N516UA

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 75,748 hrs · 28,101 cycles

LT ENG COMPRESSOR STALL ON TAKEOFF CLIMBING THRU 1000 FT. STALL WAS AUDIBLE 4X. ENG RECOVERED & CONTINUED TO OPERATE NORMALLY DURING RETURN TO FIELD. REPLACED ENG IAW 71-00-02 CONFIG 1.

Part: COMPRESSOR — STALLED (ENGINE) · airframe 75,748 hrs · 28,101 cycles

FLIGHT EXPERIENCED COMPRESSOR STALL ON CLIMB.

Part: CAP — MISSING (GROUND POWER) · airframe 75,521 hrs · 28,036 cycles

GROUND POWER INDICATION LIGHT BROKEN. REPLACED MISSING LIGHT CAP. GROUND POWER NOT IN USE, CHECKED GOOD.

Part: DEAD BOLT — FAULTY (COCKPIT DOOR) · airframe 75,460 hrs · 28,018 cycles

FLIGHT DECK DOOR ELEC SWITCH TESTS GOOD, BUT WHEN DOOR CLOSED WITH SWITCH ARMED DOOR CAN BE OPENED. DEAD BOLT WORKS NORMALLY. REPLACED DEAD BOLT ASSEMBLY, OPERATIONS CHECKED GOOD, DOOR LOCKS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 75,373 hrs · 27,993 cycles

LT ENG REVERSER CONTROL ENG SEC CONT EICAS MESSAGES ITEM ROLLED FORWARD. EPCS MESSAGES PDIU EEC & 274-18. ACCOMPLISHED EPCS 71-01-0 0 FOR PDIU EEC & 274-18 FIG 105. OPERATED ENG & REVERSER, OPERATION NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,137 hrs · 27,920 cycles

EMERGENCY EXIT LIGHT JUST FWD OF RT AFT GALLEY DOOR INOPERATIVE. REPLACED CHARGER M108 18 IAW MM 33-51-09, OPERATIONS CHECKED NORMAL.

Part: FIRE LOOP — FAULTY (APU) · airframe 75,019 hrs · 27,885 cycles

STATUS MESSAGE ON CLIMB OUT APU FIRE LOOP 2. REPLACED APU UPPER FIRE DETECTOR ELEMENT IAW AMM26-15-02. UNABLE TO DUPLICATE PROBLEM, TESTED OK.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 74,830 hrs · 27,827 cycles

LT SIDE WINDOW EICAS CAME ON AGAIN. R & R LT WINDOW HEAT CONTROLLER, OPERATIONS CHECKED GOOD.

Part: DUCT — DAMAGED (CABIN) · airframe 74,716 hrs · 27,786 cycles

AIR DUCTS OVER ROWS 8-14 REPORTED TO BE VERY LOUD. REPAIRED DUCT IAW AMM.

Part: SEAT — LOOSE (CABIN) · airframe 74,417 hrs · 27,685 cycles

SEAT 30 ABC LOOSE IN TRACK. SECURED LOOSE SEAT.

Part: SEAT — LOOSE (CABIN) · airframe 74,417 hrs · 27,685 cycles

SEAT 32ABC LOOSE IN TRACK. REPLACED BOTH FWD TRACK FITTINGS.

Part: O-RING — DAMAGED (NR 2 ENGINE) · airframe 74,041 hrs · 27,557 cycles

NR 2 ENG OTBD BYPASS VALVE ON AIR OIL COOLER IS LEAKING. REPLACED O-RINGS ON OTBD BYPASS VALVE ON AIR OIL COOLER IAW IPC 79-21-00A-007A. ACP 5 MIN IDLE LEAKED CHECKED GOOD.

Part: SOCKET — DIRTY (COCKPIT) · airframe 73,934 hrs · 27,517 cycles

BATTERY DISCHARGE LIGHT INOPERATIVE ON STANDBY POWER PANEL. CLEANED SOCKET, LIGHT OPERATIONS CHECK GOOD.

Part: SKIN — CRACKED (L4 DOOR) · airframe 73,588 hrs · 27,400 cycles

L4 DOOR INNER SKIN CRACKED AT WEB LIGHTNING HOLE, TWO AREAS. REPAIRED INNER SKIN IAW UAL ECRA 5200-01251 & REO-M0716.

Part: WINDOW — SCRATCHED (COCKPIT) · airframe 73,588 hrs · 27,400 cycles

RIGHT NR 2 FLIGHT COMPARTMENT WINDOW HAS SCRATCHES IN THE INNER PANE. R & R ADJUSTED AND OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 760-780) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 760-780 RBL 60, REPAIRED IAW NR 2046.

Part: SHEAR TIE — CORRODED (BS 1701 S27-28R) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

CORROSION ON BILGE SHEAR TIE BS 1701, S27-28R. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORROSION ON BILGE SHEAR TIE IAW SRM 51-10-02, PAR4, FIG 1. MAJOR REPAIR

Part: KEELBEAM — CRACKED (BS 1180) · airframe 73,588 hrs · 27,400 cycles

KEEL BEAM BS 1180, WL 133.00, RBL 11 ANGLE CRACKED. R & R ANGLE IAW SRN 51-40-02, PAR 7, FIG 12. MAJOR REPAIR.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

R1 DOOR LOWER GATE EDGE AND SKIN HAS CORROSION. REMOVED CORROSION FROM GATE AND FOUND OUT OF LIMITS IAW SRM 52-10-02. R & R LOWER GATE IAW SRM 51-40-02, PARA 4B, FIG 3. MAJOR REPAIR.

Part: KEELBEAM — CRACKED (BS 1180) · airframe 73,588 hrs · 27,400 cycles

KEELBEAM BS 1180, WL 133.00 LBL 11 REPAIR ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: R & R ANGLE IAW SRM 51-40-02, PARA 7, FIG 12.

Part: FITTING — CORRODED (RT OVRWING SLIDE) · airframe 73,588 hrs · 27,400 cycles

RT OVERWING SLIDE ABSORBER ASSY HAS CORROSION ON THE END FITTING. R & R RT WING SLIDE SNUBBER AND FITTING.

Part: SKIN — CRACKED (BS 513 S28R) · airframe 73,588 hrs · 27,400 cycles

FUSELAGE SKIN CRACKED BS 513 JUST ABOVE STRINGER 28R. REPAIRED SKIN IAW SRM 53-00-01, FIG 201, REPAIR 2.

Part: SKIN — PUNCTURED (LT ELEVATOR LE) · airframe 73,588 hrs · 27,400 cycles

PUNCTURE ONE LEFT ELEVATOR LOWER L/E, ES 160. REPAIRED LEFT ELEVATOR LWR L/E IAW SRM 51-70-04, REPAIR FIG 10.

Part: CUSP WEB — CORRODED (BS 1060-1080) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN BS 1060 TO 1080, S17R CUSP WEB CORRODED. FOUND TO BEYOND ALLOWABLE LIMITS IAW SRM 53-40-13. FIG 101. R & R CUSP WEB IN MAIN CABIN BS1060 TO BS1080, STR 17R IAW SRM 51-40-02, PAR 7D. MAJOR REPAIR.

Part: CUSP WEB — CRACKED (BS 996-1020) · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN BS 996 TO 1020, CUSP WEB CRACKED AT FWD END AT S17L. R & R CUSP WEB IAW SRM 51-40-02, PA R 4, FIG 8 AND PAR 7D, ITEM 6, FIG 12. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (BS 540-560) · airframe 73,588 hrs · 27,400 cycles

BS 540 TO 560, BL 0, WL 208.6, INTERCOSTAL IS CRACKED. R & R INTERCOSTAL IAW SRM 53-00-51, FIG 201, PARA 7.

Part: SEAT TRACK — DAMAGED (BS 1094) · airframe 73,588 hrs · 27,400 cycles

SEAT TRACK HAS HOLE DRILLED THROUGH IT, BS 1094, LBL 45. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 51-4 0-02, PAR 7D, FIG 12 AND PAR 9, 51-40-05, FIG2.

Part: INTERCOSTAL — CRACKED (BS 1520-1540) · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN INTERCOSTAL BS 1520 - 1540, BL 0 CRACKED SEVERAL PLACES AT UPPER ANGLE. REPAIRED INTERCOSTAL. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (BS 780-800) · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE HAS CRACKS AROUND FASTNER HOLES BS 780 TO 800, BL 0. R & R FLOOR SUPPORT IAW DWG 140N3505 AND SRM 51-40-02, PAR 7C AND 53-00-51, FIG 201. MAJOR REPAIR.

Part: CUSP WEB — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN BS 1020 TO 1040, S17L CUSP WEB HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, FIG 101. R & R CUSP WEB IAW SRM 51-40-02, PAR 7D.

Part: ATTACH FITTING — CRACKED (BS 350 S6L) · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN LT FWD ENTRY DOOR UPPER FRAME TO STRINGER ATTACH FITTING IS CRACKED AT BS 350, S6L, WL 281. R & R L1 DOOR UPPER FRAME TO STRINGER ATTACH FITTING IAW SRM 51-40-02 PAR 7, FIG 12. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681 LBL 52) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN BS 1681, LBL 52 FLOORBEAM ANGLE HAS CORROSION BS 1681, LBL 52. REPAIR IN COMPLIANCE WITH NON ROUTINE NR 20419. R & R ANGLE IAW SRM 51-40-02, PAR 7, FIG 12. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02, PARA 7, FIG 12.

Part: ATTACH BRACKET — CORRODED (BS 1140 S17R) · corrosion level 2 · airframe 73,588 hrs · 27,400 cycles

MAIN CABIN, BS 1140, S17R CUSP WEB ATTACH BRACKET HAS CORROSION BS 1140 STR 17R. SUP: REPAIR IN COMPLIANCE WITH NON ROUTINE, NR 20452, REMOVED CORROSION ON MAIN CABIN CUSP WEB ATTACH BRACKET AT BS 1140 STR 17R ORIGINAL MAT THICKNESS OF .063IN MAT REMOVED IS 008IN MAT REMAINING IS .055IN IAW SRM 51-10-02, PARA 15, FIG 1 AND 5 FOUND TO BE OUT OF LIMITS IAW SRM 51-40-13, FIG 101, DETAIL III, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW CUSP WEB ATTACH BRACKET IAW DWG NR 144N 5211 AND SRM 51-40-05, FIG 2 AND 4 51-40-02, PARA 7D, FIG 12.

Part: FLOORBEAM — DAMAGED (BS 1600) · airframe 73,588 hrs · 27,400 cycles

SCRIBE MARK DAMAGE ON CABIN FLOORBEAM AT BS 1600 RBL 27-43. REPAIRED DAMAGE ON CABIN FLOORBEAM .

Part: CAP — MISSING (CABIN) · airframe 73,483 hrs · 27,366 cycles

1B EMERGENCY FLOOR LIGHT CAP IS MISSING, AS REPORTED BY CREW. REPLACED ABOVE LIGHT CAP.

Part: LIGHT — MISSING (CABIN) · airframe 73,098 hrs · 27,256 cycles

FWD COAT CLOSET EMERGENCY LIGHT MISSING. INSTALLED EMERGENCY LIGHT PER DWG 15F6889-504 AND WD33-51-21 AND AMM 25-27-01 AND OPS GOOD.

Part: WIRE — BROKEN (COCKPIT) · airframe 73,007 hrs · 27,230 cycles

RIGHT LANDING GEAR GREEN LIGHT HALF BURNED OUT. FOUND L399 RT HALF INOP. REPLACED LANDING CARD AT P51 PANEL MR31510-9 OFF AND 123 ON. FOUND BROKEN WIRE AT L399. WHILE REMOVING P3-1 PANEL TO REPAIR WIRE LOST RIGHT HALF OF LEFT, NOSE, GEAR AND DOORS. NEEDS CAT3 FOUND TWO BROKEN WIRES ON LIGHT MODULE L399 REF WDM32-61-21, PIN 1 AND PIN 3 AND ACCOMPLISH ED CAT III TEST 30, OPS NORMAL.

Part: ADAPTER — MISSING (COCKPIT) · airframe 72,893 hrs · 27,191 cycles

NR 1 BOOM MIC IS DEFECTIVE. (01=CAPT, 02=1ST OFF, 03=1ST OBS). CREW COMMENTS: MISSING THREADED ADAPTOR FOR EARPIECE. PLACED IT IN SPARE MINITEL BAG. USING SPARE REPLACED WITH NEW MINITEL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 72,668 hrs · 27,120 cycles

INTERIOR EMERGENCY LIGHT INOPERATIVE AT SEAT 5FE. SECURED CONNECTOR TO EMERGENCY LIGHT AT SEAT 5FE, OPS NORMAL.

Part: ENGINE — FAULTY (NR 1) · airframe 72,559 hrs · 27,087 cycles

DIRTY SOCK ODOR IN COCKPIT AFTER DEPT PASSING THROUGH 7000 FT. LASTED ABOUT 5 MINUTES. REPLACED NR 1 ENGINE PER AM M 71-00-02. COMPLETED INSPECTION OF NR 3 BEARING & PNEUMATIC DUCTS, AND SPINNER. NO OIL FOUND. DRAINED GEARBOX, ONLY TWO QTS FROM GEARBOX. PERFORMED ENGINE WASH. ENGINE FAIL ON PACK BURNOUT. VERY HEAVY OIL ODOR. INCREASE WITH POWER. REPLACED LEFT AND RIGHT RECIRCULATION FILTERS. NR 1 ENGINE STARTER FAILED DURING ENGINE WASH. REPLACED STARTER ON NR 1 ENGINE.

Part: COMPUTER — FAULTED (ELEVATOR FEEL) · airframe 72,384 hrs · 27,029 cycles

ELEVATOR FEEL STATUS MESSAGE ILLUMINATED. DUE TO CHRONIC PREVIOUS HISTORY OF ELEVATOR FEEL STATUS MESSAGES. REPLACED ELEVATOR FEEL COMPUTER, IAW FIM 27-31-00 PG 117 AND SERVICE TIP 27-31-00 PG 100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,295 hrs · 26,996 cycles

MAJOR REPAIR LT FUSELAGE SKIN BS 660 - 740 WL 145.0 HAS SCRIBE MARKS AT LAP JOINT. ECRA 5330-04413 HAS BEEN APPROVED AS AMOC TO AD2007-19-07 & REQUIREMENTS OF SB757-53A0092, LR TS, HAVE BEEN TERMINATED AT THIS LOCATION. DURING THE ACCOMPLISHMENT OF EQ7735 WHICH IS SCHEDULED PRIOR TO 28,435 PTC THE REQUIREMENTS IAW AMM 53-31-93 ARE NOT TO BE ACCOMPLISHED FROM BS 600 - 740. REPAIRED LT FUSELAGE SKIN STATION 660-760 AT LAP SEAM. ACCOMPLISHED EQ7735 WHICH IS SCHEDULED PRIOR TO 28,435 PTC 21JAN IND INF. AFTER AMM 53-31-93 IS REVISED VIA A SEPARATE ECRA, WHICH DELETES THE LOCATION OF THE TWO AREA BETWEEN BS 660 - 740. THIS ITEM WILL BE CLOSED 07 NOV SFO INF. AMM 53-31-93 HAS BEEN UPDATED WITH THIS INSPECTION REQUIREMENTS. THIS CF CAN BE DELETED.

Part: FLOOR SUPPORT — DAMAGED (BS 1410-1414) · airframe 72,295 hrs · 26,996 cycles

AFT CARGO BS 1410-1414 LBL 3 FLOOR SUPPORT HAS FOUR HOLES IN UPPER FLANGE. REMOVED AND REPLACED FLOOR SUPPORT. MAJOR REPAIR

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,295 hrs · 26,996 cycles

MAJOR REPAIR LT FUSELAGE SKIN BS 657 - 661 AT STRINGER 26L HAS SCRIBE MARK DAMAGE & MUST BE INSP IAW REQUIREMENTS OF AMM53-31-93 PRIOR TO THRESHOLD OF 28,996 PTC & EVERY 2000 CYCLES THEREAFTER. ACCOMPLISH INSP IAW PART II OF ECRA 5330-04413. REPAIRED LT FUSELAGE SKIN STATION 660 - 760 AT LAP IAW ECRA 5330-04413. INSP REQUIREMENTS PERFORM INSP BS 400 - 661 SKIN LAP AT STRINGER 26LT IAW AMM 53-31-93 & DETAILED VISUAL INSP. ADDITIONAL INSP REQUIREMENTS UT PHASED ARRAY INSP IAW NDT MANUAL PART4 53 -00-02 & HFEC INSP NDT MANUAL PART6 51-00-01 OR 51-00-19. CONTACT ENGINEERING PRIOR TO 28,996 PTC FOR INSP REQUIREMENTS 07 NOV SFO INF. AMM 53-31-93 HAS BEEN UPDATED WITH INSP REQUIREMENTS. THIS CF CAN BE DELETED.

Part: SKIN — DAMAGED (BS 660-740) · airframe 72,295 hrs · 26,996 cycles

LT FUSELAGE SKIN BS 660-740 WL 145.0 HAS SCRIBE DAMAGE AT LAP JOINT. REPAIRED SKIN IAW ECRA5330-04413. MAJOR REPAIR.

Part: WIRE — DISCONNECTED (CARGO LOADER) · airframe 72,295 hrs · 26,996 cycles

WIRE BS 680 WL155 IS PULLED OUT OF TERMINAL LUG. REPLACED TERMINAL LUG. OPS CHECKED GOOD ON FWD CARGO LOADER SYSTEM.

Part: SKIN — DAMAGED (BS 1384-1401) · airframe 72,295 hrs · 26,996 cycles

FUSELAGE SKIN BS 1384-1401 S38 LT-27 RT DAMAGED REPAIRED SKIN BELOW IAW ECRA 5360-01245.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,295 hrs · 26,996 cycles

DENT IN SKIN LOCATED 18 INCHES BELOW AFT CARGO DOOR. REPAIRED SKIN IAW ECRA5360-01245.

Part: SKIN — DAMAGED (BS 660-760) · airframe 72,295 hrs · 26,996 cycles

FUSELAGE SKIN BS 660-760 WL 145 HAS SCRIBE MARKS AT LAP JOINT. REPAIR SKIN BETWEEN S25-28L.

Part: SKIN — DAMAGED (BS 657-661 S26L) · airframe 72,295 hrs · 26,996 cycles

FUSELAGE SKIN BS 657-661 S26L HAS SCRIBE DAMAGE. REPAIRED SKIN IAW ECRA5330-04413.

Part: SKIN — DENTED (BS 650 S25-26L) · airframe 72,295 hrs · 26,996 cycles

DENT BS 650 BETWEEN S25-26L, FOUND OUT OF LIMITS. REPAIRED IAW SRM 53 -00-01. MAJOR REPAIR

Part: SKIN — DAMAGED (BS 625-650 S4-7L) · airframe 72,295 hrs · 26,996 cycles

CREASES IN FUSELAGE SKIN BS 625-650 S4-7L ABOVE & FWD OF L2 DOOR. REMOVED DAMAGED SKIN BS 630-640 S5-7L AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED (BS 570-632) · airframe 72,295 hrs · 26,996 cycles

SKIN BS 570-632 S14-19L DAMAGED. SKIN REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,295 hrs · 26,996 cycles

2 CREASES IN FUSELAGE SKIN ABOVE AND FORWARD OF DOOR 2L. APPROX DIMENSIONS (11" X .5" X .015" DEEP) AND (8" X .5"X .015 DEEP). DAMAGE IS WITHIN LIMITS PER SRM 53-00-01. CREASE IS SMOOTH AND .75" FROM ANY STRINGER. CREASES ON FUSELAGE REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,295 hrs · 26,996 cycles

CREASES IN FUSELAGE SKIN ABOVE & FWD OF L2 DOOR. REMOVED DAMAGED SKIN BS 630-640 S5-7L AND INSTALLED REPAIR DOUBLER PER ECRA 5330-04411. MAJOR REPAIR.

Part: DUCT — DAMAGED (APU AIR INLET) · airframe 72,295 hrs · 26,996 cycles

APU AIR INLET ELBOW DUCT FWD FLANGE DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED APU AIR INLET DUCT IAW ESR11 & SRM 51-70-17 & ECRA 4910-01134.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 72,295 hrs · 26,996 cycles

BS 700 FLOORBEAM TEE IS CRACKED AT SEAT TRACK LBL 45.5. REPAIRED FLOORBEAM IAW ECRA 5310-05536 & 5330 -04410. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1620 S14R) · airframe 72,295 hrs · 26,996 cycles

UPPER FUSELAGE SKIN DENTED BS 1620 S14R. BLENDED DENT IAW SRM 53-00-01 DETAIL III. MAJOR REPAIR

Part: STRUCTURE — CORRODED (BS 1787) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

INTERNAL TAIL AREA ABOVE CENTER HORIZONTAL STAB, BS 1787 BETWEEN S4-5R APU INLET FWD EDGE METAL ATTACH FLANGE HAS CORROSION AT A NUT PLATE. REMOVED CORROSION ON APU INLET ATTACH FLANGE FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15. REPAIRED APU INLET. MAJOR REPAIR

Part: WEB — CRACKED (R4 DOOR) · airframe 72,295 hrs · 26,996 cycles

R4 DOOR INNER WEB CRACKED, DAMAGE AREA IN CUTOUT FWD UPPER CORNER OF DOOR. REMOVED DAMAGE AND REPAIRED. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 600 LBL 45.5) · airframe 72,295 hrs · 26,996 cycles

BS 660 FLOORBEAM TEE IS CRACKED AT SEAT TRACK LBL 45.5. REPAIRED FLOORBEAM TEE IAW ECRA5330-04407. MAJOR REPAIR

Part: ANGLE — CORRODED (BS 1440-1530) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

AFT CARGO BAY ZEE ANGLE AT DOOR CUTOUT BS 1440-1530 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ZEE ANGLE IAW DWG 146N5391, SRM 51-40-05, 51-20-01, & 51- 21-00. MAJOR REPAIR

Part: WEB — DAMAGED (BS 1400-1420) · airframe 72,295 hrs · 26,996 cycles

ELONGATED HOLE ON WEB THAT ATTACHES SUPPORT BS 1400-1420, LBL 3. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB PER DWG 146N5425-19 AND SRM 51-40-02.

Part: WIRE — BROKEN (APU SHUNT) · airframe 72,295 hrs · 26,996 cycles

APU BATTERY SHUNT HAS TWO BROKEN WIRES AT TERMINAL LUGS. TERMINATED WIRES W1024-2004R-22 AND W1024-20048-22 WITH RING TERMINALS AT THE APU BATTERY SHUNT IAW SWPM 20-30-11 AND WDM 24-34-11. OPS CHECKED GOOD IAW AMM24-31-04.

Part: TUBE — CHAFED (BS 1578, LBL 51) · airframe 72,295 hrs · 26,996 cycles

AFT CARGO BAY BS 1578, LBL 51, AT CEILING PANEL LEVEL, SMOKE DETECTOR TUBING IS CHAFING FIRE EXTINGUISHING TUBING. INSTALLED NEW TUBING BS 1578, LBL 51 IAW AMM 20-11-00 AND AMM 26-33-99.

Part: WIRE HARNESS — DAMAGED (RT MLG) · airframe 72,295 hrs · 26,996 cycles

RIGHT MLG DOWNLOCK SENSORS SYSTEM ONE HAVE TWO WIRE HARNESSES THAT ARE FOLDED SHARP PINCH ABOVE CONNECTORS, WITH LESS THAN THE MINIMUM RADIUS. INSTALLED NEW WIRE HARNESS IAWAMM 32-67-02 AND SWP 20-10-12. OPS CHECKED RIGHT MLG DOWNLOCK AMM 32-61-02, CHECKED NORMAL.

Part: TUBE — CHAFED (BS 1380, LBL 51) · airframe 72,295 hrs · 26,996 cycles

AFT CARGO BAY BS 1380, LBL 51, 2 FT BELOW CEILING PANEL LEVEL, SMOKE DETECTOR TUBING HAS CHAFE DAMAGE. INSTALLED NEW TUBE IAW AMM 20-11-00 AND AMM 26-23-99. OPS CHECKS GOOD REF AMM 26-16-00 PG 510.

Part: BONDING WIRE — CORRODED (GALLEY) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

GALLEY TABLE TOP BONDING WIRE TERMINAL, TWO ENDS CORRODED. REPLACED WIRE W9002-008AY-08 REF SWPM 20-30-11. OHMS TESTED GOOD.

Part: SHEAR TIE — CORRODED (BS 1380, RBL 26) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

AFT CARGO BS 1380, RBL 26 TIE DOWN ASSY CORRODED. FOUND SHEAR TIE CORRODED AT THIS LOCATION. FABRICATED AND INSTALLED NEW SHEAR TIE BS 1380, RBL 26, IAW DWG 146N5421, AND SRM 51-40-02. INSTALLED NEW TIE-DOWN IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

PASS CABIN FWD GALLEY FLOOR STRUCTURE, PANEL SEPARATION CHANNEL AT STA 367 RBL 57 TO RBL 64 IS CORRODED ON EACH FLANGE UPPER SURFACE AS MARKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SRM 51-10-0 2 ORIGINAL THICKNESS .053 LOSS OF .006 OUT OF LIMITS SRM 53-00-51. REMOVED FLOOR PANEL SEPARATION, FABRICATED NEW STRUCTURE PER SRM DWG 1 41N5107 & GNMM 1-0-0-023.

Part: SKIN — DENTED (LE SLAT) · airframe 72,295 hrs · 26,996 cycles

LEFT WING NR 3 SLAT EXTERNAL UPPER SURFACE HAS NUMEROUS DENTS. EVALUATED DAMAGE AND VERIFIED REPAIR MATERIALS, PREPPED AREA & FABRICATED REPAIR PARTS BONDED REPAIRS AND SEALED. PRIMED & RESTORED.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

AFT CARGO COMPARTMENT BS 1360 RBL18 RAIL FITTING IS CORRODED. REMOVED AND REPLACED AFT CARGO COMP BE 1360 RBL18 RAIL SUPPORT FITTING IAW BOEING DWG146N 1009 & SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

PASS CABIN R1 DOORWAY FLOOR SUPPORT INTERCOSTAL FROM STA 345 TO 365, RBL 62 UPPER SURFACE IS CORRODED AROUND 5 EA NUT PLATE HOLES UPPER SURFACE. REPLACED INTERCOSTAL AT STA 345 TO 365 RBL 62 IAW BOEING DIAGRAM 141N5160 AND SRM 51-40- 02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

PASSENGER CABIN FLOOR FWD GALLEY INTERCOSTAL FROM STA 332 TO 345 RBL2 HAS CORROSION ON UPPER SURFACE IN 4 AREAS. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED INTERCOSTAL P/N 141N5161U39 AT STA 324 TO 345 RBL, IAW SRM 51-40-02 & BOEING DWG 141N5160.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 61,892 hrs · 23,139 cycles

DENT 1.25 X .1875 BETWEEN STATION 1806 AND 1825 BETWEEN S-25R. EVALUATED DENT AND FOUND TO BE WITHIN LIMITS OF SRM. DENT HAS BEEN HFEC INSPECTED WITH NO CRACKS FOUND. REMOVED DAMAGE ON STA 1806 & 1825 BETWEEN STR 25R CUTOUT SIDE 2.50 X 1.25 AND INSTALLED DOUBLER REPAIR PER SRM 53-00-01 REP3 DETAIL I

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

PASSENGER CABIN FWD GALLEY FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 310 & 324 RBL 42 AFT END UPPER SURFACE IS CORRODED. BLENDED CORROSION IAW SRM 53-00-51 ORG THICKNESS .120 REMAINS .078 LOSS OF .042. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL & SHIM PER BOEING DWG141 N5160 & SRM 53-00-51.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 71,864 hrs · 26,839 cycles

LEADING EDGE ASSYMETRY ISSUE, RTFL. ROTARY ACTUATOR REPLACED. REMOVED LWR WING PANEL 511EB FOR FOM. ALSO REMOVED 2 ANTI-ICE DUCTS ADJACENT TO NR 5 L/E SLAT. ALSO DISCONNECTED AUX TRACK YOKE SUPPORT ON NR 5 L/E SLAT WHERE YOKE ATTACHES TO AUX TRACK. REMOVED AND INSTALLED ROTARY ACTUATOR PER 27-81-18 TO STEP 3F4M. ACCOMPLISHED INSPECTION OF INSTALLATION PER 27-81-18 THROUGH STEP 3F4M. COMPLETED INSTALLATION OF ROTARY ACTUATOR PER AMM, OPS TEST GOOD.

Part: MONITOR — FAULTY (VIBRATION SYS) · airframe 71,721 hrs · 26,778 cycles

RIGHT ENGINE VIBRATION INDICATION READS HIGH, LOW, ZERO, BLANK, FLUCTUATES OR INOP. NO ABNORMAL VIBRATION PERCEIVED. OTHER ENGINE PARAMETERS NORMAL. REPLACED VIBRATION MONITOR. REPLACED NR 2 ENGINE.

Part: BLADE — CHIPPED (RT ENGINE) · airframe 70,855 hrs · 26,492 cycles

CHIP ON RIGHT ENGINE FAN BLADE MAINT TEXT: NICK MEASURES .375 OF AN INCH FROM THE BLADE TIP ON THE LEADING EDGE AND IS .046 IN DEEP. DAMAGE IS WITHIN AREA 1 PER MM 72-31-02 PAGE 622 REF FIGURE 608 & 609. NO VISIBLE TEARS OR CRACKS. MAY CONTINUE IN SERVICE FOR 25 HOURS MAXIMUM AND THE BLADE REPAIR AND EDDY CURRENT MUST BE ACCOMPLISHED PER MM 72-31- 02-801. BLADE IS MARKED. PTT 70847 REPAIR IAW AMM 72-31-02. ACCOMPLISHED FINAL CHECK OF THE BLADE BLEND REPAIR REF AMM 72-31-02.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 70,647 hrs · 26,425 cycles

LEFT TRAILING EDGE INBOARD FLAP WAS REMOVED FOR ELONGATED HOLE UNDER INBOARD BRACKET ON AFT FAIRING FOR OUTBOARD TRACK. REPAIRED IAW AVO1291.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 70,556 hrs · 26,390 cycles

RUNNING FUEL LEAK FROM LT WING DRY BAY NOTED ON WALKAROUND. REPLACED LT ENGINE FUEL FEED LINE, RAN ENGINE NO LEAKS NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 70,522 hrs · 26,373 cycles

BLUE PASS CALL LIGHTS ON IN COACH CABIN WITH NO SEAT CALL BUTTON ILLUMINATED. CHIME OK. CYCLED CABIN POWER. LIGHT EXTINGUISHED AND OPS CHECK GOOD AT ALL SEATS.

Part: PUMP — FAILED (RT CENTER TANK) · airframe 70,308 hrs · 26,294 cycles

DURING INSULATION RESISTANCE CHECK FOUND RT CENTER TANK OVERRIDE PUMP FAILED TEST 500VDC. NEEDS NEW PUMP. REPLACED RT CENTER TANK FUEL OVERRIDE PUMP ASSEMBLY. PASSED RESISTANCE CHECK. ACCOMPLISHED NON RII INSP OF RT CENTER FUEL OVERRIDE PUMP PER MM. NO DEFECTS NOTED.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 69,741 hrs · 26,078 cycles

PASSENGER ENTRY-SERVICE DOORS L FWD DOOR BUSTLE NOT SECURE. REINSTALLED SAME SLIDE TO 1L MED IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,295 hrs · 26,996 cycles

PASS CABIN FWD GALLEY FLOOR STRUCTURE T CAP REPAIR AT STA 365 BETWEEN BL 0 TO RBL 64 HAS CORROSION ALL ALONG THE UPPER SURFACE AROUND MOST NUT CLIP HOLES ON FWD SIDE. REMOVED DAMAGE ORIGINAL THICKNESS.130 THE LOSS OF .036 REMAINING .094 OUT OF LIMITS PER SRM 53- 00-51, REMOVED T-CAP SRM 51-40-02 AND INSTALLED NEW T-CAP PER ECRA 5310-05536.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,241 hrs · 25,899 cycles

STA 1662 FLOOR SUPPORT ABOVE WATER TANK IS CORRODED BETWEEN FLOORBEAMS. REMOVED AFT GALLEY FLOOR MAT FOR ACCESS, BAGGED AND STOWED IN LOB.

Part: PCA — FAULTY (ELEVATOR) · airframe 69,038 hrs · 25,820 cycles

HIGH SPEED ABORTED TAKEOFF AT 95 KNOTS DUE TO LACK OF RUDDER CONTROL. R ELEV STATUS MSG. MEL COMPLIED WITH. REPLACED LEFT HYD SYS CENTER PCA ON RT ELEVATOR. NR 5 SPOILER FLOATS 10 INCHES WITH LEFT HYD SYSTEM OFF. REPLACED NR 5 SPOILER PCA, OPS CHECKS GOOD. NO LEAKS NOTED.

Part: BATTERY — FAULTY (APU) · airframe 68,469 hrs · 25,597 cycles

STATUS MSG APU OIL QTY LIGHT CAME ON 2.8 HRS INTO FLT. APU RAN FOR GEN MEL ITEM. MAINT TEXT: NO APU LEAKS UPON ARRIVAL. SERVICED 1.5 QTS OIL IN APU. RAN APU AND FOUND NO LEAKS. TAIL PIPE DRY. HUNG START AT 40 PERCENT WITH AUTO SHUT DOWN TWICE. REPLACED APU BATTERY.

Part: UNKNOWN — MALFUNCTIONED (DOOR WARNING) · airframe 68,126 hrs · 25,480 cycles

CREW REPORTS IN THE CLIMB-OUT AT 13000 FT, GOT THE 'EMERG DOORS' LIGHT AND EICAS MSG RT AFT EMERGENCY DOOR. PRESSURIZATION WAS NORMAL. CREW DESCENDED BACK TO 10,000 FT WHERE FLIGHT ATTENDANT CONFIRMED NO SLIDE DEPLOYMENT AND THEN LIGHT EXTINGUISHED AND MSG CLEARED. STARTED THE CLIMB AGAIN AND ALL OPS REMAINED NORMAL. REMOVED RIGHT AFT HATCH AND INSPECTED PROX SWITCH. FOUND CLEAN AND SECURE. REF MM FOR INSPECTION AND FOR ARM AND DISARM. TEST OKAY.

Part: PACKING — FAULTY (APU ENGINE) · airframe 67,854 hrs · 25,379 cycles

AT THE GATE WITH APU RUNNING THE PACKS CABIN BEGAN TO FILL WITH SMOKE. PACKS WERE TURNED OFF. REPLACED TURBINE BEARING CHIP DETECTOR PACKING. SERVICED OIL TO FULL. RAN APU SEVERAL HOURS, NO LOSS OF OIL. RAN ENGS, CLEARED PACKS OF OIL RESIDUE.

Part: SLIDE — DEPLOYED (CABIN) · airframe 67,709 hrs · 25,320 cycles

RT OVERWING SLIDE DEPLOYED. RIGHT OFF WING ESCAPE SYS DEACTIVATED. REMOVED DEPLOYED SLIDE FROM ACFT. REPLACED RT OVERWING SLIDE ASSY AND INFLATION BOTTLE. SQUIB TEST GOOD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 67,391 hrs · 25,209 cycles

EMERGENCY EXIT LIGHT AT ROW 16 ABC INOPERATIVE, REPLACED BATTERY. RESET SYS. ACCOMPLISHED OPERATION TEST AND ALL LIGHTS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,041 hrs · 25,090 cycles

LT OVERWING EXTERNAL SLIDE EMERGENCY LIGHT INOP. RELAMPED LT OVERWING EXTERNAL SLIDE EMERGENCY LIGHT AND OPS CHECK GOOD IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,041 hrs · 25,090 cycles

LT OVERWING EXTERNAL SLIDE EMERGENCY LIGHT INOP. REPLACED LT AFT OVERWING EXIT IDENTIFIER SIGN AND OPS CHECK GOOD IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,041 hrs · 25,090 cycles

L4 EXTERNAL DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT L-4 DOOR EXTERNAL AND OPS CHECK GOOD IAW MM.

Part: TACHOMETER — FAULTY (RAT) · airframe 67,041 hrs · 25,090 cycles

RAT TACHOMETER GREEN LIGHT DOES NOT ILLUMINATE WITH RAT BEING BACK DRIVEN. REPLACED RAT TACH IAW MM, OPS CHECKED GOOD.

Part: PLATE — CRACKED (CARGO THRESHOLD) · airframe 67,041 hrs · 25,090 cycles

FWD CARGO DOOR OPENING SILL PLATE HAS A CRACK. DOOR THRESHOLD PLATE HAD A 1.5" LONG CRACK. STOP DRILLED CRACK AND APPLIED TAPE IAW MM. CHECK CRACK FOR PROGRESSION EVERY 3SV AND REPAIR AT NEXT CHECK. WELDED CRACK IAW MM ON NON ROUTINE 36309.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 67,041 hrs · 25,090 cycles

R-1 DOOR SLIDE INDICATOR LIGHT IS INTERMITTENT WHEN ARM-DISARM LEVER IS MOVED TO ARM POSITION. REPOSITIONED FLOOR FITTINGS ON R-1 DOOR IAW MM. FOUND GIRT BAR PROXIMITY SWITCHES TO BE WITHIN LIMITS IAW MM.

Part: SEAT TRACK — CORRODED (BS 300-310) · airframe 67,041 hrs · 25,090 cycles

MAIN CABIN SEAT TRACK CORRODED BS300-BS310 LBL 11 MAJOR REPAIR ACCOMPLISHED: R & R SEAT TRACK AND FLOOR SUPPORT IAW SRM AND DWG 141T5250. SEAT TRACK PN 141T5121-219 FABRICATED ON N-R 31401.

Part: SEAT TRACK — CORRODED (BS 300-310) · airframe 67,041 hrs · 25,090 cycles

MAIN CABIN SEAT TRACK CORRODED. BS 300-310 RBL 11. MAJOR REPAIR ACCOMPLISHED: R & R SEAT TRACK FROM STA 300-420, PN 141T5121-220. INSTALLED IAW AND BAC DWG 141T5250.

Part: LEVER — OUT OF ADJUST (L4 GIRT BAR) · airframe 66,373 hrs · 24,848 cycles

DOOR 4L SLIDE DISARM LEVER WAS DIFFICULT TO DISARM. ADJUSTED FWD CAM VERTICAL SETTING ON GIRT BAR CRANK. OPERATIONAL CHECK IS NORMAL.

Part: CAM — OUT OF ADJUST (L3 GIRT BAR) · airframe 66,373 hrs · 24,848 cycles

DOOR 3L WILL NOT DISARM. ADJUSTED VERTICAL SETTING OF FWD GIRT BAR CRANK CAM. OPERATIONAL CHECK NORMAL,

Part: GUARD — FAULTY (EMERGENCY LIGHTS) · airframe 65,906 hrs · 24,681 cycles

COCKPIT EMERGENCY EXIT LIGHT WILL NOT ARM WITH SWITCH CLOSED. REPLACED GUARD.

Part: SKIN — DELAMINATED (INLET COWLING) · airframe 65,577 hrs · 24,561 cycles

NR 1 ENG INLET COWL 12:00 TO 3:00 FROM L/E TO T/E HAS OUTER SKIN DELAMINATION APPROX 3FT BY 6FT. REPLACED NOSE COWL.

Part: LIGHT — BROKEN (CABIN) · airframe 65,337 hrs · 24,471 cycles

EMERGENCY LIGHT ABOVE SEAT 31D BROKEN. SECURED LIGHT ASSY.

Part: LIGHT — LOOSE (CABIN) · airframe 65,337 hrs · 24,471 cycles

EMERGENCY LIGHT ON BULLNOSE SEAT 23D LOOSE. SECURED LIGHT ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,091 hrs · 24,378 cycles

EMERGENCY LIGHT AT AFT LAV IS INOPERATIVE. RELAMPED, OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 65,091 hrs · 24,378 cycles

EMERGENCY LIGHT AT FWD COAT CLOSET IS IN-OP. REPLACED LEAD IN WIRE. OPS CHECKS GOOD.

Part: FAN — FAILED (CABIN) · airframe 64,549 hrs · 24,175 cycles

FUMES IN CABIN, FLIGHT DIVERTED. FOUND THE EQP COOLING 1 SUPPLY FAN POPPING CB. FAN REMOVED. REPLACED COOLING FAN. IMPELLER HAD FOD TO THE L/E, CAUSED BEARING TO DAMAGE AND IMPELLER RUB ON HSG. STATOR ALSO FAILED ELECTRICAL TEST. CONFIRMED BAD. RAN PACKS AND ELECTRICAL SYS WITH ENGINES AND APU SUPPLYING POWER, NO ELECTRICAL FUMES NOTED.

Part: FAN — NOISY (RT RECIRCULATION) · airframe 64,354 hrs · 24,098 cycles

RT RECIRC FAN EXTREMELY NOISY. DEFERRED FOR LACK OF PARTS AT ORD. FOUND NEW STYLE FAN WITH RESTRICTOR PLATE INSTALLED. FAN FILTER REPLACED DUE TO BEING CLOGGED WITH DUST. DECIBLE READING WITH BOTH ENG'S RUNNING IS AT 10. THE RISER DUCTS ON THE FO'S SIDE MAKING LOAD RATTLING NOISE AND WILL NEED ESTIMATED 3 SHIFT SLOT FOR CLEANING. 3 SHIFT SLOT RQSTD. REPLACED RT RECIRC. FAN IAW MM. OPS CHECK GOOD IAW SERVICE TIP. PLACARD REMOVED.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,267 hrs · 24,064 cycles

EMERGENCY EXIT FLOOR LIGHTING STRIP DAMAGED NEAR 13C. SECURED STRIP.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 64,024 hrs · 23,968 cycles

CREW REPORTS RT ENG HAD A COMPRESSOR STALL AT 130KTS DURING TAKEOFF. (ONE BANG). PARAMETERS DECREASED SLIGHTLY THEN RETURNED TO NORMAL. NO EXCEEDANCES OCCURED, ENGINE IS OPERATING NORMALLY. CREW ALSO STATES THEY HAD A 30 DEGREE CROSSWIND AND LIGHT SNOW AT THE TIME. AC DEICED TYPE 4, RUNWAY CLUTTERED LEVEL 1, STATIC RUNUP ON TAKE OFF NORMAL. TROUBLE SHOT COMPRESSOR STALL. ACCOMPLISHED FIM TASK WITH NO DEFECTS NOTED, REPLACED MAIN ENG OIL FILTER, CHECKED CHIP DETECTOR AND EPCS PG WITH NO DEFECTS NOTED. FAILED BORO INSP OF 6TH STG. MANY BLADES WITH NICKS, TEARS, CRACKS AND MISSING MAT'L IN AREA C OF L/E AND T/E. MANY BLADES WITH CRACKS. ENGINE WAS REMOVED SHORTLY AFTER INCIDENT.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 63,971 hrs · 23,942 cycles

SPAR VALVE AND ENG VALVE CAME ON AFTER ENGINE START AND FLAMED OUT (RT ENG). SPAR VALVE LIGHT ON PEDESTAL AND ENGINE VALVE LIGHT COME ON AFTER TURNING ON ENGINE ANTI-ICE. REPLACED NR 2 ENG SPAR VALVE. OPS CHECK GOOD.

Part: CONTROL PANEL — BROKEN (EMERGENCY LIGHTS) · airframe 63,784 hrs · 23,862 cycles

EMERGENCY LIGHT SWITCH COVER ON OVER HEAD PANEL BROKEN. REPLACED EMERGENCY LIGHTS OXYGEN CONTROL PANEL.

Part: MECHANISM — OUT OF ADJUST (R3 DOOR) · airframe 63,755 hrs · 23,854 cycles

3R DOOR WON'T ARM. FOUND A STIFF BEARING ON UPPER TORQUE TUBE OF DOOR EMERGENCY MECHANISM. CLEANED AND LUBED BEARING. DOOR ARMS PROPERLY. ALSO ADJUSTED EMERGENCY MECHANISM.

Part: ACTUATOR — TRIPPED (SLATS) · airframe 63,753 hrs · 23,853 cycles

L/E SLAT DISAGREE MESSAGE, RTFL SLAT-FLAP OPS STOPPED AT AN INDICATED POSITION JUST LESS THAN 1. ACCOMPLISHED REVIEW OF FSEU LAST FLIGHT FAULT SHOWS L/E DISAGREE MSG NR 310. VISUALLY CHECK L/E ROTARY ACTUATORS. NR 6 INBD ROTARY ACTUATOR WAS TRIPPED. ALL OTHERS OK. RESET NR 6 INBD ROTARY ACTUATOR TRIP IAW SERVICE TIP. FLAPS OPERATION NORMAL 5 CYCLES WITHOUT TRIP.

Part: ACTUATOR — MALFUNCTIONED (NR 6 SLAT) · airframe 63,753 hrs · 23,853 cycles

LE SLAT DISAGREE MSG, RTFL. SLAT-FLAP OPS STOPPED AT AN INDICATED POSITION JUST LESS THAN 1. ACCOMPLISHED REVIEW OF FSEU. LAST FLIGHT FAULT SHOWS L/E DISAGREE MSG NR 310. VISUALLY CHECKED L/E ROTARY ACTUATORS. NR 6 INBD ROTARY ACTUATOR WAS TRIPPED. ALL OTHERS OKAY. RESET NR 6 INBD ROTARY ACT TRIP PER SERVICE TIP. INSPECTED ALL SLAT ROTARY ACT OVERLOAD INDICATORS. FOUND NR 6 SLAT INBD TRACK ROTARY ACT OVERLOAD IND POPPED-SECOND TIME IN TWO LEGS. REPLACED ROTARY ACTUATOR. FOUND REMOVED ACTUATOR DIFFICULT TO ROTATE WITH SEVERE BINDING. SLAT OPERATION NORMAL WITH NO MESSAGES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,746 hrs · 23,849 cycles

DOOR 2L SLIDE LIGHT NOT ON WHEN ARMED. REPLACED LAMPS FOR SLIDE LIGHT AT DOOR 2L. CYCLED DOOR ARMED LEVER NUMEROUS TIMES AND SLIDE LIGHT OPERATED NORMALLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,678 hrs · 23,827 cycles

EXT EVAC LT INOP AT DOOR 1 RT, RELAMPED.

Part: LIGHT — NOT SEATED (CABIN) · airframe 63,678 hrs · 23,827 cycles

LT AFT OVERWING EVAC LIGHT INOPERATIVE, RESEATED LAMP.

Part: SKIN — BURNED (BS 347) · airframe 62,800 hrs · 23,490 cycles

RIVET HAS BURN MARK ON LEFT SIDE OF FUSELAGE AT APPROX STATION 347 AND APPROX 10 INCHES BELOW AND AFT OF THE NUMBER SIX ON THE NOSE NUMBER. MAJOR REPAIR ACCOMPLISHED PER MM. REPLACED FASTENER.

Part: SKIN — BURNED (BS 233) · airframe 62,800 hrs · 23,490 cycles

RIVET HAS BURNT EDGE ON LEFT SIDE OF FUSELAGE AT APPROX STATION 233 AND APPROX 35 INCHES BELOW AOA SENSOR. MAJOR REPAIR ACCOMPLISHED PER MM. REPLACED FASTENER.

Part: SKIN — BURNED (FUSELAGE) · airframe 62,800 hrs · 23,490 cycles

RIVET HAS BURNT EDGE AT APPROX STATION 216.8 AND APPROX 41 INCHES BELOW AUX 2 PITOT PROBE ON LEFT SIDE OF FUSELAGE. MAJOR REPAIR ACCOMPLISHED PER MM. FASTENER REPLACED.

Part: FASTENER — BURNED (FUSELAGE) · airframe 62,800 hrs · 23,490 cycles

HIGH LOCK HAS BURNT EDGE ON LEFT SIDE OF FUSELAGE AT APPROX STATION 264 AND APPROX 17 INCHES FWD AND ABOVE THE OUTBOARD FWD CORNER OF THE LEFT NOSE GEAR DOOR. MAJOR REPAIR ACCOMPLISHED PER MM. DAMAGE NOT ON FASTENER.

Part: SKIN — BURNED (BS 280) · airframe 62,800 hrs · 23,490 cycles

RIVET HAS BURNED EDGE LEFT SIDE OF FUSELAGE AT APPROX STATION 280 AND APPROX 12 INCHES AFT AND 19 INCHES ABOVE THE OUTBOARD FWD CORNER OF THE LEFT NOSE GEAR DOOR. MAJOR REPAIR ACCOMPLISHED PER MM. REPLACED FASTENER.

Part: SKIN — BURNED (BS 367) · airframe 62,800 hrs · 23,490 cycles

RIVET HAS BURNED MARK ON THE LEFT SIDE OF THE FUSELAGE AT APPROX STATION 367 AND APPROX 29 INCHES BELOW AND AFT OF THE NUMBER SIX OF THE NOSE NUMBER. MAJOR REPAIR ACCOMPLISHED PER MM. REPLACED FASTENER.

Part: WIRE — BURNED (E&E BAY) · airframe 62,246 hrs · 23,259 cycles

FOUND 8 BURNT WIRES IN BUNDLE ABOVE E4-1, MARKED WIRE BUNDLE WITH TAPE, BURNT WIRE ARE ABOUT 2 INCHES INBOARD OF TAPE. THE SUSPECT ROOT CAUSE FOR THE WIRE DAMAGE WAS THAT THE WIRES BUNDLES WERE NOT TIED DOWN. SECURED PROPERLY. AS SUCH THE TWO WIRE BUNDLES THAT RUN PERPENDICULARLY TO EACH OTHER CAME IN CONTACT AGAINST EACH OTHER AND BECAME WORN. WIRE BUNDLES WERE REPAIRED PROPERLY AND SECURED CORRECTLY.

Part: ENGINE — FAILED (NR 2)

DIVERTED ON AMBER ALERT WITH NR 2 ENG SHUTDOWN. ACCOMPLISHED NR 2 ENGINE BORESCOPE INSP OF LPC, HPC, COMBUSTION CHAMBER INNER AND OUTER LINER, NGVS AND INJECTORS, HPT 1 AND 2 BLADES AND LPT 3 BLADES. NO LIMITING DISTRESS. ALL PLUGS INSTALLED. TROUBLESHOOT ENG 2 FLAMEOUT. FOUND PMA STATOR NR 2 ENG OPEN WINDINGS AT PHASES A,B, AND C AND OPEN SPEED WINDING AT D4846 (W1P6) AND OPEN WINDINGS AT PHASES A.B. AND C. AT D4858 (W2P6) CONFIRMED CORRECT RESISTANCE VALUES ON NEW UNIT REPLACED ON SEQ NR 2462002. PERFORMED WIRING CHECKS REF EPCS MSGS3 51-17, 275-15, AND 351-27. ALL CHECKS NORMAL.

Part: SLIDE — UNSERVICEABLE (OVERWING EXIT) · airframe 61,355 hrs · 22,922 cycles

LT OVERWING SLIDE IS UNRAVELED IN THE CRATE. REPLACED LT OVERWING SLIDE PACK.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 60,324 hrs · 22,512 cycles

DOOR 1L DIFFICULT TO ARM. LEVER VERY TIGHT. CHECKED GIRT BAR AREA AND LUBED, CK'D GOOD.

Part: ENGINE — BIRD INGESTION · airframe 60,307 hrs · 22,506 cycles

RTFL DUE TO BIRD STRIKE. PERFORM NR 1 ENG BURNOUT PROCEDURE DUE TO ODOR IN CABIN (BIRD STRIKE NR 1 ENGINE). REMOVE NR 1 ENGINE DUE TO LPC STG 1 BOOSTER DAMAGE AND LINER SEPARATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 59,168 hrs · 22,097 cycles

EEL LIGHT STRIP AT MID LAV INOP WHEN EMERGENCY LIGHTS SELECTED TO ON POSITION. *S/D* CONNECTOR DISCONNECTED AT EEL STRIP. SECURED CONNECTOR, OPS CHECKED GOOD.

Part: SKIN — CRACKED (R1 DOOR) · airframe 58,545 hrs · 21,862 cycles

1R DOOR INNER SKIN HAS A CRACK PROTRUDING FROM LIGHTENING HOLE, LWR AFT END OF DOOR. CRACK IS APPROX 0.100 INCH. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED FILLERS, REPAIR STRAP, TRIM & DOUBLER.

Part: BEARING — FAULTY (DOOR 4R) · airframe 58,545 hrs · 21,862 cycles

4R DOOR WILL NOT ARM. EMERGENCY LINKAGE TORQUE TUBE BEARINGS SEIZED. REPLACED TORQUE TUBE BEARINGS, DOOR OPS NORMALLY.

Part: BEARING — FAULTY (DOOR 1R) · airframe 58,545 hrs · 21,862 cycles

DOOR 1R WILL NOT ARM. EMERGENCY LINKAGE TORQUE TUBE BEARINGS SEIZED. REPLACED TORQUE TUBE BEARINGS, DOOR OPS NORMALLY.

Part: SLIDE — WILL NOT ARM (R3 DOOR) · airframe 58,545 hrs · 21,862 cycles

FOUND DOOR 3R WILL NOT ARM. ADJUSTED/REPAIRED DOOR 3R, OPS CHECKED GOOD, ARMS/DISARMS NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,398 hrs · 21,475 cycles

FOUND FWD EEL LAMP AT FWD CLOSET INOP. REPLACED LAMP ASSY, OPS CHECKED NORMALLY.

Part: LIGHT — UNSECURE (CABIN) · airframe 57,124 hrs · 21,383 cycles

EMERGENCY PATH LIGHTING PULLED OUT FROM FLOOR AT SEAT 1AB.

Part: WINDOW — CRACKED (COCKPIT) · airframe 56,491 hrs · 21,149 cycles

L1 WINDOW SHATTERED IN FLIGHT WITH ARCING AT BOTTOM OF WINDOW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,309 hrs · 21,084 cycles

AISLE EMERGENCY LIGHT AT SEAT 27D IS INOP. ON TROUBLESHOOTING FOUND THAT LIGHT LAMP WAS BAD. REMOVED AND INSTALLED NEW LAMP.

Part: POWER CABLE — OUT OF ADJUST (R4 DOOR) · airframe 56,307 hrs · 21,083 cycles

NR 4R EMERGENCY POWER CABLE TRIGGER FAILED TEST.

Part: PLATE — CORRODED (GIRT BAR) · airframe 56,307 hrs · 21,083 cycles

DOOR 1R, 2L & 4L GIRT BAR RESTRAINING PLATES ARE CORRODED.

Part: PULLEY — CRACKED (ELEVATOR CONTROL) · airframe 56,307 hrs · 21,083 cycles

CABIN CEILING AREA, ELEVATOR CONTROL CABLE PULLEY IS CRACKED AT STA 340, STR 4L. REMOVED AND REPLACED PULLEY.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,307 hrs · 21,083 cycles

AFT PIT FRAME DENTED AT STA 1500 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSTALLED ANGLE & REPAIR ANGLE. COLD WORKED HOLES & INSURANCE CUT.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,307 hrs · 21,083 cycles

AFT PIT FRAME DENTED AT STA 1480 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: ROUTED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLE.

Part: PANEL — GOUGED (NR 1 PYLON) · airframe 56,307 hrs · 21,083 cycles

NR 1 PYLON AFT BULKHEAD UPPER CLOSE OUT PANEL HAS DEEP GOUGE. BLENDED GOUGE AND FABRICATED PANEL PER BOEING DWG 311N3150 AND INSTALLED REPAIR PER UA ENGINEERING SPECIFICATIONS.

Part: GATE — CORRODED (L1 DOOR) · airframe 56,307 hrs · 21,083 cycles

L-1 DOOR UPPER GATE CORRODED. REPLACED UPPER GATE FOR DOOR 1L.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,062 hrs · 20,992 cycles

EMERGENCY SLIDE LIGHT ON EXTERIOR OF ACFT AFT OF LT WING TRAILING EDGE INOP. RELAMPED.

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 56,053 hrs · 20,988 cycles

NR 1 ENGINE HIGH OIL COMSUMPTION. [08-08-07] REPLACED DEOILER CARBON SEAL AND STARTER CARBON SEAL. ATTRIBUTE THE PROBLEMS TO FUEL OIL HEAT EXCHANGER MR79230 (645-9029) HAZMAT & FUEL OIL HEAT EXCHANGER BYPASS VALVE PCN 645-9061(HAZMAT) & THEIR ASSOCIATED SEALS & PACKINGS.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 55,580 hrs · 20,806 cycles

CABIN DOOR 2 RIGHT CUTOUT FOR UPPER HINGE HAS 0.25 INCH CRACK. [SUP 06-06-07] INSTALLED A DOUBLER REPAIR ON THE AFFECTED AREA WITH BOEING APPROVED UA ENGINEERING SPECIFICATION.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 55,580 hrs · 20,806 cycles

NR 2 LEFT DOOR FWD FRAME CUTOUT FOR UPPER HINGE CRACKED. [SUP 06-06-07] INSTALLED A DOUBLER REPAIR ON THE AFFECTED AREA WITH BOEING APPROVED UA ENGINEERING SPECIFICATION.

Part: UNKNOWN — UNKNOWN · airframe 55,390 hrs · 20,731 cycles

NO POTABLE WATER AVAILABLE. CREW ALSO NOTICED A STRANGE NOISE AND VIBRATION IN TAIL SECTION. [06-14-07] UPON ARRIVAL FOUND SERVICE VALVE LEFT OPENED, SECURED CLOSED AND SERVICED POTABLE WATER, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 55,032 hrs · 20,598 cycles

DOOR 2R SLIDE ARMED LIGHT INOPERATIVE. [SUP 05-18-07] REPLACED LAMPS. THIS WAS A CASE OF A FUSED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,246 hrs · 20,298 cycles

AFT EEL LIGHT STRIP B INOP. TROUBLESHOT SYSTEM AND FOUND EPL CABLE DAMAGED. REPAIRED CABLE. LIGHT BAR CHECKS GOOD.

Part: IDG — FAILED (LEFT GENERATOR) · airframe 53,195 hrs · 19,906 cycles

FOUND LEFT GENERATOR TRIPPED DURING TAKEOFF ROLL. THIS DISCREPANCY IS ATTRIBUTED TO A FAILED IDG. REPLACED IDG.

Part: WARNING LIGHT — ILLUMINATED (NR 1 ENGINE) · airframe 51,802 hrs · 19,404 cycles

DIVERTED TO PIT UNDER AMBER ALERT WITH NR 1 ENGINE SHUT DOWN DUE TO AN ENGINE OIL FILTER BYPASS EICAS MESSAGE. BUMPER BEARING FAILURE DUE POSSIBLY TO EXCESSIVE VIBRATION FROM LOWER DRIVE SHAFT. LOWER DRIVE SHAFT FAILED BALANCE CHECK PER PWA SB 72-693

Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 50,093 hrs · 18,791 cycles

RETURNED TO FIELD DUE TO HYDRAULIC PROBLEMS. FOUND HYDRAULIC PRESSURE LINE WITH STREAMING LEAK. REPLACED HOSE, REPLACED RETURN AND CASE DRAIN FILTERS, AND SERVICED SYSTEM TO FULL. LEAK CHECKED SAME. PRESSURE WASHED FUSELAGE BELLY AS REQUIRED. RETURNED AIRCRAFT TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,903 hrs · 18,716 cycles

EEL STRIP IN FRONT OF MID CABIN LAV IS INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY.

Part: DUCT — SPLIT (AIR COND) · airframe 45,628 hrs · 17,136 cycles

RETURN TO FIELD DUE TO AIR CONDITIONING CABIN TEMPERATURE PROBLEM. OVERHEAD DISTRIBUTION DUCT AT ROWS 15 TO 18 HAD 4 FOOT SPLIT. REPLACED OVERHEAD DUCT.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,607 hrs · 17,130 cycles

EXTERNAL FUSELAGE SKIN DENTED IN TWO AREAS FWD OF NR 2 LT MED AT STA 610-620 STR 15LT. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. INSTALLED FILLER AND DOUBLER REPAIR.

Part: TURBINE BLADES — FAILED (NR 1 ENGINE) · airframe 41,389 hrs · 15,602 cycles

NR 1 ENGINE COMPRESSOR STALL AT FL200, ENGINE SELF RECOVERED. ENGINE WAS REMOVED FOR METAL IN THE TAILPIPE, IT HAD A NORMAL ECM TREND PLOT. AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE.

Part: FRAME (BODY STATION 1500) · airframe 37,661 hrs · 14,231 cycles

AFT PIT FUSELAGE FRAME AT BS 1500, RBL28, GOUGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. BLENDED AREA. INSTALLED REPAIR ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,661 hrs · 14,231 cycles

AFT CABIN FLOORBEAM STATION 1640, RBL 12 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,661 hrs · 14,231 cycles

CABIN FLOORBEAM 365 CORRODED AT RBL 15, 24, 30, 36, 48. MAJOR REPAIR ACCOMPLISHED. REMOVED T-CAP, INSTALLED NEW T-CAP WITH SUPPORT ANGLES AND STRAPS.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,661 hrs · 14,231 cycles

CABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,661 hrs · 14,231 cycles

CABIN FLOOR INTERCOSTAL BETWEEN STA 324 AND 418, BL 0, HAS CORROSION ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW INTERCOSTAL.

Part: PLATE — CORRODED (FUSELAGE) · airframe 33,761 hrs · 14,231 cycles

CABIN AFT DECK PLATE CORRODED, STA 1681, RBL 1.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER ON DECK PLATE.

Part: CREASE BEAM — CORRODED · airframe 37,661 hrs · 14,231 cycles

CABIN FLOOR INNER CREASE BEAM BELOW DOR 2L DRAIN GUTTER HAS EXCESSIVE CORROSION STA.700 TO 720 LBL70" STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF INNER CREASE BEAM L-ANGLE Z ANGLE IN DOORWAY FROM STA.665 TO 754 AT FACTORY SPLICES INSTALLED NEW PART.

Part: CREASE BEAM — CORRODED · airframe 37,661 hrs · 14,231 cycles

RIGHT HAND CABIN FLOOR WEB BETWEEN INNER AND OUTER CREASE BEAM CORD WAS CORODED AT STA 1021 RBL 68. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPLACEMENT WEB FROM 7075-0 HEAT TREATED TO T6 INSTALLED NEW WEB BETWEEN STA.1020-1039 RBL68 STRINGER 17R.

Part: BYPASS VALVE — LEAKING (SLATS) · airframe 34,650 hrs · 13,142 cycles

LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. GEAR AND FLAP WERE EXTENDED BY ALTERNATE METHOD. *S/D* REPLACED SLAT BYPASS VALVE IAW AMM 27-81-09. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (LT GENERATOR)

RETURNED TO ORD DUE TO ELECTRICAL PROBLEMS. *S/D* W2018-0002-06 WAS FOUND BROKEN AT LEFT GENERATOR CIRCUIT BREAKER C901 PHASE B. LOSS OF PHASE B AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE BROKEN WIRE TERMINAL WAS REPLACED.

Part: LIGHT — LOOSE (CABIN)

AT SEAT 9D, EMERGENCY LIGHT ON BULLNOSE, JUST BELOW BIN, PUSHED IN. SECURED LIGHT ASSEMBLY.

Part: RADIO SYST — MALFUNCTIONED (COCKPIT)

FLIGHT OFFICER'S RADIO SYSTEM BLOCKING ALL TRANSMISSIONS AND RECEPTIONS WHEN ACTIVATED.

Part: FAN — FAILED (COCKPIT)

LIGHT SMOKE IN COCKPIT WITH PACS ON AND APU RUNNING. *S/D* APU WAS REPLACED DUE TO MASSIVE COOLING FAN FAILURE. FAN ROTOR FAILED, HOUSING WAS BROKEN AND MINOR FOD TO BOTH COMPRESSORS. FAILED APU REPLACED WITH NEW UNIT, OPERATION CHECKS NORMAL.

Part: HINGE — DAMAGED (RUDDER)

AIRCRAFT EXPERIENCED A SEVERE LIGHTNING STRIKE ON APPROACH TO EWR. *S/D* DUE TO LIGHTNING STRIKE, RUDDER AND IT' SUPPER HINGE WAS DAMAGED. REMOVED AND REPLACED DAMAGED RUDDER, UPPER HINGE, UPPER FITTING AND ASSOCIATED HARDWARE. RIGGED RUDDER PER MAINTENANCE MANUAL, OPERATION CHECKS NORMAL.

Part: EXCITER — MALFUNCTIONED (APU)

LEFT IDG DISCONNECTED AND APU WOULD NOT START IN-FLIGHT AFTER 3 ATTEMPTS. FLIGHT DIVERTED TO SLC. SUPPLEMENTAL DATA UPDATE: REPLACED IGNITION EXCITER, IGNITION PLUG, AND LEAD. OPERATION CHECKS NORMAL. IGNITION EXCITERS ARE BEING UPGRADED PER OEM 49-41-09, TO IMPROVE HIGH ALTITUDE STARTS.

Part: RETRACT MECH — MALFUNCTIONED (LE FLAPS)

UNABLE TO MOVE FLAPS NORMALLY, LEADING EDGE LIGHT ON AND FLAP ASYMMETRY MESSAGE. FLAPS RECYCLED IN ALT OK, BUT STILL LOCKED OUT IN NORMAL. BITE CHECK ON NR 1 FSEU SHOWS SLAT LOSS.