N306WA

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,326 hrs · 35,824 cycles

THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 SRM AND PER ER/A 097294-14AD.

Part: COFFEEMAKER — ODOR (2L AFT GALLEY) · airframe 48,279 hrs · 32,957 cycles

FLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR.

Part: ATTACH FITTING — CORRODED (VERT. STAB.) · airframe 47,897 hrs · 32,719 cycles

CORROSION WAS FOUND ON THE AFT FACE OF THE #3 LUG AND THE FORWARD FACE OF THE #6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUGS. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 47,897 hrs · 32,719 cycles

TE WEDGE DISBONDED. REPAIRED PER ER/A 418046-14.

Part: FITTING — CORRODED (48 SECTION) · airframe 47,897 hrs · 32,719 cycles

CORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: SKIN PANEL — CRACKED (KEEL BEAM) · airframe 47,897 hrs · 32,719 cycles

SEVERAL CRACKS WERE FOUND IN THE KEEL BEAM LOWER SKIN PANEL FROM FS 661 TO FS 727. THE SKIN PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 47,897 hrs · 32,719 cycles

RH INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED PER ER/A 418047-14.

Part: SPAR — DAMAGED (WING) · airframe 47,897 hrs · 32,719 cycles

WHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED.

Part: BEAM — WORN (PYLON) · airframe 47,897 hrs · 32,719 cycles

WORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 47,531 hrs · 32,483 cycles

RT WING INBOARD MID FLAP WEDGE IS DISBONDED. REPAIR PER ER/A 417696-14.

Part: WEDGE — DAMAGED (T/E FLAP) · airframe 47,520 hrs · 32,476 cycles

DAMAGE TO LT WING INBOARD MID FLAP WEDGE. REPAIR PER ER/A 417684-14.

Part: FRAME — CRACKED (BULKHEAD) · airframe 43,405 hrs · 29,858 cycles

INSPECTIONS OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A 2 INCH CRACK IN THE RT SIDE CHORD AT WL 207. THE DAMAGED CHORD WAS REMOVED AND A NEW SECTION INSTALLED TO ELIMINATE THE CRACK CONDITION. THE REPAIR WAS ACCOMPLISHED PER ER/A 379675-14AD, REV A.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 43,183 hrs · 29,706 cycles

FLT1799/16 SLC-COS. DURING DESCENT FROM FL370 RT GEN DROPPED OFFLINE, 10 SEC LATER LT GEN DROPPED OFFLINE. UNABLE TO RESET GENERATORS PER POM. DID NOT START APU. CONCLUDED DESCENT AND APPROACH. REPLACED NR 1 GCU PER MM. MCO''D NR 2 GENERATOR PER MEL 24-00-01A. AT KSLC FOUND NR 2 GENERATOR FAILED AND NR 2 CSD OVERSERVICED. REPLACED BOTH CSD AND GEN. ALSO PER ATL MCC ANALYIST REPLACED BOTH EXT PWR CONTACTORS AND BOTH ENG GEN BREAKERS. REPLACED A/C BATT, R41 AND R348 RELAYS, AND P5-4 ELEC CONTROL PANEL. ALSO, BOTH GCU''S WERE REPLACED AGAIN. BOTH GENERATOR SYSTEMS CHECKED NORMALLY.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 41,615 hrs · 28,671 cycles

THE R-1 DOOR SLIDE WAS INADVERTENTLY DEPLOYED. SLIDE INFLATED AND DEPLOYED CORRECTLY.

Part: SOCKET — FAILED (ROW 13)

ELECTRICAL SMELL IN CABIN. FOUND FLUORESCENT OVERHEAD LIGHT TUBE FWD SOCKET AT 13 A, B, C MELTING. REMOVED LIGHT TUBE AND REPLACED SOCKET.

Part: REVERSE LIGHT — ILLUMINATED (NR 2 ENGINE)

NR 2 ENG REV LIGHT CAME ON DURING TAKEOFF. ABORTED TAKE OFF JUST UNDER 100 KTS. LOCKED OUT NR 2 ENG REV PER MEL 78-00-02. MCO - CLEANED CONNECTORS. UNABLE TO DUPLICATE, REMOVED.

Part: SMOKE DETECTOR — FAILED (LAVATORY)

LAV SMOKE FALSE ALARM. ACTIVATED TWICE IN FLIGHT. CIRCUIT BREAKER PULLED TO SILENCE ALARM. REPLACED FWD SMOKE DETECTOR.

Part: SKIN — CRACKED (BS 727)

FUSE SKIN FOUND CRACKED AT BS 727E, S23L. DAMAGE REMOVAL RESULTED IN A 4.75 BY 2 INCH CUT OUT. REPAIRED PER ERA 332622-14.

Part: WEB — CRACKED (BS 727)

CRACK WAS FOUND DURING INSPECTION PER EO 5-70166-3 IN THE WEB AT BS 727, S18A (LHS). THE CRACK EXCEEDED EO/SB LIMITS. REPAIRED PER ERA 332607-14.

Part: SKIN — DAMAGED (C1 DOORWAY)

DURING INSPECTION OF C1 DOOR CUTOUT SKIN AN EXISTING REPAIR WAS REMOVED FOR INSPECTABILITY OF THE AREA. REPAIRED AND REWORKED PER ERA 332586-14.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING ACCOMPLISHMENT OF SI 5-69482-12, SEVERAL CRACKS WERE DISCOVERED ON THE FWD FACE OF THE BS 178 BLKD. REPAIRED PER ERA 332599-14.

Part: WINDOW — CRACKED (CABIN)

SEAT 10A PSGR CABIN WINDOW HAS SEVERAL CIRCULAR CRACKS ON OUTER WINDOW. WINDOW CRACKED AT SEAT 10F DURING PRESSURE CK FOR BROKEN WINDOW AT 10A. CABIN WAS PRESSURIZED TO 4.2 PSI, CABIN RATE OF CLIMB UP AND DOWN NEVER EXCEEDED 1,000 FPM.