N965DL

Part: SWITCH — MISWIRED (TAXI LIGHT) · airframe 76,569 hrs · 57,098 cycles

WHEN WE GOT ON THE GROUND NOSE WHEEL LIGHT PULSED WITH SPEED OF MOTORS. INTERIOR LIGHTS PULSED TOO. BOTH NOSE TAXI LAMPS BLOWN, NO POWER TO EITHER NOSE TAXI LAMP. R &R RT TAXI LAMP SUSPECT INPROPER WIRING "UN MARKED WIRES ON LT NOSE TAXI LAMP."WHILE TROUBLESHOOTING, FOUND BURNED TRANSFORMER "T1-5". CONTINUED TROUBLESHOOTING AND FOUND IMPROPERLY WIRED SWITCH "S1-9". SWITCH "S1-9" NOT WIRED PER MD88 WDM 33-41-01 PROPERLY WIRED SWITCH "S1-9" PER MD88 WDM 33-41-01 . REMOVED AND REPLACED TRANSFORMER "T1-S" PER MD88 WDM 33-41-01. REMOVED AND REPLACED LT TAXI LAMP PER MD88 AMM 33-41. OK FOR SVC. (LP6573966)

Part: FRAME — CRACKED (TAILCONE) · airframe 76,233 hrs · 56,773 cycles

TAILCONE CANTED SUPPORT FRAME (1)CRACKED @GUIDE PIN 1:00 (2) CRACKED @5:00 NEAR GUIDE PIN MKD. REMOVED RT. FRAME AND DRILLED NEW FRAME PER BOEING DWG5966769 (458779) BEGAN INSTALLATION OF RT FRAME (ALL FASTENERS THROUGH SKIN INSTALLED ) PER BOEING DWG 5966769. FINISH INSTALLATION OF LOWER RT FRAME PER BOEING DWG 5966769. REMOVED UPPERSUPPORT FRAME AND STARTED TO DRTII UP REPLACEMENT UPPER SUPPORT FRAME PER BOEING DRAWING 5966768. COMPLETED DRILLING UP PROCESS AND INSTALLED UPPER SUPPORT FRAME PER BOEING DWG596678. (LP1302226)

Part: FRAME — CRACKED · airframe 76,233 hrs · 56,773 cycles

LOWER FRAME CRACKED AT 7:00 POSITION (MARKED) AT TAILCONE GUIDE PIN.REMOVED LT. FRAME AND DRILLED NEW FRAME PER BOEING DWG 5966769. BEGAN INSTALLATION OF LT. FRAME (ALL FASTENERS THRU SKIN INSTALLED.) PER BOEING DWG 5966769(450401) FINISHED INSTALLATION OF LOWER LEFT FRAME PER DWG 5966769. (LP1302206)

Part: PIN — DISENGAGED (EVAC SLIDE) · airframe 76,217 hrs · 56,753 cycles

SVC CHK FOUND L1 DOOR SLIDE PIN NOT ENGAGED. REMOVED L1 DOOR SLIDE REF W/C 2561-4964 INSTALLING NEW SLIDE REF W/C 2561-4964. SLIDE, EVAC, FO OFF 88-2560-9-0003 S/N 03040. (LP5587108)

Part: DOOR — DETACHED (EXTERNAL POWER) · airframe 76,233 hrs · 56,773 cycles

EXTERNAL POWER DOOR MISSING. INSTALLED EXTERNAL POWER ACCESS DOOR ASSYM PER MD88 CMM 53-30-02.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 76,034 hrs · 56,581 cycles

F/C LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. SMOKE DETECTOR BEEPING. R AND R F/C LAV SMOKE DET REF MD88 M/M 26-17. CKS GOOD. (LP1244638)

Part: UNKNOWN — ODOR (GALLEY & COCKPIT) · airframe 75,628 hrs · 56,237 cycles

ON TAXI IN FUEL SMELL THROUGH GASPERS IN FWD GALLEY AND COCKPIT. APU RUNNING. T/S PER AMDS W.C. 2120-2367 - NO CONTAMINATION OF FLUIDS FOUND. PERFORMED FULL DUCT BURNOUT PER AMDS W.C. 7100-2619 - NO ODORS DETECTED - ALL PANELS CLOSED. ALL NO GO ODI PREVENTION REQUIREMENTS C/W FOR ATA 2172. (LP4628112)

Part: LANYARD — DEFECTIVE (EVAC SLIDE) · airframe 75,359 hrs · 55,990 cycles

SLIDE FAILED TO DEPLOY WORK CARD # 88-0525-8-0408 SLIDE D29984-213 S/N 1241 MFG DATE MAR 2000. FND LANYARD ON COVER BAD REPLCD SAME. (LP1060688)

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 74,895 hrs · 55,602 cycles

ON CLIMB OUT BETWEEN 14,500 AND 15,000 FEET WE HEARD A LOUD BANG ACCOMPANIED WITH AN AIRCRAFT SHUTTER AND NOTED LEFT ENGINE NO EPR, NO N1, EGT APPROX. 775, DID IMMEDIATE ACTION ITEMS AND SHUT DOWN LEFT ENGINE PER QRH. STABILIZED AIRCRAFT AT 16,00 FEET RETURNED TO KIAD IN DISCUSSIONS WITH THE FLIGHT ATTENDANTS NO ODORS OR SMELLS WERE NOTED IN CABIN. REMOVED AND REPLACED LT ENGINE IAW 7100-4682-LH. PEFORMED OPS CHKS. ALL OPS CHK GOOD. NO LEAKS NOTED. A/C OK FOR SVC POWER PLANT, JT OFF 88-7110-9-0010 25953 ON 88-7110-9-0010 25878. (LP5549996)

Part: GENERATOR — FAILED (RT ENGINE) · airframe 74,516 hrs · 55,276 cycles

WITH RIGHT ENGINE GENERATOR ON DEFERRAL, APPROACHING IND, RT BUS LOST POWER, WITH APU RUNNING. RESET APU ON SHORT FINAL AND REGAINED POWER TO RT BUS. AIRPLANE NOT SUITABLE FOR MC FLIGHT. APPROACH WAS SISUAL ONLY WITH AIRSPEED SETTING KNOB NOR RESPONSIVE UNTIL APU RESET. ENTIRE RIGHT SIDE OF COCKPIT DARK. R/R APU RT PWR RELAY PER MD88 MM 24-20. R/R RT ENG GENERATOR PER MD88 24-20 R/R RT CSD PER MD88 24-10. R/R RT GEN PWR RELAY PER MD88 MM 24-20. ALL OPS CHECKS NORMAL. RAN ENG. LEFT ENG GEN AND APU WILL PICK UP RT BUS W/ RT GEN OFF. A/C OK FOR SVC. R/R APU GCU PER MD88 MM 49-20. APU OPS NORMAL. SDR REPORTED DUE TO AIRCRAFT MOMENTARILY BEING DOWN TO ONE POWER SOUCE. (LP5081252)

Part: HORN — CORRODED (RT WING SLAT) · airframe 74,344 hrs · 55,132 cycles

ON WALK AROUND FOUND CORROSION CRACK ON RT WING INBOARD SLAT. REPLACED RT SLAT HORN PER MD88 AMM 27-80. (LP5059545)

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 73,380 hrs · 54,306 cycles

MAIN ENTRY DOOR UPPER AFT CORNER INTERNAL SURFACE IS CRACKED. REMOVED AND REPLACED MAIN ENTRY DOOR IAW AMM 52-11-00.

Part: SKIN — GOUGED (TE FLAP VANE) · airframe 73,380 hrs · 54,306 cycles

RT WING ON NR 3 FLAP VANE IB SIDE UPPER SURFACE GOUGED. REMOVED DAMAGED SKIN (7" X 7") AND ACCOMPLISHED PERMANENT REPAIR ON NR 3 FLAP VANE LEADING EDGE (16.5" X 12.1" DOUBLER) IAW SRM 57-03D PAR 11 AND FIGURE 11.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,380 hrs · 54,306 cycles

AFT CARGO COMPT LONGERON 29L SPLICE IS CORRODED AT FS STA 1202. AFT CARGO LONGERON 29LT SPLICE STA 1202 CORROSION DAMAGE FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS .062" IAW SRM 53-01 FIG 1 AND DRAWING 3914677 REV L. REMOVED AND REPLACED SPLICE IAW SRM 51-30-5 AND DRAWING 5936667 REV CD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,380 hrs · 54,306 cycles

AFT CARGO AT STR 29L BTW STA 1212 AND 1231 INTERCOSTAL O/B SIDE HAS CORROSION. CORROSION DAMAGE ON AFT CARGO INTERCOSTAL AT LONGERON 29LT BETWEEN STA 1212 AND 1231 FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS .050" IAW SRM 53-01 FIG 1 AND DRAWING 5936071 REV W. REMOVED, FABRICATED NEW, AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2 AND DRAWING#5936071 REV W.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,380 hrs · 54,306 cycles

AFT CARGO COMPT LONGERON 28L SPLICE IS CORRODED AT FS 1202. CORROSION DAMAGE ON AFT CARGO LONGERON 28LT STA 1202 SPLICE FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS .062" IAW SRM 53-01 FIG 1 AND DRAWING 3914677 REV L. REMOVED AND REPLACED SPLICE IAW SRM 51-30-5 AND DRAWING 5936667 REV CD.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,380 hrs · 54,306 cycles

CORROSION FOUND AT AFT PRESSURE BULKHEAD BL0. CORROSION DAMAGE ON AFT PRESSURE BULKHEAD OEM BL0 DOUBLER FOUND OUT OF LIMITS, ORIG THICKNESS .080", MAT LOSS .040", MAT REMAINING .040" IAW DRAWING 5910130 REV ET AND SRM 53-01. REMOVED, FABRICATED NEW, AND INSTALLED NEW DOUBLER IAW SRM 51-30-5, 51-30-2, AND DRAWING 9915561 REV CG, 5910130 REV ET, REV EJ, AND 5930760 REV DL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,380 hrs · 54,306 cycles

AFT CARGO JACK PAD DOUBLER IS CORRODED. FOUND AREA CORRODED ON AFT CARGO JACK PAD DOUBLER WITH ORIGINAL THICKNESS .100 MATT LOSS .060 MATT REMAINING .040 TO BE OUT OF LIMITS IAW SRM 53-01 AFTER CORROSION WAS REMOVED IAW SRM 51-10-3. REMOVED AND INSTALLED NEW DOUBLER PN 9915561-73 IAW DRW 9915561 REV C6 AND SRM 51-30-02.

Part: REPAIR — DEPARTED (RT ELEVATOR TAB) · airframe 73,380 hrs · 54,306 cycles

RT HAND ELEVATOR GEAR TAB (CENTER) HAD BONDED REPAIR THAT HAS DEPARTED AIRCRAFT. REMOVED AND REPLACED RT ELEVATOR GEAR TAB IAW AMM 27-30-04. PERFORMED SATISFACTORY OPS CHECK IAW AMM-27-30-04.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,250 hrs · 54,202 cycles

FUSELAGE LAV SVC CUTOUT STA 1322 AT L-22L CORROSION. COMPLIED WITH ERA 568960-14 REV B SECTION 1 PERMANENT REPAIR. ALL STEPS IN PRI'S 568960-14 REV O, REV 1, REV 2, REV 3, AND REV 4 MATCH STEPS IN ERA 568960-14 REV B SECTION 1 PERMANENT REPAIR.

Part: TIRE — DEFECTIVE (NLG) · airframe 73,170 hrs · 54,130 cycles

ON ROTATION IN RDU 3 LOUD BANGS FROM NOSE GEAR AREA ON LANDING, WITH GEAR EXTENDED, NOTICED A DEEP RUMBLE IN FLOOR UNDER PILOTS FEET. EMERGENCY WAS DECLARED. INSPECTED NLG AREA. NO DAMAGED NOTED. R&R BOTH NLG TIRE IAW AMM 32-40. LUBE NLG SYS. A/C OK FOR SVC.

Part: GENERATOR — FAILED (RIGHT) · airframe 72,923 hrs · 53,927 cycles

RIGHT GENERATOR FAILED. WOULD NOT RESET IN FLIGHT AND A CROSSTIE LOCK-OUT THAT WOULD NOT RESET. AN EMERGENCY WAS DECLARED.

Part: NOT REPORTED — MALFUNCTIONED (FUEL SYSTEM) · airframe 72,231 hrs · 53,391 cycles

DIVERTED TO BNA DUE TO THE FLIGHT CREW REPORTING THAT FUEL APPEARED NOT TO BE BURNING OUT OF THE LEFT WING TANK. MAINTENANCE VERIFIED THAT THE CROSS-FEEDS AND DEFUEL VALVES WERE OPERATING NORMALLY. THE LEFT TANK FUEL BOOST PUMP OPERATION CHECKED GOOD. A HIGH POWER ENGINE RUN WAS PERFORMED. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAULT. THE CHECK VALVE FLUSH PROCEDURE WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 71,023 hrs · 52,434 cycles

APU INLET SATURATED WITH HYD FLUID, CABIN HAZE WITH HYD MIST. CLEANED THE APU INLET & BELLY IAW W/C 4900-1184. PERFORMED FULL DUCT BURNOUT IAW W/C 7100-2619, NO SMOKE OR ODOR NOTED.

Part: VANE — PUNCTURED (TE FLAP) · airframe 70,697 hrs · 52,178 cycles

RT NR 2 FLAP VANE HAS PUNCTURE APPROX 45" FROM INBD EDGE AND 11" FROM TRAILING EDGE MEASURING APPROX 3/4 " X 3/4 ". REMOVED AND REPLACED FLAP VANE REF AMM 27-51-03-201, OPS CKS GOOD.

Part: ACTUATOR — DAMAGED (SPOILERS) · airframe 70,703 hrs · 52,182 cycles

AFTER LANDING, THE PREVIOUS FLIGHT CREW REPORTED A SLAT WOULD NOT RETRACT AND RIGHT FLAP INDICATED APPROX. 3 DEG WITH FLAP SET AT ZERO. FOUND THE RT INBD SPOILER ACTUATOR ROD END BROKEN AND BINDING THE FLAPS. REMOVED AND REPLACED THE SPOILER ACTUATOR, OPS AND LEAK CHECKED GOOD IAW AMM 27-62-02.

Part: CABLE — FRAYED (TAILCONE) · airframe 70,428 hrs · 51,983 cycles

TAILCONE CABLE FRAYED. REPLACED THE CABLE IAW AMM 53-53-00.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 70,282 hrs · 51,872 cycles

CARPET HAS A SOFT SPOT ABOUT 5 BY 5 INCHES. REPLACED CABIN FLOOR PANEL 256C AT CENTER OF F/C CABIN.

Part: MODULE — FAILED (EMERGENCY LIGHT) · airframe 69,635 hrs · 51,407 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ROW 30. REPLACED THE LIGHT MODULE AND HARNESS IAW AMM 33-53. CHECKED GOOD.

Part: TAB — DAMAGED (RUDDER) · airframe 69,532 hrs · 51,330 cycles

RUDDER CONTROL TAB HAS FLAME SPRAY PEELED AND DAMAGED. REPLACED THE RUDDER TAB.

Part: TAB — DAMAGED (RUDDER) · airframe 69,532 hrs · 51,330 cycles

RUDDER HAS FLAME SPRAY PEELING AND DAMAGED. REMOVED AND REPLACED RUDDER IAW AMDS 2720-4421.

Part: FRAME — CRACKED (BS 1510) · airframe 69,532 hrs · 51,330 cycles

BS 1510 CANTED FRAME CRACKED APPROXIMATE LOCATION LONGERON 28R AT TAIL CONE ALIGNMENT PIN. REMOVED AND REPLACED CANTED FRAME AND INSTALLED NEW CANTED FRAME IAW DRAWING 9911843.

Part: FRAME — CRACKED (BS 1510) · airframe 69,532 hrs · 51,330 cycles

BS 1510 CANTED FRAME CRACKED LONGERON 23R. REMOVED AND REPLACED THE FRAME IAW DRAWING 9911843.

Part: RELAY — BURNED (CABIN) · airframe 69,370 hrs · 51,207 cycles

RUBBER SMELL ON TAKEOFF WITH BURNING ODOR. DISSIPATED IN 2-3 MINUTES. UPPER SIDEWALL LIGHTS FLICKERED ON AND OFF (INTERMITTENT USE). COFFEE MAKERS ON AND OFF ALSO. AS PER QRH TURNED GALLEY POWER OFF AISLE LIGHT ON AND SIDEWALL LIGHTS OFF. UPPER SIDEWALL LIGHTS IN FIRST CLASS SECTION WERE NOT WORKING. R&R RELAY R2-229 PER AMM 20-50 AND WDM 33-22-07. SUSPECT SMELL CAME FROM BURNT UP RELAY. PERFORMED AC CROSS-TIE AND LOAD SHEET TEST PER AMM 24-20, NO FAULTS FOUND. COFFEE MAKERS OPS CHECKED GOOD, SUSPECT THEY WENT OFF WHEN GALLEY POWER SWITCHED TO OFF. A/C OK FOR SERVICE.

Part: HINGE — WORN (CARGO DOOR) · airframe 68,494 hrs · 50,547 cycles

MID CARGO DOOR FWD AND AFT HINGES LOOSE & WORN, DOOR VERY LOOSE. REPLACED THE WORN PARTS AND ADJUSTED IAW AMM 52-31-02. LEAK CHECKED GOOD.

Part: RELEASE MECH — OUT OF TOLERANCE (TAILCONE) · airframe 68,494 hrs · 50,547 cycles

DURING TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, OPENING FORCE REQUIRE TO OPEN AFT VENTRAL DOOR IS 30 LBS. PULL TEST OUT OF LIMITS. RIGGED TAILCONE IAW AMDS 5350-01077-0101. ADJUSTED TEE PIN CLIPS, LATCHES, AND LUBED IAW AMDS 5350-01077-0101. PERFORMED TAILCONE DROP FROM THE AFT VENTRAL DOOR, PULL TEST WITHIN LIMITS AND PULLED AT 19 LBS. TAILCONE WILL BE INSTALLED ON AMDS 5350-01077-0101.

Part: REPAIR — DELAMINATED (ANTI-FLOAT TAB) · airframe 68,494 hrs · 50,547 cycles

RT ANTI-FLOAT TAB, INBD REPAIR IS DIS-BONDED, TOP SURFACE. REMOVED AND INSTALLED RT ANTI-FLOAT TAB ON AMDS 2730-4382.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 68,494 hrs · 50,547 cycles

ON PRE DOCK, LT AFT SERVICE DOOR SLIDE PRESSURE LOW. REMOVED AND INSTALLED L2 DOOR SLIDE IAW AMDS 2561-4002.

Part: VANE — DAMAGED (TE FLAP) · airframe 68,494 hrs · 50,547 cycles

RT NR 4 VANE HAS RUBBING MARKS. R & R VANE REF AMM 27-51-03.

Part: VANE — DAMAGED (TE FLAP) · airframe 68,494 hrs · 50,547 cycles

RIGHT NR 3 FLAP VANE HAS A RUBBING AREA WITH A HOLE THROUGH. R & R VANE IAW AMM 27-51-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,494 hrs · 50,547 cycles

AFT RT FLOOR SUPPORT CORRODED UNDER FLOORBOARD PANEL 120E. APPROXIMATE STA 160, RBL55. R & R FLOOR SUPPORT IAW SRM 53-30-02.

Part: BUSHING — WORN (RT ANTIFLOAT TAB) · airframe 68,494 hrs · 50,547 cycles

RT ANTI-FLOAT TAB, OTBD BEARING IS WORN. R & R WORN BUSHINGS, REF PS 900-9-1, NR 06 REF NR 78 FOR TAB REPLACEMENT.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 68,448 hrs · 50,512 cycles

L1 DOOR SLIDE PARACHUTE PINS NOT INSTALLED. R & R L1 DOOR SLIDER IAW WC 2561-4964. OK FOR SERVICE.

Part: FASTENER — DAMAGED (BS 226) · airframe 68,334 hrs · 50,417 cycles

RIVET HEAD POPPED AT BS 226 AND LONGERON 20-R. REMOVED STRINGER SPLICE AND DAMAGED STRINGER SECTION AT 20R, STA 226, ITEM C/W ON LOG NR 2509285.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,232 hrs · 50,340 cycles

RT FORWARD OVERWING EXIT EMERGENCY IDENTIFIER INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY REF AMM 33-53-00. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,232 hrs · 50,340 cycles

ROWS 16-25, EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES FOR APPLICABLE LIGHTS REF AMM 33-53-00. OPS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,220 hrs · 50,334 cycles

SKIN IS CRACKED JUST ABOVE THE PYLON. FWD OF AFT ENGINE MOUNT. ACCOMPLISHED HFEC TO IDENTIFY ENDS OF CRACKS IAW NDTSPM 06-10-01.00. ACCOMPLISHED SECTION 1 OF ER/A 546967-14.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 67,938 hrs · 50,121 cycles

TOP OF FLAP DAMAGE FROM SPOILER MOVEMENT. R & R RT OTBD FLAP INBD FLAP VANE IAW AMM 27-51. OPS CK GOOD.

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 67,944 hrs · 50,127 cycles

SPOILER DEPLOYED MESSAGE. FOUND NR 2 SPOILER ON RT WING INBD ATTACH FITTING CRACKED. SPOILER MOVING AWAY FROM SENSOR WHEN RETRACTED. REPLACED ATTACH FITTING IAW CMM 27-61-10.

Part: SKIN — DAMAGED (BS 256) · airframe 67,236 hrs · 49,646 cycles

ON LIGHTNING STRIKE INSPECTION, FOUND SKIN DAMAGE AT BS 256 JUST BELOW STRINGER 27R. C/W PERMANENT REPAIR IAW SRM 53-04-2.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 64,621 hrs · 47,854 cycles

AISLE EMERGENCY LIGHT ROW 30DE INOPERATIVE. FOUND A BROKEN LOCK TAB ON PIN. PINNED WIRE. OP CHECKED GOOD.

Part: LONGERON — CRACKED (BS 1412-1429) · airframe 69,392 hrs · 51,225 cycles

LONGERON 25L CRACKED BS 1412 - 1429, DAMAGE REMOVED, REPAIR INSTALLED.

Part: SKIN — CORRODED (NOSE COWL) · airframe 63,352 hrs · 46,912 cycles

NR 1 ENGINE NOSE COWL AT FORWARD LIP SKIN EXTERIOR AT APPROXIMATELY 9 O'CLOCK BLISTERED AT FASTENER, CORRODED. REMOVED CORROSION IAW SRM 51-10-03.

Part: SKIN — CORRODED (NR 1 NOSE COWL) · airframe 63,352 hrs · 46,912 cycles

NR 1 ENGINE NOSE COWL AT FORWARD LIP SKIN EXTERIOR AT APPROXIMATELY 9 O'CLOCK HAS BLISTER AT FASTENER, POSSIBLE CORROSION. REMOVED CORROSION AT NR 1 ENG NOSE COWL AT FWD LIP SKIN EXTERIOR APPROX 9.0 O`CLOCK IAW SRM 51-10-03 DIM 1" X 1" UT INSPECTION FOUND AREA WITH TICKNESS OF .090 MATERIAL LOSS .040 MATERIAL REMAINING .050 IAW NDTSPM P4 04-00-07 ASSET 9710 MATERIAL LOSS 40 PERCENT OUT OF LIMIT IAW SRM 54-01, FIG 1 CUT OUT DAMAGE AREA DIM 1" X 1" IAW SRM 54-04A, FABRICATED FILLER FROM 2024"0" .063 PO 908DA-00203 DIM 1" X 1" AND DOUBLER FROM 2024"0" .080 PO ST00001514 SIM 5.2500" X 3.2500" IAW SRM 54-04A, FIG 5, HEAT TREAT PARTS FROM "0" TO T4 CONDITION IAW FAS ENGINNERING REPORT NR 2-37153-801A, REV A INSTALLED REPAIR PARTS IAW SRM 54-04A, FIG 5, INSTALLED ID TAG IAW DELTA PS 900-5-1, VO 04.

Part: FITTING — CORRODED (BS 1250) · airframe 63,333 hrs · 46,898 cycles

MAIN PAX CABIN RT SIDE LONGERON 18R, FRAME FITTING HAS CORROSION AT BS 1250, ON BOTH SIDES OF FITTING. REMOVED FITTING AT LONGERON 18R STA 1250 IAW SRM 51-30-5, FABRICATED NEW FITTING FROM 7075, T7351, PO 913DN-00144, IAW DWG 4911383. INSTALLED IAW SRM 51-30-05, 51-30-01 & DWG 9919604.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 63,333 hrs · 46,898 cycles

AFT CARGO BAY BS 1148, S2-6R SHEAR TIE CORRODED. REMOVED, FABRICATED AND INSTALLED SHEAR TIE SECTION IAW SRM 51-30-02 51-30-05.

Part: SEAT TRACK — DAMAGED (BS 484) · airframe 63,333 hrs · 46,898 cycles

CABIN SEAT TRACKS LT SIDE BS 484 LBL58 HAVE CHIPPED PAINT/ SCRATCHES. REMOVED CORROSION OUT SIDE OF REPAIR ON SEAT TRACK IAW SRM 51-10-3 FOUND TO BE WITHIN LIMITS IAW SRM 53-05 FIG 4B-1, PRIMED AREA IAW SRM 51-10-3. INSTALLED NEW SEAT TRACK IAW SRM 53-05 FIG 4A SHEET 1.

Part: SKIN — CORRODED (BS 760-769) · corrosion level 2 · airframe 63,519 hrs · 47,030 cycles

RT LOWER WING TO BODY FUSELAGE SKIN CORRODED, BS 760-769 BETWEEN L27-28R. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-10-3, 53-31-1, FABRICATED DOUBLER IAW SRM 53-04, FIG 57 AND INSTALLED IAW SRM 51-30-5 & 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 434-446) · airframe 63,333 hrs · 46,898 cycles

MAIN CABIN BETWEEN BS 434 - 446, LONGERON 19 INTERCOSTAL CORRODED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 53-14-2, FIG 2, SH4 51-10-04, 51-30-5, 51-30-02. HEAT TREATED TO 7075-T6 IAW FAS ENGINEERING REPORT 2-37153-801A REV A, FABRICATION AND INSTALLATION IAW DWG 9957909.

Part: CARGO TRACK — CORRODED (BS 1231-1320) · airframe 63,333 hrs · 46,898 cycles

AFT CARGO TRACK FROM BS 1231 - 1320 HAS SEVERAL SPOTS OF CORROSION . FOUND CORROSION OUT OF LIMITS IAW SRM 53-01 FIG 1 AND 53-05 FIG 4C. REMOVED, FABRICATED AND INSTALLED CARGO TRACK IAW SRM 53-65 FIG 4C.

Part: FLOORBEAM — CORRODED (BS 1322) · airframe 63,333 hrs · 46,898 cycles

LEFT AFT LAVATORY FLOORBEAM CORRODED BS 1322 LBL 20. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE. TREATED, PRIMED, TOP COAT AND INSTALLED NEW REPAIR IAW SRM 51-10-3, 53-05 FIG. 79 A AND 51-10-3.

Part: DOOR FRAME — CRACKED (BS 208-218) · airframe 63,333 hrs · 46,898 cycles

UPPER FUSELAGE, INTGERNAL AREA, L1 DOOR BETWEEN BS 208 - 218, LONGERON 9L, WEB CRACKED ON AFT FRAME DOOR. TRIMMED OUT DAMAGE WEB IAW SRM 53-65 FIG 142. FABRICATED FILLER AND DOUBLER IAW SRM 53-05 FIG. 142. INSTALLED REPAIR IAW SRM 53-05 PARA 153 FIG. 143.

Part: CUSP WEB — CORRODED (BS 1070) · airframe 63,333 hrs · 46,898 cycles

CORROSION FOUND ON MAIN CABIN CUSP WEB BS 1070 LBL 58. REMOVED CORROSION IAW SRM 51-10-03 PARA 26 AND FOUND WITHIN LIMITS IAW ERA 511165-14 MA REV. B. AFTER HFEC INSPECTION, FOUND AREA FREE OF CRACKS IAW NDTSPM P 6 06- 10-01.

Part: CUSP WEB — CORRODED (BS 594) · airframe 63,333 hrs · 46,898 cycles

MAIN CABIN RBL 56 CUSP WEB BS 594 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-01 FIG. 10. CUT OUT DAMAGE IAW SRM 53-05 FIG.. 131A-13. FABRICATED FILLER, DOUBLER AND RING DOUBLER IAW SRM 53-05 FIG. 131A-13. INSTALLED REPAIR IAW SRM 53-05 FIG. 131A-13.

Part: CUSP WEB — CORRODED (BS 721-726) · airframe 63,333 hrs · 46,898 cycles

MAIN CABIN CUSP WEB BETWEEN BS 721 - 726 CORRODED AT RBL 56. FOUND AREA OUT OF LIMITS IAW SRM 53-01 FIG. 1. CUT OUT DAMAGE AREA IAW SRM 53-05 FIG. 131A-13. FABRICATED FILLER, DOUBLER, AND RING DOUBLER IAW SRM 53-05 FIG. 131A-13 INSTALLED REPAIR IAW SRM 53-05 FIG. 131A-13.

Part: CUSP WEB — CORRODED (BS 551) · airframe 63,333 hrs · 46,898 cycles

CABIN FLOOR CUSP WEB RT SIDE BS 551 CORRODED ON SURFACE. FOUND AREA OUT OF LIMITS IAW SRM 53-01 FIG. 1. CUT OUT DAMAGE AREA IAW SRM 53-05 FIG. 131A-5, FABRICATED FILLER AND DOUBLER IAW SRM 53-05 FIG 131A-5.

Part: CUSP WEB — CORRODED (BS 475) · airframe 63,333 hrs · 46,898 cycles

RT SIDE CABIN CUSP WEB BS 475, CORRODED ON UPPER SURFACE. BLENDED AREA IAW SRM 53-01 FIG. 1 AND FOUND WITHIN LIMITS IAW ERA 511165-14 MA REV B AFTER HFEC INSPECTION FOUND AREA FREE OF CRACKS IAW NDTSPM P6 06-10-01.

Part: CUSP WEB — CORRODED (BS 615) · airframe 63,333 hrs · 46,898 cycles

CORORSION ON MAIN CABIN CUSP WEB BS 615 RBL 58. FOUND AREA OUT OF LIMITS IAW SRM 53-01 FIG. 1. CUT OUT DAMAGE AREA IAW DTM 53-05 FIG. 131A-8. FABRICATED FILLER AND DOUBLER IAW SRM 53-05 FIG. 131A-8. INSTALLED REPAIR IAW SRM 53-05 FIG. 131A-8.

Part: CUSP WEB — CORRODED (BS 850) · airframe 69,392 hrs · 51,225 cycles

CORROSION ON CUSP WEB BS 850 LBL 58. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 658-671) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN CUSP WEB HAS CORROSION BETWEEN BS 658 - 671. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 63,333 hrs · 46,898 cycles

CABIN FLOOR SUPPORT CORRODED BS 180 LBL 58. REMOVE FLOOR SUPPORT IAW SRM 51-30-2, 51-30-5. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 REV B.W., TREATED AND PRIMED NEW FLOOR SUPPORT IAW SRM 51-10-3 INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 677-690) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN CUSP WEB HAS CORROSION AT RBL 58 BETWEEN BS 677 - 690. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 628-636) · airframe 69,392 hrs · 51,225 cycles

CORROSIN ON MAIN CABIN CUSP WEB, RT SIDE BS 628 - 636 RBL 58. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 608-614) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN LBL 56 CUSP WEB BETWEEN BS 608 - 614 CORRODED. REMOVED THE CORROSION AND INSTALLED FILLERS AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 563) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN CUSP WEB AT BS 563, LBL 56 CORRODED. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 525-540) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN RBL 56 CUSP WEB BETWEEN BS 525 - 540 CORRODED. REMOVED CORROSIN, AND INSTALLED FILLERS AND DOUBLER.

Part: CUSP WEB — CORRODED (BS 480) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN CUSP WEB LBL 56 AT BS 480 CORRODED. CUT OUT THE DAMAGED AREA AND REPAIRED IAW SRM 53 -05 F. 6 131A-13.

Part: CUSP WEB — CORRODED (BS 525) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN AT BS 525 LBL 56 CUSP WEB CORRODED. REPAIRED IAW SRM 53-05 FIG 131-14.

Part: CUSP WEB — CORRODED (BS 480) · airframe 69,392 hrs · 51,225 cycles

MAIN CABIN CUSP WEB LBL 56 AT BS 480 CORRODED. REPAIRED IAW SRM 53-05 F AND ERA 479444-14.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 63,346 hrs · 46,908 cycles

DURING HEAVY CHECK, MAINTENANCE DISCOVERED THAT THE TAILCONE SLIDE WAS UNRAVELING OUT OF ITS CONTAINER. TAILCONE SLIDE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,991 hrs · 46,652 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 24 AFT. REPLACED B5-212 BATTERY PACK AND CHARGER, OPS CKS GOOD IAW AMM 33-53.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 62,895 hrs · 46,576 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHTS AFT OF THE OVERWING EXIT ROW WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,895 hrs · 46,576 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE FORWARD OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,539 hrs · 45,621 cycles

DURING ROUTINE INSPECTION, CORROSION WAS NOTED AT THE AFT CARGO DOOR JAMB ADJACENT TO LONGERON 28R AND SEVERAL LOCATIONS. REPAIRS INCORPORATED IAW SRM 53-05 AND ALL APPLICABLE INSPECTIONS COMPLETED.

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,539 hrs · 45,621 cycles

DURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE MID-CARGO DOOR THRESHOLD ON THE LOWER ZEE ANGLE BETWEEN THE DOOR STOPS. REPAIRS COMPLETED IAW SRM 53-05, FIG 123.

Part: SPAR CAP — CORRODED (VERTICAL STAB) · airframe 61,539 hrs · 45,621 cycles

DURING ROUTINE INSPECTION, 4 HOLE LOCATIONS EXHIBITED CRACK INDICATIONS AT THE LT VERTICAL STABILIZER SPAR CAP AT ZFS 52.267. DAMAGE WAS REPAIRED IAW ER/A 517684-14AD AND THE REQUIRED INSPECTIONS WERE COMPLETED.

Part: SILL — CORRODED (CARGO DOOR) · airframe 61,539 hrs · 45,621 cycles

DURING ROUTINE INSPECTION, EXFOLIATION CORROSION WAS NOTED AT THE FWD CARGO DOOR LOWER SILL PLATE. DURING CORROSION REMOVAL, A CRACK AS NOTED BELOW THE SILL PLATE. CORROSION WAS REMOVED AND THE CRACK WAS REPAIRED IAW ER/A 517680-14AD.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 61,539 hrs · 45,621 cycles

DURING ROUTINE MX, THE LT TAILCONE RELEASE MECHANISM CAM WAS NOTED TO BE WORN IN TWO PLACES AT THE BASE. THE WORN CAM WAS REPLACED IAW AMM 53-53-2 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: HINGE — CORRODED (LAV SERVICE DOOR) · airframe 61,539 hrs · 45,621 cycles

DURING ROUTINE INSPECTION, CORROSION WAS FOUND AT THE AFT LAV SERVICE PANEL HINGE AREA. CORROSION WAS DETERMINED TO BE OUT OF LIMITS AFTER BLENDING/REMOVAL IAW SRM 53-04-01. HINGE ASSY WAS REPLACED.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 61,539 hrs · 45,621 cycles

DURING SCHEDULED INSPECTION, NOTED THE LT VERTICAL STABILIZER FRONT SPAR CAP ABOVE ZFS-52.267 HAD A MISDRILLED COUNTERSINK. REPAIRED IAW ER/A 517678-14AD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 60,646 hrs · 44,964 cycles

DURING OVERNIGHT MX, THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 28DE WAS FOUND TO BE INOPERATIVE. REPLACED DAMAGED WIRE IAW AMM 33-52. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 59,264 hrs · 43,939 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 1 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE SEAT WIRE HARNESS TO BE THE CAUSE OF THE FAULT. SYSTEM WAS REPAIRED AND THE FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,124 hrs · 43,842 cycles

SEAT 25D AFT RED EMERGENCY PATH LIGHT (SEAT MOUNTED) INOP. REPLACED LIGHT ASSY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,636 hrs · 43,528 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 12D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SEAT 12D AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 12DE) · airframe 58,155 hrs · 43,209 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR EXIT ROW 12DE OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT ROW 12DE AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: SKIN — DAMAGED (RT WING) · airframe 57,804 hrs · 42,977 cycles

RIGHT LOWER WING SKIN AND AFT SPAR CAP HOLE DAMAGE. REPAIR DIA W ERA 500224-14.

Part: SPAR CAP — CRACKED (RT WING) · airframe 57,804 hrs · 42,977 cycles

RIGHT WING LOWER SPAR CAP AT ATTACH POINT FOR INBD HINGE FITTING AT STA 164 HAS A 1.6" CRACK AT INBD HOLE. INSTALLED TEMP REPAIR PER EA 09-471576-12AD ME06 OPN 0601 AND DRAWING J060271-510.

Part: SPAR CAP — CRACKED (RT WING) · airframe 57,804 hrs · 42,977 cycles

A CRACK LESS THAN 2 INCHES ON LOWER SPAR CAP RADIUS. REPAIRED IAW ERA 500101-14.

Part: WIRE — BROKEN (CABIN) · airframe 57,497 hrs · 42,787 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 23D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR AND RE-PINNED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,369 hrs · 42,693 cycles

MAIN CABIN FLOORBEAM UPPER FWD FLANGE LOWER SURFACE UNDER NUT PLATE MOUNT STRIP CORRODED STA 1680 RBL 24. FABRICATE ANGLE, STRAPS AND WEB PER SRM 53-00-51 REPAIR 2, 51-30-01 PG 17 FIG 7 AND SHIMS PER B757 SRM 53-00-51 REPAIR 2 FIG 201 STEP 5. AT INSTALLED REPAIRS PER SRM B757 53-00-51 REPAIR 201 PAGE 201. AT SAA/SAT DURING HMV.

Part: SKIN — DENTED (BS 1418) · airframe 55,956 hrs · 41,667 cycles

FUSELAGE SKIN BS 1418, S2R DENTED AND GOUGED. REPAIR IAW ERA 492689-14.

Part: SKIN — CRACKED (BS 1418) · airframe 55,956 hrs · 41,667 cycles

MAINTENANCE NOTED A CRACK COMMON TO THE FUSELAGE SKIN BS 1418 AND S2L. REPAIR IAW ERA 492487-14.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 55,956 hrs · 41,667 cycles

CORROSION WAS FOUND ON THE VERTICAL WEB OF THE AFT CARGO LOWER BEAM. REPAIR IAW ERA 492505-14.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 55,956 hrs · 41,667 cycles

VERTICAL STAB LT SKATE ANGLE CRACKED AT FS 1474 LT. REPAIRED PER ERA 492522-14 REV O.

Part: SKIN — DENTED (BS 378) · airframe 55,956 hrs · 41,667 cycles

DURING A PSV VISIT WITH CPCP TWO DENTS WERE FOUND JUST BELOW THE FORWARD CARGO DOOR AT APPROX STA 378. REPAIRED PER ER/A 492529-14.

Part: SKATE ANGLE — CRACKED (VERTICAL SSTAB) · airframe 55,956 hrs · 41,667 cycles

VERTICAL STAB RT SKATE ANGLE CRACKED AT FS 1474. REPAIRED PER ERA 492525-14 REV O.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,959 hrs · 40,343 cycles

ON EMERGENCY LIGHTS TEST, FOUND EXTERNAL OVERWING EMERGENCY LIGHTS INOP. T/S PER WDM 33-51-11. FOUND BATTERY PACK BAD. REPLACED BATTERY RACK AND BATTERY PACK (2010-D0885) (DLM88101938).

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 53,889 hrs · 40,287 cycles

UPON LANDING NOSE GEAR WOULD NOT EXTEND. PULLED ALTERNATE GEAR EXTEND HANDLE AND NOSE GEAR EXTENDED NORMALLY. DECLARED EMERGENCY. JACKED A/C AND SWUNG GEAR. NLG RETRACTS NORMALLY BUT WILL NOT EXTEND WHEN GEAR LEVER IS PLACED DOWN. SUSPECT BUNGEE ACTUATOR. REPLACED NOSE GEAR SEVERAL TIMES EXTEND AND RETRACT NORMAL (DLM88101781).

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 53,723 hrs · 40,165 cycles

MX FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 12 AND 21 TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY AT ROW 21 AND RESEATED THE CONNECTOR AT SEAT 12. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE. (DLM88101583)

Part: LINKAGE — DISENGAGED (LANDING GEAR) · airframe 52,243 hrs · 39,153 cycles

GEAR DOORS REMAINED OPEN FOR LANDING AFTER GEAR EXTENSION. DOOR SKIDS REPLACED. EXT INSP REQ OF DOORS INTERNALLY. LINKAGE TO RT DOOR UP HOOK SECURED. A/C JACKED AND GEAR SWING C/W.

Part: ENGINE — STALLED (NR 1) · airframe 47,347 hrs · 36,050 cycles

LT ENGINE COMPRESSOR STALL AT FLT LEVEL 290, NO POWER EPR WOULD NOT INCREASE. ALL OTHER INDICATIONS NORMAL. REPLACED NR 1 ENG.

Part: APU — ODOR · airframe 45,209 hrs · 34,689 cycles

AFTER TAKEOFF EXPERIENCED SMOKE IN CABIN AND COCKPIT OIL SMELL, APU WAS OPERATING. REPLACED APU PER TRANS 9T103. PERFORMED PNEUMATIC DIST CABIN SMOKE ODOR TROUBLESHOOTING PER OPN 5088. PERFORMED DUCT BU OUT PER OPN 5089.

Part: COUPLING — DAMAGED (NR 4 BRAKE) · airframe 44,938 hrs · 34,495 cycles

ON TAXI IN, CREW FELT BRAKE LOCK UP. STOPPED AND CALLED FOR MAINTENANCE. UPON INSPECTION FOUND COUPLING ON NR 4 BRAKE DAMAGED. AIRCRAFT WAS TOWED TO BLAST FENCE AFTER THE BRAKE WAS BLEED. REPLACED COUPLING. OPERATED BRAKES, OPS CHKS NORMAL.

Part: UPLOCK SENSOR — FAILED (LT MLG) · airframe 42,514 hrs · 32,809 cycles

UPON GEAR RETRACTION LEFT GEAR UNSAFE. REPLACED UPLOCK PROX SENSOR.

Part: HYDRAULIC LINE — DAMAGED (TAIL COMPARTMENT) · airframe 42,513 hrs · 32,807 cycles

AFTER TAKEOFF DURING CLEAN UP NOTICED RT HYD SYS PRESS AND QTY AT ZERO. FOUND PRESSURE LINE TO HYDRAULIC CONTROL MODULE IN SECTION 48 RT SIDE DAMAGE. REMOVED AND REPLACED SAME, RAN RT ENGINE, LEAK CHECK OK.

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 41,368 hrs · 32,006 cycles

LEFT AFT LAV SMOKE DETECTOR ACTIVATED WITH SLIGHT ODOR PRESENT. REPAIRED HYDRAULIC LINE AT LEFT THRUST REVERSER CONTROL VALVE. PERFORMED DUCT BURNOUT PROCEDURE. CHECKS GOOD.

Part: O-RING — WORN (THRUST REVERSER) · airframe 41,120 hrs · 31,828 cycles

ON SHORT FINAL AFT LAV SMOKE DETECTORS WENT OFF WITH ASSOCIATED ELEC SMELL AFTER LANDING WITHIN 5 MINS, LOST LT HYD FLUID WITH ASSOCIATED LOW QTY LIGHTS. FOUND O-RING FOR LT HYD T/REV DEACTIVATION VLV LEAKING. REPLACED O-RING LEAK CKS NORM. TURNED ON ALL CABIN LIGHTS AND COFFEE DISPENSERS NO ELEC, SMELL NOTED. ENGINE RUN AND DUCT BURNOUT IN PROGRESS.

Part: CAP — LEAKING (APU OIL) · airframe 39,960 hrs · 30,980 cycles

BOTH AFT LAV SMOKE DETECTION WENT OFF IN FLIGHT. FOUND APU OIL LEAK AT CAP. REPLACED CAP/O-RING. CLEANED APU INLET AND PERFORMED A DUCT BURNOUT PER THE M/M.

Part: BATTERY PACK — OVERHEATED (EMERGENCY LIGHT) · airframe 37,248 hrs · 29,092 cycles

ON FINAL APPROACH TO ATL CREW REPORTING BURNING ODOR, AFT LEFT LAV SMOKE DETECTOR SOUNDING. FLIGHT CREW DONNED O2 MASKS. FOUND FORWARD EMERGENCY LIGHT BATTERY PACK OVERHEATING. REPLACED SAME.

Part: O-RING — CUT (NR 1 ENG OIL) · airframe 34,850 hrs · 27,429 cycles

LT ENGINE OIL QTY DECREASED TO ZERO IN FLIGHT. OTHER ENGINE INDICATIONS NORMAL. REPLACED CUT O-RING ON OIL TRANSFER TUBE.

Part: ENGINE — LEAKING (NR 1) · airframe 34,850 hrs · 27,429 cycles

INBOUND CREW REPORTS OIL FUMES IN CABIN. FOUND OIL LEAK ON NR 1 ENGINE. REPAIRED SAME

Part: ENGINE — LEAKING (NR 1) · airframe 34,847 hrs · 27,427 cycles

ON CLIMB OUT, SMOKE VISIBLE WITH SMOKE DETECTORS AUDIBLE IN CABIN AT FL 230. PACKS NORMAL TEMPS. FOUND INTERNAL OIL LEAK ON NUMBER 1 ENGINE - REPLACED SAME.

Part: SWITCH — DIRTY (PEDESTAL) · airframe 32,876 hrs · 26,016 cycles

CLEARED FOR T/O WHEN WE GOT AUTOBRK T/O WARNING.WE ABORTEDT/O AND CONTACTED ATL MCC.WE RTN TO GATE--NO SPEED NOTED- NEVER GOT ABOVE 20KTS. CLEANED RTO SWITCHES AT SPEEDBRAKE HANDLE.AURAL WARNING NOW CKS OK.

Part: BATTERY — DISCHARGED (FWD GALLEY) · airframe 29,366 hrs · 23,456 cycles

BATTERY PACK ON EMERGENCY FLASHLIGHT FOUND LOW. REPLACED BATTERY, REF M/M.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 28,104 hrs · 22,498 cycles

PASSING 19K FT ALL O2 MASKS ON CO-PILOTS SIDE AND LEFT SIDE AFT OF AFT GALLEY, IN LAVS AND AFT JUMP SEAT PRESENTED. NO COCKPIT LIGHTS, CABIN ALTITUDE 6K, DIF PRESS 2.5, CABIN RATE OF CLIMB 300 FPM. ALL PANELS WERE RESET. REPAIRED WIRING AT S3-374 AND SECURED SAME. WIRES WERE FOUND BURNED THROUGH. ALL REPAIRED PER WDM. PERFORMING OPERATIONAL CHECK OF PASSENGER O2 SYSTEM. NTSB NOTIFIED.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 27,843 hrs · 22,300 cycles

EN ROUTE NR 1 THROTTLE WAS BINDING AT HIGH PWR SETTINGS. WOULD NOT MOVE UNLESS AUTO THROTTLE OFF. WHEN THROTTLE WAS RETARDED CONTROL LEVER MOVED PARALLEL HAD TO SHUT DOWN ENG WITH FIRE HANDLE AT GATE. FUEL LEVER FROZE IN ON POSITION. REPLACED FUEL SHUTOFF AND THROTTLE TELEFLEX CABLES DUE TO NR 1 ENG RT INLET GUIDE VANE ANTI-ICE DUCT BLOWN CAUSING TELEFLEX CABLES TO STIFFEN.

Part: ENGINE — BIRD STRIKE (NR 1)

FLT ATTENDANT REPORTED LOUD NOISE AND VIBRATION AFTER T/O. AT FL 260 NR 1 ENG COMPRESSOR STALLED. FOUND BIRD REMAINS IN NR 1 ENG INLET AND FOD DAMAGE. REPLACED ENGINE.

Part: APU — MALFUNCTIONED (APU COMPT)

EMERGENCY RETURN TO ATL FOR SMOKE IN CABIN. HEAVY WT LANDING 134.8 SMOOTH AND LESS THAN 360 FPM SINK RATE. FOUND OIL IN APU INLET. REPLACED APU, CHECKS NORMAL.

Part: HEATER — SMOKING (CARGO COMPT)

SMOKE IN CABIN. DIVERTED TO JAN. REPLACED FORWARD CARGO HEATER.

Part: CONTROL VALVE — MALFUNCTIONED (RT MLG WW)

AUTO BRAKES SLOW TO ENGAGE ON LANDING, AND RT BRAKE PEDAL WENT TO THE FLOOR WHE N AUTO BRAKES DISENGAGED. NO ANTI-SKID MESSAGE AND NO YAW. REPLACED NR 3 AND NR 4 ANTI-SKID CONTROL VALVES. NO LEAKS, AND NO DISCREPENCIES IN AUTO BRAKE SYSTEM. ALSO, REPLACED NR 3 AND NR 4 MAIN WHEEL ASSYS, DUE TO TIRES BOTH GROUND COMPLETELY DOWN TO THE NITROGEN.

Part: HOSE — RUPTURED (LEFT)

LT HYD PRESS DROPPED TO ZERO PSI AND LT HYD QTY DROPPED TO 2 QTS AFTER T/O. FOUND SUPPLY HOSE TO LT PRESS FILTER MODULE RUPTURED. REPLACED SAME.

Part: TURBINE — FAILED (RT ACM)

AIRCRAFT WOULD NOT MAINTAIN PRESSURE AT FL 250. DIVERTED TO ATL. REPLACED RIGHT ACM, OPERATION NORMAL.

Part: NOSE COWL — DAMAGED (NR 2 ENGINE)

NOSE COWL ACOUSTIC LINER DELAMINATED AT 6:OO POSITION. ALSO SKIN ERODED AROUND AIR SCOOP, REPAIRED PER SRM 54-06, DURING SHOP VISIT.

Part: SKIN — LIGHTNING STRIKE (FS 1338/1380)

FOUND DURING E-2 LETTER CHECK, TWO LIGHTNING STRIKES AT FS 1338 AND 1380 RT SIDE ABOVE NR 2 ENG PYLON. REPLACED DAMAGED FASTENERS PER SRM 53-04 FIG 38.

Part: SKIN — CRACKED (FWD FUSELAGE)

FOUND DURING E-2 LETTER CHECK, .375 INCH CRACK IN FUSELAGE SKIN AT AFT HINGE CUTOUT FOR RNLG DOOR. REPAIRED PER SRM 53-05 FIG 62A.