N919NN

Part: GIRT BAR — STUCK (ZONE 800) · airframe 37,228 hrs · 16,124 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD ENTRY DOOR GIRT BAR STUCK, VERY TIGHT IN THE HOLDER. INSPECTED SLIDE AND GIRT BAR AND FOUND SLIDE FABRIC STUFFED IN GIRT BAR HOLDER, FREED UP SLIDE FABRIC. PER AMM 52-11-00.

Part: GIRT BAR — JAMMED (ZONE 800) · airframe 36,915 hrs · 15,974 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD RIGHT DOOR GIRT BAR JAMMED WILL NOT ARM. REMOVED JAM ON FORWARD RIGHT DOOR. OPERATIONAL CHECK GOOD. PER AMM 52-11-00.

Part: DOOR LATCH — BROKEN (ZONE 900) · airframe 35,565 hrs · 15,351 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS TOTALLY DISMANTLED AS A RESULT WHEN LAVATORY OCCUPANTS TRY TO USE IT THEY GET STUCK INSIDE THE LAVATORY. REMOVED AND REPLACED FORWARD LAVATORY DOOR HANDLE. PER CMM 25-48-48.

Part: FLASHLIGHT — NOT SEATED (ZONE 200) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT OUTBOARD EMERGENCY FLASHLIGHT DOES NOT TEST UNDER AFT LEFT FLIGHT ATTENDANT SEAT. PROPERLY RESEATED EMERGENCY FLASHLIGHT IN THE BRACKET ON THE LEFT OUTBOARD AFT FLIGHT ATTENDANT SEAT, OPERTIONAL CHECK GOOD. PER AMM 25-64-00.

Part: BOTTLE — OVERPRESSURED (ZONE 200) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT WAS NOT GROUNDED: NUMBER 4 LIFE RAFT HAS AN OVER PRESSURIZED BOTTLE. REMOVE AND REPLACED LIFE RAFT.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE AT STA 500E, LBL 25. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500E, RBL 25. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500E, LBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE BAFFLE CLIP AT BS 500H, LBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT ANGLE BETWEEN BS 387 AND BS 394 AT LBL 13. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY AT BS 540, RBL2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY AT BS 540, LBL2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED FROM STA 500H TO STA 500I AT RBL 25. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT AFT SIDE OF STA 500H, AT RBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT FORWARD SIDE OF STA 500H, AT RBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT FORWARD SIDE OF STA 500H, AT LBL 25. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN BS 947 AND BS 957 AT LBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500H TO STA 500I AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500A TO STA 500B AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500D TO STA 500E AT LBL 25. REPAIRED TRANSITION PANEL SRM 53-00-53-2R-5 AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500F TO STA 500G AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500E TO STA 500F AT LBL 25. REPAIRED TRANSITION PANEL SRM 53-00-53-2R-5 AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500C TO STA 500D AT RBL 26. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500F TO STA 500G AT LBL 25. REPAIRED TRANSITION PANEL SRM 53-00-53-2R-5 AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500E TO STA 500F AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500G TO STA 500H AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500C TO STA 500D AT LBL 25. REPAIRED TRANSITION PANEL SRM 53-00-53-2R-5 AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500D TO STA 500E AT RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN BS 770 AND BS 778 AT RBL 25. REPLACED SHIELD PER AARD 51-0-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500A TO STA 500B AT LBL 25. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R AND AARD 51-00-05-1.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT BS 500I FROM RBL 25 TO LBL 25. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

**SUPPLEMENTAL REPORT FOR AALA202503127151: QC REVIEWED THIS EVENT AND DETERMINED THAT THE CORROSION LEVEL SHOULD BE 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY.** AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500A TO STA 500B AT LBL 25. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,156 hrs · 15,173 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 500B TO STA 500C AT LBL 25. REPAIRED TRANSITION PANEL SRM 53-00-53-2R-5 AND AARD 51-00-05-1.

Part: THRESHOLD — OUT OF ADJUST (ZONE 200) · airframe 33,806 hrs · 14,536 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR HARD TO OPEN AND CLOSE. LAVATORY-D DOOR LOWER THERSHOLD CONTACTING LAVATORY DOOR. MADE ADJUSTMENTS TO LOWER THRESHOLD. PER AARD 20-00-00-1.

Part: DOOR — OUT OF ADJUST (ZONE 900) · airframe 32,839 hrs · 14,044 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS HARD TO OPEN. ADJUSTED FORWARD LAVATORY DOOR TRIM. PER AMM 25-40-00. OPERTIONAL CHECK NORMAL.

Part: TRIM PANEL — LOOSE (LAVATORY DOOR) · airframe 32,150 hrs · 13,726 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. RESECURED LAVATORY DOOR LOOSE TRIM

Part: HINGE — MISSING (ZONE 800 - DOORS) · airframe 13,419 hrs · 31,497 cycles

AIRCRAFT WAS GROUNDED: FORWARD ENTRY DOOR IS MISSING RETAINING PIN ON THE GUST LOCK ASSEMBLY. FORWARD ENTRY DOOR WILL NOT CLOSE. REPLACED L1 DOOR HINGE, OPERATIONAL CHECKS GOOD. PER AARD 52-10-00-4 REPAIR 4.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 31,439 hrs · 13,391 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY D DOOR OFF TRACK, HARD TO OPEN AND CLOSE. RESECURED LAVATORY D DOOR ONTO TRACK PER AMM 25-40-14.

Part: MOUNT — BINDING (AFT LAV DOOR) · airframe 28,970 hrs · 12,174 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR DIFFICULT TO OPEN. ADJUSTED DOOR TO HINGE MOUNTS.

Part: WINDSHIELD — DELAMINATED (ZONE 200 - FUSE) · airframe 27,474 hrs · 11,459 cycles

AIRCRAFT IN BASE MAINTENANCE: COCKPIT CAPTAIN'S # 1 WINDSHIELD HAS OVERHEAT AND DELAMINATION MARKS NEAR THE UPPER BUS BARS. CAPTAINS #1 WINDSHIELD REPLACED PER AMM 56-11-11.

Part: SLIDE — OUT OF POSITION (ZONE 800 - DOORS) · airframe 26,021 hrs · 10,817 cycles

AIRCRAFT WAS GROUNDED: AFT SERVICE DOOR SLIDE COMING OUT OF STORAGE POUCH. RE-ATTATCHED DOOR SLIDE INTO SLIDE PACK "Z" FOLD VELCRO.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 24,657 hrs · 10,187 cycles

AIRCRAFT WAS GROUNDED: MID CABIN EMERGENCY EXIT SIGN (OVERWING) NEEDS TO BE INSTALLED. REINSTALLED THE MID CABIN EXIT SIGN FOR OVERWING IN REFERENCE WITH AMM 33-51-01.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 24,657 hrs · 10,187 cycles

AIRCRAFT WAS GROUNDED: MID CABIN EXIT LOCATOR SIGN BLUE CONNECTOR D15242 BROKEN. MANUFACTURER PART NUMBER IS AMC02PA03B. REPLACED MID CABIN EXIT LOCATOR SIGN BLUE CONNECTOR D15242 PER SWPM 20-61-28 LIGHT OPERATIONS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 23,660 hrs · 9,752 cycles

AIRCRAFT WAS NOT GROUNDED. RT AFT LAVATORY SMOKE LIGHT ILLUMINATED IN COCKPIT. PASSENGER IN LAVATORY AT THE TIME, FLIGHT ATTENDANTS VERIFIED NO SMOKE AND NO EVIDENCE OF VAPING OR SMOKING. ACCOMPLISHED LAVATORY SMOKE DETECTOR TEST, IAW AMM 26-14-00. OPERATIONS CHECK GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,904 hrs · 9,424 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT LEFT HAND INBOARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY FROM THE AFT LEFT HAND INBOARD FLIGHT ATTENDANT FLASHLIGHT INSTALLED TEMPER SHIELD OPERATIONS CHECK GOOD PER 25-64-00.

Part: FMC — MALFUNCTIONED · airframe 21,216 hrs · 8,632 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON TAKEOFF ROLL AT OR ABOUT V1, ALL V SPEEDS DISAPPEARED. V SPEEDS WERE CONFIRMED ON TAXI OUT, SPEEDS WERE 140,142,147. CALLED ROTATION AT ABOUT 155 KTS. MAINTENANCE ACCOMPLISHED BITE OF FMS, DFCS, AND CDS, ALL NORMAL. NO FAULTS DISPLAYED FOR PREVIOUS FLT LEG. OPERATIONAL TEST OF DFCS NORMAL IAW AMM 22-11-00. OPERATIONAL TEST OF FMC NORMAL IAW AMM 34-61-00. OPERATIONAL TEST OF CDS NORMAL IAW AMM 31-62-00. ALL TESTS GOOD.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 21,089 hrs · 8,573 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS UPON ARRIVAL TO AIRCRAFT FOUND L1 DOOR SLIDE LOOSE FROM CASING. MAINTENANCE INSTALLED NEW SLIDE ON L1 DOOR IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: CONNECTING ROD — OUT OF ADJUST (RT SPOILER) · airframe 18,933 hrs · 7,588 cycles

THE AIRCRAFT WAS NOT GROUNDED. FLIGHT SPOILERS 8 AND 9 START DEPLOYING AT 1.4 TO 1.5 UNITS RIGHT WING DOWN AILERON INPUT CONSISTENTLY. MAINTENANCE OBSERVERS DE-BRIEFED. ADJUSTED RATIO CHANGER INPUT ROD PER AMM 27-61-00. SPOILERS LIFT AT 1.8. OPERATIONS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 18,933 hrs · 7,588 cycles

CORROSION FOUND ON THE CABIN FLOORBEAM, BS 947.5. REPAIRED THE FLOORBEAM IAW SRM 53-70-51.

Part: WEB — CORRODED (BS 793-847) · corrosion level 2 · airframe 18,933 hrs · 7,588 cycles

AFT CARGO DOOR THRESHOLD WEB HAD CORROSION. REPLACED THE THRESHOLD WEB IAW RD 51-00-05-1, AND SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 18,933 hrs · 7,588 cycles

CRACKED CABIN FLOOR SUPPORT BETWEEN BS 328 AND 344, LBL 46. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1

Part: FLOORBEAM — CRACKED (BS 540) · airframe 18,933 hrs · 7,588 cycles

CRACKED CABIN FLOORBEAM, BS 540 BETWEEN BL 0 AND RBL 24. REPLACED THE FLOORBEAM IAW RD 51-00-05-1.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 18,933 hrs · 7,588 cycles

CRACKED CABIN FLOORBEAM AT BS 540, BETWEEN BL 0 AND LBL 24. REPLACED THE FLOORBEAM IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 18,933 hrs · 7,588 cycles

CRACKED CABIN FLOOR SUPPORT BETWEEN BS 344 AND 360, LBL 12. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 18,933 hrs · 7,588 cycles

CRACKED CABIN FLOOR SUPPORT BETWEEN BS 312 AND 328, LBL 46. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 18,933 hrs · 7,588 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 312 AND 328, RBL 32. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500D-500E) · airframe 18,933 hrs · 7,588 cycles

CORROSION FOUND ON THE FORWARD CARGO BAY LEFT TRANSITION PANEL BETWEEN BS 500D AND 500E. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 18,923 hrs · 7,581 cycles

BS 663 BULKHEAD FOUND CRACKED BETWEEN RBL 25 AND RBL 31.83. REPAIRED THE BULKHEAD WEB IAW RD 57-10-10-9.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,510 hrs · 7,405 cycles

CEILING EMERGENCY LIGHT OVERWING EXITS FOUND INOPERATIVE DURING BASE MAINTENANCE TESTING. REPLACED THE LIGHT ASSEMBELY. CHECKED GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 18,203 hrs · 7,279 cycles

AIRCRAFT WAS GROUNDED. A/C DIVERTED TO CLE ACCOUNT OF NUMBER 1 ENGINE SHUT DOWN (FAILURE). OIL PRESSURE WAS 0 PSI OIL QTY WAS 17, WE HAD N-1 AND N-2 ROTATION PERFORMED EMERGENCY SHUT DOWN CHECK LIST. ACCOMPLISHED EEC NR 1 BITE FOUND SEVERAL FAULTS-INCLUDING FMV DEMAND AND POSITION SIGNALS DISAGREE, THE VBV DEMAND AND POSITION SIGNALS DISAGREE, FUEL FLOW WAS NOT DETECTED, HPTACC/DEMAND & POSITION SIGNALS DISAGREE. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME REPORTED AS 20 MINUTES. REMOVED ENGINE SN 874880 AND INSTALLED ESN 874831 AT LT POSITION ON CLE BOW DATED 10/22/2018.

Part: GIRT BAR — OUT OF ADJUST (SERVICE DOOR) · airframe 17,791 hrs · 7,112 cycles

THE GIRT BAR AT THE FORWARD SERVICE DOOR WAS OUT OF ADJUSTMENT, FALLS OUT OF BRACKET. CHECKED AND ADJUSTED GIRT BAR RETAINERS IAW 25-66-01. OKAY FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,748 hrs · 6,261 cycles

AIRCRAFT WAS GROUNDED. L2 SLIDING WINDOW "OVERHEAT" LIGHT ILLUMINATED, FOLLOWED BY WINDOW CRACKING BEYOND LIMITS. REPLACED L2 WINDOW OPS CHECK NORMAL PER MCM 56-94-01. (SEE ALSO SDR AALA201801129025)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT)

AIRCRAFT WAS GROUNDED. L2 SLIDING WINDOW "OVERHEAT" LIGHT ILLUMINATED, FOLLOWED BY WINDOW CRACKING BEYOND LIMITS. REPLACED WINDOW HEAT CONT NR 3, PER 30-41-11, OPS CHECK NORMAL. (SEE ALSO SDR AALA201801129022)

Part: COVER — MISSING (CABIN) · airframe 15,714 hrs · 6,244 cycles

THE AIRCRAFT WAS NOT GROUNDED. LOWER FORWARD ENTRY WAY WALL LIGHT MISSING COVER. REMOVED AND REPLACED EMERGENCY LIGHT R SIDE PER MM 33-51-00.

Part: COVER — MISSING (CABIN) · airframe 15,710 hrs · 6,243 cycles

THE AIRCRAFT WAS NOT GROUNDED. LOWER FORWARD ENTRY WAY WALL (RIGHT SIDE) MISSING LENS COVER. REMOVED AND REPLACED EMERGENCY LIGHT R SIDE PER MM 33-51-00.

Part: LIGHT — MISSING (CABIN) · airframe 15,515 hrs · 6,163 cycles

AIRCRAFT WAS NOT GROUNDED. AFT RIGHT SERVICE DOOR EXIT SIGN COVER MISSING. REPLACED EMERGENCY LIGHT AT 4R PER AMM 33-51-00.

Part: HOLDER — BROKEN (EXIT SIGN) · airframe 13,549 hrs · 5,331 cycles

R1 DOOR EMERGENCY SIGN BEZEL HOLDER IS BROKEN. R&R LITE ASSY IAW AMM 33 51 01 CKS GOOD. THE AIRCRAFT WAS NOT GROUNDED.

Part: LENS — MISSING (EXIT SIGN) · airframe 12,780 hrs · 5,004 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN ON WALL JUST AFT OF FORWARD GALLEY HAS A MISSING LENS COVER. REPLACED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: SIGN — DETACHED (CABIN) · airframe 12,428 hrs · 4,857 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EXIT SIGN DETACHED. SECURED EXIT SIGN IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: SLIDE — MALFUNCTIONED (ZONE 800) · airframe 10,443 hrs · 4,069 cycles

AIRCRAFT WAS GNDED. FWD ENTRY SLIDE CAME OUT OF PACK WITH GIRT BAR STILL ATTACHED. SLIDE DID NOT DEPLOY. R & R SLIDE ASSEMBLY IAW AMM 25-66-01. CORRECT TIMES & CYCLES.

Part: LENS — BROKEN (CABIN) · airframe 7,801 hrs · 3,005 cycles

EMERGENCY EXIT LIGHT CAPSULE NOT ARMED LENS IS BROKEN. R & R LIGHT NOT ARMED LIGHT CAPSULE IAW AMM 33-12-00. SYS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 4,330 hrs · 1,665 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. RETRACTED & EXTENDED LG MULTIPLE TIMES WITH NO FAULTS FOUND. SYS GND CHECKED NORMAL OPERATION CLOSED.