N909DA

Part: FITTING — LEAKING (SHUTOFF VALVE) · airframe 61,719 hrs · 33,533 cycles

SHIP 9209 - SMKE / FUME - WHILE TAXIING, CABIN BEGAN TO FILL WITH LIGHT/WHISPY WHITE SMOKE. STOPPED WHILE TAXIING. TURNED OFF R A/C SUPPLY SWITCH. WENT NO FURTHER AS WE TAXIED AND PULLED INTO THE GATE. LEFT ENGINE AND APU WERE ONLY ITEMS RUNNING. FOUND HYD FLUID LEAK FROM TAIL. INSPECTED TAIL CONE. FOUND RT SIDE RUDDER PWR SHUT-OFF VALVE FWD FITTING LEAKING. R/R RUDDER PWR SHUTOFF VALVE PER MD90 AMM 27-23. NO LEAKS NOTED. PERFORMED MINI DUCT BURNOUT PER WORK CARD 4950-2001. REPLACED COALESCER BAGS. OK FOR SVC. (LP# 5068544)

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 61,375 hrs · 33,306 cycles

ON CLIMBOUT ON SLAT RETRACTION NR 2 HYD QUANITYWENT TO 3 QTS RAN QRH QTY STABALIZED AT 13 QTS WITH PUMPS OFF ON DESCENT REPRESSURIZED SYSTEM FOR GEAR LOWERING QTY WENT TO 0 ON LANDING STILL WITH GOOD PRESSURE. FOUND LEAKING POWER SHUT OFF. REMOVED AND REPLACED POWER SHUT OFF VALVE. CK GOOD. COMPLIED WITH NO GO ODI PREVENTION AMDS WORK CARD 2900-2006. COMPLETED WITH NO ADDITIONAL FINDINGS. REFERENCE LOG 0783863 FOR REPLACEMENT OF O-RING ON NR 2 ENG LOWER I/B ACTUATOR TELEFLEX CABLE. (LP 4480414)

Part: LIGHT — UNKNOWN (CABIN) · airframe 59,659 hrs · 32,304 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE LOCATIONS:603. INSTALLED LIGHT STRIP PER AMM 33-41 OPS CK NORMAL MCO/PLAC RMVD.

Part: LIGHT — DETACHED (CABIN) · airframe 59,402 hrs · 32,144 cycles

EMERGENCY LIGHT STRIP THROWN IN OVERHEAD BINS AT ROW 26. RE-ATTACHED STRIP. OPERATION CHECKS GOOD.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,263 hrs · 32,067 cycles

LONGERON AT STA 1475 CRACKED ON BOTH SIDES AT THE VERY END OF THE LONGERON. COMPLIED WITH ERA 564026-14, REV O.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,263 hrs · 32,067 cycles

SKIN CLIP CRACKED AT STATION 1475 BETWEEN STRINGER 1 AND 2R. COMPLIED WITH ERA 564054-14, REV O.

Part: LINKAGE — WORN (COWLING) · airframe 59,263 hrs · 32,067 cycles

HINGE LINKAGE WORN ON LOWER COWL EXTENSION. HARDWARD AND LINKS REPLACED IAW CMM 71-13-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,886 hrs · 30,743 cycles

EMERGENCY OVERHEAD LIGHT IN AISLE FIRST ROW OF SEATS INOPERATIVE. REPLACED THE LAMPS AND SECURED.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS) · airframe 56,923 hrs · 30,766 cycles

LOST ALL ELECTRICAL POWER ON TOUCHDOWN. EMERGENCY POWER DID NOT PICK UP BUSS. EMERGENCY POWER AUTO FAULT WARNING ANNUNCIATED ON EOAP. EMERGENCY LIGHTS WORKED. WHEN EXTERNAL POWER APPLIED ALL BUSSES CAME ONLINE. NOTED LEFT AND RIGHT COOLING FAN CIRCUIT BREAKERS POPPED. CORRECTIVE ACTION: MAINTENANCE FOUND LEFT HEAT EXCHANGER FAN CIRCUIT BREAKER POPPED. RESET 2 EACH PHASE BREAKERS. RAN ENGINES AND 3 PHASES BREAKERS POPPED. FWD LEFT HEAT EXCHANGER FAN TO MCO/PLAC PER MEL 21-55-01. REMOVED AND REPLACED EPCU. REMOVED AND REPLACED HEAT EXCHANGER COOLING FAN IAW MM. OPERATION CHECKS OK.

Part: NOT REPORTED — DENTED (BS 249) · airframe 54,575 hrs · 29,384 cycles

DENT IN UPPER LEFT SIDE OF ACFT, BS 249. REPAIRED IAW PRI/ERA 516495-14, REV A.

Part: SKIN — DAMAGED (BS 229) · airframe 54,575 hrs · 29,384 cycles

DAMAGE TO PREVIOUS REPAIR AT BS 229 L18L. REPAIRED IAW PRI/ERA 516495-14, REV B.

Part: SKIN — DENTED · airframe 54,575 hrs · 29,384 cycles

DENT FOUND LT SIDE OF FUSELAGE AFT OF MAIN CABIN DOOR ABOVE THE CREASE LINE. REPAIR IAW ERA 516495-14, REV A.

Part: CONTROL VALVE — MALFUNCTIONED (SLAT SYS) · airframe 54,414 hrs · 29,290 cycles

AFTER TAKEOFF, SLATS SELACTED TO UP POSITION. DISAGREE LIGHT ILLUMINATED. PILOTS OBSERVED SLATS IN EXTEND POSITION DURING FLIGHT. MAINTENANCE REMOVED AND INSTALLED SLAT CONTROL VALVE.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 54,082 hrs · 29,113 cycles

FUSELAGE C3 LOWER SILL HAS CORROSION. REPAIR IAW PRI 541500-14, REV 1 AND ERA 541500-14, REV O.

Part: FRAME — CRACKED (BS 962) · airframe 54,070 hrs · 29,106 cycles

UPPER RADIUS OF FRAME TAB ON OVERWING FRAME BS 962 CRACKED. REPLACED FRAME AT BS 962 IAW AMDS 5310-01375-09-RT.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 54,070 hrs · 29,106 cycles

CORROSION ON C2 LOWER SILL. REPAIRED IAW PRI 541853-14, REV 2 AND ERA 541853-14, REV O.

Part: SKIN — CRACKED (BS 1493) · airframe 54,070 hrs · 29,106 cycles

SKIN CRACK, BS 1493, LONGERON 3R. REPAIRED IAW PRI 541952-14, REV O AND ERA 652952-14, REV O.

Part: PAN — CORRODED · airframe 56,326 hrs · 30,434 cycles

SERVICE PAN IS HEAVILY CORRODED. COMPLIED WITH PRI/ERA 541499-14, REV O.

Part: SKIN — CRACKED (BS 1520) · airframe 54,070 hrs · 29,106 cycles

TAIL INTERIOR, WEB AT CBS 1520 HAS CRACK ABOVE AND OTBD OF LOWER CHORD. REPAIRED IAW SRM 53-10-03.

Part: SKIN — CRACKED (BS 1508) · airframe 54,070 hrs · 29,106 cycles

TAIL INTERIOR-ACFT CROWN SKIN HAS 1" LONG CRACK, 8" RBL AT CBS 1508. REPAIRED STRAP DOUBLERS IAW SRM 51-11-01 AND DWG 5912141.

Part: PIN — MISSING (TAILCONE) · airframe 54,070 hrs · 29,106 cycles

NO TAIL CONE ALIGNMENT PINS INSTALLED IN CANTED FRAME, CBS 1567. INSTALLED NEW PINS IAW SRM 51-00-01.

Part: STIFFENER — CRACKED (BS 1542) · airframe 54,070 hrs · 29,106 cycles

TAIL INTERIOR CRACKED AT CBS 1542 LT WEB INBD EDGE, STIFFENER CHORD. REPAIRED IAW SRM 53-10-03.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 49,192 hrs · 26,025 cycles

VERTICAL STAB LEADING EDGE, FRONT SPAR CAP DAMAGED. REPAIRED IAW 5530-01044 SECT 02.

Part: SPAR — CRACKED (WING) · airframe 49,192 hrs · 26,025 cycles

WING REAR SPAR CRACKING. REPAIRED IAW 5710-01119,SECT 01/05.

Part: LONGERON — CORRODED (BS 1379) · airframe 49,192 hrs · 26,025 cycles

AFT CARGO BAY FS 1379, LONGERON 30 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED LONGERON NR 30 BETWEEN BS1354 -1382, FABRICATED AND INSTALLED NEW LONGERON AND SPLICE IAW SRM 53-10-01 AND 51-30-05.

Part: WEB — CORRODED (BS 160-200) · airframe 49,192 hrs · 26,025 cycles

CABIN FLOOR WEB CORRODED BS 160-200, LBL 10- RBL 10. CUT OUT DAMAGED FLOOR WEB. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-11-01 AND ERA 520330-14, REV O.

Part: SPACER — CORRODED (CARGO DOOR FRAME) · airframe 49,192 hrs · 26,025 cycles

CENTER CARGO DOOR FRAME SPACER CORRODED. REMOVED AND INSTALLED SPACER IAW SRM 53-60-02, FIG 9.

Part: SKIN — CRACKED (BS 1531-1542) · airframe 49,192 hrs · 26,025 cycles

LT FUSELAGE SKIN AT BS 1531-1542 BELOW AFT STAIRS CUTOUT IS CRACKED. HFEC INSPECTION AREA. FABRICATED AND INSTALLED PERMANENT REPAIR DOUBLER IAW SRM 53-00-01.

Part: SKIN — CORRODED (BS 850-870) · airframe 49,192 hrs · 26,025 cycles

AFTER REMOVAL OF RT BODY FAIRING RUB STRIP FOUND FUSELAGE SKIN AT BS 850-870, LONGERON 29 TO 30R CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-01, FIG 9 AND 51-30-05.

Part: SEAL BRACKET — CORRODED (R1 DOORWAY) · airframe 49,192 hrs · 26,025 cycles

R1 DOOR CUT OUT LOWER SEAL PANEL AT RBL 54 CORRODED. R & R SEAL PANEL.

Part: SEAT TRACK — CORRODED (BS 300) · airframe 49,192 hrs · 26,025 cycles

CABIN SEAT TRACK CORRODED AT RBL 54, BS 300. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-01, 51-30-05 AND 53-40-01, FIG 6.

Part: SKIN — GOUGED (BS 1227-1250) · airframe 49,192 hrs · 26,025 cycles

GOUGE FOUND ON PREVIOUS DOUBLER REPAIR AT BS 1227-1250, LONGERON 18R. REMOVED DAMAGED DOUBLER. FABRICATED AND INSTALLED INTERNAL DOUBLER REPAIR IAW ERA 464017 AND SRM 51-30-2, 51-30-05.

Part: SEAT TRACK — CORRODED (BS 992-996) · airframe 49,192 hrs · 26,025 cycles

LEFT OTBD SEAT TRACK BS 992-996 CORRODED. FOUND MATERIAL LOSS 50 PERCENT. R & R SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 237) · airframe 49,192 hrs · 26,025 cycles

SEAT TRACK, RBL 44. BS 237, CORRODED. FOUND OUT OF LIMITS. REMOVED & REPLACED IAW SRM 53-40-01, FIG 6 AND 53-00-01.

Part: SEAT TRACK — CORRODED (BS 1330) · airframe 49,192 hrs · 26,025 cycles

CORROSION FOUND ON SEAT TRACK, BS 1330, LBL 22. R & R SEAT TRACK SECTION IAW SRM 53-40-01, FIG 6, STA 1260-1363, LBL 22.

Part: CUSP WEB — CORRODED (BS 924-943) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 924- 943. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-03 AND DWG 9940443.

Part: SEAT TRACK — CORRODED (BS 1148-1190) · airframe 49,192 hrs · 26,025 cycles

BS 1148 -1190, LBL 55, SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK SECTION FROM BS 1183 -1089 IAW SRM 53-40-01 AND 53-00-01.

Part: SEAT TRACK — CHAFED (BS 1204) · airframe 49,192 hrs · 26,025 cycles

RT OTBD SEAT TRACK, BS 1204, CHAFED. FOUND AREA TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-40-01, FIG 6 AND 53-00-01.

Part: CUSP WEB — CORRODED (BS 614) · airframe 49,192 hrs · 26,025 cycles

MAIN CABIN CUSP WEB BS 614, LBL 54 LIGHTNING HOLE CORRODED. FOUND 100 PERCENT MATERIAL LOSS. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 18.

Part: SEAT TRACK — CORRODED (BS 382) · airframe 49,192 hrs · 26,025 cycles

MAIN CABIN, BS 382, LBL 22 SEAT TRACK GOUGED. MAINTENANCE R & R SEAT TRACK SECTION IAW SRM 51-10-05, 53-40-01, FIG 6 AND 53-40-9, FIG 6.

Part: SEAT TRACK — CORRODED (BS 674) · airframe 49,192 hrs · 26,025 cycles

CABIN SEAT TRACK CORRODED AT RBL 22, BS 674. TASK 53-211-02. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK FROM BS 579+12 TO 674+12, RBL 22 IAW SRM 51-30-01, 51-30-05, AND 51-40-01, FIG 6.

Part: CUSP WEB — CORRODED (BS 636-655) · airframe 49,192 hrs · 26,025 cycles

CABIN CUSP WEB CORRODED BETWEEN BS 636-655. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 560-580) · airframe 49,192 hrs · 26,025 cycles

CABIN CUSP WEB CORRODED, BS 560-580, RBL 54-59. CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 14.

Part: CUSP WEB — CORRODED (BS 1173-1190) · airframe 49,192 hrs · 26,025 cycles

CABIN CUSP WEB CORRODED BS 1173-1190, RBL 54-59 AROUND FASTENERS. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-02 AND 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 541-560. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 617-636) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 617 - 636. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-03, FIG 13.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 560 TO 579. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 674-693) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 674-693. 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 522 - 541. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 200-218) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 200-218, RBL 44-54. MATERIAL LOSS OF 50 PERCENT, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 22.

Part: CUSP WEB — CRACKED (BS 693-172) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 693 - 712. REMOVED CORROSION. CRACK NOTED. FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 769-788) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BS 769 - 788, RBL 54-59. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILL IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 962-984) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED BETWEEN BS 962-984. FABRICATED AND INSTALLED NEW CUSP WEB BETWEEN 962-1003, LBL 44-59 IAW SRM 51-30-02 AND DWG 9910151.

Part: CUSP WEB — CORRODED (BS 1204-1220) · airframe 49,192 hrs · 26,025 cycles

CUSP WEB CORRODED, BS 1204-1220 RBL 54-59. REPAIRED IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 484-503) · airframe 49,192 hrs · 26,025 cycles

DURING CHECK, CABIN CUSP WEB FOUND CORRODED AT BS 484-503, RBL 59 AROUND FASTENERS. REMOVED CORROSION. FOUND MATERIAL LOSS AT 50 PERCENT. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 AND 53-20-02, FIG 18.

Part: OVEN — SMOKE (GALLEY) · airframe 48,184 hrs · 25,382 cycles

FLIGHT CREW COMPLAINED OF ODOR AND SMOKE COMING FROM GALLEY OVEN. R & R FORWARD GALLEY OVEN. OPS CHECKS GOOD.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 44,529 hrs · 23,412 cycles

DENT ON UPPER DOUBLER ABOVE MID CARGO DOOR 4.5 INCHES ABOVE DOOR CUTOUT. FORWARD CORNER 1.5 INCHES X 0.7 INCHES X 0.030 DEPTH. MAINTENANCE C/W ERA 499992-14 REVISION ORIGINAL. PERMANENT REPAIR WILL NEED TO BE ACCOMPLISHED WITHIN 30 DAYS FROM 02/03/12.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,191 hrs · 22,773 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE AT SEAT 1. MAINTENANCE REMOVED AND REPLACE POWER SUPPLY B5-236. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE. (2011-D0953)

Part: GLOWSTRIP — MISSING (CABIN) · airframe 43,191 hrs · 22,773 cycles

DURING LINE CHECK, MAINTENANCE FOUND 7 INCHES OF PHOTOLUMINESCENT EMERGENCY PATHWAY LIGHT MISSING AT ROW 26E. MAINTENANCE FORWARD TO MCO AND PLACARD. MAINTENANCE REPLACED MISSING SECTION OF PHOTO LUMINESCENT STRIP AT 26E. OPERATION CHECKS GOOD. MCO/PLAC REMOVED. AIRCRAFT OK FOR SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,983 hrs · 22,225 cycles

TAIL INTERIOR STRINGER 2L AT STA 1475 (AFT) HAS CRACK IN STRINGER. REPAIRED PER ER/A 490622-14 REV 0 & 01 STEPS 1-9. INSTALLED NEW STRINGER & SPLICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,983 hrs · 22,225 cycles

TAIL INTERIOR STRINGER 2L AT STA 1475 (AFT) HAS CRACK IN STRINGER. ACCOMPLISHED ER/A 490622-14 REV 0 & 01 STEPS 1-9.

Part: CUSP WEB — DENTED (BS 252) · airframe 49,277 hrs · 26,074 cycles

DENT IN CUSP WEB BS 252.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,655 hrs · 22,085 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 1DC, 16CDE AND FWD OF ROW 10CDE WERE INOPERATIVE. MX REPLACED THE LIGHT LENS ASSEMBLIES AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: BULB — MISSING (EMERGENCY LIGHTS) · airframe 40,085 hrs · 21,387 cycles

CREW WROTE UP NUMEROUS EMERGENCY LIGHTS WERE INOPERATIVE THRU OUT CABIN MISSING COVERS AND MISSING BULBS. MSP MX TAPED ROW 3, 4, AND 38. LIGHT INOPERATIVE AT ROW 2 AND FOWARD TO MCO/PLACARDED. BOS MX REPLACED ALL MISSING BULBS AND LENS COVERS. NOW LIGHT AT 2C INOPERATIVE DUE TOO BROKEN LIGHT HARNESS. PART NOT IN STOCK. MCO STILL ON BOARD REF IPC 33-51-00-61 ITEM 65. AWAITING DPN 332210024.

Part: LIGHT — DAMAGED (SEAT 32C) · airframe 39,496 hrs · 21,064 cycles

DAMAGED SECTION OF EMERGENCY TRACK LIGHTING AT SEAT 32C.

Part: LIGHT — DAMAGED (SEAT 3C) · airframe 39,496 hrs · 21,064 cycles

EMERGENCY TRACK LIGHT LENS AND LIGHT DAMAGED AT SEAT 3C. REPAIRED AS REQD.

Part: FRAME — DENTED (FS 148 L6-8R) · airframe 38,849 hrs · 20,702 cycles

ACFT ENCOUNTERED A BIRD STRIKE ON THE FUSELAGE JUST ABOVE THE F/O EYEBROW WINDOW AT THE FS 148 FRAME BETWEEN L-6R AND L-8R. THE SKIN WAS REPAIRED ON ERA 478136-14 AND THE FRAME HAS BEEN REPAIRED ON ERA 478189-14.

Part: SKIN — DENTED (FS 229 S18L) · airframe 37,606 hrs · 19,958 cycles

ACCOMPLISHED PERMANENT REPAIR PER ERA 469965-14 REV C LOCATED FWD OF FS 229 ABOVE S-18L. INSTALLED STRAPS TO EXISTING SKIN REPAIRS TO COMBINE WITH ADJACENT REPAIR INSTALLED BY ERA 466737-14.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 36,028 hrs · 19,007 cycles

BURNING ODOR AFT CABIN NEAR ROW 39 CDE. FOUND 2 EA SIDEWALL LIGHTS INOP AND INOP BALLAST BAD AFT OF O/H BAG BIB 39 CDE. REPLACED BALLEST AND LIGHTS OPS GOOD.

Part: SKIN — DENTED (BS 237 L17-18L) · airframe 34,692 hrs · 18,237 cycles

FUSELAGE SKIN AND FORMER DENTED AT STA 237 BETWEEN L17L AND L18L DAMAGE CUTOUT. AREA INSPECTED, FORMER REPLACED AND SKIN REPLACED.

Part: MONITOR — INOPERATIVE (PASSENGER CABIN) · airframe 34,557 hrs · 18,162 cycles

VIDEO MONITOR AT 22F EMITTED SMOKE DURING VIDEO OPERATION. SYSTEM WAS TURNED OFF AND SMOKE DISSIPATED. REMOVED AND REPLACED VIDEO MONITOR AT SEAT 22A PER AMM. CHECKS REMOVED MCO/PLAC.

Part: SKIN — PUNCTURED (BS 210) · airframe 34,197 hrs · 17,947 cycles

HOLE PUNCTURED IN FUSELAGE SIDE BELOW L-1 DOOR AIRSTAIR CUT OUT STA 210. REPAIRED FUSELAGE SKIN IAW DELTA ERA 464537-14 REV ORG DATE NOV 20 2007 ON N/R 1000-0009 AT HMV-2 IN OKC.

Part: DOOR FRAME — CORRODED (BS 1211-1268) · airframe 34,197 hrs · 17,947 cycles

AFT CARGO COMPT LOWER JAMB OUTER SURFACE HAS CORROSION STA 1211 TO 1268. REPAIRED AFT CARGO DOOR CUTOUT LOWER JAMB IAW MD-80 53-05D FIG 63 ON N/R 1000-0074, AT HMV-2 IN OKC.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 34,197 hrs · 17,947 cycles

RIGHT WING NR 2 SLAT DENTED LEADING EDGE NEAR CENTER. REPAIRED RT WING NR 2 SLAT L/E IAW MD-90 SRM 57-20-05D FIG 4 VOL 1, ON N/R 6600-0002 AT HMV-2 IN OKC.

Part: SHEAR TIE — CORRODED (FS 1288 S29L/R) · airframe 34,197 hrs · 17,947 cycles

AFT SHEAR TIE CORRODED AT FS 1288 LONGERON 29L TO 29R. REPAIRED AFT PIT SHEAR TIE AT STA 1288 BETWEEN LONGERON 29L TO LONGERON 29R IAW MD-90 SRM 53-10-02D ON N/R 1600-0178 AT HMV-2 IN OKC.

Part: VANE — GOUGED (TE FLAP) · airframe 34,197 hrs · 17,947 cycles

LEFT WING O/B FLAP O/B VANE GOUGED TOP SIDE ABOVE I/B ATTACH POINT. REPAIRED LEFT O/B FLAP VANE IAW MD-90 SRM 51-10-02D PG 84 ON N/R 5400-0052 AT HMV-2 IN OKC.

Part: SHEAR TIE — CORRODED (FS 1344 26L-28R) · airframe 34,197 hrs · 17,947 cycles

AFT PIT SHEAR TIE CORRODED AT FS 1344 BETWEEN LONGERONS 27R-29L. REPAIRED AFT PIT SHEAR TIE AT STA 1344 BETWEEN LG 26L AND 28R IAW MD-90 SRM 53-10-02D FIG 3 ON N/R 1600-0204 AT HMV-2 IN OKC.

Part: VANE — CHAFED (T/E FLAP) · airframe 34,197 hrs · 17,947 cycles

LEFT WING OUTBOARD FLAP MID VANE CHAFED APPROX 18 INCHES FROM NR 3 FLAP FAIRING. REPAIRED DAMAGED AREA OF THE LEFT WING O/B FLAP MID VANE IAW MD-90 SRM 51-10-02D PG 18B. INDENTIFIED PER DELTA PS 900-5-1 NR 4 ON N/R 5400-0002 AT HMV-2 IN OKC.

Part: VANE — DENTED (LT TE FLAP) · airframe 34,197 hrs · 17,947 cycles

LT O/B FLAP I/B VANE DENTED ON TOP O/B END. INSTALLED BONDED REPAIR DOUBLER IAW MD-90 SRM 51-10-02D PARA 17 P84 ON N/R 5400-0077 AT HMV-2 IN OKC.

Part: VANE — GOUGED (TE FLAP) · airframe 34,197 hrs · 17,947 cycles

LT O/B FLAP VANE GOUGED ON TOP SIDE I/B END. INSTALLED HOT BOND REPAIR DOUBLER IAW MD-90 SRM 51-10-02D PARA 17 PG 83 ON N/R 5400-0076 AT HMV-2 IN OKC.

Part: VANE — DENTED (TE FLAPS) · airframe 34,197 hrs · 17,947 cycles

LT WING O/B FLAP I/B VANE WAS A DENT IN L/E BETWEEN NR 2 AND NR 3 SUPPORTS. INSTALLED METAL BOND REPAIR DOUBLER IAW MD-90 SRM 51-10-02D PARA 17 PAGE 84 ON N/R 5400-0003 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 455-520 RBL 54. REPAIRED DAMAGED SEAT TRACK FROM FS 332-864 RBL 54 IAW MD-90 SRM 53-40-01 FIG 6 ON N/R 2700-0199 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,197 hrs · 17,947 cycles

RT CUSP WEB CORRODED OUT OG LIMITS- FS 693-769. REMOVED AND REPLACED WEB IAW MD-88 SRM 5305D FIG 828D ON N/R 2400-0232 AT HMV-2 IN OKC.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,197 hrs · 17,947 cycles

AFT PIT FRAME AT STA 1363 CORRODED ON AFT SIDE LONGERON 28L-28R. REPAIRED FRAME IAW MD-90 SRM 53-10-02 FIG 2 ON N/R 1600-0201 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (FS 543) · airframe 34,197 hrs · 17,947 cycles

RT CUSP WEB CORRODED OUT OF LIMITS FS 543. REPAIRED RT CUSP WEB FS 503-597 IAW MD-88 SRM 53-05D ON N/R 2400-0233 AT HMV-2 IN OKC.

Part: CUSP WEB — CRACKED (FS 342) · airframe 34,197 hrs · 17,947 cycles

RT CUSP WEB AT FS 342 CRACKED AT LIGHTNING HOLE. REPAIRED RT CUSP FS 342 AT LIGHTNING HOLE IAW MD80 SRMD FIG 827D ON N/R 2700-0282 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 826) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 826 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I FIG 6 ON N/R 2700-0205 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 598-700) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 598-700 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL I ON N/R 2700-0204 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 1140-1160) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 1140-1160 RBL 54. REMOVED AND REPLACED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I FIG 6 ON N/R 2700-0202 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 455-530) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 455-530 LBL 24. REPAIR SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL II ON N/R 2700-0209 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 237) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 237 RBL 24. REPAIRED CABIN SEAT TRACK IAW MD-90 SRM 53-40-01 FIG B VOL I ON N/R 2700-0207 AT HMV-2 IN OKC.

Part: SKIN — GOUGED (NR 3 SLAT) · airframe 34,197 hrs · 17,947 cycles

RT WING SKIN GOUGED 20 INCHES I/B OF NUMBER 3 SLAT TRK. REPAIRED RT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1 ON N/R 6200-0040 AT HMV-2 IN OKC.

Part: SKIN — DENTED (BS 229 L17L) · airframe 34,197 hrs · 17,947 cycles

LEFT FUSELAGE SKIN AT STATION 229 AND LONG 17 LT IS A DENT. CUT OUT DAMAGE AND REPAIRED IAW MD-80 SRM 53-04D FIG 12 B SH 35 ON N/R 2000-0068 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (BS 705 LBL 24) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 705 LBL 24. REMOVED AND REPLACED SEAT TRACK FS 705 LBL 24 PER SRM 53-40-01 VOL II ON N/R 2700-0210 AT HMV-2 IN OKC.

Part: SKIN — GOUGED (LT WING) · airframe 34,197 hrs · 17,947 cycles

LT WING FIXED L/E JUST O/B OF SLAT-TRACK NR 4 SKIN IS GOUGED. REPAIRED L/E WING IAW SRM 57-20-01 FIG II VOL II ON N/R 5200-0045 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,197 hrs · 17,947 cycles

LT SEAT TRACK CORRODED 1255-1364 LBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I ON N/R 2000-0238 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 870) · airframe 34,197 hrs · 17,947 cycles

LT CUSP AT FS 870 CORRODED OUT OF LIMITS. REPAIRED LT CUSP WEB IAW MD-80 ERA 53-05D FIG 827D ON N/R 2400-0241 AT HMV-2 IN OKC.

Part: DOUBLER — CORRODED (CARGO BAY) · airframe 34,197 hrs · 17,947 cycles

MID CARGO LOWER JAMB DOUBLER PLATE HAS CORROSION FROM FWD END TO AFT END REF TASK 53-12-02-02. REPAIRED LOWER DOOR JAMB DOUBLER IAW MD-90 53-05D FIG 63 ON N/R 1000-0043 ON HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 485-579) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 485-579 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL I ON N/R 2700-0208 AT HMV-2 IN OKC.

Part: SEAT TRACK — CORRODED (FS 1212-1364) · airframe 34,197 hrs · 17,947 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 1212-1364 RBL 24. REMOVED AND REPLACED SEAT TRACK IAW MD-90 SRM 53-40-01 AND 51-30-02 ON N/R 2700-0206 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 924-962) · airframe 34,197 hrs · 17,947 cycles

RT CUSP WEB CORRORED OUT OF LIMITS FS 924-962 RBL 54. REPAIRED RT CUSP WEB IAW ERA 398191-14MA REV ORG 9-18-02 ON N/R 2400-0234 AT HMV-2 IN OKC.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 34,197 hrs · 17,947 cycles

VERTICAL STABILIZER ANGLE IS CRACKED ON RT SIDE BELOW INLET SCOOP. REMOVE AND REPLACE ANGLE IAW MD-90 SRM 51-30-05 ON N/R 3000-0048 AT HMV-2 IN OKC.

Part: MEMBRANE — CORRODED (FS 195-200) · airframe 34,197 hrs · 17,947 cycles

FWD CABIN SUBFLOOR MEMBRANE CORRODED AT FS 195-200 RBL 54. REPAIRED WEB IAW MD-90 SRM 51-11-01 ON N/R 2400--0283 AT HMV-2 IN OKC.

Part: INTERCOSTAL — CORRODED (FS 1326 L30) · airframe 34,197 hrs · 17,947 cycles

AFT CARGO FS 1326 L-30 INTERCOSTAL TIE CLIP CORRODED ON LOWER SURFACE. FABRICATED NEW PART IAW MD-90 SRM 51-10-05 VOL II ON N/R 1600-0248 AT HMV-2 IN OKC.

Part: PRESSURE SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 29,789 hrs · 15,451 cycles

AIRCRAFT RETURNED TO CVG BECAUSE THE AIRCRAFT FAILED TO PRESSURIZE. FLOW LIGHT AND NO MODE LIGHT ILLUMINATED WITH CR POWER SELECTED. OUTFLOW VALVE DROVE FULL CLOSED AND NO AIR FLOW FROM PACKS. REPLACED NUMBER 1 ENGINE AUTO PRESS DIFF SWITCH. CHECKS OK.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 29,083 hrs · 15,057 cycles

ON APPROACH LOST ALL RIGHT SIDE HYDRAULIC QUANTITY. REPLACED LEAKING RT ENGINE PUMP PRESSURE LINE.

Part: STARTER — INOPERATIVE (APU) · airframe 27,389 hrs · 14,180 cycles

APU WOULD NOT START. REPLACED APU STARTER AND START CONTROL RELAY. REPLACED WIRE AT B1-1058 PIN 5A.

Part: STRUT — DISCHARGED (NLG) · airframe 27,001 hrs · 13,978 cycles

ON LANDING GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ON. ACCOMPLISHED ABNORMAL CHECKLIST. RECYCLED LANDING GEAR AND NOSE GEAR LIGHT REMAINED ON, BUT WITH THE ADDITION OF LOUD AIR NOISE. LOWERED LANDING GEAR AND RETURNED TO DFW. CHECKED NOSE GEAR. SERVICED NOSE STRUT PER M/M 32-21-01-619-801. JACKED NOSE GEAR CYCLED NOSE GEAR ALL INDICIATIONS NORMAL.

Part: TERMINAL — BURNED (APU) · airframe 26,043 hrs · 13,534 cycles

AFTER PUSHBACK STRONG SMELL OF ELECTRICAL FIRE, NO VISIBLE SMOKE. RAN ELECTRICAL FIRE CKLIST, STRONG SMELL NEAR F/C FLIGHT ATTENDANT JUMPSEAT. FOUND APU POWER RELAY PHASE A1 TERMINALS BURNT. REPLACED RELAY BASE AND CONTROL. FWD TO MCO/PLAC 49-10-01. APU INOP DUE TO TERMINALS BURNT.

Part: STARTER — BURNED (APU) · airframe 26,023 hrs · 13,526 cycles

FIVE MINUTES AFTER FAILED START ATTEMPT SMOKE COMING FROM APU AREA. SMALL FIRE AT APU STARTER EXTINGUISHED WITH DRY CHEM EXT. APU REPLACEMENT IN PROGRESS. REPLACED APU ASSY AND APU START RELAY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,000 hrs · 13,025 cycles

FIVE EMERGENCY TRACK LIGHTS AT SEAT 10 ABC INOPERATIVE. RELAMPED, CHECKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,000 hrs · 13,025 cycles

THE L1 DOOR EMERGENCY FLASHLIGHT OUTBOARD RED POWER LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY, OPS NORMAL NOW.

Part: EXTINGUISHER — LEAKING (CABIN) · airframe 24,046 hrs · 12,592 cycles

FD POSITION H2O PORTABLE FIRE EXTINGUISHER LEAKING FLUID. DAL LEAD SEAL INTACT WITH NO EVIDENCE OF ACTIVATION OR TAMPERING. CARTRIDGE CKS OK. REPLACED SAME.

Part: ACM — SEIZED (A/C BAY) · airframe 23,865 hrs · 12,497 cycles

AFTER T/O SMOKE REPORTED IN AFT CABIN. FOUND RT ACM FROZEN. REPLACED ACM AND COALESCER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,485 hrs · 8,716 cycles

THE CANTED STATION 1520 BULKHEAD WAS FOUND WITH TWO 2 INCH CRACKS AT THE 1:00 O CLOCK POSITION (LOOKING AFT). THE CRACKS ARE NEAR THE JOGGLE LINE FOR THE FACTORY WEB SPLICE. THE DAMAGED SECTION OF WEB WAS TRIMMED OFF AND AN ALUMINUM DOUBLER AND TRIPLER INSTALLED TO REPLACE THE REMOVED AREA AND REPLACED THE JOGGLED SPLICE. THE REPAIR WAS ACCOMPLISHED PER ER/A 379779-14, REV A.

Part: TIRE — FAILED (NR 2) · airframe 16,410 hrs · 8,678 cycles

AIRCRAFT TOUCHDOWN OCCURRED EARLY AND IMPACTED APPROACH LIGHTS - DAMAGE OCCURRED TO NR 2 ENGINE, LT SPRAY DEFLECTOR, AND NR 2 TIRE - REPLACED TIRE, REPAIRED DAMAGE, REPLACED DEFLECTOR - WEATHER WAS A FACTOR

Part: LINK — FAILED (NOSE GEAR) · airframe 14,663 hrs · 7,744 cycles

CLIMBING THROUGH 10,000 FT AND 265 KNOTS, A LOUD AIR NOISE IN THE COCKPIT APPEARED TO BE COMING FROM THE PILOTS LOWER FOOT AREA. POSSIBLE GEAR DOOR PROBLEM. REPLACED RT NOSE GEAR LINK (BUNGEE). CLEANED FWD E & E DOOR SEAL AND SECURED INSULATION AFT RT OF NOSE GEAR ACCESS AREA. SECURED LEADING EDGE PANEL ON RAM AIR DOOR. SWUNG GEAR, OPS NORMAL.

Part: FILTER — DIRTY (RT ENGINE)

RIGHT GEN OIL FILTER MSG ILLUMINATED ON T/O ROLL. T/O WAS DISCONTINUED. FWD VSCF TO MAO AND PLACARD. VSCF GEN FILTER CHECKED PER MEL 24-12-02A ONCE EA FLT DAY.

Part: POWER SUPPLY — INOP (R1 DOOR)

R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.

Part: FLASHLIGHT — INOP (CABIN)

ONE OF TWO EMERGENCY FLASHLIGHT AT FORWARD F/A STATION NOT BLINKING. REPLACED FLASHLIGHT ASSY AND BATTERY.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

AFTER TAKEOFF, RIGHT ENGINE FIRE LIGHT FLICKERS. ON SHORT, FINAL FIRE WARNING 4 TIMES UNTIL LANDING. REPLACED ELEMENT.

Part: BULB — FAILED (CABIN)

LEFT OVERWING EMERGENCY EVACUATION LIGHT FAILED TO TEST ON LAYOVER CHECK. RELAMPED, TESTS GOOD.

Part: TIRE — FAILED (NR 3 MAIN)

NR 3 MAIN TIRE LOST TREAD DURING T/O ROLL, LEFT GEAR EXTENDED. RETURNED FOR UNEVENTFUL LANDING. RECAP SEPARATED FROM TIRE CAUSING EXTENSIVE DAMAGE TO RT I/B FLAP AND NR 2 ENGINE.

Part: SKIN — DENTED (FS 261-286)

THE FUSELAGE SKIN WAS SEVERELY DENTED BETWEEN FS 261 AND FS 286 AND BETWEEN LONGERONS 25R AND 27R. THE FRAME FORMER SKIN ATTACH ANGLES AT FS 275. ALSO, ABOVE AND BELOW LONGERON 26R ARE BROKEN. REPAIRED GROUND DAMGE PER DL ERA 273532-14.

Part: ACCESS PANEL — MISSING (NR 2 ENGINE)

POST-FLIGHT, NR 2 ENGINE LATCH ACCESS PANEL FOUND MISSING. REPLACED NR 2 ENGINE ACCESS PANEL. FERRY FLT TO DFW FOR REPAIRS.