N827NN

Part: HEAT SHRINK — MISSING (ZONE 800) · airframe 45,732 hrs · 19,458 cycles

AIRCRAFT WAS NOT GROUNDED: RED HEAT SHRINK MISSTING AT L1 DOOR GIRT BAR. REPLACED RED HEAT SHRINK TUBING. PER AARD 25-66-00-4.

Part: HEAT SHRINK — MISSING (GIRT BAR) · airframe 45,732 hrs · 19,458 cycles

AIRCRAFT WAS NOT GROUNDED: RED HEAT SHRINK MISSING AT L1 DOOR GIRT BAR. (OPEN).

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 44,041 hrs · 18,677 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING THE ACCOMPLISHMENTS OFOF CPCP 53-050-00 TASK, LEFT HAND WHEEL WELL FORWAFRD WHEEL CUT OUT HAS CORROSION AROUND FASTENERS. REMOVED CORROSION AT LEFT HAND WHEEL WELL FORWARD WHEEL CUT OUT. PER B737 SRM 51-10-02.

Part: DUCT — BLOWN (ZONE 100) · airframe 43,647 hrs · 18,501 cycles

AIRCRAFT WAS GROUNDED: ON THE TAKEOFF ROLL A SOUR MUSTY ODOR OCCURRED. UPON CLIMBOUT THE SMELL COMPLETELY DISSIPATED. THEN ON APPROACH AT APPROXIMATELY 5000FT THE ODOR CAME BACK. IN RIGHT HAND PACK BAY, FOUND ORANGE FLEX DUCT BLOWN. REMOVE AND REPLACED THE FLEX DUCT. OPERTIONAL AND LEAK CHECK GOOD. PER AMM 21-51-04.

Part: DOOR — STUCK (ZONE 800) · airframe 43,396 hrs · 18,377 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR OFF TRACKS AND STUCK SHUT. REMOVE AND REPLACED LEFT AFT LAVATORY-D BI-FOLD DOOR. PER CMM 25-40-64.

Part: LATCH — LACK OF LUBE (ZONE 800) · airframe 43,319 hrs · 18,335 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR EXTREMELY DIFFICULT TO OPEN FROM OUTSIDE (WITH SYSTEM OFF). APPLIED LUBRICANT TO FLIGHT DECK DOOR LATCH. DOOR WORKS PROPERLY NOW, AND OPERTIONAL CHECKK GOOD. PER AMM 52-51-00.

Part: LIGHT — MISSING (ZONE 200) · airframe 42,591 hrs · 17,974 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EQUIPMENT CEILING LIGHTS MISSING LIGHTING END CAP AT SEAT 23D. INSTALLED NEW CEILING LIGHT END CAP ON ROW 23D AS REQUIRED.

Part: LIGHT — MISSING (ZONE 200) · airframe 42,591 hrs · 17,974 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EQUIPMENT CEILING LIGHTS MISSING LIGHTING END CAP AT 21D. INSTALLED NEW CEILING LIGHT END CAP ON ROW 21D AS REQUIRED.

Part: PUMP — FAILED (LT WING FUEL) · airframe 42,176 hrs · 17,766 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FORWARD LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. REMOVE AND REPLACED LEFT FORWARD BOOST PUMP. NO LEAK FOUND PUMP OPERTIONAL CHECK GOOD. PER AMM 28-22-41.

Part: FUEL SYS — LEAKING (NR 2 ENGINE) · airframe 41,182 hrs · 17,310 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ENGINE 2 SUSPECTED FUEL LEAK, ENGINE SECURED IN FLIGHT; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT ORD. (OPEN).

Part: COMPENSATOR — FAULTY (FUEL SYSTEM) · airframe 41,182 hrs · 17,310 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ENGINE 2 SUSPECTED FUEL LEAK, ENGINE SECURED IN FLIGHT; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT ORD.**SUPPLEMENTAL REPORT FOR (AALA202403018508): REPLACED 1 MAIN FUEL QUANTITY COMPENSATOR F156. OPERATIONAL AND LEAK CHECKS GOOD. PER FUEL VENDOR TANK TIGERS WORK ORDER #12446R264

Part: DOOR — UNSECURE (LAVATORY D) · airframe 41,052 hrs · 17,246 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR JAMMED AND IS HARD TO OPEN. RESECURED UPPER DOOR TRIM. PER AMM 25-40-00.

Part: FUEL SYS — MALFUNCTIONED · airframe 40,880 hrs · 17,176 cycles

AIRCRAFT WAS GROUNDED: UNWANTED FUEL TRANSFER LEFT WING TO CENTER. NOTED THAT WITH ALL PUMPS ON AND CROSSFEED CLOSED THE LEFT WING FUEL INDICATED 7.85,CENTER .30 AND RIGHT WING 8.63.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: FUEL SYS — MALFUNCTIONED (LT WING) · airframe 40,880 hrs · 17,176 cycles

AIRCRAFT WAS GROUNDED: UNWANTED FUEL TRANSFER LEFT WING TO CENTER. NOTED THAT WITH ALL PUMPS ON AND CROSSFEED CLOSED THE LEFT WING FUEL INDICATED 7.85,CENTER .30 AND RIGHT WING 8.63.**SUPPLEMENTAL REPORT FOR (AALA202401233069): ACCOMPLISHED FIM 28-21-00-810-803 STEP A TO C-8 OPEN CENTER TANK SUMP DRAIN FOR 1 HOUR, NO DRIPS NOTED. OPERATED LEFTHAND FORWARD & LEFTHAND AFT BOOST PUMP FOR 1 HOUR, NO DRIPS NOTED. BALANCED FUEL LEFT HAND AND RIGHT HAND WING. NO FAULT FOUND**(CLOSED).

Part: LIGHT — DISCONNECTED (ZONE 200 - FUSE) · airframe 39,462 hrs · 16,476 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND EMERGENCY AISLE LIGHTS INOPERATIVE IN ROW 32 FED. RE-CONNECTED EMERGENCY AISLE LIGHTS IAW AMM 33-51-03-960-805. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DISCONNECTED (ZONE 200 - FUSE) · airframe 39,462 hrs · 16,476 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND EMERGENCY AISLE LIGHTS INOPERATIVE IN ROW 14 ABC. RE-CONNECTED EMERGENCY AISLE LIGHTS IAW AMM 33-51-03-960-805. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: PIN — FAULTY (ZONE 800 - DOORS) · airframe 39,198 hrs · 16,341 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR WILL NOT OPEN. FORWARD ENTRY DOOR GUIDE ARM PIN REMOVED AND REPLACED.

Part: NONE — LOOSE (ZONE 800 - DOORS) · airframe 37,253 hrs · 15,412 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR LOOSE ON RIGHT CLIP OF LEFT AFT SERVICE DOOR. ADJUSTED GIRT BAR RETAINING CLIPS PER AMM 25-66-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,125 hrs · 15,341 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER RIB CRACKED AT FORWARD BOTTOM END STABILIZER STA 92.70. REMOVED AND REPLACED RIB PER SRM 51-40-02.

Part: NONE — NONE · airframe 36,092 hrs · 14,842 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT OVERWING EXIT WINDOW SHADE DAMAGE. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: SHADE — DAMAGED (ZONE 800 - DOORS) · airframe 36,092 hrs · 14,842 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT OVERWING EXIT WINDOW SHADE DAMAGE. **SUPPLEMENTAL REPORT FOR AALA202204281310: REMOVED AND REPLACED LEFT AFT OVERWING EXIT WINDOW SHADE (ROW 17 ABC) PER B-737 AMM 25-21-12.** (CLOSED)

Part: INDICATOR — INOPERATIVE (ZONE 200 - FUSE) · airframe 35,966 hrs · 14,777 cycles

AIRCRAFT WAS GROUNDED: FLAPS FAILED TO EXTEND AS COMMANDED. STOPPED JUST INTO THE 5 BAND. PER QUICK REFERENCE HANDBOOK USED ALTERNATE FLAPS TO EXTEND TO 15. EMERGENCY WAS DECLARED AND NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED FLAP/SLAT ELECTRONIC UNIT (AALA202204044578) PER AMM 27-51-01. REMOVED AND REPLACED FLAP POSITION INDICATOR PER AMM 27-58-02. OPERATIONS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (ZONE 200 - FUSE) · airframe 35,966 hrs · 14,777 cycles

AIRCRAFT WAS GROUNDED: FLAPS FAILED TO EXTEND AS COMMANDED. STOPPED JUST INTO THE 5 BAND. PER QUICK REFERENCE HANDBOOK USED ALTERNATE FLAPS TO EXTEND TO 15. EMERGENCY WAS DECLARED AND NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED FLAP/SLAT ELECTRONIC UNIT PER AMM 27-51-01. REMOVED AND REPLACED FLAP POSITION INDICATOR (AALA202204046154) PER AMM 27-58-02. OPERATIONS CHECK GOOD.

Part: FSEU — FALSE INDICATION (ZONE 100 - FUSE) · airframe 35,802 hrs · 14,704 cycles

AIRCRAFT WAS GROUNDED: ON APPROACH TO DEN, DURING FLAP EXTENSION FROM 2 TO 5, FLAPS SPLIT, THEN LOCKED OUT. FLIGHT DECLARED AN EMERGENCY, LANDING SAFELY. ACCOMPLISHED FLAP / SLAT ELECTRONICS UNIT BITE TEST PER FIM 27-51-00. ACCOMPLISHED TRAILING EDGE FLAP TRANSMISSION TORQUE TRIP INSPECTION PER FIM 27-51-00. ACCOMPLISHED FLAP SKEW DETECTION FUNCTIONAL TEST PER AMM 27-59-00. ACCOMPLISHED FLAP POSITION TRANSMITTER ADJUSTMENT / TEST PER AMM 27-58-00. ALL SYSTEMS CHECK OK. NO FAULTS NOTED.

Part: GIRT BAR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 35,768 hrs · 14,683 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR WOULDN'T DISARM. CLEANED AND LUBRICATED GIRT BAR ATTACH FITTINGS PER AMM-25-66-01.

Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 35,764 hrs · 14,681 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NEAR 2R DOOR JUMPSEAT DOES NOT TEST CORRECTLY. REPLACED FLASHLIGHT PER AMM 25-64-00.

Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 35,764 hrs · 14,681 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT JUMPSEAT 2L DOES NOT TEST. REPLACED FLASHLIGHT PER AMM 25-64-00.

Part: ANGLE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR SUPPORT Z ANGLE LOCATED BETWEEN STA 990 AND STA 1016 AT RBL 30. REPLACED ANGLE PER AARD 51-00-05-01 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: 1 INCH CRACK FOUND IN LEFT FLOOR SUPPORT LOCATED AT STA 540 AND LEFT BUTT LINE 2. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-02.

Part: ATTACH ANGLE — INOPERATIVE (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CRACKED ANGLE LEFT AIRCRAFT BAY AFT UPPER ATTACH AREA. LOCATED AT STA 540 AND STR 23L AND LEFT BUTT LINE 35. REMOVED AND REPLACED ATTACH ANGLE PER SRM 57-10-10-2R-5.

Part: SKIN PANEL — CORRODED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FUSELAGE SKIN LOCATED AT STA 972 BETWEEN LBL 26 AND LBL 27. REPAIRED SKIN PER EA 333893.

Part: RIB — CRACKED (ZONE 300 - STABS) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK ON RIB OF HORIZONTAL STABILIZER LOCATED AT STA 92.7 AND 19.5 INCHES AFT OF FRONT SPAR. INSTALLED REPAIR DOUBLER PER SRM 55-10-09-2R-4.

Part: RIB — CRACKED (ZONE 300 - STABS) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON RIB OF HORIZONTAL STABILIZER LOCATED AT STA 92.7 29 INCHES AFT OF THE FRONT SPAR. INSTALLED DOUBLER REPAIR PER SRM 55-10-09-2R-4.

Part: RIB — CRACKED (ZONE 300 - STABS) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIB OF RH HORIZONTAL STABILIZER AT STA 92.70, 38.0 IN AFT OF FRONT SPAR, MEASURING L=1.25 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-09-2R-5.

Part: INTERCOSTAL — CRACKED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL AT STA 344 TO 360, STR 17 AND BUT LINE 0 IS CRACKED AT APPROXIMATELY STA 353 AT FLOORBOARD ATTACH HOLE. INSTALLED REPLACEMENT INTERCOSTAL PER AARD 51-00-05.

Part: RIB — CRACKED (ZONE 300 - STABS) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER RIB LOCATED AT STABILIZER STA 92.70. REPLACED RIB PER SRM 55-10-01-2R-11.

Part: INTERCOSTAL — CRACKED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK ON INTERCOSTAL LOCATED AT STA 320 AND LEFT BUTT LINE 45. REMOVED AND REPLACED INTERCOSTAL PER AARD 5-00-05.

Part: INTERCOSTAL — CRACKED (ZONE 200 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL LOCATED BETWEEN STA 328 AND STA 344 AT LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO AREA LEFT HAND TRANSITION PANEL LOCATED BETWEEN STA 490 AND STA 500I AT LBL 25. REPAIRED PER SRM 53-30-53.

Part: SUPPORT — CORRODED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: LOWER CHANNEL OF REMOVABLE BULKHEAD CORRODED AT STA 500I AND LEFT BUTT LINE 24 TO RIGHT BUTT LINE 24. REMOVED AND REPLACED LOWER CHANNEL OF REMOVABLE BULKHEAD PER SRM 51-40-02.

Part: SHIELD — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION SHIELD BETWEEN STA 767 AND STA 787 AT RBL 22, MEASURING L=1.0 IN, W=0.5 IN, D=0.015 IN. REPLACED SHIELD WITH NEW IAW AARD 51-00-05-1.

Part: INTERCOSTAL — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN INTERCOSTAL LOCATED BETWEEN STA 946 AND 964 AT LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1 AND AIPC 53-42-51.

Part: NONE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND CREASE ANGLE LOCATED FROM STA 940 TO STA 987 AT LBL 50. REPLACED CREASE ANGLE PER SRM 51-40-02 AND DWG 147A8501.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND TRANSITION PANEL LOCATED BETWEEN STA 727A AND STA 727E AT RBL 22. REPAIRED PER SRM 51-10-02.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND TRANSITION PANEL LOCATED BETWEEN STA 727I AND STA 787 AT RBL 22. REPLACED TRANSITION PANEL PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON FLOOR SUPPORT LOCATED BETWEEN STA 947 TO 967, RIGHT BUTT LINE 24 TO 27. REMOVED AND REPLACED FLOOR SUPPORT PER AARD 51-00-05, AND SRM 51-40-02.

Part: WEB — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON WEB LOCATED BETWEEN 987 TO 992, RIGHT BUTT LINE 30.5 TO 34. INSTALLED DOUBLER REPAIR PER EA 334023.

Part: FLOORBEAM — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION NON FLOORBEAM LOCATED AT STA 986.5 BETWEEN LBL 43 AND LBL 44. REPAIRED PER SRM 53-70-51-2R-6 AND EA 334090

Part: CAP — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON T CAP LOCATED AT STA 986 AND RBL 3. REPAIRED PER SRM 53-70-51-2R-6 AND EA 334057.

Part: ANGLE — INOPERATIVE (ZONE 200 - FUSE) · corrosion level 2 · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON CREASE ANGEL 2 INCHES BY 2 INCHES. CORROSION LOCATED BETWEEN 947 AND 990, AND STR 17R. REMOVED AND REPLACED RIGHT AFT CREASE ANGLE PER EA 334174.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · airframe 35,761 hrs · 14,678 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL BETWEEN STA 727I AND STA 787 AT RBL 22, MEASURING L=2.0 IN, W=1.3 IN, D=0.012 IN. REPLACED TRANSITION PANEL WITH NEW IAW SRM 51-10-02.

Part: BATTERY PACK — FAILED (ZONE 200 - FUSE) · airframe 35,720 hrs · 14,658 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY PACK M1672 FAILED EMERGENCY LIGHTS FUNCTIONAL CHECK. REPLACED BATTERY PACK PER AMM 33-51-06. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: BATTERY PACK — FAILED (ZONE 200 - FUSE) · airframe 35,720 hrs · 14,658 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY PACK M1670 FAILED EMERGENCY LIGHTS FUNCTIONAL CHECK. REPLACED BATTERY PACK PER AMM 33-51-06. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: RELAY — STICKING (ZONE 700 - GEARS) · airframe 35,629 hrs · 14,615 cycles

AIRCRAFT WAS GROUNDED: NOSE WHEEL STEERING IS BINDING WHEN INITIATING TURNS BOTH LEFT AND RIGHT OF CENTER. REQUIRES HIGHER THAN NORMAL FORCE BEYOND THAT BUT DOES NOT CONTINUE TO BIND UP. REMOVED AND REPLACED RELAY R596 PER SWPM 20-15-46. OPERATIONS CHECK GOOD.

Part: NONE — NONE · airframe 35,422 hrs · 14,523 cycles

AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE STUCK AT EXIT ROW SEAT 17A. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: SHADE — STICKING (ZONE 800 - DOORS) · airframe 35,422 hrs · 14,523 cycles

AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE STUCK AT EXIT ROW SEAT 17A. **SUPPLEMENTAL REPORT: REPLACED WINDOW SHADE WITH NEW, OPS CHECK GOOD.** (CLOSED)

Part: PSEU — FAULTED (MLG) · airframe 34,458 hrs · 14,076 cycles

AIRCRAFT WAS NOT GROUNDED: PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) LIGHT ILLUMINATED ON TAKEOFF AT APPROXIMATELY 50% N1. REJECTED TAKEOFF BELOW 45 KNOTS. MAINTENANCE FOUND FAULT MESSAGE 32-62011. (LANDING WARNING INHIBIT FLIGHT). PERFORMED FIM 32-61-00. FAULT CORRECTED.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 34,314 hrs · 14,014 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR GIRT BAR CLIP LOOSE. SECURED GIRT BAR CLIP IAW STANDARD MAINTENANCE PRACTICES, OPS CHECK GOOD.

Part: WINDOW — LEAKING (COCKPIT) · airframe 33,964 hrs · 13,865 cycles

AIRCRAFT WAS GROUNDED: LOUD SQUEAL FROM FLIGHT DECK WINDOWS WHILE CLIMBING FROM 3,700 THROUGH 10,000 FT, FLIGHT RETURNED TO FIELD. REPLACED L1 (AALA202106239018) AND R1 WINDOWS IAW WORKCARDS 08L21056003 AND 08L21056004, LEAK AND OPS CHECK GOOD.

Part: WINDOW — LEAKING (COCKPIT) · airframe 33,964 hrs · 13,865 cycles

AIRCRAFT WAS GROUNDED: LOUD SQUEAL FROM FLIGHT DECK WINDOWS WHILE CLIMBING FROM 3,700 THROUGH 10,000 FT, FLIGHT RETURNED TO FIELD. REPLACED L1 AND R1 (AALA202106239019) WINDOWS IAW WORKCARDS 08L21056003 AND 08L21056004, LEAK AND OPS CHECK GOOD.

Part: GIRT BAR — LACK OF LUBE (R1 DOOR SLIDE) · airframe 33,116 hrs · 13,493 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR ON FORWARD SERVICE DOOR IS DIFFICULT TO ARM AND DISARM ON THE RIGHT SIDE. LUBRICATED GIRT BAR BRACKET R1 DOOR WITH STANDARD MAINTENANCE PRACTICES.

Part: BATTERY PACK — NO TEST (FLASHLIGHT) · airframe 31,133 hrs · 12,613 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD INBOARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY PACK AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-00.

Part: WATER HEATER — ODOR (LAVATORY) · airframe 29,618 hrs · 11,927 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS COCKPIT SMOKE LIGHT CAME ON MOMENTARILY, F/A REPORTED THE AFT RIGHT LAV SMELLS LIKE BURNING RUBBER BUT COULD NOT CONFIRM ANYTHING REALLY. MAINTENANCE REMOVED AND REPLACED AFT RH LAV WATER HEATER IAW AMM 38-13-01. NO FURTHER ODOR NOTED.

Part: DRAIN — CLOGGED (DOOR SILL) · airframe 29,185 hrs · 11,727 cycles

AIRCRAT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED THERE WAS AN IRRITATING ODOR THAT HAD A FRUITY SMELL THAT GAVE THEM A HEADACHE ON TAKE OFF AND VERY PROMINENT ON LANDING. MAINTENANCE ACCOMPLISHED CARD 05-96-70 AS APPLICABLE. UPON INITIAL TROUBLESHOOTING FOUND L1 SILL DRAIN CLOGGED AND WITH HEAVY SMELL OF CITRUS CLEANER INSIDE CLOGGED LINE. ACCOMPLISHED CARD 38-94-14, AND UNCLOGGED LINE. OPS CHECK GOOD.

Part: SILL DRAIN — ODOR (L1 DOOR) · airframe 29,174 hrs · 11,723 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN ENTRY DOOR 1L SILL DRAIN ODOR. MAINTENANCE ADDED BIOZYME AT 1L DOOR SILL DRAIN PLUGS PER AMM 38-35-00, NO FAULTS NOTED.

Part: HOSE — LEAKING (L1 DOOR) · airframe 28,796 hrs · 11,565 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS L1 DOOR WATER LEAK , BAD ODOR. MAINTENANCE REMOVED AND REPLACED L1 DOOR Y HOSE ASSY IAW AMM 38-31-00. NO LEAKS NOTED. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,741 hrs · 11,088 cycles

EMERGENCY FLASHLIGHT BENEATH FORWARD FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. REPLACED THE FLASHLIGHT IAW MM 25-64-00.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 25,410 hrs · 10,084 cycles

A CRACK WAS FOUND IN THE PRESSURE BULKHEAD WEB BS 663, BETWEEN RBL 40 TO 45.64. REPLACED THE PRESSURE BULKHEAD WEB IAW SRM 57-10-10-2R-3.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 25,410 hrs · 10,084 cycles

INDICATIONS OF TWO CRACKS IN THE LOWER SKIN ON THE RIGHT HORIZONTAL STABILIZER HSS 101.90. REPAIRED THE HORIZONTAL STABILIZER SKIN IAW SRM 55-10-01-2R-11.

Part: NOT REPORTED — MALFUNCTIONED (TE FLAP) · airframe 24,528 hrs · 9,719 cycles

AIRCRAFT WAS NOT GROUNDED. WHEN SELECTING LANDING FLAPS 30, FLAPS INDICATED 28. ON GO AROUND, SELECTED FLAPS 15 AND FLAPS DID NOT MOVE FROM 28 POSITION. LANDED NORMALLY. FLAPS RETRACTED PROPERLY ON GROUND. ACCOMPLISHED TRAILING EDGE FLAP PRIMARY CONTROL OPERATIONAL LOCKOUT PROCEDURE PER FIM 27-51-00. NO FAULTS NOTED. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 24,510 hrs · 9,709 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT THE L2 DOOR HAS A MISSING LENS COVER. REMOVED AND REPLACED LIGHT/SIGN ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: SEAL — UNSECURE (SMOKE DETECTOR) · airframe 23,023 hrs · 9,125 cycles

AFT RIGHT LAV SMOKE DETECTOR AURAL/VISUAL ALERT WITH NO VISUAL CONDITION . TAPE/SEAL NOT SECURED. SELF TEST AFT RIGHT LAV SMOKE DETECTION, SYS TEST OK AND RESECURED SEAL TAPE PER AMM 26-14-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 22,967 hrs · 9,097 cycles

EMERGENCY EXIT SIGN BASE IS CRACKED, LIGHT OPERATES AS REQUIRED LOCATED AT AFT GALLEY SERVICE DOOR. REMOVED AND REPLACED EXIT SIGN ASSY IAW AMM 33-51-01 AT AFT GALLEY SERVICE DOOR. OPS CHECKS OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 22,967 hrs · 9,097 cycles

EMERGENCY EXIT SIGN BASE IS CRACKED, LIGHT OPERATES AS REQUIRED AT THE AFT SERVICE DOOR. REMOVED AND REPLACED EXIT SIGN ASSY IAW AMM 33-51-01. OPS CHECK OK AT AFT ENTRY DOOR.

Part: LENS — DISCONNECTED (CABIN) · airframe 22,293 hrs · 8,829 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT IN FORWARD COMPARTMENT HAS A DISCONNECTED LENS COVER. REMOVED AND REPLACED THE LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 22,203 hrs · 8,783 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE PRESSURE IS BELOW LIMITS. REMOVED AND REPLACED SLIDE IAW CARD 25-94-12. OPERATIONAL CHECK GOOD.

Part: SENSOR — FAILED (THRUST REVERSER) · airframe 21,041 hrs · 8,305 cycles

LEFT ENGINE THRUST REVERSER LIGHT ILLUMINATED DURING TAKE OFF ROLL. TAKE OFF ABORTED. REMOVED & REPLACED THE LT THRUST REVERSER SLEEVE STOW PROXIMITY SENSOR AND WIRE BUNDLE HARNESS ASSEMBLY IAW AMM 78-34-02-000-801-F00. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (ZONE 400) · airframe 21,041 hrs · 8,305 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT ENGINE THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKE OFF ABORTED, ABORT SPEED UNKNOWN. REMOVED AND REPLACED LEFT THRUST REVERSER SLEEVE STOW PROXIMITY SENSOR (AALA20160920002) AND WIRE BUNDLE HARNESS ASSEMBLY IAW AMM 78-34-02-000-801-F00. OPERATIONAL CHECK GOOD.

Part: BULKHEAD — WARPED (FUSELAGE) · airframe 18,978 hrs · 7,488 cycles

AIRCRAFT WAS IN BASE MX. MLG BULKHEAD WEB AT FS 663.75 HAS THREE AREAS OF DEFLECTION, BETWEEN LBL 25 & LBL 45. REPAIRED BULKHEAD WEB IAW SRM 57-10-10-2R-3 & EA 257421.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,978 hrs · 7,488 cycles

AIRCRAFT WAS IN BASE MX. MAIN CABIN FLOOR SUPPORT AT FS 540 & LBL 1 IS CRACKED. R & R FLOOR SUPPORT IAW SRM 51-10-02 & 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,978 hrs · 7,488 cycles

AIRCRAFT WAS IN BASE MX. MAIN CABIN FLOOR SUPPORT AT FS 540 & RBL 1 IS CRACKED. R & R FLOOR SUPPORT IAW SRM 51-10-02 & 51-40-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,647 hrs · 6,956 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. FLIGHT DIVERTED BECAUSE OF THUNDERSTORMS. DURING APPROACH, THE NR 2 LE FLAP DISAGREE LIGHT CAME ON. ACCOMPLISHED FIM TASK FIM 27-AD800 WITH NO CURRENT FAULTS. NO 30 DAY FAULT HISTORY. ALL TESTS PASSED. ACCOMPLISHED VISUAL INSPECTION OF PROXIMITY SENSOR, NO FAULTS FOUND.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 17,546 hrs · 6,913 cycles

AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & AIRCRAFT OVERWEIGHT. DURING CLIMB CREW ENGAGED VNAV & SIMULTANEOUSLY LOST BOTH THE CAPTAIN’S & FIRST OFFICER`S FLIGHT DIRECTORS. R & R NUMBER 1 FCC COMPUTER IAW AMM 22-11-33. ALL REQUIRED TESTS PASSED. NO FAULTS NOTED ON FCC NUMBER 1 & ACCOMPLISHED DFCS BITE IAW FIM 22-11-00. SYSTEM CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,349 hrs · 4,511 cycles

LIGHT SURFACE CORROSION ON SKIN AT STRINGER 25 LT FROM STATIONS 986.5 TO 1006. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B737-53-031516.

Part: SIGN — BROKEN (CABIN) · airframe 9,531 hrs · 3,800 cycles

LEFT AFT DOOR EXIT IDENTIFIER BROKEN. REPLACED LEFT AFT DOOR EXIT IDENTIFIER L1190. OPS CHECK NORMAL.

Part: SIGN — BROKEN (CABIN) · airframe 9,531 hrs · 3,800 cycles

RIGHT FORWARD DOOR EXIT IDENTIFIER BROKEN. REPLACED RIGHT FORWARD DOOR EXIT IDENTIFIER L1186. OPS CHECK NORMAL.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 9,531 hrs · 3,800 cycles

DFW - CREW REPORTED LEFT HYDRAULIC LOW PRESSURE LLIGHT ILLUMINATED DURING CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE ENGINE HYDRAULIC PUMP AND CASE DRAIN FILTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 4,312 hrs · 1,595 cycles

LEFT AFT OVERWING EMERGENCY EXIT DOOR EXTERIOR LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.