N907DE

Part: WINDSHIELD WIPER — DETACHED · airframe 69,762 hrs · 51,337 cycles

CAPTAIN'S WINDSHIELD WIPER IS MISSING. FELL OFF ON SHORT FINAL. REPLACED THE WINDSHIELD WIPER ARM AND BLADE IAW AMM 30-42, OPS CKECKED GOOD.

Part: LANDING LIGHT — MISSING · airframe 69,248 hrs · 50,852 cycles

ON WALK AROUND, NOSE GEAR LANDING LIGHT ON F/O SIDE MISSING, WIRES HANGING OUT. FOUND RT TAXI LIGHT BULB AND RETAINING RING MISSING. INSTALLED NEW BULB REF MD88 AMM 33-41. SECURED BULB PER MEL 33-00-07C. C/B L-14 PULLED AND COLLARED PER RI 580440-14. NEW BULB INST AND SPEED TAPE IN PLACE. NDS STK NBR 88-3300-3-0121. NIS/CHS. "M"PROC C/W. INSTALLED RETAINING RING CKD NML MCO/PLAC RMVD. (LP6121808)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,241 hrs · 50,845 cycles

O/H EMERGENCY LIGHTS INOPERATIVE FROM ROW 16-29. REPLACED BATTERY PACKS B5-104 AND B5-102. OPS CHECKED GOOD IAW AMM 33-53.

Part: TERMINAL — SHORTED (WINDOW) · airframe 69,201 hrs · 50,816 cycles

TAXING INTO RAMP, BIG SPARK OUT OF CAPT WINDSHIELD ANTI-ICE CONNECTOR. FOUND WIRE TERMINAL IN CONTACT WITH SPRING ON WINDOW TEMP SENSOR. ADJUSTED WIRE TERMINAL FOR CLEARANCE. CKS OK. (LP5490390)

Part: SKIN — DAMAGED (BS 180) · airframe 68,934 hrs · 50,584 cycles

FUSELAGE SKIN DAMAGE AT BS 180. REPAIRED THE SKIN IAW SRM 53-04-3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,468 hrs · 50,165 cycles

BOTH FWD OVERWING EXIT DOOR EMERGENCY LTS INOP. R/R BATTERIES FOR FWD OVERWING DOOR LTS. OPS CHECK OK. BATTERIES R/R PER AMM 33-53.

Part: STRUCTURE — MISSING (RUDDER) · airframe 68,101 hrs · 49,849 cycles

DURING PAINT VISIT, FOUND RUDDER TO HAVE MISSING FLAME SPRAY. RUDDER P/N SN5955501-1 S/N 403. REMOVED AND REPLACE RUDDER WITH SERVICEABLE REDDER PER WORK CARD 2720-4421. RUDDER, ASSEMBL OFF 88-5554-9-0005 00403 ON 88-5554-9-0005 49321. (LP0941022)

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 67,930 hrs · 49,706 cycles

BOTH AUTO PRESSURIZATION SYSTEMS FAILED DURING DESCENT AT APPROXIMATELY 22000 FEET RESULTING IN CABIN PRESSURE LOSS. REMOVED AND REPLACED A/C MOTOR DRIVE ASSY, NR 1 & NR 2 PRESSURE CONTROLLERS AND ADJUSTED AFT OUTFLOW VALVE PER AMM 21-32 AND TSM 21-32. PERFORMED NO GO ODI CHECKLIST 2120, 2130 AND 2150. ALL OPERATIONS NOW NORMAL(LP5057728)

Part: UNKNOWN — HAZE (CABIN) · airframe 67,532 hrs · 49,371 cycles

RIGHT AFTER GEAR RETRACTION BOTH AFT LABS SMOKE ALARMS STARTED BEEPING. NO SMOKES, LIGHT HAZE AND BURNING SMELL-LIGHT TO MEDIUM. WE COULD SMELL IN THE COCKPIT. AFTER 2 MINUTES THE ALARMS STOPPED & SMELL ,HAZE DISSIPATED. AT LANDING AFTER STARTING APE SMELL CAME BACK. ACCOMPLISHED ODI-PREVENTION PROCEDURE 2172 SMOKE-FUME UNKNOWN. RADIO RACK FANS, RECIRC FAN, PACK COOLING FANSOPS CHK OK. L&R ENGINE BLEED DUCTS, PACK PNUE INLET & OUTLET, CROSSBREED DUCKS FOUND TO HAVE NO CONTAMINATION. PACK BURN-CLEAN, SOCK CHANGE ACCOMPLISHED PER 7100-2619; 2120-2367. OK FOR SERVICE. (LP4789130)

Part: CHANNEL — DAMAGED (LT SPOILER) · airframe 67,525 hrs · 49,367 cycles

AIRCRAFT DAMAGE: LT IB FLIGHT SPOILER HAT CHANNEL DAMAGED FROM SPOILER TORSION BAR REACTION BOLT. REPAIRED PER PRI 572530-14 REV O MATCHES ERA 572530-14 REV O. (LP0799992)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,525 hrs · 49,367 cycles

EVIDENCE OF CORROSION FOUND ON REPAIR EDGE AT AFT LAVATORY SERVICE PANEL- MARKED. SKIN/REPAIR BULGING OUT AT LOWER END OF CUTOUT. REPAIRED PER PRI 485410-14 REV A REV 0-3 MATCH ERA 485410-14 REV A. (LP0800060)

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,525 hrs · 49,367 cycles

STA 886 RT MAIN FRAME FOUND TO BE CRACKED THROUGH HFEC INSPECTION PERFORMED ON ROUTINE CARD 5310-01415-04D. REPLACED MAIN FRAME AT STA 886 RT PER 5310-01415-0302.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,161 hrs · 49,040 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM SEATS 17 - 26 WERE INOPERATIVE. R & R THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 66,796 hrs · 48,728 cycles

LAVATORY (AFT RT) SMOKE DETECTOR WILL NOT SHUT OFF. R&R AFT RT LAV SMOKE DETECTOR AND BATT, CKS OK. REF AMM 26- 7.

Part: WIRE — BROKEN · airframe 65,537 hrs · 47,749 cycles

EMERGENCY NAV INSTRUMENT CIRCUIT BREAKER TRIPPED. NO RESET. FOUND A WIRE 1F700A24 BROKEN AND ARCING. REPAIRED THE WIRE IAW MM 20. OPS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 64,496 hrs · 46,885 cycles

MIDDLE EMERGENCY LIGHT ON CATWALK INOPERATIVE. TERMINATED A BROKEN WIRE ON CATWALK EMERGENCY LIGHT IAW SWPM 20 AND EWIS. OPS CHECKED GOOD.

Part: FIREWALL — WORN (NR 2 NACEL;LE) · airframe 64,388 hrs · 46,801 cycles

NR 2 ENGINE FIREWALL PASS THRU WORN AT PREVIOUS REPAIR LOCATED AT HYD PRESS LINE. SAME AREA HYD PRESS LINE LOOSE. FOUND DOUBLER AT PASS THRU FOR HYD LINES WORN. REMOVED OLD DOUBLER AND BAD HYD LINE. INSTALLED NEW DOUBLER IAW ERA 553921-14 REV ORIG. REINSTALLED HYD LINES IAW AMM 29-10. LEAK CHECED GOOD.

Part: SWITCH — FAILED (TAILCONE RELEASE) · airframe 63,862 hrs · 46,412 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM USING AFT PASSENGER ENTRANCE DOOR EMERGENCY HANDLE, AFTER TAILCONE RELEASED FROM ACFT A TAILCONE UNSAFE MESSAGE ON EOAP PANEL IN FLIGHT COMPARTMENT FAILED TO COME ON. REPLACED THE SWITCH S1-538 IAW WDM 52-73-11. OPS GOOD. OK FOR SERVICE.

Part: LINE — NO TEST (EXTINGUISHER) · airframe 63,379 hrs · 46,077 cycles

FOUND THREE FIRE EXTINGUISHER SUPPLY FLEX LINES BAD DURING A EXTINGUISHING LINE LEAK TEST IAW AMM 26-20-01-201. REPLACED THE LINES. (LP9119701)

Part: INDICATOR — MALFUNCTIONED (MLG) · airframe 62,811 hrs · 45,653 cycles

NOSE GEAR LIGHT WOULD NOT ILLUMINATE WITH GEAR LEVER DOWN. NLG INDICATOR PIN EXTENDED. LIGHT TESTED OK. NLG LIGHT ILLUMINATED GREEN AFTER APPROX. 3 MINUTES FLYING AT 180KIAS. REPLACED WARN LIGHT DIM AND TEST UNIT 2 RELAY B5-75 IAW WDM 32-61-00.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,500 hrs · 45,401 cycles

CRACK ON LOWER PAN AFT EDGE BTW BEAM 1 AND 2 STA Y= 693 AT MID CARGO DOOR. MID CARGO DOOR WAS REPAIRED PER ER/A 550293-14 REV ORG.

Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 62,500 hrs · 45,401 cycles

DELAMINATED LOWER SKIN ON MID VANE GUIDE OF OUTBD FLAP NEXT TO INBD EDGE, AT RT WING. SERVICEABLE MID VANE GUIDE OUTBD FLAP RT WAS REPLACED PER AMM 27-51-03.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 62,492 hrs · 45,396 cycles

CP DELAMINATED OUBT GUIDE VANE OUBT FLAP LOWER SKIN INB SECTION AND CLOSE TO LEADING EDGE AT LEFT WING. COMPOSITES. LW. GUIDE VANE REMOVED P/N 5910043-509 S/N DL10 AND GUIDE VANE INSTALLED P/N 5910043-509 S/N 268364. (LP2702347)

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON LT MLG RETRACT ACTUATOR SUPPORT FITTING BEARING BORE IN REF AD 5740-01139-04A. REPAIR WAS PERFORMED IAW ER/A 550286-14AD, REV ORIGINAL PERMANENT REPAIR.

Part: SKIN — PUNCTURED (TE FLAP VANE) · airframe 62,492 hrs · 45,396 cycles

PUNCTURED LOWER SKIN ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING. DUE TO EXCESSIVE DAMAGE ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING WAS REPLACED IAW IPC 27-50-04-01A.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: DELAMINATED LT CONTROL TAB. ELEVATOR CONTROL TAB LT WAS REPLACED IAW AMM 27-30-03-201.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACK OF 0.5" ON STR 17LT XCW=12 AT LT CENTER TANK. STRINGER 17LT WAS REPAIRED IAW ER/A 549299-14, REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM THE FORM 8100-9 APPROVAL DATE: 16/SEP/16.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,492 hrs · 45,396 cycles

AWR HIDDEN DISCREPANCY: CRACKED UPPER PAN STA Y=674 AT MID CARGO DOOR. CRACKED UPPER PAN STA Y=674 AT MID CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACK ON INTERCOSTAL AND ANGLE OF MID CARGO DOOR ON STA PROJECTION Y = 674 BETWEEN BEAM NR 5 AND UPPER EDGE. INTERCOSTAL AND ANGLE OF MID CARGO DOOR ON STA PROJECTION Y = 674 BETWEEN BEAM NR 5 AND UPPER EDGE WERE REPALCED IAW SRM:51-30-1, 51-30-2, 51-30-5 AND DWG: 9957664, REV: N.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

AWR CORROSION ON FLOOR PANEL NR 541E. FLOOR PANEL NR:541E WAS MANUFACTURED BY EXCESSIVE CORROSION IAW AMM 53-20-01-201.

Part: SKIN — WORN (TE FLAP VANE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: WEAR ON OTBD EDGE UPPER SKIN OF OUTBD VANE GUIDE ON INBD FLAP AT RT WING. RT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007, CARD 2000-8149-02 AND SRM 57-03D, PARA 11, FIG 11.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACK ON STR STA Y= 1463 BETWEEN 10 AND 11 O`CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. STR AT STA Y= 1463 BETWEEN 10 AND 11 CLOCK POSITION WAS REPLACED IAW SRM 51-30-5 AND DWG 9911839, REV DP.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACKED AND ELONGATED AND HOLES ON SCUFF PLATE, PN 5936070-29 AT MID CARGO. SCUFF PLATE WAS REPAIRED IAW ER/A 491023-14MA, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACK ON FRAME STA Y=1510 BETWEEN 10 AND 11 O`CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1510 WAS REPLACED IAW SRM 51-30-2.

Part: SKIN — CRACKED (RUDDER) · airframe 62,492 hrs · 45,396 cycles

CRACK ON LT RUDDER SKIN AT STA ZR=16 53" TO T/E. DAMAGE ON RUDDER SKIN AT STA ZR=16.53" TO T/E WAS REPAIRED BY SRM 51-70- 1AD, PARA 13 AND JIC CARD 2000-8149-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT SEAT TRACK FIRST OFFICIAL STA Y 120 TO Y 140 X- 28 AT, CP. RT SEAT TRACK FIRST OFFICIAL STA, Y 120 TO Y 140 X-28 AT WAS REPLACED IAW SRM 51-30-1 AND DWG 9957871, REV V.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CM WORN UPPER PREVIOUS DOUBLER REPAIR ON OUTBD GUIDE VANE INBD FLAP OUTBD SECTION AT LT WING. LT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007 CARD 2000-8149-01, JOB 000-0014 AND SRM 57-03D, PARA 11, FIGURE 11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,721 hrs · 45,586 cycles

CORROSION ON CEILING SUPPORT ON STA Y= 1231 BTW X=17 LT TO X= 34 LT, STA Y= 1309 BTW X=35 LT TO 35 RT, BTW STA Y= 1231 TO 1309 X= 17 LT, BTW STA Y=1250 TO 1309 X=0 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED PER SRM 51-10-3 PAR 26 AND SUPPORTS WERE REPLACED PER SRM 53-24-0D FIG 11. MEASURE UT WAS ACCOMPLISHED PER NDTSPM 04-00-07 PAR 5, FIG 3 SHEET 1 AND 2. ORIGINAL THICKNESS ON STA Y= 1231 BTW X=17 LT TO X= 34 LT IS 0.040" AND REMAINING IS 0.038". ORIGINAL THICKNESS ON STA Y= 1309 BTW X=35 LT TO X=-25 RT IS .040" AND REMAINING IS .039", ORIGINAL THICKNESS ON STA Y= 1231 TO 1250 X=17LH .032" AND REMAINING IS .030" AND ORIGINAL THICKNESS ON STA Y=1250 TO 1309 X=0 ORIGINAL THICKNESS IS .063" AND REMAINING IS .062" THEREFORE IS WITHIN LIMITS, AREAS OUT OF LIMITS ON STA Y= 1309 BTW X=-25 X=-35 ORIGINAL THICKNESS IS .040" AND REMAINING IS .020", Y=1250 TO Y=1309 ORIGINAL THICKNESS IS .032" AND REMAINING IS .018" THEREFORE ITS OUT LIMITS PER ER/A 511165-14MA REV C AND SRM 53-01 FIG 1 SHEET 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKS 3 EAS ON FRAME STA Y= 1510 LOWER. RT SIDE AT AFT ACCESSORY COMPARTMENT CAT FRAME WAS REPLACED IAW SRM 51-30-2 AND DWG 9911843, REV AC.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON INTERCOSTAL BETWEEN LONGERON 28 LT TO 27 LT AND STA Y= 769 TO Y= 788 AT MID CARGO. INTERCOSTAL WAS REPLACED IAW SRM 51-30-5 AND DWG 9915554, REV J.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,492 hrs · 45,396 cycles

AWR HIDDEN DISCREPANCY: CRACKED PAN JUST ON SEATING AREA OF STOP FITTING PROJECTION BEAM 4, FWD SIDE, AT FWD CARGO DOOR. CRACK ON PAN JUST ON SEATING AREA OF STOP FITTING PROJECTION BEAM 4, FWD SIDE, WAS REPAIRED IAW SRM 52-05-D, FIG 50.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 62,492 hrs · 45,396 cycles

WEAR ON FWD AND AFT PRODUCTION DOUBLERS AT FWD CARGO COMPARTMENT DOOR SKIN LOWER SECTION. DOUBLERS WERE REPLACED IAW SRM 51-30-2 AND ERA 486624-14, MA REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (BS 1322-1338) · airframe 62,492 hrs · 45,396 cycles

CRACKED CANTED INTERCOSTAL BETWEEN BS 1322 - 1338, X 0, Z 0 TO Z -5, IN AFT CARGO COMPARTMENT. INTERCOSTAL REPAIRED IAW SRM 53-01 FIG 2.

Part: SKIN — WORN (PAX DOOR) · airframe 62,492 hrs · 45,396 cycles

WEAR ON MAIN ENTRANCE DOOR SKIN LWR EDGE BTW BS 170 AND 180. DAMAGE ON MAIN ENTRACE DOOR LOWER SKIN WAS REPAIRED IAW SRM 52-05 D FIG 37.

Part: CARGO TRACK — CORRODED (BS 1022-1155) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RIGHT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 1022 AND 1155 IN AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5 AND DWG:5936660 REV BZ.

Part: ANGLE — CORRODED (BULKHEAD) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON AFT PRESSURE BULKHEAD ANGLE BETWEEN LONGERONS 28L TO 28R IN AFT CARGO BAY. ANGLE WAS REPLACED IAW SRM 51-30-02,51-30-05 AND DWG 9915561 REV CG.

Part: INTERCOSTAL — CRACKED (BS 1322-1338) · airframe 62,492 hrs · 45,396 cycles

CRACKED CANTED INTERCOSTAL BETWEEN BS 1322 - 1338 X 0, Z 0 TO Z -5, AT AFT CARGO COMPARTMENT. INTERCOSTAL REPAIRED IAW SRM 53-01 FIG 2.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION AND ELONGATED HOLES ON RIGHT CARGO TRACK DOWN FROM BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, 51-30-1 AND DWG 5936660 REV BZ.

Part: CARGO TRACK — CORRODED (BS 1222-1322) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON LEFT CARGO TRACK DOWN FROM BS 1222 TO 1322 IN AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 5936660 REV BZ.

Part: CARGO TRACK — CORRODED (BS 1022-1221) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON LEFT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 1022 AND 1221. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 ,51-30-2 AND DWG 5936660 REV:BZ.

Part: SKIN — DAMAGED (BS 636) · airframe 62,492 hrs · 45,396 cycles

FUSELAGE SKIN FWD OF C2 DOOR BS 636, DAMAGE WAS BLENDED OUT AND EVALUATED. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3 PARAGRAPH 14 AND 21.

Part: DOUBLER — CORRODED (BS 1287-1330) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON PRODUCTION DOUBLER FROM BS 1287 - 1330 LONGERON 26L IN AFT CARGO BAY. DOUBLER WAS REPLACED IAW DWG 5936021 REV EH AND SRM 51-30-02.

Part: SKIN — SCRATCHED (ELEVATOR TAB) · airframe 62,500 hrs · 45,401 cycles

SCRATCH RT CONTROL TAB EXTERNAL SKIN LOWER SURFACE NEAR OF HINGE AND LEADING EDGE. RT ELEVATOR CONTROL TAB WAS REPLACED PER AMM 27-30-03.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 62,500 hrs · 45,401 cycles

DELAMINATED LT GEARED TAB. LT ELEVATOR GEARED TAB WAS REPLACED PER AMM 27-30-04.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

BROKEN CHANNELS AND FLOOR PANELS NRS 1155A, 389A, 693A, 1079A. FLOOR PANEL NR 389A AND 693A WERE REPAIRED FOR CRACKS IAW SRM 53-05, FIG 131 AND CHANNELS AT FLOOR PANELS NRS 1155A AND 1079A WERE REPAIRED IAW SRM 51-70-1D, PAR 10, HFEC INSPECTION WAS ACCOMPLISHED ON CHANNEL AND FLOOR PANEL NR 693A AND NO CRACKS WERE FOUND, IAW NDT SPM 06-10-01.001. EQUIPMENT MENTOR C/N 1205, EXP DATE: 24-AUG-17 STOP DRILL ON CHANNEL AND FLOOR PANEL, NR 389A WAS NOT FOUND.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,492 hrs · 45,396 cycles

AWR HIDDEN DAMAGE: DELAMINATION UPPER SKIN OF OTBD VANE GUIDE ON INBD FLAP AT RT WING. DAMAGE AREA WAS REPAIR IAW SRM 57-03D, P11, FIG 11 AND JIC OPN 1031.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

MISSING MATERIAL AND DAMAGED FERRULES ON FLOOR PANELS NR 160A AND 1250C. FERRULES ON FLOOR PANELS NR 1250C WERE REPLACED AND DUE MISSING MATERIAL ON FLOOR PANELS NR 160 A WAS REPLACED AMM 53-20-01-201.

Part: ACCESS PANEL — DELAMINATED (RT HEATER) · airframe 62,492 hrs · 45,396 cycles

DELAMINATION ON RT HEATER BLANKET FUEL ACCESS, PN 3075-10. ON RT HEATER BLANKET FUEL ACCESS, PN 3075-10 WAS REPAIRED IAW ER/A 530866-14AD MA, REV ORIGINAL.

Part: ACCESS PANEL — DELAMINATED (LT HEATER) · airframe 62,492 hrs · 45,396 cycles

DELAMINATION ON LT HEATER BLANKET FUEL ACCESS PLATE, PN 3075-100. LT HEATER BLANKET FUEL ACCESS PLATE, PN 3075-100 WAS REPAIRED IAW ER/A 530866-14AD MA, REV ORIGINAL.

Part: DOUBLER — WORN (SERVICE DOOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: WEAR ON PREVIOUS REPAIR DOUBLER AT FORWARD SERVICE DOOR STA Y=198 BETWEEN BEAM 2 AND 3. WEAR ON PREVIOUS REPAIR DOUBLER AT FORWARD SERVICE DOOR STA Y=198 BETWEEN BEAM 2 AND 3 WAS ATTENDED IAW ER/A 333066-14, REV ORIGINAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON RT CUSP WEB FROM STA Y = 912 TO Y= 916 BETWEEN X=- 44 AND X=-60 AT CPAX. RT CUSP WEB FROM STA Y=912 TO Y=916 BETWEEN X=-44 AND X=-60 AT CPAX WAS REPAIRED IAW SRM 53-05, FIG 131A-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON LT SEAT TRACK X=54 AT STA Y=674, Y=731 AND Y=750. CORROSION ON LT SEAT TRACK X=54 AT STA Y=674, Y=731 AND Y=750 WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACK ON INTERCOSTAL BETWEEN STA Y=1287-Y=1307, X=0 AT PASSENGER CABIN. REPLACED IAW DWG 5930560, REV BW AND SRM 51-30-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON UPPER, LOWER LT CUSP WEB FROM STA Y=984 TO Y=1003 BETWEEN X =44 AND X=60 AT CABIN PASSENGER. LT CUSP WEB FROM STA Y=984 TO Y=1003 BETWEEN X=44 AND X=60 WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 62,492 hrs · 45,396 cycles

CRACKED CHANNELS ON GENERATION FLOOR PANELS NR 541F, 927A, 465A. FLOOR PANEL WERE REPAIR FOR CRACKS IAW SRM 53-05, FIG 131.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL CP: CORROSION ON CUSP ANGLE UPPER/LOWER SURFACE RT SIDE X=-54 TO X=-60 BETWEEN STA Y=147 AND Y=218 PASSENGER FLOOR STRUCTURE. W1, PERMANENT REPAIR WAS ACCOMPLISHED IN CUSP ANGLE IAW SRM 53-05, FIG 55.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

AWR: CORROSION OUT OF LIMITS ON CUSP WEB ON RT BETWEEN STA Y=1136 TO Y=1142. CUSP WEB ON RT BETWEEN STA Y=1136 TO Y=1142 WAS REPAIRED IAW SRM 53-05, FIG 131A-9.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BETWEEN STA Y=1193 TO Y=1212 BETWEEN X=54 AND X=60. DOUBLER REMOVED DUE TO CORROSION IAW SRM 51-30-5, PAR 8. NEW DOUBLER AND RING DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A, 51-10-3 PAR 14 & 21, AND 51-30-5, PAR 7.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACK ON RT CUSP WEB FROM STA Y=1292 TO Y=1295 BETWEEN X=-44 AND X=-60 AT CPAX. RT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG.

Part: FRAME — WORN (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: WEAR ON FRAME STA Y=1338 BETWEEN LONGERON 29RT TO 28RT AT FWD DOOR JAMB APU COMPARTMENT AFT ACCESSORY COMPARTMENT. WEAR WAS FOUND ON PREVIOUS WELDING REPAIR AND FOLLOW WITHIN CONDITION IAW ER/A 094719-14MA, REV A. FPI WAS ACCOMPLISHED IAW DPS 4.707, REV BB AND NO CRACKS WERE FOUND ON WEAR ON FRAME STA Y=1338 BETWEEN LONGERON 29RT TO 28RT AT FWD DOOR JAMB APU.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACK ON RT CUSP WEB OF STA Y: 840 BETWEEN STA X: -54 TO -60 AT PAX CABIN. RT CUSP WEB AT STA Y=840 BETWEEN X=-54 AND X=-60 WAS REPAIRED IAW SRM 53-05, FIG. 131A-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT SEAT TRACK X=-54 BETWEEN STA Y=215 TO Y=265. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4F.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

DAMAGED FERRULES, MISSING MATERIAL AND PUNCTURED FLIGHT COMPARTMENT AND FORWARD FUSELAGE FLOOR PANELS NR 120C, 160C, 200E, 200B, 256B, 256C, 256D, 313C, 389E, 398C, 465C, 465B, 541B, 541541C, 541E, 693B, 693B, 769C, 826F. FERRULES ON FLOOR PANELS NRS 256B, 256D,256C, 769C, 389C, 465B, 541B, 693C, 541C, 120C, 541D, 826F, 465C, 389E, 313C AND 693B WERE REPLACED FERRULES IAW AMM 53-20-01-201. FLOOR PANELS NRS 200E, 200B AND 541E WERE FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL 160C WAS ATTENDED IAW NRC 01052.

Part: PAN — CRACKED (ENTRY DOOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKED FORWARD UPPER PAN AT FORWARD ENTRY DOOR. CRACKED FORWARD PAN WAS REPAIRED IAW SRM 52-05D, FIG 18A.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON FLOOR PANEL 160G AT CABIN PASSENGER. FLOOR PANEL 160G WAS REPLACED IAW SRM 51-10-4 AND DWG 9957828, REV Y.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL : CORROSION ON RT CUSP WEB FROM STA Y = 601 TO Y= 612 BTW X= - 44 AND X=-60 AT CPAX. CUSP WEB FROM STA Y=602 TO Y=609 BTW X=54 AND X=60 WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKED BEAM NR 1 BETWEEN STA Y=160 TO Y=170 AT FORWARD ENTRY DOOR. CRACKED BEAM NR 1 AT FORWARD ENTRY DOOR WERE REPAIRED IAW SRM 52-05-D, FIG 98.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

LIGHTNING STRIKES ON FUSELAGE SKIN ON STA Y=460, 486, 491, 494, 503, 536, 546. BETWEEN LONGERON 27R-28R. FUSELAGE SKIN ON STA Y= 460, 486, 491, 494, 503, 536, 546, BETWEEN LONGERON 27R-28R WERE REPAIRED IAW 53-04-2, PARA 3, C2, A, 1, A PERMANENT REPAIR AND FIG 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON UPPER /LOWER RT CUSP WEB FROM STA Y=712 TO Y=788 BETWEEN X=-44 AND X=- 60. WEB WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9930538, REV CF.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON LT CUSP WEB BETWEEN STA Y=1041-Y=1046 AND X=54 TO X=60 AT PASSENGER CABIN. CORROSION ON LT CUSP WEB BETWEEN STA Y=1041-Y=1046 AND X=54 TO X=60 AT PASSENGER CABIN IN REF CARD NR 260, SM, CS WAS REPAIRED DUE TO EXCESSIVE DAMAGE. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-13, 51-30-2 AND 51-30-05, PAR 7.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 62,492 hrs · 45,396 cycles

DELAMINATED LT CONTROL TAB. ELEVATOR CONTROL TAB LT WAS REPLACED IAW AMM 27-30-03-201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

AWR: LIGHTNING STRIKES ON PASSENGER CABIN WINDOW EXTERNAL CUTOUT BETWEEN STA Y=1079 TO Y=1098. WINDOW BELT LT WAS REPAIRED IAW ER/A 550277-14, REV ORIGINAL WILL BE MONITORED WITH LOG PAGE 2668777.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACK ON RT CUSP WEB BETWEEN STA Y: 788 TO 807 AND STA X: -54 TO -60 AT PASSENGER CABIN. RT CUSP WEB BETWEEN STA Y=788 AND Y=807, FROM X=-54 TO X=-60 WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

SEVERAL CORROSION ON RT CUSP WEB BETWEEN STA Y=1079 TO Y=1089 AND X=-54 TO X=-60, UPPER AND LOWER SURFACE. CABIN PASSENGER AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACKS ON RT CUSP WEB, 3 EA, FROM STA Y=218 TO Y=226 BETWEEN X=-44 AND X=-60 AT CPAX. CUSP WEB FROM STA Y=218 TO Y=226 BETWEEN X=-44 AND X=-60 WAS REPLACED IAW SRM 51-10-4 , 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

AWR LIGHTNING STRIKES ON PAX CABIN WINDOWS EXTERNAL CUT OUT STA Y=1041 TO Y=1060, LT SIDE. WINDOW BELT WAS REPAIRED IAW ER/A 550276-14, REV. MONITORED WITH LOG PAGE NR 2668875.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACK ON LT CUSP WEB BETWEEN STA Y=1287 TO Y=1307 AND BETWEEN X=54 AND X=60 AT CABIN PASSENGER. CRACK ON LT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKED BEAM NR 1 BETWEEN STA Y=190 TO Y=200 AT FORWARD ENTRY DOOR. CRACKED BEAM NR 1 WAS REPAIRED IAW SRM 52-05D, FIG 97.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

AWR HIDDEN DAMAGE. CORROSION ON BULKHEAD FWD FACE LOWER SIDE OF STA Y:1338 AND PROJECTION LONGERON 29 LT. BULKHEAD FWD FACE LOWER SIDE OF STA Y:1338 AND PROJECTION LONG 29LT. REPAIRED IAW ETI 88-16-328, REV 1, ER 549251-14, REV ORIGINAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON RT CUSP WEB FROM STA Y = 1067 TO Y= 1076 BETWEEN X=- 44 AND X=- 60 AT CPAX. AREA OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACK ON RT CUSP WEB OF STA Y: 875 BETWEEN STA X: -54 TO -60 AT PAX CABIN. RT CUSP WEB ON STA Y=875 BTW X=-54 AND X=-60 WAS REPAIRED IAW SRM 53-05 FIG 131A-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT CUSP WEB OF STA Y: 638 TO Y: 642 BETWEEN STA X:-54 TO -60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW-80 SRM 53-05, FIG 131A.

Part: ACCESS PANEL — BENT (RT WING) · airframe 62,492 hrs · 45,396 cycles

BENT RIGHT WING ACCESS PANEL 1476C. THE ACCESS PANEL WAS REPLACED.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

DELAMINATED FLOOR PANEL 120E. FLOOR PANEL 120E WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL, CORROSION AT FLOORBEAMS AT STA Y= 1322 AND 1338, LT AFT LAVATORY, PASSENGER CABIN. FLOORBEAM AT STA Y= 1322 LT AFT LAVATORY, PASSENGER CABIN WAS REPAIRED IAW SRM 53-05, PAR-21, FIG-20.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL, CORROSION ON UPPER /LOWER LT CUSP WEB FROM STA Y=579 TO Y=598 BETWEEN X=54 AND X =60 AT CABIN PAX. LT CUSP WEB FROM STA Y=579 TO Y=598 BETWEEN X=54 AND X=60 WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL, CORROSION ON FLOOR SUPPORT BEAMS AT STA Y=1322 AND 1338 RT AFT LAVATORY, PASSENGER CABIN. FLOOR SUPPORTS BEAMS AT STA Y= 1322 AND 1338 RT AFT LAVATORY, PASSENGER CABIN WERE REPAIRED IAW SRM 53-05, PAR-21, FIG-20.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON FLOORBEAM OF LT AFT LAVATORY STA Y: 1338, PASSENGER CABIN. FLOORBEAM OF LT AFT LAVATORY STA Y: 1338 WAS REPAIRED IAW SRM 53-05 FIG-20.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL, CORROSION ON RT CUSP WEB FROM STA Y=297 TO Y=300 BETWEEN X=-44 AND X=- 60 AT CPAX. REPAIRED IAW SRM 53-01, FIG 131A-13.

Part: FLOORBEAM — CORRODED (BS 1307) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON FLOORBEAM BS 1307 X 20 LEFT SIDE AT PAX CABIN. REPAIRED IAW SRM 51-70-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT CUSP WEB FROM STA Y:487 TO Y:501 AND STA X:-54 TO -60 AT PAX CABIN. RT CUSP WEB FROM STA Y:- 487 TO Y:501 AND STA X: -54 TO -60 WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CORRODED (BS 400-405) · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT CUSP WEB FROM BS 400 - 405, BETWEEN RBL 44 - 60. THE CUSP WEB WAS REPAIRED SRM 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT CUSP WEB FROM BS 446 - 465, BETWEEN RBL 44 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A -14.

Part: SPAR — UNKNOWN (LT WING) · airframe 62,492 hrs · 45,396 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, 7 DIFFERENT FASTENERS OF PSE, ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING. THESE NRC IS ATTENDED WITH ER/A NR 549305-14AD, REV ORIGINAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CM CORROSION ON PREVIOUS DOUBLER REPAIR STA Y=1309 BETWEEN LONGERON 28 LT-28 RT. AT AFT CARGO COMPARTMENT C3. CORROED PARTS OF PREVIOUS REPAIR WERE REMOVED IAW SRM 51-30-5 AND REPAIR PLATE WAS FABRICATED IAW SRM 53-03D, FIG 2A AND ALSO NEW REPAIR ANGLE AND FRAME SEGMENT WERE DRILLED AND AJUSTED IAW SRM 51-10-4, WAS TREATED AND PAINTED ALL PARTS IAW SRM 51-10-03 PARAGRAPH 14 AND 21, THEREFORE REPAIR PARTS WERE INSTALLED IAW SRM 51-30-05 AND 53-03D, FIG 2A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON UPPER, LOWER LT CUSP WEB FROM STA Y=560 TO Y=579 BETWEEN X=54 AND X=60 AT PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: SPAR — UNKNOWN (RT WING) · airframe 62,492 hrs · 45,396 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, 7 DIFFERENT FASTENERS OF PSE, ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT RT WING. THESE NRC IS ATTENDED WITH ER/A NR 549305-14AD, REV ORIGINAL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,492 hrs · 45,396 cycles

PARTS RACKS: DAMAGED FERRULES, PUNCTURED AND MISSING MATERIAL ON FLOOR PANELS NR 1003C, 1117D, 1174D, 1174C, 1250B, 1307B WING BOX AND AFT FUSELAGE. FLOOR PANEL NRS: 1307B, 1117D AND 1174C WERE REPLACED FERRULES IAW AMM 53-20-01-201 FLOOR PANEL NBR: 1003C, 1174D AND 1250B WERE REPAIRED IAW AMM 25-00-00-801.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKED FRAME STA Y=1322 AND LONGERON 17TH PASSENGER CABIN. FRAME WAS REPAIRED IAW ER 493697-14MA, REV B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON UPPER, LOWER RT CUSP WEB FROM STA Y=503 TO Y=598 BETWEEN X=-44 AND X =-60. DUE TO EXCESSIVE CORROSION, CUSP WEB WAS REPLACED IAW DWG 9930538 REV CF AND SRM 51-30-2, SRM 51-30-5, SRM 51-30-1.

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON FUEL ACCESS PLATE NR 1303C. FUEL ACCESS DOOR 1303C WAS REPLACED IAW SRM 51-22-2A CONDITION 3, PAR B AND IPC 57-30-00.

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON FUEL ACCESS PLATE NR 1409C. FUEL ACCESS DOOR 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION 3, PAR B AND IPC:5730-00.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,492 hrs · 45,396 cycles

DAMAGE FERRULES AND DELAMINATED FLOOR PANELS NRS 200D, 160B, 160E, 148B, 160D, 148A, 148C, 160F, 160C, 210C AT PASSENGER CABIN. FLOOR PANELS NRS 200D, 160B, 160E, 148B, 160D, 148A, 148C, 160F, 160C, 200C WERE FABRICATED AND IDENTIFIED IAW AMM 53-20-01-201, FLOOR PANEL 200C WAS FABRICATED INSTEAD OF 210C, DUE TO NRC DESCRIPTION ENTRY ERROR.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL, CRACKED LONGERON 2LT AND STA Y:160 AT PASSENGER CABIN INTERNAL STRUCTURE. LONGERON NR 2 BETWEEN STA 180 TO STA 190 WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON AFT RT TRACK AT MID CARGO, C2. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON INTERCOSTAL BETWEEN LONGERON 28 RT TO 27 RT AND STA Y=769 TO Y=788 AT MID CARGO. NEW INTERCOSTAL WAS REPLACED IAW SRM 51-30-5 AND DWG 9915554, REV U.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL, CRACK ON FUSELAGE SKIN ON STA Y=1380 BETWEEN LONGERONS 13R-14R. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04, FIG 18.

Part: PAN — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

CRACKS ON LT WINDOW RING PAN BETWEEN STA Y=788/807 LOWER/FORWARD, BETWEEN STA Y =984/1003 LOWER/FORWARD AND UPPER/FORWARD, BETWEEN STA Y=1022/1041 LOWER/FORWARD, BETWEEN STA Y =1174-STA 1193 UPPER/AFT AT PASSENGER CABIN. LT WINDOW RING PANS BETWEEN STA Y =788- STA 807 LOWER/FORWARD, BETWEEN STA Y =984/ STA1003 LOWER/FORWARD AND UPPER/FORWARD, BETWEEN STA Y=- 1022/ STA1041 LOWER/ FORWARD, BETWEEN STA Y =1174/ STA1193 UPPER/AFT WERE REPAIRED IAW SRM 53-05, FIG 122, ER/A 493648-14MA REV A AND ER/A 487747-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKS ON RT WINDOW RING PAN BETWEEN STA Y=769/788 AFT/LOWER CORNER, BETWEEN STA Y=1041/1060 LOWER, FORWARD CORNER AT PASSENGER CABIN. RT WINDOW RING PAN BETWEEN STA Y=769/788 AFT/LOWER CORNER, BETWEEN STA Y=1041/1060 LOWER/FORWARD CORNER WERE REPAIRED IAW SRM 53-05, FIG 122, ER/A 493648-14MA, REV A AND ER/A 487747-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 62,492 hrs · 45,396 cycles

INITIAL: CRACKS ON LT WINDOW RING PANE, STA Y=902 LOWER/AFT CORNER, STA Y=930 UPPER/FWD CORNER, STA Y=1098 UPPER /AFT CORNER. LT WINDOW RING PANS STA Y=902 LOWER/AFT CORNER, STA Y= 930 UPPER/ FWD CORNER, STA Y=1098 UPPER /AFT CORNER WERE REPAIRED IAW SRM 53-05, FIG 122, ER/A 493648-14MA REV A AND ER/A 487747-14MA, REV A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

CORROSION ON RT CUSP WEB FROM STA Y:474 TO Y:479 AND STA X: -54 TO -60 AT PASSENGER CABIN. RT CUSP WEB FROM STA Y:- 474 TO Y:479 AND STA X: -54 TO -60 WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,492 hrs · 45,396 cycles

INITIAL: CORROSION ON LT SEAT TRACK X=22 AND SETTLEMENT AREA FROM STA Y = 218-Y = 256 AT CPAX. SEAT TRACK WAS REPLACED DUE TO WAS FOUND OUT OF LIMITS BETWEEN Y=200 TO Y=306 IAW SRM 53-05, FIG 4F.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 61,871 hrs · 44,938 cycles

LEFT ELEVATOR TIP LIGHTNING EXIT DAMAGE. REPLACED LT ELEVATOR.

Part: REPAIR — CRACKED (NLG DOOR HINGE) · airframe 61,487 hrs · 44,639 cycles

WHILE IN C-CHECK, MAINTENANCE DISCOVERED THAT PREVIOUS REPAIRS TO THE LT AND RT AFT NOSE GEAR DOOR HINGE CUTOUTS WERE CRACKING. PREVIOUSLY, THE SRM AUTHORIZED A REPAIR USING A 0.050 THICK DOUBLER TO REPAIR 0.063" SKIN; THIS REPAIR HAS SINCE BEEN SUPERSEDED BECAUSE IT WAS FOUND TO CRACK AND FAIL. AT THIS VISIT, MAINTENANCE REMOVED AN OLD SRM REPAIR AND INSTALLED A REPAIR WITH THE SAME FOOTPRINT BUT IAW THE INSTRUCTIONS OF THE NEW REPAIR. SRM 53-05, PARA 162. HOWEVER THERE IS A FASTENER COUNT MISMATCH BETWEEN THE OLD AND NEW SRM REPAIRS. ER/A 545552-14 AUTHORIZES THE CONTINUED INSTALLATION OF THE DOUBLER WITH THE OLD SRM REPAIR FASTENER COUNT. COMPLIED WITH ER/A 545552-14, REV, ORIGINAL, ASSOCIATED ER/A 14-545552, ADDED FOR AC 9007.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 61,488 hrs · 44,640 cycles

LT MLG W/W DOOR IS CRACKED AT INBD FWD CORNER. REPLACED DOOR.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 61,488 hrs · 44,640 cycles

LT MLG W/W DOOR IS CRACKED AT INBD FWD CORNER. REPLACED DOOR.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 60,855 hrs · 44,245 cycles

CREW FOUND EMERGENCY OVERWING LIGHTS INOPERATIVE. MAINTENACE REPLACED THE BATTERY POWER SUPPLY BASE. LIGHTS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,725 hrs · 44,140 cycles

THE FLIGHT CREW FOUND INTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY OVERWING EVACUATION BATTERY PACK AND THE LIGHTS CHECKED OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 59,781 hrs · 43,438 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT ROW 18 WAS INOPERATIVE. MAINTENANCE REPAIRED AND SECURED THE WIRING AND THE LIGHT RETURNED TO NORMAL OPERATION.

Part: CAM — LOOSE (TAILCONE RELEASE) · airframe 59,345 hrs · 43,112 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CAM LEVER LOOSE ON THE SPLINES. MAINTENANCE REPLACED THE CAM LEVER ASSEMBLY AND THE FUNCTIONAL TEST WAS SATISFACTORY.

Part: RECEPTACLE — WORN · airframe 59,345 hrs · 43,112 cycles

DURING CHECK, MAINTENANCE FOUND NUMEROUS ALIGNMENT PIN RECEPTICLES WORN. MAINTENANCE REPLACED THE ALIGNMENT PIN RECEPTICLES. LP 1952193.

Part: CLEVIS — IMPROPER PART (TAILCONE RELEASE) · airframe 59,345 hrs · 43,112 cycles

DURING CHECK, MAINTENANCE FOUND IMPROPER SAFETY ON 3 CLEVISES ON THE TAILCONE RELEASE CABLE. MAINTENANCE RESAFETIED THE CLEVIS AND THE FUNCTIONAL TEST WAS SATISFACTORY. LP 1951354.

Part: RELEASE CABLE — OUT OF ADJUST (TAILCON) · airframe 59,345 hrs · 43,112 cycles

DURING CHECK, THE TAILCONE RELEASE CABLE FAILED GAP CLEARENCE DURING FUNCTIONAL TEST. THE TAILCONE RELEASE CABLE WAS ADJUSTED AND THE TEST WAS PERFORMED SATISFACTORILY. LP 1951349.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,063 hrs · 41,475 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS CABIN SECTION INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: RELEASE CABLE — LOOSE (TAILCONE) · airframe 56,143 hrs · 40,834 cycles

THE CAPTAIN REPORTED THAT THE OVERHEAD WARNING ALERTED FOR THE TAILCONE NOT BEING SECURED. MAINTENANCE FOUND THAT THE TAILCONE RELEASE SYSTEM CABLE WAS LOOSE AND REQUIRED REPLACEMENT. CABLE REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: PAN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 56,137 hrs · 40,830 cycles

DURING CHECK, NOTED C2 CARGO DOOR CUTOUT LOWER PAN WITH NUMEROUS AREAS OF CORROSION. REPAIRED IAW SRM 53-05, FIG 123.

Part: ACM — LEAKING (RIGHT) · airframe 56,096 hrs · 40,805 cycles

THE CREW REPORTED A HOT ODOR AND VISIBLE HAZE IN THE CABIN ENROUTE. NO EMERGENCY DECLARED AND THE HAZE AND ODOR DISSIPATED AFTER THE RT PACK WAS TURNED OFF. MAINTENANCE PERFORMED CABIN SMOKE-ODOR TROUBLESHOOTING AND FOUND THE RT ACM LEAKING. MAINTENANCE REPLACED THE RT ACM AND PERFORMED A DUCT BURNOUT. ACFT RELEASED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CABIN PRESSURE) · airframe 53,490 hrs · 38,977 cycles

ON DESCENT THRU 17,000FT, RECEIVED A FLOW LIGHT WITH CABIN PRESSURE CLIMBING. FOLLOWED QRH PROCEDURE, NO HELP. DESCENDED TO 10,000 FT DUE TO LOSS OF BOTH LT AND RT PACKS. THE CABIN PRESSURE REMAINED WITHIN RANGE AND THE MASKS DID NOT DEPLOY. MX R & R PRESSURE SUPPLY INDICATOR AND AUGMENTATION VALVE FILTER ELEMENT AS A PRECAUTION. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,766 hrs · 38,434 cycles

DURING SERVICE CHECK, MX FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. FOUND BATTERIES IN POWER SUPPLY BAD. REMOVED AND REPLACED SAME.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 52,614 hrs · 38,337 cycles

COCKPIT EMERGENCY LIGHTS WOULD NOT TURN OFF. MX CYCLED EMERGENCY LIGHT CIRCUIT BREAKERS. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,063 hrs · 37,972 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED BATTERY PACK ASSEMBLY PER AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,345 hrs · 37,484 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT STAIRWAY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN 2R LAVATORY CEILING EMERGENCY LIGHTS. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,169 hrs · 37,359 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT AND FORWARD CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,327 hrs · 36,788 cycles

FLOOR STRUCTURE SEAT TRACK FS 207 TO 230 LBL 50 CORROSION. REMOVED FLOOR STRUCTURE SEAT TRACK FILLER FS 212 IAW DC9/MD80 SRM 51-30-3 PG 19. FILLER FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 PG 8.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,460 hrs · 36,139 cycles

HOLES/COUNTERSINKS WORN FIXED L/E, V/S HOLES COMMON TO SPLICE WITH REM L/E

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,336 hrs · 36,048 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS DID NOT TURN ON FROM F/A PANEL SWITCH. MX TROUBLESHOT AND R & R OVERWING EMERGENCY EVACUATION LIGHTS AFT B/B RACK AND BATTERY PACK. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,336 hrs · 36,048 cycles

DURING LINE CHECK, MX FOUND BOTH EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MX R & R AFT B/B RACK AND BATTERY PACK. OPS CHECK WAS GOOD. (2011-D0455)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,336 hrs · 36,048 cycles

DURING LINE CHECK, MX FOUND OVERHEAD EMERGENCY ESCAPE LIGHTING AT FWD AND SERVICE ENTRANCES INOPERATIVE DURING TEST. MX R & R POWER SUPPLY AND BATTERIES B5-23. OPS CK WAS GOOD.

Part: WIRE — BROKEN (AC BAY) · airframe 49,139 hrs · 35,920 cycles

DURING LINE CHECK MAINTENANCE FOUND TAIL COMPARTMENT EMERGENCY PATHWAY LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 47,947 hrs · 35,136 cycles

DUE ERA 484488-14, REV A CODE 53-16 PERMANENT REPAIR TO C-3 CARGO DOOR SURROUND, LOWER JAMB BEAM CORROSION.

Part: FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 47,947 hrs · 35,136 cycles

EA 09-093855-03 ME02 PITTING CORROSION ON RT MLG FITTING BUSHING BORE AT VERT TRANSITION AND BEARING. REPAIRED PER DWG 5935812 REV AU ON N/R T0183179 AT HMV3 IN GDL(DLM88102435).

Part: SKIN PANEL — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 47,947 hrs · 35,136 cycles

PITTING CORROSION ON BARREL NUT HOLE OF LT HORIZONTAL STAB UPPER FWD SKIN PANEL AT STA XH 28. REPAIRED PER AMR REPAIR DOCUMENT 0955141 AT HMV3 IN GDL ON N/R T0182701.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · corrosion level 2 · airframe 47,947 hrs · 35,136 cycles

PITTING CORROSION ON BARREL NUT HOLES OF RT HORIZ STAB UPPER FWD AND UPPER AFT SKIN PANELS 1 EA. REPAIRED IAW AMR DOCUMENT 0955141 BARREL NUT HOLE NR3 AND NR 26 ON T0182702 AT HMV3 IN GDL.

Part: SKIN — CORRODED (BS 1098-1105) · corrosion level 2 · airframe 47,947 hrs · 35,136 cycles

CORROSION ON FUSELAGE SKIN BETWEEN STA 1098 AND 1105 AND LONG 28 LT. REPAIRED IAW SRM 53-04D, FIG 53 ON N/R T0183481 AT HMV3 IN GDL.

Part: PAN — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 47,944 hrs · 35,135 cycles

C-1 DOORWAY JAMB PAN WAS CORRODED. REPAIRED IAW SRM 53-05D, FIG 804D. MAJOR REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,479 hrs · 34,799 cycles

OVERWING FRAME CRACK. REPAIRED PER EO 09-460094-12, ME03 (DLM88102004).

Part: SWITCH — HOT (CABIN LIGHTS) · airframe 47,089 hrs · 34,536 cycles

STRONG ELECTRICAL SMELL IN CABIN AND COCKPIT. NO VISUAL INDICATIONS OF FIRE. REPORT AFT UPPER/SIDEWALL LIGHT SWITCH EXTREMELY HOT TO TOUCH. C/W OP 5088 PNEUMATIC DIST CABIN SMOKE/ODOR T/S. C/W OP 5090 ALTERNATE DUCT BURNOUT. C/W OP 7904 REPLACED WATER SEPARATOR COALESCER BAGS. ACFT OK FOR SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,005 hrs · 34,500 cycles

DISSIMILAR CORROSION ON INTERNAL DOUBLER ON FUSELAGE SKIN AFT LAVATORY SERVICE PANEL AREA. MRB 53-100-01. REF T0182159 PARTS WHERE REMOVED, FABRICATED AND INSTALLED IAW AMR 0953783REV2. REPAIR WAS DONE IAW ERA 485410-14. REF AM N/R T0183480(DLM88102460)

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 46,854 hrs · 34,405 cycles

FOUND ON CHECK EMRG PATH LIGHTS OUT AT ROWS 11 E/D. RECONNECTED OPEN HARNESS CONNECTION BENEATH SEAT 11 D. OPEN CHECKS GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,854 hrs · 34,405 cycles

FOUND ON CHECK. EMERG PATH LIGHTS OUT ROW 15 E/D. RESET HARNESS CONNECTOR. OPEN CHECKS GOOD.

Part: DIODE — OVERHEATED (REVERSE CURRENT) · airframe 44,105 hrs · 32,677 cycles

IN FLT 23000, CAPT SMELLED FUMES IN ACFT FWD LAV SMOKE DET ALARMED 1 RADIO STATIC AND UNREADABLE AFTER 5 MINUTES FUMES AND ODOR DIED DOWN AND SMOKE DETECTOR STOPPED. NO CB OR WARNING ASSOCIATED WITH THIS. FOUND EVIDENCE OF HEAT DAMAGE TO REVERSE CURRENT DIODES R7-48 AND R7-49. REPLACED SAME PER EA 09-472174-12 REV B AN M/M 24-30-00-201. CKS GOOD. DIODES REPLACED OUT OF PRECAUTION DUCT BURNOUT PORTION OF OPN 5089 C/W. NDS CLOSE UP AND H2O BAGS REPLACED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 42,228 hrs · 31,401 cycles

STRANGE ODOR THROUGHOUT CABIN WITH ASSOCIATED HAZE. SMOKE ALARM WENT OFF IN AFT LAV. REMOVED BORO PLUGS ON BOTH ENGINES PER AMM 72-00-00-6012. PERFORMED BORESCOPE OF 6TH AND 7TH STAGE AND 8TH STAGE BLEED DUCT ON NR 1 AND NR 2 ENGINES. NO OIL OR RESIDUE WAS NOT INSTALLED BORO PLUGS AND SECURED ENGINE COWLING. REMOVED BOTH WATER SEPARATORS. INSPECTED WATER SEPARATORS AND REINSTALLED. REMOVED APU DOOR. CLEANED AREA AND DOOR. REINSTALLED DOOR. TROUBLESHOT IAW OPN 5088. COULD NOT FIND ANY PROBLEMS. EVERYTHING CHECKS GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 41,720 hrs · 31,098 cycles

DURING FLT AT FL370, SMELLED SMOKE IN ACFT CABIN AND COCKPIT. AFT LEFT SMOKE DETECTOR WENT OFF W/SIGNIFICANT HAZE IN CABIN. RAN SMOKE FUMES CHECK LIST. LANDED IN KCHS. T/S PER M/M 05-50-01. RAN ENGINE AT HIGH POWER. PERFORMED DUCT BURNOUT PER OP 5089 AND 5088. FOUND HYD SYSTEM OVERSERVICED AND OVERFLOW BOTTLES FULL. DRAINED LEFT AND RT HYD SYSTEM TO PROPER LEVEL EMPTIED OVERFLOW BOTTLES. FOUND HYD LEAK AT AUX PUMP RESEATED LINE, LK CKS GOOD. APU INLET CLEAN ENGINE INTAKE CLEANED, NO SMELL OR SMOKE NOTED IN CABIN.

Part: FITTING — BENT (NLG SUPPORT) · airframe 40,400 hrs · 30,206 cycles

NLG SUPPORT BEAM FITTING BENT AND WHEELWELL WEB CRACKED. REPLACED SUPPORT BEAM FITTING AND REPAIRED WEB.

Part: ROLLER — MISSING (CONTROL LEVER) · airframe 24,233 hrs · 19,008 cycles

WHEN PERFORMING T/O WARNING CHECK PRIOR TO T/O THE AUTOBRAKES AURAL WARNING SOUNDED AND COULD NOT BE SILENCED. T/S AND FOUND ROLLER MISSING FROM SPEEDBRAKE CTRL LEVER ARMING SWITCH PACK ON PEDESTAL. REMOVED AND REPLACED SAME PER M/M. PERF ADJ TEST PER M/M FUNCT CK OK. PERF DFGC RTS 1-2 BOTH PASS OK. AUTOSPOILER SYST CKS OK.

Part: TURBINE — FAILED (APU) · airframe 24,200 hrs · 18,978 cycles

APU FAILED IN FLIGHT, WOULD NOT RESTART ON GROUND. REPLACED SPEED SENSOR AND CONTROLLER, NO HELP. APU HANGS AT 20 PERCENT WITH SPARKS OUT OF TAILPIPE SUSPECT TURBINE FAILURE. REMOVED AND REPLACED APU ASSY PER M/M. OPS / LK CK OK. MCO/PLAC REMOVED.

Part: HANDLE — NOT SEATED (COCKPIT) · airframe 21,567 hrs · 17,034 cycles

LANDING GEAR DOWN UNSAFE INDICATION WHEN GEAR DOWN SELECTED. PULLED EMERGENCY HANDLE AND GEAR SHOWED 3 GREEN. FOUND GEAR HANDLE NOT FULLY IN GEAR DOWN DETENT. JACKED AIRCRAFT AND SWUNG GEAR. UNABLE TO DUPLICATE.

Part: BATTERY — DISCHARGED (L 1 DOOR)

R1 AND L1 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND RELAMPED, OPS NOW OK.

Part: BATTERY — DISCHARGED (BS 211)

EMERGENCY LIGHT IN COCKPIT OVERHEAD AND GALLEY/FWD ENTRY OVERHEAD EMERGENCY LIGHTS WOULD NOT TEST DURING LAYOVER. REPLACED BATTERIES AT FS 211 LOCATED IN OVERHEAD DROP DOWN PANEL.

Part: ENGINE — FAILED (NR 2)

ON TAXI OUT, DURING START OF NR 2 ENG, REPORTED TAIL PIPE FIRE AND EGT REACHED 600 DEGREES. REPLACED ENGINE.

Part: WIRE — EXPOSED (CABIN)

EMERG TRACK LIGHTING HAS EXPOSED WIRES AT LAST ROW OF FIRST CLASS. REPLACED EMERGENCY TRACK LIGHT BULB AND LENS ASSY.

Part: FIRE DET UNIT — FAILED (NR 1 ENGINE)

LEFT ENG FIRE WARNING. SHUT DOWN LEFT ENG, NO SECONDARY INDICATIONS. REPLACED FIRE DETECTOR UNIT.

Part: AIR DISTRIBUTION — ODOR (CABIN)

BURNING SMELL IN COCKPIT. DISSIPATED AFTER T/O, PERFORMED BURNOUT. INSPECTED APU INLET.

Part: COALESCER BAGS — CONTAMINATED (CABIN)

STRONG ODOR IN AC SYSTEM DURING INITIAL CLIMB. REPLACED WATER SEPARATORS, RAN PACKS, NO SMELL.

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

EN ROUTE DFW/OAK, F/O R1 WINDSHIELD SHATTERED. REPLACED R1 WINDOW AND CONTROLLER.

Part: NOSE COWL — DENTED (NR 1 ENGINE)

DURING SHOP INSPECTION, A DENT WAS FOUND IN THE LEADING EDGE LIP OF THE NOSE COWL. THE DAMAGE WAS REPAIRED PER SRM 54-04A.