N805NN

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 47,850 hrs · 20,180 cycles

AIRCRAFT WAS NOT GROUNDED: EXTERIOR EMERGENCY LIGHT INOPERATIVE BEHIND LEFT AFT OVERWING EMERGENCYEXIT. CHECKED LIGHT TERMINALS FOR VOLTAGE PER WDM 33-51-13, NO VOLTAGE PRESENT. REMOVED AND REPLACED POWER SUPPLY (M1670). PER AMM 33-51-04. OPERATIONAL CHECK GOOD.

Part: SOCKET — INOPERATIVE (ZONE 200) · airframe 47,850 hrs · 20,180 cycles

AIRCRAFT WAS NOT GROUNDED: EXTERIOR EMERGENCY LIGHT INOPERATIVE BEHIND LEFT AFT OVERWING EMERGENCY EXIT. R & R SOCKET AND CONTACT AT EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04, NO FIX. CHECKED LIGHT TERMINALS FOR VOLTAGE PER WDM 33-51-13, NO VOLTAGE PRESENT. FURTHER TROUBLESHOOTING REQUIRED. (OPEN).

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 47,835 hrs · 20,171 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED LEFT AFT REAR LAVATORY-D DOOR IS DIFFICULT TO OPEN. LUBRICANTED LAVATORY-D AS REQUIRED, OPERATIONAL CHECKED GOOD.

Part: TRACK — LACK OF LUBE (ZONE 800) · airframe 47,835 hrs · 20,171 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISES LEFT AFT LAVATORY-D HAS DIFFICULTY OPENING. APPEARS TO BE STICKING AT THE TOP OF THE DOOR TRACK. CLEANED TRACK AND LUBED TRACK FOR LAVATORY-D. PER AMM 25-40-00.

Part: PUMP — FAILED (ZONE 400) · airframe 47,587 hrs · 20,053 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT 37K FEET OVER CUBA, NUMBER 1 ENGINE ROLLED BACK TO 40-50% N1. AUTO THROTTLES DISENGAGED. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REMOVED AND REPLACED (HMU)-HYDROMECHANICAL UNIT LEFT HAND ENGINE (AALA202508222533), PER W/C 08L40073001. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL PUMP PACKAGE (AALA202508221159), PER AMM 73-11-01. ACCOMPLISHED LEFT HAND ENGINE CHIP DETECTOR INSPECTION, PER W/C 08T40079001. ALL OPERATIONAL CHECK NORMAL. NO LEAKS NOTED.

Part: HMU — FAILED (ZONE 400) · airframe 47,587 hrs · 20,053 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT 37K FEET OVER CUBA, NUMBER 1 ENGINE ROLLED BACK TO 40-50% N1. AUTO THROTTLES DISENGAGED. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REMOVED AND REPLACED (HMU)-HYDROMECHANICAL UNIT LEFT HAND ENGINE (AALA202508222533), PER W/C 08L40073001. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL PUMP PACKAGE (AALA202508221159), PER AMM 73-11-01. ACCOMPLISHED LEFT HAND ENGINE CHIP DETECTOR INSPECTION, PER W/C 08T40079001. ALL OPERATIONAL CHECK NORMAL. NO LEAKS NOTED.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 47,535 hrs · 20,024 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY-D (AALA202508165377) AND LAVATORY-E (AALA202508160396) DOORS ARE HARD TO OPEN AND CLOSE. LUBED LAVATORY DOOR TRACKS. OPERATIONAL CHECK GOOD.

Part: DOOR — LACK OF LUBE (ZONE 900) · airframe 47,535 hrs · 20,024 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY-D (AALA202508165377) AND LAVATORY-E (AALA202508160396) DOORS ARE HARD TO OPEN AND CLOSE. LUBED LAVATORY DOOR TRACKS. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 45,126 hrs · 18,903 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR GRIT BAR COLLAR/FITTING REPORTED LOOSE ON THE RIGHT SIDE OF BAR. RESECURED L1 DOOR GIRT BAR COLLAR RETAINING CLIP. PER AMM 25-66-01.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 44,967 hrs · 18,827 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE CENTER SUPPORT AT STA 500I, LBL 24. REPLACED SUPPORT PER SRM 51-40-02-0G.

Part: TRIM MOTOR — OUT OF TOLERANCE (ZONE 300) · airframe 44,591 hrs · 18,645 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AFTER TAKEOFF LOST STAB TRIM, NON OPERATIONAL WITH NO AUTOPILOT; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CLT. PARTIAL WORK ACCOMPLISHED. TROUBLESHOT PER TSM 27-41-00-810-804. FOUND VOLTAGE OF PINS ON STAB TRIM MOTOR OUT OF LIMITS. REMOVE AND REPLACED STAB TRIM MOTOR. OPERTIONAL CHECK GOOD. PER AMM 27-41-71.

Part: OVEN — SMOKE (FWD GALLEY) · airframe 44,292 hrs · 18,498 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: SMOKE HOT SMELL CLIMBING THROUGH 32000. SMELL IN FLIGHT DECK AND FIRST CLASS; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT AUS. FOUND BOTH FORWARD GALLEY OVENS PRODUCING ODORS WHILE OPERATING. REMOVE AND REPLACED FORWARD GALLEY OVENS 1 (AALA202406146203) AND 2 (AALA202406148779), OPERTIONAL CHECK GOOD. PER AMM 25-32-03-400-801.

Part: OVEN — SMOKE (FWD GALLEY) · airframe 44,292 hrs · 18,498 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: SMOKE HOT SMELL CLIMBING THROUGH 32000. SMELL IN FLIGHT DECK AND FIRST CLASS; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT AUS. FOUND BOTH FORWARD GALLEY OVENS PRODUCING ODORS WHILE OPERATING. REMOVE AND REPLACED FORWARD GALLEY OVENS 1 (AALA202406146203) AND 2 (AALA202406148779), OPERTIONAL CHECK GOOD. PER AMM 25-32-03-400-801.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 43,779 hrs · 18,236 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOGHOUSE FLASHLIGHT APPEARS TO BE DISCHARGED. REPLACED THE BATTERY PACK ON THE FORWARD LEFT FLIGHT ATTENDANT SEAT. PER AMM 25-64-00.

Part: DOOR — STUCK (LAVATORY) · airframe 43,387 hrs · 18,065 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY DOOR STUCK. PUT DOOR BACK IN TRACK.

Part: HINGE — LOOSE (ZONE 900 - LAV/G) · airframe 43,096 hrs · 17,926 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR HINGE IS LOOSE. REATTACHED LEFT AFT LAVATORY DOOR HINGE PER CMM.

Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 42,401 hrs · 17,594 cycles

AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT WON'T TEST. REPLACED FLASHLIGHT. PER JOB CARD 08C00005024.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 41,750 hrs · 17,255 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED LAMP PER AMM 33-51-04. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (ZONE 800 - DOORS) · airframe 41,288 hrs · 17,021 cycles

AIRCRAFT WAS NOT GROUNDED: LIGHT BULBS NEED REPLACING AT EMERGENCY EXIT LIGHT. RELAMPED EMERGENCY EXIT LIGHT.THIS SDR WAS SUBMITTED VIA EMAIL UNDER FAA OPERATOR CONTROL NUMBER: AALA202305246691

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 37,677 hrs · 15,323 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE LOOSE. SECURED FORWARD LAVATORY FASTENER DOOR HANDLE PER MAINTENANCE PRACTICES.

Part: SHADE — DAMAGED (ZONE 800 - DOORS) · airframe 37,287 hrs · 15,133 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN WINDOW SHADE DAMAGED AT EMERGENCY EXIT SEAT 16A. **SUPPLEMENTAL REPORT: REPLACED CABIN WINDOW SHADE WITH NEW AT SEAT 16A IAW AMM 25-21-12, OPS CHECK GOOD.** (CLOSED)

Part: NONE — NONE · airframe 37,287 hrs · 15,133 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN WINDOW SHADES DAMAGED AT EMERGENCY EXIT SEATS 16A & 17A. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: SUPPORT ANGLE — CRACKED (BS 663 RBL 13) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN UPPER SUPPORT ANGLE OUTBD OF KEEL BEAM AT STA 663.75 AND RBL 13, MEASURING L=0.5 IN, W=0.001 IN, D=0.071 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 57-10-10 AND EA 329337.

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: TEMPORARY REPAIR IN PRESSURE DECK SKIN AT STA 663 BETWEEN RBL 40 AND RBL 45, MEASURING L=26.0 IN, W=14.0 IN, D=0.05 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 57-10-10-2R-3.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SKIN OF LOWER RH STABILIZER AT RH STAB STA 101 AND 11 IN FWD OF REAR SPAR, MEASURING L=0.75 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-R2-8.

Part: WINDOW FRAME — DAMAGED (BS 217) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: REINFORCING MODIFICATION NEEDS TO BE INSTALLED ON RIGHT SIDE OF FIRST OFFICERS #1 OUTBOARD WINDOW FRAME. INSTALLED EXTERNAL DOUBLER REINFORCING MODIFICATION REF ECO 5319J023-008.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT SIDE CAPTAIN'S OUTBOARD WINDOW POST 1 HAS 3/4 INCH CRACK. INSTALLED EXTERNAL DOUBLER/TRIPLER REPAIR.

Part: ANGLE — CRACKED (BS 500G-500H) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD LEFT HAND CARGO AREA CRACKED BAFFLE CLIP LOCATED BETWEEN STA 500G AND 500H AT S27L. REPLACED BAFFLE CLIP PER AARD-51-00-05-1.

Part: ANGLE — CRACKED (BS 500G S27R) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD RIGHT HAND CARGO AREA CRACKED BAFFLE CLIP LOCATED AT STA 500G AT S27R. REPLACED BAFFLE CLIP PER SRM 53-30-53-01 AARD 51-40-05.

Part: BAFFLE — CRACKED (BS 500G S27L) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP CRACKED AT STR 27L AND 500G. REMOVED AND REPLACED BAFFLE CLIP REF BOEING DRAWING #143A7505-SHEET 108-110, SRM 53-30-53-01, AND AARD 51-40-05.

Part: BAFFLE — CRACKED (BS 500H S27R) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP CRACKED AT STA 500H AND STR 27R. REMOVED AND REPLACED BAFFLE CLIP REF DRAWING #143A7505-SHEET 108-110, SRM 53-30-53-01 AND AARD 51-40-05.

Part: BAFFLE — CRACKED (BS 500H S27L) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK ON BAFFLE CLIP LOCATED AT STA 500H AND STR 27L. REMOVED AND REPLACED BAFFLE CLIP PER BOEING DRAWING 142A7505/AA.

Part: BAFFLE — CRACKED (BS 500F S27R) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON BAFFLE CLIP LOCATED AT STA 500F, STR 27 R. REMOVED AND REPLACED BAFFLE CLIP PER BOEING DRAWING 143A7505.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STIFFENERS OF RH HORIZONTAL STABILIZER RIB AT RH HSTAB STA 92.7 AND 12" AFT, MEASURING L=1.25 IN, W=0.25 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-09-R2-4.

Part: STRUCTURE — CRACKED (BS 540 RBL35-45) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: BRAKE ASSEMBLY CRACKED AT STA 540, RIGHT BUTT LINE 35 TO RIGHT BUTT LINE 45. REMOVED AND REPLACED BRAKE ASSEMBLY PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL LOCATED AT STA 325 AND LBL 45. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: SHEAR WEB — CORRODED (BS 992 RBL 31) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF SHEAR WEB AT STA 992 AND RBL 31, MEASURING L=1.0 IN, W=1.0 IN, D=0.009 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW EA 329311.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL LOCATED AT STA 285 AND RBL 1. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: WEB — CORRODED (BS 986 LBL43) · corrosion level 2 · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB LOCATED AT STA 986.5 AND LBL 43. REPAIRED PER EA 329366.

Part: FLOORBEAM — CORRODED (BS 986 LBL44) · corrosion level 2 · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM LOCATED AT STA 986.5 AND LBL 44, MEASURING L=1.50 IN, W=1.00 IN, D=0.023 IN. REPAIRED PER SRM 53-70-51 AND EA 329364.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK WAS FOUND AROUND SCREW HOLE OF INTERCOSTAL LOCATED AT STA 325, WATERLINE 0 AND BUTTLNE 32. INSTALLED NEW INTERCOSTAL WITH FAYING SURFACE SEALANT AND WET FASTENERS PER AMM 51-31-00 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF T-CAP ON FLOORBEAM AT STA 986 BETWEEN RBL 32 AND RBL 45, MEASURING L=3.0 IN, W=1.5 IN, D=0.09 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR WITH NESTED ANGLES IAW EA 329294.

Part: TRANSITION PANEL — CORRODED (BS 727G S27) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO LEFT TRANSITION PANEL HAS CORROSION AT STA 727G AND STR 27. REMOVED AND REPLACED AFT CARGO LEFT TRANSITION PANEL REF SRM 51-10-02.

Part: ANGLE — CORRODED (BS 947-995 S17L) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF CREASE ANGLE AT 2L DOOR BETWEEN STA 947.5 AND STA 997 AT STR 17L, MEASURING L=1.8 IN, W=3.4 IN, D=0.022 IN. REPLACED ANGLE WITH NEW IAW SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (AFT CARGO) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO LEFT TRANSITION PANEL CORRODED. REMOVED AND REPLACED CORRODED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 727E-767 S27) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON TRANSITION PANEL LOCATED AT 727E + 10 TO 767 AND STR 27. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: MOUNT — CORRODED (BS 987 LBL 43) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY 4 MOUNT LOCATED AT STA 986.5 AND LBL 43. REPAIRED PER SRM 53-70-51-2R

Part: FLOORBEAM — CORRODED (BS 947 LBL 52-57) · corrosion level 2 · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT STA 947 BETWEEN LBL 52 AND LBL 57, MEASURING L=4.375 IN, W=2.187 IN, D=0.092 IN. REPLACED T-CAP IAW SRM 53-70-51-2R-1.

Part: TRANSITION PANEL — CORRODED (BS 490-500L S27L) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO AREA LEFT TRANSITION PANEL LOCATED BETWEEN STA 490 AND 500L AT S27L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: TRANSITION PANEL — CORRODED (BS 500C-500I) · airframe 36,163 hrs · 14,595 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO RIGHT TRANSITION PANEL HAS CORROSION AT STA 500C AND 500I. REMOVED AND REPLACED RIGHT TRANSITION PANEL IAW SRM 51-40-02.

Part: LATCH — DIRTY (LAVATORY DOOR) · airframe 36,156 hrs · 14,591 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAV DOOR LATCH DIFFICULT TO OPERATE. CLEANED AND LUBED THE LATCH OF LEFT AFT LAVATORY DOOR.

Part: GIRT BAR — STICKING (L1 DOOR) · airframe 36,043 hrs · 14,541 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L GIRT BAR EXTREMELY DIFFICULT TO UNHINGE FROM HOLDER. PERFORMED ADJUSTMENT DOOR 1L GIRT BAR HOLDER AS REQUIRED.

Part: BRACKET — LOOSE (L1 DOOR GIRT BAR) · airframe 36,036 hrs · 14,537 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR BRACKET THAT HOLDS GIRT BAR LOOSE. ADJUSTED BRACKET.

Part: RECEIVER — FAILED (WX RADAR SYS) · airframe 35,795 hrs · 14,430 cycles

AIRCRAFT WAS GROUNDED: WEATHER RADAR FAILED IN FLIGHT, FLIGHT DIVERTED TO OKC AND LANDED WITHOUT FURTHER INCIDENT. REPLACED WEATHER RADAR RECEIVER/TRANSMITTER IAW AMM 34-43-41, OPS CHECK GOOD.

Part: SENSE LINE — LOOSE (LT ENGINE) · airframe 34,094 hrs · 13,701 cycles

AIRCRAFT WAS NOT GROUNDED. RETURN TO GATE. LEFT ENGINE N1 TAKEOFF, REF 93.0 RT ENGINE N1 93.7 A/C SYSTEM RUNS HOT. SUPPLEMENTAL REPORT: SECURED LOOSE SENSE LINE ON RIGHT FLOW CONTROL AND SHUTOFF VALVE AND OPERATIONAL CHECK GOOD, PER AMM 21-51-01.

Part: ACTUATOR — DEFECTIVE (RAM AIR INLET) · airframe 33,989 hrs · 13,653 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTS: FMC N1 T/O SPLIT24/35 RIGHT 95.6 LEFT 96.5, RIGHT HAND PACK NOT COMMING ON AND A SPLIT BETWEEN THE LEFT HAND AND RIGHT HAND ENGINES. AIRCRAFT RETURNED TO GATE. REPLACED RIGHT PACK RAM AIR INLET DOOR ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-52-21

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 33,934 hrs · 13,628 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PRESSURE DECK OF OF RH UPPER WHEEL WELL AT STA 663 BETWEEN RBL 40 AND RBL 45, MEASURING L=0.6 IN, W=0.3 IN, D=0.4 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 57-10-10-2R-3.

Part: ENGINE — POWER LOSS (NR 1) · airframe 32,936 hrs · 13,198 cycles

AIRCRAFT WAS GROUNDED: ABORTED TAKE OFF AT APPROX. 85 KNOTS NO.1 ENGINE N1 AT 91.5, NO.2 AT 96.5. TAKE OFF POWER THROTTLES WERE,ALIGNED. NO.1 ENGINE WOULD NOT REACH TAKE OFF POWER. ACCOMPLISHED SIC # 05-96-17, HIGH ENERGY RTO.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 32,374 hrs · 12,942 cycles

AIRCRAFT WAS NOT GROUNDED: DURING TEST OF EMERGENCY LIGHTS PER JOB CARD 2904, FOUND FORWARD GALLEY AND L1 DOOR LIGHTS WOULD NOT RESET. MAINTENANCE REPLACED BATTERY CHARGER PACK PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 28,608 hrs · 11,237 cycles

WHILE ACCOMPLISHING WORKCARD 2908, EMERGENCY LIGHTS ON SEATS 13-15, RIGHT FOWARD AND AFT OVERWING EXIT SIGNS, CENTER ISLE EXIT SIGN AND LIGHT AND RIGHT AFT OVERWING EXIT SIGNS ON THE WALL WERE INOPERATIVE AFTER 15 MINUTES. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-06 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FABRIC — LOOSE (R1 DOOR SLIDE) · airframe 26,849 hrs · 10,461 cycles

R1 DOOR SLIDE HAS CLOTH HANGING DOWN WHEN GIRT BAR IS DOWN. RESET LOOSE SLIDE FABRIC. OK FOR SERVICE IAW MM 25-94-10.

Part: LENS — MISSING (CABIN) · airframe 26,823 hrs · 10,447 cycles

AIRCRAFT NOT GROUNDED. LIGHT CLEAR LENS COVER MISSING AT DOOR 4L AREA. REPLACED LIGHT LENS COVER AT DOOR 4L PER AMM 33-26-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,549 hrs · 10,322 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY THE R2 DOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-14. OPERATIONAL CHECK GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 25,805 hrs · 10,015 cycles

EMERGENCY EXIT LIGHT BY THE FORWARD SERVICE DOOR HAS AN UNSECURE LENS. SECURED THE LENS IAW AMM 33-20-00. OPERATIONAL CHECKED GOOD.

Part: GCU — FAULTY (NR 2) · airframe 23,346 hrs · 9,007 cycles

AIRCRAFT WAS GROUNDED. PBI, AIR INTERRUPT, MIA-PHL. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING FLIGHT THE NR 2 GENERATOR SOURCE LIGHT ILLUMINATED WITH THE APU INOPERABLE. MAINTENANCE REMOVED AND REPLACE THE NR 2 GENERATOR CONTROL UNIT IAW AMM 24-21-81 AND NR 2 INTEGRATED DRIVE GENERATOR IAW AMM 24-11-11. OPERATIONAL AND LEAK CHECKS NORMAL IAW AMM 71-00-00. SEE ALSO AALA20161107031.

Part: IDG — FAULTY (NR 2) · airframe 23,346 hrs · 9,007 cycles

AIRCRAFT WAS GROUNDED. PBI, AIR INTERRUPT, MIA-PHL. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING FLIGHT THE NR 2 GENERATOR SOURCE LIGHT ILLUMINATED WITH THE APU INOPERABLE. MAINTENANCE REMOVED AND REPLACE THE NR 2 GENERATOR CONTROL UNIT IAW AMM 24-21-81 AND NR 2 INTEGRATED DRIVE GENERATOR IAW AMM 24-11-11. OPERATIONAL AND LEAK CHECKS NORMAL IAW AMM 71-00-00. SEE ALSO AALA20161106006.

Part: BRAKE ASSY — FAULTY (MLG) · airframe 21,830 hrs · 84,399 cycles

AIRCRAFT WAS GNDED. DURING POST LANDING WALK AROUND THE NR 3 & 4 WHEEL FUSIBLE PLUGS BLEW. A FIRE WAS ALSO REPORTED WHICH WAS EXTINGUISHED. POST EVENT INSPECTION FOUND LARGE AMOUNTS OF METAL SHAVINGS ON THE NR 3 & 4 BRAKE ASSEMBLIES. R & R NR 3 & 4 BRAKE ASSEMBLIES IAW AMM 32-41-41. SYS CHECKED NORMAL. SEE ALSO AALA 20160516015.

Part: BRAKE ASSY — FAULTY (MLG) · airframe 21,830 hrs · 8,399 cycles

AIRCRAFT WAS GNDED. DURING POST LANDING MX WALK AROUND THE NR 3 & 4 WHEEL FUSIBLE PLUGS BLEW. A FIRE WAS ALSO REPORT WHICH WAS EXTINGUISHED. POST EVENT INSPECTION FOUND LARGE AMOUNTS OF METAL SHAVINGS ON THE NR 3 & 4 BRAKE ASSEMBLIES. R & R NR 3 & 4 BRAKE ASSEMBLIES IAW AMM 32-41-41. SYS CHECKED NORMAL. SEE ALSO AALA 20160518007.

Part: SUPPORT BEAM — WORN (FUSELAGE) · airframe 19,404 hrs · 7,453 cycles

CENTER WING SUPPORT BEAM HAS A WORN AREA, FROM PNEUMATIC GND AIR ACCESS DOOR LATCH AT STATION 540 & RBL 26. ACCOMPLISHED STRAP REPAIR IAW EA 253772 DATED 8 25 15.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,404 hrs · 7,453 cycles

CRACK INDICATION ON AFT OUTBOARD HOLE IN FWD SEAT TRACK AT STATION 727B & RBL 45.50. INSTALLED SPLICE STRAP REPAIR IAW EA 253719, DATED 8 23 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,404 hrs · 7,453 cycles

CRACK INDICATION ON AFT OTBD HOLE IN FWD SEAT TRACK AT STATION 727B & LBL 45.50. INSTALLED SPLICE STRAP REPAIR IAW EA 253719, DATED 8 23 2015.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 19,404 hrs · 7,453 cycles

AFT CARGO COMPARTMENT LT TRANSITION Z PANEL IS CORRODED OUT OF LIMITS IN SEVERAL AREA BETWEEN STATIONS 727I & 827. INSTALLED SPLICE REPAIR IAW SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 19,404 hrs · 7,453 cycles

AFT CARGO COMPARTMENT RT TRANSITION Z PANEL IS CORRODED BETWEEN STATIONS 727E & 767. INSTALLED SPLICE REPAIR IAW SRM 53-00-53-2R-5.

Part: SENSOR — DEFECTIVE (ZONE 200) · airframe 17,386 hrs · 6,684 cycles

AIR INTERRUPT & RETURNED. AIRSPEED INDICATION ON CAPTAINS PRIMARY FLIGHT DISPLAY WENT BLANK THEN RETURNED MULTIPLE TIMES. TROUBLE SHOT SYS IAW FIM 34-21-00 & FOUND BAD LT ANGLE OF ATTACH SENSOR. R & R SENSOR IAW AMM 34-21-05. SYS CHECKED NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,456 hrs · 6,319 cycles

NUMBER 1 WINDOW ARCED THEN OUTER PANE CRACKED. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 WINDOW. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: COVER — BROKEN (CABIN) · airframe 6,639 hrs · 2,432 cycles

RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REPLACE LIGHT ASSEMBLY FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT.

Part: FIRE LOOP — SHORTED (RT MLG WW) · airframe 963 hrs · 375 cycles

MIA - CAPTAIN REPORTED THAT THE RIGHT WHEEL WELL FIRE INDICATION ILLUMINATED. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED SERVICE. FOUND WHEEL WELL FIRE LOOP M270 SHORTED. REMOVED AND REPLACED M270 FIRE LOOP. SYSTEM GROUND CHECK NORMAL OPERATION.