N901DA

Part: COVER — BROKEN (EXIT SIGN) · airframe 60,525 hrs · 34,060 cycles

EMERGENCY EXIT SIGN ROW 26 BROKEN. INSTALLED NEW LIGHT COVER.

Part: POWER SUPPLY — FAILED (SEAT 10E) · airframe 59,222 hrs · 33,312 cycles

DURING CRUISE, FL310, FLIGHT ATTENDANTS AND PASSENGERS IN MID CABIN NOTICED A BURNING ELECTRICAL ODOR. FIRST OFFICER NOTED A RISE IN CABIN TEMP. SUPPLY BETWEEN 90 AND 120 DEGREES APPROXIMATELY 10 MINUTES BEFORE FLIGHT ATTENDANTS CALLED. MAINTENANCE TROUBLESHOT AND FOUND IN SEAT POWER SUPPLY UNIT INOPERATIVE AT SEAT 10E AS POSSIBLE ODOR SOURCE. REPLACED. OPS CHECKED GOOD. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. NO ODOR NOTED.

Part: RELEASE MECH — OUT OF ADJUST (TAILCONE) · airframe 58,673 hrs · 33,034 cycles

TAIL CONE FAILED INTERNAL RELEASE MECHANISM TEST. ADJUSTED TAIL CONE JETTISON. PULL WAS WITHIN LIMITS.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 58,644 hrs · 33,020 cycles

VERTICAL STABILIZER LEADING EDGE IS DAMAGED BEYOND REPAIR LIMITS. COMPLIED WITH ERA 556744-14, REV O.

Part: FRAME — CRACKED (BS 1542) · airframe 58,644 hrs · 33,020 cycles

CANTED FRAME HAS A CRACK AT BS 1542. COMPLIED WITH ERA 556775-14, REV O.

Part: FRAME SPLICE — DAMAGED (BS 1395 BULKHEAD) · airframe 58,644 hrs · 33,020 cycles

BS 1395 AFT PRESSURE BULKHEAD TEE SPLICE BETWEEN LONGERONS 26 AND 27L DAMAGED. REPAIRED THE BULKHEAD FRAME SPLICE IAW PRI/ERA 556133-14, REV O.

Part: TEE FITTING — DAMAGED (BS 1395) · airframe 58,644 hrs · 33,020 cycles

AFT PRESSURE BULKHEAD TEE SPLICE BS 1395 BETWEEN LONGERONS 26 AND 27R DAMAGED. REPAIRED IAW PRI/ERA 556133-14, REV O.

Part: FRAME — CRACKED (BS 1542) · airframe 58,644 hrs · 33,020 cycles

CRACK ON CANTED FRAME, BS 1542. COMPLIED WITH PRI/ERA 556789-14, REV O.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 58,644 hrs · 33,020 cycles

VERTICAL STABILIZER LEFT LEADING EDGE FRONT SPAR CAP FORWARD FLANGE HAS DAMAGED FASTENER HOLES . REPAIRED.

Part: PIN — WORN (EMERGENCY EXIT) · airframe 58,644 hrs · 33,020 cycles

TAIL INTERIOR EMERGENCY EXIT PULL TEE PIN IS WORN AT BS 1554. REPLACED IAW MM.

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,515 hrs · 32,956 cycles

AFT RIGHT OVER WING EMERGENCY EXIT SIGN INOPERATIVE. FOUND GROUND TERMINAL BROKEN AT GROUND 5232. RETERMINATED WIRE. OPERATION CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,262 hrs · 32,819 cycles

TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: DUCT — DAMAGED (CARGO HEATER) · airframe 58,004 hrs · 32,684 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR. CIRCUIT BREAKER 1-12 AND 1-13, CARGO HEATER TRIPPED. ODOR DISSIPATED. FOUND ELEMENTS SHORTED ON THE HEATER DUCT. REMOVED AND REPLACED CARGO HEATER DUCT ASSEMBLY PER MM. OPERATION CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,652 hrs · 32,456 cycles

EMERGENCY EXIT SIGH INOPERATIVE ABOVE DOOR L2 DOOR. REMOVED AND REPLACED BATTERY PACK. OPERATION CHECKED GOOD.

Part: SKIN — DAMAGED (BS 1174) · airframe 55,785 hrs · 31,320 cycles

SEVERAL HOLES DAMAGED AT FS 1174, LONGERON 30L AND 29L. COMPLIED WITH PRI/ERA 543071-14, REV C.

Part: SUPPORT CHANNEL — CRACKED (VERTICAL STAB) · airframe 54,337 hrs · 30,436 cycles

VENTRAL STABILIZER ACTUATOR SUPPORT CHANNEL CRACKED. REPAIRED IAW PRI ERA 537315-14.

Part: LINE — DISCONNECTED (MLG BRAKE) · airframe 53,700 hrs · 30,068 cycles

REPORTED NR 4 BRAKE FIRE DURING TAXI AFTER LANDING. NR 4 BRAKE OVERHEATED TO APPROXIMATELY 700C. ACFT WAS STOPPED AND TOWED INTO GATE. MAINTENANCE FOUND THE NR 4 BRAKE FORWARD QD DISCONNECTED FROM THE BRAKE ASSY. FORWARD TO MCO/PLACARD INSTALLED. MAINTENANCE R & R THE NR 4 BRAKE AND TIRE ASSEMBLIES, AS WELL AS, THE NR 4 BRAKE QUICK DISCONNECT. ACFT WAS RETURNED TO SERVICE. LP 6538942.

Part: SKIN — CRACKED (BS 1475) · airframe 53,519 hrs · 29,957 cycles

FUSELAGE SKIN CRACKED AT STA 1475, INBD OF L1R . CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR IAW SRM 53-30-01, FIG 16.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,504 hrs · 29,947 cycles

LEFT HORIZONTAL CENTER SKIN HAS LFEC INDICATION. COMPLY WITH PRI 533591-14AD, REV 1. REPAIR IAW ERA 533591-14AD, REV O.

Part: LANYARD — FRAYED (GIRT BAR) · airframe 53,427 hrs · 29,903 cycles

FORWARD ENTRY DOOR GIRT BAR LANYARD FRAYED. R & R LANYARD IAW AMM 25-61.

Part: UNKNOWN — SMOKE (CABIN) · airframe 53,361 hrs · 29,860 cycles

HAZE AND SMOKE APPEARED DURING LANDING IN THE CABIN. ODOR WAS MUSTY AND NOTHING APPEARED TO BE BURNING. HAZE DISAPPEARED IN LESS THAN 5 MINUTES. APU WAS NOT RUNNING WHEN HAZE APPEARED. INSPECTED AND TROUBLESHOT PNEUMATIC SYSTEM. R & R RT TI SENSOR IAW MM. ACFT IS OK FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 52,884 hrs · 29,578 cycles

AT 30000 FEET, CRANKED APU AND ELECTRICAL BACKUP, F/A CALLED AND REPORTED ODOR IN CABIN. SHUTDOWN APU IMMEDIATELY. ODOR DISSAPATED. MAINTENANCE TROUBLESHOT AND FOUND APU OIL OVERSERVICED.. REMOVED .5 QUART OF OIL FROM APU AND CLEANED COMPARTMENT. RAN APU AND ENGINE. NO ODORS. PERFORMED DUCT BURNOUT AND REPLACED LT/RT COALESCER BAGS. AIRCRAFT CHECKS OK.

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 52,792 hrs · 29,514 cycles

EMERGENCY LIGHT IN TAIL INTERIOR SOCKET BROKEN, LOOSE AND LENSE MISSING ABOVE CATWALK. R & R AND CHECKED EMERGENCY LIGHT ASSEMBLY IAW AMM. CHECKS GOOD.

Part: STRUCTURE — DENTED (L1 DOOR) · airframe 50,639 hrs · 28,116 cycles

SMALL DENT ON BOTTOM OF L1 DOOR AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-01-01. AIRCRAFT OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 50,072 hrs · 27,748 cycles

DURING SERVICE CHECK, FOUND TWO EMERGENCY LIGHTS AT ROW 5-7 INOPERATIVE. MAINTENANCE FOUND LOOSE WIRE SPLICE FOR CEILING EMERGENCY LIGHTING. WIRE TERMINAL RESEATED. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (DIMMER SWITCH) · airframe 49,317 hrs · 27,281 cycles

F/A REPORTS STRONG ELECTRICAL BURNING ODOR IN AFT OF ACFT. RETURN TO BLOCKS. MX FOUND SIDEWALL LIGHT DIMMER SWITCH WITH BROKEN TERMINAL AND WIRE. MX SECURED BROKEN WIRE TO SWITCH AT AFT F/A PANEL IAW AMM. CHECKED OK.

Part: STRUCTURE — DENTED (L1 DOOR) · airframe 49,221 hrs · 27,225 cycles

LOWER EDGE OF L1 DOOR DENTED. RESHAPED LOWER EDGE OF L1 DOOR IAW SRM 52-01-01. OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 49,170 hrs · 27,198 cycles

RT OVERWING EMERGENCY PATHWAY LIGHT, AFT DOOR LIGHT MISSING. INSTALLED EMERGENCY EXIT SIGN AND LIGHT ASSY. OPS CHECKS GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,037 hrs · 27,123 cycles

EMERGENCY FLOOR PATHWAY LIGHTS WAS DAMAGED/INOPERATIVE. MX REINSTALLED STALLED. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,037 hrs · 27,123 cycles

EMERGENCY FLOOR PATHWAY LIGHTS DAMAGED/INOPERATIVE. MX REINSTALLED LIGHT. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 1364) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BILGE, BS 1364, LONGERON 26R - 26L, FRAME IS CORRODED IN SEVERAL PLACES. TASK 53-302-07. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. REPLACED L29R FRAME IAW SRM 53-10-02 FIG 2.

Part: LONGERON SPLICE — CORRODED (BS 1348-1359) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BILGE, BS 1348 - 1359, LONGERON 30, SPLICE IS CORRODED SEVERAL PLACES. TASK 53-302-07. REMOVED OLD SPLICE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 51-30-05, PG 5 AND 51-10-02.

Part: WEB — CORRODED (BS 1271) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT STA 1271, RBL14-16 WEB HAS CORROSION AROUND NUTPLATE TASK 53-302-07. R & R WEB IAW SRM 51-30-05 AND 51-30-02.

Part: FRAME — CORRODED (BS 1379 L27R) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BS 1379, LONGERON 27R FRAME HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-10-02, SRM 51-10-03.

Part: LONGERON — CORRODED (BS 1359) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BILGE, STA 1359, LONGERON 29R IS CORRODED AT AFT END OF SPLICE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. WORK COMPLETED ON WO 26896-1600-0028, CARD 1757038.

Part: LONGERON SPLICE — CORRODED (BS 1348-1359) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BILGE, STA 1348-1359, LONGERON 29R SPLICE CORRODED IN SEVERAL PLACES. 100 PERCENT MATERIAL LOSS. OUT OF LIMITS. WORK COMPLETED ON WO 26896-1600-0029.

Part: STRUCTURE — DAMAGED (L1 DOORWAY) · airframe 49,026 hrs · 27,116 cycles

FORWARD CABIN ENTRYWAY FLOOR, JUST INBD OF L1 DOOR CUTOUT, PREVIOUS WEB REPAIR HAS 3EA MISDRILLED HOLES JUST UNDER FLOOR PANEL SUPPORT ANGLE, STATION 170-180. R & R DAMAGED WEB AND REPAIRED MISDRILLED HOLES IAW ER/A 513584, REV O.

Part: STOP FITTING — CRACKED (FWD CARGO DOOR) · airframe 49,026 hrs · 27,116 cycles

FORWARD CARGO DOOR FORWARD STOP PAD FITTING, 4TH FROM TOP, CRACKED. R & R IAW DWG 5910141 AND SRM 51-10-05.

Part: SHEAR TIE — CORRODED (BS 1379) · airframe 49,026 hrs · 27,116 cycles

SHEAR TIE CORRODED, AFT CARGO BAY BS 1379 L26 - 27L. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED IAW SRM 53-10-03 AND 51-30-00 VOL II.

Part: SHEAR TIE — CORRODED (BS 1269) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO SHEAR TIE BS 1269 L28-29R CORRODED ON FWD SIDE. R & R SHEAR TIE IAW SRM 51-30-05 AND DWG 9936073.

Part: LONGERON SPLICE — CORRODED (BS 1359) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO COMPARTMENT BILGE, BS 1359, LONGERNON 28L IS CORRODED IN AFT END OF SPLICE. REMOVED CORROSION. LONGERON 28L, WITHIN LIMITS. SPLICE FOUND TO BE OUT OF LIMITS. R & R SPLICE IAW SRM 51-30-05, PAGE 1.

Part: STOP FITTING — CRACKED (FWD CARGO DOOR) · airframe 49,026 hrs · 27,116 cycles

FORWARD CARGO DOOR, AFT STOP PAD FITTING, 3RD FROM TOP CRACKED. R & R DOOR STOP FITTING IAW DWG 5910141 AND SRM 51-10-05.

Part: CARGO TRACK — CORRODED (BS 1307-2169) · airframe 49,026 hrs · 27,116 cycles

CARGO TRACK FROM FS 1307 AND FS 2169 LONGERON 27R HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED AND INSTALLED CARGO TRACK IAW SRM 53-40-01 AND 51-10-03, AND 51-30-03.

Part: FRAME — CORRODED (VERTICAL STAB) · airframe 49,026 hrs · 27,116 cycles

VERTICAL STABLILIZER UPPER FORWARD FRAME HAS CORROSION. R & R FWD FRAME IAW DWG 5957208 AND SRM 51-10-05 VOLII, PG 1.

Part: SEAT TRACK — DAMAGED (BS 766) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK BS 766, RBL 54 HAS ENLARGED ATTACH NODE. R & R SEAT TRACK BS 766-815 IAW SRM 53-40-01, FIG 6.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,026 hrs · 27,116 cycles

FORWARD CARGO DOOR, FORWARD STOP PAD FITTING CRACKED. R & R STOP PAD FITTING IAW DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,026 hrs · 27,116 cycles

FORWARD CARGO DOOR, FORWARD STOP PAD FITTING CRACKED. R & R IAW DWG 591014.

Part: SEAT TRACK — DAMAGED (BS 1020-1041) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK GOUGED AND CORRODED RBL 54.5, BS 1020 -1041. FOUND TO BE OUT OF LIMITS. REMOVED AND REPAIRED SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01, PG 1.

Part: SEAT TRACK — CORRODED (BS 1146-1366) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK, RBL 54, BS 1146 TO 1366 HAS SEVERAL AREAS OF CORROSION. FOUND OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-40-01 PG 36.

Part: CUSP WEB — CRACKED (BS 1352) · airframe 49,026 hrs · 27,116 cycles

BS 1352 CUSP WEB IS CRACKED. REPAIRED IAW SRM 53-20-02, FIG.

Part: SEAT TRACK — CORRODED (BS 579-595) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK RBL 54, BS 579 - 595 IS CORRODED IN MIDDLE GROVE UPPER SURFACE. BLENDED DAMAGE. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, VOL I, PG 32, FIG 6.

Part: SEAT TRACK — WORN (BS 280-282) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK, RBL 54, BS 280 TO BS 282 IS WORN. R & R SEAT TRACK IAW SRM 53-40-01, VOL I, PAGE 29-38.

Part: SEAT TRACK — WORN (BS 455-458) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK, RBL 54, BS 455 - 458 HAS WEAR ON UPPER AND MIDDLE SURFACE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01.

Part: CARGO TRACK — CORRODED (BS 1176-1307) · airframe 49,026 hrs · 27,116 cycles

AFT CARGO TRACK FROM FS 1307 - 1176 BETWEEN LONGERONS 28L AND 27L HAS MULTIPLE AREAS OF CORROSION. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR IAW DWG 5965794 AND SRM 53-40-01, PG 40.

Part: ANGLE — CORRODED (BS 1269) · airframe 49,026 hrs · 27,116 cycles

CORROSION, UNDER AFT CARGO DOOR SILL WEB, ON ANGLE ATTACHED TO FS 1269 AND LONGERON 28R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW ANGLE IAW SRM 51-30-05, PG 1.

Part: SEAT TRACK — CORRODED (BS 218-256) · airframe 49,026 hrs · 27,116 cycles

RT BS 218 - 256 RBL 45 SEAT TRACK CORRODED. R & R SEAT TRACK IAW SRM 53-40-01 FIG 6, PG 30.

Part: FLOOR SUPPORT — CORRODED · airframe 49,026 hrs · 27,116 cycles

BS 180-200 FLOOR SUPPORT CORRODED ON UPPER SURFACE TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-02 AND 51-30-05.

Part: FLOORBEAM — DAMAGED (BS 1364) · airframe 49,026 hrs · 27,116 cycles

RT SIDE BS 1364, RBL 20, FLOORBEAM TEE CAP CORRODED ON UPPER SURFACE. REPAIRED DAMAGE FLOORBEAM IAW SRM 53-20-01, FIG 3 AND 51-70-01, FIG 2.

Part: SEAT TRACK — CORRODED (BS 1136-1193) · airframe 49,026 hrs · 27,116 cycles

LEFT BS 1136-1193 LBL 55 SEAT TRACK CORRODED ON UPPER SURFACE. SEAT TRACK FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-01, PG 36.

Part: FLOORBEAM — CORRODED (BS 1364) · airframe 49,026 hrs · 27,116 cycles

BS 1364 LBL 20 FLOORBEAM TEE CORRODED. REPAIRED DAMAGED FLOORBEAM TEE IAW SRM 53-20-01, FIG 3 AND 51-70-01, FIG 3.

Part: SUPPORT — CRACKED (WNG-BDY FAIRING) · airframe 49,026 hrs · 27,116 cycles

WING TO BODY FILLET FAIRING SUPPORT, BS 977, LBL 7, CRACKED IN WEB OF SUPPORT. REMOVED FRAME FROM WHEEL WELL. DRILLED, SEALED AND INSTALLED IAW DWG 5930584 AND SRM 51-30-02.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 49,026 hrs · 27,116 cycles

NR 2 ENGINE AFT MOUNT HAT BUSHINGS CORRODED. R & R NR 2 ENGINE AFT MOUNT BUSHINGS IAW CMM 71-20-14.

Part: ATTACH ANGLE — CRACKED (BS 1508) · airframe 49,026 hrs · 27,116 cycles

AFT FUSELAGE BS 1508 FRAME TO SKIN ATTACH ANGLE CRACKED BETWEEN L1 AND L2R. REMOVED AND REPLACED CRACKED ANGLE AT STA 1508 IAW SRM 51-30-02 PG 1.

Part: CAP — ERODED (RT AILERON) · airframe 49,026 hrs · 27,116 cycles

RIGHT AILERON CONTROL TAB ENDCAP INBD AFT CORNER IS CRACKED AND ERODED. REPAIRED DAMAGE IAW SRM 57-50-02, PGS 21-22.

Part: STEP — CORRODED · airframe 49,026 hrs · 27,116 cycles

AFT VENTRAL STAIRS 11TH STEP FROM BOTTOM STEP TREAD LBL 11 HAS AREA OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. WO 5220-4001 COMPLETED IAW SRM 53-00-01, PG 5-9, FIG 3.

Part: CUSP WEB — CORRODED (BS 1146) · airframe 49,026 hrs · 27,116 cycles

RT CUSP WEB AT BS 1146 IS CORRODED ON UPPER SURFACE AROUNG LIGHTNING HOLE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED CUSP WEB SECTION AT BS 1146 RIGHT IAW SRM 51-10-05, PG 1.

Part: CUSP WEB — CORRODED (BS 1150) · airframe 49,026 hrs · 27,116 cycles

MAIN CABIN BS 1150, RBL 54 CUSP WEB HAS CORROSION UNDER SEAT TRACK. PER LP STATES WORK ACCOMPLISHED ON WO 1757445. REPLACED CUSP WEB.

Part: SEAT TRACK — GOUGED (BS 788) · airframe 49,026 hrs · 27,116 cycles

SEAT TRACK, RBL 22 BS 788 GOUGED. BLENDED DAMAGE. OUT OF LIMITS. R & R SECTION RBL 22 STA 788 TO STA 850 IAW SRM 53-40-01, PG 30, FIG 6.

Part: FLOORBEAM — CORRODED (BS 1379) · airframe 49,026 hrs · 27,116 cycles

PASSENGER CABIN RT SIDE FLOORBEAM BS 1379, RBL 25 TO RBL 51 CORRODED ON UPPER SURFACE AROUND NUTPLATES. REMOVED CORROSION. MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR PARTS, PRIMED AND INSTALLED IAW SRM 53-20-01, VOL I.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 49,026 hrs · 27,116 cycles

PASSENGER CABIN BS 200 LBL 9-13 FLOORBEAM CORRODED. TASK NR 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED FLOORBEAM IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 859) · airframe 49,026 hrs · 27,116 cycles

PASSENGER CABIN SEAT TRACK RBL 22 BS 859 HAS UPPER SURFACE CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-40-01 VOL I.

Part: SEAT TRACK — CORRODED (BS 1084-1087) · airframe 49,026 hrs · 27,116 cycles

PASSENGER CABIN SEAT TRACK RBL 22, BS 1084 TO BS 1087 HAS UPPER SURFACE CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-30-05 TABLE I PAGE 1.

Part: SEAT TRACK — CORRODED (BS 1193) · airframe 49,026 hrs · 27,116 cycles

DURING CHECK, FOUND CABIN FLOOR STRUCTURE LT SIDE BS 1193- LBL 36 SEAT TRACK CORRODED ON UPPER SURFACE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM VOL 2, 51-30-01 FIG 1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 49,026 hrs · 27,116 cycles

L2 DOOR CUTOUT AFT GIRT BAR MOUNT CHANNEL IS CORRODED ON UPPER SURFACE AT NUTPLATE HOLES. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R BAR MOUNT IAW SRM 51-30-05, SRM 51-10-03, AND 51-00-01.

Part: CREASE BEAM — GOUGED (BS 250) · airframe 49,026 hrs · 27,116 cycles

LEFT CREASE BEAM WEB GOUGED UNDERSIDE AT BS 250. REMOVED CORROSION FROM CUSP WEB. 100 PERCENT MATERIAL LOSS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02.

Part: CREASE BEAM — CORRODED (BS 550) · airframe 49,026 hrs · 27,116 cycles

LEFT CREASE BEAM WEB CORRODED AROUND CENTER LIGHTENING HOLE BS 550. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. NDT, REPAIRED, INSTALLED REPAIR AND CIC'D IAW SRM 53-20-02 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 533) · airframe 49,026 hrs · 27,116 cycles

RIGHT CUSP WEB BS 533 HAS UPPER SURFACE CORROSION. BLENDED DAMAGE. OUT OF LIMITS. REPAIRED IAW SRM 53-20-02.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 49,026 hrs · 27,116 cycles

FLOORBEAM BS 200 LBL 5 - RBL 5 CORRODED. BLENDED DAMAGE. OUT OF LIMITS. R & R IAW SRM 51-30-02 AND DWG 9936534.

Part: CREASE BEAM — CORRODED (BS 610-650) · airframe 49,026 hrs · 27,116 cycles

CABIN LT CREASE BEAM WEB CORRODED STA 610-650. REMOVED CORROSION. OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-20-02, FIG 19 AND 51-30-02, PG 1.

Part: BATTERY PACK — ACTIVATED (EMERGENCY LIGHT) · airframe 48,821 hrs · 27,006 cycles

DURING SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY BATTERY SUPPLY. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,407 hrs · 26,755 cycles

EMERGENCY LIGHT ABOVE SEAT 30AB INOPERATIVE. REPLACED LIGHT ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,086 hrs · 26,592 cycles

DURING SERVICE CHECK, MX FOUND 2 EA CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. LAMPED TWO CABIN CEILING LIGHTS. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,848 hrs · 26,454 cycles

DURING SERVICE CHECK, MX FOUND AFT VENTRAL STAIRS EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN BEHIND LIGHT ASSY. RECONNECTED EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SHEAR TIE — CORRODED (BS 1344 L26R) · airframe 47,620 hrs · 26,336 cycles

DURING PSV, FOUND CORROSION ON SHEAR TIE AT BS 1344 BETWEEN L26-27R. FABRICATED SHEAR TIE AND INSTALLED IAW SRM 53-10-02, FIG 3.

Part: FAIRING — PUNCTURED (ELEVATOR) · airframe 47,620 hrs · 26,336 cycles

RIGHT GEAR TAB FIXED FAIRING DAMAGED ON INBD SIDE. REPAIRED IAW ERA 507327-14, REV ORIG.

Part: LONGERON SPLICE — CORRODED (BS 1360 L27R) · airframe 47,620 hrs · 26,336 cycles

DURING PSV, FOUND CORROSION ON LONGERON 27R AT BS 1360. CORROSION WITHIN LIMITS BUT LONGERON SPLICE OUT OF LIMITS AND REPAIRED IAW ERA 507294-14.

Part: LONGERON — CRACKED (BS 1475 L2R) · airframe 47,620 hrs · 26,336 cycles

DURING PSV, FOUND A CRACK TO LONGERON 2R AT BS 1475. CUT OUT DAMAGE AND INSTALL SPLICE REPAIR.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 45,967 hrs · 25,439 cycles

PERFORMED BOLT HOLE INSPECTION PER PRI 499823-14 AND DOUGLAS/BOEING NDTSP MANUAL PART 6 CHAPTER 06-10.003. NO CRACKS NOTED. PRI REPLACED BY ERA 499823-14 REV O.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

COMPLY WITH STEP 6 OF PRI. REPLACED P/N 99-11524-3, SHEAR TIE ANGLE. DRILLED UP NEW SHEAR TIE ANGLE AND INSTALLED PER ERA 499823-14 REV O.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

PERFORMED HFEC L-17L 2 INCHES FORWARD AND AFT OF FS 238 PER DOUGLAS BOEING NDTSP MANUAL PART 06-10-01-001 STEP 5 OF PRI 499823-14. NO CRACKS NOTED. STEP 5 OF PRI 499823-14 REPLACED BY ERA 499823-14 REV O.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

COMPLY WITH ITEM 7 OF PRI, RE-ACCOMPLISH AFT QUADRANT SKIN REPAIR. DRILLED, INSTALLED AND PAINTED AFT QUADRANT SKIN REPAIR DOUBLER PER ERA 499823-14 REV O.

Part: PAN — CRACKED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

DURING REPAIR OF DOUBLER FOUND CRACK IN FLOOR PAN AT FS 229 INBOARD OF L-18L APPROXIMATELY 2.25 INCHES LONG. REMOVED DAMAGED FLOOR WEB, DRILLED AND INSTALLED REPLACEMENT FLOOR WEB PER SRM 51-30-02, FS 229 INBOARD OF L-18L.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

REMOVED DAMAGED FORMER SHEAR TIE ANGLE PER PRI499823-14. PRI REPLACED BY ERA 499823-14 REV ORIGINAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 45,967 hrs · 25,439 cycles

REMOVED DOUBLER REPAIR INSTALLED PER ERA385357-14 PER PRI499823-14. PRI REPLACED BY ERA 499823-14 REV O.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 45,965 hrs · 25,438 cycles

RAMP REPORTS DENT DAMAGE ON EXTERNAL DOUBLER REPAIR LOCATED AFT OF L1 DOOR AT STATION 229.

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 44,142 hrs · 24,528 cycles

FUSELAGE C-1 CARGO DOOR CUTOUT LOWER JAMB PAN CORROSION FOUND AT PSV-N NON ROUTINE 78.

Part: WIRE — BROKEN (CABIN) · airframe 42,753 hrs · 23,922 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT ROW 24 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT ROW 24. OPERATION OF THE LIGHT NOW CHECKS GOOD. (2010-D1248) (DLM90102853)

Part: HANDSET — SHORTED (FA PANEL) · airframe 39,784 hrs · 22,321 cycles

IN CRUISE FWD F/A PANEL HANDSET CORD BECAME VERY HOT, SMOKED AND MELTED. PULLED C/B'S A10 AND A8 IAW MX CORD COOLED. FOUND FWD F/A HANDSET CORD SHORTED. REPLACED HANDSET. OPS NORMAL.

Part: BOOT — WORN (RT A/C PACK) · airframe 37,889 hrs · 21,250 cycles

LEVELING AT 33000 ALT FLOW LIGHT ILLUMINATED RT PACK FLOW DROPPED TO ZERO DESCENDED TO 24000 RAN QRH PROCEDURES FOR FLOW LIGHT AND LOSS OF PACK DID NOT RESTORE PRESSURIZATION CABIN ALT REACHED 13500 DESCENDED TO 10000 ALT CABIN DOOR LIGHT ILLUM OUT OF 24000. REPLACED RT A/C WATER SEPARATOR BAG AND CLAMP ASSY.

Part: SKIN — CORRODED (FS 826-845) · airframe 37,235 hrs · 20,871 cycles

CORROSION ON THE FUSELAGE SKIN BETWEEN BS 826-845 AT THE ATTACH POINT FOR THE LOWER WTB FAIRING. REPAIRED IAW ERA 470201-14.

Part: COALESCER BAG — ODOR (AFT) · airframe 35,803 hrs · 20,051 cycles

ON LANDING ROLLOUT, SIGNIFICANT SMOKE/ODOR NOTICED IN CABIN AND COCKPIT. PERFORMED DUCT BURNOUT PROCEDURE PER AMM AND INSPECTED ACM TURBINES. NO CONTAMINATION FOUND. INSPECTED APU INLET. NO CONTAMINATION NOTED. REPLACED COALESCER BAGS. RAN PACKS WITH APU AND ENGS. NO SMOKE/ODOR NOTED.

Part: PROXIMITY SENSOR — MALFUNCTIONED (LT MLG) · airframe 35,655 hrs · 19,968 cycles

LT MAIN GEAR RED LIGHT WAS SLOW TO EXTINGUISH AFTER TAKEOFF. ASSOCIATED OAP MESSAGE AUTO SPOILER FAIL. QRH PROCEDURE FOR AUTOSPOILER FAIL MESSAGE DID NOT EXTINGUISH MESSAGE. RETURN SLC AS DIRECTED BY COMPANY. CHECKED NOSE GEAR PROX SENSORS WIRES AND TARGETS ALL CK GOOD REPLACED PROX ELECTRONICS UNIT PER M/M. REPLACED BOTH NOSE PROX SENSORS D1-32 D1-31 SWUNG GEAR PER M/M ALL OPS NML.

Part: BYPASS SWITCH — OUT OF ADJUST (MLG) · airframe 34,369 hrs · 19,251 cycles

LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. FOUND BYPASS HANDLE IN BYPASS POSITION. CYCLED AND STOWED HANDLE SEVERAL TIMES. ALL OPERATIONS NORMAL.

Part: PAN — CORRODED (FWD CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

FOUND LWR FLANGE OF FWD CARGO DOOR CUTOUT CORRODED. REPAIR PER SRM 51-70-01 FIG 1 REF N/R 1400-0343 AT HMV 2.

Part: SKIN — CRACKED (RT WING) · airframe 33,543 hrs · 18,771 cycles

RT WING L/E SKIN CRACKED AT O/B END OF THE REFUELING PANEL CUT OUT. REPAIR PER SRM 57-20-01 FIG 2 HMV 2 REF N/R 6200-0002.

Part: SKIN — GOUGED (MID CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

FOUND MID CARGO DOOR SKIN AFT LWR CORNER GOUGED. REMOVED AND REPLACED DOUBLER PER SRM 51-30-02 AT HMV2 REF N/R 8000-0035.

Part: SKIN — BENT (L1 DOOR) · airframe 33,543 hrs · 18,771 cycles

FOUND L1 DOOR LOWER AFT CORNER SKIN IS BENT. REPAIR PER SRM 52-10-01 AT HMV2 REF N/R 8000-0003.

Part: FRAME — CORRODED (FS 1364 L26-30R) · airframe 33,543 hrs · 18,771 cycles

AFT CARGO PIT STA 1364 AFT SIDE OF FRAME CORRODED LONG 26-30R. REPAIR PER SRM 53-00-01 REF N/R 1600-0286.

Part: LONGERON SPLICE — CORRODED (BS 1136-1155) · airframe 33,543 hrs · 18,771 cycles

FOUND AFT CARGO PIT LONG CORRODED AT STA 1136-1155. REPAIR PER SRM 51-30-05 REF N/R 1600-0151.

Part: FRAME — CORRODED (FS 1379 L30) · airframe 33,543 hrs · 18,771 cycles

FOUND AFT B/B FRAME AT STA 1379 LONG 30 CORRODED. REPAIR PER SRM 53-10-02D.

Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

C-1 DOOR HAS DENT 15IN ABOVE LWR AFT CORNER GOUGED. REPAIR PER SRM 53-30-01 FIG REF8000-0001.

Part: SKIN — DENTED (FS 185 S23-24R) · airframe 33,543 hrs · 18,771 cycles

FOUND FUSE SKIN DENTED AT FS 185 BETWEEN LONG 23R AND 24R. REPAIR PER SRM 53-30-02 FIG 07.

Part: CUSP WEB — CORRODED (FS 788-807) · airframe 33,543 hrs · 18,771 cycles

AT HMV2, CUSP WEB AT STA 788-807 LT CORRODED. REPAIRED IAW ERA 398191-14MA REF N/R 2400-0214.

Part: ATTACH ANGLE — CRACKED (FS 1475) · airframe 33,543 hrs · 18,771 cycles

RT DORSAL TO FUSELAGE ATTACH ANGLE CRACKED 2 PLACES STA 1475HMV2. REPLACED ANGLE PER SRM 51-30-05 PG 10A AND 15 REF N/R 3300-0076.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

AFT CARGO DOOR INNER PAN CRACKED UNDER 2ND FROM BOTTOM STOP FITTING. REPAIRED PER SRM 52-30-02D.

Part: DOOR FRAME — CRACKED (FS 200) · airframe 33,543 hrs · 18,771 cycles

FOUND FWD ENTRY DOOR JAMB AFT WEB CRACKED FS 200. FAB AND INST REPAIR IAW SRM 51-11-01 PG 05.

Part: FLOORBEAM — CORRODED (FS 1364) · airframe 33,543 hrs · 18,771 cycles

FOUND CABIN FLOORBEAM FS 1364 CORRODED. REPAIR PER SRM 51-70-01 FIG 1.

Part: WEB — CORRODED (FS 370 L26R) · airframe 33,543 hrs · 18,771 cycles

FOUND FWD PIT WEB SURFACE CORROSION AT STA 370 LONG 26R. FABBED AND INSTALLED REPAIR PER SRM 53-00-01AT HMV2 REF N/R 1400-0073.

Part: WEB — CORRODED (FS 370 S26L) · airframe 33,543 hrs · 18,771 cycles

FOUND FWD PIT WEB FS 370 BELOW L26 CORRODED OUT OF LIMITS. FABBED AND REP PER SRM 51-30-02 ,51-30-05,51-30-04 REF N/R 1400-0325 AT HMV2.

Part: CUSP WEB — CORRODED (FS 1192-1231) · airframe 33,543 hrs · 18,771 cycles

AT HMV 2, FOUND CUSP WEB CORRODED LT STA 1193-1231. FABBED 2 DOUBLERS IAW MD90 SRM 53-00-01 AND 51-10-03 REF N/R 2400-0239.

Part: CUSP WEB — CORRODED (BS 798) · airframe 33,543 hrs · 18,771 cycles

RT CUSP WEB OUT OF LIMITS STA 798 FOUND AT HMV2. REPAIRED PER SRM 53-05D FIG 827 REF N/R 2700-0223.

Part: PAN — CRACKED (CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

FOUND FWD CARGO DOOR INNER PAN CRACKED AT AFT LATCH. REPAIR IAW SRM 52-30-02D FIG 3 REF N/R 8100-0038.

Part: CUSP WEB — DAMAGED (FS 735-750) · airframe 33,543 hrs · 18,771 cycles

DURING HMV 2 FOUND CUSP WEB FS 735-750 OUT OF LIMITS. REPAIRED PER ERA 398191-14MA ON N/R 2700-0222.

Part: SKIN — CRACKED (NLG DOOR) · airframe 33,543 hrs · 18,771 cycles

FUSELAGE CRACKED AND RIVETS PULLED THROUGH AT LT NOSE GEAR STRUT DOOR AFT HINGE CUT OUT. REPAIR PER SRM 53-05D REF FIG 62 PG1 REF N/R 1000-0004 AT HMV2.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 33,543 hrs · 18,771 cycles

FOUND AFT CARGO DOOR SKIN DENTED 2 AREAS. REPAIR IAW SRM 53-30-02 PG 20 FIG 7 SH1 REF N/R 8300-0015.

Part: CUSP WEB — CORRODED (FS 645-654) · airframe 33,543 hrs · 18,771 cycles

FOUND RT CUSP WEB OUT OF LIMITS FS 645. REPLACED CUSP WEB IAW SRM 51-30-02 REF NR 2700-0224.

Part: CUSP WEB — CORRODED (FS 607) · airframe 33,543 hrs · 18,771 cycles

FOUND RT CUSP WEB AT STA 607 OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-30-02 REF N/R 2700-0221 AT HMV2.

Part: ENGINE — HOT START (NR 1) · airframe 31,136 hrs · 17,398 cycles

ON DESCENT, NR 1 ENGINE EGT PEGGED AT TOP OF RED RANGE 881 DEG WITH OIL PRESS AT 260 PSI AND OIL TEMP 96 DEG. NO OTHER UNUSUAL INDICATIONS. RETARDED TO IDLE WITH NO IMPROVEMENT. SHUT ENGINE DOWN IAW QRH. REPLACED ENGINE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 30,813 hrs · 17,222 cycles

FLOOR EMERGENCY LIGHTS INOP ROW 10 -13 CDE. FOUND BROKEN WIRE. RESPLICED, CHECKS NORMAL NOW.

Part: INSULATION — LOOSE (A/C SUPPLY) · airframe 27,818 hrs · 15,638 cycles

FLIGHT ATTENDANT OBSERVED EXTENSIVE AMOUNT OF SMOKE STRONG ODOR AND HOT AIR IN AFT CABIN PRIOR TO BOARDING. FOUND RIGHT A/C SUPPLY DUCT INSULATION OFF AND TAPE ON DUCT REMOVED TAPE AND REPLACED INSULATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,108 hrs · 14,793 cycles

DURING L/O FOUND 2R & 1L EXTERIOR LIGHTS INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY AND BATTERY RACK (B5-125). CHECKS GOOD.

Part: STRUT — LEAKING (NLG) · airframe 24,737 hrs · 14,064 cycles

AFTER TAKEOFF NOSE GEAR UNSAFE LIGHT STAYED ILLUMINATED. CYCLED GEAR IAW POM GEAR REMAINED UNSAFE. FOUND NOSE STRUT LEAKING. REPACKING NOSE STRUT.

Part: VALVE — FAILED (NLG) · airframe 23,803 hrs · 13,585 cycles

UNSAFT NOSE GEARUP. RECYCLED GEAR AS PER POM PROCEDURE. ON GEAR UP NOSE GEAR UNSAFE (RED) STAYED ON 35 SECONDS LONGER THAN OTHER GEAR LIGHTS AND THE AIRFLOW NOISE DURING THAT TIME WAS LOUD AND UNUSUAL. JACKED NOSE, RAN GEAR, OPS CHECK GOOD. CHECKED DOWN RIGGING GOOD. SERVICED NOSE STRUT AND REPLACED SHRADER VALVE. CHECKED AIR GAP ON PROX SENSOR FOUND OK. AIRCRAFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (RT MLG W/W) · airframe 22,559 hrs · 12,956 cycles

GEAR DOOR OPEN ANNUNCIATOR YELLOW WITH LANDING GEAR HANDLE UP AND LANDING GEAR LITES EXTINGUISHED. REPLACED RT GEAR DOOR PROX SENSOR. INDICATIONS CHECK NORMAL.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 21,218 hrs · 12,276 cycles

AT CRUISE EOAP-LT HYD PRESS LO-ILLUMINATED. L/R HTD QTY OK. COULD NOT RESTORE L HYD PRESS PER POM. FOUND METAL CHUNKS IN LT ENG HYD PUMP. REMOVED AND REPLACED LT ENG HYD PUMP PER MM. REPLACED LT EDP CASE DRAIN / PRESS FILTERS. REPLACED L SYS RETURN FILTERS. FLUSHED SYS. RAN LT ENG / EDP. CHECKED EDP CASE DRAIN/ PRESS FILTERS. NO METAL FOUND. REPLACED EDP CASE DRAIN. OK FOR SERVICE.

Part: ADC — FAULTY (E/E BAY) · airframe 20,299 hrs · 11,816 cycles

ABORTED TAKEOFF AT 100 KTS. CAPTAINS AIRSPEED FROZE AT 80 KTS, F/O AIRSPEED INDICATED 100 KTS. ALSO HAD WINDSHEER INOP ON OAP. REPLACED CAPTAINS AIR DATA COMPUTER. BITE COMPUTER CHECKS GOOD. PERFORMED PITOT TEST NR 1 AND NR 2, CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,535 hrs · 11,414 cycles

OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. CKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 19,384 hrs · 11,334 cycles

EMERGENCY PATH LIGHTS FROM SEAT 34 AFT INOP. REPLACED POWER SUPPLY, CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,975 hrs · 11,112 cycles

EMERGENCY TRACK LIGHTING AT SEAT 15C INOP / BROKEN. REPLACED TRACK AND LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,975 hrs · 11,112 cycles

EMERGENCY TRACK LIGHT INOP NEAR SEAT 1A. RELAMPED LIGHT.

Part: MODULE — MISSING (SEAT 15) · airframe 17,648 hrs · 10,424 cycles

EMERGENCY TRACK LIGHT DAMAGED BY ROW 15. RELAMPED AND INSTALLED NEW COVER.

Part: ENGINE — FAILED (NR 2) · airframe 16,771 hrs · 9,945 cycles

ABORTED T/O AT APPROX 50 KNOTS DUE TO SEVERAL LOUD POPS ON RT ENGINE. AT IDLE N1 AND N2 APPEARED NORMAL. EGT WAS APPROX 80 DEG WARMER AND FUEL FLOW APPROX 150 PPH HIGHER THAN LEFT ENGINE. FOUND METAL IN TAILPIPE. ENGINE CHANGED.

Part: HOUSING — MISSING (ROW 18) · airframe 16,145 hrs · 9,592 cycles

EMERGENCY FLOOR TRACK MODULE MISSING AT ROW 18. REPLACED BULB AND LENS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,768 hrs · 9,395 cycles

THE STATION 1520.225 CANTED BULKHEAD WEB WAS FOUND CRACKED AT THE JOGGLED SPLICE FOR THE UPPER AND LOWER WEBS AT STR 8L & 8R (11 O''CLOCK AND 1 O''CLOCK POSITIONS). ONE CRACK WAS 10 INCHES AND THE OTHER WAS 18 INCHES. THE CRACKED SECTIONS OF WEB WERE CUT OFF AND REPAIRED WITH TWO ALUMINUM DOUBLERS PER ER/A 369732-14, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 15,768 hrs · 9,395 cycles

FRAME CRACKED TAIL COMPT LT SIDE 7 O''CLOCK CRACKED FROM LIGHTENING HOLE THRU OUTER RADIUS STA 1531.604. REPAIRED SAME.

Part: WIRE — DAMAGED (CABIN)

ON PREFLIGHT, FOUND FWD FLOOR EMERGENCY LIGHTS INOP. REPAIRED WIRING.

Part: TRANSFER RELAY — FAILED (COCKPIT)

WHEN THE A/C EMERGENCY PWR IN USE LIGHT CAME ON, PER POM THE EMERGENCY PWR SWITCH WAS PLACED TO THE OFF POSITION. THE EMERGENCY AC BUS OFF LIGHT CAME ON INDICATING THE EMERGENCY AC BUS WAS BEING POWERED FROM THE BATTERY. ACFT WAS DIVERTED TO LAS. REPLACED A/C EMERGENCY POWER TRANSFER RELAY R2-47.

Part: GENERATOR — FAILED (RT ENGINE)

ON DEPARTURE OUT OF DFW LOST RT GENERATOR. NO OTHER ELECTRICAL MALFUNCTIONS NOTED.

Part: DE ICE — FAILED (LT STRAKE)

ANTI-ICE FAULT ILLUMINATES ON O.A.P. WITH ACFT IN AIR MODE AND ENG A/I ON...LEFT STRAKE LOWER SURFACE NOT HEATING AND ARCING. REPLACED STRAKE ASSEMBLY OPERATION NORMAL.

Part: GENERATOR — FAILED (NR 2 ENGINE)

INFLIGHT 310 FL, RIGHT GEN FAILED WITH R GEN OFF AND R AC PWR FAULT ON, OAP LT ALREADY ON MCO. NEEDS RT VSCF, REMOVED RT VSCF, INSTALLED NEW VSCF, RAN ENG TEST NORMAL. METERED OIL TEMP SENSOR AND WIRES FROM CONVERTER TO GEN, ALL NORMAL.

Part: STRAKE DE-ICE — FAILED (LT FWD FUS)

EWR - FLT 0282 - AFT ANTI-ICE FAULT MSG IN-FLIGHT WHEN USING ANTI-ICE. APPROACHING GATE 46B NOTICED A LARGE AMOUNT OF WHITE SMOKE ON LEFT SIDE OF AIRCRAFT. LEFT STRAKE OVERHEATED CAUSING PAINT TO CHAR AND BLISTER OFF. LEFT STRAKE CIRCUIT BREAKERS TRIPPED. FOUND LEFT STRAKE BURNED, REPLACED LEFT STRAKE, CONTROLLER AND THREE CIRCUIT BREAKERS. TESTS OK PER 30-13-00. (X)