N965DN

Part: HINGE — DAMAGED (TAILCONE SLIDE) · airframe 42,910 hrs · 24,800 cycles

DURING A TAILCONE DEPLOYMENT TEST FROM THE BULKHEAD DOOR, THE DECORATIVE COVER PREVENTED THE SLIDE DEPLOYMENT. REPLACED HINGE AND INSTALLED DECORATIVE COVER.

Part: WIRE — BURNED (WINDOW HEAT) · airframe 42,711 hrs · 24,685 cycles

WITH ANTI-FOG SWITCH ON, GET AN ELECTRICAL ODOR IN COCKPIT. NO CIRCUIT BREAKERS OPEN, TURN SWITCH OFF, ODOR DISAPPEARS. TROUBLESHOT AND FOUND THE SLIDING F/O WINDOW ANTI-FOG WIRING SPLICES NOT MAKING GOOD CONTACT AND BURNING. REPAIRED THE WIRING IAW SWPM 20. OPS CHECKED ANTI-FOG SYSTEM. NO ODOR.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 42,529 hrs · 24,583 cycles

L1 SLIDE LANYARD DISCONNECTED AND DANGLING. REINSTALLED. OPERATION CHECKS OK.

Part: SIGN — UNSECURE (CABIN) · airframe 42,369 hrs · 24,489 cycles

FLIGHT ATTENDANT REPORTS EXIT SIGNS FALLING OFF AT LOCATION 608-104. REATTACHED SIGNS AND SECURE IAW MM.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 42,035 hrs · 24,308 cycles

R1 EMERGENCY EXIT SIGN MISSING. REPLACED. OPERATION CHECKED GOOD.

Part: HOOK AND LOOP — FAILED (EMERGENCY LIGHT) · airframe 41,574 hrs · 24,082 cycles

EMERGENCY EXIT SIGN COVER LOOSE. REPLACED THE HOOK AND LOOP. CHECKED OK.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 41,182 hrs · 23,849 cycles

EMERGENCY EXIT SIGN LOOSE. REATTACHED SIGN. OK FOR SERVICE.

Part: SKIN — DENTED (L1 DOOR) · airframe 40,443 hrs · 23,430 cycles

DENT ON EXTERIOR OF L1 DOOR BOTTOM LEFT SIDE. REPAIRED IAW SRM 52-01-01.

Part: SUPPORT ANGLE — BROKEN (WING TO FUSE) · airframe 40,053 hrs · 23,170 cycles

FOUND TWO SUPPORT ANGLES BROKEN, UNDER UPPER WING TO FUSELAGE FAIRING. REPLACED CENTER SUPPORT IAW DWG 9951259.

Part: FRAME — CRACKED (BS 1508) · airframe 39,981 hrs · 23,128 cycles

FORWARD FLANGE CRACKED, BS 1508. REPLACED FRAME SECTION IAW DWG 9911860.

Part: DOUBLER — CRACKED (BS 1520) · airframe 39,981 hrs · 23,128 cycles

AIRCRAFT SKIN DOUBLER CRACKED, 10 LBL, BS 1520, UPPER CHORD. REPAIRED IAW PRI/ERA 549409-14.

Part: THRESHOLD — DAMAGED (BS 173) · airframe 39,981 hrs · 23,128 cycles

R1 DOOR THRESHOLD WEB HAS HOLE IN IT, BS 173, RBL 54. REPLACED THE THRESHOLD IAW SRM 51-00-00.

Part: THRESHOLD — DAMAGED (BS 196) · airframe 39,981 hrs · 23,128 cycles

R1 DOOR THRESHOLD WEB HAD HOLE IN IT, BS 196, RBL 54. REPLACED THRESHOLD WEB IAW SRM 51-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 218) · airframe 39,981 hrs · 23,128 cycles

FLOOR SUPPORT CORRODED, BS 218, LBL 1. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-00-00.

Part: SEAT TRACK — CORRODED · airframe 39,981 hrs · 23,128 cycles

CORROSION FOUND AT INBOARD SEAT TRACK UNDER G2 GALLEY. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-40-01.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

FLOOR SUPPORT CORRODED BS 200, LBL 7. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

FLOOR SUPPORT CORRODED BS 200, RBL 7. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-00-00.

Part: WEB — CORRODED (BS 218) · airframe 39,981 hrs · 23,128 cycles

G2 GALLEY WEB CORRODED, BS 218, RBL 11. REPAIRED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 178-198) · airframe 39,981 hrs · 23,128 cycles

FLOOR SUPPORT CORRODED, BS 178-198 RBL 43. REPAIRED IAW SRM 51-00-00.

Part: SEAT TRACK — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

SEAT TRACK, RBL 46, BS 200 CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-40-01.

Part: FLOOR PANEL — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

FLOOR PANEL CORRODED, BS 200, RBL 9 - 46. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG 9936534.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

FLOORBEAM CORRODED, BS 200, RBL 46-56. REPLACED IAW SRM 53-00-01.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 39,981 hrs · 23,128 cycles

FLOORBEAM CORRODED, BS 200, RBL 5- LBL 5. REPLACED IAW SRM 53-00-01.

Part: SKIN — CRACKED (WINDOW) · airframe 39,981 hrs · 23,128 cycles

CAPTAIN'S SLIDING WINDOW CUTOUT CRACKED. REPLACED IAW DWG 591365.

Part: SUPPORT — CRACKED (BS 750) · airframe 36,671 hrs · 21,133 cycles

SLANT SUPPORTS CRACKED, BS 750 ABOVE LONGERON 27L. FABRICATED AND INSTALLED IAW SRM 412247-14MA AND SRM 51-30-02.

Part: FLANGE — BENT (L1 DOOR) · airframe 34,779 hrs · 19,920 cycles

L1 DOOR BOTTOM FLANGE BENT. STRAIGHTENED DOOR FLANGE IAW SRM 52-01-01. DOOR OPERATES NORMAL AT THIS TIME.

Part: SKIN — CORRODED (BS 1234) · airframe 34,698 hrs · 19,879 cycles

ACFT SKIN HAS STRIP OF LIGHT CORROSION BETWEEN L28R AND SEAL DEPRESSOR AT APPROXIMATELY BS 1234. FOUND TWO AREAS BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-60-02, FIG 9.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 34,687 hrs · 19,874 cycles

LEFT WHEEL WELL FORWARD CUTOUT WAS CRACKED UNDER HYDRAULIC SUPPORT BRACKET. REPLACED CHANNEL IAW SRM 51-30-02 AND DWG 5930584.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 34,687 hrs · 19,874 cycles

VERTICAL STABILIZER, ZFS-52.267, NUMEROUS LOOSE FASTENERS ON LOWER SIDE OF SPLICE, AMDS 5530-01044-05.

Part: LANYARD — MISSING (ESCAPE SLIDE) · airframe 34,687 hrs · 19,874 cycles

SLIDE FOUND WITH MANUAL INFLATION LANYARD NOT INSTALLED. INSTALLED SLIDE IAW AMDS 2561-4641.

Part: PIN — MIGRATED (R1 DOOR SLIDE) · airframe 34,687 hrs · 19,874 cycles

PIN MIGRATED FROM RECEPTACLE ON R1 SERVICE DOOR SLIDE. R & R SLIDE IAW AMDS 2551-4641.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,368 hrs · 19,692 cycles

CAT WALK FLOOR ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM. OPS CHECKED GOOD.

Part: WEDGE — DAMAGED (LT WING TE FLAP) · airframe 33,037 hrs · 18,861 cycles

LEFT INBD T/E FLAP WEDGE DAMAGED. REPAIRED IAW ERA 509956-14MA, REV O.

Part: WEDGE — DAMAGED (LT WING TE FLAP) · airframe 33,037 hrs · 18,861 cycles

LEFT INBD T/E FLAP WEDGE DAMAGED. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-00-01.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 33,028 hrs · 18,853 cycles

LEFT INBD LOWER SKIN AND T/E WEDGE AFT LT FLAP DAMAGED. FABRICATED AND INSTALLED REPAIR IAW PRI 521487-14, REV O.

Part: UNKNOWN — SMOKE (CABIN) · airframe 30,054 hrs · 17,156 cycles

CREW SMELLED SMOKE AND SAW A WISP OF SMOKE BY CAUTION LIGHTS. MX COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW AMM. CAUTION LIGHTS CHECK NORMAL. NO EVIDENCE OF OVERHEAT OR DAMAGE OF WIRING BEHIND CAUTION LIGHTS.

Part: TEE FITTING — CORRODED (BS 1437) · airframe 29,624 hrs · 16,892 cycles

AFT ACCESSORY COMPARTMENT BILGE AREA HAS CORROSION AT FS 1437 LBL 16 INCHES RBL16 INCHES BELOW THE CROSSOVER DUCT. REMOVED AND REPLACED LOWER TEE FRAME AT FS 1437 P/N 9912246U115.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,624 hrs · 16,892 cycles

FWD AIRSTAIR CUT OUT LOWER CENTER AREA BEHIND SEAL RETAINER IS BENT AND POSSIBLE CRACK AT FASTENER HOLE. REPAIRED PER ERA 501336-14 REV O.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,624 hrs · 16,892 cycles

AFT FUSELAGE APU CUT OUT LT TEE ANGLE WITH HEAVY CORROSION AT SEVERAL NUTPLATE LOCATIONS. REMOVED AND REPLACED TEE ANGLE PER SRM 51-30-02 VOL II AND 51-30-05 VOL II.

Part: INTERCOSTAL — CORRODED (BS 1438) · airframe 29,624 hrs · 16,892 cycles

AFT ACCESSORY COMPARTMENT BILGE AREA INTERCOSTAL AT BS 1438 RBL 13 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED INTERCOSTAL WITH FABRICATED INTERCOSTAL PER MD90 SRM 51-30-02 VOL II, 51-10-02 VOL II, AND DWG 9915563.

Part: FRAME — CORRODED (BS 465) · airframe 29,624 hrs · 16,892 cycles

FUSELAGE SKIN HAS BULGE SUSPECTED CORROSION AT BS 455 L30 ABOUT 3 INCHES FROM VHF ANTENNA. REPAIRED PER ERA 503597-14. CUT SECTION OF FRAME STA 465 AT L26L TO L27L FOR ACCESS AND REPAIRED FRAME PER SRM 53-10-02 FIG 2 P 17 VOL I.

Part: DOUBLER — CORRODED (BS 807-826) · airframe 29,624 hrs · 16,892 cycles

CENTER CARGO COMPTARTMENT BETWEEN BS 807-826 AND BETWEEN L29 - 30R SKIN HAS CORROSION. REPAIRED PER ERA 503600-14.

Part: LONGERON — CORRODED (BS 769 L29R) · airframe 29,624 hrs · 16,892 cycles

MID CARGO COMPARTMENT LONGERON 29R HAS CORROSION ON TOP OF LOWER FLANGE BS 769. REPAIRED PER ERA 503603-14.

Part: SHEAR TIE — CRACKED (BS 1364 L15-16L) · airframe 29,624 hrs · 16,892 cycles

NR 1 PYLON FRONT SPAR FWD END BETWEEN L15L AND L16L AT BS 1364 SHEAR TIE HAS CRACK AS VIEWED FROM CABIN. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-05 VOL II.

Part: FRAME — CORRODED (BS 750 L28R) · airframe 29,624 hrs · 16,892 cycles

MID CARGO COMPARTMENT UPPER SURFACE LOWER FLANGE ON FRAME AT BS 750 OTBD OF LONGERON 28R, HAS CORROSION AT TIP AREA AROUND FASTENER. REPAIRED PER ERA 503602-14.

Part: FINGER DOUBLER — DAMAGED (FS 459 L26L) · airframe 29,624 hrs · 16,892 cycles

LT ALTERNATE STATIC PORT SEMI-CRITICAL AREA HAS DEPRESSION NEXT TO RIVET FS 459 LONGERON 26L. REPAIRED PER ERA 503594-14.

Part: SKIN — CRACKED (BS 1435) · airframe 29,624 hrs · 16,892 cycles

BS 1435 TITANIUM SKIN-CRACKED JUST FWD OF CUT OUT FOR AFT VENTRAL STAIR MANUAL CONTROL. REMOVED AND REPLACED SKIN PER DWG 5911429 AND SRM 51-30-02 VOL II.

Part: SHEAR TIE — CORRODED (BS 1269) · airframe 29,624 hrs · 16,892 cycles

AFT CARGO BS 1269 STRINGER 29RT SHEAR TIE CORRODED, FOUND OUT OF LIMITS PER REF SRM 53-00-01. REPLACE WITH NEW SHEAR TIE.

Part: SEAT TRACK — CORRODED (BS 237-256) · airframe 29,624 hrs · 16,892 cycles

PITTING CORROSION ON SEAT TRACK BS 237 TO 256. REMOVED DAMAGED AREA AND REPLACE WITH NEW SPLICED SECTION PER SRM 53-40-01 VOL I FIG 6.

Part: SEAT TRACK — CORRODED (BS 221 LBL 44.5) · airframe 29,624 hrs · 16,892 cycles

CORROSION ON SEAT TRACK AT BS 221, LBL 44.5. REMOVED AND REPLACED SEAT TRACK AT BS 200-228 LBL44.5 PER SRM 53-40-01 VOL I FIG 6.

Part: SEAT TRACK — CORRODED (BS 1262) · airframe 29,624 hrs · 16,892 cycles

SEAT TRACK CORRODED BS 1262. REMOVED AND REPLACED SEAT TRACK FROM BS 1146 TO 1280.

Part: INTERCOSTAL — CORRODED (BS 845) · airframe 29,624 hrs · 16,892 cycles

CENTER CARGO COMPARTMENT STBS A 845 LT TIE DOWN TRACK WITH CORROSION AT LOWER SURFACE ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-01.

Part: CARGO TRACK — CORRODED (BS 826-845) · airframe 29,624 hrs · 16,892 cycles

CENTER CARGO BAY BETWEEN BS 826-845 LOWER SURFACE CARGO TRACK CORRODED ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER MD90 SRM 51-30-02 AND 51-30-05 VOL II.

Part: INTERCOSTAL — CORRODED (BS 826-845) · airframe 29,624 hrs · 16,892 cycles

CENTER CARGO COMPARTMENT BETWEEN BS 826 AND 845 LOWER SURFACE RT TIE DOWN TRACK WITH CORROSION ON INTERCOSTAL. REMOVED AND REPLACED THE INTERCOSTAL PER SRM 51-30-01.

Part: LONGERON SPLICE — CORRODED (BS 1354 L30L) · airframe 29,624 hrs · 16,892 cycles

CORRODED LONGERON SPLICE 30L AT BS 1354. REMOVED AND REPLACED PER SRM 51-30-05 VOL II AND 51-10-05 VOL II.

Part: SEAT TRACK — CORRODED (BS 256) · airframe 29,624 hrs · 16,892 cycles

FWD NR 2 GALLEY AREA SEAT TRACK HAVE TOPCOAT PAINT FLAKING OFF BS 256 RBL 44. REMOVED AND REPLACED AT BS 200-247 RBL 44 PER SRM 53-40-01 FIG 6 VOL I.

Part: LONGERON — CORRODED (AFT CARGO BAY) · airframe 29,624 hrs · 16,892 cycles

AFT CARGO LONGERON 29L CORRODED ON LOWER SIDE OF UPPER FLANGE AT BS 1258 SPLICE. REMOVED CORROSION, FOUND OUT OF LIMITS AND REPAIRED PER ERA 503587-14 REV O.

Part: DOOR FRAME — CORRODED (BS 693-750) · airframe 29,624 hrs · 16,892 cycles

CENTER CARGO BAY DOOR FRAME AT LOWER SIDE BETWEEN BS 693 AND 750 WITH SURFACE CORROSION. REPLACED DOUBLER PER 53-00-01.

Part: SKIN — CRACKED (BS 1475 L1-2R) · airframe 29,624 hrs · 16,892 cycles

BS 1475 FUSELAGE CROWN, FOUND SKIN CRACKED BETWEEN L1 AND L2R. REPAIRED PER DWG SG9055003 INSTALLATION -7007.

Part: FRAME — CORRODED (BS 1310) · airframe 29,624 hrs · 16,892 cycles

CARGO BAY BS 1310 STR 30 FRAME HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME FROM LONGERON 26R TO 27L. INSTALLED FRAME REPAIR PER MD90 SRM 53-10-07 VOL I INSTALLATION -703.

Part: CUSP WEB — CORRODED (BS 588 RBL 45) · airframe 29,624 hrs · 16,892 cycles

CABIN CUSP WEB CRACKED AT SEAT TRACK SPLICE FS 588 RBL45. REMOVED AND REPLACED CUSP WEB PER DWG 9930538 SRM 51-30-02.

Part: CUSP WEB — CORRODED (BS 1224) · airframe 29,624 hrs · 16,892 cycles

LT CUSP WEB AND BRACKET FS 1224 HAVE CORROSION. REMOVED DAMAGED AREA OF CUSP WEB AND FABRICATED REPLACEMENT SECTION WEB, SPLICE, AND DOUBLER RING. INSTALLED REPAIR PARTS PER SRM 53-20-02 FIG 26 VOL I.

Part: CUSP WEB — CRACKED (BS 588) · airframe 29,624 hrs · 16,892 cycles

CABIN FLOOR CUSP WEB CRACKED AT SEAT TRACK SPLICE FS 588 RBL 45. REPLACED PER DRWG 9930538.