N945DN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,782 hrs · 34,208 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE ROW 24. REPLACED THE BATTERY PACK. OPS CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (BS 1475) · airframe 40,089 hrs · 33,202 cycles

LONGERON TO FRAME ATTACH ANGLE IS CRACKED AT BS 1475, LONGERON 2L. REMOVED AND REPLACED IAW SRM 51-30-05 AND DWG 9964460, REV AB AND AA.

Part: SKIN — CRACKED (BS 1474) · airframe 40,089 hrs · 33,202 cycles

FUSELAGE SKIN HAS A CRACK, BS 1474, LONGERON 2R. REPAIRED IAW SRM 53-30-01.

Part: STIFFENER — CRACKED (BS 1520) · airframe 40,089 hrs · 33,202 cycles

STIFFENER CRACKED AT BSW 1520, BULKHEAD FRAME BETWEEN LONGERONS 7 AND 8L. REMOVED AND REPLACED IAW DWG 9911839 AND SRM 51-30-05.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 40,089 hrs · 33,202 cycles

RIGHT VERTICAL STABILIZER ATTACH ANGLE CRACKED. BS 1458-1486. REMOVED AND REPLACED IAW SRM 51-30-02 AND DWG 5912188, REV BD.

Part: ATTACH ANGLE — CRACKED (BS 1458-1486) · airframe 40,089 hrs · 33,202 cycles

LEFT VERTICAL STABILIZER ATTACH ANGLE, BS 1458 - 1486 CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02, 51-30-05, AND DWG 5912188, REV BD.

Part: SEAT TRACK — CORRODED (BS 932-937) · airframe 40,089 hrs · 33,202 cycles

RIGHT OUTBOARD RBL 54 SEAT TRACK BS 932 - 937.5 HAS SIGNS OF LIGHT SURFACE CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-10-05, AND 51-10-03.

Part: LONGERON CLIP — CRACKED (BS 1475) · airframe 40,089 hrs · 33,202 cycles

LONGERON CLIP FOUND TO HAVE A CRACK AT BS 1475, LONGERON 2R. FABRICATED A NEW LONGERON CLIP IAW SRM 51-10-05, 51-10-03, AND DW 5911432, REV CE, AND CF.

Part: FRAME — CRACKED (BS 45) · airframe 40,089 hrs · 33,202 cycles

NOSE LANDING GEAR WHEEL WELL CUTOUT FRAME CRACKED, BS 45, RIGHT SIDE. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 9910088, REV CJ.

Part: SKIN — CRACKED (BS 1530) · airframe 40,089 hrs · 33,202 cycles

CRACK ON EXTERNAL SKIN, BS 1530, LONGERON 25L. REPAIRED THE SKIN IAW ERA 2953999.

Part: ATTACH FITTING — CRACKED (BS 1475) · airframe 40,089 hrs · 33,202 cycles

FRAME ATTACHMENT IS CRACKED AT BS 1475 LONGERON 2R. REMOVED AND REPLACED IAW SRM 53-30-01.

Part: SWITCH — FAILED (PARKING BRAKE) · airframe 39,834 hrs · 33,054 cycles

ON APPROACH, AFTER LANDING GEAR LOWERED, THE PARKING BRAKE ILLUMINATED, QRH PROCEDURE COMPLIED WITH. TROUBLESHOT. REMOVED AND REPLACED SWITCH S1-130 AND AACU IAW MM OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,440 hrs · 32,828 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY IN AFT RIGHT LAVATORY. OPERATION CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 37,889 hrs · 31,850 cycles

THE CREW PERFOMED AN AIR TURN BACK TO ATL. AFTER TAKEOFF, CLIMBING THROUGH 1000 GL, THE LEFT CAPTAINS SIDE OF ACFT, O2 MASKS DROPPED. PRESSURIZATION NORMAL. MAINTENANCE FOUND SHORTED WIRES IN BUNDLE BACK WALL CONNECTOR PLUG SIDE FROM SWITCH 889347. REPAIRED IAW SWPM. ALL CHECKS GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 37,889 hrs · 31,850 cycles

THE CREW PERFORMED AN AIR TURN BACK. ALL LT SIDE PASSENGER O2 MASKS DROPPED. CABIN PRESSURIZATION NORMAL. MAINTENANCE REPLACED R2-315 RELAY. RESTOWED MASKS AND PERFORMED DROP TEST IAW AMM. ALL O2 MASKS DROPPED NOMALLY. ALL OPERATIONS NORMAL.

Part: LINE — FAILED (HYD SYSTEM) · airframe 37,581 hrs · 31,646 cycles

CREW EXPERIENCED A LOSS OF RT HYDRAULIC SYS FLUID DURING FLIGHT. AN EMERGENCY WAS DECLARED AND THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION FOR LANDING. MAINTENANCE FOUND THE RT ENGINE HYD PRESSURE LINE CRACKED AT THE B-NUT AT THE PRESSURE FILTER MODULE. INSTALLED A TEMPORARY HYD LINE IAW AMM 20-12. LINE TO BE INSPECTED EVERY 175 FLIGHT HOURS AND A PERMANENT LINE INSTALLED WITHIN 350 FLIGHT HOURS. RT HYDRAULIC SYS OPERATES AND LEAK CHECKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,449 hrs · 30,947 cycles

DAMAGE AFT OF R1 DOOR, JUST FORWARD OF WINDOW PLUG.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,248 hrs · 30,807 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM. OPS CHECKS OK.

Part: SLIDE — UNSECURE (TAILCONE) · airframe 35,036 hrs · 30,066 cycles

TAILCONE SLIDE OUT OF PACK. R & R TAILCONE EVACUATION SLIDE IAW AMDS 2461-4643. LP 1917510.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 35,019 hrs · 30,056 cycles

L1 DOOR SLIDE INOPERATIVE. R & R L1 DOOR SLIDE IAW JIC 2561-4641. LP 7291306.

Part: WIRE — BURNED (LIGHT SWITCH) · airframe 34,178 hrs · 29,531 cycles

SMOKE FROM CAPTAINS WING & NOSE LIGHT PANEL DURING SHORT FINAL. THE LIGHTS WERE TURNED OFF AND SMOKE CEASED. INSPECTED AND FOUND WIRE END BURNED ON NGL LIGHT SWITCH TERMINAL B2. SPLICED AND REPAIRED WITH NEW WIRE AND REPLACED NOSE TAXI LIGHT SWITCH IAW AMM. OPERATION CHECKS GOOD.

Part: LANYARD — INOPERATIVE (ESCAPE SLIDE) · airframe 30,428 hrs · 27,179 cycles

ON SERVICE CHECK, FOUND SLIDE LANYARD HANGING OUTSIDE BUSSLE AT L1 DOOR. REMOVED AND INSTALLED SLIDE IAW AMM. RII COMPLIED WITH. OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 30,334 hrs · 27,129 cycles

FLIGHT CREW REPORTED EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. MX REPLACED 20" OF MISSING LIGHT IAW MM.

Part: LANYARD — FRAYED (SLIDE COVER) · airframe 29,770 hrs · 26,762 cycles

DOOR SLIDE COVER LOCK LANYARDS ARE FRAYED, R & R LANYARDS IAW W/C 2500-4332.

Part: ANGLE — CORRODED (VENTRAL STAIRS) · airframe 29,770 hrs · 26,762 cycles

AFT VENTRAL STAIRS, LOWER SEGMENT IS CORRODED IN INTERNAL SKIN UNDER STEPS IN SEVERAL PLACE. REMOVED ANGLE FOUND 100 PERCENT OUT OF LIMITS, AND AREAS ON STRINGER SPLICES. REMOVED CORROSION IAW SRM 52-00-01, VOL 1 FIG 3 AND 51-10-03, PAR 26 & 27. FOUND WITHIN LIMITS IAW SRM 53-00-01, VOL. 1. FABRICATED NEW ANGLE IAW SRM 51-10-05 VOL 2 AND 52-60-01, FIG 2. INSTALLED ANGLE IAW SRM 51-30-02, VOL 2.

Part: STRUCTURE — CRACKED (BS 913) · airframe 29,770 hrs · 26,762 cycles

MAIN CABIN CENTER WING BOX UPPER SURFACE LT SIDE UPPER CHORD CRACKED AT FORWARD FASTENER GOING VERTICAL APPROX STA 913, LBL 48. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW ERA 498192-14MA AND SRM 51-30-02.

Part: CUSP WEB — CHAFED (BS 218) · airframe 29,770 hrs · 26,762 cycles

RT MAIN CUSP WEB, STA 218, RBL 46 FORWARD OF LIGHTNING HOLE HAS CHAFE MARKS. FOUND CRACKED AREA, CUT OUT DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED DOUBLER, FILLER AND SEAT TRACK IAW SRM 51-30-01 AND 53-20-02.