N962DN

Part: TURNBUCKLE — ABNORMAL (ELEVATOR) · airframe 51,170 hrs · 29,644 cycles

ELEVATOR CONTROL CABLE TURNBUCKLES WERE FOUND UN-SAFETIES. RIGGING VERIFIED.

Part: CONTROL CABLE — ABNORMAL (RUDDER) · airframe 51,170 hrs · 29,644 cycles

RUDDER CONTROL CABLES NR 1 AND 2 WERE FOUND UN-SAFETIES. RIGGING WAS VERIFIED.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

ELONGATED HOLES ON LOWER DOOR JAMB BEAM OUTBOARD EDGE AT AFT CARGO COMPARTMENT. REPAIRED IAW ERA 564792-14 REV O.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 51,170 hrs · 29,644 cycles

CRACK ON VERTICAL STABILIZER RIGHT HAND SIDE INTERNAL DOUBLER FROM STA 1486. REPLACED IAW DWG 5910242 REV BV AND SRM 51-30-02 AND 51-30-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACKED ANGLE STA 152 CANT BETWEEN LONGERON 1L AND 18L, AFT ACCESSORY COMPARTMENT. REPAIRED IAW ERA 564748-14.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,170 hrs · 29,644 cycles

CORROSION ON DOOR JAMB BEAM OVER PROJECTION LONGERON 29R, STA 1193 TO 1288. REPAIRED IAW ERA 564739-14.

Part: SKIN — DENTED (TE FLAP VANE) · airframe 51,170 hrs · 29,644 cycles

DENT ON UPPER SURFACE MID SECTION OF OUTBOARD VANE GUIDE, INBOARD FLAP AT RIGHT HAND WING. REPAIRED IAW SRM 57-20-05, FIG 4.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 51,170 hrs · 29,644 cycles

CRACK ON HORIZONTAL SUPPORT Y=1054 OF FORWARD BULKHEAD IN THE AFT CARGO BAY. REPAIRED THE BULKHEAD IAW ERA 564745-14.

Part: FRAME — CRACKED (BS 1520) · airframe 51,170 hrs · 29,644 cycles

CRACKED FRAME ANGLE BS 1520 CANT LONGERON 18R IN THE AFT ACCESSORY BAY. REPAIRED THE FRAME IAW ERA 564746-14.

Part: LONGERON — CRACKED (BS 1364) · airframe 51,170 hrs · 29,644 cycles

CRACKED LONGERON, BS 1364. REPAIRED IAW SRM 53-10-01 AND 51-30-05, 51-30-02.

Part: CARGO TRACK — CORRODED (BS 503-522) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON THE LT CARGO TRACK, BS 503 TO 522 IN FORWARD CARGO BAY. REPLACED THE CARGO TRACK IAW SRM 51-30-02, AND 51-30-05.

Part: PAN — DAMAGED (CARGO DOOR FRAME) · airframe 51,170 hrs · 29,644 cycles

ELONGATED HOLES AND PLUGS WERE FOUND ON FORWARD CARGO COMPARTMENT DOOR JAMB PAN. REPLACED DOOR JAMB PAN IAW SRM 53-60-02.

Part: LONGERON SPLICE — CORRODED (BS 1136-1155) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON LONGERON SPLICE 30 BETWEEN BS 1136 AND 1155 IN THE AFT CARGO COMPARTMENT. REPLACED IAW SRM 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACKED FRAME CLIP AND FRAME, STA 1494 BETWEEN LONGERON 3R AND 3L AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-05 AND DWG 9911860.

Part: CONNECTOR — CORRODED (FUEL CONTROL PNL) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON ELECTRICAL CONNECTORS ON FUEL QUANTITY CONTROL PANEL AT RIGHT HAND WING. REPLACED CONNECTOR J2 AND CLEANED CONNECTOR J1. OPERATION CHECKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CREASE ON FUSELAGE SKIN, STA 1269 BETWEEN LONGERON 25L AND 28L. REPAIRED IAW SRM 53-31-02 AND 53-30-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON SEAT TRACK STA 1261 TO 1264, X=44. REPAIRED IAW SRM 53-40-01 AND 51-10-05.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 51,170 hrs · 29,644 cycles

CRACKED NOSE LANDING GEAR DOOR JAMB STA 47 RIGHT AND LEFT HAND SIDE AT WHEEL WELL. REPAIRED IAW SRM 53-90-01 AND ERA 562420-14, REV O.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACKED LEFT AND RIGHT HAND ANGLES AT STA 883, X-42 AND X=-42 AT WING BOX AREA. PERMANENT REPAIR IAW ERA 498192-14MA.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION LONGERON SPLICE STA 1560 AT AFT CARGO COMPARTMENT. REPLACED IAW DWG 3913208, REV I AND SRM 51-30-01 AND 51-30-05.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 51,170 hrs · 29,644 cycles

LOWER EDGE SKIN MAIN ENTRY DOOR BENT AND NICK. REPAIRED IAW SRM 52-01-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON SEAT TRACK STA 200-256 X=-44 RIGHT HAND SIDE. REPLACED IAW SRM 53-40-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACKS WERE FOUND ON INTERCOSTAL BETWEEN 25R-26R, STA 1475-1486 AFT ACCESSORY COMPARTMENT. ERA 511165 COMPLIED WITH.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 51,170 hrs · 29,644 cycles

CRACK AND ELONGATED RIGHT HAND TIE TRACK BETWEEN STA 351-370 AT FORWARD CARGO COMPARTMENT. REPAIRED IAW ERA 562422-14 REV O.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON MEMBRANE STA 37, X=-11. REPAIRED IAW SRM 53-00-01.

Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 51,170 hrs · 29,644 cycles

CRACKED SCUFF PLATE AROUND HOUSING HANDLE AT FORWARD CARGO DOOR. REPLACED IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CUSP WEB UPPER /LOWER SURFACE ON STA 1262 TO 1269 BETWEEN X=44 AND X-60 AT LEFT HAND SIDE. CORROSION WAS ATTENDED IAW SRM 53-20-02.

Part: SEAT TRACK — CORRODED (BS 206-256) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON SEAT TRACK RBL 22 BETWEEN BS 206 TO 256. REPLACED IAW SRM 53-40-01.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 51,170 hrs · 29,644 cycles

EXCESSIVE CORROSION ON FLOOR PANEL AT COCKPIT AREA BETWEEN BS 120 TO 148, RBL 15 TO 56. REPLACED I AW SRM 51-10-05.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON ANGLE BETWEEN STA 1395, AFT PRESSURE BULKHEAD, LONGERON 29L=29R. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON SEAT TRACK STA 1260 TO 1273 X=22. REPLACED IAW SRM 51-10-05 AND 53-40-01.

Part: ANGLE — CORRODED (BS 1395 BULKHEAD) · airframe 51,170 hrs · 29,644 cycles

AFT FACE WEB ANGLE WITH CORROSION WAS FOUND BS 1395, LONGERON 29R IN AFT PRESSURE BULKHEAD. REPLACED IAW SRM 51-30-05 AND 51-30-02. (LP# 0346062)

Part: PAN — CRACKED (PAX DOOR) · airframe 51,170 hrs · 29,644 cycles

CRACKS ON UPPER/FORWARD PAN AT MAIN ENTRY. REPAIRED IAW SRM 52-10-02.

Part: CUSP WEB — CORRODED · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CUSP WEB UPPER/LOWER SURFACE FROM STA 698 TO 713, 727 TO 732 AND 747 TO 754, BETWEEN X=-54 TO -60. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02. (LP# 0345151)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CUSP WEB UPPER/ LOWER SURFACE ON STA 1236 TO 1247 BETWEEN X=-44 AND X=-60. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02.

Part: SEAT TRACK — CORRODED (BS 250-256) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON SEAT TRACK RBL 22 BETWEEN BS 250 TO 256. REPAIRED IAW SRM 53-40-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON FUEL ACCESS PLATE 200AT AND 520DT. REPLACED PER SRM 57-00-04. (LP# 0345792)

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

MAJOR REPAIR OF CRACK/DISBONDING ON CHANNEL OF FLOOR PANEL. REPAIRED IAW SRM 53-20-03 AND 51-20-00.

Part: BUSHING — CORRODED (LT HORIZ STAB) · airframe 51,170 hrs · 29,644 cycles

CORROSION IN FITTING BUSHINGS ON LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE, STA XHS 32.00. REPLACED AND LINE REAM PER MM.

Part: SUPPORT — CORRODED · airframe 51,170 hrs · 29,644 cycles

CORROSION ON LOWER SPAR SUPPORTS AND LOWER RETAINER AT MID CARGO DOOR BARRIER. REPLACED IAW SRM 51-30-01. (LP# 0344577)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACK ON CHANNEL OF FLOOR SUPPORT. REPAIRED IAW SRM 53-20-03.

Part: BEAM — CRACKED · airframe 51,170 hrs · 29,644 cycles

CRACK FORWARD/AFT EDGE ON BEAM NR 1 AT MAIN ENTRY DOOR. REPAIRED IAW SRM 52-10-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CUSP WEB UPPER/LOWER SURFACE STA 1251 TO 1252 BETWEEN X=44 AND X=60, LEFT HAND SIDE. CORROSION WAS ATTENDED PER SRM 53-20-02.

Part: ACCESS PANEL — CORRODED (WING) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON FUEL TANK ACCESS PLATES 520CT AND 620CT. REPLACED IAW SRM 57-00-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON R1 DOOR GIRT BAR LATH FLOOR SUPPORTS. DUE TO EXCESSIVE DAMAGE R1 DOOR GIRT BAR LATCH FLOOR SUPPORTS WERE REPLACED PER SRM 51-10-05.

Part: INTERCOOLER — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACK ON INTERCOSTAL BETWEEN BEAM NR 4 AND NR 5 STA 175 AT MAIN ENTRY DOOR. REPLACED IAW SRM 51-30-02 AND DWG 995576, REV K.

Part: RETAINER — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CHANNEL RETAINER ON PAN ASSEMBLY DRAIN L1 DOOR. REMOVED AND REPLACED CHANNEL IAW DWG 5936084, REV F AND SRM 51-30-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACKED FLOOR SUPPORT STA 1366 X=-19 . REPAIRED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON FLOOR SUPPORT AT BS 160 TO 200 X=7. REPLACED IAW SRM 51-10-05 AND 53-10-01.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 51,170 hrs · 29,644 cycles

CORROSION OUT OF LIMITS ON PASSENGER CABIN FLOOR SUPPORTS, BS 200,X=0, 54 AND 7. REPLACED IAW SRM 51-10-05 AND 53-10-01. (LP# 0340255)

Part: FLOOR SUPPORT — CORRODED (BS 170-200) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON CABIN FLOOR SUPPORT, BS 170 TO 200, X=-44. REPLACED IAW SRM 5130-05, 53-10-01 AND 51-30-02.

Part: PAN — WORN (CARGO DOOR) · airframe 51,170 hrs · 29,644 cycles

WORN INNER PAN ON AFT EDGE LOCATED BETWEEN BEAM NR 1 AND 2 AT CENTER CARGO DOOR. REPAIRED IAW SRM 52-30-02.

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CRACK ON FUSELAGE SKIN AROUND AFT HINGE OF LEFT HAND AFT NOSE LANDING GEAR DOOR. REPAIRED I AW SRM 53-30-01.

Part: CUSP WEB — OUT OF LIMITS (BS 495-498) · airframe 51,170 hrs · 29,644 cycles

CUSP WEB OUT OF LIMITS, REPAIRED BS 495 TO 498, RBL 54 AND 60 IAW SRM 53-20-09.

Part: SUPPORT — CRACKED (BS 1117) · airframe 51,170 hrs · 29,644 cycles

CRACKED SLANT PANEL SUPPORT STA 1117 BETWEEN LONG 23R AND 28R AT AFT CARGO COMPARTMENT. REPLACED IAW ERA 412247-14 MA, REV E. (LP# 0339404)

Part: LONGERON — CORRODED (BS 218-228) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON LONGERON 28L BETWEEN STA 218-228 AT FORWARD CARGO COMPARTMENT. REPAIRED IAW SRM 53-10-01. (LP#)0339394)

Part: LONGERON SPLICE — CORRODED (BS 218-237) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON LONGERON SPLICE BETWEEN Y=218 T O 237, 28L AT FORWARD CARGO COMPARTMENT. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5913508, REV CB. (LP# 0339130)

Part: FLOOR SUPPORT — CORRODED (BS 207) · airframe 51,170 hrs · 29,644 cycles

CORROSION ON FLOOR SUPPORT AT BS 207, RBL 4. REPLACED IAW SRM 51-30-01 AND 53-10-01.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 51,170 hrs · 29,644 cycles

CRACK ON FORWARD EDGE BEAM NR 4 AT FORWARD GALLEY SERVICE DOOR. REPLACED BEAM IAW SRM 51-30-01, 51-30-02, AND 51-30-05.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

PUNCTURE ON LEFT HAND CUSP WEB BETWEEN STA 864-883 AND X= 54 TO 60. REPAIRED IAW SRM 53-20-02.

Part: DOUBLER — WORN (BS 1437) · airframe 51,170 hrs · 29,644 cycles

WEAR ON PREVIOUSLY REPAIRED DOUBLER ON FRAME STA 1437, LONGERON 5LH AT AFT ACCESSORY COMPARTMENT. (LP$0333740)

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 51,170 hrs · 29,644 cycles

CORROSION FOUND ON DIAPHRAGM STA 180-200, LONGERON 0-8. REPAIRED IAW SRM 51-11-01.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 51,170 hrs · 29,644 cycles

WEAR ON DOUBLERS ON LOWER CORNERS AT AFT CARGO DOOR. REPLACED IAW SRM 51-30-02. (LP$ 0332986)

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 51,170 hrs · 29,644 cycles

DAMAGE FLOOR PANEL NBR 181DF. REPLACED FLOOR PANEL. (LP# 0324093)

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 51,170 hrs · 29,644 cycles

DAMAGE FLOOR PANEL NR 181FF. REPLACED FLOOR PANEL. (LP# 0324089)

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 51,170 hrs · 29,644 cycles

DAMAGED FLOOR PANEL NBR 181HF. REPLACED FLOOR PANEL. (LP# 0324099)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 50,787 hrs · 29,401 cycles

FOUND THE STAIR CATWALK EMERGENCY LIGHT BATTERY FAILED. R & R THE BATTERY.

Part: LIGHT — DAMAGED (CABIN) · airframe 50,109 hrs · 29,017 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED OR INOPERATIVE. REPLACED AFT CABIN DOOR EMERGENCY LIGHT ASSEMBLY. OPERATION CHECKS GOOD.0086832)

Part: TAIL CONE — OUT OF POSITION · airframe 48,872 hrs · 28,339 cycles

TAILCONE RELEASE PUSH IN EXTERIOR DOOR NOT IN POSITION. REPOSITIONED TAILCONE IAW SRM 51-30-02.

Part: GIRT BAR — DAMAGED (R1 DOOR) · airframe 48,456 hrs · 28,124 cycles

GIRT BAR WIRE MISSING ON R1 DOOR. INSTALLED R1 DOOR MM. OPS CHECKED GOOD.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 48,272 hrs · 28,018 cycles

EXIT SIGN OVER L1 DOOR FELL OFF. REINSTALLED EXIT COVER.

Part: FRAME — CRACKED (BS 1520) · airframe 46,324 hrs · 26,818 cycles

TAIL INTERIOR, CANTED FRAME WEB BS 1520 HAS CRACK. REPAIRED IAW SRM 53-10-03.

Part: HINGE — CRACKED (RT NLG DOOR) · airframe 46,324 hrs · 26,818 cycles

RT NLG DOOR AFT HINGE HAS A SKIN CRACK. REPAIRED IAW SRM 53-30-01, FIG 17.

Part: FRAME — CORRODED (BS 1364) · airframe 46,324 hrs · 26,818 cycles

AFT CARGO BIN B FRAME AT BS 1364 WEB AFT SIDE HAS CORROSION BETWEEN L29R TO L29L. REPAIRED IAW SRM 53-10-02, FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,324 hrs · 26,818 cycles

SKIN CRACK OTBD OF AIR STAIR CUTOUT LT EDGE. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 4 AND ERA 489806-14MA.

Part: CHANNEL — CRACKED (BS 1520) · airframe 46,324 hrs · 26,818 cycles

TAIL INTERIOR HAT CHANNEL ON AFT FACE OF CANTED BULKHEAD CBS 1520 CRACKED. REPLACED HAT CHANNEL IAW SRM 51-00-01.

Part: LATCH — WORN (TAILCONE) · airframe 46,324 hrs · 26,818 cycles

TAILCONE LATCH SPADE WORN AT 1O'CLOCK POSITION. REPLACED SPADE IAW MM.

Part: LATCH — WORN (TAILCONE) · airframe 46,324 hrs · 26,818 cycles

TAILCONE LATCH SPADE WORN AT 4 O'CLOCK POSITION. REPLACED SPADE IAW MM 535-52-01.

Part: LATCH — WORN (TAILCONE) · airframe 46,324 hrs · 26,818 cycles

TAILCONE LATCH SPADE WORN AT 8 O'CLOCK POSITION. REPLACED SPADE IAW MM.

Part: CONNECTOR — DIRTY (FIRE DETECTOR) · airframe 46,099 hrs · 26,709 cycles

CREW PERFORMED AN AIR TURN BACK, DUE TO RT ENGINE FIRE DETECTOR LOOP "A" FAULT. GOT AN INTERMITTENT RT ENGINE FIRE DETECTOR FAULT ON DESCENT. BEFORE LANDING, ALL WARNING LIGHTS AND ANNUNCIATIONS HAD EXTINGUISHED. MAINTENANCE DEFERRED RT ENGINE FIRE LOOP A TO MEL 26-11-01. 07JAN TPA PERFORMED FIM TASK. CLEANED AND CHECKED INTEGRITY OF CONNECTORS P1-874, P1-875, P1-8006 AND P1-8087. INSPECTED LOOP A AND B DETECTORS. ALL CHECKS OK.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 46,099 hrs · 26,709 cycles

TAILCONE GUIDE PIN RECEPTICALS, 4 EACH, WORN. REMOVED AND INSTALLED 4 LOWER GUIDE PINS IAW SRM 51-30-02.

Part: CABLE — FRAYED (TAILCONE) · airframe 46,099 hrs · 26,709 cycles

TAILCONE NITROGEN BOTTLE CABLE FRAYED, R & R.

Part: CABLE — DISCONNECTED (TAILCONE) · airframe 45,929 hrs · 26,622 cycles

TAILCONE UNSAFE LIGHT AT 60 KIAS. FOUND LOCKING CABLE DISCONNECTED AT INTERNAL RELEASE HANDLE. RECONNECTED LOCKING CABLE IAW MM. OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 43,250 hrs · 25,021 cycles

DURING SERVICE CHECK, FOUND LT OVERWIND EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE LIGHT. OPS CHECKED GOOD.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 42,623 hrs · 24,581 cycles

NITROGEN CYLINDER PULL CABLE HAS BROKEN STRANDS. R & R LANYARD.

Part: BULKHEAD — CORRODED · airframe 41,284 hrs · 23,779 cycles

DURING SCHEDULED MAINTENANCE, CORROSION FOUND ON BULKHEAD. REPAIRED IAW ERA 498949-14, REV A.

Part: SKIN — CRACKED (BS 1531) · airframe 41,107 hrs · 23,671 cycles

FUSELAGE SKIN CRACKED ON LT SIDE BS 1531. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01.

Part: FRAME — CRACKED (BS 902) · airframe 41,100 hrs · 23,667 cycles

LEFT FRAME AT FLOOR LINE, CRACKED IN RADIUS, BS 902.

Part: LONGERON — CRACKED (BS 1475) · airframe 41,100 hrs · 23,667 cycles

CRACK FOUND LONGERON 2R END FITTING AT BS 1475. REMOVED, FABRICATED AND INSTALLED NEW LONGERON SECTION IAW SRM 51-30.

Part: PIN — MISSING (ESCAPE SLIDE) · airframe 39,540 hrs · 22,727 cycles

DURING L1 DOOR MOUNTED ESCAPE SLIDE INSPECTION, WC 2561-01358-02A, SLIDE WAS FOUND TO BE MISSING SAFETY THREAD FROM THE LOWER PARACHUTE PIN IAW CMM PUB44608. R & R L1 DOOR SLIDE IAW AMM. RII COMPLIED WITH QC2084.

Part: ANGLE — CRACKED (LT WING) · airframe 39,540 hrs · 22,727 cycles

SUPPORT ANGLE LEFT WING, INBD WING RIB TO BODY FAIRING ATTACH POINT CRACKED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW DWG 5937452.

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 39,540 hrs · 22,727 cycles

DURING L2 DOOR MOUNTED ESCAPE SLIDE INSPECTION, FOUND TO BE MISSING SAFETY THREAD FROM LOWER PARACHUTE PIN IAW CMM 460100. REMOVED AND REPLACED SLIDE. SAFETIED CORRECTLY OK FOR SERVICE.

Part: OVEN — SMOKE (GALLEY) · airframe 39,540 hrs · 22,727 cycles

FORWARD GALLEY OVEN BEGAN TO SMOKE. CREW PULLED CIRCUIT BREAKER (F203) IN GALLEY AND IT STOPPED. PLACARD INSTALLED. MX OPERATED OVEN ON HIGH FOR OVER 20 MINUTES. COULD NOT DUPLICATE. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,435 hrs · 22,671 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AND CHARGER. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,531 hrs · 21,053 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND 4 EMERGENCY LIGHTS INOPERATIVE IN AFT AIRSTAIR AREA. REMOVED AND REPLACED BATTERY POWER SUPPLY PACK PER AMM. OPERATION CHECKS GOOD.

Part: BOTTLE — LOW (EVAC SLIDE) · airframe 36,476 hrs · 21,022 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND INSTALLED L1 DOOR SLIDE PER AMM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 36,474 hrs · 21,020 cycles

VERT STAB LT ANGLE CRACKED. REPAIRED INNER DORSAL FIN JOINT IAW ERA 498946-14 REV ORIG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

LT PYLON SUPPORT FRAME 1475 L 16L ANGLE IS CRACKED ON FWD SIDE BETWEEN FRAME AND FUSELAGE SKIN. REPAIRED IAW ERA 498952-14 REV ORIGINAL.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

CORROSION FOUND ON AFT PRESSURE BULKHEAD SKIN AT STA 1395 L27L. REPAIRED PER ERA 498949-14 REV ORIGINAL AND SRM 53-10-03 VOL 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

AFT CARGO STATION 1288 FRAME CORRODED ON UPPER SURFACE AND REAR SIDE. REPAIRED PER MD90 SRM 53-10-02 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

FRAME AT STATION 1307 CORRODED FROM 27L TO 28R. REPAIRED IAW MD90 SRM 53-10-02 FIG 2.

Part: RETAINER — DENTED (WINDSHIELD) · airframe 36,474 hrs · 21,020 cycles

RT FLIGHT COMPARTMENT WINDSHIELD AFT SEAL RETAINER HAS SCRIBE LINES AND IS DENTED IN MANY AREAS. REPAIRED FLIGHT DECK RT WINDOW ENCLOSURE LOWER SILL SEAL RETAINER IAW PRI 498951-14 REV ORIG (NR AAR 826739).

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 36,474 hrs · 21,020 cycles

CARGO TRACK CORRODED L28L STA 218-522. REPAIRED TRACK IAW SRM 53-40-01 FIG 7.

Part: SUPPORT FITTING — UNKNOWN (RT MLG) · airframe 36,474 hrs · 21,020 cycles

INSP/REPLACE RT MLG RETRACT ACTUATOR SUPPORT FITTING. CW EA 02-093855-03AD IAW MEO 0201.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

FWD CARGO PIT RT UPPER CUSP WEB AT STA 389 HAS CORROSION. REPAIRED CUSP WEB IAW MD90 SRM 53-20-02 FIG 26 VOL 1.

Part: PAN — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

C1 DOOR FRAME PAN CORRODED. REPAIRED IAW 53-60-02 PARA 13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,474 hrs · 21,020 cycles

MID CARGO BAY LEFT ZEE ANGLE CORRODED. REMOVED AND REPLACED CARGO TRACK LT FROM STA 605 TO 845 WITH REPAIR SPLICES LOCATED AT STA 665 AND 705 IAW WITH SRM VOL I 53-40-01 FIG 7.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 36,474 hrs · 21,020 cycles

CARGO TRACK CORRODED FROM STA 427-522 L29R. REPAIRED IAW MD90 SRM 53-40-01.