N469FE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,533 hrs · 31,679 cycles

DURING STANDBY POWER CHECK, EMEGENCY LIGHT OVER MAIN ENTRY DOOR INOPERATIVE. LIGHT UNIT WAS NOT INSTALLED FULLY. RESEATED ASSY, NO HELP. REPLACED LIGHT BULBS AND LIGHT ILLUMINATED FOR A SPLIT SECOND AND DIED. R & R L1 DOOR EMERGENCY LIGHT ASSY IAW MM. OPS CHECKED NORMAL IAW CH 33.

Part: LIGHT — FAILED (CABIN) · airframe 45,533 hrs · 31,680 cycles

DURING STANDBY POWER CHECK, EMEGENCY LIGHT OVER MAIN ENTRY DOOR INOPERATIVE. LIGHT UNIT WAS NOT INSTALLED FULLY. RESEATED ASSY, NO HELP. REPLACED LIGHT BULBS AND LIGHTS ILLUMINATED FOR A SPLIT SECOND AND DIED. R & R L1 DOOR EMERGENCY LIGHT ASSY IAW MM. OPS CK NORMAL IAW CH 33.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 45,525 hrs · 31,672 cycles

UNABLE TO CLOSE F/O WINDOW. ADJUSTED F/O SLIDING WINDOW IAW MM 56-12-011-05. OPS CKS. FINAL CLOSED.

Part: COALESCER BAG — ODOR · airframe 45,522 hrs · 31,670 cycles

FAINT ELECTRICAL ODOR AFTER DEPARTURE, ODOR GOT MUCH WORSE AFTER 10 MINUTES AND LEVEL OFF AT 320. VERY IRRITATING ELECTRICAL SMELL ALSO ALMOST A VERY STRONG ONION - LIKE SMELL GOT WORSE ON INITIAL DESCENT. PUT O2 MASKS ON AND BY THE TIME WE LANDED AND REMOVED MASKS AND WERE DEPRESSURIZED, SMELL WAS MOSTLY GONE. UPON ARRIVAL, SMELL OF SMOKE COULD NOT BE DETECTED OR DUPLICATED. RAN BOTH PACKS, 3 ENGINES, ALL ELECTRICAL COMPONENTS, HYD, FANS, AND ACFT ACCESSORIES. INSPECTED UPPER, LOWER CARGO COMPARTMENTS, WHEEL WELL BAY, AFT STAIRWELL, E&E BAY. R & R WATER SEPARATOR COALESCER BAGS IAW MM 21-55-051-4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,474 hrs · 31,627 cycles

MAIN DECK & MAIN ENTRY EMERGENCY LIGHTING DID NOT TEST PROPERLY. DURING S/O STBY CHECK LIGHTS CAME ON FOR APPROX 3 SECONDS AND DIMMED & WENT OUT. (B.P.B) REPLACED EMERGENCY LIGHT BATTERIES FOR CABIN AND L1 EXITS IAW SMP FOR 33-50-101-2-0. SDR ENTERED IN ERROR- PLEASE DELETE.

Part: LIGHT — NO TEST (CABIN) · airframe 45,474 hrs · 31,627 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT DOES NOT TEST. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,474 hrs · 31,627 cycles

MAIN DECK & MAIN ENTRY EMERGENCY LIGHTING DID NOT TESET PROPERLY DURING S/O STBY CHECK. LIGHTS CAME ON FOR APPROX 3 SECONDS AND DIMMED & WENT OUT. (B.P.B) REPLACED EMERGENCY LIGHT BATTERIES FOR CABIN AND L1 EXITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,430 hrs · 31,587 cycles

L1 DOOR UPPER HINGE CUT OUT DOUBLER HAS THE MAX OVERSIZED FASTENER HOLES. REMOVED DOUBLER AT L-1 DOOR UPPER HINGE, FABRICATED NEW DOUBLER AND FILLER REPAIR, AND INSTALLED DOUBLER AND FILLER REPAIR IAW EA 7-5330-136770 AND EO 7-5330-7-2345 PT2 SECTION 4.A.

Part: FRAME — CORRODED (BS 950E S27-28L) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

CORROSION ON UPPER FLANGE OF FRAME AT BS 950E BETWEEN STRINGER 28L AND 27L. CUT OUT DAMAGED SECTION OF UPPER FRAME FLANGE IAW SRM 51-40-3 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 REV 103

Part: SKIN — GOUGED (BS 480-620) · airframe 45,430 hrs · 31,587 cycles

INNER SKIN IS GOUGED IN NUMEROUS PLACES FROM BS 480 TO 620 BETWEEN STR 2L AND 3L. CUTOUT DAMAGED AREA AT MCD INNER SKIN BS 480 AND BS 620 BETWEEN STR 2L AND 3L, FABRICATED REPAIR FILLERS AND REPAIR DOUBLERS, AND INSTALLED REPAIR PARTS IAW EA 7-5310-152402.

Part: SKIN — DAMAGED (BS 440 S14L) · airframe 45,430 hrs · 31,587 cycles

MAIN CARGO DOOR CUT-OUT, SKIN LAP JOINT - THRU DAMAGE AT STA 440, STR 14L. CUTOUT DAMAGED AREA AT FUSELAGE SKIN MCD CUTOUT LAP JOINT, FABRICATED DOUBLER, STRUCTURAL FILLER, TAPER FILLER, AND INTERNAL FILLER. INSTALLED REPAIR PARTS IAW EA 7-5330-126868.

Part: FRAME — DAMAGED (BS 783) · airframe 45,430 hrs · 31,587 cycles

CABIN BS 783, LT FRAME 6.2500" ABOVE CUSP WEB HAS HOLE BELOW FASTENER HOLE. REMOVED DAMAGED AREA AT CABIN. FABRICATED FREEZE PLUG, INSTALLED FREEZE PLUG AND FASTENER IAW EA 7-5310-136773 AND SRM 51-10-7.

Part: SUPPORT ANGLE — CRACKED (BS 1263) · airframe 45,430 hrs · 31,587 cycles

AFT AIRSTAIRS RT LOWER TORQUE BOX BS 1263 FWD SIDE OF ANGLE IS CRACKED IN 2 PLACES. REMOVED ANGLE AT AFT AIRSTAIRS RT LOWER TORQUE BOX BS 1263 FWD SIDE IAW SRM 51-30-2. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED ANGLE IAW DWG 65-17517.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 45,430 hrs · 31,587 cycles

LT ELEVATOR TIP LOWER SKIN IS CRACKED AROUND RIVET. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-20-3 FIG 2.

Part: TORQUE BOX — MISREPAIRED (BS 1273) · airframe 45,430 hrs · 31,587 cycles

AFT AIRSTAIRS RT LOWER TORQUE BOX, BS 1273 MISREPAIRED. REMOVED ANGLE AT AFT AIRSTAIRS RT LOWER TORQUE BOX IAW SRM 51-30-2. FABRICATED AND INSTALLED ANGLE IAW DWG 65-17518 AND SRM 51-30-2.

Part: FRAME — CORRODED (BS 970 S27-28L) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

CORROSION ON UPPER FLANGE OF FRAME AT BS 970, BETWEEN STRINGER 28L AND 27L. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-40-3 FIG 1 REV 103

Part: REINFORCEMENT — DAMAGED (BS 950E) · airframe 45,430 hrs · 31,587 cycles

UPPER REINFORCEMENT DAMAGED AT BS 950E BETWEEN 28L AND 27L. CUT OUT DAMAGED REINFORCEMENT SECTION IAW SRM 51-40-4 FIG 1. FABRICATED NEW REINFORCEMENT SECTION AND 2 EACH ANGLE DOUBLERS AND RADIUS FILLER IAW SRM 51-40-4 FIG 1. INSTALLED SECTION, 2 EACH DOUBLERS AND RADIUS FILLER IAW SRM 51-40-4 FIG 1 REV 103.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 45,430 hrs · 31,587 cycles

GALLEY DOOR EXTERIOR SKIN CRACKED SERVERAL PLACES AROUND ROW OF RIVETS BELOW LOWER HINGE ARM. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLER, AND INSTALLED REPAIR PARTS IAW SRM 52-00-3 FIG 4 AT GALLEY DOOR EXTERIOR SKIN BELOW LOWER HINGE ARM.

Part: SHEAR TIE — CORRODED (BS 450) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

CORROSION ON SHEAR TIE AT BS 450 BETWEEN STRINGER 28R AND 28L. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15 REV 103.

Part: FRAME — DAMAGED (BS 1070) · airframe 45,430 hrs · 31,587 cycles

AFT PIT - ELONGATED FASTENER HOLE IN FRAME AT BS 1070 RBL 30 CUT OUT DAMAGED AREA OF UPPER FLANGE OF FRAME IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER, FILLER AND SHIM IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR DOUBLER, FILLER AND SHIM IAW SRM 51-30-2 AND 51-40-3 FIG 1 REV 103.

Part: SEAT TRACK — CORRODED (BS 760-850) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

SEAT TRACK HAS CORROSION AT BS 760-850 LBL 45.5. REMOVED SEAT TRACK SECTION AT BS 760-850 LBL 45.5 IAW SRM 51-30-2. LOCATED NEW SECTION IAW DWG 65-19601 AND SRM 51-30-5. INSTALLED SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 740-850) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

SEAT TRACK HAS CORROSION AT BS 740-850, RBL 45.5. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. LOCATED SECTION IAW DWG 65-19601 AND SRM 51-30-2. INSTALLED SECTION IAW SRM 51-30-2.

Part: SPAR — CRACKED (LT WING) · airframe 45,430 hrs · 31,587 cycles

LT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL118. REMOVED WEB AND DOUBLER IAW SRM 51-30-2 REV 103. CUT OUT CRACKED LOWER SPAR CHORD IAW DRAWING SR 27-57-038 REV C. FABRICATED NEW WEB, DOULER, SPAR CHORD SECTION, RADIUS FILLER, 2EA RADIUS BLOCKS AND 2EA REPAIR ANGLES IAW DRAWING SR 27-57-038 REV C. INSTALLED ALL REPAIR PARTS IAW DRAWING SR 27-57-038 REV C.

Part: STRINGER — CORRODED (BS 450 S28R) · corrosion level 2 · airframe 45,430 hrs · 31,587 cycles

E&E COMPARTMENT- CORROSION ON STRINGER 28R AT BS 450. REMOVED CORRODED SECTION OF STRINGER IAW SRM 51-30-2. FABRICATED NEW SECTION OF STRINGER IAW SRM 51-30-5 AND 51-20-1 FIG 2. INSTALLED STRINGER IAW SRM 51-30-2 REV 103

Part: SUPPORT — DAMAGED (BS 1183 BULKHEAD) · airframe 45,430 hrs · 31,587 cycles

BS 1183, PRESSURE BULKHEAD VERT BEAM HAS FASTENER WITH SHORT SPACE AT LBL 17.8. TRIMMED DAMAGED AREA OFF THE AFT FLANGE TEE VERTICAL BEAM AT STA 1183 LBL 17.8 PRESSURE BULKHEAD, FABRICATED TEE VERTICAL BEAM REPAIR DOUBLER, FILLER, AND INSTALLED REPAIR TEE VERTICAL BEAM, DOUBLER, AND FILLER IAW EA 7-5310-136767.

Part: LINE — LEAKING (RUDDER ACTUATOR) · airframe 45,374 hrs · 31,540 cycles

LOSS OF A SYS PRESSURE AND ALL A SYS HYD FLUID AFTER SUSPECTED LIGHTNING STRIKE. CREW COMPLIED WITH ALL QRH PROCEDURES TO SAFELY RECOVER ACFT. HYD SYS A FLUID SHUTOFF SWITCHES WERE OFF FOR APPROX 50 MINUTES WITH ENGINES 1 AND 2 OPERATING. CREW COMPLETED MANUAL GEAR EXTENSION AND ALT FLAP EXTENSION IAW QRH. FOUND LWR RUDDER ACT. PRESSURE LINE LEAKING. REF IPC 27-20-00-21F ITEM 045, REMOVED LINE. R & R NR 2 ENG DRIVEN HYDRAULIC PUMP PER AMM 29-11-033-4 R & R NR 1 & 2 ENGINE SYS A HYDRAULIC PUMP CASE DRAIN FILTER ELEMENTS IAW MM 29-11-041-2 UP TO STEP 2(D)4. NO CONTAMINATION FOUND IN EITHER ELEMENT. R & R SYSTEM A RETURN FILTER IAW MM 29-11-102-2 UP TO STEP 2(B)6. NO CONTAMINATION FOUND. R & R NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW MM 29-11-033-4. INSTALLED NEW PRESSURE LINE ON LWR RUDDER ACTUATOR PER AMM 20-10-012-4-0 AND AMM 27-20-141- 2, PRESSURE & LEAK CHECKED LINE REF. AMM 29-00-000-2-0, NO LEAKS.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 45,216 hrs · 31,422 cycles

CLIMBING THROUGH 20,000 MSL STANDBY ALTIMETER INDICATED AN ALTITUDE THAT WAS 10,000 HIGHER THAN THE ACTUAL ALTITUDE AS INDICATED ON THE CAPTAIN'S AND F/O'S ALTIMETERS. REMAINED IN ERROR THROUGHOUT THE FLIGHT. UPON ARRIVAL FOUND STANDBY ALTIMETER INDICATING 10,000 FEET ABOVE FIELD ELEVATION. R & R STANDBY ALTIMETER IAW AMM 34-12-024-4. ACCOMPLISHED LOW LEVEL PITOT STATIC TEST IAW AMM 34-11-000-5. OPS TEST OK. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF. FINAL CLOSED.

Part: SWITCH — OUT OF ADJUST (AIRSTAIR DOOR) · airframe 45,152 hrs · 31,371 cycles

AT FL 360" AFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.

Part: SWITCH — OUT OF ADJUST (AIRSTAIR DOOR) · airframe 45,152 hrs · 31,371 cycles

AFT AIRSTAIR " LIGHT ILLUMINATED FOR 10 MINS, THEN BECAME INTERMITTENT NO BUFFET FELT AT ANY TIME. FOUND UPPER DOOR HANDLE SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW MM 52-70-001-5. CHECKED GOOD.

Part: RELAY — BURNED (EMERGENCY LIGHTS) · airframe 44,962 hrs · 31,210 cycles

DURING COCKPIT PREFLIGHT, NOTICED HEAVY WHITE SMOKE COMING FROM OVERHEAD CONTROL PANEL. ADVISED 2ND OFFICER TO REMOVE ELECTRICAL POWER FROM ACFT. ADVISED CREW TO EVACUATE. INSP O/H PANEL AREA & FOUND NO SIGNS OF BURNED WIRES, SWITCHES, CONNECTOR'S OR RELAYS, OPENED PANEL JUST AFT OF OVERHEAD PANEL & INSPECTED AREA FOR BURNED WIRES, CONNECTORS OR RELAYS AND FOUND RELAY R70 FOR EMERGENCY LIGHTS OVERHEATED & FOUND EVIDENCE ON RECEPTICAL & AREA AROUND RECEPTICAL OF AREA BEING OVERHEATED. R & R R70 RELAY, CONGFIGURED COCKPIT AS FLT CREW WOULD FOR PRE-DISPATCH CHECK. RAN APU FOR APPROX 1 HR & HAD NO EVIDENCE OF SMOKE. EMERGENCY EXIT LIGHT SYS OPS CHECK'S NORMAL. ACFT OK FOR CONTINUED SERVICE.

Part: INDICATOR — FAILED (FUEL QTY) · airframe 44,017 hrs · 30,442 cycles

NUMBER 2 FUEL GAUGE INDICATED ZERO DURING CRUISE THEN PASSING THROUGH APPROX 12000 FT GAUGE STARTED TO COME UP TO READ FUEL QUANTITY. SUMPED NR 3 TANK. NO WATER FOUND. NO FAULT CODES ON INDICATOR. CLEANED CANNON PLUG ON NR 3 VTO ON FWD SPAR. R&RD NR 3 FUEL QUANTITY GAGE INDICATOR AS A PRECAUTION PER AMM 28-41-040-4 AND OPS CHECKED PER 28-41-000-5 AND I. NO FAULTS . TRANSFERED ALL FUEL FROM TANK TO 0 READING. TRANSFERED FUEL BACK INTO NR 3 TO READING OF 11.1 WITH NO BLANKING OUT OF GAGE. ACFT OK FOR SERVICE.

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 44,006 hrs · 30,433 cycles

LT WING L/E SLAT ACTUATOR SUPPORT BRACKET CRACKED INBD SIDE AT NR 1 SLAT. REMOVED AND REPLACED NR 1 SLAT STA 390.9 RIB, WEB, AND DOUBLER IAW EA 7-5750-126863.

Part: BRACKET — CRACKED (ZONE 600) · airframe 44,005 hrs · 30,431 cycles

RT WING NR 7 SLAT ACTUATOR MOUNTING BRACKETS BOTH INBD AND OTBD ON WING SIDE ARE CRACKED AT WS 635. REMOVED AND REPLACED INBD AND OTBD NR 7 SLAT ACTUATOR MOUNTING BRACKETS AND STEEL DOUBLERS IAW FEDEX EA 7-5750-126869, WINGS, RT NR 7 SLAT STA 281.4 AND 288.6 ACTUATOR SUPPORT RIB, REPAIR OF STIFFENER AND DOUBLER CRACKS PER SB 727-57-130.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 44,003 hrs · 30,427 cycles

LT WING NR 1 SLAT ACTUATOR RIB SUPPORT INBD SIDE IS CRACKED REPAIRED BY ACCOMPLISHING EA 7-5750-126863 WINGS - LT NR 1 SLAT STA 390.9 ACTUATOR SUPPORT RIB. REPAIR OF DOUBLER CRACKS PER SB 727-57-0130.

Part: SKIN — DAMAGED (ZONE 200) · airframe 44,003 hrs · 30,427 cycles

INNER AFT EDGE OF MCD CUTOUT HAS NUMEROUS AREAS DAMAGED BY GILL LINER FASTENERS. REPAIRED BY ACCOMPLISHING EA 7-5310-126861 "FUSELAGE - AD 98-11-03 R1 - SSI 6.19A - P-F MOD MCD CUTOUT LOWER CORNER INNER SKIN, REPAIR OF GOUGE MARKS AT BS 620 S16L - EO 7-5100-7-4304".

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 44,003 hrs · 30,427 cycles

FASTENERS WITH IMPROPER SPACING STA 460 STR 10L. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330-126862 AD 98-11-03 R1 MAIN CARGO DOOR TRIPLER, DOUBLER AND FUSELAGE SKIN THRU DAMAGE AT STA 460 S10L EO 7-5100-7-4304.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

NOSE WHEEL WELL "T" ANGLE CORRODED STA 280 STR 26R. FABRICATED NEW "T" ANGLE FROM 60-10936 7075-0 EXTRUSION PO NR 8270223 DIMS 19 INCH BY 3 INCH, HEAT TREATED EXTRUSION TO T-6 CONDITION INSTALLED NEW "T" ANGLE AT BS 280 STR 26R IAW MM 51-30-5 AND BOEING DWG 65-18414 AND SRM 51-30-2.

Part: SKIN — DAMAGED (ZONE 200) · airframe 44,003 hrs · 30,427 cycles

FASTENERS WITH IMPROPER SPACING STA 440 ABOVE AND BELOW STR 14L. REPAIRED AREA IAW EA 7-5330-126868 FUSELAGE SKIN AD 98-11-03 MAIN CARGO DOOR CUTOUT FUSELAGE SKIN LAP JOINT THRU DAMAGE AT STA 440 S14L.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

E AND E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION RBL 12 BS 344. REMOVED AND REPLACED LWR CHORD WALKWAY BEAM AT RBL12 BS 294-360 WITH NEW CHORD P/N 65-19861-8 PO NR 827074 IAW SRM 51-30-5 AND SRM 51-30-2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

FWD CARGO COMPT STR 26R IS CORRODED WITH EXFOLIATION BETWEEN STA 720E AND 720F. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330-126860 FUSELAGE AD 98-03-01 SECTION 43 SKIN REPAIR OF SKIN CORROSION AT STA 720E-720F AND S26R-S27R EO 7-5100-7-4304.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

E/E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION LBL 12 BS 32. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED LT LWR CHORD AND INSTALLED NEW LWR CHORD PART NUMBER 5715216 PO NR 827075 AT E/E COMPT STA 328 LBL12 IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

CORROSION ON FLOORBEAM BETWEEN BL0 AND RBL25 STA 1110. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SECTION DIMS 2 3/4 INCH BY 2 1/2 INCH. FABRICATED REPAIR ANGLES USING BAC1490-2785 PO NR 9007702 DIMS 11 3/4 INCH BY 2 1/2 INCH AND BAC1490-2831 PO NR 9006081 DIMS 7 1/2 INCH BY 3 INCH, FILLER USING BAC1505-100617 PO NR 8270109 DIMS 2 3/4 INCH BY 2 1/2 INCH REPAIR STRAPS USING 7075-T6 .050 PO NR 9007861 DIMS 11 3/8 INCH AND 8 1/2 INCH. INSTALLED REPAIR PARTS IAW FEDEX DWG SR27-53-034.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

CORROSION ON SEAT TRACK STA 1090 TO 1130 ANS BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SECTION OF SEAT TRACK FROM BS 1010 TO 1130 AT BL0. FABRICATED NEW SECTION OF SEAT AND INSTALLED SECTION IAW SRM 51-10-2 AND 53-10-5.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

FWD CARGO COMPT CORROSION ON SKIN AT BS 680 STR 26L TO 27L. FOUND CORROSION OUT OF LIMITS CUT OUT DAMAGED AREA DIMS 2 5/8 INCH BY 2 INCH. FABRICATED DOUBLER USING 2024-T3 .063 PO NR 9008017 DIMS 8 1/2 INCH BY 2 INCH INSTALLED REPAIR PARTS IAW SRM 51-10-2 AND 53-30-3.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 44,003 hrs · 30,427 cycles

ON SKIN, IMPROPER FASTENERS USED ON REPAIR AT STA 1183 STR 21L TO 22L. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-40-2.

Part: SEAT TRACK — CHAFED (ZONE 200) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

FOUND CORROSION ON SEAT TRACK STA 1130 TO 1180 BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED SEAT TRACK IAW DWG 53FX976.

Part: SKIN — DAMAGED (BS 251) · airframe 44,003 hrs · 30,427 cycles

SKIN AT STA 251 STR 20R HAS NUMEROUS TOOL MARKS. REMOVED PREVIOUS DOUBLER REPAIR. FABRICATED NEW DOUBLER REPAIR USING 2024-T3 .050 PO NR 9007753 DIMS 13 1/2 INCH BY 13 5/8 INCH. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

CORROSION ON SEAT TRACK STA 970 TO 1030 LBL 45. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA FROM BS 960 TO 1060 DIMS 101". FABRICATED SEAT TRACK USING BAC1590-792 7178T65 PO NR 9006020. INSTALLED REPAIR PARTS IAW SRM 53-10-5.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,003 hrs · 30,427 cycles

CORROSION ON SEAT TRACK FLANGES AND ATTACH FASTENERS RBL 45 STA 1030 TO 1110. FOUND CORROSION OUT OF LIMITS, FABRICATED NEW SEAT TRACK USING BAC1520-792 PO# 9006020 DIMS 100" INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 44,003 hrs · 30,427 cycles

PREVIOUS REPAIR AT STA 188 STR 26L HAS 1 DENT AND NUMEROUS IMPROPERLY INSTALLED FASTENERS. REMOVED DOUBLER, FABRICATED NEW DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 51-30-5, 53-30-2 AND 53-30-3.

Part: SKIN — DENTED (ZONE 100) · airframe 44,003 hrs · 30,427 cycles

SKIN DENTED AT LAP SEAM STA 1115 STR 20R. EVALUATED DENT AND FOUND OUT OF LIMITS, REMOVED DAMAGED SKIN DIMS 3.3 INCH BY 1.8 INCH. FABRICATED FILLER 3.3 INCH BY 1.8 INCH, DOUBLER 12.250 INCH BY 8.5 INCH IAW SRM 53-30-3 FIG 24. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 24.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,202 hrs · 29,797 cycles

HORIZONTAL WALKWAY BEAM L/SIDE HAS EVIDENCE OF CORROSION AT APPROX STA 320. REMOVED CORROSION ON TOP OF LT WALKWAY BEAM FROM STA 320 TO STATION 330 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) IAW 727 200 SRM 53-10-4 FIG 7. MECHANICS WROTE ITEM AS BEING A WALKWAY BEAM AND STRUCTURES MECHANICS SIGNED THE REPAIR OFF AS A WALKWAY BEAM. THE BOEING SRM REFERS TO THE ITEM AS A WALKWAY BEAM CORD AND THE BOEING DRAWING 65-18415 PL REFERS TO IT AS A CORD.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,202 hrs · 29,797 cycles

HORIZONTAL WALKWAY BEAM R/SIDE STATION 320 HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON TOP OF RT WALKWAY BEAM FROM STA 328 TO STATION 336 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) REFERENCE 727-200 SRM 53- 10-4 FIG 7.

Part: STRIKER — WORN (AIRSTAIR) · airframe 42,568 hrs · 29,265 cycles

AFT AIRSTAIR LIGHT ILLUMINATED PASSING F220 CLIMBING LEVELED AT F230 PER ATC AND RETURNED TO MEMPHIS, UNEVENTFUL LANDING. RELEASED FOR SERVICE PER MEL/CDL: 52-06-BCATEGORY: C EXPIRATION: 23NOV06. DISCREPANCY HAS BEEN REASSIGNED TO WRI 52-70/9033. DURING INSPECTION OF THE AFT AIRSTAIR SWITCHES, FOUND STRIKER PLATE FOR THE UP POSITION MICROSWITCH WORN. REPLACED WORN PLATE WITH .032" 301 STAINLESS STEEL PLATE SECURED WITH 1559 ADHESIVE M/M 52-70-001-5 STEP 1E.

Part: PRESSURE SWITCH — CORRODED (BOOST PUMP) · airframe 42,331 hrs · 29,076 cycles

IN LEVEL FLIGHT AT 16,000 W/ 6000 NR OF FUEL IN NR 2 TANK THE RT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. NO CB'S WERE OUT. TROUBLESHOT SYSTEM CHECKED WIRING TO PRESSURE SW. WIRING CKS OK. READ PRESSURE SW WITH PUMP ON AND OFF. SW STAYS CLOSED. VERIFIED PUMP RUNNING WHEN SW IN ON POSITION. BACKED OFF B-NUT AT PRESSURE SW. NO PUMP PRESSURE. SUSPECT BAD PUMP IMPELLER. REMOVED AND INSTALLED SERVICEABLE NR 2 TANK AFT RT BOOST PUMP, IAW MM CH NR 28-22-021-4. FOUND CORROSION ON RT AFT PUMP PRESSURE SWITCH, REMOVED AND REPLACED SAME IAW MM, CHAPTER 28-42-001-4 FUNCTIONAL TEST GOOD.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG) · airframe 41,062 hrs · 28,033 cycles

ON GEAR RETRACTION RED GEAR UNSAFE & DOOR LIGHTS ON FRONT PANEL, AND MAIN GEAR DOOR LIGHTS ON S/O PANEL GEAR WAS RECYCLED AND GEAR LIGHTS NOT OUT, WOULD NOT RETRACT. ALL QRH PROCDURES WERE ACCOMPLISHED 7000LBS OF FUEL DUMPED AND AIRCRAFT LANDED AT MEM. JACKED AIRCRAFT AND PERFORMED NORMAL GEAR SWING SEVERAL TIMES IN REFERENCE TO 727-200 AMM 32-32-000-5, GEAR WORKED NORMALLY. AS PRECAUTIONARY REMOVED AND REPLACED LANDING GEAR ACCESORY UNIT IN REFERENCE TO 727-200 AMM 32-09-121-4. PERFORMED LANDING GEAR ELECTRONIC MODULE ADJUSTMENT/TEST IN REFERENCE TO 727-200 AMM 32-09-121-5. ALL TESTS PASSED. AGAIN CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS AND SWINGS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,265 hrs · 27,404 cycles

DOOR EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY IN EMERGENCY EXIT LIGHT PER 727-200 MM 33-50-121-2. OPS CHECK GOOD, AIRCRAFT OK TO CONTINUE.

Part: SWITCH — FAULTY (KRUEGER FLAP) · airframe 40,137 hrs · 27,316 cycles

DURING FLAP RETRACTION NR 3 KRUEGER FLAP FAILED TO RETRACT, RECYCLED WITH NO CHANGE. NO RESTRICTION NR 3 KRUEGER FLAP HAS THE RETRACT SWITCH JUMPER INSTALLED. RAN FLAPS THRU, FWD & AFT INDICATOR LIGHTS CK NORMAL. REPLACED NR 3 KRUEGER FLAP INDICATION SWITCH REF 27-82-001-4. GROUND OPS CK NORMAL AT THIS TIME. JUMPER INSTALLED BACK IN F/E DESK. CLEARS CONTROL NR 182339. A/C OK FOR SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

BS 1150 FRAME GOUGED AT LBL 13 & LBL 15 WL 163 IN RADIUS. REPAIRED FRAME FAIL SAFE BS 1150, LBL 13 & 15, WL 163. ALL IAW SRM 51-40-3.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON FUSELAGE INNER SKIN BETWEEN STR 28L - STR 27L, STA 720D TO 720E. INSTALLED REPAIR IAW SRM 53-30-3 FIG 1.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON OB FLANGE OF S28-R KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON OUTBOARD FLANGE OF S28-L KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

STRINGER CLIP CRACKED AT BS 950C STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950C STRINGER 4 LT IAW SRM 51-30-2 AND 51- 30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950C STRINGER 6RT. ** SD ** COMING

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

STRINGER CLIP CRACKED AT BS 950E STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950E STRINGE 4LH IAW SRM 51-30-2 AND SRM 51-30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950C, STRINGER 5 RT. REPLACED CLIP. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 5RH IAW SRM 51-30-2 & 51-30-5

Part: SKIN — CHAFED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

EXTERNAL SKIN CHAFED BS 720D 13 INCHES, STR 19R ** SD ** COMING

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950C, STRINGER 4 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 4 RT IAW SRM 51-30-2 & 51-30-5

Part: FRAME — DENTED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

STA 680 FRAME IS DENTED BETWEEN STRS 24 - 25R. REPAIRED IAW SRM 51-40-3 AND EA 7-5310-70536

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950D, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950D, STRINGER 6 RT IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON LONGITUDINAL BEAM AT STA 760 TO 850 LBL 29 WL 208. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208, AND INSTALLED NEW LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208. ALL WORK DONE PER SRM 51-30-2

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

STRINGER CLIP CRACKED AT BS 950D STRINGER 9 LT. ** SD ** COMING

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

STRINGER CLIP CRACKED AT BS 950C, STRINGER 9 LT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 9 LT IAW SRM 51-30-2

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950C STRINGER 7 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, 7RH IAW SRM 51-30-2 & 51-30-5

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON LOWER FLANGE OF FLOORBEAM STA 720, WL 201, RBL 18. REMOVED 1 X 1 X .031 CORROSION ON LOWER FLANGE OF FLOORBEAM BS 720, WL 201, RBL 18. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED PER SRM 53-10-1, 53-10-8, 51-30-2, 51-10-2

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STRINGER CLIP AT BS 950B, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950B, STRINGER 6 RT IAW SRM 51-30-2 & 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON BEAM BS 269, LBL 3, WL 208. REMOVED CORROSION IN A 3.0 X 3.0 AREA, .050 MATERIAL LOSS FROM AN ORIGINAL THICKNESS OF .125 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG. 1. REMOVED FE'S SEAT TRACK AT BS 268, REMOVED 4EA FLOOR SUPPORTS AT BS 266-276, LBL 3,RBL 3,RBL 14, AND BS 260-276, LBL 8, WL 208. REMOVED BEAM UPPER CHORD, FABRICATED CHORD FROM P/N 65-17588-66, ALOODINED, PRIMED, RESTORED SURFACE FINISH, INSTALLED REPLACEMENT CHORD AT BS 269, LBL 8-RBL 21, WL 208. REINSTALLED FLOOR SUPPORTS, INSTALLED FASTENERS IN FLOOR WEB REMOVED FOR BEAM REMOVAL, REINSTALLED F.E.'S SEAT TRACK. ALL WORK DONE PER SRM 51-30-2, 51-10-2, 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION GOUGE IN UPPER SURFACE OF FLOOR BEAM B/S 328, LBL 33, WL 208. REPAIRED IAW SRM 53-10-8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

EXTERNAL FUSELAGE SKIN CRACKED BS 685 JUST BELOW STR 26 RT. EXTERNAL FUSELAGE SKIN DAMAGE B.S. 685 BELOW STR 26 RT REPAIRED PER EA 7-5330- 70519.

Part: STIFFENER — CRACKED (BS 171.5) · airframe 39,996 hrs · 27,202 cycles

RT WING FUEL TANK RIB, OB VERTICAL STIFFENER CRACKED, UPPER END, WS 171.5 BETWEEN STR 9 AND STR 10. REMOVED DAMAGED VERTICAL RIB STIFFNER AT WS 171.5 BETWEEN STR 9 & 10 RIGHT. DRILLED UP & INSTALLED NEW STIFFNER (P/N 65-8338-30) IAW SRM 51-30-5, SRM 51-30-2 & SRM 51-40-4.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION AFT CARGO BAY ON STRINGER CLIP BS 1050, RBL 14, WL 163. REMOVED CORROSION FROMS TR CLIP. ORIGINAL THICKNESS .040. AREA REMOVED 1 X 1 X .010 INCH. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR. CLIP AT BS 1050, RBL 14, WL 163. IAW SRM 51-30-2, 51-30-5, 53-10-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. REMOVED CORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. AREA REMOVED 2 X 1 X .022 INCH. ORIGINAL THICKNESS .125 OUT OF LIMITS CUT OUT DAMAGED AREA. 2 X 1 INCH FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PARTS PER SRM 51-10-6, 53-10-1, DRAWING SR 27-53-017A.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON STRINGER AT BS 720F 18, STR 27R. CUT OUT DAMAGED STR B/S 720F 9 FABRICATED AND INSTALLED STR 27R. REPAIRED IAW SRM 53-10-3 FIG 1.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON FUSELAGE INNER SKIN BETWEEN STR S26-R AND S27-R, STA 720E TO 720F, UNDER STRINGER S27-R. REPAIRED IAW EA 7-5330-55027.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION AND DOUBLE HOLE IN FLOORBEAM AT BS 950E.75, BL 0, WL 201. CORROSION AND DOUBLE HOLE IN FLOORBEAM AT BS 950E .75, BL 0, WL 201 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA OF LWR CHORD OF FLOORBEAM BS 950E .75", BL 0, WL 208 AND REPAIRED FLOOR BEAM LWR CHORD B S950E .75", BL 0, WL 208 PER SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION (C53-111-01, 3) ON FLOORBEAM BS 1070, LBL 39-42.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT . REMOVED CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT OF A AREA 2 X 2 X .005 OF ORIGINAL .063 MATERIAL. FOUND IN LIMITS I.A.W. BOEING SRM 53-30-1. WORK DONE IAW BOEING 727 SRM 53-10-1, BOEING 727 SRM 53-30-3, BOEING 727 SRM 51-30-2, BOEING 727 SRM 51-10-6.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

CRACK IN STR CLIP AT BS 950B STR 9 LT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON BS 1070 FLOORBEAM LBL 45 - RBL 50.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,996 hrs · 27,202 cycles

EXTERNAL FUSELAGE SKIN CREASED BS 189 LBL 9-12 LWR HALF.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION BS 950F FLOORBEAM LWR CHORD NUTPLATE HOLES LBL 45 - RBL 45 WL 200. REPAIRED IAW SRM 53-10-8

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION 3) BS 990 FLOORBEAM RBL 23 WL 200.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON FLOOR BEAM B/S 312, LBL 42.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,996 hrs · 27,202 cycles

CORROSION ON LOWER STRUCTURE BS 1010 FLOORBEAM, LBL 43-LBL 2. BLENDED CORROSION DAMAGE ON LOWER STRUCTURE BS 1010 FLOORBEAM LBL 43-LBL 2 PER SRM 51-10-1. DAMAGE AT BS 1010, LBL 4-LBL 14, WL 200 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 AND 53-10-6. ALL OTHER BLEND AREAS WERE FOUND TO BE IN LIMITS PER SRM 53-10- 1. REPAIRED DAMAGE LOWER STRUCTURE BS 1010, LBL 4 - LBL 14, WL 200 PER SRM 53-10-8 FIG 8.

Part: INDICATOR — FAILED (PRESS CONTROL) · airframe 39,937 hrs · 27,148 cycles

ON CLIMBOUT OF TUS, CABIN CONTINUED TO CLIMB TO 2000 27QRH PROCEDURES WERE PERFORMED AND CABIN PRESSURE DID NOT RESPOND.

Part: SWITCH — FAILED (NLG)

AFT T/O GEAR WAS RETRACT NORMAL WHEN HANDLE IN OFF POS. REMOVED AND REPLACED RIGHT AND LEFT NOSE LAND GEAR DOOR SWITCH PER MM 32-33-00-5.

Part: ACCESSORY UNIT — INOP (E & E COMPT)

AFT T/O, GEAR HANDLE WOULD NOT RAISE, GEAR LATCH FAILED TO RELEASE. PINS INSTALL. FOUND LAND ASSY UNIT BAD. REMOVED AND REPLACED UNIT PER MM 32-09-121. PERFORMED FUNC TEST PER MM 32-09-122, ALL CK OK. REMOVED PLACARD AND INSTALLED ALIGN ON SIDE PANEL IN CORRECT PLACE.

Part: DOOR — MISSING (HYD SERVICE)

98-0146, HYDRAULIC SERVICE DOOR MISSING. INSTALLED MISSING DOOR WITH NEW UNIT PER MAINTENANCE MANUAL 52-00-5 PAGE 2, OPERATION GOOD.

Part: ACCESSORY UNIT — FALSE WARNING (E/E COMPT)

LEFT LANDING GEAR INTRANSIT LIGHT STAYS ON. REMOVED AND REPLACED DOWN LOCK PROXIMITY SWITCH IN LEFT WHEEL WELL, NO HELP. REPLACED LEFT UPLOCK SWITCH, NO HELP. REPLACED LANDING GEAR ACCESSORY UNIT. CHECKS GOOD PER B727 MAINTENANCE MANUAL 32-09-122.

Part: LOCK SOLENOID — MALFUNCTIONED (LANDING GEAR)

REPEAT WRITE UP - ON INITIAL RETRACTION, GEAR WOULD NOT COME UP, SEVERAL ATTEMPTS WITH NO SUCCESS. RED TAB CHECKLIST RAN, LANDING GEAR LEVER LATCH FAILED TO RELEASE RESULTING IN LATCH BEING RAISED, AND GEAR RETRACTED. FOUND LANDING GEAR CONTROL LEVER LOCK SOLENOID BAD. REMOVED AND REPLACED LOCK SOLENOID PER MM 32-31-16, CHECKS NORMAL. ALSO, RAN GEAR RETRACTION AND EXTENSION WHILE A/C ON JACKS, OPS GOOD.

Part: LINES — CHAFED (B-HYD SYST)

THE B-SYS LOSS NR 1 PUMP IND LOW PRESS, 20 SEC LATER PRESS ZERO, QTY ZERO. CREW REPORTED B-SYS SHUTOFF BEFORE QTY DROPPED. REMOVED AND REPLACED NR 1 AND NR 2 B-SYS CASE DRAIN FILTERS. NO METAL CONTAMINATION FOUND FLL-1365, FILTERS LEAK CK'D OK. FOUND SUPPLY AND CASE DRAIN LINES AT B-PUMP NR 1 CHAFED AND LEAKING. REMOVED AND REPLACED BOTH LINES, LEAK CK'D AND NO LEAKS FOUND. SERVICED HYD QTY IAW MM 29-12-0.

Part: DECTECTOR — FALSE WARNING (E/E COMPT)

DURING FLT AT FL290 THE NR 2 MAIN CARGO SMOKE INDICATOR ILLUMINATED. COMPLIED WITH ALL APPLICABLE CHECKLIST AND THE LIGHT WENT OUT. FOUND SMOKE DECTECTOR TO BE BAD. REMOVED BAD REPLACED DETECTOR, GROUND OPS CK GOOD.

Part: RETRACT MECH — LACK OF LUBE (NLG)

ON FINAL APPROACH, NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS LOWERED, GEAR WAS RAISED AND WHEN EXTENDED AGAIN, ALL GEAR LOCKED DOWN NORMALLY. INSPECTED NOSE GEAR COMPONENTS NO DAMAGE, FOUND WATER AND ICE IN KNUCKLE, LUBED KNUCKLE, OK FOR SERVICE.