N371UA

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 51,851 hrs · 35,876 cycles

DOOR 1L SLIDE PACK HAS FALLEN OUT. *S/D* SUSPECT IMPROPERLY INSTALLED. ADJUSTED GIRT BAR, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 50,880 hrs · 35,260 cycles

ESCAPE SLIDE AT 1L HAS SLACK. REPACKED SLIDE.

Part: SLIDE — DISLODGED (DOOR 1L) · airframe 49,744 hrs · 34,561 cycles

DOOR 1L SLIDE FELL OUT OF CASING. SUSPECT SLIDE IMPROPERLY INSTALLED. REPLACED L1 DOOR SLIDE ASSEMBLY IAW MM-25-61-35. AC OK FOR SERVICE.

Part: DOOR — DAMAGED (RT NLG) · airframe 49,450 hrs · 34,379 cycles

RIGHT NOSE LANDING GEAR DOOR DAMAGED LOWER EDGE FRONT 14 INCHES. REPLACED RIGHT NOSE LANDING GEAR DOOR.

Part: LANDING GEAR — INOPERATIVE · airframe 49,341 hrs · 34,311 cycles

ONCE AIRBORNE LANDING GEAR WOULD NOT RETRACT. GEAR FINALLY RETRACTED AFTER RUNNING THRU CHECKLIST. 10-11-07 FOUND AIR SAFETY SENSOR S106 GAP TO BIG. REPLACED SENSOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,328 hrs · 34,302 cycles

RIGHT OFF WING (AFT OF TRAILING EDGE) EMERGENCY EXIT LIGHT INOP. FAILED LAMP. RELAMPED- OPS CHECK GOOD.

Part: SKIN — CRACKED (BS 942 S24L) · airframe 49,326 hrs · 34,301 cycles

EXTERNAL FUSELAGE SKIN HAS A CRACK JUST FORWARD OF POTABLE WATER SERVICE PANEL BS 942 STR 24L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL FUSELAGE DOUBLER & INTERNAL TEAR STRAP DOUBLER.

Part: INTERCOSTAL — CRACKED (CABIN BODY FRAME) · airframe 49,326 hrs · 34,301 cycles

CABIN BODY FRAME INTERCOSTAL OUTBOARD CHORD IS CRACKED BS 301.1 INCH ABOVE STR 10L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REPLACEMENT INTERCOSTAL & REPLACED PARTS PER AAR EA-I070596.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

FWD GALLEY DOOR LOWER HINGE CUTOUT FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED EXTERNAL FUSELAGE DOUBLER REPAIR.

Part: INTERCOSTAL — CRACKED (CABIN BODY FRAME) · airframe 49,326 hrs · 34,301 cycles

CABIN BODY FRAME INTERCOSTAL OUTBOARD CHORD IS CRACKED BS 301 STR 13L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED INTERCOSTAL & RELATED PARTS PER AAR EA-I070550 ON NR12432-2500-0014.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

FWD ENTRY DOOR UPPER HINGE CUTOUT ONE EACH FASTENER HOLE HAS CRACK INDICATION AT FWD END OF HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REPAIR DOUBLER.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 49,326 hrs · 34,301 cycles

LEFT MLG WHEEL WELL HORIZONTAL BULKHEAD WEB IS CRACKED BS 672, LBL 42, WL 202; BS 665, LBL 39, WL 202 AND BS 665, LBL 32, WL 202. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED WEB REPLACEMENTS, DOUBLERS AND TRIPLER REPAIRS AT BOTH LBL 42 AND LBL 39.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

PASSENGER CABIN STA 294 STR 12L FRAME ATTACH ANGLE CRACKED ON LOWER SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED, FABRICATED & INSTALLED INTERCOSTAL WEB.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 49,326 hrs · 34,301 cycles

AFT CARGO DOOR FWD LOWER CORNER IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW DOUBLER & FILLER AFTER SKIN REPLACEMENT.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

AFT LAV AREA RIGHT CROSSBEAM CORRODED AT BS 1006 TO BS 1016 BL 4R TO 10R WL 208. MAJOR REPAIR ACCOMPLISHED: REPLACED CROSSBEAM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

FWD ENTRY DOOR AFT FRAME STOP SIXTH STOP FITTING CUTOUT HOLE FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACK. INSTALLED ANGLE REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

CABIN BODY FRAME INTERCOSTAL CLIP IS CRACKED BS 295 STR 11L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

PASSENGER CABIN STA 290 JUST ABOVE & BELOW STR 13R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED ANGLE. DRILLED UP & INSTALLED NEW ANGLES. DINOLED AREA.

Part: CROSSBEAM — CORRODED (FUESLAGE) · airframe 49,326 hrs · 34,301 cycles

AFT LAV AREA LEFT CROSSBEAM CORRODED AT BS 1006 TO BS 1016 AT BL 4L TO 10L WL 208. MAJOR REPAIR ACCOMPLISHED: REPLACED CROSSBEAM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

AFT LAV AREA SMALL WALL ANGLE CORRODED AT BS 1013 TO BS 1016 BL 4L TO 6L AT WL 208. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED AFT LAV WALL ANGLE.

Part: SHEAR TIE — DAMAGED (BS 727A S20-21L) · airframe 49,326 hrs · 34,301 cycles

AFT PIT SHEAR TIE DAMAGED STA 727A STR 20L TO 21L. MAJOR REPAIR ACCOMPLISHED: REMOVED OLD SHEAR TIE MFG AND INSTALLED NEW SHEAR TIE.

Part: SKIN — CRACKED (BS 814-816) · airframe 49,556 hrs · 34,120 cycles

EXTERNAL FUSELAGE SKIN HAS CRACK INDICATION AT STR 14L CHEM MILL STEP BTWN BS 814 AND BS 816. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED EXTERNAL FUSELAGE DOUBLER REPAIR.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,326 hrs · 34,301 cycles

DORSAL FIN SKIN STA 860 PHENOLIC STRIP TORN AND POSSIBLE SKIN WEAR WHERE STRIP WAS TORN. REPAIRED AND INSTALLED DORSAL FIN.

Part: CREASE BEAM — CRACKED (BS 639) · airframe 49,556 hrs · 34,120 cycles

FOUND CREASE BEAM WEB CRACKED AT BS 639L, LBL 62. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR ON CREASE BEAM WEB.

Part: TORQUE TUBE — FAULTY (PAX DOOR) · airframe 49,326 hrs · 34,301 cycles

AFT ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REPLACED UPPER AND LOWER BEARING TORQUE TUBE.

Part: DOOR FRAME — CRACKED (FWD CARGO DOOR) · airframe 49,326 hrs · 34,301 cycles

FWD CARGO DOOR LOWER AFT FRAME CRACKED IN RADIUS OF OUTER CHORD. MAJOR REPAIR ACP'D, REMOVED AND REPLACED FRAME SECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

AFT LAV AREA FLOORBEAM CORRODED BS 1016 BL 4R-8R. MAJOR REPAIR: REMOVED DAMAGED SECTION OF STA 1016 FLOORBEAM CAP LBL 10 TO RBL 21 AND REPAIRED.

Part: DOOR FRAME — CRACKED (FWD GALLEY DOOR) · airframe 49,326 hrs · 34,301 cycles

FWD GALLEY DOOR LOWER FWD FRAME IS CRACKED AT 2 EA FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

AFT CARGO DOOR CUTOUT STA 847 STR 22, PREVIOUS REPAIR REMOVED FOR SKIN REPLACEMENT. MAJOR REPAIR ACCOMPLISHED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 49,326 hrs · 34,301 cycles

FWD ENTRY DOOR CRACK ON INNER SKIN AND FRAME AFT SIDE AT SEVENTH STOP FITTING FROM TOP. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER/ANGLE REPAIR.

Part: FRAME — CRACKED (BS 616) · airframe 49,326 hrs · 34,301 cycles

FOUND OVERWING FRAME INNER CHORD IS CRACKED AT BS 616L, JUST BELOW STR 17. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME INNER CHORD AT STA 616L BELOW S17L WITH STIFFENER ANGLE AND FILLER.

Part: ANGLE — CRACKED (BS 290) · airframe 49,326 hrs · 34,301 cycles

FOUND PASSENGER CABIN STA 290 JUST BELOW STR 11R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. REPLACED WITH NEW ANGLE (REF SRM 51-40-02 PGS 1-2-6)

Part: FLOORBEAM — CORRODED (BS 294) · airframe 49,326 hrs · 34,301 cycles

FLOORBEAM CORRODED: CABIN BS 294.5, LBL 6-7 WATERLINE 208, UPPER FLANGE CAP. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 49,326 hrs · 34,301 cycles

ANGLE CRACKED, PASS CABIN FWD OF GALLEY DOOR STA 290 JUST ABOVE STR 10R, INTERCOSTAL WEB ATTACH ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED CRACKED ANGLE.

Part: ANGLE — CRACKED (FUSLEAGE) · airframe 49,326 hrs · 34,301 cycles

PASSENGER CABIN STA 290 JUST ABOVE STR 11R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. REPLACED WITH NEW ANGLE.

Part: SLIDE — UNSECURE (DOOR 1R) · airframe 48,865 hrs · 34,037 cycles

DOOR 1R SLIDE PACK IS HANGING DOWN. [07-24-07] REPACKED SLIDE.

Part: SLIDE — UNSECURE (DOOR 1L) · airframe 47,750 hrs · 33,379 cycles

DOOR 1L SLIDE FELL OUT OF SLIDE CONTAINER. SECURED DOOR SLIDE.

Part: DOOR FRAME — CRACKED (BS 440 S24R) · airframe 47,453 hrs · 33,177 cycles

FWD PIT DOOR CUTOUT FWD FRAME CRACKED AT BS 440 NEAR STR S24R. MAJOR REPAIR: REMOVED CRACK AND ACCOMPLISHED NDT. FABRICATED AND INSTALLED TWO NESTED ANGLE EXTERNAL REPAIRS TO FRAME. REFERENCE AAR EA I060515 AND UA-EVA 60714.

Part: DOOR FRAME — CRACKED (BS 400) · airframe 47,453 hrs · 33,177 cycles

FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 400 NEAR STRINGER S24R. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED TWO NESTED ANGLE REPAIR DOUBLERS. REFERENCE AAR EA I060515 AND UA-EVA-60714.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,453 hrs · 33,177 cycles

FWD CARGO PIT DOOR CUTOUT AFT FRAME CRACKED AT INBD RADIUS NEAR STRINGER S24R. MAJOR REPAIR: REMOVED AND REPLACED FORWARD CARGO PIT DOOR CUTOUT AFT FRAME. REFERENCE SRM 51-40-02 PG 1-30.

Part: SKIN — GOUGED (BS 807 S26R) · airframe 47,453 hrs · 33,177 cycles

EXTERNAL SKIN HAS BLENDED GOUGE AT BS 807 JUST BELOW STRINGER S-25R & ANOTHER AT BS 801 JUST ABOVE STR S-26R AT FWD LWR CORNER OF AFT PIT DOOR CUTOUT. MAJOR REPAIR: BLENDED GOUGES. FABRICATED AND INSTALLED EXTERNAL DOUBLER, TRIPLER AND STRUCTURAL FILLER REPAIR. REFERENCE EA I060528.

Part: WIRE HARNESS — BURNED · airframe 47,453 hrs · 33,177 cycles

E&E COMP DRIP SHIELD MOISTURE BARRIER ABOVE E-3 SHELVES IS BURNED AND ABOVE NR 2 TR UNIT, WIRE BUNDLE ABOVE HAS SIGNS OF BURN, HEAT DAMAGE. FOUND NR 2 TRANSFORMER RECTIFIER UNIT FOUND OVERHEATED. REPLACED NR 2 TRU AND REINSTALLED A NEW DRIP SHIELD.

Part: FRAME — CRACKED (BS 695) · airframe 47,453 hrs · 33,177 cycles

RH WHEEL WELL BS 695 FRAME INNER CHORD ANGLE CRACKED JUST ABOVE AND AFT OF MLG UPLOCK MECHANISM. MAJOR REPAIR: INSTALLED REPLACEMENT FRAME ANGLE. REFERENCE SRM 51-40-02 AND MM 53-10-98 PG 1-3.

Part: FRAME — CRACKED (BS 695) · airframe 47,453 hrs · 33,177 cycles

BS 695 FRAME CRACKED IN LOWER RADIUS ABOVE & AFT OF LT MLG UPLOCK MECHANISM IN LT MLG WW. MAJOR REPAIR: REMOVED AND REPLACED ANGLE. REFERENCE SRM 51-40-02 AND MM 53-10-98.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,891 hrs · 32,819 cycles

LANDED ORD UNDER AMBER ALERT DUE TO FLAP PROBLEM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,704 hrs · 32,703 cycles

DOOR 1L EMERGENCY EXIT LIGHT AND FIRST CLASS EEL FLOOR STRIP IS INOP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,412 hrs · 31,889 cycles

FUSELAGE HAS THREE INCH CRACK BEHIND LT WING EMERGENCY EXIT LIGHT AREA. ACCOMPLISHED CATEGORY B REPAIR REF. SRM 53-00-01. CRITICAL FASTNER ROW WILL NEED INSPECTION AT 60,000 CYCLES AFTERINSTALLATION OF REPAIR. ** MF5633 CREATED TO MONITOR **

Part: RECEPTACLE — FAILED (GALLEY) · airframe 43,986 hrs · 30,965 cycles

AFT VACUUM CB OUT. FA REPORTED SPARKS IN GALLEY POPPED. FAILED RECEPTACLE NOT RECOVERED. AMT SAYS FOUND IT IN TWO PIECES. CAUSE OF FAILURE MAY BE DETERIORATION OVER TIME. INCONCLUSIVE WITHOUT FAILED PART.

Part: WARNING LIGHT — ACTIVATED (COCKPIT) · airframe 42,995 hrs · 30,392 cycles

FLIGHT RETURNED TO DEN DUE TO B-SYSTEM HYDRAULIC PRESSURE LIGHT. PROBLEM COULD NOT BE REPEATED ON GROUND. OPS CHECKED OK. NO UNITS REPLACED.

Part: SPAR — CRACKED (LT WING) · airframe 40,240 hrs · 28,408 cycles

LT WING SPAR UPPER CHORD CRACKED AT MLG BEAM SUPPORT FITTING. MAJOR REPAIR ACCOMPLISHED. SPLICED NEW CHORD.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

LWR FUSELAGE SKIN DENTED AT STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

FUSELAGE SKIN DENTED STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

FUSELAGE SKIN GOUGED AT STA 737 STR 1L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

FORWARD CARGO DOOR FRAME GOUGED STA 490. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA AND INSTALLED REPAIR PARTS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

STRINGER CLIP AT STA 727C LBL 52 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER CLIP.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,240 hrs · 28,408 cycles

DENTED FUSLAGE SKIN AT BS 311 BELOW STR 18R REQUIRES REPAIR. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 37,745 hrs · 26,619 cycles

FLIGHT ABORTED TAKEOFF AT HIGH SPEED DUE TO ERRATIC AIRSPEED INDICATION. ABORT TAKEOFF DUE TO AIRSPEED INDICATOR RED FLAG AND LOSS OF POINTER. REPLACED THE CAPTAINS MACH AIRSPEED INDICATOR AND THE NR 1 AIR DATA COMPUTER. THE MACH AIRSPEED INDICATOR REMOVED WAS FOUND TO HAVE A FAULTY POWER SUPPLY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,937 hrs · 24,264 cycles

BS 178 BULKHEAD RT LOWER WEATHER RADAR ANTENNA MOUNT HAS THREE CRACKS. REPAIRED CRACKED WEATHER RADAR ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED.

Part: ACTUATOR — FAILED (LE FLAPS) · airframe 34,801 hrs · 24,153 cycles

LEADING EDGE FLAP EXTENSION PROBLEM. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR. OPS CHECKED NORMAL.

Part: WARNING SYSTEM — ACTIVATED (AFT BODY) · airframe 33,999 hrs · 23,454 cycles

AFT BODY OVERHEAT INDICATION FOLLOWED BY AN ABNORMAL ODOR IN THE COCKPIT. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED ENGINE RUN-UP ON BOTH ENGINES, AND PERFORMED PNEUMATIC SYSTEM TEST. NO BURNING SMELL AND NO AFT BODY OVERHEAT LIGHT ILLUMINATED.

Part: ROD — OUT OF ADJ (MLG DOOR ACT) · airframe 32,695 hrs · 22,295 cycles

LANDING GEAR INDICATION PROBLEM. *S/D* ADJUSTED RIGHT HAND GEAR DOOR ACTUATION ROD. OPERATIONS CHECK GOOD.

Part: ACTUATOR — FAILED (NLG) · airframe 31,214 hrs · 20,941 cycles

THE NOSE LANDING GEAR RED LIGHT WOULD NOT EXTINGUISH WITH THE LANDING GEAR HANDLE IN THE RETRACTED POSITION. *S/D* REPLACED THE NOSE LANDING GEAR ACTUATOR. TESTED THE NOSE LANDING GEAR LOGIC, POSITION AND WARNING SYSTEM.

Part: FLOORBEAM — CRACKED (BS 927)

DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF THE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEVERAL EEL LIGHTS IN THE AFT CABIN ARE INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: CONTROLLER — INOPERATIVE (E/E COMPT)

AIRCRAFT DIVERTED TO LAX DUE TO LOSS OF CABIN PRESSURIZATION. *S/D* REPLACED CABIN PRESSURE CONTROLLER, CHECKS OK.

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 THROUGH ROW 17. REPLACED BATTERY PACK. CHECKS OK.