N928DN

Part: LUG — CRACKED (TERMINAL BLOCK) · airframe 47,007 hrs · 30,817 cycles

SHIP 9228 - FLIGHT CREW REPORTED AN ELECTRICAL ODOR IN THE FLIGHT DECK AND NOTICED SMOKE FROM THE F/O WINDSHIELD HEAT ELEMENT. TURNED OFF ANTI-ICE AND ODOR DISSIPATED. CORRECTIVE ACTION: APPLIED MEL. FOUND LUG ON LEFT WINDOW HEAT TERMINAL BLOCK R5-38 CRACKED AND ARCING/BURNING. R/R TERMINAL BLOCK R5-38 AND HARNESS. REPLACED F/O SIDE WINDOW. REPLACED RT WINDOW HEAT CONTROLLER. (LP# 0869935)

Part: CONNECTOR — LOOSE (LIGHT) · airframe 46,999 hrs · 30,812 cycles

AFTER GEAR EXTENDED ON FINAL FO SMELLED SMOKE OR A SMOKE LIKE SMELL DESCRIBED AS ACIDIC OR ELECTRICAL. PULLED AND OPENED C/B PANELS C/B PANELS BEHIND CAPT'S SEAT, INSPECTED FOR LOOSE CONNECTIONS OR DAMAGE. OPENED OVHD PANEL. FOUND F.O. GRIMES LIGHT BACKSHELL LOOSE, PINNED GEAR AND CYCLED GEAR HANDLE AND INSPECTED FOR ANY CONTACT WITH WIRING, NONE FOUND. FOUND F/O'S SIDE COMPARTMENT HAD WATER, REMOVED WATER AND VERIFIED IT DID NOT LEAK PAST COMPARTMENT. OPERATED ANTI-ICE AND ANTI-FOG IAW MD90 AMM 30-41-00. OPENED STATION 110 RELAY + JUNCTION PANELS, CHKD FOR EVIDENCE OF ARCING, NONE FOUND. UNABLE TO PIN POINT ANY FAULTS WITH A/C. ALL CHECKS GOOD. CONTACTED MCC, SATISFIED WITH INSPECTIONS PERFORMED. REMOVED PINS. RAN APU AND INSPECTED FOR LEAKS, NONE FOUND. NO SMELLS FROM PACKS. RAN ENGINES WITH PACKS NO SMELL OR ODORS TO NOTE. OK FOR SERVICE. (LP#4429684)

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 46,725 hrs · 30,637 cycles

ON TAKEOFF DOOR SLIDE AT 1L PARTIALLY CAME OUT OF ITS CASE. REINSTALLED L1 DOOR SLIDE PER AMM 25-61. A/C OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,589 hrs · 30,552 cycles

RT WHEEL WELL FWD DOOR JAM CRACKED. REMOVED, DRILLED AND BEGAN INSTALLATION OF RT WHEEL WELL FWD FRAME PER DWG 5930584U124 (889397). COMPLETED RT WHEEL WELL FWD FRAME INSTALLATION PER DWG 5930584U124. CHECKED MLG INBD DOOR OPERATION PER AMM 32-34. (LP 4183452)

Part: CONTROL UNIT — FAULTY (ANTI-SKID SYS) · airframe 46,576 hrs · 30,544 cycles

SHIP 9228 - CREW DECLARED EMERGENCY AND EXECUTED GO-AROUND AND LANDED WITH INOPERATIVE ANTI-SKID. WHEN GEAR WAS LOWERED, L INBD ANTI-SKID MESSAGES PRESENTED ON EOAP. CORRECTIVE ACTION: REPLACED AACU AND LEFT OUTBOARD WHEEL SPEED TRANSDUCER. NO-GO-ODI TASK 3246 C/W. AIRCRAFT OK FOR SERVICE. (LP# 4183443)

Part: DOOR — MISSING (VACUUM SERVICE) · airframe 46,441 hrs · 30,460 cycles

VACUUM WASTE SERVICE DOOR MISSING. INSTALLED NEW LAV SVC DOOR PER IPC 52-40.

Part: WIRE — BROKEN (CABIN) · airframe 45,984 hrs · 30,193 cycles

DURING SERVICE CHECK FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHT L2-847 INOP. FOUND WIRES BROKEN AT LIGHT CONNECTOR REPAIRED PER WDM 33-51-14 OPS CHECK GOOD OK FOR SVC.

Part: SKIN — WORN (L1 DOOR) · airframe 43,416 hrs · 28,637 cycles

WEAR ON L1 DOOR OUTER SKIN AROUND DOOR HOOK. REPAIRED IAW ETI-90-17-066 AND ERA 559490-14.

Part: BEAM — CRACKED (R1 DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACKED NR 4 BEAM FORWARD EDGE OF R1 DOOR. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: DOOR FRAME — CRACKED · airframe 43,416 hrs · 28,637 cycles

CRACK ON RIGHT DOOR FRAME BEAM AT BS 45. REPAIRED IAW SRM 53-90-01.

Part: BEAM — CRACKED (NLG DOOR FRAME) · airframe 43,416 hrs · 28,637 cycles

CRACK ON LEFT DOOR FRAME BEAM AT BS 45, NLG WHEEL WELL. REPAIRED IAW SRM 53-90-01.

Part: SKIN — CRACKED (BS 1520) · airframe 43,416 hrs · 28,637 cycles

CRACKED SKIN, BS 1520, BETWEEN 12 AND 1 HRS. REPAIRED IAW SRM 51-10-03.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

BENT AND WEAR ON OUTER SKIN, STA 408 BOTTOM EDGE AT FORWARD CARGO COMPARTMENT DOOR. REPAIRED IAW ETI-90-12-063 AND ERA 558140-14.0091876)

Part: SKIN — WORN (VERTICAL STAB) · airframe 43,416 hrs · 28,637 cycles

WEAR ON VERTICAL STABILIZER SKIN LEFT HAND SIDE. REPLACED IAW DWG 5936143 AND SRM 51-30-02 AND 51-30-05.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 43,416 hrs · 28,637 cycles

CRACK ON REPAIR PART ANGLE AT LEFT HAND VERTICAL STABILIZER. REPAIRED IAW ERA 558150-14 AND ETI-90-17-055.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CRACKED LONGERON 20R, STA 1055. REPAIRED IAW SRM 53-10-01 AND 51-30-05.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON AFT LOWER CARGO COMPARTMENT DOOR JAMB BEAM. REPAIRED IAW SRM 53-60-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FRAME STA 1250 BETWEEN LONGERON 29L-29R AT AFT CARGO COMPARTMENT. REPLACED IAW SRM 53-10-03.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FRAME STA 1328 BETWEEN LONGERON 27L AND 27R AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-10-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CRACK ON FUSELAGE SKIN BETWEEN STA 100 AND 120 LONGERON 27R, 28R AND 27L,28L. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-30-01.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CRACKED CENTER WING TO FUSELAGE ATTACH ANGEL LONGERON 20L BETWEEN STA 1041 AND 1060. REPAIRED IAW SRM 53-10-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FRAME CLIP STA 1364 BETWEEN LONGERON 26L AND 26R AFT CARGO COMPARTMENT. REPLACED IAW SRM 53-10-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON COUNTERSINK OF ACCESS PANEL 520PB. REPAIRED IAW SRM 57-00-04.

Part: WEB — CORRODED (BS 1212-1269) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON LOWER WEB BETWEEN BS 1212 - 1269 AT THE AFT CARGO DOOR FRAME. REPLACED IAW SRM 51-10-03 AND 53-30-02.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

WEAR ON PRODUCTION DOUBLERS ON AFT CARGO DOOR CORNERS. REPLACED IAW SRM 51-30-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON COUNTERSINK OF ACCESS PANEL 520FT. REPLACED IAW SRM 57-00-04.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

SEVERAL DENTS ON OUTER SKIN BETWEEN BEAMS 3 AND 5 IN THE FORWARD CARGO DOOR. COMPLIED WITH ERA 558137-14 AND ETI 90-17-062.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACKED AFT PAN ON AFT CARGO DOOR AT THE NR 1 BEAM. REPAIRED IAW SRM 52-0-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON COUNTERSINK ON ACCESS PANEL 620DB. REPAIRED IAW SRM 57*00-04.

Part: INTERCOSTAL — CRACKED (BS 1009) · airframe 43,416 hrs · 28,637 cycles

CRACKED INTERCOSTAL ON FORWARD DOOR FRAME, BS 1009, LBL 60, IN THE LT WHEEL WELL. REPLACED IAW DWG 5930584, SRM 51-30-02, AND 51-30-05.

Part: FRAME — CRACKED (BS 1520) · airframe 43,416 hrs · 28,637 cycles

CRACKED FRAME WEB AFT FACE, BS 1520 BETWEEN 1 AND 2 HRS POSITION. REPAIRED IAW SRM 53-00-01.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK ON INBOARD AND OUTBOARD PAN BELOW STOP FITTING NR 3, FORWARD EDGE OF AFT CARGO DOOR. REPAIRED IAW SRM 52-30-02.

Part: SKIN — DENTED (RT NACELLE) · airframe 43,416 hrs · 28,637 cycles

DENT ON RIGHT UPPER SKIN STATION 1364 AT RIGHT PYLON. COMPLIED WITH ERA 559786-14, REV O.

Part: DOUBLER — CORRODED (BS 769-788) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON PRODUCTION DOUBLER BS 769 - 788 BETWEEN LONGERON 28L AND 29R MID CARGO BAY. REPLACED IAW SRM 51-30-02, 51-30-05, AND 51-10-03.

Part: LONGERON — CRACKED (BS 1494) · airframe 43,416 hrs · 28,637 cycles

CRACKED LONGERON 3R, BS 1494 AT AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-01.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FUEL ACCESS PANEL 520CB, ON THE LEFT WING. REPLACED IAW SRM 57-10-05.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FUEL ACCESS PANEL 620CB, RIGHT WING. REPLACED IAW SRM 57-10-05.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1410) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOOR SUPPORTS BETWEEN BS 1364 TO 1410, LBL 20 , RBL 20. REPLACED IAW SRM 51-30-01.

Part: LONGERON — CRACKED (BS 1494) · airframe 43,416 hrs · 28,637 cycles

CRACK ON LONGERON 3R, BS 1494 IN THE AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 51-10-05, 51-10-03, AND 51-30-05

Part: DOOR — CRACKED (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK BELOW STOP FITTING NR 3 FROM OUTER PAN AT MID CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 52-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CRACKED FRAME ON STA 1458 LONGERON 1 AT AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON LEFT HAND FLOOR SUPPORT BETWEEN STA 1364 TO 1398 X=54 AT AFT WET AREA. REPLACED IAW SRM 51-10-03 AND 551-30-05.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK ON INNER PAN AFT EDGE, BEAM 5, FORWARD CARGO COMPARTMENT. REPAIRED IAW SRM 52-30-02.

Part: WEB — CORRODED (BS 1100-1136) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON LEFT UPPER WEB AND SURFACE, BS 1100 - 1136, LBL 54 TO 60. REPAIRED IAW SRM 53-20-02.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACKED ANGLE ON THE R1 DOOR BEAM NR 1 FORWARD EDGE. REPLACED IAW SRM 51-30-04 AND 51-30-05.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK ON INTERCOSTAL OF FORWARD MAIN ENTRY DOOR BETWEEN BEAMS 4 - 5, BS 188. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 9955766, REV K.

Part: SCUFF PLATE — CRACKED (L1 DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK ON SCUFF PLATE FROM HANDLE OUTER SKIN AT L1 DOOR. REPAIRED IAW ERA 501106-14MA, REV B.

Part: FRAME ANGLE — CORRODED (BS 1269) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FRAME ANGLE, BS 1269 BETWEEN LONGERONS 29 AND 30L IN THE AFT CARGO BAY. REPAIRED IAW SRM 53-10-02, 51-30-02, AND 51-30-05.

Part: SUPPORT ANGLE — CRACKED (BS 883) · airframe 43,416 hrs · 28,637 cycles

CRACK ON ANGLE SUPPORT, BS 883, LBL 41 AND RBL 41, Z=-8. THE SUPPORT ANGLE WAS REPAIRED IAW ERA 498192-14MA.

Part: LONGERON — CRACKED (BS 200) · airframe 43,416 hrs · 28,637 cycles

CRACK ON LONGERON 3R, BS 200. REPAIRED IAW SRM 53-10-01.

Part: WEB — CORRODED (BS 1231-1307) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON WEB RIGHT UPPER SURFACE, BS 1231 TO 1307, RBL 54 AND 60. REPAIRED IAW SRM 53-20-02.

Part: LONGERON — CRACKED (BS 1494) · airframe 43,416 hrs · 28,637 cycles

CRACKED LONGERON 12L, BS 1494 AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-01.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1402) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON THE FLOOR SUPPORTS BETWEEN BS 1364 - 1402, RBL 44. REPLACED THE FLOOR SUPPORT.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACK ON ANGLE OF FORWARD MAIN ENTRY DOOR BELOW BEAM NR 4, BS 174. REPLACED THE ANGLE.

Part: WEB — CORRODED (BS 148-160) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON LOWER WEB SURFACE BS 148 - 160, RBL 44. REPAIRED IAW SRM 53-00-01, 51-10-03, 51-30-02, 51-30-05, AND 51-30-08.

Part: WEB — CORRODED (BS 1079-1136) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON LEFT WEB UPPER SURFACE, BS 1079 - 1136, LBL 54 TO 60. REPAIRED IAW ERA 511165-14.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON THE GRIT BAR LATCH FITTINGS AT THE R1 DOOR. REPLACED IAW SRM 51-10-05, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON THE FLOOR SUPPORT BS148 - 200, LBL 7. REPLACED THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1410) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON THE RIGHT FLOOR SUPPORT BS 1364 - 1410, RBL 20, IN THE AFT WET AREA. REPLACED THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 160 - 200, RBL 43 AND 52. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: FLOORBEAM — CORRODED (BS 172) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOORBEAM BS 172 BETWEEN RBL 9 TO 42. REPLACED THE FLOORBEAM.

Part: SEAT TRACK — CORRODED (BS 200-256) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON SEAT TRACK BS 200 - 256, LBL 22. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-40-01.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOORBEAM BS 200 BETWEEN LBL 15 - 42. REPLACED THE FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (BS 199-204) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 199 - 204, LBL 15. REPLACED IAW SRM 51-10-05, 51-30-02 AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (BS 200-255) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON FLOOR SUPPORT BS 200 - 255, LBL 15. REPLACED IAW SRM 51-30-05 AND 51-30-01.

Part: BEAM — CRACKED (PAX DOOR) · airframe 43,416 hrs · 28,637 cycles

CRACKED FORWARD MAIN ENTRY DOOR BEAM NR 1 FORWARD AFT EDGES. REPAIRED IAW SRM 52-10-02.

Part: ACCESS PANEL — CORRODED (WING) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON COUNTERSINK OF FUEL PANELS 620AT AND 620DT. FOUND TO BE OUT OF LIMITS. REPLACED 620DT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON RIGHT HAND SEAT TRACK STA 200-256, X=-44. REPLACED IAW SRM 51-30-01 AND 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON RIGHT HAND SEAT TRACK STA 200-273, X=-22. REPLACED SEAT TRACK IAW SRM 53-20-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,416 hrs · 28,637 cycles

CORROSION ON WEB STA 389-408 X=-54 AND -60. REPAIRED IAW SRM 51-11-01, 51-30-01, 51-30-05.

Part: PIN — DETACHED (L1 DOOR SLIDE) · airframe 42,311 hrs · 28,076 cycles

L1 DOOR SLIDE PACK DEPLOYMENT PINS FELL OUT. REMOVED AND REPLACED L1 DOOR SLIDE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,606 hrs · 27,640 cycles

OVERWING EMERGENCY LIGHTS DO NOT TURN OFF WITH OVERHEAD PANEL SWITCH IN THE "OFF" POSITION. REMOVED AND REPLACED BATTERY PACK IAW MM. OPERATION CHECKS GOOD.

Part: SKIN — TORN (FUSELAGE) · airframe 41,606 hrs · 27,640 cycles

FUSELAGE SKIN TORN AT L1 DOOR GUST LOCK CUTOUT. REMOVED AND REPLACED DAMAGED AREA IAW ERA 548946-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,594 hrs · 27,632 cycles

STA 1520, STR 7L AND 8L AFT FRAME WEB IS CRACKED AT LOWER CAP. REPAIRED IAW SRM 53-10-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,594 hrs · 27,632 cycles

STA 1520, BETWEEN STR 7R AND STR 8R AFT FRAME WEB IS CRACKED. REPAIRED IAW SRM 53-10-03.

Part: SKIN — CRACKED (RT WING) · airframe 41,606 hrs · 27,640 cycles

RIGHT WING LOWER LEADING EDGE XOS 282 PANEL AT FUELING PANEL IS CRACKED. REPAIRED IAW SRM 57-20-01.

Part: SKIN — CORRODED (BS 231) · airframe 41,594 hrs · 27,632 cycles

EXTERNAL FUSELAGE SKIN HAS A BULGE AND PULLED FASTENERS AT BS 231 LONGERON 28L. REPAIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,562 hrs · 27,610 cycles

EXTERIOR EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK IAW AMM. OPS CHECKED GOOD.

Part: OVEN — ODOR (GALLEY) · airframe 41,167 hrs · 27,399 cycles

FLIGHT ATTENDANTS REPORT BURNING, ELECTRICAL ODOR DURING CLIMB. GALLEY AND SIDEWALL LIGHTS POWER SECURED PER QRH. ODOR DISSIPATED. TROUBLESHOT. ODOR NOTED WHEN RUNNING OVEN. REMOVED AND REPLACED OVEN PER MM.

Part: SKIN — DENTED (R1 DOOR) · airframe 37,443 hrs · 25,173 cycles

FOUND SMALL DENT ON FORWARD R1 DOOR AT 5 O`CLOCK POSITION. REPAIRED DENT IAW SRM 52-01-01.

Part: SUPPORT — CHAFED · airframe 36,273 hrs · 24,418 cycles

VENTRAL STAIRS, LT UPPER SUPPORT ARM IS CHAFED AT UPPER INBD AFT CORNER. REPAIRED IAW ERA 528279-14, REV O.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,989 hrs · 22,994 cycles

DURING SERVICE CHECK, FOUND LOWER EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,989 hrs · 22,994 cycles

DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROW 24 AND 25 FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: DOOR FRAME — UNKNOWN (CARGO DOORWAY) · airframe 33,840 hrs · 22,889 cycles

FUSELAGE, AFT CARGO DOORWAY, LOWER JAMB BEAM, L-28R CORROSION REPAIRED IAW ERA 398119-14.

Part: FIRE DETECTOR — CHAFED (NR 2) · airframe 32,572 hrs · 22,149 cycles

NR 2 ENGINE FIRE DETECTOR ILLUMINATED FOLLOWED BY RT ENGINE FIRE WARNING. PERFORMED QRH PROCEDURE, DISCHARGED NR 2 ENGINE. PERFORMED VISUAL CHECK. ALL EXTERNAL VISUAL CHECK NORMAL. NO ABNORMAL ENGINE INDICATIONS PRIOR TO FIRE WARNINGS. MX FOUND LOWER FAN ACCESSORY ZONE FIRE DETECTOR CHAFED FROM COWL OPEN ROD. REPLACED A/B LOOP ASSEMBLY IAW AMM. TESTED GOOD. REPOSITIONED COWL OPEN ROD AND R & R NR 2 FIRE BOTTLE IAW AMM. ENGINE CHECKS GOOD.

Part: SKIN — UNKNOWN (HORIZONTAL STAB) · airframe 31,114 hrs · 21,395 cycles

HS UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD CATWALK EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT CONNECTOR. REPINNED PER SWPM. OPS CHECKED GOOD.

Part: SKIN — UNKNOWN (HORIZONTAL STAB) · airframe 30,415 hrs · 20,987 cycles

HORIZONTAL STABILIZER RT UPPER AFT SKIN FASTENER HOLES WITH SHORT E/D & BUSHING REPAIRS IAW ERA 491786-14, LOG 0613380, 0938307.

Part: SKIN — UNKNOWN (BS 1475) · airframe 30,381 hrs · 20,970 cycles

FUSLAGE, SKIN, STA 1475 BETWEEN L1-L2L & L1-L2R REPAIRED IAW ERA 491769-14, LOG 0613380,0938307.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,647 hrs · 20,612 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD ATTENDANT EMERGENCY LIGHT L2-787 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: WIRE — BROKEN (CATWALK) · airframe 28,024 hrs · 19,805 cycles

DURING LINE CHECK, MAINTENANCE FOUND ON LEFT SIDE OF CATWALK, WHITE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE AT BLUE QUICK DISCONNECT PIN. CRIMPED NEW PIN PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: RAIL — CORRODED (UNKNOWN) · airframe 27,895 hrs · 19,730 cycles

CORROSION ON 2 LT GUIDE RAILS OF AFT PASSENGER COMPARTMENT FROM BS 1184 - 1288. SRM 53-40-01, VOL 1, FIG 6, REPAIR IAW SRM 53-40-01,

Part: SKIN — UNKNOWN (BS 243) · airframe 27,895 hrs · 19,730 cycles

DENT ON LT FUSELAGE SKIN AT STA 243 L17, SRM 53-30-01, VOL 1, FIG 1.

Part: SPAR — CRACKED (WING) · airframe 27,895 hrs · 19,730 cycles

WING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.

Part: JACKSCREW — UNKNOWN (HORIZONTAL STAB) · airframe 27,895 hrs · 19,730 cycles

HORIZONTAL STABILIZER JACKSCREW REPAIRED IAW EA 02-075254-12.

Part: LUG — UNKNOWN (HORIZONTAL STAB) · airframe 27,895 hrs · 19,730 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5510-01083.

Part: FRAME — UNKNOWN (BS 883 - 962) · airframe 27,895 hrs · 19,730 cycles

BS 883-BS 962 OVERWING FRAMES REPAIRED IAW AA 5310-01375.

Part: UNKNOWN — UNKNOWN (CARGO DOOR) · airframe 27,895 hrs · 19,730 cycles

FWD CARGO DOOR REPAIRED IAW EA 02-451701-12.

Part: STOP FITTING — UNKNOWN (CARGO DOOR) · airframe 27,895 hrs · 19,730 cycles

CARGO DOOR STOP PAD FITTINGS REPLACED IAW AA 5230-01136.

Part: JACKSCREW — UNKNOWN (HORIZONTAL STAB) · airframe 27,895 hrs · 19,730 cycles

HORIZONTAL STABILIZER -JACKSCREW ASSY REPAIRED IAW AA 2740-01071.

Part: NONE — NONE (NONE) · airframe 27,895 hrs · 19,730 cycles

PYLON AFT SUPPORT FITTING UPPER FASTENERS REPLACED IAW AA 5440-01069.

Part: SPAR CAP — UNKNOWN (VERTICAL STAB) · airframe 27,895 hrs · 19,730 cycles

VERTICAL STABILIZER, L/E FRONT SPAR CAP REPAIRED IAW AA 5530-01044.

Part: BULKHEAD — UNKNOWN (BS 1344) · airframe 27,895 hrs · 19,730 cycles

STA 1344, TEE BULKHEAD REPAIR BETWEEN L30 & 23R, SRM 53-10-02.