N545DA

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 58,759 hrs · 43,701 cycles

WHILE ACCOMPLISHING INSPECTION OF THE FS 1183 BULKHEAD AFT ENTRY DOOR FRAMES AT RBL 17.8 PER AD 99-18-05 AND BAC S/B 727-53-0210, 2 FASTENER HOLES WERE ELONGATED.

Part: INDICATOR — INOPERATIVE (NR 1 ENGINE) · airframe 57,988 hrs · 43,169 cycles

NR 1 ENG LOW OIL PRESSURE / BYPASS LIGHT ILLUMINATED IN FLIGHT INSPECTED MAIN OIL FILTER FOUND APPRECIABLE COKE DEPOS RAN ENGINE WITH NEW FILTER INSPECTED FOUND VERY LITTLE COKE NOMETAL FOUND AT ANY TIME REPLACED SEC FILTER OIL PRESS INDIC NML.

Part: BOLT — MISSING (RT MLG WW) · airframe 56,193 hrs · 41,923 cycles

ON APPROACH TO SLC AT LANDING GEAR EXTENSION, FLIGHT CREW NOTICED RIGHT MAIN GEAR DID NOT EXTEND. RED GEAR DOOR LIGHT WAS ON AND SECOND OFFICERS AMBER R GEAR DOOR LIGHT ON. LANDING GEAR FINALLY EXTENDED AFTER ROLLING INTO RIGHT BANK. ALL INDICATIONS NORMAL. LANDING UNEVENTFUL. REPLACED MISSING BOLT IN GEAR DOOR SAFETY LINK, ALSO REPLACED SAFETY LINK, GEAR SEQUENCE VALVE AND GEAR DOOR ACTUATOR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,178 hrs · 41,912 cycles

CORROSION WAS FOUND ON THE BS 1166 FRAME AT THE SKIN CLIP BETWEEN STR 29R AND 30. THE DAMAGE WAS CUT OUT AND A REPAIR DOUBLER INSTALLED PER ERA 334767-14 AT MV.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,178 hrs · 41,912 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 930 AND STR 18A. THE DAMAGE WAS CUT OUT AND A DOUBLER INSTALLED AT HMV.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,178 hrs · 41,912 cycles

CORROSION WAS FOUND ON THE AFT DOOR OPENING FRAME OF THE C2 CARGO DOOR AT FS 1142.7. THE CORROSION WAS FOUND ON THE FORWARD SIDE OF THE WEB. THE DAMAGE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED AT MV.

Part: LIGHT — DAMAGED (SEAT 1) · airframe 56,172 hrs · 41,908 cycles

EMERGENCY TRACK LIGHT DAMAGED AT SEAT 1B. REPLACED BULB AND LENS.

Part: FRAME — CUT (FUSELAGE) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT THE STA 990 FRAME CHORD AT STR 29R WAS CUT TO FACILITATE REPAIR OF STR 29R. REMOVED STA 990 FACTORY FRAME SPLICE PLATE O/B OF STR 29R. CUT FRAME AT FS 990 JUST I/B OF S29R AS PER MM 53-12-0 FIG 804. DRILLED UP SPLICE ANGLE PER MM 53-12-0 FIG 804. REINSTALLED 990 FRAME SPLICE REPAIR DOUBLER PER MM 53-12-0 FIG 804.

Part: FITTING — LOOSE (NR 13 SPOILER) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT THE NR 13 SPOILER ATTACH FITTING SHIMS WERE FOUND TO BE LOOSE. THIS WAS REPAIRED PER MM 57-42-0.

Part: FITTING — LOOSE (NR 3 SPOILER) · airframe 56,114 hrs · 41,868 cycles

AT MV-2/E1 CK, FOUND LW NR 3 SPOILER MOUNT FITTING LOOSE AT LOWER O/B BOLT ON SPAR. REPAIRED PER M/M 57-42-0.

Part: FITTING — LOOSE (NR 14 SPOILER) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT THE NR 14 FLT SPOILER ACT MOUNT FITTING WAS FOUND TO BE LOOSE. THIS WAS REPAIRED PER MM 57-42-0.

Part: STRUCTURE — WORN (RT WING TE FLAP) · airframe 56,114 hrs · 41,868 cycles

AT MV-2/E1 CK, FOUND RW NR 4 MID FLAP L/E WORN AND GROOVED I/B END. TRIMMED OUT DAMAGE AND FAB REPAIR PARTS PER M/M 57-52-0 FIG 803, INSTALLED PER M/M 57-52-0 FIG 803.

Part: STRINGER — CRACKED (VERT STAB) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT STRINGER 9L AT RIB NR 2 WAS FOUND TO BE CRACKED. STOP DRILLED CRACK PER MM 55-30-0 PG 803. BEGAN FAB DOUBLER PER MM 55-30-0, CHEM TREATED PER PS 900-2-4-1 NR 2 INSTALLED DOUBLER PER MM 55-30-0 FIG 803.

Part: FITTING — LOOSE (NR 11 SPOILER) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT THE NR 11 SPOILER ATTACH FITTING WAS FOUND TO BE LOOSE. THIS WAS REPAIRED PER MM 57-42-0.

Part: FITTING — LOOSE (NR 4 SPOILER) · airframe 56,114 hrs · 41,868 cycles

AT MV-2/E1 CK, FOUND LW NR 4 SPOILER MOUNT FITTING LOOSE AT LOWER BOLT ON SPAR. REPAIRED PER M/M 57-42-0.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,114 hrs · 41,868 cycles

AT MIDVISIT STRINGER 29R STA 1000 WAS FOUND TO BE CORRODED. CUT AND REMOVED OLD CHORD PER MM 53-10-11D FIG 802D. DYE PENETRANT INSP, NO DAMAGE FOUND. FABRICATED REPAIR CHANNELS PER MM 53-10-11D FIG 802D AND INSTALLED REPAIR CHANNELS AFTER HEAT TREATING CAD PLATING AND TREATING SAME.

Part: SWITCH — INTERMITTENT (NLG WW) · airframe 55,214 hrs · 41,222 cycles

NOSE GEAR DOWN AND LOCKED GREEN INDICATION DID NOT ILLUMINATE PRIOR TO LANDING. COMPLIED WITH POM. PINNED GEAR TO TAXI TO GATE. REPLACED NOSE GEAR POSITION SWITCH AND NOSE GEAR LOCK SWITCH, PERFORMED NOSE GEAR SWING. ALL INDICATIONS CKS NML.

Part: SKIN — CRACKED (BS 481-681)

LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INIDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN THE PANEL. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367826-14AD, REV A.

Part: SKIN — CRACKED (NR 2 LE FLAP)

NR 2 MID FLAP COVE LWR COVE SKIN CRACKED ABOVE AFT FLAP I/B ROD. REPAIRED PER MM 57-20-0 FIG 809.

Part: POWER SUPPLY — INOPERATIVE (ROW 3)

ON PREFLIGHT, EMERGENCY EXIT SIGN INOP ROW 3. REPLACED RACK AND BATTERIES, OPN NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON PREFLIGHT, EMERG EXIT SIGN AT ROW 3 INOP. REPLACED RACK AND BATTERIES, OPN NORMAL.

Part: CONTROLLER — FAILED (L-1 WINDOW)

NOTIFIED OF SMELL IN THE CABIN, PERFORMED EMERGENCY DESCENT. AFTER LANDING, FOUND L-1 AC CONTROL CIRCUIT BREAKER POPPED IN WINDOW HEAT SECTION. ALSO, FOUND WINDOW HEAT NR 1L CIRCUIT BREAKER POPPED ON LOWER P-6 PANEL. AIRCRAFT DIVERTED TO YKM. MAINTENANCE FOUND L-1 WINDOW CONTROLLER FAILED. REPLACED L-1 CONTROLLER, FUNCTIONAL TEST SYSTEM. ALL CKS NML.

Part: FAN — FAILED (CABIN)

ON TOP OF DESCENT, CREW AND PASSENGERS COMPLAINED OF AN ELECTRICAL SMELL IN CABIN WITH NO SIGN OF SMOKE. AFTER A SAFE LANDING AND NORMAL DEPLANING, CONTRACT MAINTENANCE FOUND GASPER FAN CAUSING SMELL. REPLACED FAN.

Part: BRACKET — CRACKED (NR 6 LE FLAP ACT)

REF. SHIP 545 TPA LTR. CHECK C2 10/28/98, NO. 6 L/E FLAP ACTUATOR SUPPORT BOX FOUND CRACKED AT UPPER I/B ANGLE. REPAIRED PER MM 57-20-21 PG. 811

Part: FLOORBEAM — CORROSION (BS 344)

CORROSION ON FLOORBEAM STA 344 HAS CORROSION FROM ENTRY DOOR TO FWD LAV WALL. REPAIRED PER SRM 53-10-8.

Part: BATTERY — DISCHARGED (CABIN)

AFT EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOP. REPLACED LIGHT ASSY.

Part: TRANSVERSE BEAM — CRACKED (BS 1273)

A CRACK WAS FOUND IN THE UPPER FWD TRANSVERSE BEAM ANGLE AT STA 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE SERVICE BULLETIN.

Part: DOUBLER — CRACKED (RT ELEVATOR)

PREVIOUS DOUBLER CRACKED 1.5 INCH AT FASTENER. LOWER RT ELEVATOR I/B END. REPAIRED PER SRM 55-20-3 FIG 4.

Part: LIGHT — INOPERATIVE (CABIN)

FLASHLIGHT INOP. BASE CRACKED AND BATTERY DEAD, REPLACED FLASHLIGHT ASSY WITH FRESH BATTERY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS OVER R-1 DOOR ARE INOP. INSTALLED NEW BATTERIES, CKS GOOD.

Part: ANGLE — CRACKED (NR 3 SLAT)

FOUND .5 INCH CRACK BELOW NR 3 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER SRM 57-54-0.

Part: ANGLE — CRACKED (RT MLG WW)

FWD KEEL BEAM ANGLE CRACKED 1 INCH BELOW APU RT SIDE, FOUND DURING A-1 LTR CK TPAMM. TIME LIMITED REPAIR ACCOMPLISHED PER SRM 53-10-9 FIG 13. DAILY INSP REQUIRED AND PERM REPAIR TO BE ACCOMPLISHED WITHIN 100 FLT HOURS.

Part: ANGLE — CRACKED (NR 2 SLAT)

FOUND .5 INCH CRACK BELOW NR 2 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.

Part: BATTERY — DISCHARGED (CABIN)

AFT BULLNOSE EMERGENCY LIGHT DIM. C/A REPLACED BATTERIES, OPS CHECK GOOD.

Part: FUEL TANK — FUEL LEAK (RT WING)

IN FLIGHT RT WING WAS LEAKING FUEL 3 TO 6 FT INBD FROM WINGTIP. FOUND SEVERAL SCREWS MISSING FROM TANK ACCESS PANEL NR 5. REMOVED PANELS 3, 4 AND 5, CLEANED SEALS, INSTALLED NEW SCREWS, LEAK CHECK NORMAL.

Part: SPAR — OVERSIZED HOLES (RT ELEV)

OVERSIZED HOLES WERE FOUND IN THE REAR SPAR AND SKIN. THE SPAR WAS REPAIRED PER SRM 55-20-1 AND THE SKIN WAS REPAIRED PER SRM 55-20-3, FOR THE RIGHT ELEVATOR AT HMV.

Part: LE SKIN — WORN (NR 4 FOREFLAP)

DURING SHOP INSPECTION, NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E AT 86 FROM THE I/B END. REPAIRED PER SRM 57-50-4 FIG 1.

Part: STRINGER — CRACKED (WS 656.5)

AT HMV, RT WING STA 656.5, FOUND STR 9 CRACKED JUST OUTBOARD OF BOLT HOLE. REPAIRED PER MM 57-13-0 FIG 802.

Part: SKIN — CORRODED (FS 570-590)

DURING HMV INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN STA 570 AND STA 590 UNDER STRINGER 27L REQUIRING A 5 BY 9 CUTOUT. THE CUTOUT WAS REPAIRED IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3.

Part: CHORD — CRACKED (NR 2 TE MIDFLAP)

NR 2 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO AFT LOWER CHORD CRACKED AT THREE PLACES I/B AT I/B MOST AFT FLAP TRACK AND AFT FLAP I/B DRIVE. REPAIRED PER MM 57-52-0.

Part: LE SKIN — WORN (NR 1 FOREFLAP)

DURING SHOP INSPECTION, NR 1 FOREFLAP L/E SKIN WAS FOUND DAMAGED AT 7 TO 11 FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4.

Part: LE SKIN — DAMAGED (NR 1 FOREFLAP)

DURING SHOP INSPECTION, NR 1 FOREFLAP WAS FOUND WITH DAMAGE TO L/E SKIN AT 52 TO 55 FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4.

Part: ANGLE — DAMAGED (NR 2 SLAT)

TOOLMARKS ON INNER CLOSE OUT SKIN ATTACH ANGLE INSIDE AT 8TH RIB IN FROM OUTBD END OF NR 2 SLAT. REPAIRED PER MM 57-54-0 FIG 805A.

Part: FRAME — CRACKED (BS 804)

AT HMV, FRAME TO STRINGER ATTACH ANGLE FOUND CRACKED AT FS BS 804 STR 14L. REPAIRED PER SRM 53-10-4 PG 87 TO 89.

Part: SUPPORT BEAM — CORRODED (FS 830-850)

RT FAIRING SUPPORT BEAM HAS AREAS OF HEAVY CORROSION FROM STA 830 TO STA 850, FOUND AT HMV.

Part: BOLT — DAMAGED (NR 1 TE MIDFLAP)

NR 1 MIDFLAP, DURING HMV SHOP INSP FOUND THE FOURTH HOLE FOR THE THRUST BEARING RETAINER BOLTS IS DAMAGED. REPAIRED PER SRM 57-50-4.

Part: RIB — CRACKED (NR 4 TE MIDFLAP)

DURING SHOP INSPECTION, THE I/B AFT RIB WAS FOUND CRACKED AT BOTTOM AFT CORNER. REPAIRED PER MM 57-52-0, RT WING NR 4 MIDFLAP.

Part: SKIN — CRACKED (NR 3 MIDFLAP)

NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A CORNER CRACKED ON CUTOUT COVER SKIN 32 FROM I/B END. INSTALLED DOUBLER PER M/M 57-52-0.

Part: THRUST BEARING — CORRODED (NR 4 TE MIDFLAP)

DURING HMV FOUND CORROSION, I/B THRUST BEARING BORE NR 4 MIDFLAP. REPAIRED PER SRM 57-50-4.

Part: DOUBLER — CRACKED (NR 3 MIDFLAP)

NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A REPAIR DOUBLER CRACKED TWO PLACES AT I/B AFT FLAP TRACK. REPAIRED PER SRM 57-52-0.

Part: DOUBLER — CRACKED (NR 3 MIDFLAP)

NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A REPAIR DOUBLER CRACKED TWO PLACES AFT OF I/B BELL CRANK ON AFT ATTACH ANGLE. REPAIRED BY SPLICING IN NEW ANGLE WITH ATTACH DOUBLER PER SRM 57-52-0.

Part: FLOORBEAM — CORROSION (FS 400)

AT HMV, FOUND CABIN FLOOR SUPPORT BEAM AT FS 400 WITH CORROSION DAMAGE TO UPPER CAP AT RBL 12 TO LBL 24. REPAIRED PER SRM 53-10-8 FIG 3.

Part: FRAME — DOUBLE DRILLED (FS 720)

AT HMV, FOUND FS 720B FUSELAGE FRAME WITH DOUBLE DRILLED HOLE JUST INBOARD OF STRINGER 4R. REMOVED DAMAGED SECTION OF FRAME AND SPLICED IN REPAIR PER SRM 53-10-4 FIG 26.

Part: FRAME — CRACKED (FS 277)

AT HMV, FRAME CRACKED .5 CRACK IN FRAME STA 277 STGR 16L. ROUTED OUT DAMAGE IN FRAME STGR 16L STA 277. FABRICATED REPAIR PER SRM 51-40-2 FIG 1, INSTALLED REPAIR PER SRM 51-40-2 FIG 1.

Part: STRINGER — CRACKED (FS 720)

AT HMV, FOUND STRINGER 15R CRACKED AT ITS END JUST FWD OF WING ICE LIGHT HOUSING AT FS 720B. REPAIRED PER SRM 53-10-3 FIG 1.

Part: SKIN — DENTED (C-3 CARGO DOOR)

AT HMV, FOUND DENT IN C-3 DOOR OUTER SKIN 1.25 BY 1.5 BY .1562 INCH DEEP. INSTALLED REPAIR PER SRM 52-20-2 PG 1.

Part: FRAME — CRACKED (FS 804)

FRAME CRACKED, FS 804 FUSELAGE FRAME IS CRACKED AT STR 14R. REPAIRED AS PER SRM 53-10-4 FIG 22. FOUND AT HMV.

Part: FITTING — CORRODED (NR 1 TE MIDFLAP)

THE NR 1 MIDFLAP O/B CARRIAGE SUPPORT FITTING HAD 4 EACH, THRUST BEARING RETAINER BOLT HOLES CORRODED FOUND DURING SHOP INSP. THE HOLES WERE REPAIRED PER SRM 57504 FIG 14, BY REAMING HOLES TO REMOVE THE CORROSION AND INSTALLING A BUSHING. FOUND AT HMV SHOP VISIT.

Part: RIB — CRACKED (NR 2 SLAT)

RIB CRACKED, NR 2 SLAT, RIB MARKED NR 19 CRACKED AT LOWER AFT END BY CUT OUT. REPAIRED PER MM 57-54-0 FIG 805.

Part: RIB — CRACKED (NR 2 SLAT)

RIB CRACKED, NR 2 SLAT, RIB MARKED NR 10 CRACKED LOWER AFT CORNERBY N/P. REPAIRED PER MM 57-54-0 FIG 814.

Part: RIB — CRACKED (NR 6 SLAT)

RIB CRACKED, NR 6 SLAT RIB MARKED NR 11 CRACKED LOWER AFT CORNER BY N/P (1 RIB OUTBOARD OF ACTUATOR). REPAIR PER MM 57-54-0 FIG 814.

Part: ANGLE — CRACKED (NR 7 SLAT)

ANGLE CRACKED, ANGLE BELOW TAI DUCT CRACKED AT BOTTOM OF CUTOUT FOR TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A, FOR NR 7 L/E SLAT AT HMV.

Part: SKIN — CRACKED (RUDDER)

RUDDER SKIN CRACKED. ONE .125 CRACK, ONE .25 CRACK AND 3 SHEARED RIVETS ON LEFT SIDE OF LWR RUDDER, 6 BELOW A. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV.

Part: RIB — CRACKED (NR 6 SLAT)

RIB CRACKED, NR 6 SLAT-RIB MARKED NR 7 O/B OF TAI DUCT. REPAIR IS CRACKED AFT LOWER CORNER OF RIB. REPLACED REPAIR AS PER MM57-54-0 FIG 805. FOUND AT HMV.

Part: SPAR — CRACKED (NR 7 SLAT)

SPAR CRACKED, TOP I/B CORNER OF CUTOUT FOR TAI DUCT. NR 7 SLAT. REPAIRED PER MM 57-54-0 FIG 810. FOUND AT HMV.

Part: SPAR — CRACKED (NR 8 SLAT)

SPAR CRACKED, NR 8 SLAT-TOP I/B CORNER OF CUTOUT FOR TAI DUCT INSIDE OF SLAT, BN525. REPAIRED PER MM 57-54-0 FIG 802A.

Part: RIB — CRACKED (NR 2 SLAT)

RIB CRACKED, NR 2 SLAT, RIB MARKED NR 8 CRACKED LOWER AFT CORNER BY N/P. REPAIRED PER MM 57-54-0 FIG 814.

Part: RIBS — CRACKED (NR 2 SLAT)

RIB CRACKED NR 2 SLAT O/B ACTUATOR MARKED NR 11 LOWER AFT CORNER. RIB CRACKED NR 2 SLAT I/B ACTUATOR MARKED NR 12 LOWER AFT CORNER. REMOVED DOUBLER AND INSTALLED NEW DOUBLER PER MM 57-54-0 FIG 805. REMOVED DOUBLER FABRICATED NEW DOUBLER PER MM 57-54-0 PAGE 804. DAMAGE FOUND AND REPAIRED DURING HMV.

Part: RIB — CRACKED (NR 1 LE SLAT)

AT HMV, FOUND NR 1 SLAT PANEL WITH CRACKED RIB JUST O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0 FIG 804.

Part: RIBS — CRACKED (NR 5 LE SLAT)

AT HMV, FOUND NR 5 L/E SLAT WITH 2 CRACKED RIBS INBD AND OTBD OF SLAT ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0.

Part: RIB — CRACKED (NR 8 LE SLAT)

AT HMV, FOUND NR 8 SLAT WITH CRACKED RIBS INBD OF TAI DUCT AND IB RIG AT W/P. REPAIRED PER SRM 57-54-0.

Part: SKIN — CORROSION (AFT OF E/E COMP)

AT HMV, FOUND LOWER FUSELAGE SKIN WITH CORROSION DAMAGE JUST AFT OF E/E COMPARTMENT OPENING. REPAIRED DAMAGE PER SRM 53-30-3 FIG 2.

Part: FITTING — CORRODED (NR 1 TE MIDFLAP)

THE NR 1 MIDFLAP I/B CARRIAGE SUPPORT FITTING THRUST BEARING BORE WAS FOUND CORRODED. FOUND AT HMV SHOP VISIT. THE BORE WAS REPAIRED BY MACHINING BORE TO REMOVE CORROSION AND INSTALLING A BUSHING PER SRM 57504 FIG 15.

Part: FITTING — CORRODED (NR 1 TE MIDFLAP)

THE NR 1 MIDFLAP I/B CARRIAGE SUPPORT FITTING THRUST BEARING RETAINER BOLT HOLES, 3 EACH WERE FOUND CORRODED. THE HOLES WERE REPAIRED PER SRM 57504 FIG 14, BY REAMING HOLES TO REMOVE DAMAGE AND A BUSHING WAS INSTALLED. FOUND AT HMV SHOP VISIT.

Part: STRINGER — CRACKED (FS 34)

A HMV, STRINGER CRACKED, .25 INCH CRACK IN STGR 20R JUST FWD OF STA 344. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED REPAIRS PER SRM 53-10-3.

Part: SKIN — HOLE (C3 DOOR)

HOLE IN INNER SKIN, C3 DOOR ABOUT 6 FWD OF FWD LOWER DOOR STOP FITTING. REPAIRED PER MM 52-30-2 FIG 3.

Part: ANGLE — CRACKED (NR 2 TE MIDFLAP)

NR 2 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE AFT CHORD ATTACH ANGLE CRACKED. REPAIRED PER MM 57-52-0.

Part: SKIN — DENTED (FS 1243)

SMALL DENT 1 BY 1 BY .09375 AFT LT FUSELAGE 3 FEET SWD OF AFT LAV SVC PANEL STA 1243 ST 20L. REPAIRED SKIN PER SRM 53-30-3 PG 74.

Part: ANGLE — BROKEN (NR 7 SPOILER)

ANGLE IS BROKEN AT LOWER MOUNT OF NR 7 SPOILER FITTING. REMOVED REPAIR ANGLE AND MANUFACTURED NEW AS PER MM 57-20-22. FOUND AT HMV.

Part: STRINGER — CORRODED (FS 560)

STRINGER 27L BETWEEN STA 560 AND STA 580 FWD CARGO CORRODED. REMOVED DAMAGED SECTION OF STRINGER, SPLICED PER SRM 53-10-3 PG 3, FOUND AT HMV.

Part: FRAME — CRACKED (FS 930)

AT HMV, FUSELAGE FRAME CRACKED STA 930 RIGHT SIDE STR 14. REPAIRED FRAME PER SRM 53-10-4.

Part: STRINGER — CORROSION (FS 1144)

AT HMV, FOUND FUSELAGE STRINGER 26R WITH CORROSION DAMAGE AT FS 1144. REPAIRED PER SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (FS 740)

AT HMV, FOUND CORROSION DAMAGE TO STRINGER 27R AT FS 740. REPAIRED PER SRM 53-10-3 FIG 1.

Part: FITTING — CORRODED (RT TE MID FLAP)

NR 4 MID FLAP, I/B CARRIAGE SUPPORT FITTING, BOTTOM I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. ALSO, O/B CARRIAGE SUPPORT FITTING, BOTH BOTTOM THRUST BEARING RETAINER BOLT HOLES CORRODED. REPAIRED PER SRM 57-50-04 PG 34. REAMED OVERSIZE AND INSTALLED BUSHINGS.

Part: LE SKIN — WORN (RT TE FLAP)

NR 4 FORE FLAP, L/E WORN 86 FROM I/B END OF FLAP. REPAIRED PER SRM 575004 FIG 1, FOUND AT HMV, SHOP VISIT.