N948WP

Part: OVEN — FAILED (FWD GALLEY) · airframe 52,316 hrs · 33,027 cycles

ON TAKEOFF, SMOKE FROM FWD GALLEY OVEN. REPLACED SAME.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 51,956 hrs · 32,820 cycles

CAPTS VSI STARTED SPARKING WHEN AT THE GATE IN SLC BRIEF ELECTRICAL FIRE FOLLOWED BY SMOKE IN COCKPIT. C PERFORMED EXTERNAL LEAK CHECK OF AREA ABOVE CAPT'S INSTRMENT CLUSTER NO FLUID LEAKS DETECTED. FOUND AN EMPTY SCREW HOLE IN THE GLARE SHIELD ABOVE THE INSTREMENT CLUSTER THAT HAD A BROWN FLUID IN IT. INITIALLY THE FLUID ON THE EXTERIOR CASE OF THE IVSI WAS WET. IT HAS DRIED TO A STICKY TEXTURE. SUSPECT IT TO BE COLA PRODUCT. REPLACED IVSI TESTED OK.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 51,224 hrs · 32,417 cycles

AT 33000 FT WARNING HORN SOUNDED AND COCKPIT LOST PRESURIZATION. CABIN ALT CLIMBED TO 12500 AND AUTO FAIL LIGHT ILLUMINATED ON CABIN PRESSURIZATION CONTROLLER. RAN PRESSURIZATION CONTROLLER CHECK, PRESSURIZED ACFT CHECKED ENGINE PNEUMATICS ALL CHECKED GOOD. WHILE CHECKING PACK SYSTEM FOUND LT PACK CONTROL VALVE WILL NOT SHUT OFF. REPLACED VALVE SYSTEM CHECKS GOOD.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 49,449 hrs · 31,351 cycles

FLT ATTENDANT REPORTED SMOKE/ELECTRICAL SMELL COMING FROM F/C GALLEY OVEN AND CONTROL PANEL. FIRE EXTINGUISHER USED. NO FIRE NOTICED. GALLEY POWER SECURED. ELECTED TO DIVERT TO LBB. REMOVED AND REPLACED OVEN, OP CKS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 48,487 hrs · 30,781 cycles

L2 DOOR EMERGENCY EXIT IDENT NEAR FLOOR DAMAGED. REPLACED BASE, OP CKS GOOD.

Part: SKIN — PUNCTURED (FS 280, S-20R) · airframe 46,383 hrs · 29,446 cycles

FUSELAGE / SKIN / FS 277-295 / STRG. 19R-20R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN BETWEEN FS 277 & 295 AT STRINGERS 19R & 20R WAS STRUCK BY GROUND EQUIPMENT RESULTING IN A PUNCTURE AND SEVERAL DENTS AND GOUGES. THE DAMAGE AREA WAS REMOVED WITH A 19" X 10" CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381091-14, REV A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,324 hrs · 29,405 cycles

INSPECTION OF THE FS 178 BULKHEAD WEB REVEALED A CRACK IN A TOOLING HOLE AT WL 234 AND LBL 12. A SECOND CRACK WAS FOUND AT A FASTENER HOLE AT WL 233 AND LBL 12. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. THE AREA WAS THEN REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380947-14AD.

Part: OVEN — MALFUNCTIONED (FWD GALLEY) · airframe 45,645 hrs · 28,974 cycles

FWD OVEN HAD AN ELECTRICAL /BURNT SMELL. GALLEY PWR WAS REMOVED, CONDITION IMPROVED. REPLACED FWD GALLEY OVEN AND BOTH CONTROLLERS. OVEN DPN 255701023, S/N 98-12-0066, CONTROL DPN 255701024, S/N OFF 8601-0701 & 8612-1728.

Part: OVEN — ODOR (GALLEY) · airframe 44,468 hrs · 28,197 cycles

A/C DIVERTED TO CYS AFTER EXPERIENCING FUMES IN THE CABIN. REPLACED F/C OVEN.

Part: OUTFLOW VALVE — INOPERATIVE (AFT FUSELAGE) · airframe 43,596 hrs · 27,571 cycles

CABIN HORN SOUNDED AT 10,000 FT AND CABIN DID NOT PRESSURIZE WORKING OFF A SINGLE PACK OPERATION. REPLACED AFT OUTFLOW VALVE, PRESSURIZED A/C TO 7.0 WITH NO PROBLEMS.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY, CONTROL POSSIBLE IN MANUAL A/C. REPLACED PRESSURE CONTROLLER PER MM. OPS CHECKED OK. RAN ENGINES TO PRESSURIZE ACFT PER PFHB, CKS OK.

Part: SLIDE — DEPLOYED (PAX DOOR)

WHILE REPOSITIONING A/C TO GATE FOR FIRST FLIGHT DEPARTURE, R1 SLIDE WAS INADVERTENTLY DEPLOYED DUE TO GIRT BAR APPARENTLY SHIFTED AND WHEN OPS ATTEMPTED TO BOARD A/C GIRT BAR GOT CAUGHT ON DOOR FRAME AND DEPLOYED WHEN DOOR WAS OPENED FULLY. MTC FERRY A/C TO SLC FOR SLIDE REPLACEMENT. REPLACED SLIDE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

PRESSURIZATION LOST AFTER T/O FROM COS. UNABLE TO REGAIN PRESSURATION ANY CONFIGURATION. CHECKED ALL DOORS, RAN ENGS AND PACKS ON GROUND. ACFT PRESSURIZATION NORMAL.

Part: SKIN — GOUGED (BS 807)

FUSELAGE SKIN FS 807-907, STRINGER 25L-27R, SKIN GOUGE REPAIR. THE FUSELAGE SKIN WAS BADLY SCRATCHED AND GOUGED FROM FS 807 TO FS 907 BETWEEN STRINGERS 25L AND 27R DUE TO IMPACT WITH GROUND EQUIPMENT. THE SKIN WAS CUT AT FS 807 BETWEEN STRINGER 25L AND 27R AND THE AFT SECTION REMOVED TO THE EXISTING BUTT SPLICE AT FS 907. A NEW SECTION OF SKIN WAS SPLICED IN WITH AN EXTERNAL REPAIR STRAP PER ER/A 368360-14, REV A.

Part: BEARING — FAILED (LT AILERON)

AILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARING AND SYS OPS NORMAL.

Part: FITTING — GOUGED (PAX DOOR)

PAE- FWD ENTRY DOOR UPPER AND LOWER FWD CATCH ROLLER FITTINGS GOUGED. BLENDED UPPER FWD LATCH, PLACED LOWER FITTING. OUT OF LIMITS.

Part: ANGLE — CRACKED (E/E COMPT)

PAE- E AND E BAY RACK SUPPORT CRACKED. REMOVED CRACKED ANGLE, FABRICATED NEW SUPPORT ANGLE AND INSTALLED.

Part: SUPPORT — CORRODED (BS 500)

PAE- FWD CARGO BAY, CORROSION ON FLR TO SIDEWALL SUPPORT, BS 500C-500C+3, LBL 25. REMOVED CORROSION, REMOVED AND REPAIRED. FLOOR SUPPORT, OUT OF LIMITS.

Part: ANGLE — WORN (LT VERT STAB)

PAE- LT VERTICAL STABILIZER TO BODY CLOSURE ANGLE IS CHAFED AND WORN THROUGH ON AFT END. REMOVED ANGLE, INSTALLED NEW ANGLE.

Part: BULB — FAILED (CABIN)

LEFT OVERWING EMERGENCY EXIT LIGHTIS INOPEIS INOPERABLE. RELAMPED EXIT LIGHT, OPS CHECK GOOD. (X)

Part: LENS — LOOSE (CABIN)

RIGHT HAND FUSELAGE EMERGENCY LIGHT JUST AFT OF WHEELWELL HAS LOOSE LENS. REMOVED AND REPLACED EMERGENCY LIGHT LENS. (X)

Part: FAIRING — BROKEN (RT TE FLAP)

AFTER DEPARTING EWR RIGHT MAIN LANDING GEAR WOULD NOT FULLY RETRACT, GEAR OPERATED NORMALLY IN DOWN POSITION. AFTER LANDING IN IND FOUND RIGHT INBOARD FLAP TRACK FAIRING WEDGED IN GEAR MECHANISM. REPLACED RIGHT INBOARD FLAP TRACK FAIRING. (M)

Part: HYD PUMP — LEAKING (B-HYD SYSTEM)

AIRCRAFT HAD A LOSS OF B-SYSTEM HYDRAULIC FLUID. REPLACED B-SYSTEM ELECTRIC HYDRAULIC PUMP ASSY. (M)

Part: DOUBLER — CORRODED (BS 794)

DURING C-CHECK, FOUND CIRCULAR DOUBLER AT AFT CARGO BAY LIGHT SWITCH IS CORRODED AROUND NUTPLATES. FORWARD SIDE OF BS 794, FRAME RBL 33, WL 162. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER. (M)

Part: STIFFENER — CORRODED (BS 314)

DURING C-CHECK, FOUND CORROSION ON STIFFENER AT LBL 16.5, BS 314, 320, 325, WL 208. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, REMOVED CORRODED PARTS AND INSTALLED NEW PARTS IAW SRM 51-10-02. (M)

Part: SUPPORT — CORRODED (BS 847-867)

DURING C-CHECK, FOUND CORROSION ON BOTTOM SIDE OF FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATES BS 847-867, RBL 19-24, WL 161. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW SUPPORT. (M)

Part: RIB — CRACKED (WS 185)

DURING C-CHECK, LEFT INBOARD FLAP UPPER FIXED PANEL APPROXIMATELY, WBL 85, OUTBOARD SUPPORT RIB IS CRACKED. REMOVED CRACKED RIB AND INSTALLED NEW RIB. (M)

Part: FLOORBEAM — CORRODED (BS 947)

DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 947, RBL 6, WL 208. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICATED INSTALLED PARTS PER SRM 53-30-51. (M)

Part: FLOORBEAM — CORRODED (BS 294)

DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20, WL 208. REMOVED CORROSION, REPAIRED UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20, WL 208. (M)

Part: HAT CHANNEL — CORRODED (BS 996)

DURING C-CHECK, FOUND CORROSION BS 996, RBL 5-49, WL 208-209. (HAT CHANNEL AND GALLEY ATTACH ANGLE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW ATTACH ANGLE AND HAT CHANNEL. (M)

Part: FLOORBEAM — CORRODED (BS 344)

DURING C-CHECK, FOUND CORROSION BS 967, FOUND ON UPPER CHORD OF THE FLOORBEAM AT BS 344, RBL 8.5, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: HAT CHANNEL — CORRODED (BS 996)

DURING C-CHECK, FOUND CORROSION BS 996, LBL 22-34, WL 208, (HAT CHANNEL FORWARD FLANGE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW HAT CHANNEL. (M)

Part: SUPPORT — CORRODED (BS 967)

DURING C-CHECK, FOUND CORROSION BS 967, LBL 53 - RBL 53, WL 208, (AROUND FLOOR BOARD ATTACH HOLES). CORROSION FOUND TO BE OUT LIMITS. REPAIRED UPPER CHORD. (M)

Part: FLOORBEAM — CORRODED (BS 1006)

DURING C-CHECK, FOUND CORROSION BS 1006, LBL 36-RBL 36, WL 208, AROUND FLOOR BOARD ATTACH HOLES. REMOVED OUT OF LIMITS AREA AT BS 1006, LBL 29, WL 208. REPAIRED IAW SRM 51-70-11. (M)

Part: FLOOR SUPPORT — CORRODED (BS 953)

DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 45, BS 953, AND BS 957.5, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL (FLOOR SUPPORT).

Part: CLIP — CORRODED (BS 867)

DURING C-CHECK, FOUND CORROSION ON STRINGER CLIP BS 867, RBL 21, WL 164. REMOVED CORROSION FROM STRINGER CLIP FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STRINGER CLIP. (M)

Part: SKIN — CORRODED (CARGO DOOR)

DURING C-CHECK, FORWARD CARGO DOOR, INNER SKIN CRACKED AND/OR GOUGED AT LIGHTENING HOLE 17 INCH AFT OF FORWARD, EDGE 33 INCH ABOVE LOWER EDGE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER. (M)

Part: HAT CHANNEL — CORRODED (BS 307)

DURING C-CHECK, FOUND CORROSION ON CORNER OF HAT CHANNEL AND SUPPORT BRACKET BS 307, LBL 11, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: CHANNEL — CORRODED (BS 500)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500, LBL 24, WL 155. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE. (M)

Part: FLOORBEAM — CORRODED (BS 294)

DURING C-CHECK, FOUND CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: ANGLE — CORRODED (BS 1012)

DURING C-CHECK, CORROSION BS 1012-1030, LBL 6 - 1030, LBL 6 - RBL 15, WL 208-209, (FLOOR WEB ATTACH STRAPS AND GALLEY ATTACH ANGLES). REMOVED CORROSION, FROM GALLEY ATTACH ANGLES AND FOUND TO BE OUT OF LIMITS, AFTER CORROSION REMOVAL FOUND OTHER AREAS TO BE IN LIMITS. FABRICATED AND INSTALLED NEW ATTACH ANGLES. (M)

Part: FLOORBEAM — CORRODED (BS 328)

DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 328, LBL 28.5, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: INTERCOSTAL — CORRODED (BS 787-907)

DURING C-CHECK, INTERCOSTAL CRACKED AT AFT CARGO DOOR UPLATCH ATTACH BS 787-807, RBL 16.5, WL 203. REPLACED INTERCOSTAL WITH NEW PART. (M)

Part: FORMER — CRACKED (BS 295)

DURING C-CHECK, FORMED SECTION CRACKED AT BS 295, RBL 54, WL 209. REMOVED AND REPAIRED CRACKED AREA. (M)

Part: FLOORBEAM — CORRODED (BS 312)

DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, RBL 34.5, WL 208. BLENDED CORROSION. FOUND PART OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: ANGLE — CORRODED (BS 305-323)

DURING C-CHECK, FOUND CORROSION ON NUTPLATES OF FSD MOP SILL L-ANGLE SUPPORT FROM BS 305-323. REMOVED CORROSION, PART OUT OF LIMITS, REMOVED L-ANGLE SUPPORT AND TREATED, PRIMED INSTALLED NEW PART. (M)

Part: INTERCOSTAL — CORRODED (BS 996-1006)

DURING C-CHECK, FOUND CORROSION BS 996-1006, LBL 10 - 13, WL 208 (INTERCOSTAL). REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL. (M)

Part: FITTING — CORRODED (ENTRY DOOR)

DURING C-CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR GIRT BAR FITTING MOUNTS. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, INSTALLED NEW FITTING MOUNTS IAW SRM 51-40-02. (M)

Part: ANGLE — CRACKED (BS 290)

DURING C-CHECK, INTERCOSTAL TO SKIN TIE ANGLE IS CRACKED AT STATION 290, WL 241, BETWEEN STRINGER 13 AND 14 RIGHT. REMOVED AND REPLACED ANGLE. (M)

Part: INTERCOSTAL — CORRODED (BS 988)

DURING C-CHECK, FOUND CORROSION BS 988, RBL 17, WL 208, INTERCOSTAL FLOOR ATTACH HOLE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW AND INSTALLED NEW INTERCOSTAL. (M)

Part: INTERCOSTAL — CORRODED (BS 1008)

DURING C-CHECK, FOUND CORROSION BS 108, LBL 8, WL 208 (INTERCOSTAL). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL. (M)

Part: CHANNEL — CORRODED (BS 347)

DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 11.5, BS 347, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL. (M)

Part: INTERCOSTAL — CRACKED (BS 279)

DURING C-CHECK, INTERCOSTAL CRACKED AT BS 279, RBL 56, WL 231. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL. (M)

Part: EXTRUSION — CORROSION (BS 753)

DURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON BOTTOM SIDE OF CARGO TRACK BS 753.5, LBL 8, WL 141, (IN AFT CARGO BAY). REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED. (M)

Part: PANEL — CRACKED (LEFT WING)

DURING C-CHECK, FOUND UPPER PANEL JUST INBOARD OF NR 3 TRANSMISSION CRACKED. REPAIRED IAW SRM 51-70-10. (X)

Part: SKIN — PUNCTURED (RT TE FOREFLAP)

DURING C-CHECK, FOUND SMALL PUNCTURE ON UNDERSIDE OF INBOARD FOREFLAP JUST OUTBOARD OF CENTER TRACK. REPAIRED IAW SRM 51-70-10. (X)

Part: ANGLE — CRACKED (RIGHT WING)

DURING C-CHECK, FOUND SUPPORT ANGLE FOR UPPER SURFACE PANEL CRACKED (INBOARD OF INBOARD-MOST SPEED BRAKE, DIRECTLY ABOVE NR 5 FLAP TRACK). REPAIRED IAW SRM 51-30-01. (X)

Part: SUPPORT — CORRODED (BS 727)

DURING C-CHECK, FOUND CORROSION UNDER FLOOR SUPPORT AT BS 727D+15, LBL 3, LBL 8.10, AND LBL 12.5; WL 156. REMOVED DAMAGED AREAS OF FLOOR SUPPORTS AND REPAIRED IAW SRM 53-00-53. (X)

Part: SUPPORT — CORRODED (BS 727)

DURING C-CHECK, FOUND COROSION UNDER FLOOR SUPPORT AT BS 727D+A5, RBL 3, RBL 8.10, AND RBL 13.8; WL 156. REMOVED DAMAGED AREAS OF FLOOR SUPPORTS AND REPAIRED IAW SRM 53-00-53. (X)

Part: SKIN — PUNCTURE (LT TE FOREFLAP)

DURING C-CHECK, FOUND INBOARD FOREFLAP HAS PUNCTURE ON LOWER SKIN. REPAIRED IAW SRM 57-70-10. (X)

Part: FLOOR BEAMS — CORRODED (BS 727)

DURING C-CHECK, FOUND CORROSION AT NUTPLATES AT NUMEROUS LOCATIONS AT FLOOR STRAP, AFT CARGO BAY; BS 727D-5; LBL 40; WL 156. REMOVED STRAP, FOUND DAMAGED FLOOR BEAMS, REMOVED DAMAGED AREAS OF FLOOR BEAMS AND REPAIRED IAW SRM 53-0-53. (X)

Part: SKIN — GOUGED (LEFT WING)

DURING C-CHECK, FOUND FIXED LEADING EDGE GOUGED. REPAIRED IAW SRM 51-70-11. (X)

Part: LONGERON — GOUGED (LEFT PYLON)

DURING C-CHECK, FOUND LEFT PYLON INBOARD UPPER LONGERON CRACKED. REPAIRED IAW SRM 51-40-02. (X)

Part: ANGLE — CORRODED (BS 344)

DURING C-CHECK, FOUND CRACK IN ATTACH ANGLE COMMON TO CLOSE-OUT WEB IN FORWARD ENTRY DOORWAY, AFT END OF FUSELAGE CUT-OUT. REMOVED AND REPLACED DAMAGED ANGLE IAW SRM 51-20-02. (X)

Part: PANEL — GOUGED (LEFT WING)

DURING C-CHECK, FOUND UPPER OUTBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW SRM 51-70-03. (X)

Part: SUPPORT — CORRODED (BS 794)

DURING C-CHECK, FOUND CORROSION ON BOTTOM SIDE OF FLOOR SUPPORT AROUND NUTPLATE AT BS 794, LBL 3, WL 158. FLOOR SUPPORT EXFOLIATED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-53. (X)

Part: ANGLE — CRACKED (BS 500)

DURING C-CHECK, FOUND CRACKED SUPPORT ANGLE UNDER FORWARD CARGO BAY FLOOR AT BS 550 AND LBL 2 AND WL 155. REMOVED AND REPLACED DAMAGED ANGLE. (X)

Part: SKIN — DENTED (BS 947)

DURING C-CHECK, FOUND DENT ON FUSELAGE SKIN. DENT MEASURES 6 INCHES LONG AND 3.7 INCHES WIDE AND 0.12 INCH DEEP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PATCH IAW SRM 53-00-01. (X)

Part: SKIN — DENTED (BS 420)

FOUND SMOOTH DENT RT FUSELAGE .0937 INCH DEEP BY 3 INCH BY 2.5 INCH. REPAIRED IAW SRM 53-00-01 AND SRM 53-40-08. (X)