N244WA

Part: CONNECTOR — SHORTED (COFFEEMAKER) · airframe 48,838 hrs · 36,216 cycles

AFT GALLEY NR 2 COFFEEMAKER C/B POPPED. LATER TRASH CAN FILLED UP WITH WATER. WATER SUPPLY SHUT OFF. REMOVED BOTH COFFEEMAKERS. FOUND ARCING ON NR 2 COFFEEMAKER CANNON PLUG. TURNED WATER SUPPLY ON. CANNOT FIND SOURCE OF LEAK. REPLACED BOTH COFFEEMAKERS AND PLUG.

Part: ODOR — DETECTED (COCKPIT) · airframe 48,099 hrs · 35,673 cycles

EN ROUTE AT 33,000 FT STRONG ELEC ODOR IN THE VICINITY OF THE COPILOTS CIRCUIT PANEL. NO SMOKE. INSPECTED AREA AND RAN ENGINES/PACKS. UNABLE TO DUPLICATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARKS WERE FOUND IN THE LOWER SKIN OF THE S19L LAP BETWEEN BS 360 AND 540. ISSUED REPAIR VIA ERA 090436-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S4R LAP SPLICE, LOWER SKIN, BETWEEN BS 259.5 AND 360. ISSUED REPAIR 089821-14.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRATCHES WERE FOUND ON THE LOWER FUSELAGE SKIN AT THE STR 14L LAP SPLICE BETWEEN STA 345 AND 360. REPAIRED PER ERA 090265-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARKS ON THE FUSELAGE SKIN AT STRINGER 10R BETWEEN STA 986 T0 1016. AREA REPAIRED IAW ER/A 089689-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARK DAMAGE AT STR 16L FROM STA 540 - 727. REPAIRED IN ACCORDANCE WITH ER/A 090576-14.

Part: DOOR FRAME — UNKNOWN (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

FASTENER INSTALLATION REQUIRED RADIUS BLOCKS AND OVERSIZED FASTENER WHILE PERFORMING EO 03-055852-03AD AT THE FWD SERVICE DOOR CUTOUT AFT FRAME. VA 72553AD ISSUED AND 8110-3 RECEIVED PROVIDING APPROVAL.

Part: SKIN — TORN (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

TEAR IN THE UPPER FUSELAGE SKIN ADJACENT TO THE STR 25 R LAP JOINT. DAMAGE TO BE INCORPORATED INTO LAP SPLICE REPAIR. AREA REPAIRED IN ACCORDANCE WITH ERA 090580-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARKS FOUND AT S16R BETWEEN BS 540 AND 727. DAMAGE REMOVED AND REPAIRED PER ERA 090575-14.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRATCH WAS FOUND ON THE LOWER SKIN AT THE S14 SKIN LAP FROM STA 259-312. REPAIRED PER ERA 089694-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,026 hrs · 35,621 cycles

SCRIBE MARKS WERE NOTED IN THE S10R LAP, LOWER SKIN, BETWEEN BS 540 AND 727. ISSUED REPAIR VIA 089765-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

FUSELAGE SKIN FS 259-360 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW THE LAP SPLICE ALONG S19R BETWEEN FS 259 AND FS 360. REPAIR DOUBLERS INSTALLED ER/A 089739-14, REVISION INITIAL.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

SCRIBE MARK DAMAGE WAS FOUND DUE TO METAL PAINT SCRAPER USE ON THE LOWER SKIN AT THE STRINGER 14L LAP SPLICE, LOCATED BETWEEN FUSELAGE STA 259 AND 312. REPAIRED PER ERA 089672-14.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

STATION 1016 BULKHEAD WEB, STIFFENERS AND CHORDS CORRODED AT BL 0. CHORD SUFFERED DAMAGE AT BL 0 DURING COURSE OF REPAIR. AREA REPAIRED IAW ERA 089856-14AD.

Part: FLAP TRACK — STRIPPED (RT WING) · airframe 48,024 hrs · 35,620 cycles

RIGHT WING O/B FLAP I/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 BOLT HOLES THAT ATTACH MAIN CARRIAGE STOP TO O/B FLAP I/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090835-14, REVISION INITIAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

FUSELAGE SKIN FS 908 - FS 1016 S4R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE AT S4R BETWEEN FS 908 AND FS 1016. REPAIR DOUBLERS INSTALLED ER/A 090115-14, REV A.

Part: FLAP TRACK — STRIPPED (RT WING) · airframe 48,024 hrs · 35,620 cycles

RIGHT WING O/B FLAP O/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 HOLES THAT ATTACH MAIN FLAP CARRIAGE STOP TO O/B FLAP O/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090836-14, REVISION INITIAL.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

SCRATCHES ON THE FUSELAGE SKIN AT STRINGER 19L FROM STATIONS 259 - 360. AREA REPAIRED IN ACCORDANCE WITH ERA 090232-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

DAMAGE ON FUSELAGE SKIN ALONG THE TRAILING EDGE WING-TO-BODY FAIRING. REPAIRED IAW ERA 090712-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

FUSELAGE SKIN FS 360 - FS 440 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE. REPAIR DOUBLERS INSTALLED ER/A 090445-14, REVISION INITIAL.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

SCRATCHES IN THE FUSELAGE SKIN AT STRINGER 10L BETWEEN STATION 345 AND 360. REPAIR IAW ERA 090206-14.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

FUSELAGE SKIN FS 727, S16L - BL 0 FILLET PANEL PERIMETER + FS 770-908, S20L LAP SPLICE REPAIR OF SCRIBE MARKS, TOOLING DAMAGE BELOW THE LAP SPLICE ALONG S20L BETWEEN FS 727 AND FS 908 AND ALONG THE EDGE OF THE FILLET PANEL AFT OF THE WING. REPAIR DOUBLERS WERE INSTALLED ERA 090669-14, REV INITIAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,024 hrs · 35,620 cycles

SKIN AT STATION 178 AND WL 195 SUFFERED DAMAGE AND REQUIRED OVERSIZE FASTENERS THRU THE STATION 178 BULKHEAD CHORD AND AN EDGE TRIM. REPAIRED IAW ERA 089942-14AD.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 48,022 hrs · 35,619 cycles

HORIZONTAL STABILIZERS ATTACH FITTINGS LUGS AND CLEVIS LUGS CORROSION: CORROSION BLENDED AND O/S BUSHINGS INSTALLED ER/A 090581-14AD, REVISION INITIAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10R LAP JOINT BETWEEN BS 908 AND 960. DAMAGE WAS REMOVED AND THE AREA REPAIRED PER ERA 089670-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 360 AND 540. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 090052-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089710-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089715-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089708-14.

Part: SKIN — DAMAGED (S10R, BS360-540) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089757-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089703-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089714-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089712-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089713-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089716-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,022 hrs · 35,619 cycles

THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH SEVERAL AREAS OF SCRIBE MARK DAMAGE IN THE PRESSURIZED FUSELAGE AREA BETWEEN FS 360 & 1016, IN THE UPPER PORTION BETWEEN STRINGERS 14L & 14R. THE DAMAGE LAP JOINTS ARE CUT AND REMOVED AND REPAIRED WITH ALUMINUM DOUBLERS. THE DAMAGED BUTT JOINT STRAPS ARE REMOVED AND NEW SECTIONS INSTALLED. THE REPAIRS ARE DOCUMENTED IN ER/A 089653-14.

Part: REGULATOR VALVE — LEAKING (NR 1 ENGINE) · airframe 44,896 hrs · 33,747 cycles

AIR TURNBACK FROM FLL TO BDL, RETURNED TO FLL. BLEED TRIP OFF NR 1 ENG ON TAKEOFF ROLL. REPLACED PRESSURE REGULATOR BLEED LINES FOR LEAKING.

Part: GASPER FAN — FAILED (CARGO BAY) · airframe 44,391 hrs · 33,537 cycles

ON ARRIVAL PBI CREW OFF FLT 2309 REPORTED UNIDENTIFIABLE ODOR THROUGHOUT THE AIRCRAFT. AIRCRAFT WAS CARRYING HUMAN REMAINS, AND CREW SUSPECTED THIS TO BE THE SOURCE OF THE ODOR. BOTH MTC AND GROUND CREW INSPECTED CARGO COMPARTMENTS AND FOUND CLEAN. GRD CREW REPORTED REMAINS WERE LOADED PER DELTA STANDARDS, AND NO LEAKS WERE NOTED. CREW REFUSED FLIGHT. MTC REPLACED GASPER FAN AND AIRED CABIN. REMOVED FAN BEARINGS WERE FOUND TO BE WORN AND FAN SMELLED OF BURNING INSULATION.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 42,459 hrs · 32,716 cycles

FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,243 hrs · 32,628 cycles

INSPECTION OF THE FS 178 BULKHEAD PER AD 2000-05-29, REVEALED A CRACK IN THE LT SIDE CHORD NEAR WL 207. THE DAMAGED SECTION OF CHORD WAS CUT OUT AND A NEW SECTION SPLICED IN. THE WORK WAS ACCOMPLISHED IN ACCORDANCE WITH BAC S/B 737-53A1173 AND ER/A 382503-14AD.

Part: APU — FAILED (APU BAY) · airframe 41,941 hrs · 32,501 cycles

DURING TAXI OUT, APU DROPPED OFF LINE. TOWER CONFIRMED SMOKE AND FLAME COMING FROM APU AREA. CREW ACCOMPLISHED APU FIRE CHECKLIST. REPLACED APU AND APU FIRE BOTTLE.

Part: HINGE PIN — OUT OF POSITION (L1 DOOR) · airframe 40,978 hrs · 32,095 cycles

PILOT REP - LOUD SQUEAL FROM L1 ENTRY DOOR UPPER HINGE AREA. FOUND UPPER HINGE/SEAL FLOATING BRACKET HINGE PIN OFF . REINSTALLED PIN AND HINGE. PRESS A/C TO 4.5 DIFF PRESS CKS OK

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,922 hrs · 32,070 cycles

FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK AT STRINGER 19L AT FS 767. THE CRACK WAS JUST ABOVE THE WAFFLE DOUBLER AT THE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER THE B737 SRM AND ER/A 381488-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,777 hrs · 31,590 cycles

THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18 RT AT APPROXIMATELY FS 760. THE CRACK LOCATION WAS FWD OF AN EXISTING REPAIR FOR SIMILAR CRACKING. THE NEW CRACK WAS REMOVED WITH A 3 INCHES X 1.5 INCHES CUTOUT AND THE EXISTINGREPAIR REMOVED. THE 2 CUTOUTS OF THE PREVIOUS REPAIR AND ALL FASTENER HOLES WERE HFEC INSPECTED WITH NO CRACKING. THEDAMAGED AREAS WERE REPAIRED WITH AN ALUMINUM DOUBLER PER ERA

Part: CONTROLLER — FAILED (AVIONICS BAY) · airframe 39,269 hrs · 31,381 cycles

DUE TO F/OS WINDSHIELD CRACKED IN FLT. REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK.

Part: WINDOW — CRACKED (COCKPIT) · airframe 39,269 hrs · 31,381 cycles

FIRST OFFICERS FRONT WINDOW CRACKED AT FL 310. REMOVED AND REPLACED F/OS R-1 WINDOW AND WINDOW HEAT CONTROLLER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,405 hrs · 31,010 cycles

A CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE L2 DOOR OPENING. THE CRACK WAS REMOVED WITH A .75 INCH CUTOUT. THE DAMAGED AREA WAS REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 36 AND ER/A 379182-14, REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,405 hrs · 31,010 cycles

THE UPPER HINGE CUTOUT OF THE L2 DOOR OPENING WAS FOUND CRACKED IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT TO REMOVE THE DAMAGE. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 21A AND ER/A 379178-14, REV A.

Part: LANDING GEAR — LACK OF LUBE (MAIN) · airframe 38,209 hrs · 30,924 cycles

DURING AFTER T/O CHECKLIST GEAR HANDLE PLACED TO OFF, HEARD A THUMP AND GOT A LEFT GEAR GREEN AND RED LIGHT. LEFT GEAR DOWN AND DIVERTED TO BOSTON. JACKED A/C, SWUNG GEAR SEVERAL TIMES AND ALL INDICATIONS NORMAL. FOUND NOSE GEAR LOCKING ARM MAKING LOUD BANG. LUBED GEAR, RETRACTED GEAR SEVERAL TIMES AND ALL INDICATIONS NORMAL. A/C OK FOR SERVICE.

Part: DRAG BRACE — CRACKED (NLG) · airframe 38,009 hrs · 30,835 cycles

LOUD POP WHEN RAISING GEAR ON TAKEOFF. AS WE PICKED UP SPEED, LOUD VIBRATION AND ALL ENGINE INDICATIONS WERE NORMAL. FOUND NLG DRAG BRACE BROKEN. REMOVED SAME. FOUND DRAG BRACE BEARINGS BINDING. REMOVED BEARINGS. INSTALLED NEW DRAG BRACE AND BEARINGS.

Part: GASPER FAN — FAILED (CARGO BAY) · airframe 37,374 hrs · 30,550 cycles

STRONG ELECTRICAL BURNING ODOR IN COCKPIT AND CABIN SEEMS TO BE COMING FROM VENT SYSTEM. FOUND C/B POPPED FOR GASPER FAN POPPED. REPLACED FAN, GROUND CHECKS NORMAL. NO FURTHER ELECTRICAL ODOR NOTED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,304 hrs · 30,083 cycles

STRINGER 27R WAS FOUND CORRODED FROM FS 727 + 16 TO FS 727 + 11. ADDITIONALLY, THE FUSELAGE SKIN WAS FOUND CORRODED FROM FS 727 + 15 TO FS 727A. A NEW SECTION OF STRINGER WAS SPLICED IN AND AN EXTERNAL REPAIR WAS INSTALLED ON THE SKIN PER ERA 334261-14. THE DAMAGE WAS FOUND AT MV.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 36,304 hrs · 30,083 cycles

A CRACK WAS FOUND IN THE WEB OF STRINGER R18A SIMILAR TO THOSE NOTED IN S/B 737-53-1170. THE S/B REPAIR WAS INSTALLED PER ERA 334260-14 AT HMV.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 36,304 hrs · 30,083 cycles

THE LONGITUDINAL FLOORBEAM AT BL 0 WAS FOUND TO HAVE CRACKS FROM THE FLOOR PANEL ATTACH HOLES BETWEEN FS 650 AND FS 675. THE DAMAGE WAS REPAIRED PER ERA 334274-14 DURING MV.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,304 hrs · 30,083 cycles

TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN JUST BELOW STR 18R AT FS 727B AND FS 747. THE CRACK AT FS 727B WAS 4 INCHES LONG AND THE ONE AT FS 747 WAS 1.25 LONG. THE DAMAGE WAS FOUND AT MV AND WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ERA 334287-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,304 hrs · 30,083 cycles

CRACKS WERE DISCOVERED IN THE UPPER FORWARD AND AFT CORNERS OF THE R1 DOOR CUTOUT IN THE BEARSTRAP. THE CRACKS WERE CUT OUT AND AN EXTERNAL REPAIR WAS INSTALLED PER ERA 334291-14 AT MV.

Part: DOUBLER — TORN (FUSELAGE) · airframe 36,304 hrs · 30,083 cycles

WHILE REMOVING THE EXHAUST COOLING DUCT, THE SURROUND DOUBLER WAS DAMAGED RESULTING IN TWO CUTOUTS MEASURING 3.5 X 2.5 ERA 334266-14. INSTALLS AND EXTERNAL REPAIR AT HMV.

Part: NBR 2 SLAT — DAMAGED (NBR 2 SLAT)

ON T/O FROM MSY, GOT NR 2 L/E SLAT LIGHT ON. CREW REPORTED SLAT HANGING OUT. OFF LANDED IN JAN. FOUND SLAT MOUNTS BROKEN. REPLACED SLAT ASSY, REPAIRED SHEET METAL DAMAGE TO AIRCRAFT.

Part: LINE — LEAKING (NLG)

AFTER TAKEOFF, THE NOSE GEAR INDICATED UNSAFE. BOTH RED AND GREEN LIGHT WITH THE GEAR HANDLE IN UP POSITION. FURTHER INSPECTION REVEALED THE A SYSTEM HYD RAULIC DECREASING RAPIDLY TO ZERO. THE POM C/W AND LANDING MADE. ALL GEAR AND FLAP INDICATION WERE NORMAL. REPLACED PRESS LINE TO LOCK RETRACT ACTUATOR.

Part: BATTERY PACK — DISCHARGED (CABIN)

L2 DOOR EXTERIOR EMER LIGHT INOP AND 3 AFT LEFT CABIN LIGHTS INOP. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (FUSELAGE)

THE UPPER OUTBD CORNER OF THE COCKPIT L1 WINDOW SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. WHILE STOP DRILLING THE CRACK PER SRM, THE DRILL HOLE WAS MISTAKENLY DRILLED THROUGH THE WINDOW POST. THE DRILL HOLE WAS ROUTED OUT OF THE POST AND POST STRAP. AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE SKIN AND WINDOW POST. THE REPAIR WAS ACCOMPLISHED PER ER/A 364718-14.

Part: BLKHD STIFFENER — CRACKED (BS 178)

DURING ACCOMPLISHMENT OF S.I. 3-69482-12, CRACKS WERE DISCOVERED IN THE BS 178 BULKHEAD WEB AND THE RBL 5.7 VERTICAL STIFFENER. THE VERTICAL STIFFENER AT RBL 5.7 ADJACENT TO WL 15 HAS A 1 INCH CRACK ALONG THE RADIUS. THE CHORD IS MANUFACTURED FROM BAC1505-100361 7075-T6 ALTERED EXTRUSION. THE WEB WAS FOUND CRACKED AT SEVERAL LOCATIONS BETWEEN WL 184.5 AND WL 207 AND LBL 5.7 TO RBL 5.7. THE WEB IS MANUFACTURED FROM 0.040 INCH 2024-T3 CLAD.

Part: ALTIMETER HOSE — LEAKING (LT COCKPIT)

AT FL 240, CAPT AND F/O ALTIMETERS DIFFER BY 150 FT, PLACING CAPT ON ALT STATIC AND F/O NORMAL, F/O READ 150 FT HIGH AND CAPT READ CLOSE TO STANDBY. WITH F/O ON ALT AND CAPT NORMAL, F/O READS 100 FT LOW. FOUND HOSE TO STANDBY IND LEAKING AND REPLACED WITH APPROVED HOSE. LEAK CHECKS NORMAL PER M/M CHAPTER 34.

Part: EEL — INOP (CABIN)

ON PRE-FLIGHT, FOUND EMERGENCY TRACK LIGHTS INOP AT SEAT ROWS 10 TO 15, FOUND SHORTED WIRES IN TRACK. REPAIRED WIRES, OPERATION NORMAL. ALSO, HAD FWD GALLEY AND BOTH AFT GALLEY DOORS EMERGENCY LIGHTS INOP. REPLACED FWD GALLEY LIGHT ASSEMBLY AND LENS. FOUND LEADS SHORTED TO GROUND AT AFT DOOR LIGHTS, REPAIRED WIRES OPERATION NORMAL.

Part: SKIN — CRACKED (LT HORIZ STAB LE)

DURING SHOP INSPECTION, THE LEFT HORIZONTAL STABILIZER LEADING EDGE PANEL WAS FOUND CRACKED. REPAIRED PER SRM 55-10-3.