N612DL

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 89,657 hrs · 43,690 cycles

EMERGENCY LIGHT AT SEAT 3C INOPERATIVE. REPLACED DAMAGED WIRE HARNESS CONNECTOR IAW SWPM 20-30. OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,641 hrs · 43,682 cycles

FIRST CLASS EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED FUSE IN M9101, IAW AMM 33-51. OPS CHECKED GOOD.

Part: ARM — LOOSE (L3 DOOR) · airframe 89,014 hrs · 43,357 cycles

L3 DOOR INOPERATIVE, WILL NOT OPEN FULLY. FOUND GUIDE ARM HARDWARE LOOSE. TIGHTENED HARDWARE, DOOR OPS NORMALLY. CHECKED DOOR RIGGING IAW AMM 52-11-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 88,627 hrs · 43,211 cycles

DURING EMERGENCY LIGHT CHECK . FOUND SEAT LIGHT INOPERATIVE IN SEAT 19 THRU 26 FOUND BROKEN WIRE IN SEAT 26 F. REPAIRED WIRE IAW SWPM 20-30. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 87,247 hrs · 42,631 cycles

PAX SEAT 22D EMERGENCY LIGHT COVER MISSING. REPLACED EMERGENCY LIGHT ASSY AT SEAT ROW 22D. OPS CHECKED GOOD IAW AMM 33-51-05.

Part: LIGHT — INOPERATIVE (SEAT ROW 22 FED) · airframe 87,247 hrs · 42,631 cycles

SEAT 22 FED EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY AT SEAT ROW 22D. OPS CHECKED GOOD IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,840 hrs · 42,033 cycles

DURING EMERGENCY LIGHTS TEST, LIGHTS INOPERATIVE. FOUND BATTERY PACK BAD. REPLACED IAW AMM 33-51. OPS NOW OK.

Part: WIRE HARNESS — DAMAGED (L1 DOOR SLIDE) · airframe 85,493 hrs · 41,911 cycles

DOOR WOULD NOT ARM. FOUND SLIDE BUSTLE LOOSE. SECURED BUSTLE OPS CHECKED GOOD.

Part: BUSHING — LACK OF LUBE (L4 DOOR) · airframe 85,370 hrs · 41,860 cycles

L4 DOOR FAILED. PASSENGER DOOR ASSIST TRIGGER INSPECTION, BUNGEE WILL NOT RETURN TO NORMAL POS WHEN RELEASED REQUIRES MANUAL ASSISTANCE. LUBRICATED BUSHING AND OPS CHECKS NORMAL IAW AMM 52-11-32.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,548 hrs · 41,498 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/ INOP 2C36C. REPLACED LAMP IAW AMM 33-51.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 84,196 hrs · 41,351 cycles

ROW 31 EMERGENCY AISLE LIGHT INOPERATIVE. INSTALLED SPLICE AT BROKEN WIRE IAW AMM 33-51. FUNCTIONAL CHECKED GOOD.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 84,196 hrs · 41,351 cycles

ROW 43, EMERGENCY LIGHT INOPERATIVE, FOUND BAD CONNECTOR UNDER SEAT. REPLACED WIRE HARNESS UNDER SEAT IAW AMM 33-51. OPS CHECKED GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 83,882 hrs · 41,225 cycles

DURING SERVICE CHECK, FOUND ALL OF F/C EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT AND FOUND WIRE SHORTING ON FRAME AND POWER SUPPLY FUSE BLOWN. REPAIRED AND SECURED IAW AMM 33-51. ALL CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 81,883 hrs · 40,382 cycles

DURING EMERGENCY LIGHT INSPECTION FOUND SEAT 19 TO 26 PATH LIGHTS INOPERATIVE. REPAIRED WIRING AND TESTS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 81,739 hrs · 40,324 cycles

DURING EMERGENCY LIGHT INSPECTION FOUND SEAT 19D PATH LIGHT INOPERATIVE. REPAIRED WIRING AND TESTS OK.

Part: FUSE — BLOWN (CABIN) · airframe 81,304 hrs · 40,141 cycles

LINE MAINTENANCE FOUND ALL EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE IN FIRST CLASS CABIN. REPLACED BLOWN FUSE IN M9101 BATTERY PACK, ALL LIGHTS OPERATION NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 80,938 hrs · 39,992 cycles

LINE MAINTENANCE FOUND INOPERATIVE EMERGENCY LIGHT IN FIRST CLASS CABIN. REPLACED OPEN FUSE IN M9101 POWER SUPPLY. LIGHT OPERATION NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,829 hrs · 39,519 cycles

FUSELAGE SKIN FS 472, 482 & 497, S-10R LIGHTNING STRIKES. COMPLIED WITH ERA 486867-14 REV A SECTION III PERMANENT REPAIR REF NR5.

Part: WIRE — LOOSE (CABIN) · airframe 79,588 hrs · 39,426 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 19D INOPERATIVE. MAINTENANCE SECURED THE WIRING. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — LOOSE (CABIN) · airframe 79,588 hrs · 39,426 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 2C INOPERATIVE. MAINTENANCE SECURED THE WIRING. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 78,978 hrs · 39,175 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 28 TO BE INOPERATIVE. MAINTENANCE RESEATED THECONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 78,978 hrs · 39,175 cycles

DURING A MAINTENANCE LAYOVER, MAINTENANCE FOUND THE ROW 2 EMERGENCY PATH LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE SEAT CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,144 hrs · 38,337 cycles

DURING FLIGHT CREW REPORTED POSSIBLE LIGHTNING STRIKE. FOUND 2 LIGHTNING STRIKES AT FS 710 AND FS 741 BETWEEN STR 5R AND 6R. BOTH DAMAGES WERE REPAIRED PER ERA 486943-14. (DL757102992)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,144 hrs · 38,337 cycles

LIGHTNING STRIKE RIGHT SIDE OF FUSELAGE AT APPROX STATION 383 STRINGER 13. REPAIRED PER ERA 486902-14. (DL757102976)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 75,499 hrs · 37,625 cycles

EMERGENCY LIGHTS INOP ROWS 19-26. FOUND WIRE BROKEN AT CONNECTION ON ROW 26. REPLACED CONNECTOR. LIGHTS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 1640 RBL42) · airframe 75,013 hrs · 37,373 cycles

MAIN CABIN FLOOR FRAME WEB AT STA 1640 FWD SIDE RBL 42 IS CRACKED AND FASTENER IS MISSING/ ACCOMPLISHED ERA 478213-14 REV ORIGINAL AT SAA SAT REF NON ROUTINE CARD 142468.

Part: FLOORBEAM — CORRODED (BS 345 BL0-LBL24) · airframe 75,013 hrs · 37,373 cycles

MAIN CABIN FLOORBEAM HAS CORROSION ON UPPER CHORD AT STA 345 FROM BL0 TO LBL 24 CP 53-212-01-02.051, ACCOMPLISHED ERA 478033-14 ORIGINAL AT SAT REF NON ROUTINE 142174.

Part: SHEAR TIE — CORRODED (BS 1520 S23R) · airframe 75,013 hrs · 37,373 cycles

CORROSION ON FRAME AT STA 1520 FWD SIDE ABOVE S23RT BEHIND INSTRUMENT RACK AND GILL LINER STRAP, IN AFT CARGO PIT CP53-162-01I. FABRICATED AND INSTALLED NEW ANGLE/SHEAR TIE AT SAT SAA REF NON ROUTINE 142157.

Part: FLOOR SKIN — CORRODED (BS 1700 LBL 56) · airframe 75,013 hrs · 37,373 cycles

MAIN CABIN FSTA 1700-1720 LBL 56 TO RBL 41 CORROSION ON UPPER SURFACE OF FLOOR, INCLUDES CORROSION ON 2 DOUBLERS. REMOVED CORROSION AND REPLACED DOUBLERS AT SAA SAT REF NON ROUTINE CARD 140176.

Part: INTERCOSTAL — CORRODED (BS 1320 S28R) · airframe 75,013 hrs · 37,373 cycles

AFT CARGO LWR BILGE INTERCOSTAL VERTICAL WEB HAS CORROSION INBD AND OTBD SIDES BETWEEN STR 28R-29R STA 1320 TO 1340 CP 53-156-01I. R & R INTERCOSTAL AT SAA SAT REF NON ROUTINE CARD 142114.

Part: INTERCOSTAL — CORRODED (BS 1400 S30R) · airframe 75,013 hrs · 37,373 cycles

CORROSION ON INTERCOSTAL WEB AT BOTTOM FWD END 2 INCHES AFT OF STA 1400, AND BETWEEN S30AND S29RT, IN AFT CARGO PIT CP53-156-01I. REMOVED INTERCOSTAL AND REPLACED AT SAA SAT REF NON ROUTINE CARD 142141.

Part: STRINGER — CORRODED (BS 1444 S26R) · airframe 75,013 hrs · 37,373 cycles

AFT CARGO COMP BELOW E-6 EQUIPMENT RACK FWD END OF STR 26R IS EXFOLIATED IN 2 PIECES STA 1444 CP53-156-O1I. REPLACED STR AT SAA SAT ON NON ROUTINE CARD 144712.

Part: SKIN — DENTED (BS 297 S20-21L) · airframe 75,013 hrs · 37,373 cycles

DENT LOCATED LT FWD FUSELAGE BETWEEN STA 297 AND 310, S20L AND 21L. ACCOMPLISHED ERA 478375-14 REV ORIGINAL AT SAA SAT REF NON ROUTINE CARD 136282.

Part: SKIN — DENTED (BS 1391 S28R) · airframe 75,013 hrs · 37,373 cycles

DENT ON LOWER FUSELAGE SKIN AT STA 1391, BETWEEN STRINGERS 28R AND 29R. ACCOMPLISHED ERO 478389-14 REV ORIG AT SAA SAT REF NON ROUTINE CARD 136277.

Part: SKIN — DENTED (BS 1644 S20L) · airframe 75,013 hrs · 37,373 cycles

DENT ON FUSELAGE SKIN EXTERNAL SURFACE AT STA 1644, 1" ABOVE STR 20L, ACCOMPLISHED ERA 478388-14 REV ORIG AT SAA SAT REF NON ROUTINE CARD 136278.

Part: SKIN — DENTED (BS 710 S22L) · airframe 75,013 hrs · 37,373 cycles

DENT AT F-STA 710 STR 21 & 22L/ CUT OUT DAMAGE AND INSTALLED DOUBLER AT SAT REF NON ROUTINE CARD 136263.

Part: SKIN — DENTED (BS 1680 S21R) · airframe 75,013 hrs · 37,373 cycles

DENT ON FUSELAGE SKIN INNER SURFACE AT STA 1680 1" ABOVE STRINGER 21R / ACCOMPLISHED ERA 478686-14A AT SAT REF NON ROUTINE CARD 136268.

Part: MOUNT — CORRODED (FS 1473) · airframe 75,013 hrs · 37,373 cycles

SKIN AT FS 1473 ANTENNA MOUNT CORRODED, ACCOMPLISH REPAIR IAW ERA 301676-14, REV C.

Part: SKIN — CORRODED (BS 1440 S28R) · airframe 72,357 hrs · 36,198 cycles

FUSELAGE SKIN, FRAME AND STRINGER FOUND CORRODED AT STA 1440 STR 28R. A SKIN DENT WAS ALSO FOUND AT STA 1425. DAMAGE WAS CUTOUT, STRINGER AND BEAR STRAP WERE SPLICED AND SKIN REPAIRS WERE INSTALLED.

Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 71,557 hrs · 35,789 cycles

INSERVICE DAMAGE TO THE RT HORIZTONTAL STABILIZER LEADING EDGE, AUX SPAR WEB, AND AUX SPAR LOWER CHORD. REWORKED THE LEADING EDGE, SPLICED IN A NEW SECTION OF AUX SPAR WEB, AND INSTALLED A REPAIR FOR THE AUX SPAR LOWER CHORD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,492 hrs · 31,936 cycles

INSPECTION OF THE L1 DOOR CUTOUT UPPER FWD CORNER PER AD 2004-09-32 REVEALED A CRACK IN THE SKIN SURROUND BEAR STRAP. THE CRACK WAS REMOVED WITH A CUTOUT TO THE BEAR STRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092906-14AD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,193 hrs · 30,215 cycles

THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL DAMAGE. A NEW SECTION OF CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 384541-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,193 hrs · 30,215 cycles

THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 620 BETWEEN STRINGERS 16L & 17L NEAR AN EXISTING SKIN CUTOUT REPAIR. THE EXISTING REPAIR WAS REMOVED AND UNDERLYING SKIN AND CUTOUT INSPECTED. THE DENT WAS REMOVED WITH A CUTOUT, BOTH AREAS WERE REPAIRED WITH A SINGLE ALUMINUM REPAIR. DOUBLER INSTALLED PER ER/A 384552-14, REV A.

Part: STRUCTURE — DENTED (HORIZONTAL STAB) · airframe 57,193 hrs · 30,215 cycles

THE LOWER STRUCTURE OF THE RT HORIZONTAL STABILIZER AUXILIARY SPAR WAS FOUND DENTED AT SPAR STA 330. THE STRUCTURE WAS CUT AND THE DAMAGED SECTION REMOVED. A NEW SECTION OF STRUCTURE WAS INSTALLED WITH 2 STEEL REPAIR ANGLES AND A STRAP PER ER/A 384563-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,193 hrs · 30,215 cycles

THE FUSELAGE SKIN WAS FOUND GOUGED AND DENTED NEAR THE R4 DOOR CUTOUT BETWEEN FS 1686 & 1691 AND BETWEEN STRINGERS 15R & 17R. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384536-14, REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,193 hrs · 30,215 cycles

THE FUSELAGE SKIN WAS FOUND WITH CORROSION AT FS 1610 BETWEEN STRINGERS 28L & 29R. THE UNDERLYING STRINGERS ALSO HAD AREAS OF CORROSION. THE STRINGERS WERE REPAIRED WITH CHANNEL SECTIONS PER THE SRM. THE SKIN DAMAGE WAS REMOVED WITH A 10 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384582-14, REV A.

Part: FITTING — DAMAGED (LT WING) · airframe 57,191 hrs · 30,214 cycles

WHILE ACCOMPLISHING THE ENGINE PYLON AND WING MODIFICATIONS REQUIRED BY AD 2000-20-09, 2 ATTACH HOLES FOR THE INBOARD SIDE LOAD FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED TO CLEAN AND ROUND CONDITION AND INSPECTED FOR CRACKS. OVERSIZE BOLTS WERE INSTALLED IN THE HOLES PER ER/A 384569-14AD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,860 hrs · 28,208 cycles

R2 EMERGENCY LIGHT INOP. RELAMPED.

Part: ODOR — DETECTED (CABIN) · airframe 52,762 hrs · 28,164 cycles

HEAVY ELECTRICAL SMELL IN ROWS 43-45 CO-PILOTS SIDE. TURNED OFF PASSENGER ENTERTAINMENT SYSTEM, SMELL WENT AWAY. TURNED ON PASSENGER ENTERTAINMENT SYSTEM. NO SMELL PRESENT. INSPECTED PSU'S AND BALLASTS FROM ADJACENT SIDEWALL LIGHTS. NO TROUBLE/SMELL FOUND. A/C OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (HYD SYSTEM) · airframe 48,036 hrs · 25,929 cycles

EICAS MESSAGE CTR HYD PRESS RESERVOIR AND RESERVOIR LIGHT. QTY DROPPED FROM 1.08 TO 1.05 AND AS LOW AS .99. FOUND RESERVOIR PRESS READING LOW. REPLACED HYD RESERVOIR PRESS MODULE, CHECKED GOOD. CREW REPORTED THAT LIGHT AND MESSAGE WENT OUT 15 MINS AFTER THEY DIVERTED.

Part: DUCT — RUPTURED (TAIL COMP)

APU BLEED DUCT LOCATED IN THE AFT ACCESSORY COMPARTMENT RUPTURED ON TAXI OUT. DUCT MATERIAL BROKE ONE OF THE ALTERNATE STAB TRIM CONTROL CABLE PULLEYS CAUSING THE ALTERNATE STAB TRIM CONTROL CABLE TO BIND. REPLACED DUCT, REPAIRED STAB CONTROL SYSTEM.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR)

RT AFT ENTRY DOOR LIGHT ON OVERHEAD PANEL. ADJ DOOR PER M/M 52-11. PRESSURIZED A/C TO 8 PSI. DOOR WAS FAIRED AND EVEN, OK FOR SERVICE.

Part: WEDGE — DELAMINATION (NR 7 LE SLAT)

DELAMINATION WAS FOUND ON THE LEADING EDGE OF THE TRAILING EDGE WEDGE ON THE NR 7 SLAT. THE DAMAGE MEASURED 24 INCHES LONG AND IS LOCATED 6 INCHES FROM THE OUTBOARD EDGE OF THE SLAT AND .75 INCH FROM THE LEADING EDGE. BECAUSE THE LEADING EDGE SLATS ARE THE SUBJECT OF AN AD, THIS WILL GIVE INSTRUCTIONS TO REPAIR THE DAMAGE. REPAIR THE NR 7 SLAT TRAILING EDGE WEDGE PER B757 SRM 51-70-10, FIG 11.

Part: ENGINE — DAMAGED (NR 2)

FOUND DURING PREFLIGHT, NOSE COWL ACOUSTIC LINER PUNTURED BY A PIECE OF FAN BLADE. REPAIRED PER SRM 54-01-01 PG 204. ALSO, REPLACED 1 PAIR OF FAN BLADES, DUE TO BIRD STRIKE.

Part: ENGINE — FAILED (NR 2)

RIGHT ENGINE EGT WENT INTO THE RED AT ABOUT 500 FT AGL ON APPROACH, FOLLOWED BY A RED INDICATION ON RIGHT ENGINE OIL PRESSURE. FLIGHT ATTENDANT REPORTED FIRE FROM RIGHT ENGINE. PERFORMED ENGINE FIRE CHECKLIST INCLUDING USING BOTH FIRE BOTTLES.

Part: TRACK LIGHT — DAMAGED (CABIN)

DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT FOUND DAMAGED IN FWD CABIN. REPLACED DAMAGED FLOOR TRACK SECTION, OPERATION NORMAL.

Part: RADOME — DELAMINATED (NOSE)

RECEIVED RADOME INTO SHOP AND UPON INITIAL INSPECTION FOUND DELAMINATION AT 12, 9, AND 6 O'CLOCK POSITIONS AROUND STATIC STRIP INSERT HOLES. ALSO FOUND MOISTURE IN CORE OF RADOME. REMOVED INSIDE SKIN TO DRY CORE AND REPLACED DAMAGED CORE AT INSERT HOLES, THEN REPLACED INSIDE SKIN PER SRM 53-10-72. APPLIED EROSION BOOT AND PAINT AS PER PS 900-9-1-11, NR 05. RADOME PASSED TRANSMISSIVITY TEST WITH 90.6 PERCENT. RADOME PASSED FINAL INSPECTION AND SENT TO STOCK.

Part: LIGHTNING HOLE — CRACKED (NR 1 PYLON)

NR 1 PYLON OUTBD LIGHTNING HOLE SHOWS CRACK INDICATION BY E/C ON UPPER AFT CORNER. FOUND AT HMV, REPAIRS ACCOMPLISHED PER DL ERA 270637-14.

Part: FLOORBEAM — CORRODED (FS 345)

AT HMV, FLOORBEAM AT FS 345 IS CORRODED FROM LBL 5 TO LBL 19. REPAIRED PER SRM 53-30-51 PG 212.

Part: FLOORBEAM — CORRODED (FS 324)

AT HMV FOUND FLOORBEAM CORRODED, FS 324 BETWEEN RBL 16 AND RBL 64. REMOVED DAMAGED SECTION OF CHORD, FABRICATED REPAIR PARTS PER SRM 53-10-08 FIG 201. INSTALLED T-CAP SECTION PER SRM 53-10-08 FIG 201.

Part: FLOORBEAM — CORRODED (FS 365)

AT HMV, FLOORBEAM AT FS 365 IS CORRODED IN SEVERAL AREAS FROM OBL TO RBL 64. REPAIRED PER SRM 53-00-51 PG 212.

Part: SKIN — HOLE (BS 1330)

AT HMV, BELLY SKIN AT FS 1330 HAS PUNCTURE DAMAGE AT FUSELAGE STATION 1330 ABOVE STRINGER 25L. REPAIRED PER SRM 53-00-01 FIG 208.

Part: SKIN — DENTED (FS 1595)

AT HMV, FOUND LOWER FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 1595 BETWEEN STRINGERS 24L AND 23L. REPAIRED PER SRM 53-00-01 PG 212-214.

Part: DOOR — DENTED (APU ACCESS DOOR)

DURING HMV VISIT, HANGAR INSPECTION FOUND THAT THE OUTER SKIN WAS DENTED JUST FORWARD OF CENTER LATCH. THE DENT WAS REPAIRED PER SRM 52-40-01.

Part: DOOR — DENTED (APU ACCESS DOOR)

DURING HMV VISIT IN ATLANTA, HANGAR INSPECTION FOUND THAT THE APU ACCESS DOOR HAD A DENT IN THE OUTER SKIN. THE SKIN WAS REPAIRED PER SRM 52-40-01.

Part: SKIN — CRACKED (RT ENG STRUT)

AT HMV, FOUND NR 2 ENG STRUT CRACKED AT OVAL ACCESS HOLE AT FWD END OF STRUT RT SIDE ABOVE FWD ENG MOUNT. REPAIRED PER SRM 54-51-01 FIG 203.

Part: FORMER — DENTED (FS 1540)

AT HMV, FOUND RT FORMER DENTED AT STA 1540 ABOVE FIXED FLOOR PANEL. CUT OUT DAMAGED AREA AND INST REPAIR DOUBLER PER SRM 51-70-11 PAGE 1 TO 5.

Part: RADOME — DAMAGED (FWD FUS)

RECEIVED RADOME INTO SHOP WITH TWO INCH GOUGE AT 4 O'CLOCK, TWENTY FOUR INCHES FROM AFT EDGE. REMOVED DAMAGED SKIN AND CORE. REPLACED SKIN AND CORE AS PER SRM 53-10-72. APPLIED ERROSION BOOT AND PAINT AS PER PS 900-9-1-11, NR 05. FINAL INSPECTED AND SENT TO STOCK.

Part: INTERCOSTAL — CRACKED (FS 365)

DURING LETTER CHECK K1, FOUND INTERCOSTAL STRAP CRACKED FS 365 IN E/E COMPT RT TUNNEL. REPAIRED PER M/M 53-01-04-8.

Part: INTERCOSTAL — CRACKED (FS 365)

DURING LETTER CHECK K1, FOUND INTERCOSTAL STRAP CRACKED FS 365 IN E/E COMPT LT TUNNEL. REPAIRED PER M/M 53-01-04-8.

Part: FLOOR PANEL — DEFECTIVE (MID GALLEY)

DURING LETTER CHECK K1, FOUND MID GALLEY FLOOR HAS SOFT SPOT LEFT CENTER BETWEEN OVENS. REPAIRED FLOOR PANEL PER SRM 53-00-50.