N338UA

Part: LIGHT — BUCKLED (ROW 6) · airframe 56,259 hrs · 31,463 cycles

FOUND EMERGENCY LIGHTS AT ROW 6 BUCKLED. STRAIGHTENED LIGHT AT ROW 6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,259 hrs · 31,463 cycles

AFT SECTION EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED POWER STRIP.

Part: SKIN — CRACKED (BS 890-892 S10R) · airframe 55,339 hrs · 30,865 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT CHEM-MILLED STEP, AT STR 10R, FROM STA 890-892. FABRICATED AND INSTALLED EXTERNAL DOUBLER-FILLER REPAIR PER MM 53-31-96 FIGURE 602.

Part: SLAT SYSTEM — SLOW (NR 2) · airframe 55,186 hrs · 30,760 cycles

NR 2 L/E SLAT SLOW TO EXTEND. LAGS NR 1 & 3 L/E SLATS IN EXTEND AND RETRACT. [07-06-07] FOUND FAULTY NR 2 ACTUATOR. REPLACED NR 2 ACTUATOR. FOUND WORN SEALS. REPLACED SEALS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,413 hrs · 30,278 cycles

LEFT AFT OVERWING EMERGENCY EXIT LIGHT ON EXTERIOR OF ACFT INOPERATIVE. RELAMPED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 52,596 hrs · 29,142 cycles

AFT EMERGENCY LIGHT SCAM ON AFTER T/O. RECYCLED F/A SWITCH AND LIGHT TURNED OFF BUT CAME BACK ON. REPLACED BATTERY PACK CHARGER AND REPAIRED EEL LIGHTING STRIP AT AFT GALLEY CART LOCATION.

Part: SKIN — GOUGED (BS 362 S17L) · airframe 51,247 hrs · 28,349 cycles

FUSELAGE SKIN GOUGED AT STA 362, STR 17L. *S/D* TRIPLER REPAIR WITH RE-INFORCING STRINGER REPAIR ACP'D.

Part: STRINGER — CRACKED (BS 297 S10L) · airframe 51,247 hrs · 28,349 cycles

STRINGER 10L UPPER FLANGE CRACKED AT STA 297. *S/D* INSTALLED STRAP AND STRINGER CLIP REPAIR PER EA I060076-IR & EVA-60082.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 51,247 hrs · 28,349 cycles

LEFT HORIZONTAL STAB LWR SURFACE CRACKED, AFT SIDE JUST FWD OF ELEV STA 98. LT HORIZONTAL STAB LOWER SURFACE FOUND CRACKED. NEW SKIN SECTION WAS SPLICED IN BETWEEN STATIONS 105.7 AND 180. REFERENCE AAR EO 1060094 AND APPROVED WITH AN 8100-9 FORM.

Part: DOOR FRAME — CRACKED (BS 1618) · airframe 51,247 hrs · 28,349 cycles

FWD CARGO DOOR BS 1618 CRACK AT INBD RADIUS AT AFT LOWER FRAME. *S/D* DAMAGE REMOVED, INSTALLED NEW FRAME PER SRM 51-40-02. ACCOMPLISHED ON BASE WRITE UP, 10991-8100-0013. NO FURTHER FINDINGS, OK FOR SERVICE.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 51,247 hrs · 28,349 cycles

RIGHT HORIZONTAL STABILZER HAS DENT APPROX 4 FT OUTBOARD ON LEADING EDGE. DENT MEASURES 2"L X 1.25W X .125D. RIGHT HORIZONTAL STABILIZER LEADING EDGE SKIN REPLACED TO ADDRESS DENT.

Part: STRINGER — MISDRILLED (S20L BS 907) · airframe 51,247 hrs · 28,349 cycles

STR 20L STA 907 HAS MISDRILLED HOLE IN UPPER FLANGE OF STRINGER. REMOVED DAMAGE SECTION ACCOMPLISHED REPAIR PER SRM 53-00-03. INSTALLED A SPLICE.

Part: FASTENER — MISINSTALLED (BS 864) · airframe 51,247 hrs · 28,349 cycles

STRINGER CLIP AT STA 867 STRINGER 20R INSTALLED WITH LOCK FASTENER THAT FAIL MAXIMUM PROTRUSION TEST ON GO-NO GO GAGE. REMOVED & INSTALLED NEW STRINGER CLIP & FASTENERS REF 51-40-02.

Part: SKIN — DENTED (BS 1050 S25R) · airframe 51,247 hrs · 28,349 cycles

AFT FUSELAGE STA 1050 S25R IN JACK SCREW COMPARTMENT HAS DENT. DAMAGE REMOVED AND STR 25R REPAIRED REF SRM 53-00-03 REPAIR 1.

Part: BULKHEAD — DAMAGED (BS 727) · airframe 51,247 hrs · 28,349 cycles

AFT CARGO PIT FWD BULKHEAD STA 727 STRINGER 27R FWD ATTACHMENT FASTENERS 3RD AND 4TH FROM BOTTOM ARE WORKING. INSTALLED NEW STA 727 BULKHEAD FITTING AT STR 27R REF SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (RT MLG) · airframe 51,247 hrs · 28,349 cycles

THE RIGHT MLG BEAM O/B ATTACH FITTING WAS FOUND CRACKED AT HOLE D. RIGHT MAIN LANDING GEAR SUPPORT BEAM FITTING REPLACED PER JIC 4S127. RELATED TO AD 2005-18-08. COA 930022 SIGNED OFF TO RECORD TERMINATING ACTION FOR AD.

Part: ATTACH ANGLE — CRACKED (BS 727) · airframe 51,247 hrs · 28,349 cycles

AFT PIT BILGE STA 727 STR 27L ATTACH ANGLE COMMON TO BULKHEAD IS CRACKED AT 4TH FASTENER FROM BOTTOM OF ANGLE. INSTALLED NEW STA 727 BULKHEAD FITTING AT STR 27L REF SRM 51-40-02.

Part: STRINGER — DENTED (BS 907) · airframe 51,247 hrs · 28,349 cycles

AFT CARGO PIT STA 907 STR 24L, STR AND STR SPLICE DENTED AT HOLES FROM FASTENER REMOVAL. MAJOR REPAIR ACP'D, HAT CHANNEL DOUBLER REPAIR ACP'D PER SRM 53-00-03 PG 201.

Part: CREASE BEAM — CORRODED (BS 294-336) · airframe 51,247 hrs · 28,349 cycles

FWD RIGHT ENTRY DOOR CREASE BEAM HAS SEVERAL AREAS OF CORROSION STA 294 TO 336, RBL 70, WL 208. NEW CREASE BEAM INSTALLED PER SRM 51-40-02.

Part: STRINGER — DAMAGED (S20R BS 727A) · airframe 51,247 hrs · 28,349 cycles

STR 20R DAMAGED AT STA 727A. REPAIRED STRINGER REF SRM 53-60-03 REPAIR 1.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 51,247 hrs · 28,349 cycles

FWD SIDE OF 1016 BULKHEAD FOUND 3 EACH CRACKS AT FASTENERS IN WEB ABOVE STIFFENER 7L RIVETS 7, 8, AND 9. *S/D* REMOVED DAMAGE INSTALLED FILLER, DOUBLER, TRIPLER SEALED EDGES, & DINOLED REF SRM 53-80-08.

Part: ANGLE — CRACKED (BS 1142) · airframe 51,247 hrs · 28,349 cycles

AFT RIGHT FUSELAGE, BS 1142, CUTOUT FOR HORIZONTAL STAB AFT SPAR ATTACH FITTINGS, UPPER-INSIDE CHORD ANGLE, CRACK, 2 INCH -3 INCH LONG. *S/D* REPAIRED CHORD ANGLE REF MM 53-10-93.

Part: SKIN — CRACKED (AFT GALLEY DOOR) · airframe 51,247 hrs · 28,349 cycles

AFT GALLEY DOOR LOWER HINGE CUTOUT, SKIN CRACKED IN FWD RADIUS BY SPRING LOADED DOOR. REPAIRED CRACK AT AFT GALLEY DOOR LOWER HINGE CUTOUT REF SRM 53-60-01 REPAIR 7.

Part: ANGLE — CRACKED (BS 1142) · airframe 51,247 hrs · 28,349 cycles

AFT LEFT FUSELAGE BS 1142, CUTOUT FOR HORIZ STAB AFT SPAR FITTINGS, UPPER-INSIDE CHORD ANGLE, CRACK APPROX 2.5 INCHES LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE REF SRM 51-70-11.

Part: LAP JOINT — CRACKED (STR 10L BS 421) · airframe 51,247 hrs · 28,349 cycles

SKIN LAP AT STR 10L STA 421 TO STA 429 IS CRACKED AT CHEM MILLED STEP. PER JC REPAIR PER MM 53-31-96 OR SRM 53-00-01 FIG 229 IF WITHIN SRM LIMITATIONS. FASTENERS AND DAMAGE REMOVED, NDT FOR CRACKS. INSURANCE CUT MADE & DEBURRED. REPAIR DOUBLERS MADE & AREA TREATED & PRIMED. REPAIRS INSTALLED, PRIMED & PAINTED, REF SRM 53-00-01 REPAIR NR 31 DETAIL XV, 737 NDT MAN. PART 6 51-00-00 FIG 23, FIG 16 & 53-30-00, 057806 FIG 3, 53-30-18. NO DEFECTS, & GNMM 5-0-4-024.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,100 hrs · 28,255 cycles

EMERGENCY FLOOR LIGHTING INOP AT ROW 17 AFT.

Part: LIGHT — SHORTED (ROW 15) · airframe 49,425 hrs · 27,296 cycles

EMERGENCY EXIT FLOOR LIGHTS BEYOND ROW 15 INOP. LIGHT STRIP SHORTED, REPLACED.

Part: RIVET — CRACKED (UNKNOWN) · airframe 51,247 hrs · 28,349 cycles

CRACKED RIVETS. REPLACED RIVETS REF SRM 51-40-02 & 53-00-01.

Part: CIRCUIT CARD — FAILED (MLG) · airframe 45,978 hrs · 25,326 cycles

UNABLE TO RAISE THE LANDING GEAR AFTER TAKEOFF. REPLACED MAIN GEAR LOGIC CARD M991.

Part: MANIFOLD — BROKEN (APU FUEL)

FUEL LEAK APU AUTO SHUTDOWN. APU DEFERRED. C/B PULLED. FOUND LEAK AT FUEL HEATER. HEATER NOT LEAKING. MAIN FUEL MANIFOLD CRACKED AT 11:00 O`CLOCK POSITION AT FUEL NOZZLE (INJECTOR) MANIFOLD HAS 14 FUEL TUBES. ONE HAS A BROKEN TUBE BETWEEN THE FLEXIBLE FIRE SLEEVE AND THE B-NUT TO THE FUEL INJECTOR. PART SENT TO LAB FOR ANALYSIS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

FRAME 188 AT WL 207 STRINGER 17L HAS CRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR DOUBLER AND INSTALLED EXTERNAL FUSELAGE DOUBLER.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

LEFT WHEEL WELL UPPER BULKHEAD CRACKED AT LBL 31 STATION 663.75 + 2. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

STATION 312-360, WL 208, LBL 56 INBOARD CHORD ON CREASE BEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. CHORD REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

CABIN BODY FRAME WEB IS CRACKED AT PSU SUPPORT BRACKET FASTENER BODY STATION 380, STRINGER 8L - 9L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

CABIN BODY STUB FRAME OUTER FLANGE IS CRACKED AT BODY STATION 296 STRINGER 8R. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME STUB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

STATION 1006, WL 208 LBL 26, FLOORBEAM MATERIAL LOSS AFTER CORROSION REMOVAL EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLOORBEAM REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

FUSELAGE SKIN DENTED AT STATION 1005 AFT OF DOOR 2L BETWEEN STRINGER 12L AND 13L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FITTING — CHAFED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

CABIN FLOORBEAM EXPANSION BOLT IS WEARING INTO FITTING AT STATION 520, RBL 45 AFT SIDE OF FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. EXPANSION JOINT REPLACED.

Part: FRAME — CHAFED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

EXPANSION JOINT BOLT IS WEARING INTO FRAME, AT STATION 520 RBL 24, AFT SIDE OF FRAME. MAJOR REPAIR ACCOMPLISHED. EXPANSION JOINT REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

FLOORBEAM AT BODY STATION 294.5, REPAIR PLATE ON CAP BETWEEN RBL 28 AND RBL 44, UPPER SURFACE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED SPLICE REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

AFT CABIN FRAME AT STATION 827 NEAR STRINGER 9L IS CRACKED WHERE AIR GRILL CLIP ATTACHES TO FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

AFT CABIN FRAME STATION 987, NEXT TO STRINGER 9L CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR USING CHANNEL AND FILLER.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

CABIN FLOORBEAM STATION 967 RBL 10 HOLE ELONGATED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE. INSTALLED ANGLE REPAIR WITH FILLER.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

AFT CABIN FLOORBEAM STATION 947 RBL 46 WL 208 BLENDED REPAIR OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. MANUFACTURED NEW T-CAP. INSTALLED NEW CAP AND SPLICE ANGLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,137 hrs · 22,271 cycles

AFT CABIN FRAME (STATION 847) NEXT TO STRINGER 9L IS CRACKED WHERE AIR GRILL CLIP ATTACHES TO FRAME. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVAL VERIFIED. DOUBLER INSTALLED.

Part: IRU — FAILED (COCKPIT) · airframe 37,018 hrs · 19,945 cycles

LOSS OF THE CAPTAINS INERTIAL REFERENCE SYSTEM. *S/D* REPLACED NR 1 DIGITAL TO ANALOG ADAPTER AND NR 1 INERTIAL REFERENCE UNIT. OPS CHECKED SYSTEM. DAA, P/N DG1035AB03. IRU, P/N HG1050AD05/AD04.

Part: GCU — FAILED (NR 1 ENGINE) · airframe 36,238 hrs · 19,548 cycles

ONE ENGINE GENERATOR OFF BUS WOULD NOT RESET. *S/D* REPLACED GENERATOR CONTROL UNIT. OPS CHECK GOOD.

Part: OIL TEMP BULB — FAILED (NR 2 ENGINE)

ERRATIC OIL TEMPERATURE INDICATION ON NUMBER TWO ENGINE. REPLACED THE TEMPERATURE BULB AND PERFORMED OPERATIONAL CHECK.

Part: HARDWARE — WORN (RT ELEV TAB)

AIRCRAFT VIBRATING DURING FLIGHT. *S/D* RIGHT HAND ELEVATOR BALANCE TAB INBOARD HINGE HARDWARE WAS WORN. REPLACED SAME.

Part: STRIP — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHTING IN AFT CABIN HAS A 12 FOOT SECTION INOPERATIVE. REPLACED AFT SECTION LIGHT STRIP. CHECKS O.K.

Part: CIRCUIT BREAKER — DEFECTIVE (E/E COMPT)

LOST CAPTAIN'S AND FIRST OFFICER'S INSTRUMENTS. RESTORED POWER TO FIRST OFFICER'S INSTRUMENTS BUT NEVER REGAINED CAPTAIN'S INSTRUMENTS. THE NUMBER ONE ELECTRICAL BUS CIRCUIT BREAKER AND THE NUMBER TWO GENERATOR BREAKER AUXILIARY CONTACTS WERE FOUND DEFECTIVE. BOTH PARTS WERE REPLACED AND WIRING CHECKS ACCOMPLISHED AS A PRECAUTIONARY. TWO VERIFICATION FLIGHTS WERE ACCOMPLISHED.

Part: CHANNEL — CRACKED (HORIZ STAB)

HORIZONTAL STABILIZER CENTER SECTION, LEFT U-CHANNEL OF BOX WEB ASSEMBLY CRACKED. REPLACED LEFT U-CHANNEL OF BOX WEB ASSEMBLY.