N917DN

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,133 hrs · 19,376 cycles

FAILED OVER WING EMERGENCY LIGHTS. REPLACED BATTERY POWER SUPPLY. TEST OK. (LP# 0876006)

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 37,133 hrs · 19,376 cycles

CRACK ON VERTICAL STABILIZER UPPER WEB AND DOUBLER AROUND JACKSCREW HOLE. VERTICAL STABILIZER UPPER WEB AND DOUBLER AROUND JACKSCREW HOLE WAS REPAIRED PER ETI-90-18-064 R1 AND ER/A 574084-14 SECTION I REV. ORIGINAL. FOLLOWED UNDER LOG PAGE 0872434. ASSOCIATED ER/A 90-574084 ADDED FOR AC 9217. (LP# 0873976)

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 37,133 hrs · 19,376 cycles

CRACK ON CHANNEL (STIFFENER) RH SIDE STA ZV= 72 AT VERTICAL STABILIZER. CHANNEL (STIFFENER) RH SIDE STA ZV= 72 AT VERTICAL STABILIZER WAS REPAIRED PER ETI-90-18-068 REV. 3 AND ER/A 574101-14 REV.ORIG AND WAS ATTENDED WITH NRC 00276 AND LOG PAGE : 0873621. ASSOCIATED ER/A 90-574101 ADDED FOR AC 9217. (LP# 0873925)

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 37,130 hrs · 19,375 cycles

CORROSION ON CO-PILOT AFTER OUTBOARD SEAT TRACK AT COCKPIT. CO-PILOT SEAT TRACK AT COCKPIT (CPIL) WAS REPLACED PER MD90 SRM VOL II 51-30-01. (LP# 0871806)

Part: RETAINER — WORN (AFT CARGO DOOR) · airframe 37,130 hrs · 19,375 cycles

WEAR ON INNER/OUTER PAN AND SEAL RETAINERS AT AFT CARGO COMPARTMENT DOOR LOWER AREA (C3). DAMAGE ON INNER/OUTER PAN WAS REPAIRED PER ER/A 413163-14MA REVISION B AND SEAL RETAINERS LOWER AREA WERE REPLACED PER MD-90 SRM VOL III 52-30-01 FIG 1 AND 51-30-01 VOL II. (LP# 0862064)

Part: PAN — WORN (FWD CARGO DOOR) · airframe 37,130 hrs · 19,375 cycles

WEAR ON INNER/OUTER PAN AND SEAL RETAINERS AT FWD CARGO COMPARTMENT DOOR LOWER AREA. DAMAGED AREAS WERE BLENDED OUT ON INNER/OUTER PAN AT FWD CARGO COMPARTMENT DOOR LOWER AREA PER ERA 413163-14MA REV. B. NO CRACKS WERE FOUND AFTER BLEND OUT PER ER/A 413163-14 MA REV. B STEP 2 & DC-MD/BOEING NDTSPM PART 6, 06-10-01.001 REWORKED AREAS WERE MEASURED AS FOLLOW: FWD EDGE ORIGINAL EDGE MARGIN: 0.400" AND REMAINING EDGE MARGIN:0.300", AFT EDGE ORIGINAL EDGE MARGIN: 0.400" AND REMAINING EDGE MARGIN: 0.290" THEREFORE ARE WITHIN LIMITS PER ERA 413163-14MA REV. B. LOWER AREA WERE REPLACED PER MD-90 SRM 51-30-01 PAR. 6 E (2) VOL II. (LP# 0862074)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,048 hrs · 18,688 cycles

TWO EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY IAW MM 33-50. OP CHECKED GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 35,247 hrs · 18,217 cycles

TWO SOFT SPOTS IN GALLEY FLOOR. FOUND ONE SOFT SPOT AT GALLEY AISLE THRESHOLD, AND ONE SPOT AT R1 GALLEY DOOR THRESHOLD. BOTH EXCEED ALLOWABLE DAMAGE LIMITS, WIP 957193. REMOVED RIGHT FWD GALLEY, REMOVED DAMAGE FLOORBOARDS 221LK, 221KF. 221QF STILL REQ. REPLACEMENT.WIP 359055. FABRICATED NEW FLOOR PANELS 221KF, 221LF IAW SRM 53-20-03. INSTALLED PANELS,

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,276 hrs · 17,619 cycles

LEFT SIDE 1 INCH SKIN CRACK IN EMPENNAGE CANTED STA 1531.604 ABOUT 1 FOOT UP FROM STAIR OPENING. CLEANED AREA AND REMOVED FASTENERS PER SRM 53-00 FOR INSP. VERIFIED CRACK INDICATION PER NDT 06-10-01.001. MARKED ENDS OF CRACK. DRILLED OUT 6 RIVETS TO ALLOW BACKING PLATE FOR STOP DRILL. CUT OUT DAMAGE 1.0 INCH HOLE. HFEC PER SPM 06-10-01.001. DAMAGE CONTAINED. FABRICATED DOUBLER AND FILLER .040 2024 T3. CONTINUED DRILLING UP DOUBLER AND INSTALLED IAW SRM 53-00-01. OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,276 hrs · 17,619 cycles

RIGHT SIDE 3/4 INCH SKIN CRACK IN EMPENNAGE CANTED STA 1531.604 ABOUT 1 FOOT UP FROM STAIR OPENING. CLEANED AREA AND REMOVED FASTENERS PER SRM 53-00 FOR INSP. VERIFIED CRACK INDICATION PER NDT 06-10-01.001. MARKED ENDS OF CRACK. DRILLED OUT 6 RIVETS TO ALLOW BACKING PLATE FOR STOP DRILLING. CUT OUT DAMAGE 1.0 INCH X 2.0 INCH HOLE. DAMAGE CONTAINED. FABRICATED DOUBLER AND FILLER .040 2024 T3. CONTINUED DRILLING UP DOUBLER AND INSTALLED IAW SRM 53-00-01 OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,956 hrs · 17,433 cycles

EXIT SIGN ABOVE AFT STAIRWAY DOOR INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK AND CHARGER BASE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,741 hrs · 17,312 cycles

CATWALK SIDEWALL EMERGENCY LIGHTS INOPERATIVE. INSTALLED A NEW BATTERY IN THE POWER SUPPLY. OPS CHECKED OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,997 hrs · 16,919 cycles

AFT EMERGENCY EXIT SIGN ILLUMINATED. REMOVED AND REPLACED AFT BATTERY PACK CHARGER. OPERATION CHECKS GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 32,913 hrs · 16,873 cycles

LEFT HYDRAULIC TEMP HIGH DURING CRUISE. TURNED ON TRANSFER PUMP PRESSURE WENT TO ZERO. LEFT ENGINE HYDRAULIC PUMP ON. PRESSURE IS ZERO. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN PUMP IAW MM. OPERATIONS CHECKED GOOD.

Part: WEB — CRACKED (BS 1520) · airframe 31,624 hrs · 16,133 cycles

THREE INCH CRACK ON WEB AT BS 1520 RIGHT CANTED FRAME. REMOVED DAMAGED AREA IAW SRM 53-10-03.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 27,501 hrs · 13,685 cycles

L1 DOOR SLIDE PINS PULLED. R & R L1 DOOR SLIDE IAW JIC 2561-4641.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,197 hrs · 13,487 cycles

FORWARD ATTENDANT PANEL EMERGENCY LIGHT SWITCH IS INOPERATIVE. FOUND OVERWING EMERGENCY EXIT POWER SUPPLY BAD. R & R POWER SUPPLY IAW AMM. OPERATION CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,241 hrs · 13,514 cycles

OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: FRAME — CORRODED · airframe 27,190 hrs · 13,480 cycles

AFT ACCESSORY COMPARTMENT, CANTED FRAME AT BASE OF FRAME CORRODED ON FORWARD SIDE OF FRAME, L24L. TASK 53-131-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION AND REPAIR SPLICES IAW SRM 53-10-02, FIG 11. LP 1852770.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 27,190 hrs · 13,480 cycles

AFT CARGO, SLANT PANEL SUPPORT, CORRODED AROUND SEVERAL FASTENER HOLES, STA 1245-1307, ABOVE L27L. TASK 53-302-07. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-40-01, FIG 7 AND 51-10-05. LP 1850686.

Part: SUPPORT — CORRODED (BS 1058-1148) · airframe 27,190 hrs · 13,480 cycles

AFT CARGO, LT SIDE SLANT PANEL SUPPORT, CORRODED, STA 1058-1148, ABOVE L27L. TASK 53-302-07. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R DAMAGED SECTION IAW SRM 53-40-01, RIG 7. LP 1851631.

Part: CUSP WEB — CORRODED (BS 1079-1098) · airframe 27,190 hrs · 13,480 cycles

MAIN CABIN LEFT CUSP WEB CORRODED BS 1079-1098, LBL 60, TASK 53-211-02. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 1.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 27,190 hrs · 13,480 cycles

RIGHT MAIN CABIN CUSP WEB CORRODED, STA 1231-1250, RBL 60, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED CUSP WEB IAW SRM 51-30-02, 51-30-05 AND DWG 9930612, REV BU.

Part: SEAT TRACK — CORRODED (BS 200-323) · airframe 27,190 hrs · 13,480 cycles

CORROSION ON SEAT TRACK FROM FS 200 TO FS 323, LBL 22. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, 51-10-03 AND 51-10-00.

Part: SEAT TRACK — CORRODED (BS 200-342) · airframe 27,190 hrs · 13,480 cycles

CORROSION ON SEAT TRACK FROM FS 200 TO FS 342, LBL 44. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-03, 51-10-00, AND 53-40-02, FIG 6.

Part: SEAT TRACK — DAMAGED (BS 855-1089) · airframe 27,190 hrs · 13,480 cycles

CABIN SEAT TRACK, LBL 58, BS 855-1089, SCRATCHED, WEAR MARKS AND BARE METAL. BLENDED OUT DAMAGE. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-30-01 AND DWG S00482, REV A.

Part: WEB — CORRODED (BS 730-750) · airframe 27,190 hrs · 13,480 cycles

RT MAIN CABIN WEB BS 730-750, RBL 60 CORRODED, TASK 52-211-02. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-01, 51-30-05, 53-20-02, 53-42-01, AND DWG 9940443, REV A.

Part: CUSP WEB — CORRODED (BS 1230-1250) · airframe 27,190 hrs · 13,480 cycles

LEFT MAIN CABIN CUSP WEB BS 1230-1250 CORRODED, LBL 60. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 2.

Part: SKIN — CORRODED (BS 693-712) · airframe 27,190 hrs · 13,480 cycles

LOWER EXTERIOR ANTENNA CUT-OUT, STA 693-712, L30-L29, CORRODED. TASK 53-100-02. R & R ANTENNA DOUBLER IAW DWG 5936004, REV AN, SRM 51-30-02 AND 51-30-05.

Part: SKIN — CORRODED (BS 731-750) · airframe 27,190 hrs · 13,480 cycles

CORROSION AROUND ANTENNA BASE CUTOUT LOWER EXTERIOR FUSELAGE, STA 731-750, L30-29L. TASK 53-100-02. R & R ANTENNA DOUBLER IAW SRM 51-30-02, 51-30-05 AND DWG 5936004, REV AN. FOUND TO BE OUT OF LIMITS.

Part: CUSP WEB — CORRODED (BS 598-617) · airframe 27,190 hrs · 13,480 cycles

RT CABIN CUSP WEB BS 598-617, RBL60 CORRODED. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-05 AND DWG 9940443, REV A.

Part: SEAT TRACK — CORRODED (BS 200-237) · airframe 27,190 hrs · 13,480 cycles

CABIN SEAT TRACK, RBL 44 CORRODED, BS200-237 SEVERAL AREAS. TASK 53-211-02. R & R SECTION OF SEAT TRACK IAW SR 09530085, REV D AND SRM 53-20-01.

Part: CUSP WEB — CORRODED (BS 904-984) · airframe 27,190 hrs · 13,480 cycles

MAIN CABIN LT CUSP WEB CORRODED, BS 904-984, LBL 50. TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-03, FIG 7 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 1136-1153) · airframe 27,190 hrs · 13,480 cycles

RIGHT MAIN CABIN CUSP WEB CORRODED BS 1136-1153, RBL 60. TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 53-20-02, 51-10-03 AND 53-40-02, FIG 26.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 27,190 hrs · 13,480 cycles

L1 DOOR SLIDE PIN IS NOT ENGAGED AT LOWER LOCATION. R & R L1 DOOR SLIDE IAW AMDS 2561-4641.

Part: SUPPORT FITTING — GOUGED (LT MLG ACTUATOR) · airframe 27,190 hrs · 13,480 cycles

LEFT MLG ACTUATOR RETRACT SUPPORT FITTING BEARING BORE IS GOUGED. MACHINED BORE TO 1.533. WITHIN LIMITS IAW DWG SR09570087. ACCOMPLISHED FPI OF LMLG ACTUATOR RETRACT SUPPORT FITTING BEARING BORE IAW PS 900-6-3 NR 2.

Part: SUPPORT FITTING — GOUGED (RT MLG ACTUATOR) · airframe 27,190 hrs · 13,480 cycles

RIGHT MLG ACTUATOR RETRACT SUPPORT FITTING BUSHING BORE IS GOUGED. MACHINED BORE TO 2.2835. WITHIN LIMITS IAW DWG SR09570087. ACCOMPLISHED FPI OF RMLG ACTUATOR RETRACT SUPPORT FITTING BUSHING BORE IAW PS 900-6-3, NR 2.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 27,190 hrs · 13,480 cycles

AFT CARGO DOOR INBD SKIN GOUGED NEAR AFT LATCH. FOUND PUNCTURE IN RADIUS AND GOUGE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-02.

Part: SEAT TRACK — CORRODED (BS 521-569) · airframe 27,190 hrs · 13,480 cycles

CABIN SEAT TRACK, RBL 58 CORRODED, SCRATCHED AND BARE METAL SEVERAL AREAS. BS 21-569, TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: STRAP — CORRODED (BS 693-750) · airframe 27,190 hrs · 13,480 cycles

MID CARGO REPAIR SPACER STRAP HAS CORROSION, BS 693-750. R & R REPAIR SPACER STRAP IAW SRM 53-60-02, FIG 9.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,190 hrs · 13,480 cycles

CORROSION IN FORWARD LAVATORY FITTING AND CHANNEL ON FLOOR AFT CENTER OF FLOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIRED PART IAW SRM 51-20-00 AND 51-30-02.

Part: DOOR FRAME — CORRODED (FWD CARGO BAY) · airframe 27,190 hrs · 13,480 cycles

FORWARD CARGO DOOR LOWER FORWARD FRAME CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-02 AND 51-30-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,778 hrs · 13,208 cycles

AFT AIRSTAIR SIDEWALL EMERGENCY LIGHTING INOPERATIVE. R & R EMERGENCY POWER SUPPLY. OPS CHECKED OK.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,333 hrs · 11,691 cycles

DURING SERVICE CHECK, FOUND TAIL COMPARTMENT WALK WAY EMERGENCY LIGHT INOPERATIVE. R & R QUICK DISCONNECTS AT LIGHT ASSEMBLY IAW SWPM. OPS CHECKS GOOD.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 24,259 hrs · 11,649 cycles

MAIN CABIN ENTRY DOOR SKIN DAMAGED TEN INCHES AFT OF FORWARD EDGE TOP OF DOOR. STRAIGHTENED DAMAGED AREA AND BURNISHED IAW SRM 52-01-01 HFEC. NO CRACKS NOTED. ALODINED, PRIMED AND PAINTED. OK FOR SERVICE.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 24,259 hrs · 11,649 cycles

MAIN CABIN DOOR SKIN DAMAGED LOWER AFT CORNER. STRAIGHTENED DAMAGED AREA AND BURNISHED IAW HFEC. NO CRACKS NOTED. ALODINED, PRIMER AND PAINTED. OK FOR SERVICE.

Part: SKIN — CRACKED (BS 1475) · airframe 24,096 hrs · 11,542 cycles

FUSELAGE SKIN CRACKED JUST OUTBOARD OF VERTICAL STABILIZER SKATE ANGLE AT BS 1475 LEFT SIDE. REPAIRED IAW ERA 520731-14 REV O.

Part: SKIN — CRACKED (BS 1475) · airframe 24,096 hrs · 11,542 cycles

FUSELAGE SKIN CRACKED JUST OUTBOARD OF STABILIZER SKATE ANGLE AT BS 1475. REPAIRED IAW ERA 520732-14, REV O.

Part: FRAME — CRACKED (BS 1520) · airframe 24,096 hrs · 11,542 cycles

CANTED FRAME WEB CRACKED, BS 1520. REPAIRED IAW ERA 520724-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1549) · airframe 24,089 hrs · 11,538 cycles

BS 1549 FRAME CRACKED. REPAIRED IAW SRM 53-10-03.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 24,089 hrs · 11,538 cycles

VERTICAL STABILIZER, L/E FRONT SPAR CAP FOUND DAMAGED. REPAIRED IAW AA 5530-01044.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 24,089 hrs · 11,538 cycles

HORIZONTAL STAB UPPER CENTER SKIN PANEL FOUND DAMAGED. REPAIRED IAW AA 5510-01085.

Part: PIN — OUT OF POSITION (L1 DOOR SLIDE) · airframe 22,936 hrs · 10,886 cycles

DURING ROUTINE INSPECTION, L1 DOOR SLIDE PINS WERE FOUND OUT OF POSITION. THE SLIDE WAS REPLACED IAW TC 2500-4332.

Part: SUPPORT CHANNEL — CRACKED (TAIL CONE) · airframe 21,519 hrs · 10,112 cycles

WHILE PERFORMING TAIL CONE FUNCTIONAL CHECK, FOUND TAIL CONE CABLE SUPPORT CHANNEL CRACKED. REMOVED CHANNEL, FABRICATED, ALODINED, PRIMED AND INSTALLED IAW SRM.

Part: CABLE — FRAYED (TAIL CONE) · airframe 21,519 hrs · 10,112 cycles

DURING TAILCONE FUNCTIONAL CHECK, FOUND TAILCONE JETTISON BOTTLE ACTIVATION CABLE FRAYED. R & R WORN CABLE WITH NEW CABLE. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,008 hrs · 9,813 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY EXIT LIGHT AFT FACE OF ATTENDANT O2 BOX (L2-790) INOPERATIVE. REMOVED AND REPLACED AND OPERATION CHECK BATTERY PACK PER MM. CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,338 hrs · 9,402 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT AIR STAIR EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY B5-237 AND BATTERY PER AMM. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,109 hrs · 9,277 cycles

FLIGHT CREW FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE, REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK AND RELAY R2-273 PER AMM. OPERATION CHECKED NORMAL.

Part: CONTACT — DIRTY (BATTERY PACK) · airframe 20,094 hrs · 9,272 cycles

DURING TAKEOFF, AFT EMERGENCY EXIT SIGN, ABOVE AFT FLIGHT ATTENDANT JUMPSEAT, CAME ON AND STAYED ON FOR A FEW MINUTES, THEN WENT OFF. MAINTENANCE REMOVED EMERGENCY LIGHT BATTERY PACK B5-237, CLEANED CONNECTOR AND REINSTALLED BATTERY PACK PER AMM. OPERATION CHECKED GOOD.

Part: STRUCTURE — DENTED (FWD CARGO DOOR) · airframe 19,882 hrs · 9,161 cycles

ON ARRIVAL FOUND DAMAGE TO FORWARD CARGO DOOR FORWARD EDGE 12 1/2 INCHES FROM BOTTOM OF DOOR, 2 INCHES HIGH, 1 1/4 INCHES WIDE AND .14 INCHES DEEP. MAINTENANCE REPAIRED FLANGE PER SRM 52-01-01 PAGE 23, PARAGRAPH G. NO CRACKS NOTE AIRCRAFT OKAY FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,569 hrs · 8,982 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. RELAMPED. OPS CHECKED NORMAL. AIRCRAFT OKAY FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,880 hrs · 8,667 cycles

CREW REPORTS EXIT SIGN ABOVE AFT CABIN DOOR STILL BLINKS ON AND OFF IN FLIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,880 hrs · 8,667 cycles

CREW REPORTS TAIL LIGHT ABOVE EXIT, FLASHES DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED. OPERATION TESTS GOOD.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 18,880 hrs · 8,667 cycles

FLIGHT CREW REPORTS THAT TAIL EMERGENCY EXIT LIGHT FLASHES IN THE AIR, ON THE GROUND LIGHT ILLUMINATES NORMAL. MAINTENANCE REPLACED THE AFT EMERGENCY EXIT LIGHT POWER PACK PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: ATTACH FITTING — CRACKED (VERT TO FUSE) · airframe 18,845 hrs · 8,645 cycles

VERTICAL STABILIZER ATTACH ANGLES BS 1520 CRACKED. REPAIRED IAW ERA 497544-14.

Part: LUG — DAMAGED (HORIZONTAL STAB) · airframe 18,845 hrs · 8,645 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG WAS DAMAGED. REPAIRED IAW AA 5510-01083.

Part: RELEASE MECH — OUT OF RIG (TAIL CONE) · airframe 18,277 hrs · 8,381 cycles

EMERGENCY EVACUATION SYSTEM FAILED WHEN MAINTENANCE TESTED THE TAIL CONE RELEASE MECHANISM. AFTER RE-RIGGING THE SYSTEM AND LUBRICATING THE LATCHES CONE RELEASED FUNCTIONED NORMALLY.

Part: DOOR — DAMAGED (ENTRY DOOR) · airframe 18,218 hrs · 8,351 cycles

AT GATE JETWAY MOVED UP WITH FORCE CAUSING DOOR DAMAGE, GUST LOCK DAMAGED. REPAIRED DAMAGE PER ERA495116-14 REV ORIG. REMOVED AND INSTALLED SLIDE PER AMM 25-61-01, REQUIRED INSPECTION COMPLETED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,472 hrs · 7,999 cycles

DURING LINE CHECK MAINTENANCE FOUND THE EMERGENCY LIGHTS IN CENTER CABIN WON'T TEST. MAINTENANCE REPLACED BATTERY PACK AND LIGHT BULBS. OPERATION OF LIGHTS NOW CHECK OK.

Part: BALLAST — BURNED (CABIN) · airframe 17,267 hrs · 7,907 cycles

INBOUND CREW REPORTS SMOKE IN THE CABIN AT THE GATE. FOUND BALLAST INOPERATIVE AND BURNT AT SEAT ROW 11CDE. DEACTIVATED BALLAST AND SIDEWALL LIGHTS AND FORWARDED TO MEL. REMOVED AND REPLACED BALLAST PER AMM 33-20-07 PB401. SIDEWALL LIGHT OPERATIONALLY CHECKS NORMAL.

Part: COFFEEMAKER — ODOR (1ST CLASS GALLEY) · airframe 16,917 hrs · 7,753 cycles

F/A REPORTED ELECTRICAL ODOR IN FIRST CLASS GALLEY. FLIGHT CREW PERFORMED QRH, PULLED THE GALLEY POWER SWITCH OFF, AND THE ODOR DISSIPATED. MX OPERATED FWD GALLEY OVEN AND COFFEEMAKERS BUT NO SMOKE OR ODOR WAS NOTED. SOME SPILLED/BURNED COFFEE WAS FOUND ON THE COFFEEMAKER HOT PLATE AND THAT RESIDUE WAS CLEANED UP. ACFT OK FOR SERVICE.

Part: WATER SEPARATOR — FROZEN (LT PACK) · airframe 16,429 hrs · 7,566 cycles

ON FINAL APPROACH THE CABIN CREW REPORTED THAT THE CABIN WAS FILLING WITH SMOKE AND PASSENGERS WERE COMPLAINING OF THE SMELL. LAVATORY SMOKE DETECTORS DID NOT GO OFF. NO EMERGENCY WAS DECLARED AND THE ACFT ARRIVED AT THE GATE WITH NORMAL OPERATIONS AND NO SMOKE PRESENT IN CABIN. MX FOUND LT WATER SEPARATOR SOCK FROZEN SOLID. ALSO, FOUND LT 35 DEGREE VALVE NOT OPENING. VALVE WAS DEFERRED. R & R BOTH SOCKS IAW MM. RAN BOTH ENGINES AT POWER AND VERIFIED NO SMOKE OR ODOR FROM PACKS. LEAK CHECK GOOD.

Part: JACKSCREW — DAMAGED (HORIZONTAL STAB) · airframe 14,856 hrs · 6,922 cycles

HORIZONTAL STABILIZER JACKSCREW ASSY DAMAGED. REPAIRED IAW AA 2740-01071.

Part: FRAME — DAMAGED (BS 883 - 962) · airframe 14,856 hrs · 6,922 cycles

BS 883-962 OVERWING FRAME WAS DAMAGED. REPAIRED IAW AA 5310-01375.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 14,856 hrs · 6,922 cycles

CARGO DOOR STOP PAD FITTINGS DAMAGED. REPAIRED IAW AA 5230-01136.