NR 5 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.

Part: BALANCE PANEL — CORRODED (LT HORIZ STAB)

INSPECTION TYPE-D, CORROSION ON NR 3 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.

Part: RIB — CORRODED (VERT STAB)

INSPECTION TYPE:D TENSION TIE RIB ATTACH FITTINGS FWD AND AFT VERTICAL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NR 727-55-0374.

Part: BALANCE PANEL — CORRODED (RT HORIZ STAB)

INSPECTION TYPE-D, RT STAB, LIGHT SURFACE CORROSION ON NR 5 BALANCE PANEL. BALANCE PANEL REPLACED IAW MM 27-30-21.

Part: BALANCE PANEL — CRACKED (RT HORIZ STAB)

INSPECTION TYPE-D, RT STAB NR 4 BALANCE PANEL CRACKED. BALANCE PANEL REPLACED IAW MM 27-30-21.

Part: PANEL — CORRODED (WS 180)

INSPECTION TYPE:D NR 1 FUEL TANK ACCESS PANEL CORRODED (FRONT SPAR) LT WING. REPLACED PANEL IAW 28-11-10.

Part: PANEL — CORRODED (WS 491)

INSPECTION TYPE:D LT WING BOLT ON FUEL TANK ACCESS PANELS ARE CORRODED PANELS NR 15 - NR 19. REPLACED PANELS IAW 28-12-11.

Part: BRACKET — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:D FRAME BS 488 OUTER CHORD ATTACH BRACKET CRACKED AT MAIN CARGO SUPPORT FITTING (FWD SIDE OF FRAME). CARRIED OUT REPAIR IAW SRM 53-10-4 FIG 11.

Part: BRACKET — CRACKED (LT TE FLAP)

INSPECTION TYPE:D LT OUTBD FLAP OUTBD SUPPORT RAMP STAY ROD REAR SPAR ATTACH BRACKET SUSPECT CRACKED. REPLACED SUPPORT BRACKET IAW SRM 51-30-2.

Part: CASTING — CORRODED (NR 6 SPOILER)

INSPECTION TYPE:D ON FURTHER INVESTIGATION OF NR 6 SPOILER LINKAGE SUPPORT CASTING MIGRATED REWORK SLEEVE REMOVED AND CORROSION FOUND IN REWORKED AREA. REPLACED SUPPORT CASTING IAW DRAWING NR 65-16216.

Part: RIB — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:D CRACK AT NR 6 SLAT I/B TRACK O/B RIB. REPAIRED RIB IAW SRM 51-40-2.

Part: WEB — CRACKED (LT AILERON)

INSPECTION TYPE:D LT OUTBD AILERON FIXED WEIGHT BAY, INBOARD WEB IS CRACKED. REPAIRED IAW SRM 51-30-02.

Part: BULB — FAILED (CABIN)

CABIN ENTRY DOOR EMERGENCY EXIT 1 LIGHT INOP. RELAMPED, GROUND CHECKS OK.

Part: HOSE — LEAKING (B-HYD SYST)

INSPECTION TYPE-N/A, LOSS OF HYDRAULIC SYSTEM 'B' FLUID AT 15,000 FT BOTH 1 AND 2 'B' PUMPS LOW PRESS LIGHTS CAME ON, QTY INDICATION 0. DECLARED EMERGENCY, COMPLIED WITH CHECKLISTS, LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 'B' PUMP PRESSURE LINE CHAFED THROUGH. REMOVED AND REPLACED NR 1 'B' PUMP PRESSURE LINE AND NR 2 PUMP SUPPLY LINE. CHECKED CASE DRAIN FILTERS, AND SUPPLY FILTERS FOR FOD. SERVICED SYSTEM, LEAKED AND OPS CHECKED GOOD.

Part: ACTUATOR — LEAKED (NR 5 LE SLAT)

INSPECTION TYPE-N/A, LOSS OF HYDS, GEAR EXTENDED MANUALLY. FOUND LEAK AT NR 5 LE SLAT ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW MM 27-81-3 2, SERVICED HYDS, RAN ENGINES, CYCLED ALL FLT CONTROLS, CKD FOR LEAKS, OK FOR SERVICE.

Part: MID SPAR — CHAFED (VERT FIN)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRED PER UPS EO 727-55-0309.

Part: WEDGE — CORRODED (RT TE MIDFLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2.

Part: ANGLE — CRACKED (NR 7 SLAT TRACK)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51-30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1.

Part: HINGE TAB — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0.

Part: SLAT — CRACKED (NR 5)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW MM 27-81-11.

Part: RIB — CRACKED (HORZ STAB)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT END. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2.

Part: BONDING JUMPER — CORROSION (NR 6 K-FLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00.

Part: ROD END — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILERON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00.

Part: HINGE FITTING — CORRODED (RT INBD AILERON)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND REPLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-20-1 AND 51-30-2.

Part: HINGE ARM — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE ARM IS CORRODED AROUND BOLT HOLE. REMOVED AND REPLACED HINGE ARM IAW MM 27-10-01 AND 27-10-0.

Part: FITTING — CORRODED (LT TE MIDFLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT FITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443.

Part: FITTING — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON TAB HINGE FITTINGS CORRODED, 3 EA. REMOVED AND REPLACED LT AILERON TAB FITTINGS IAW SRM 51-30-2 AND MM 27-10-0.

Part: INTERCOSTAL — CORRODED (BS 682)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 682, RBL 10 - LBL 10, WL 152. REPLACED STRUCTURE LBL 10 - RBL 10, STA 682, WL 152 I/A/W SRM 51-29-1.

Part: FITTING — CORRODED (LT TE MIDFLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT FITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443.

Part: MID SPAR — CORRODED (LT TE MIDFLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR AFT SIDE 54 AND 58 O/B OF THE I/B END OF MID SPAR. REPLACED ON NRC 368443.

Part: MID SPAR — CORRODED (LT TE MIDFLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR UPPER INTERIOR SURFACE AFT SIDE 49 AND 55 I/B OF THE O/B END OF MID SPAR. REPLACED ON NRC 368443.

Part: SWITCH — OUT OF ADJUST (RT MLG DOOR)

DURING CLIMBOUT, THE RT MAIN GEAR DOOR ANNUNCIATOR LIGHT ILLUMINATED, AFTER POSITIONING THE GEAR HANDLE TO THE OFF POSITION. MAINTENANCE CYCLED THE LANDING GEAR AND THE RT MAIN LIGHT ILLUMINATED AGAIN WITH THE GEAR. ADJUSTED AND TESTED DOOR SWITCH PER MM 32-62-11, OPS NORMAL.

Part: HYD FLUID — LEAKING (B HYD SYST)

BEGINNING OF DESCENT INTO SDF, AS THRUST LEVERS WERE BROUGHT TO IDLE THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYSTEM 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO 0. LOSS OF SYSTEM 'B' CHECKLIST WAS ACCOMP AND EMERGENCY DECLARED, UNEVENTFUL LANDING. STILL OPEN.

Part: HYD PUMP — MALFUNCTIONED (1/2 B HYD SYS)

(SUPPLEMENTAL MRR) PILOT REPORTED THAT AT BEGINNING OF DESCENT WHEN THRUST LEVERS WERE BROUGHT TO IDLE, THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYS 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO ZERO. LOSS OF SYSTEM 'B' CHECKLIST WAS ACCOMPLISHED AND EMERGENCY DECLARED. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED NR 2 SYSTEM 'B' ELECTRIC PUMP. REPLACED BR 1 SYSTEM 'B' PUMP, RAN BOTH PUMPS, OPS AND LEAK CK OK.