N441US

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,228 hrs · 43,632 cycles

PASSENGER CABIN (2 EACH ) EMERGENCY LIGHTS BATTERY INOPERATIVE. REMOVED AND REPLACED 2 EACH BATTERY PACK OF EMERGENCY LIGHT IAW AMM 33-51-51, PAGE 202, OPERATIONAL CHECK GOOD IAW AMM 33-51-51, PAGE 204. REMOVED UNITS S/N: 35570 AT STA 753L AND S/N: 53156 AT STA 727G (M1435).

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 62,928 hrs · 42,950 cycles

R1 DOOR SLIDE FOUND TO HAVE SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED THE DOOR SLIDE IAW AMM 25-61-35.

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 62,928 hrs · 42,950 cycles

R2 DOOR SLIDE FOUND TO HAVE SEVERAL EMERGENCY LIGHTS ON THE SLIDE INOPERATIVE. REMOVED AND REPLACED THE R2 DOOR SLIDE IAW AMM 25-61-35.

Part: SLIDE — NO TEST (R1 DOOR) · airframe 62,928 hrs · 42,950 cycles

R1 DOOR SLIDE FAILED TO DEPLOY DURING DEMONSTRATION. INFLATION BOTTLE SHOWED DEPLETED AFTER ATTEMPT. REMOVED AND REPLACED THE R1 DOOR SLIDE IAW AMM 25-61-35.

Part: STRUCTURE — HANDLER ERROR (VERTICAL STAB) · airframe 65,857 hrs · 44,474 cycles

DURING TOWING RH VERTICAL STABILIZER HIT ANOTHER AIRCRAFT. DAMAGE LOCATED BETWEEN FIN STATION 283.50 AND 209.90. RUDDER STATION 196.46 APPROXIMATELY

Part: LIGHT — BROKEN (CABIN) · airframe 60,378 hrs · 41,507 cycles

EMERGENCY EXIT LIGHT ASSY BROKEN FWD OF RT PAX DOOR. R & R EMERGENCY EXIT SIGN.

Part: WIRE — BROKEN (CABIN) · airframe 60,171 hrs · 41,380 cycles

MAINTENANCE FOUND BROKEN WIRING IN LOWER PORTION OF FORWARD COAT CLOSET. MAINTENANCE REPAIRED BROKEN WIRING IN FORWARD COAT CLOSET (EMERGENCY LIGHT) PER MPPM 54-01-10. OPS CHECK GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 59,685 hrs · 41,086 cycles

MAINTENANCE REPORTED THAT PAX SEAT 11C EMERGENCY LIGHT IS LOOSE AND HANGING. MAINTENANCE SECURED EMERGENCY LIGHT ASSEMBLY AT PAX SEAT 11C.

Part: WIRE — DISCONNECTED (CABIN) · airframe 59,685 hrs · 41,086 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT PAX SEAT 21C INOP. MAINTENANCE RECONNECTED WIRES FOR EMERGENCY EXIT LIGHT AT PAX SEAT 21C. OPS CHECK OK.

Part: ATTACH BOLT — MISSING (L2 DOOR) · airframe 59,632 hrs · 41,053 cycles

CREW REPORTED THE L2 DOOR DOES NOT CLOSE PROPERLY. MAINTENANCE FOUND L2 DOOR UPPER GATE NOT MOVING. REMOVED DOOR LINER AND REPLACED UPPER GATE PUSHROD ATTACH BOLT PER AMM 52-13-61. OPS CHECKED GOOD PER AMM 52-13-00-705-034. OK FOR SERVICE.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,496 hrs · 40,968 cycles

C6 CHECK - DELAMINATION ON UPPER SURFACE OF RIGHT OUTBOARD FOREFLAP ASSEMBLY AT CENTER SECTION OF TRAILING EDGE WEDGE. REPLACED RIGHT OUTBOARD FOREFLAP ASSEMBLY IAW B737 AMM 27-51-37.

Part: SIGN — MISSING (CABIN) · airframe 59,180 hrs · 40,773 cycles

CREW REPORTED THE EXIT SIGN AT SIDEWALL OF EXIT ROW, AIRCRAFT RIGHT, MISSING. MAINTENANCE INSTALLED EXIT SIGN AT EXIT ROW SEAT.

Part: LENS — UNSECURE (CABIN) · airframe 58,921 hrs · 40,600 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LENS ABOVE ROW 11 LEFT HAS FALLEN OFF. MAINTENANCE RE-INSTALLED EXIT SIGN LENS ABOVE LEFT AIRCRAFT ROW 11. OPS CHECK NORMAL.

Part: MECHANISM — FAULTY (AILERON) · airframe 58,163 hrs · 40,114 cycles

EN ROUTE FROM EWR TO CLT, CREW REPORTED WHEN MOVING AILERON TO THE LEFT, THERE SEEMS TO BE A "CATCH" AT ABOUT 4 UNITS ON THE AILERON TRIM INDICATOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AILERON ARTIFICIAL CENTERING AND TRIM MECHANISM PER AMM 27-11-81-004-001 AND AMM 27-11-81-404-006.

Part: GUIDE ARM — OUT OF ADJUST (ENTRY DOOR) · airframe 58,053 hrs · 40,053 cycles

CREW REPORTED THE AFT LEFT ENTRY DOOR IS HARD TO CLOSE. MAINTENANCE ADJUSTED GUIDE ARM ON AFT LEFT ENTRY DOOR PER AMM 52-13-31-401 AND PERFORMED AN OPERATIONAL TEST PER AMM 52-13-00-703. OPS CHECK GOOD. DOOR FUNCTIONS NORMALLY.

Part: BEARING — DAMAGED (AILERON) · airframe 57,983 hrs · 40,009 cycles

CREW REPORTED THE AILERONS BINDING WHEN YOU ARE TURNING THE YOKE TO ABOUT 2 ON BOTH TURNING LEFT OR RIGHT. MAINTENANCE TROUBLESHOT TO AILERON ARTIFICIAL FEEL AND CENTERING BEARING FROZE AND FLAT SIDED. REMOVED AND REPLACED BEARING PER AMM 27-11-81-410-801. ACCOMPLISHED AILERON ARTIFICIAL FEEL, CENTERING AND TRIM ADJUSTMENT. REFERENCE AMM 27-11-81-805-018.

Part: PLACARD — MISSING (CABIN) · airframe 57,689 hrs · 39,825 cycles

MAINTENANCE REPORTED THE EXIT PLACARD AT ROW 11 MISSING. MAINTENANCE INSTALLED PLACARD. OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 57,585 hrs · 39,762 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS AT EMERGENCY EXIT ROW WAS MISSING. MAINTENANCE REPLACED EMERGENCY LIGHT LENS AT EMERGENCY EXIT ROW.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,420 hrs · 39,657 cycles

C5 CHECK - 2 CRACKS ON LOWER FUSELAGE SKIN AT EXHAUST PORT DUCT AT BS 380, LBL 3. REPAIRED LOWER FUSELAGE SKIN AT EXHAUST PORT DUCT AT BS 380, LBL 3 IAW EA 103809.

Part: SEAL — DETERIORATED (EMERGENCY LIGHT) · airframe 57,419 hrs · 39,657 cycles

C5 CHECK - EMERGENCY LIGHTING AFT OF THE RIGHT WING TRAILING EDGE, WING TO BODY FAIRING IS INOP. FOUND MOISTURE DETERIORATED SEAL & BAD LIGHT BULB. CLEANED OUT MOISTURE IN AREA, REPLACED LIGHT BULB & GASKET & SEALED OUTER LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CUSHION — INTERFERENCE (CABIN) · airframe 57,260 hrs · 39,563 cycles

CREW REPORTED THE FORWARD ENTRY DOOR WAS HARD TO OPEN/CLOSE. NEEDS LUBE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT HEAD CUSHION TO PREVENT INTERFERENCE WITH FORWARD ENTRY DOOR WHILE CLOSING. OPERATIONAL CHECK GOOD.

Part: BOLT — BROKEN (FLAP TRACK) · airframe 56,936 hrs · 39,366 cycles

CREW REPORTED THAT THE AIRCRAFT REQUIRES 2.5 UNITS OF RUDDER TRIM TO THE LEFT. (FLAPS 40 DEGREES, FUEL BALANCED AILERON TRIM 0 BALL IN CENTER) NOTE: AT CRUISE, RUDDER TRIM 0. MAINTENANCE REPLACED BROKEN AND MISSING BOLT AT NR 3 AFT OUTBOARD FLAP TRACK PER AMM 27-51-39. OPS CHECK GOOD.

Part: PUSHROD — OUT OF ADJUST (R1 DOOR) · airframe 56,922 hrs · 39,356 cycles

MAINTENANCE REPORTED THE R1 SERVICE DOOR FOR NOT CLOSING. MAINTENANCE FOUND THE UPPER ROLLER TO BE ROTATING BEFORE GOING INTO THE LATCH FITTING. ADJUSTED HORIZONTAL PUSH ROD FROM TORQUE TUBE. ALSO, ADJUSTED GUIDE ARM SO THE FORWARD AND AFT LATCH ROLLERS ENTER THE LATCH FITTING AT THE SAME TIME. ACCOMPLISHED PER AMM 52-41-00-705.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 56,601 hrs · 39,158 cycles

MEGAPHONE INOPERATIVE, WILL NOT TEST. REMOVED AND REPLACED MEGAPHONE IAW AMM 25-60-00, OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 56,301 hrs · 38,970 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS AT ROW 11L MISSING. MAINTENANCE INSTALLED LENS. AIRCRAFT OK FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 56,101 hrs · 38,842 cycles

DURING CRUISE (APPROXIMATELY 1 HOUR FLIGHT), FLIGHT ATTENDANTS REPORTED AN ODOR OF DIRTY SOCKS/BURNING OIL SMELL IN THE AREA OF SEAT ROWS 18-23. WHEN APPROACHING ROW 18 IT WAS LIKE WALKING INTO A WALL OF ODOR. ON DESCENT, IT SEEMED TO DISSIPATE AND WE ISOLATED THE PACKS BUT NO CONCLUSIONS COULD BE DRAWN. MAINTENANCE ACCOMPLISHED J/C 03L00021001 AND FOUND UPON ENTERING THE AFT CARGO FORWARD WALL AREA, A BURNT SMELL. NOTICED APU BLEED DUCT INSULATION DISCOLORED AND HOT. REMOVED PANEL, INSPECTED AND FOUND NO LEAKS. UPGRADED INSULATION AND REINSTALLED PANEL. FOUND FRONT SIDE OF APU ACCESSORY SECTION WET WITH OIL. UNABLE TO DETERMINE LEAK. PLACED APU ON MEL 49-01A. CHECKED FOR OIL WETNESS IN DUCTS FROM ACM'S, NONE NOTED. REPLACED BOTH HEPA FILTERS. THE FOLLOWING DAY, MAINTENANCE CHECKED APU FOR OIL LEAKS. NONE FOUND. FOUND APU OIL QUANTITY OVERSERVICED. REMOVED EXCESS OIL. REMOVED/CLEARED MEL 49-01A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,767 hrs · 38,636 cycles

FPBH INSPECTION - CRACK ON SKIN CLIP ANGLE BETWEEN BS 294.5 TO BS 303.9, S10L. REPLACED SKIN CLIP ANGLE IAW B737 SRM 51-20-05 & BOEING DRAWING 65-17684.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,767 hrs · 38,636 cycles

FPBH INSPECTION - CRACK ON CLIP AT BS 360 BETWEEN S14L TO S15L. REPLACED CLIP AT BS 360 BETWEEN S14L TO S15L IAW B737 SRM 51-40-02 & AIRBUS DRAWING 69-58280.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 55,767 hrs · 38,636 cycles

FPBH INSPECTION - CRACK ON U-CHANNEL AT BS 360, S14L. REPLACED U-CHANNEL AT BS 360, S14L IAW B737 SRM 51-40-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,767 hrs · 38,636 cycles

FPBH INSPECTION - CRACK ON WEB AT BS 180, WL 207, LBL 27. REPLACED WEB AT BS 180, WL 207, LBL 27 IAW BOEING DRAWING 65-45833.

Part: LIGHT — MISSING (CABIN)

CLT - CREW REPORTED THE EMERGENCY EXIT LIGHT MISSING ON SEAT ROW 12, LEFT SIDE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ON SEAT ROW 12, LEFT SIDE. OPS CHECK SATISFACTORY IN ASSOCIATION WITH B737 MM 33-51.

Part: SKIN — DELAMINATED (SPOILER) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - DELAMINATION ON NR 6 SPOILER PANEL UPPER SKIN AT WBL 210. REPLACED NR 6 SPOILER PANEL IAW B737 AMM 27-61-11.

Part: SKIN — DELAMINATED (SPOILER) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - DELAMINATION ON NR 3 SPOILER PANEL UPPER SKIN. REPLACED NR 3 SPOILER IAW B737 AMM 27-61-11.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - L-1 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR SLIDE IAW JOB CARD 03C10552002.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - TWO CRACKS ON FUSELAGE SKIN AT BS 727F + 3 INCHES & BS 727F + 8.5 INCHES, S21L. REPAIRED FUSELAGE SKIN AT BS 727F + 3 INCHES & BS 727F + 8.5 INCHES, S21L IAW B737 SRM 53-00-01 REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - CRACK ON FUSELAGE SKIN AT BS 727F, S23L. REPAIRED FUSELAGE SKIN AT BS 727F, S23L IAW B737 SRM 53-00-01 REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,958 hrs · 38,125 cycles

CLT - C4 - CRACK ON FUSELAGE SKIN JUST FORWARD OF BS 727F, S24R. REPAIRED FUSELAGE SKIN JUST FORWARD OF BS 727F, S24R IAW B737 SRM 53-00-01 REPAIR 31.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FLL - MAINTENANCE REPORTED THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS, FORWARD AND AFT OF EMERGENCY EXIT HATCHES LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1479 POWER SUPPLY IN ASSOCIATION WITH MM 33-51-51. OPERATIONAL TEST OF EMERGENCY LIGHTS GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN)

DCA - MAINTENANCE REPORTED THE AFT MEGAPHONE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT MEGAPHONE. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS)

ORD - MAINTENANCE REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT 7ABC INOPERATIVE. MAINTENANCE REPAIRED WIRE CONNECTOR AT FLOOR LEVEL EMERGENCY LIGHT AT SEAT 7ABC PER SWPM CHAPTER 20-13-13. OPERATIONAL CHECK NORMAL.

Part: SKIN — DELAMINATED (SPOILER) · airframe 52,442 hrs · 36,562 cycles

CLT - C3 - MAJOR REPAIR - DELAMINATION ON LEFT WING NR 2 SPOILER UPPER SURFACE ABOVE ACTUATOR ATTACH POINT. REPLACED LEFT WING NR 2 SPOILER IAW B737 AMM 27-61-11.

Part: FUSE — BLOWN (CABIN) · airframe 52,442 hrs · 36,562 cycles

CLT - C3 - EEL - SEAT MOUNTED EMERGENCY LIGHTS ARE NOT WORKING ON ROW 24 LEFT & 25 LEFT. REPLACED FUSE F1 ON BATTERY PACK M1137.

Part: WIRE — DISCONNECTED (CABIN)

CLT - MAINTENANCE REPORTED THE FORWARD COAT CLOSET EMERGENCY LIGHTS WERE INOPERATIVE. THE WIRING HARNESS WAS EXPOSED AND THE PROTECTIVE COVER WAS BROKEN. MAINTENANCE RECONNECTED WIRES AND SECURED PROTECTIVE COVER. OPERATIONAL CHECK NORMAL.

Part: FUSE — BLOWN (CABIN)

ORD - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT SEAT ROWS 24, 25 AND RIGHT AFT SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED FUSE IN BATTERY SUPPLY UNIT IN AFT CABIN. OPS CHECK GOOD PER MM 33-51-51.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,226 hrs · 36,428 cycles

CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727E + 12.5 INCHES, S23R. REPAIRED FUSELAGE SKIN AT BS 727E + 12.5 INCHES, S23R IAW B737 SRM 53-00-01 REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,226 hrs · 36,428 cycles

CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727G, S25L. REPAIRED FUSELAGE SKIN AT BS 727G, S25L IAW EA 101763.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

CLT - MAINTENANCE REPORTED THE BULLNOSE EMERGENCY LIGHT ON OVERHEAD BIN, ROW 22 RIGHT, IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT CHARGER ASSEMBLY/BATTERY AT RIGHT AFT GALLEY PER MM 33-51-51-201. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

BDL - MAINTENANCE REPORTED THE L1 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: FUSE — BLOWN (POWER SUPPLY)

BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS ON LAST TWO SEAT ROWS (24 & 25 LEFT SIDE) AND EXTERIOR EMERGENCY LIGHT FOR AFT SERVICE DOOR (STA 1000R) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE ON POWER SUPPLY M1137 AT STA 960 OVERHEAD. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,423 hrs · 35,944 cycles

CLT - RON - EEL - LEFT FORWARD CABIN AND L1 DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY BATTERY PACK M1133 IAW AMM 33-51-51-2. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT LEFT EXIT HATCH AND CENTER AISLE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M1134 PER MM 33-51-51. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,109 hrs · 35,760 cycles

CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, S23R. REPAIRED FUSELAGE SKIN AT BS 727D, S23R IAW B737 SRM 53-00-01 REPAIR 31.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLL - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT LEFT WING FORWARD AND LEFT AFT WING LOWER EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND BATTERY. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - EEL - EMERGENCY LIGHTS INOP FROM PASSENGER SEATS ROW 1 TO ROW 5 LEFT SIDE ONLY. REPLACED FORWARD & AFT BATTERY SUPPLY IAW B737 AMM 33-51-51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 500C BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS500C BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON EXTERNAL DOUBLER AT AFT SERVICE DOOR CUTOUT AT FUSELAGE SKIN LOWER LOBE, BS 527 BETWEEN S28L TO S28R. REPAIRED EXTERNAL DOUBLER AT AFT SERVICE DOOR CUTOUT AT FUSELAGE SKIN LOWER LOBE, BS 527 BETWEEN S28L TO S28R IAW US AIRWAYS TYPICAL REPAIR 53-30-10.

Part: SUPPORT ANGLE — CRACKED (ENTRY DOOR) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON LOWER SUPPORT ANGLE AT BS 990, WL 213 OF AFT ENTRY DOOR. REPLACED LOWER SUPPORT ANGLE AT BS 990, WL 213 OF AFT ENTRY DOOR IAW B737 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT FORWARD ENTRY DOOR CUTOUT BS 312 BETWEEN S9L TO S10L. REPAIRED FUSELAGE SKIN AT FORWARD ENTRY DOOR CUTOUT BS 312 BETWEEN S9L TO S10L IAW US AIRWAYS EA 132366.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON LOWER SUPPORT ANGLE AT BS 344, WL 209.8 OF FORWARD ENTRY DOOR. REPLACED LOWER SUPPORT ANGLE AT BS 344, WL 209.8 OF FORWARD ENTRY DOOR IAW B737 SRM 51-10-02.

Part: PIN — CORRODED (HORIZ STAB) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON INNER PIN SURFACE AT LEFT HORIZONTAL STABILIZER CENTER SECTION HINGE. REPLACED INNER PIN AT LEFT HORIZONTAL STABILIZER CENTER SECTION HINGE IAW US AIRWAYS TASK CARD 03T70927003.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER HARDWARE ATTACHMENT HINGE FITTING 1 TO 6. REPLACED LEFT HORIZONTAL STABILIZER HARDWARE ATTACHMENT HINGE FITTING 1 TO 6 IAW B737 AMM 20-50-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500G AT S21L. REPAIRED FRAME AT BS 500G AT S21L IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500F AT S21R. REPAIRED FRAME AT BS 500F AT S21R IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500C BETWEEN S20L TO S21L ALSO BETWEEN S20R TO S21R. REPAIRED FRAME AT BS 500C BETWEEN S20L TO S21L & ALSO BETWEEN S20R TO S21R IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500D BETWEEN S20L TO S21L. REPAIRED FRAME AT BS 500D BETWEEN S20L TO S21L IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500B BETWEEN S20L TO S21L. REPAIRED FRAME AT BS 500B BETWEEN S20L TO S21L IAW B737 SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FRAME AT HOLE EDGE AT BS 500E BETWEEN S20L TO S21L ALSO BETWEEN S20R TO S21R. REPAIRED FRAME AT BS 500E BETWEEN S20L TO S21L & ALSO BETWEEN S20R TO S21R IAW B737 SRM 53-00-07.

Part: STOP FITTING — CORRODED (ENTRY DOOR) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON STOP FITTING (4 EA) OF LEFT AFT ENTRY DOOR FORWARD EDGE. REPLACED STOP FITTING (4 EA) OF LEFT AFT ENTRY DOOR FORWARD EDGE IAW B737 OHM 52-16-03.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN BETWEEN BS 1016 TO BS 1032 & BETWEEN S24R TO S27L. REPAIRED FUSELAGE SKIN BETWEEN BS 1016 TO BS 1032 & BETWEEN S24R TO S27L IAW US AIRWAYS EA 132357.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 400 BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 400 BETWEEN S8R TO S9R IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 500,863 hrs · 5,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 867 BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 867 BETWEEN S8R TO S9R IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 727F BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 727F BETWEEN S8L TO S9L IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 727B BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 727B BETWEEN S8R TO S9R IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 727D BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 727D BETWEEN S8L TO S9L IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 727F BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 727F BETWEEN S8R TO S9R IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 500A BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 500A BETWEEN S8L TO S9L IAW US AIRWAYS EA 132382.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 480 BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 480 BETWEEN S8R TO S9R IAW US AIRWAYS EA 132382.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - EEL - LOW BATTERY ON EMERGENCY LAMP AT AFT FLIGHT ATTENDANTS SEAT, 2 EACH LEFT SIDE. REPLACED BATTERY ON EMERGENCY LAMP AT AFT FLIGHT ATTENDANTS SEAT, 2 EACH LEFT SIDE IAW B737 AMM 25-60-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - FRAME CRACKED AT BS 400 BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 400 BETWEEN S8L TO S9L IAW US AIRWAYS EA 132382.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON NR 6 SLAT LOWER SKIN SURFACE BETWEEN SS293 TO SS380. REPAIRED NR 6 SLAT LOWER SKIN BETWEEN SS293 TO SS380 IAW B737 SRM 57-43-01 REPAIR 6.

Part: SLAT — DELAMINATED (LT WING) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - DELAMINATION ON OUTBOARD END OF NR 2 SLAT AT SLAT STA 247.27 TO SLAT STA 254.27, WBL 420 TO WBL 426. REPAIRED OUTBOARD END OF NR 2 SLAT AT SLAT STA 247.27 TO SLAT STA 254.27, WBL 420 TO WBL 426 IAW B737 SRM 51-70-10.

Part: SLAT — DELAMINATED (NR 2) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - NR 2 SLAT DELAMINATED ON INBOARD END AT SLAT STA 124.53 TO SLAT STA 130.53, WBL 323.75 TO WBL 329.75. REPAIRED NR 2 SLAT ON INBOARD END IAW B737 SRM 51-70-10.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON NR 6 SLAT UPPER SKIN AT OUTBOARD END BETWEEN SS363 TO SS389. REPAIRED NR 6 SLAT UPPER SKIN AT OUTBOARD END BETWEEN SS363 TO SS389 IAW B737 SRM 57-43-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FLOORBEAM SUPPORT "T" CHORD UPPER FLANGE AT BS 727 +17 INCHES, RBL 24.75. REPAIRED FLOORBEAM SUPPORT "T" CHORD UPPER FLANGE AT BS 727 +17 INCHES, RBL 24.75 IAW US AIRWAYS EA 132351.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK IN FLOORBEAM UPPER CHORD AT BS 727A + 17 INCHES, RBL 45.5. REPAIRED FLOORBEAM UPPER CHORD AT BS 727A + 17 INCHES, RBL 45.5 IAW US AIRWAYS EA 132351.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT BS 727C TO BS 727D + 6 INCHES, LBL 45.50. REPAIRED SEAT TRACK AT BS 727C TO BS 727D + 6 INCHES, LBL 45.50 IAW B737 SRM 53-00-52 REPAIR 4.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON LOWER SUPPORT ANGLE AT FORWARD ENTRY DOOR BS 312, WL 209.8. REPAIRED LOWER SUPPORT ANGLE AT FORWARD ENTRY DOOR BS 312, WL 209.8 IAW B737 SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,086 hrs · 24,812 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON INTERCOSTAL AT BS 537.5, LBL 2.75. REPLACED INTERCOSTAL AT BS 537.5, LBL 2.75 IAW B737 SRM 51-10-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK IN VERTICAL BEAM WEB OF BS 178 BULKHEAD AT RBL 17.1 BETWEEN WL 220 TO WL 234. REPAIRED VERTICAL BEAM WEB OF BS 178 BULKHEAD AT RBL 17.1 BETWEEN WL 220 TO WL 234 IAW B737 SRM 53-10-08 REPAIR 12.

Part: PAN — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK IN SUPPORT PAN AT BS 500C, S21L. REPLACED SUPPORT PAN AT BS 500C, S21L IAW B737 SRM 51-10-02 & BOEING DRAWING 65C27308.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT BS 1006 BETWEEN S27R TO S27L. REPLACED SHEAR TIE AT BS 1006 BETWEEN S27R TO S27L IAW B737 SRM 51-10-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION SEAT TRACK AT BS 540.5, RBL 24.75. REPAIRED SEAT TRACK AT BS 540.5, RBL 24.75 IAW B737 SRM 53-00-51 REPAIR 6.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON UPPER ZEE CHORD AT BS 270 BETWEEN RBL 11 TO LBL 11. REPAIRED UPPER ZEE CHORD AT BS 270 BETWEEN RBL 11 TO LBL 11 IAW B737 SRM 51-70-12.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON VERTICAL BEAM UPPER WEB AT BS 178 BULKHEAD, LBL 17.1. REPAIRED VERTICAL BEAM UPPER WEB AT BS 178 BULKHEAD, LBL 17.1 IAW B737 SRM 53-10-08 REPAIR 12.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON STIFFENER BETWEEN BS 590 TO BS 640, LBL 40. REPLACED STIFFENER BETWEEN BS 590 TO BS 640, LBL 40 IAW SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 500G, S26L. REPLACED TIE CLIP AT BS 500G, S26L IAW B737 SRM 51-10-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON SUPPORT ANGLE AT BS 500D, S21R. REPLACED SUPPORT ANGLE AT BS 500D, S21R IAW B737 SRM 51-10-02.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 50,086 hrs · 35,130 cycles

MAJOR REPAIR - CORROSION ON SUPPORT ANGLE BETWEEN BS 601 TO BS 610, WL 208.1, RBL 64.5. REPAIRED SUPPORT ANGLE BETWEEN BS 601 TO BS 610, WL 208.1, RBL 64.5 IAW SRM 51-70-11. REMOVED LEVEL 2 CORROSION INDICATOR AS THIS ITEM WAS SELECTED IN ERROR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FUSELAGE FRAME WEB AT BS 1006, BETWEEN S27R TO S27L. REPAIRED FUSELAGE FRAME WEB AT BS 1006, BETWEEN S27R TO S27L IAW B737 SRM 53-00-07 REPAIR 1.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON CHANNEL AT BS 537.75, RBL 2.75. REPLACED CHANNEL AT BS 537.75, RBL 2.75 IAW B737 SRM 51-10-2.

Part: SLAT — DELAMINATED (NR 4) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - DELAMINATION ON MID POSITION OF NR 4 SLAT TRAILING EDGE AT SLAT STA 72.25. REPAIRED NR 4 SLAT TRAILING EDGE AT SLAT STA 72.25 IAW B737 SRM 51-70-10 REPAIR 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN FORWARD OF ENTRY DOOR UPPER & LOWER HINGE CUTOUTS AT BS 303.9, BETWEEN S12L TO S13L. REPAIRED FUSELAGE SKIN FORWARD OF ENTRY DOOR UPPER & LOWER HINGE CUTOUTS AT BS 303.9, BETWEEN S12L TO S13L IAW US AIRWAYS EA 132341.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - EEL - LOW BATTERY ON EMERGENCY LAMP AFT GALLEY AREA RIGHT SIDE. REPLACED BATTERY ON EMERGENCY LAMP AFT GALLEY AREA RIGHT SIDE.

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR WEB AT BS 989, LBL 32. REPLACED SHEAR WEB AT BS 989, LBL 32 IAW SRM 53-60-051 & DRAWING 65C33533.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT BS 336 BETWEEN, RBL 45 TO RBL 60. REPLACED FLOOR SUPPORT AT BS 336 BETWEEN, RBL 45 TO RBL 60 IAW SRM 51-10-02 & 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON STIFFENER BETWEEN BS 312 TO BS 328, AT RBL 11. REPLACED STIFFENER BETWEEN BS 312 TO BS 328, AT RBL 11 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION SUPPORT Z-ANGLE AT BS 962 & BS 967, LBL 60 AT L2 DOOR. REPLACED SUPPORT Z-ANGLE AT BS 962 & BS 967, LBL 60 AT L2 DOOR IAW B737 SRM 51-10-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE BETWEEN BS 294.5 TO BS 329, RBL 60. REPLACED SUPPORT ANGLE BETWEEN BS 294.5 TO BS 329, RBL 60 IAW B737 SRM 51-10-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 500,863 hrs · 5,130 cycles

SAL - Q6 - MAJOR REPAIR - FILIFORM CORROSION ON BEAM ZEE AT BS 933.5 BETWEEN LBL 33 TO LBL 43.5. REPLACED BEAM ZEE AT BS 933.5 BETWEEN LBL 33 TO LBL 43.5 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE INNER CHORD BETWEEN BS 963 TO BS 994, LBL 53. REPAIRED SUPPORT ANGLE INNER CHORD BETWEEN BS 963 TO BS 994, LBL 53 IAW B737 SRM 51-70-11.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE INNER CHORD BETWEEN BS 955 TO BS 993, RBL 53. REPLACED SUPPORT ANGLE INNER CHORD BETWEEN BS 955 TO BS 993, RBL 53 IAW B737 SRM 51-10-02 & BOEING DRAWING 65-45855.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK AT BS 344, RBL 24.75. REPAIRED SEAT TRACK AT BS 344, RBL 24.75 IAW SRM 53-00-52.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON CHORD AT BS 296, RBL 17. REPLACED CHORD AT BS 296, RBL 17 IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER CHORD AT BS 344 BETWEEN BL 0 TO LBL 45. REPAIRED FLOORBEAM UPPER CHORD AT BS 344 BETWEEN BL 0 TO LBL 45 IAW B737 SRM 53-10-51.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT Z-ANGLE AT BS 982 AT L2 DOOR. REPLACED SUPPORT Z-ANGLE AT BS 982 AT L2 DOOR IAW B737 SRM 51-10-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,083 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE OF SCUFF PLATE LOWER SILL AREA BETWEEN BS 312 TO BS 344, LBL 64. REPAIRED SUPPORT ANGLE OF SCUFF PLATE LOWER SILL AREA BETWEEN BS 312 TO BS 344, LBL 64 IAW B737 SRM 51-70-12.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 947 TO BS 967, RBL 49. REPLACED INTERCOSTAL BETWEEN BS 947 TO BS 967, RBL 49 IAW SRM 51-10-02 & 51-40-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON WEB BETWEEN BS 312 TO BS 328, RBL 33. REPLACED WEB BETWEEN BS 312 TO BS 328, RBL 33 IAW B737 SRM 51-10-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - C6 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK AT BS 294, RBL 45. REPLACED SEAT TRACK AT BS 294, RBL 45 IAW SRM 53-00-52.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FITTING BETWEEN BS 967 TO BS 982 AT L-2 DOOR. REPAIRED FITTING BETWEEN BS 967 TO BS 982 AT L-2 DOOR IAW B737 SRM 51-10-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - DOUBLER CRACKED ON FRAME AT FORWARD ENTRY LOWER DOOR STOP AT BS 303.9, S16L. REPAIRED DOUBLER ON FRAME AT FORWARD ENTRY LOWER DOOR STOP AT BS 303.9, S16L IAW US AIRWAYS TASK CARD M1L53001.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION SUPPORT Z-ANGLE AT BS 977 AT L2 DOOR. REPLACED SUPPORT Z-ANGLE AT BS 977 AT L2 DOOR IAW B737 SRM 51-10-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 277 TO BS 294, RBL 17. REPLACED SEAT TRACK BETWEEN BS 277 TO BS 294, RBL 17 IAW SRM 53-00-52.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE OF LOWER SILL SCUFF PLATE AT L1 DOOR AT BS 312 TO BS 344, LBL 67. REPLACED SUPPORT ANGLE OF LOWER SILL SCUFF PLATE AT L1 DOOR AT BS 312 TO BS 344, LBL 67 IAW B737 SRM 51-10-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BEAM ASSEMBLY BETWEEN BS 294.5 TO BS 360 AT S17L, LBL 60. REPLACED LOWER SILL BEAM ASSEMBLY BETWEEN BS 294.5 TO BS 360 AT S17L, LBL 60 IAW B737 SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 947 TO BS 967, RBL 16. REPLACED FLOOR SUPPORT BETWEEN BS 947 TO BS 967, RBL 16 IAW SRM 51-10-02 & DRAWING 65C33375.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - GALVANIC CORROSION ON WEB UPPER SURFACE BETWEEN BS 294.5 TO BS 312, RBL 3. REPLACED WEB UPPER SURFACE BETWEEN BS 294.5 TO BS 312, RBL 3 IAW DRAWING 65-45834.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON LOWER STRAP BETWEEN BS 807 TO BS 847, S25R. REPLACED LOWER STRAP BETWEEN BS 807 TO BS 847, S25R IAW B737 SRM 51-10-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CHANNEL AT BS 727E, RBL 8.10 ABOVE S26R. REPAIRED CHANNEL AT BS 727E, RBL 8.10 ABOVE S26R IAW SRM 53-00-53.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CORROSION ON CHANNEL BETWEEN BS 767 TO BS 787 & BETWEEN S25R TO S26R. REPLACED CHANNEL BETWEEN BS 767 TO BS 787 & BETWEEN S25R TO S26R IAW B737 SRM 51-10-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 807, S25L. REPLACED TIE CLIP AT BS 807, S25L IAW B737 SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL WEB BETWEEN BS 847 TO BS 867 & BETWEEN S25R TO S26R. REPLACED INTERCOSTAL WEB BETWEEN BS 847 TO BS 867 & BETWEEN S25R TO S26R IAW B737 SRM 51-10-02.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 50,086 hrs · 35,130 cycles

SAL - Q6 - MAJOR REPAIR - DELAMINATION ON LEFT ELEVATOR LEADING EDGE UPPER SKIN AT ELEV STA 24.90. REPAIRED LEFT ELEVATOR LEADING EDGE UPPER SKIN AT ELEV STA 24.90. REPAIRED IAW US AIRWAYS EA 132372.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,902 hrs · 35,022 cycles

CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 942, S24L. REPAIRED FUSELAGE SKIN AT BS 942, S24L IAW US AIRWAYS EA 100911.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,730 hrs · 33,706 cycles

CLT - MAJOR REPAIR - C1 CHECK - CRACKED FUSELAGE SKIN, BS 727F, S26L. REPAIRED FUSELAGE SKIN, BS 727F, S26L IAW B737 SRM 53-00-01 REPAIR 31.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

DFW - MAINTENANCE REPORTED THE LOWER EMERGENCY PATH LIGHTING AT SEAT 17, LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED WIRING BENEATH SEAT 17L. OPERATIONAL CHECK GOOD.

Part: INDICATOR — FAULTY (COCKPIT)

PIT FLT 1512 - ON APPROACH TO PIT, AS CREW SELECTED FLAPS PAST 5 UNITS, A SPLIT FLAPS CONDITION OCCURRED AND THE FLAPS STOPPED MOVING. CREW RETURNED FLAP LEVER TO 5 UNITS AND FLAPS CAME BACK TO A SYMMETRICAL POSITION. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT 5 UNITS. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41-4. OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED A WORN RIGHT-HAND INBOARD FOREFLAP AND TOGGLE ASSEMBLY. OPERATIONAL CHECK OF FLAPS NORMAL.

Part: FLAP — MALFUNCTIONED (WING)

JAX - FLT 1652 - ON APPROACH TO JAX, CREW REPORTED WHEN SELECTING FLAPS TO 15 UNITS, FLAPS STAYED AT 10 UNITS. CREW ACCOMPLISHED GO-AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. WHEN CREW PLACED FLAP SELECTOR BACK TO 10 UNITS, FLAP INDICATOR WAS NOW IN AGREEMENT. CREW THEN SELECTED FLAPS TO 15 UNITS AND FLAPS OPERATED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED FLAPS, TORQUE TUBES AND CABLES WITH NO DISCREPANCIES FOUND. OPERATED FLAPS SEVERAL TIMES. FLAPS OPERATED NORMAL.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 45,647 hrs · 32,403 cycles

A .5 INCH CRACK AT FWD CARGO DOOR OPENING, AFT FRAME BS 492, LOWER DOOR STOP FITTING, S-24R. CUT OUT DAMAGED AREA, FABRICATED & INSTALLED REPAIR FILLER & ANGLES PER EA 98795.

Part: WEDGE — WORN (T/E FLAP) · airframe 45,180 hrs · 45,180 cycles

WEAR MARKS LEFT INBOAD MID FLAP TRAILING EDGE WEDGE, UNDERSIDE 34 INCHES FROM I/B END. INSTALLED BONDED REPAIR DOUBLER PER EA 98647, DEFECT SIZE: 6 INCHES.

Part: SLAT — CRACKED (L/E SLAT) · airframe 45,180 hrs · 45,180 cycles

LOWER L/E WBL 279.25 IN LINE WITH O/B AUX TRACK. FAB'D & INSTALLED FILLER & DOUBLER PER SRM 57-43-01. DEFECT SIZE: .25"

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,180 hrs · 45,180 cycles

STA 727E + 2", S-24L. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, REPAIR 31. DEFECT SIZE: 1.5"

Part: WEDGE — DAMAGED (T/E FLAP) · airframe 45,180 hrs · 45,180 cycles

LT I/B TE FLAP WEDGE. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER PER EA 98647. DEFECT SIZE: 3" DIA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,180 hrs · 45,180 cycles

UPPER AFT CORNER OF DOOR HANDLE CUTOUT. REMOVED DAMAGE, INSTALLED FABRICATED REPAIR PARTS PER TR 52-10-01A. DEFECT SIZE: 1/4" CRACK

Part: SKIN — CRACKED (BS 727E) · airframe 45,070 hrs

A 3 INCH CRACK FOUND ON SKIN, RIGHT SIDE AT STA 727E + 3 INCHES. REMOVED DAMAGED AREA & INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REP 31.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 44,904 hrs · 31,917 cycles

A 2.25 INCH CRACK FOUND AT LT HORIZONTAL STAB LWR SKIN STA 115. INSTALLED DOUBLER PER SRM 55-10-01.

Part: LIGHT — INOPERATIVE (CABIN)

CLT MAINTENANCE REPORTED THE EMERGENCY LIGHT, AT SEAT ROW 12, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,823 hrs · 42,823 cycles

STRINGER 24R BETWEEN STA 727E AND 727F CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01, DEFECT SIZE: .25 INCH.

Part: CABLE — FAULTY (NR 1 ENGINE VSV)

DURING CRUISE AT FL340, CREW REPORTED ENGINES WERE FLUCTUATING 0.4% N1 FUEL FLOW FROM 2,600 TO 2,630 LBS. ALL GAUGES FLUCTUATING. ENGINES WOULD NOT STAY IN SYNC. PMC ON OR OFF MADE NO DIFFERENCE. AUTOTHROTTLES OFF FLUCTUATED AT 0.6%. DURING A TURN, FLUCTUATION WAS 1.0% N1 AND 2,600 TO 2,700 LBS FUEL FLOW. DIVERTED TO CLT. ON DESCENT AT FL170, OPERATION RETURNED TO NORMAL. MX TROUBLESHOT PER MM 71-00-42 AND FOUND THE NR 1 ENGINE VSV FEEDBACK CABLE BAD. REPLACED CABLE PER MM 75-31-00. RAN ENGINES PER MM 71-00-00 TEST 8, ACCEL/DECEL TEST. OPERATIONAL CHECK NORMAL. ALSO, REPLACED BOTH ENGINE FUEL FILTERS PER MM 73-11-02. NO FUEL OR FUEL FILTER CONTAMINANTS FOUND. RAN ENGINES. NO LEAKS NOTED.

Part: SKIN — GOUGED (RUDDER) · airframe 42,036 hrs · 42,036 cycles

BELOW RUDDER STA 17.25 COMPOSITE LEADING EDGE. REPAIRED PER EA 82094 FIG 1 PG 2 & 3. DEFECT SIZE: 6 EA. GOUGES

Part: SKIN — CRACKED (BS 757F) · airframe 41,145 hrs · 29,396 cycles

FOUND 2.25" CRACK FOUND AT BS 727F S-25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201.

Part: SUPPORT FITTING — CRACKED (MLG BEAM ATTACH)

CLT - Q5 - AFT SUPPORT FITTING, 1 INCH, CRACKED, FASTENER HOLE AT MLG BEAM ATTACH PT TO AFT SPAR ON AFT SUPPORT FITTING UP CHRD. REPAIR OF FITTING INCLUDED REAMING OF DISCREP HOLE, SHIMMING IAW EA. (K)

Part: SKIN — WORN

CLT - Q - SKIN, 12 INCHES X .250 INCH X .015 INCH, SKIN WEAR, BS870, WL306.5, LBL3. INSTALLED REPAIR DOUBLER AND INSTALLED NEW RUB STRIPS IAW EA, WEIGHT CHANGE OF 1.5 LBS. (K)

Part: BALANCE ARM — WORN (RUDDER)

CLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)

Part: ANGLE — CRACKED (LT SIDE)

CLT - Q5 - ANGLE, .375 INCH, CRACKED AT STA 601LT SIDE BODY WING TERMINAL FORGING ANGLE CRACKED ON AFT SIDE. REMOVED DAMAGED AND INSTALLED REPAIR ANGLE IAW SRM. (K)

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

CLT - FOUND PRESSURE DECK CRACKED .750 INCH, STATION 664 LBL 32.5. REMOVED DAMAGED DAMAGED AREA, INSTALLED REPAIR IAW SRM 53-60-04. (M)

Part: SPLICE — CORRODED (FLOOR PANEL)

CLT - FOUND SPLICE STRAP CORRODED .5 INCH, AFT CARGO FLOOR PANEL SPLICE STRAP. FABRICATED NEW STRAP AND INSTALLED IAW SRM 51-10-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED .5 INCH, CENTER AISLE FRAME BETWEEN STATION 380 AND 400. FABRICATED AND INSTALLED NEW PART IAW SRM 51-10-02. (M)

Part: SPLICE — CRACKED (FUSELAGE)

FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4R. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

CLT - FOUND SKIN WITH LIGHTNING STRIKE .125 INCH BY .125 INCH, STATION 500B, 2 INCHES BELOW STRINGER 18L AND 12 AFT. FASTENER INSTALLED IN SKIN IAW 53-00-01 FIG 219. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, FORWARD CABIN FLOOR STRUCTURE STATION 310 RBL 13 TOP OF SUPPORT INBOARD SCREW HOLE. REMOVED DAMAGED STIFFENER, FRILLED UP AND INSTALLED PART IAW SRM 53-10-51 FIG 101, PAGE 105. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

CLT - FOUND SKIN WITH LIGHTNING STRIKE, STATION 469, 4 INCHES ABOVE STRINGER 21L. FASTENER INSTALLED IN SKIN IAW 737 SRM 53-00-01 FIG 219. (M)

Part: SPLICE — CRACKED (FUSELAGE)

CLT - FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4L. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ANGLE CRACKED .750 INCH, STATION 616 LT SIDE BODY WING TERMINAL FORGING ANGLE, CRACKED ON FORWARD SIDE. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW RT 53-62-01. (M)

Part: FITTING — CORRODED (HORIZONTAL STAB)

FOUND FITTING CORRODED .25 BY .25, HORIZONTAL STAB CTR SECTION, RT SIDE, FORWARD SPAR. SPOT FACED FORWARD FACE OF FORWARD LUG IAW 55-10-10. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, BS 306 LBL 11 FORWARD CABIN FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL IAW SRM 53-10-51, 51-10-02, 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CLT - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1.5 INCH, STATION 312 RBL 10. NEW TEE CAP INSTALLED IAW SRM 53-10-01, AND SRM 53-00-51. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

CLT - Q5 - FLOOR STIFFENER, 2 INCH X 16 INCH CORROSION, STA 312-328, LBL12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLT - Q5 - STA 328-344, LBL9, 2 INCH X 2 INCH, CORROSION, FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLT - Q5 - FLOOR SUPPORT, 2 INCH X 2 INCH CORROSION, STA 312-328, RBL 13. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER SUPPORT IAW SRM. (K)

Part: SKIN — GOUGED (TE FLAP)

CLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K)

Part: SKIN — WORN (LT OB MID FLAP)

MID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K)

Part: CIRCUIT CARD — FAULTY (E/E BAY)

CLT - FLT 255 - ON APPROACH TO CLT, AT APPROX 5,000 FEET, THE CREW DID NOT RECEIVE A GREEN LIGHT FOR THE RIGHT MAIN LANDING GEAR UPON GEAR EXTENSION. CAPTAIN ABORTED APPROACH AND HAD A DEAD HEAD FIRST OFFICER VISUALLY CHECK FOR GEAR EXTENSION. IT WAS DETERMINED THAT THE GEAR WAS DOWN. FLIGHT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE CHECKED THE INTEGRITY OF THE RIGHT MLG DOWNLOCK SENSOR S73. SENSOR CHECKS GOOD. FOUND D4574 CONTAMINATED. CLEANED D4574. PERFORMED INDICATION CHECK PER MM TASK 32-61-31-714-017. INDICATION CHECKS GOOD. REMOVED AND REPLACED M981 LOGIC CARD PER MM TASK 32-09-20-844-019. INDICATION CHECKS GOOD. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND SKIN CRACKED 3 INCHES, RIGHT SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACK SECTION OF SKIN AND INSTALLED .63 INCHES EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND SKIN CRACKED 3 INCHES, RIGHT FUSELAGE SKIN BETWEEN STATION 727E-727F AT STATION 25R. REMOVED CRACKED SECTION OF SKIN AND INSTALLED .063 INCH EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TPA - MAINTENANCE FOUND A SEGMENT OF SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY ON SEAT ROW 9ABC. OPS CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (CABIN)

BDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6, 7, 8 AND 9ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK NORMAL. (M)

Part: FRAME — CORRODED (BS 794)

PIT - FOUND FRAME CORRODED 4 INCHES BY .500 INCHES CORRODED, FORWARD FUSELAGE DOOR FRAME BS 794 ABOVE S25R. CORROSION LEVEL 1, TASK NR C53-100-01. INSTALLED DOUBLER PER SRM 53-60-15 AND EA 71737. (M)

Part: SKIN

PIT - FOUND SKIN WITH OVAL WEAR MARK, .071 INCH .375 INCH DIAMETER, RIGHT A/C BAY ABOVE ACM VALVE CENTER TANK LOWER SKIN. REAMED DAMAGE TO .25 INCH DIAMETER, INSTALLED FASTENER SAME SIZE AS HOLE PER EA 71719. (M)

Part: ELEVATOR

PIT - FOUND ELEVATOR HAS CARBON DELAMINATION, .040 INCH DEEP BY .25 INCH DIAMETER, BOTTOM SIDE OF ELEVATOR 52 INCHES FROM BOTTOM END. REPAIR PER SRM 55-20-1 AND 51-70-17 PER EA 71791. (M)

Part: REGULATOR — FAILED (NR 2 ENGINE)

DCA - FLT 1893 - EN ROUTE FROM CLT-DCA, AT FL270, THE RIGHT ENGINE BLEED TRIPPED OFF FOLLOWED BY THE LEFT ENGINE BLEED TRIPPING OFF. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DESCENDED TO FL100. PERFORMED AUTO FAIL AND UNSCHEDULED PRESSURE CHANGE CHECKLIST. BOTH ENGINE/WING ANTI-ICE WERE NOTED ON AT THE TIME. FLIGHT LANDED AT DCA WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED THE NR 2 ENGINE PRSOV BLEED AIR REGULATOR. PERFORMED GROUND RUN. ALL BLEED PARAMETERS WITHIN LIMITS. ALSO, REMOVED AND RPLACED THE NR 1 AND NR 2 ENGINE 490 DEGREE TEMPERATUR SWITCHES (P/N 975-0172-006) AND THE NR 1 ENGINE PRSOV BLEED AIR REGULATOR (P/N 107492-2) AS PRECAUTIONARY. NO OTHER DEFECTS NOTED. (M)

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

CLT - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHT INOP. MAINTENANCE CLEANED THE LIGHT SOCKET, RELAMPED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M)

Part: STRAP — CORROSION (BS 798)

CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION. CORRODED STRAP MEASURING 1 INCH AT STATION 798 R, FRAME REINFORCING STRAP LOCATED AT 798 R FRAME. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. FABRICATED NEW DOUBLER AND TRIPLER AS PER EA 59179. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE - MAINTENANCE FOUND THE AFT RIGHT FUSELAGE, EXTERNAL EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

TPA - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE, 10R, 12L AND 20L OVERHEADS, RIGHT OVERWING AND LEFT LOWER FUSELAGE LIGHTS. MAINTENANCE REPLACED THE BATTERY PACK IN OVERHEAD AT STATION 753L. OPS CHECK GOOD. (M)

Part: FAIRING — LOOSE (WING)

CLT - FLT 2442 - ON CLIMB, AIRFRAME VIBRATION AT HGH POWER SETTNGS. NO VIBRATION AT IDLE POWER DESCENT OR LOW POWER SETTING. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE RUN AT ALL POWER SETTINGS. VIBRATION INDICATION NEVER EXCEEDED .5. PERFORMED AVM SIGNAL CHECK, BITE CHECKED OK. FOUND WING TO BODY FAIRING SEAL LOOSE. SEALED WING TO BODY FAIRINGS. OK FOR SERVICE. (W)