N9409F

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,068 hrs · 33,629 cycles

CEILING EMER LIGHTS FROM ROW 3 - 6 INOPERATIVE. R & R BATTERY PACK. CEILING EMER LIGHTS FROM ROW 3 - 6 OPERATIONALLY CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,068 hrs · 33,629 cycles

OVERHEAD EMER LIGHTS AT ROWS 24 & 25 ARE INOPERATIVE. R & R BATTERY PACK. CEILING EMER LIGHTS AT ROWS 24 & 25 OPERATIONALLY CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,068 hrs · 33,629 cycles

EMERGENCY POWER LIGHTS FROM ROW 21 - 31 VERY DIM WHEN POWERED BY BATTERY PACK AB5-3. R & R BATTERY PACK AB5-3. LIGHTS OPERATIONALLY CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,068 hrs · 33,629 cycles

EMERGENCY POWER LIGHTS FROM ROW 3 - 19 VERY DIM WHEN POWERED BY BATTERY PACK AB5-1. R & R BATTERY PACK AB5-1. LIGHTS OPERATIONAL CHECKED NORMAL.

Part: HOUSING — CRACKED (FUEL SYSTEM) · airframe 62,937 hrs · 33,539 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CTR TANK FUEL BOOST PUMPS NOT FEEDING FROM CTR TANK. CTR LOW PRESS LIGHT ILLUMINATED. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07, DIFFERENTIAL PRESS SWITCHES S1-266 & S1267 IAW AMM 28-41-01 & CTR TANK VOLUTE & VOLUTE HOUSING IAW AMM 28-20-07. SEE ALSO AALA20150907002, AALA20151005002, AALA20151005003 & AALA20151005005.

Part: PUMP — FAULTY (FUEL BOOST) · airframe 61,937 hrs · 33,539 cycles

DURING CLIMB, CTR TANK FUEL BOOST PUMPS NOT FEEDING FROM CTR TANK. CTR LOW PRESSURE LIGHT ILLUMINATED. DIVERTED, EMERGENCY DECLARED, & LANDING UNEVENTFUL. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07, DIFFERENTIAL PRESS SWITCHES S1-266 & S1267 IAW AMM 28-41-01 & CTR TANK VOLUTE & VOLUTE HOUSING IAW AMM 28-20-07.

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 62,937 hrs · 33,539 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CTR TANK FUEL BOOST PUMPS NOT FEEDING FROM CTR TANK. CTR LOW PRESS LIGHT ILLUMINATED. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07, DIFFERENTIAL PRESS SWITCHES S1-266 & S1267 IAW AMM 28-41-01 & CTR TANK VOLUTE & VOLUTE HOUSING IAW AMM 28-20-07. SEE ALSO AALA20150907002, AALA20151005003, AALA20151005004 & AALA20151005005.

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 62,937 hrs · 33,539 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CTR TANK FUEL BOOST PUMPS NOT FEEDING FROM CTR TANK. CTR LOW PRESS LIGHT ILLUMINATED. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07, DIFFERENTIAL PRESS SWITCHES S1-266 & S1267 IAW AMM 28-41-01 & CTR TANK VOLUTE & VOLUTE HOUSING IAW AMM 28-20-07. SEE ALSO SEE ALSO AALA20150907002, AALA20151005002, AALA20151005004 & AALA20151005005.

Part: VOLUTE — FAULTY (FUEL SYSTEM) · airframe 62,937 hrs · 33,539 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CTR TANK FUEL BOOST PUMPS NOT FEEDING FROM CTR TANK. CTR LOW PRESS LIGHT ILLUMINATED. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07, DIFFERENTIAL PRESS SWITCHES S1-266 & S1267 IAW AMM 28-41-01 & CTR TANK VOLUTE & VOLUTE HOUSING IAW AMM 28-20-07. SEE ALSO AALA20150907002, AALA20151005002, AALA20151005003 & AALA20151005004.

Part: WIRE — SHORTED (PRESSURE SWITCH) · airframe 60,870 hrs · 32,885 cycles

BOTH PACKS FAILED AFTER TAKEOFF. UNABLE TO PRESSURIZE. EMERGENCY DECLARED. LANDING UNEVENTFUL. FOUND LT & RT DIFFERENTIAL PRESSURE SWITCH WIRES SHORTED TO GROUND. REPAIRED WIRES IAW SWPM 20-10-01. OPS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 60,844 hrs · 32,874 cycles

FORWARD CARGO DOOR FWD SIDE OF DOOR BOTTOM STOP IS CRACKED. R & R CARGO DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 60,844 hrs · 32,874 cycles

AFT SIDE OF FWD CARGO DOOR BOTTOM DOOR STOP IS CRACKED. R & R CARGO DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: CASTING — CRACKED (CARGO DOOR) · airframe 60,844 hrs · 32,874 cycles

FORWARD SIDE OF AFT CARGO DOOR LOWER DOOR STOP CASTING CRACKED. R & R CASTING IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 60,844 hrs · 32,874 cycles

FORWARD CARGO DOOR FWD SIDE OF DOOR SECOND FROM BOTTOM STOP IS CRACKED. R & R CARGO DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 60,844 hrs · 32,874 cycles

FORWARD CARGO DOOR FWD SIDE OF DOOR CTR STOP IS CRACKED. R & R CARGO DOOR STOP IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,844 hrs · 32,874 cycles

AFT ACCESSORY CRACK IN FRAME AT FS 1510 AT LONGERON 3 RT. INSTALLED DOUBLER IAW SRM 53-01-00-001.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,844 hrs · 32,874 cycles

AFT ACCESSORY CRACK IN SHEAR TIE ON FWD SIDE OF FRAME AT FS 1380 ABOVE LONGERON 14 RT. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-20.

Part: FORMER — CRACKED (LT WING) · airframe 60,641 hrs · 32,745 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WC 57-98-05.

Part: FORMER — CRACKED (RT WING) · airframe 60,641 hrs · 32,745 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WC 57-98-06.

Part: GENERATOR — OVERHEATED (LT ENGINE) · airframe 59,734 hrs · 32,241 cycles

LEFT CONSTANT SPEED DRIVE TEMP WENT TO THE RED LINE. DISCONNECTED CONSTANT SPEED DRIVE IAW CHECKLIST. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG GEN.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 59,651 hrs · 32,189 cycles

PRIMARY & ALTERNATE TRIM FAILED DURING CRUISE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED PRIMARY & ALTERNATE TRIM MOTORS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 59,622 hrs · 32,171 cycles

PRIMARY & ALTERNATE STABILIZER TRIM INOPERATIVE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED BOTH DIGITAL FLIGHT GUIDANCE COMPUTERS & ALTERNATE TRIM MOTOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,116 hrs · 31,865 cycles

EMERGENCY LIGHTS FROM ROWS 18 TO 22. REPLACED BATTERY PACK FOR EMER LIGHTS FROM SEAT ROWS 18 TO 22. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 59,116 hrs · 31,865 cycles

EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. RESEATED CONNECTOR FOR EMER LIGHT AT SEAT 8D. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,351 hrs · 30,882 cycles

AFT AISLE OVERHEAD EMERGENCY LIGHTS STAY ON WITH AIRCRAFT POWER REMOVED & SWITCH OFF. REPLACED AFT AISLE EMERGENCY LIGHT BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,349 hrs · 30,880 cycles

MID CARGO DOOR AFT DOOR STOP CASTING CRACKED. INSTALLED MID CARGO DOOR IAW MM 52-31-00-4.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,349 hrs · 30,880 cycles

FWD CARGO DOOR AFT DOOR STOP CASTING CRACKED. INSTALLED FORWARD CARGO DOOR IAW AMM 52-31-00-4.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 55,241 hrs · 29,667 cycles

RIGHT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

CORROSION AFT CARGO DOOR JAMB BEAM FROM STATIONS 1155 TO 1212. INSTALLED DOUBLER ON AFT CARGO DOOR BEAM PER AARD 53-10-00-3.

Part: CASTING — CRACKED (SPOILER) · airframe 53,512 hrs · 28,690 cycles

GROUND SPOILER ACTUATOR CASTING IS CRACKED. INSTALLED DOUBLER PER AARD 57-20-00-15.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

FUSELAGE CRACKED IN AFT HINGE CUTOUT OF RIGHT AFT NOSE LANDING GEAR DOOR. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 62.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

DENT AND SCRATCH IN FUSELAGE SKIN AT STATION 207 ABOVE LONGERON 11 LEFT. INSTALLED DOUBLER PER SRM 53-04-03.

Part: STRAP — GOUGED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

GOUGES ON STRAP, ABOVE 28 RIGHT BETWEEN STATIONS 429 AND 434. NEW STRAP INSTALLED PER AARD 51-10-00-5 AND BOEING DRAWING 5910142.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

RIGHT CUSP HAS CORROSION FROM STATIONS 845 TO 864. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

DAMAGED AREA LEFT SUBFLOOR AT STATION 198 LEFT BUTTLINE 44. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

LEFT CUSP CRACKED AT STATION 874. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

CORROSION ON THE BOTTOM OF THE LEFT CUSP STATIONS 756 TO 760. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

LEFT CUSP SHEET HAS CORROSION FROM STATIONS 1136 TO 1174. INSTALLED CUSP SHEET SPLICE PER BOEING DRAWING SG09530019.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

RIGHT CUSP HAS CORROSION FROM STATIONS 905 TO 927. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

RIGHT CUSP DAMAGED AT STATION 1004 BELOW NUMBER 5 SEAT TRACK. REMOVED DAMAGE AND INSTALLED CUSP REPAIR DOUBLER AT RIGHT STATION 1004 PER AARD 53-20-00-16.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

FUSELAGE AFT LAVATORY SERVICE PANEL HAS CORROSION AT BOTTOM DOOR LANDING. INSTALLED A TITANIUM REPAIR DOUBLER PER EA MD80-53-023696.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

CORROSION ON THE BOTTOM OF THE RIGHT CUSP AT STATIONS 735 TO 740. INSTALLED DOUBLER ON RIGHT CUSP AT STATION 735 PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

THE 1510 CANT FRAME CRACKED AT TAIL CONE ALIGNMENT PIN ABOVE LEFT UPPER TAIL CONE LATCH. INSTALLED DOUBLER AT 1510 CANT FRAME LEFT PER EA MD80-53-023694.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

CORROSION FOUND UNDER G1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

CORROSION ON SUBFLOOR AT STATION 215 RIGHT BUTTLINE 56. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

TOP OF LEFT CUSP CORRODED FROM STATIONS 453 TO 456. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRAP — CRACKED (FUSELAGE) · airframe 53,512 hrs · 28,690 cycles

STRAP IS CRACKED AT STATION 208 LONGERON 11 LEFT. INSTALLED REPAIR STRAP AT FORWARD ENTRY AREA AT STATION 208 PER AARD 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

LEFT TOP CUSP STATIONS 415 TO 417 CORRODED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,512 hrs · 28,690 cycles

FORWARD CARGO LOWER DOOR PAN CORRODED, STATIONS 376 TO 417 AT LONGERON 28 RIGHT. SPLICED IN NEW SECTION OF FORWARD CARGO DOOR PAN PER SRM 53-05-00.

Part: A/C PACK — DIRTY (AC BAY) · airframe 50,857 hrs · 27,148 cycles

ORD - FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN AND COCKPIT CREW REPORTED ACRID FUMES. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN. NO ADDITIONAL ODORS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MOUNT BRACKET — DAMAGED (LT MLG) · airframe 50,852 hrs · 27,144 cycles

BNA - CREW REPORTED LANDING GEAR DOORS UNSAFE LIGHT ILLUMINATED. QRH ACCOMPLISHED BUT IDICATION DID NOT CLEAR. EMERGENCY DECLARED FLIGHT LANDED BNA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GEAR DOOR SENSOR MOUNT BRACKET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,266 hrs · 26,264 cycles

FRAME CRACKED AT STATION 1418 LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,266 hrs · 26,264 cycles

LEFT AFT NOSE WHEEL WELL DOOR AFT HINGE CUTOUT CRACKED BEYOND ROUTED OUT AREA. INSTALLED DOUBLER PER SRM 53-05-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,266 hrs · 26,264 cycles

FRAME CRACKED STATION 1418 LONGERON 2 RIGHT. INSTALLED DOUBLER PER SRM 53-03-00.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 45,641 hrs · 24,243 cycles

PORTABLE EMERGENCY LIGHT B5-29 NO ARM LIGHT. INSTALLED LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,641 hrs · 24,243 cycles

EMERGENCY LIGHT BATTERY PACK HAS NO POWER. REPLACED BATTERY PACK AND CHECKED PER MM 33-53-00-6 AND CARD 4289.

Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 45,639 hrs · 24,242 cycles

GROUND SPOILER CASTING CRACKED ON INBOARD SIDE AT ACTUATOR FORWARD MOUNT (LEFT WING). REMOVED AND REPLACED GROUND SPOILER FITTING PER SRM 51-01-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 45,283 hrs

LGA - EMERGENCY LIGHTS AT FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD LAVATORY.

Part: LIGHT — INOPERATIVE (CABIN) · 43,538 cycles

LGA EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: STRUT — INOPERATIVE (NLG) · airframe 42,312 hrs

DFW INFLIGHT T1033/21FEB, NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. NOSE GEAR STRUT BOTTOMED OUT DURING TAXI TO GATE. ACCOMPLISHED NOSE LANDING GEAR SHOCK STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISLODGED (EMERGENCY LIGHTS) · airframe 42,122 hrs

LGA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 42,040 hrs

LGA - EMERGENCY EXIT SIGN LIGHT AT AFT CABIN DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DEFLECTOR — BROKEN (NLG)

ORD - RED GEAR LIGHT ON IN FLIGHT WITH GEAR HANDLE UP. UNABLE TO RETRACT GEAR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. FOUND BROKEN SPRAY DEFLECTOR. REPLACED SPRAY DEFLECTOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY PATH LIGHTING FORWARD AND AFT SECTION INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY PATH LIGHTING FORWARD AND AFT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY PATH LIGHTING FEED FROM AFT BATTERY FORWARD INOPERATIVE. REPLACED CHARGERS/CONTROL MODULES FOR EMERGENCY PATH LIGHTING FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,740 hrs · 15,187 cycles

THE L1 DOOR EMERGENCY PORTABLE LIGHT, THE AFT FLIGHT ATTENDANT SEAT CEILING LIGHT JUST FWD OF RT LAV, AND THE FLOOR EGRESS LAMP AT SEAT ROWS 6 AND 9, WERE ALL INOPERATIVE. REPLACED THE PORTABLE LIGHT, REPLACED THE BATTERY PACK AT AFT LAV, AND REPLACED BOTH EGRESS LIGHT LAMPS.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 28,660 hrs · 15,137 cycles

THE CABIN ROW 22 EGRESS LIGHTS WERE INOPERATIVE AND HAD A BROKEN TRACK COVER. REPLACED THE COVER AND RECONNECTED THE EGRESS LIGHT CONNECTOR.

Part: BATTERY — DISCHARGED (ROW 28) · airframe 22,145 hrs · 11,359 cycles

THE AFT GALLEY DOOR EMERGENCY LIGHT AND THE EGRESS LIGHTING AFT OF CABIN ROW 28 WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY FOR ROW 28. CHECK-C 6-30-00 MCI.

Part: SKIN — GOUGED (LT ELEVATOR) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT THE LT ELEVATOR HAD LOWER SKIN GOUGED AND CRACKED, ALSO L/E CAP DENTED. REPAIRED PER ARA 16727 AND BALANCED PER SRM 55-20-2 PAGE 17. ---CLOSED---

Part: FRAME — CRACKED (RT MLG WW) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT IN THE RT WHEEL WELL, THE REAR O/B UPPER CORNER OF THE WHEEL WELL FRAME WAS CRACKED. STOP DRILLED CRACK. ACCOMP HIGH FREQ EDDY CURRENT PER NDT 51-00-03 PART 6. REPAIRED PER SRM 53-01, PAGE 10 FIG 2.

Part: WEB — DAMAGED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND MEMBRANE UNDER FLOOR PANEL 3A I/B AFT CORNER HAD DAMAGE. THE MEMBRANE WAS CORRODED AT STA 200 I/B OF RIGHT FWD SERVICE DOOR. REPLACED MEMBRANE PER SPM 6-70-01 ITEM 4A-2, AND REF SRM 53-14-1, FIG 11. TREATED PER SRM 51-10-3 AND SEALED PER SRM 51-20-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CRACK IN FLOOR MEMBRANE AT LONGERON 18R, STA 1293 TO 1297. REMOVED MEMBRANE AND REPLACED WITH NEW PER SRM 53-05, PAGES 361 TO 372.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE FLOOR AREA ON RT SIDE BETWEEN FORMER STA 1155 RT AND 1174 RT, UNDER O/B RT SEAT TRACK HAD CORROSION, AND UNDER RIVET HEADS. REMOVED CORROSION AND REPAIRED FLOOR MEMBRANE BETWEEN STA 1155R AND 1174 PER SRM 53-01, FIG 4 PAGE 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE FLOOR AREA ON RT SIDE BETWEEN FORMERS AT STA 1136R AND 1155R, AND UNDER RT SEAT TRACK HAD CORROSION AROUND RIVETS. REPAIRED PER SRM 53-01-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, CHAIR TRACK NUMBER 5 HAD LIGHT CORROSION AND WORN SPOTS AT STA 1297 TO 1309. CORROSION GROUND BEYOND LIMITS. REPLACED TRACK AT STA 1297 TO 1309, X44-00. SPLICED WITH SPLICE (P/N 17-9492), PLATE 17-9493 AND BLOCK 16-0795. TRACK INSTALLED WITH NAS 6233 BOLTS PER SRM 53-05 FIG 4F.

Part: WEB — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON AND UNDER FLOOR MEMBRANE AT REAR GALLEY DOOR AREA, STA 1136 TO 1174. REPLACED MEMBRANE PER DRAWING 9930612, SRM 51-30-5 AND 51-30-2, AND SPM 6-70-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE AREA BETWEEN STA 1212 AND 1231 AT LONGERON 18R WAS CORRODED. REMOVED CORROSION DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 53-01, PAGE 18 AND 22.

Part: WEB — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE 18L BETWEEN STA 1136 AND 1117. REPLACED MEMBRANE PER DRAWING 9930612 AND SRM 51-30-5, 51-30-5, AND SPM 6-70-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CRACK IN FLOOR MEMBRANE AT LONGERON 18R STA 1277. REMOVED MEMBRANE AND REPLACED WITH NEW PER SRO 9530205-11 PER SRM 53-05, PAGE 361 TO 371.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE FLOOR SUPPORT AT STA 168 TO 200, RT BODY LINE 12 AND 60 HAD CORROSION. FABRICATED NEW SUPPORTS AND EXTRUSION PER SAMPLE AND INSTALLED PER SPM 6-70-1 AND SRM 51-30-02. TREATED AND SEALED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND AFT CARGO, RT CARGO TIE DOWN TRACK WITH CORROSION PITTING IN CENTER AND ON FLANGES AT STA 1211 TO 1320. REMOVED CORRODED TIE DOWN TRACK AND INSTALLED NEW TIE DOWN TRACK PER SPM 6-70-01, PAGE 3B AND DRAWING 5936663.

Part: SUPPORT BRACKET — PUNCTURED (RT WING) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE RT WING T/E BUTE DOOR SUPPORT RAIL, INBOARD RIGHT T/E HAD HOLE PUNCTURED IN IT. MADE BEAM (P/N 5936844-7), CLIP (5936844-13), CLIP (5936814-15) AND HEAT TREATED AND PAINTED PER DOUGLAS DRAWING 5936844. MADE CLIP (P/N 5936824-7) PER DRAWING 5936824. MADE INTERCOSTAL PER SPM 6-70-01 PAGE 2 AND SRM 57-23-3 PAGE 6. INSTALLED PER DRAWING 5936844 AND 5936824.

Part: BEAM — CORRODED (THRESHOLD) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT IN THE AFT CARGO, FOUND CORROSION IN THRESHOLD BEAM AREA, BETWEEN BOTTOM CARGO DOOR STOPS. REMOVED CORROSION PER SPM 6-80-01 PAGE 1, ITEM 3A, B, PAGE 2 AND PAGE 3. REMOVED CORRODED BEAM PER SPM 6-70-01 PAGE 3 DRAWING 5930483, SRM 51-60-0 PAGE 15, SRM 51-60-0 PAGE 36, SRM 51-60-0 PAGE 8, AND SRM 51-30-4 PAGES 1 TO 11.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, THE MID CARGO DOOR JAMB AT APPROX LONGERON 24R HAD IMPACT DAMAGE WITH SHARP CORNER AND EDGE APPROX 20 INCHES UP FROM THRESHOLD PLATE, STA 693. BLENDED IMPACT DAMAGE ON MID CARGO DOOR JAMB PER SPM 53-05 PAGE 495 FIG 109. ALODINED PER SRM 51-10-3 PAGE 18 PARA 30. PRIMED PER SRM 51-10-3 PAGE 16.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION IN AFT CARGO THRESHOLD PLATE, STA 1212. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 ITEMS 3A AND B, AND PAGE 2 AND 3. REPAIRED PER SRM 53-01 FIG 4 SHEET 3, AND ARA 16728A DATED 5-26-00, SRM 51-60-0 PAGE 36, SRM 51-60-0 PAGE 8. CORROSION TREATED PARTS PER SRM 51 AND DRAWING 5910085 AND 5930483.

Part: WEB — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE ON RT SIDE NEXT TO STA 728 AROUND LIGHTNING HOLE. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 TO 3. MADE REPAIR PER SRM 53-01 FIG 4. INSTALLED RIVETS PER SRM 51-30-03.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND GROOVES WORN IN NUMBER 3 CHAIR TRACK STA 1041 TO 1072, 1147, 1240 AND 1260. CORROSION WAS AT STA 1058, 1072, 1079 TO 1136, 1200 AND 1226. REMOVED AND REPLACED CHAIR TRACK FROM PRODUCTION SPLICE AT STA 1032 TO STA 1261, PER SRM 53-05, PAGE 10G.

Part: SKIN — DAMAGED (LT WING) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT ON LT WING LOWER SURFACE OF THE TRAILING EDGE, THE I/B FIXED FIBERGLASS PANEL HAD A HOLE IN IT. SANDED AREA AND INSTALLED 3 LAYERS OF FIBERGLASS LAYUPS AND SANDED SMOOTH PER SRM 51-70-1B, FIG 5.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION UNDER WATER LINE PLATE AT STA 160, RBL 50 AT O/B AFT CORNER. REPLACED MEMBRANE WITH NEW PART PER SPM 6-70-01, AND INSTALLED PER SRM 51-30-02. TREATED PER SRM 51-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, BETWEEN STA 1022 AND 1002. REPAIRED MEMBRANE PER SRM 53-01, PAGE 9 (TYPICAL DOUBLER REPAIR).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT AT STA 148, RBL 59. REMOVED CORROSION PER SPM 6-80-01. TREATED PER SRM 51-10-3 AND REINSTALLED PART PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 750 TO 731, AND STA 712 TO 731. CUT OUT CORRODED AREA AND REPAIRED PER SRM 53-01. TREATED AREA PER SRM 51-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CABIN CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 560 TO 579 AND STA 541 TO 522. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER 51-10-3. REPAIRED PER SRM 53-01 FIG 4 PAGE 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CABIN CORROSION ON MEMBRANE AT LONGERON 18R, STA 1098 TO 1079 AND STA 1098 TO 1117. CUT OUT CORROSION AND FABRICATED DOUBLER FROM 0.025, 7075-T6 MATERIAL. INSTALLED DOUBLER WITH 1422 SEALANT AND 2 ROWS OF FASTENERS PER SRM 53-01 FIG 4, SHEET 3 AND 4 PAGE 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, IN LT CABIN FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L STA 655 TO 674. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER SRM 51-10-3B. INSTALLED FASTENERS PER SRM 51-10-05.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, CHAIR TRACK HAD GOUGES AT STA 356 TO 389, RBL 22, AND AT STA 243 TO 313 RBL 22. REMOVED AND BLENDED GOUGES PER SRM 53-05, FIG 4B-1, AND SPM 6-80-01. PRIMED, SANDED AREA PER SRM 51-10-3.

Part: SPLICE PLATE — CRACKED (RT WING) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, ON RT WING, WING STA 164 L/E SPLICE PLATE WAS CRACKED AT BOLT HOLE. EDDY CURRENT INDICATED CRACK FROM 1 HOLE THRU ANOTHER HOLE TO EDGE PER PART 6-57-00-03 OF NDT MANUAL. FABRICATED AND INSTALLED WING L/E DOUBLER AT WING STA 164, PER SSRM 57-40-103.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 674 TO 693 AND STA 845 TO 826. REMOVED CORROSION PER SPM 6-80-01. TREATED SURFACES PER SRM 51-10-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT STA 1212 TO 1231 AT LONGERON 18L. REMOVED DAMAGED SECTION OF MEMBRANE, AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON ATTACH ANGLE AT FLOOR LEVEL OF EPC PANEL, AFT SIDE, STA 160L. REMOVED CORROSION PER SPM 6-80-01, PAGE 1 ITEM 2(A).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND CORROSION IN CHAIR TRACK AT RBL 22 AT THE FOLLOWING STATIONS: 363 TO 368, 237, 530 TO 460, 427 TO 462, 408 TO 420, 636, 788, AND 484 TO 503. REMOVED CORROSION PER SRM 51-10-3, 53-05 FIG 4B-1, AND SPM 6-80-01. PRIMED PER SRM 51-10-3.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CHECK-C MAINT, FOUND DOUBLER AT AFT CARGO DOOR STA 1300 TO 1231, LONGERON 29 TO 26R, WAS CORRODED. REMOVED CORROSION PER SPM 6-80-01, PAGE 1 ITEM 3, A, B PAGE 2 AND 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,081 hrs · 11,316 cycles

DURING CC 8C, FOUND A CRACK IN THE LOWER FUSELAGE AT LT AND RT SIDES OF THE SUPPORT INTERCOSTAL AT STATIONS 988, 5 INCHES LT SIDE AND 5 INCHES RT SIDE OF LONGERON 30 BETWEEN THE AFT END OF THE MAIN GEAR. INSTALLED REPAIR PER SRM 51-01 PG 1, FABRICATED PART PER SRM 6-70-01 DAC DRAWING 5936373, INSTALLED FASTENERS PER SRM 51-30-05, PRIMED AND PAINTED PER SRM 51-10-3B. CC8C 05-19-00 MCI.

Part: LENS — CRACKED (CABIN)

EGRESS LIGHT LENS AT MID CABIN CLASS DIVIDER CRACKED. REPLACED LIGHT LENS AC 04 01/29/2000 JFK.

Part: LIGHT — DISCONNECTED (ROW 11)

THE EGRESS LIGHTING AT SEAT ROW 11 WAS DISCONNECTED. REPLACED BROKEN TRACK LIGHTING COVER AND RECONNECTED THE LIGHT. CHECK-C 5-18-99 STL.

Part: BULB — FAILED (ROW 2,4,10&33)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 2, 4, 10, AND 33. REPLACED LAMP AT EACH LOCATION. CHECK-C 5-18-99 STL.

Part: HARNESS — WORN (ROW 15 & 16)

THE CABIN EGRESS LIGHTS TRACK COVERS WERE BROKEN AT ROWS 15 AND 16, CAUSING WIRES TO PULL OUT OF HARNESS. REPLACED HARNESS AND TRACK COVERS. CHECK-C 5-6-98 STL.

Part: COVER — CRACKED (CABIN)

STL - FLT 74 - THE EMERGENCY FLOOR LIGHTING STRIP AT ROW 1 WAS FOUND BROKEN. REPLACED EMERGENCY FLOOR LIGHTING STRIP AT ROW 1. CHECK-C 5-6-98 STL. ACFTR TT: 15,970 HOURS. ACFT TC: 8,193. (X)

Part: ENGINE — FAILED (LEFT)

AM - FLT 1508 - DURING CRUISE, VIBRATION OCCURED ON THE LEFT ENGINE. ENGINE SHUT DOWN. REPLACED LEFT ENGINE DUE TO FAILURE CAUSED BY BLUE ICE. (M)

Part: SLIDE — DEPLOYED (L1 DOOR)

STL - FLT 422 - WHILE AIRCRAFT WAS PARKED AT GATE, A VENDOR INADVERTENTLY DEPLOYED L-1 DOOR EMERGENCY ESCAPE SLIDE, WHICH FUNCTIONED PROPERLY. REMOVED AND REPLACED L-1 DOOR SLIDE, MFG P/N 100504-201, MANUFACTURED BY BF GOODRICH CO. (M)

Part: ENGINE — FAILED (NR 2)

STL - DURING DESCENT, SHUT DOWN NR 2 ENGINE, S/N 1213, DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES ON OIL SYSTEM CHIP DETECTORS. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME 22,333, ENGINE TOTAL CYCLES 11,261.

Part: BEARING — FAILED (NR 2 ENGINE)

STL - FLT 315 - INVESTIGATION OF NR 2 ENGINE, S/N 1213, SHUT DOWN DUE TO VIBRATION REVEALED THE NR 3 BEARING, MFG P/N 804061, RIVETS FRACTURED LIBERATING METAL PARTICLES INTO OIL SYSTEM. THE NR 3 BEARING WAS REPLACED AND ENGINE REPAIRED AND RETURNED TO SERVICE.

Part: CONTROL VALVE — FAILED (NR 2 PACK)

STL - FLT 463 - DURING CRUISE, AIRCRAFT CABIN PRESSURIZATION BLED OFF. REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE, MFG PN 396130-1-1. OPERATIONAL CHECK AND LEAK CHECK NORMAL. CHECK C-1D - 5-18-95 - MCI.

Part: ENGINE — BIRD STRIKE (RIGHT)

FLT NR 312 - SMF - AFTER TAKEOFF, SMOKE EMITTED INTO CABIN. FLIGHT RETURNED. FOUND RIGHT ENGINE HAD INGESTED A BIRD. REPLACED RIGHT ENGINE, S/N 3256. ENGINE OPERATION AND AIR CONDITIONING SYSTEMS OPERATION CHECKED NORMAL.

Part: COALESCER BAGS — CONTAMINATED (CABIN)

STL - FLT 176 - DURING CRUISE, EXPERIENCED SMOKE IN CABIN AND COCKPIT. TURNED OFF RIGHT SUPPLY HIGH PRESSURE BLEED AIR, SMOKE DISSIPATED. FOUND WATER SEPARATOR COALESCERS OIL CONTAMINATED, MFG PN 179460-8-1. REPLACED WATER SEPARATOR COALESCERS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL.

Part: OIL — OVERSERVICED (APU)

IND - FLT 444 - DURING CRUISE, SMOKE STARTED ENTERING CABIN. DESCENDED TO 8,000 FEET. FOUND APU OIL OVERSERVICED. SERVICED APU TO PROPER LEVEL AND REPLACED BOTH COALESCER BAGS, MFG P/N 22D10. AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-1A - 5-18-95 - MCI.

Part: STRUCTURE — LIGHTNING STRIKE (AIRFRAME)

STL - FLT 464 - DURING CRUISE, EXPERIENCED A POSSIBLE LIGHTNING STRIKE WITH ACCOMPANYING AIR NOISE AND SMOKE IN THE CABIN. ALL OPERATIONS AND INDICATIONS WERE NORMAL. PERFORMED LIGHTNING STRIKE/STATIC DISCHARGE CONDITION CHECK. CHECKED NR 1 ENGINE FOR POSSIBLE COMPRESSOR STALL, CHECKED TAIL COMPARTMENT AIR CONDITIONING SYSTEM. ALL CHECKS WERE FOUND TO BE NORMAL. CHECK C-1D - 5-18-95 - MCI.