N955NN

Part: GROUND WIRE — LOOSE (ZONE 500 K FLAP) · airframe 30,699 hrs · 12,704 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 IN TRANSIT KRUEGER LIGHT WOULD NOT EXTINGUISH WITH ASSOCIATED LEADING EDGE FLAPS TRANSIT LIGHT; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. PERFORMED TROUBLESHOOTING PER FIM 27-88-00-810-805, REF WDM 27-81-11, FOUND LEADING EDGE FLAP 1 RETRACT SENSOR (S168) GROUND TERMINAL (GD614AC) LOOSE. SECURED GROUND TERMINAL (GD614AC), PER AMM20-50-11 AND AMM 27-88-11. ACCOMPLISHED LEADING EDGE FLAP AND SLAT PROXIMITY SENSOR TEST, PER AMM 27-88-11, OPERTIONAL CHECKS GOOD.

Part: GIRT BAR — BROKEN (ZONE 200) · airframe 28,758 hrs · 11,790 cycles

AIRCRAFT WAS GROUNDED: DIFFICULT TO ARM AND DISARM BOTH FORWARD DOORS. FOUND R1 DOOR SLIDE GIRT BAR STOP BROKEN. REMOVED AND REPLACED GIRT BAR STOP AT R1 DOOR. PER AMM 25-66-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,577 hrs · 11,237 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY ESCAPE SLIDE, AFT ENTRY AND GALLEY DOOR LIGHT ON LEFT SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE SLIDE, AFT ENTRY (AALA202403040313) AND GALLEY DOOR (AALA202403047704) LIGHT BULB AND PERFORMED SATISFACTORY CHECK. PER B737NG-AMM 33-51-04

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,577 hrs · 11,237 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY ESCAPE SLIDE, AFT ENTRY AND GALLEY DOOR LIGHT ON LEFT SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE SLIDE, AFT ENTRY (AALA202403040313) AND GALLEY DOOR (AALA202403047704) LIGHT BULB AND PERFORMED SATISFACTORY CHECK. PER B737NG-AMM 33-51-04

Part: DOOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 26,210 hrs · 10,618 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR HANDLE MIGRATED ON LANDING. DOOR WARNING INDICATION EXTINGUISHED WHEN DOOR HANDLE CLOSED. ACCOMPLISHED FORWARD ENTRY DOOR ADJUSTMENT. PER M/M 52-11-00.

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 26,210 hrs · 10,618 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND COCKPIT SLIDER WINDOW IS EXTREMELY DIFFICULT TO TO OPEN AND CLOSE. ADJUSTED SLIDING WINDOW PER AMM 56-12-11.

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 26,210 hrs · 10,618 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND COCKPIT SLIDER WINDOW IS EXTREMELY DIFFICULT TO TO OPEN & CLOSE. ADJUSTED SLIDING WINDOW. PER AMM 56-12-11.

Part: FLOOR PANEL — DAMAGED (ZONE 200 - FUSE) · airframe 26,173 hrs · 10,600 cycles

AIRCRAFT WAS GROUNDED: AISLE CABIN FLOOR PANEL BETWEEN SEAT ROWS 1 AND 2 VERY SOFT AND BOUNCY. MAINTENANCE REPAIRED FLOOR PANEL PER AARD 53-00-00-6.

Part: COMPENSATOR — FAULTY (ZONE 500 - LH WI) · airframe 25,704 hrs · 10,382 cycles

AIRCRAFT WAS GROUNDED: FUEL IMBALANCE / LEAK ON TAKEOFF BETWEEN 10K CLIMBING. EMERGENCY DECLARED; FLIGHT RETURNED TO DFW LANDING SAFELY. MAINTENANCE REPLACED LEFT WING FUEL COMPENSATOR UNIT PER AMM 28-41-21-401.

Part: RETAINER CUP — LOOSE (ZONE 800 - DOORS) · airframe 25,316 hrs · 10,205 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY GIRT BAR IS LOOSE. ADJUSTED GIRT BAR RETAINING CLIP. ALL SECURE. OKAY FOR SERVICE.

Part: DOOR — UNSERVICEABLE (LAVATORY) · airframe 23,893 hrs · 9,531 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. **SUPPLEMENTAL REPORT FOR AALA202211012937: REPLACED LAVATORY D DOOR HARDWARE PER CMM 25-47-21.** (CLOSED)

Part: NONE — NONE · airframe 23,893 hrs · 9,531 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: NONE — STICKING (ZONE 800 - DOORS) · airframe 22,685 hrs · 8,970 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY DOOR SLIDE GIRT BAR CLIP VERY TIGHT (HARD TO USE). ADJUSTED AND FIT GIRT BAR RETAINER CLIPS ON DOOR COVER LEFT PER 25-66-01.

Part: DOOR LATCH — BROKEN (ZONE 900 - LAV/G) · airframe 22,154 hrs · 8,738 cycles

AIRCRAFT WAS GROUNDED: FORWARD LAVATORY DOOR LATCH IS BROKEN. UNABLE TO OPEN DOOR. REPLACED DOOR LATCH PER CMM 25-48-48 AND ESO 60869. OPS CHECK NORMAL.

Part: BRACKET — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 21,041 hrs · 8,272 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS R1 DOOR GRIT BAR BRACKET NEEDS ADJUSTING. ADJUSTING TO R1 DOOR SLIDE BRACKET OPERATIONS CHECK OK PER AMM 25-66-02.

Part: ANTI-ICE VALVE — FAULTY (ZONE 400 - NAC/P) · airframe 20,964 hrs · 8,232 cycles

AIRCRAFT WAS GROUNDED: DURING TAKEOFF ROLL #1 ENGINE AMBER COWL VALVE ANTI ICE LIGHT ILLUMINATED. REJECTED TAKEOFF AT 20 KNOTS. RETURNED TO GATE. REPLACED #1 ENGINE COWL THERMAL ANTI ICE VALVE PER AMM 30-21-11.

Part: POWER SUPPLY — ODOR (SEAT 8 ABC) · airframe 20,636 hrs · 8,091 cycles

AIRCRAFT WAS GROUNDED: RUBBER, ELECTRICAL TYPE ODOR REPORTED NEAR ROW 8, ODOR QUICKLY DISSIPATED WHEN RE CIRCULATION FANS WERE TURNED OFF. FOUND ROW 8 ABC IN SEAT POWER SUPPLY INOPERATIVE. FOUND POWER SUPPLY HAD STRONG ODOR. REMOVED AND REPLACED SEAT 8 ABC POWER SUPPLY PER AMM 23-81-05. OPERATIONS CHECK OK.

Part: SETSCREW — OUT OF POSITION (EMERGENCY LIGHT) · airframe 19,481 hrs · 7,602 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT COVER CAME OFF AT 20 D,E,F. REMOVED AND REPLACED SET SCREWS FOR EMERGENCY EXIT LIGHT COVER AT 20 D,E,F.

Part: FLOOR SUPPORT — CRACKED (BS 323) · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN FLOOR INTERCOSTAL AT STA 323 AND RBL 31, MEASURING L=1.0 IN, W=0.1 IN. REPLACED INTERCOSTAL WITH NEW, IAW AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 335) · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN FLOOR INTERCOSTAL AT STA 335.5 AND LBL 45, MEASURING L=1.0 IN, W=0.1 IN. REPLACED INTERCOSTAL WITH NEW, IAW AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 321) · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN FLOOR INTERCOSTAL AT STA 321 AND LBL 45, MEASURING L=1.0 IN, W=0.1 IN. REPLACED INTERCOSTAL WITH NEW, IAW AARD 51-00-05-1.

Part: CREASE BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF CREASE ANGLE AT L2 DOOR CUTOUT AT STA 974 AND LBL 53, MEASURING L=1.5 IN, W=1.0 IN, D=0.01 IN. ACCOMPLISHED PERMANENT BLEND REPAIR, IAW EA309669.

Part: TRANSITION PANEL — CORRODED (AFT CARGO) · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF LT TRANSITION PANEL IN AFT CARGO BETWEEN STA 727 AND STA 847 AT STR 25L, MEASURING L=70.0 IN, W=1.0 IN, D=0.003 IN. ACCOMPLISHED PERMANENT BLEND REPAIR, IAW SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 727-767) · corrosion level 2 · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF RT TRANSITION PANEL IN AFT CARGO BETWEEN STA 727 AND STA 767 AT STR 25R, MEASURING L=16.0 IN, W=1.0 IN, D=0.021 IN. REPLACED TRANSITION PANEL WITH NEW, IAW AARD 51-00-05-1, DRAWING 146A7500, AND SRM 53-00-53-2R.

Part: TRANSITION PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF LT TRANSITION PANEL BETWEEN STA 500D AND STA 500I AT LBL 25, MEASURING L=20.0 IN, W=2.0 IN, D=0.009 IN. REPLACED TRANSITION PANEL WITH NEW, IAW SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,166 hrs · 7,067 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF RT TRANSITION PANEL BETWEEN STA 500D AND STA 500I AT RBL 25, MEASURING L=20.0 IN, W=2.0 IN, D=0.01 IN. REPLACED TRANSITION PANEL WITH NEW, IAW SRM 53-00-53-2R-5.

Part: SENSOR — MALFUNCTIONED (AUTOPILOT A) · airframe 17,601 hrs · 6,819 cycles

AIRCRAFT WAS NOT GROUNDED: UPON SELECTING CMD A. THERE WAS A NOTEABLE PITCH DOWN DURING CLIMB OUT. VNAV WAS WAS ENGAGED. FLIGHT WAS OPERATED IN CMD B. WITH NO FURTHER ISSUES. TROUBLESHOT AUTO PILOT A PITCH FOUND FAULT CODE 22-11127 (ELEVATOR POSITION SENSOR. ACCOMPLISHED FIM 22-13-810-806 AND ALL SYSTEM OPERATIONAL CHECKS NORMAL.

Part: WINDOW — ARCED (COCKPIT L1) · airframe 16,355 hrs · 6,280 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK L1 WINDOW SHOWS SIGNS OF ARCING ALONG THE BUS BAR. REPLACED WINDOW PER TASK CARD 56-94-03.

Part: GIRT BAR — DISPLACED (SERVICE DOOR) · airframe 15,320 hrs · 5,819 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON PREFLIGHT, FOUND GIRT BAR FOR FORWARD SERVICE SLIDE OUTSIDE OF DOOR WITH DOOR CLOSED. MAINTENANCE SECURED GIRT BAR IAW AMM 25-66-00. CHECKS OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,788 hrs · 5,596 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. REPLACED WINSHIELD PER TASK CARD 56-94-04.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 13,308 hrs · 4,967 cycles

AIRCRAFT WAS GROUNDED: FORWARD GALLEY DOOR SLIDE PARTIALLY OUT OF HOLDER WHEN DOOR OPENED. MAINTENANCE REPLACED R1 DOOR SLIDE PACK PER MCM 25-94-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 11,459 hrs · 4,256 cycles

FORWARD GALLEY DOOR SLIDE PARTIALLY OUT OF THE HOLDER WHEN DOOR WAS OPENED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE R1 DOOR SLIDE IAW MCM 25-94-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PROBE — INACCURATE (FUEL QTY) · airframe 11,459 hrs · 4,256 cycles

DIVERTED DUE TO A FUEL IMBALANCE OF 3500 POUNDS. AN EMERGENCY DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND REMOVED FROM SERVICE. DETERMINED THAT THE RIGHT FUEL QUANTITY WAS INCORRECT. PERFORMED FIM 28-41-00-810-814, NO FAULTS NOTED. TEST PASSED. FQIS BITE PROCEDURE PASSED.

Part: LENS — BROKEN (CABIN) · airframe 9,645 hrs · 3,514 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT THE FORWARD GALLEY HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER PER AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 9,260 hrs · 3,355 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE R1 DOOR HAS A DETACHED LENS COVER. REPLACED LENS COVER PER AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 8,038 hrs · 2,857 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY R1 DOOR HAS A DETACHED LENS COVER. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: OUTLET — DAMAGED (SEAT 7DE) · airframe 7,628 hrs · 2,717 cycles

HEAVY WHITE SMOKE FROM POWER PORT AT SEAT 7D/E. SMOKE STOPPED AFTER POWER TURNED OFF. FOUND LIQUID DAMAGE. REMOVED AND REPLACED SEAT POWER BOX AT 7DEF IAW AMM 44-22-44-000-801 (AALA201703179018) AND AC OUTLET UNIT AT 7D IAW AMM 44-22-43-000-801. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: POWER UNIT — DAMAGED (SEAT 7DE) · airframe 7,628 hrs · 2,717 cycles

HEAVY WHITE SMOKE FROM POWER PORT AT SEAT 7D/E. SMOKE STOPPED AFTER POWER TURNED OFF. FOUND LIQUID DAMAGE. REMOVED AND REPLACED SEAT POWER BOX AT 7DEF IAW AMM 44-22-44-000-801 AND AC OUTLET UNIT AT 7D IAW AMM 44-22-43-000-801. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: SIGN — CRACKED (CABIN) · airframe 7,069 hrs · 2,495 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT R1 DOOR IS CRACKED. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-51-14. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 7,003 hrs · 2,468 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT R1 DOOR HAS A DETACHED LENS COVER. SECURED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: TAT PROBE — DAMAGED (ZONE 100) · airframe 1,427 hrs · 507 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB TOTAL AIR TEMP WENT TO 72 DEGREES. ENGS LIMITED TO 81% POWER. FOUND BIRD STRIKE TO LT SIDE OF FUSELAGE & INTO LT TOTAL AIR TEMP PROBE. R & R TOTAL AIR TEMP PROBE & PERFORMED OPERATIONAL CHECK IAW AMM 34-21-06. SYS CHECKED NORMAL.

Part: HEATER — ABNORMAL (CABIN) · airframe 97 hrs · 38 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING WAS UNEVENTFUL & ACFT WAS OVERWEIGHT. STRONG SMELL OF SMOKE IN FLIGHT COMPARTMENT & CABIN FROM FLIGHT ATTENDANT JUMP SEAT TO ROW 4. TROUBLESHOOTING FOUND L1 DOOR AREA HEATER CB POPPED. REPLACED L1 DOOR AREA HEATER IAW MM 21-45-01. OPERATIONS CHECKED GOOD.