N972DL

Part: SMOKE DETECTOR — INTERMITTENT (FWD LAVATORY) · airframe 75,038 hrs · 55,570 cycles

FORWARD LAV SMOKE DETECTOR INTERMITTLY SOUNDING. REPLACED F/C LAV SMOKE DETECTOR PER MD-88 AMM 26-13. SMOKE DETECTOR TESTS GOOD. (LP5428124)

Part: CHECK VALVE — BYPASSING (HYD SYSTEM) · airframe 75,028 hrs · 55,563 cycles

SHIP 972 - ATB - DUE TO NLG FAILED TO RETRACT, EXTENDED THE MLG AND RETURNED TO ATL, NO EMERGENCY DECLARED. CORRECTIVE ACTION. TROUBLESHOOTING IN PROGRESS. RESTRICTOR VALVE NO HELP. C/W NO-GO ODI PREVENTION. FOUND UPPER SIDE CHECK VALVE BYPASSING ON NLG HYDRAULIC SYSTEM T-FITTING. REPLACED UPPER CHECK VALVE. NOW CHECKS GOOD. SDR REPORTED DUE TO FACT THAT THE MCC NOTIFICATION MENTIONED A DECLARED EMERGENCY. (LP5428112)

Part: STIFFENER — CRACKED (NR 2 NACELLE) · airframe 74,977 hrs · 55,511 cycles

NUM 2 ENG NOSE COWL EXTERNAL AFT STIFFENER CRACKED AT 07:00 MKD INTERNAL FWD BULHHEAD STIFFENER CRACKED 206:00 MKD INTERNAL STIFFENER FASTENERS LOOSE AT 07:00 MKD. NUM 2 ENG NOSE COWL REPL AND INST ON AMDS CARD 7100-4682-RH COWL, NOSE, LT OFF 88-7110-9-0001 S/N OFF: 00082. (LP1362735)

Part: OIL FILTER — CLOGGED (LT ENGINE) · airframe 74,883 hrs · 55,435 cycles

SDR REPORTED DUE TO EMERGENCY DECLARED ACCORDING THE MCC NOTIFICATION - DESCENDING THRU 9000 FT, GOT "L OIL STRAINER CLOG" ON OAP. ALL OTHER ENG PARAMETERS REMAINED IN LIMITS. RAN QRH PROCD'R, REDUED THRUST ON LEFT ENG. TO KEEP LIGHT OUT ON OAP. REMOVED ENG OIL FILTER FOUND CARBON IN FILTER INSTALLED NEW OIL FILTER MD88 AMM 79-10 ADMS 7200-6468(988446)VT/S PER NO 60 ODI ATA 7934. C/W AMDS 7200-6468 STEP F, FILTER TO BE REMOVED FOR INSP. AFTER 75 HRS (LP5586512)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,281 hrs · 54,883 cycles

LT OVERWING EMERG EXIT DOOR LIGHT INOP. RELAMPED SAME PER AMM 33-53 OPS CK GOOD. (LP6256107)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,503 hrs · 54,203 cycles

ON WAKE UP CK FOUND ROW 31 AND AFT EMERGENCY LIGHTS INOP. REPLACED BATTERY, NO HELP PER AMM 33-53. REMOVED AND REPLACED POWER SUPPLY P/N RPS1B S/N 1093 OK:P/N 11-0049 S/N 8243 OFF. EMERGENCY LIGHTS CK GOOD. OK OFR SVC PER AMM 33-53. (LP5311048)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,094 hrs · 53,855 cycles

EMERGENCY LIGHTS INOP TO ROW 1A. FOUND SEVERAL LTS OUT IN F/C SECTION OF AIRPLANE/ REMOVED & REPLACED ASSOCIATED BATTERY PACK PER AMM 33-53. OPS NORMAL OK FOR SVC. (LP5001473)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,907 hrs · 53,711 cycles

LEFT AND RIGHT OVERWING EXIT LIGHTS WILL NOT TURN ON. REPLACED B5-49 OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK REF MD88 AMM 33-53-00. (LP0840106)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 72,907 hrs · 53,711 cycles

AFT CARGO COMPT: CORROSION IN C-3 DOOR JAMB. REMOVED AND REPLACED THE -9 SPACER REF MD88 SRM 53-05 PARA 140 FIG 123. (LP0831081)

Part: SKIN — WORN (AILERON TAB) · airframe 72,907 hrs · 53,711 cycles

RIGHT AILERON INBOARD TAB FIBER EXPOSE ON TOP SURFACE. REPLACED AILERON. REMOVAL STOCKNUMBER:88-2710-9-0011 SERIAL NUMBER:00240. (LP0829943)

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 72,860 hrs · 53,668 cycles

EMERG LIGHTS ROW 10 TO FIRST OVERWING DOOR INOP. INSTALLED DIOD ON BATTERY PACK @ 3CD OPS CHECK GOOD IAW MD88 AMM 33-55. (LP4755523)

Part: FASTENER — MISSING (LT WING TE FLAP) · airframe 72,867 hrs · 53,674 cycles

LEFT WING TRAILING FLAP & VANE BRACKET HARDWARE MISSING (3RD BRACKET FROM INBD). INSTALLED NEW HARDWARE IAW AMM 27-51-00. SDR REPORTED DUE TO POSSIBILITY THAT THE MISSING HARDWARE MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP4755522)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,817 hrs · 53,631 cycles

CABIN EMERGENCY LIGHT AT ROW 13 TO 23 INOP AND FROM 31 TO AFT EMERG EXIT DOOR ALSO INOP. FOUND CEILING EMERGENCY LIGHT IN FWD AND MID CABIN INOP ALSO. R/R BATTERY AT SEATS 2C, 4DC 25DE, AND 35ED. ALL EMERGENCY LIGHT OPS CK NORMAL REF AMM 33-51 A/C OK FOR SVC. (LP5000389)

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 72,587 hrs · 53,430 cycles

THE FLIGHT CREW PERFORMED AIR TURN BACK AFTER THE NR 1 ENGINE STALLED, ROLLED BACK, AND THEN DID NOT HAVE ANY THROTTLE RESPONSE. THE NR 1 ENGINE WAS SHUT DOWN BY FLIGHT CREW. MAINTENANCE FOUND TURBINE DAMAGE AND THE NR 1 ENGINE WAS REPLACED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,337 hrs · 53,207 cycles

L1 EMERGENCY LIGHT INOPERATIVE. FOUND THE BULB OUT. REPLACED THE BULB. OPS GOOD IAW AMM 33-50.

Part: PLATE — MISSING (TE FLAP FAIRING) · airframe 72,409 hrs · 53,263 cycles

RIGHT WING, INBD FLAP HINGE FAIRING WAS MSSING A PLATE. INSTALLED THE HINGE FAIRING PLATE IAW SECTION III, ERA 570416-14. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,073 hrs · 52,974 cycles

AFT UPPER OVERWING LT AND RT EMERGENCY LIGHT INOP. R&R BATTERY FOR AFT LT AND RT EMERGENCY LIGHT PER AMM 33-53. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,709 hrs · 52,659 cycles

EMERGENCY LIGHT AT PASSENGER SEAT 17D IS INOP. R&R EMERGENCY LIGHT ON SEAT 17D REF AMM 33-53. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,627 hrs · 52,586 cycles

FOUND CEILING EMERGENCY LIGHTS BETWEEN ROWS 14-30 INOPERATIVE, ALSO ALL FOUR OVERWING EXIT IDENTIFIERS INOPERATIVE. TROUBLESHOT IAW SSM 33-51. FOUND BATTERY WITH DEAD CELL AT B5-102. POWER SUPPLY OK. REPLACED THE BATTERIES IAW AMM 33-50. ALL EMERGNECY LIGHTS NOW OP NORMAL. OK FOR SERVICE.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 71,236 hrs · 52,281 cycles

5510-01074-11 STEP 14 PERFORMED LFEC INSPECTION OF UPPER RT AFT SKIN PANEL. CRACK INDICATION ACQUIRED CRACK LENGTH 1/4" MARKED. STOP DRILLED CRACK REF SERVICE REWORK DRAWING SR09550028 NOTE 43 INSTRUCTIONS. C/W BHEC OF STOP DRILL- CRACK DOES NOT EXTEND PAST STOP DRILL PER SERVICE REWORK DRAW SR 09550028 NOTE 43 STEP 4. C/W 5510-01074-11 INSTALLED TEMPORARY REPAIR PER 5510-0107424 SERV DRAWING SR 09550028 NOTE 43.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,087 hrs · 52,159 cycles

EMERGENCY LIGHTS ON CEILING PANELS FROM ROW 14-20 INOP. EXTERNAL EMERGENCY LIGHTS INOP. REPLACED PART NUMBER AD4002P FOR CEILING EMERGENCY LIGHTS. REMOVED AND REPLACED PART NUMBER AD-3110 FOR EXTERNAL EMERGENCY LIGHTS REF AMM 33-53-00. OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 70,904 hrs · 52,007 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS BROKEN AT 34DE. REPAIRED WIRING. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 70,567 hrs · 51,739 cycles

TWO DENTS AT THE NEW WIFI DOUBLER EDGE. THE DENTED REGION WAS CUTOUT AND A COMBINED DOUBLER WAS MADE AND INSTALLED FOR THE REGION PER ERA 552781-14 ON 18NOV16. THE REPAIR WAS CLASSIFIED AS MAJOR AND IS THEREFORE SDR REPORTABLE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,271 hrs · 50,694 cycles

AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: ACCESS PANEL — DELAMINATED (LT WING) · airframe 68,009 hrs · 49,757 cycles

LEFT WING DELAMINATED FWD BOOST PUMP SECONDARY ACCESS COVER. REPAIRED IAW ER/A 530866-14AD MA REV.ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 1271) · corrosion level 2 · airframe 68,009 hrs · 49,757 cycles

AFT CARGO BAY CORROSION ON LT CARGO TRACK AT BS 1271. CARGO TRACK WAS REPLACED. IAW SRM 51-30-1 AND SRM 51-30-5.

Part: PANEL — CRACKED (RT WING SLAT) · airframe 68,029 hrs · 49,771 cycles

RIGHT WING SLAT PANEL WAS FOUND CRACKED XOS=240. THE SLAT PANEL WAS REMOVED IAW AMM 27-80-01 AND A NEW PANEL WAS INSTALLED.

Part: PANEL — BULGED (RT WING) · airframe 67,580 hrs · 49,413 cycles

WING PANEL FORWARD OF INBD SPOILER ON RT WING BULGING IN FLIGHT. REMOVED PANEL. INSTALLED NEW PANEL IAW DWG 5936824-508.

Part: CONNECTOR — BROKEN (CABIN) · airframe 67,118 hrs · 49,056 cycles

SEAT 34DE EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT CONNECTOR BROKEN AT SEAT 34DE. REPLACED CONNECTOR IAW SWPM 20-90-03. OPS CHECKS GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,200 hrs · 48,391 cycles

THE CREW OF FLIGHT 2198, FOUND AN EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 17. SAV MAINTENANCE REPLACED THE LIGHT ASSY AT SEAT 17 AND IT CHECKED OK.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,316 hrs · 47,740 cycles

CREW ON FLT 907 REPORTED THAT THE ESCAPE SLIDE AT L1 DOOR DISLODGED WHILE AT GATE BUT DID NOT DEPLOY. MAINTENANCE R & R THE EMERGENCY ESCAPE SLIDE.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,184 hrs · 47,653 cycles

ACFT MAINTENANCE SLIDE BUNDLE AT 1L DOOR LOOSE. MAINTENACE REPLACED L-1 DOOR SLIDE IAW JIC 2561-4964. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,998 hrs · 47,510 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 63,772 hrs · 46,674 cycles

MAINTENANCE FOUND TWO PINS PULLED ON L1 DOOR SLIDE. THE SLIDE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,749 hrs · 46,656 cycles

MAINTENANCE FOUND THE RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE DURING TEST. MAINTENANCE REPLACED THE RT WING EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-53. LIGHT TEST OPS CK GOOD. LP6712456.

Part: LIGHT — INOPERATIVE (SEAT 16DE) · airframe 63,425 hrs · 46,433 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 16DE WAS INOPERATIVE. MAINTENANCE INSTALLED A NEW LIGHT ASSEMBLY AND OPS CHECKED GOOD.

Part: ATTACH FITTING — MISSING (TAILCONE RELEASE) · airframe 62,840 hrs · 46,015 cycles

MAINTENANCE FOUND A MISSING CLIP ON THE INTERNAL RELEASE HANDLE OF THE TAILCONE. MAINTENANCE INSTALLED A CLIP.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,832 hrs · 46,010 cycles

CORROSION ON LT HORIZONTAL STABILIZER. REPAIRED IAW SRM 55-03, PAR 30 AND ER/A 529348-14, REV ORIGINAL FIG 32 AND ETI-88-14-192, REV 2.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,832 hrs · 46,010 cycles

CORROSION ON RT HORIZONTAL STABILIZER SKIN. REPAIRED IAW SRM 55-03D, PAR 30, FIG 32 AND EA/A 529348-14 REV ORIGINAL AND ETI-88-14-190, REV. 2.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 62,832 hrs · 46,010 cycles

CRACKED PAN UNDER MID CARGO DOOR FWD ANGLE BETWEEN BEAMS 1 AND 2 IAW ORNRC 79 ACFT ZONE 100.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 62,790 hrs · 45,976 cycles

CORROSION AND SCRATCHES ON HOLES OF LT HORIZONTAL STABILIZER UPPER MID PLATE. MRB 55-060-02. REPAIRED IAW ER/A 529052-14.

Part: WEB — CORRODED (BS 1150-1155) · airframe 68,009 hrs · 49,757 cycles

COROSION ON FWD DOOR FRAME WEB BS 1150-1155, OVER LONGERON 26R . THE WEB WAS REPAIRED IAW ERA.

Part: PLACARD — DAMAGED (CABIN) · airframe 62,790 hrs · 45,976 cycles

EXIT PLACARD DAMAGED. REPLACED EXIT PLACARD.

Part: PRESSURE BLKHD — CORRODED (BS 1338) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FWD PRESSURE DOME SPLICE DOUBLER BS 1338 BETWEEN LONGERONS 29L - 29RT. FOUND TO BE OUT OF LIMITS IAW SRM 53-01. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. REPAIRED IAW SRM 53-14-3, FIG 7 AND 51-10-3, PAR 14 AND 21. UT, WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PARAGRAPH 5, FIG 3.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACKED PAN INTERNAL STRUCTURE BS 637 AND BEAM NR MID CARGO DOOR. CRACKED PAN WAS STOPPED AND DRILLED IAW SRM 52-03, FIG 8, SH (1) TO (7), DOUBLER WAS FABRICATED IAW SRM 52-03, FIG 8 HEAT TREAT ON NEW DOUBLER AND AREA WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2. SEAL RETAINER WAS INSTALLED IAW SRM 51-30-1.

Part: SKIN — CORRODED (BS 1102) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING ON STA Y= 1102 L28R . AREA WAS REPAIRED IAW SRM 53-04, FIG 57.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 62,790 hrs · 45,976 cycles

CRACKS ON THE HORIZONTAL STABILIZER RT REAR CAP. RIGHT UPPER SPAR CAP WAS REMOVED, NEW UPPER SPAR CAP WAS DRILLED AND ADJUSTED SPAR CAP WAS TREATED AND PAINTED UPPER SPAR CAP WAS INSTALLED IAW DWG SR09550030, REV C AND SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,790 hrs · 45,976 cycles

CRACKED CHANNELS ON FLOOR PANELS. FLOOR PANELS WERE REPAIRED AND REPLACED IAW SRM 51-10-4 AND 51-10-3, PAR 14 & 21, SRM 51-70-1, PAR 10, 51-10-3, PAR 14 & 21 AND 53-05 FIG 131B.

Part: TEE FITTING — CORRODED (BS 1380) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FRAME TEE FITTING BS 1380, LONGERON 24L, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. FRAME WAS REPLACED IAW SRM 51-30-2, 51-30- 5 AND DWG 9912246, REV CE, UT, WAS ACCOMPLISHED IAW NDT SRM 04-00-07, PAR 5, FIG 3.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION FOUND ON CARGO TRACK BS 1003-1155. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-41, 51-10-3 AND PAR 14, 21; 51-30-2, 51-30-1, 53-05, FIG 4C, NDT SPM 04-00-07, PAR 5, FIG 3.

Part: TAB — DAMAGED (RUDDER) · airframe 62,790 hrs · 45,976 cycles

DAMAGED FLAME SPRAY ON LT/RT SURFACES OF RUDDER CONTROL TAB. FLAME SPRAY ON LT/RT SURFACES OF RUDDER CONTROL TAB WERE REPAIRED IAW SRM 51-70-1AD, PAR 23B.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON AFT CARGO BAY DOOR FRAME UPPER BEAM BETWEEN BS 1155 - 1174. DOOR FRAME UPPER BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 21-14-38.

Part: PAN — CRACKED (L1 DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACKED AFT PAN BETWEEN UPPER PAN AND BEAM 1 AT L1 DOOR STRUCTURE. REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-4.

Part: PAN — CRACKED (L1 DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACKED FWD PAN BETWEEN UPPER PAN AND BEAM 1 AT L1 DOOR STRUCTURE. PAN REPLACED IAW SRM 51-30-1, 51-30-2, & 51-30-4.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 62,790 hrs · 45,976 cycles

CRACKED PAN FWD EDGE BEHIND STOP NR 5 AT MID CARGO DOOR. STOP NR 5 WAS REMOVED IAW SRM 51-30-7, CRACK WAS STOPPED IAW SRM 52-05, FIG-50 REPAIR DOUBLER WAS FABRICATED IAW SRM 52-05, FIG 50. REPAIR DOUBLER AND REWORKED AREA WERE TREATED AND PAINTED IAW SRM 51-10-3. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: BEAM — CRACKED (L1 DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACKED BEAM FWD AND AFT ENDS IN L1 DOOR STRUCTURE. BEAM STOPPED DRILLED IAW SRM 52-05. DOUBLERS FABRICATED IAW SRM 52-05. TREATED AND PAINTED IAW SRM 51-10-3. DOUBLERS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL, NR 1460C ON RT WING. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,790 hrs · 45,976 cycles

DAMAGED PAINT COAT AND METALIZED COATING ON RUDDER SKIN BOTH SIDES. METALIZED COATING ON RUDDER SKIN BOTH SIDE WERE REPAIR IAW SRM 51-70-1AD, PAR 23B.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 62,790 hrs · 45,976 cycles

CORROSION ON HORIZONTAL STABILIZER LOWER SKIN STA XH=27. BHFE INSPECTED IAW NDTPM 6.10.01.003 AND NO CRACKS FOUND. HORIZONTAL STABILIZER LOWER SKIN REPAIRED IAW SRM 55-03D, PAR 30 FIG 32.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 62,790 hrs · 45,976 cycles

CORROSION ON HORIZONTAL STABILIZER LOWER SKIN STA XH=-27. HFEC INSPECTED IAW NDTSPM 06.10.01.003, NO CRACKS NOT FOUND. REPAIRED IAW SRM 55-030, PAR 30, FIG 32. M

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL NR 1363C AT LT WING ALSO SETTLEMENT AREA. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-21-2A AND REPLACED.

Part: RETAINER — CRACKED (BS 1401) · airframe 62,790 hrs · 45,976 cycles

CRACKED RETAINER ON BS 1401. RETAINER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 5913596.

Part: CUSP WEB — CORRODED (BS 1041-1079) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB, BS 1041-1079 BETWEEN X-54 AND X-60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON CONUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1436C ON RT WING. CORROSION REMOVED AND WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A. REPLACED.

Part: ANGLE — CRACKED (BS 905) · airframe 62,790 hrs · 45,976 cycles

CRACKED ANGLE, BS 905 X-44 Z-8 TO Z-10. ANGLE REPLACED DWG 9923417, REV B. IAW SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 170) · airframe 62,790 hrs · 45,976 cycles

CRACKED INTERCOSTAL BS 170. INTERCOSTAL WAS REPAIRED IAW SRM 53-01 FIG 2, SRM 51-10-3 PAR 14, 21 ARM 51-30-2, SRM 51-30-5.

Part: SKIN — CORRODED (BS 750-769) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FUSELAGE SKIN BETWEEN BS 750 AND 69 AND LONGERONS 27 AND 28RT AT MID CARGO COMPARTMENT, H1L1-SM, CARD 144, ZONE 201. SKIN WAS REPAIRED IAW SRM 53-04 FIG 57, SRM 51-30-2, SRM 51-10-2, PAR 14, 21.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK HOLES, 2 EA OF FUEL ACCESS DOOR NR 1371C. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPAIRED IAW SRM 51-10-3, PARA 21.

Part: FITTING — CRACKED (BS 1320) · airframe 62,790 hrs · 45,976 cycles

CRACKED FITTING BS 1320 LAVATORY AREA,. FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND DWG 9915563-33, REV P.

Part: FLOOR PANEL — WORN · airframe 62,790 hrs · 45,976 cycles

WORN FLOOR PANEL IN AFT ACCESSORY COMPARTMENT. REPLACED IAW ER/A 497244-14, MA REV.

Part: CUSP WEB — MISREPAIRED (BS 1008-1014) · airframe 62,790 hrs · 45,976 cycles

MISINSTALLED REPAIR DOUBLER ON LT CUSP WEB BETWEEN BS 1008 AND 1014 X 60 AND X 52. REPAIR WAS REPLACED IAW SRM 51-30-2, 53-05, FIG 131A-13. 51-10-3, PAR 21 AND 14-51-20-0 PAR -8.

Part: FRAME — CORRODED (BS 1170) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FRAME BS 1170 BETWEEN LONGERONS 18 - 21L IN AFT CARGO BAY LEFT UTILITARY TUNNEL. CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3, PARS 14, 21 AND 26. FOUND TO BE OUT LIMITS IAW SRM 53-01, FIG 1.

Part: ANGLE — CRACKED (BS 1485 FRAME) · airframe 62,790 hrs · 45,976 cycles

CRACKED ANGLE ON BS 1485 FRAME AT 11 O`CLOCK POSITION. ANGLE WAS FABRICATED IAW DWG 9911842-111, REV DH, SRM 51-30-5, 51-10-2, 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 807) · airframe 62,790 hrs · 45,976 cycles

CRACKED CUSP WEB BS 807, X-47. CRACK WAS DRILL STOPPED, DOUBLER WAS FABRICATED , TREATED, PAINTED AND DOUBLER WAS INSTALLED IAW SRM 53-01, FIG 2, SHT 3 AND 51-10-3 PAR 14 AND 21.

Part: INTERCOSTAL — CRACKED (BS 1022-1041) · airframe 62,790 hrs · 45,976 cycles

CRACKED INTERCOSTAL, BS 1022 - 1041 BETWEEN X=22 AND X=-22 . INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-30-5, PAR 8 AND 51-30-2.

Part: CUSP WEB — CRACKED (BS 807) · airframe 62,790 hrs · 45,976 cycles

CRACKED CUSP WEB, BS 807 X-54. CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 3 AND 51-10-3, PAR 14, 21, 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL ACCESS PANEL NR 1462C AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 62,790 hrs · 45,976 cycles

CRACKED LT MLG DOOR FRAME BS 984. FRAME REMOVED IAW SRM 51-30-2 AND A NEW FRAME WAS DRILLED IAW SRM 50-10-4 AREA, TREATED AND PAINTED IAW SRM 51-10-3 AND INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1367C AT LT WING. CORROSION ON SETLEMENT AREA WAS REMOVED, COUNTERSINK HOLES WERE MEASURED AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: DOOR — CRACKED (SLAT TRACK) · airframe 62,790 hrs · 45,976 cycles

CRACK ON LEFT SLAT TRACK DOOR NR 3. SLAT TRACK DOOR WAS FABRICATED IAW ERA 512356-14, MA REV ORIGINAL.

Part: CAM — WORN (TAILCON) · airframe 62,790 hrs · 45,976 cycles

WORN TAILCONE RELEASE CAM BS 1510 AT 10 O'CLOCK POSITION. TAIL ONE RELEASE CAM REPLACED IAW AMM 53-53-02.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON CONUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1456C AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS.

Part: SUPPORT — CRACKED (BS 1485) · airframe 62,790 hrs · 45,976 cycles

CRACKED SUPPORT BS 1485 LONGERON 24 LT. SUPPORT REPLACED IAW DWG 9911946, 3 REV R, SRM 51-30-2, 51-20-4, M51-20-3 PAR 14 AND 21 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1454C AT RT WING. CORROSION ON SETLEMENT AREA AND COUNTERSINK WAS REMOVED, AND FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-22-2A .

Part: DOOR — CRACKED (RT SLAT TRACK) · airframe 62,790 hrs · 45,976 cycles

WEAR AND CRACK ON RT SLAT TRACK DOOR NR 11. SLAT TRACK DOOR WAS FABRICATED IAW ERA 512356-14 MA REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1464C AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAE SRM 51-22-2A AND FOUND OUT LIMITS IAW SRM 51-22-2A AND WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL NR 1361C AT LT WING,. CORROSION ON COUNTERSINK HOLES WAS REMOVED AND WAS FOUND TO BE OUT OF LIMITS AND WAS REPLACED IAW 51-22-2A .

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL NR 1357C AT LT WING,. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 62,790 hrs · 45,976 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: STRIP — CORRODED (BS 1188-1200) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON STRIP BELOW LONGERON 26 LT BS 1188-1200 IN CARGO BAY. STRIP REPAIRED IAW SRM 51-30-2;51-10-3 P 26,21,14, 51-30-5; 53-04 FIG 12D, 12F, AND ER/A 511165-14MA, REV B.

Part: DOUBLER — CORRODED (LAVATORY) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON INNER DOUBLER OF AFT LAVATORY SERVICE PANEL. INNER DOUBLER WAS REPAIRED IAW ERA 397822-14, MA REV A.

Part: FITTING — CRACKED (BS 1350) · airframe 62,790 hrs · 45,976 cycles

CRACKED FITTING BS 1350 AND X-5. FITTING WAS R & R IAW SRM 51-30-2 AND DWG 5917579, REV EE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON AFT CARGO LOWER DOOR JAMB BEAM HORIZONTAL L/E BELOW PREVIOUS REPAIR DOUBLER BETWEEN BS 1158-1205. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: DOUBLER — WORN · airframe 62,790 hrs · 45,976 cycles

WEAR ON INNER DOUBLER OF TITANIUM AT AFT LAVATORY SERVICE PANEL TRAY. DOUBLER WAS REPLACED IAW DWG 5911423, REV CD AND SRM 51-30-2, SRM 51-30-5, SRM 51-10-3, PAR 14.

Part: CUSP WEB — CRACKED (BS 825-826) · airframe 62,790 hrs · 45,976 cycles

NDT FOUND A CRACK OF 0.625 ON LT CUSP WEB BETWEEN X=54 AND X=60 BS 825-826. LT CUSP WEB BETWEEN X=54 AND X=60 AND Y=825-826 WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: FLOOR SUPPORT — DAMAGED (BS 1079-1117) · airframe 62,790 hrs · 45,976 cycles

ELONGATED HOLES ON FLOOR SUPPORT BS 1079 - 1117, BETWEEN LONGERONS 28LT AND 28RT IN AFT CARGO BAY. FLOOR SUPPORT REPLACED IAW SRM 51-30-5 AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (BS 1155) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND ELONGATED HOLES ON FLOOR SUPPORT AT BS 1155. CORROSION REMOVED IAW SRM 51-10-3 PAR26. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-FIG1 AND WAS REPLACED IAW SRM 51-10-04 AND DWG 5936660, REV BZ.

Part: HINGE FITTING — CORRODED (SLIDE DOOR) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON HINGE FITTING OF R1 SLIDE DOOR. FITTINGS WERE REPLACED IAW SRM 51-10-3 AND 51-10-4, DWG 3936190.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON AFT CARGO DOOR LOWER FRAME BEAM REPAIR SPACER BETWEEN BS 1155-1212. SPACER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: INTERCOSTAL — CRACKED (BS 210) · airframe 62,790 hrs · 45,976 cycles

CRACK ON INTERCOSTAL BS 210, LONGERON 15 L . INTERCOSTAL REPLACED IAW SRM 51-30-2 AND DWG 9957884, REV H.

Part: SEAT TRACK — CORRODED (BS 213-216) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON SEAT TRACK X - 44, BS 213-216. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: CUSP WEB — CORRODED (BS 834-838) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB BS 834 - 838 BETWEEN X-54 TO X-60 . CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-10-3, PAR 14 21.

Part: FRAME — CORRODED (BS 1193) · corrosion level 2 · airframe 62,832 hrs · 46,010 cycles

CORROSION ON FRAME ANGLE BS 1193 BETWEEN LONGERONS 29 - 30L . FRAME ANGLE WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, 53-01, FOG 1, 53-03.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 62,790 hrs · 45,976 cycles

CORROSION FOUND ON INBD AND OTBD FACE OF VERTICAL STABILIZER PLATES, ZRS= 178. CORROSION WAS REMOVED IAW SRM 55-02, PAR 24 AND 51-10-3, PAR 26, 21, 14.

Part: FLOORBEAM — CRACKED (BS 120) · airframe 62,790 hrs · 45,976 cycles

CRACK FLOORBEAM ANGLE BS 120 X -54 Z 0. R & R FLOORBEAM ANGLE IAW DWG 9911559-8, SRM 51-10-3, PARA 21 & 14, SRM 51-30-5.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 62,790 hrs · 45,976 cycles

CRACKED CHANNEL N2 FROM ROOT TO TIP ON REAR SPAR OF HORIZONTAL STABILIZER RT SIDE. . CHANNEL WAS FABRICATED IAW SRM 55-12-0, FIG 4, 51-10-3, PAR 21 AND 14.

Part: CUSP WEB — CORRODED (BS 674-693) · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 674 - 693 AND X-54 TO X 60 . RT CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-5.

Part: ATTACH ANGLE — CRACKED (BS 1003) · airframe 62,790 hrs · 45,976 cycles

CRACKED RT ATTACH ANGLE FUSELAGE AT LONGERON 20R BS 1003. REPAIRED IAW SRM 53-02, FIG 22.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 62,790 hrs · 45,976 cycles

CRACKED SHEAR TIE BS 1380 BETWEEN LONGERONS 13 - 14R. NEW SHEAR TIE WAS FABRICATED AND PAINTED TREATED IAW SRM 53-14-4 AND 51-10-3 PAR 14,21.

Part: FLOORBEAM — CRACKED (BS 120) · airframe 62,790 hrs · 45,976 cycles

CRACKED FLOORBEAM ANGLE BS 120, X 54 Z 0. R & R FLOORBEAM ANGLE IAW DWG 9911559-7, SRM 51-10-3, PARA 21 & 14, SRM 51-30-5.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACK ON FWD STOPS NR 2 AND 4 AT FWD CARGO BAY DOOR. CRACK STOP FITTING WERE REMOVED IAW SRM 51-30-1 AND 51-30-5. NEW STOPS WERE DRILLED IAW SRM 51-10-4. NEW STOP FITTINGS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21 NEW STOP FITTING NR 2 AND 4 WERE INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,790 hrs · 45,976 cycles

CRACKED LONGERON 13R BS 1437. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: RIB — CRACKED (LT WING) · airframe 62,790 hrs · 45,976 cycles

CRACKED RIB ON SPAR, X05=322 AT LT WING. RIB WAS REPLACED IAW DWG 94375588, REV G AND SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 252-254) · airframe 68,009 hrs · 49,757 cycles

CORROSION ON LT CUSP WEB BS 252 - 254, X 54 AND X 60. DAMAGE WAS REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 298-306) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 298 - 306 BETWEEN X 60 TO X-56. REPAIR DOUBLER WAS REMOVED AND NEW DOUBLER RING. DOUBLER AND FILLER WERE FABRICATED IAW SRM 53-05, FIG 131A/6.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL NR1355C AT LT WING, MRB 57-083-02, CARD 70, ZONE 00. THE CORROSION ON COUNTERSINK HOLES WAS REMOVED AND MEASURED COUNTERSINK HOLES, MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .600" IN (4) ADJACENT HOLES, FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL NR 1365C AT LT WING, LW, MRB 57-083-02, SM, CARD 64, ZONE 00. THE CORROSION ON COUNTERSINK HOLES WAS REMOVED AND MEASURED COUNTERSINK HOLES. MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .605" IN 3 ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A, THE ACCESS DOOR WAS REPLACED IAW IPC 57-30-00.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,790 hrs · 45,976 cycles

CORROSION ON SETTLEMENT AND HOLES, FUEL ACCESS DOOR 1335C LT WING, MRB 57-084-02, H1L1-SM, CARD 40, ZONE 23. THE CORROSION ON COUNTERSINK HOLES WAS REMOVED AND WERE MEASURED COUNTERSINK HOLES, MAX DIAMETER ALLOWABLE IS 0.660" AND MAX DIAMETER MEASURED IS .681 IN, 3 ADAJCENT HOLES, WAS FOUND OUT OF LIMITS IAW SRM 51-22-21, THE ACCESS DOOR WAS REPLACED IAW IPC 57-30-00.

Part: BEAM — CRACKED (R1 DOOR FRAME) · airframe 62,790 hrs · 45,976 cycles

CRACKED BEAM NR 1 FWD AND AFT ENDS AT R1 DOOR STRUCTURE. DAMAGED BEAM WAS REPLACED IAW SRM 51-30-1, 51-30-2 , 51-30-5.

Part: SEAT TRACK — DAMAGED (BS 638-765) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND SCRATCHED ON SEAT TRACK X 22 BETWEEN BS 638-765. SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4F, SRM 51-10-3, PAR 14,21.

Part: TEE FITTING — CRACKED (BS 995) · airframe 62,790 hrs · 45,976 cycles

CRACKED REPAIR TEE FITTING BS 995 AND X=-60. DAMAGE TEE FITTING WAS R & R IAW SRM 51-30-5 AND SRM 51-30-2.

Part: CUSP WEB — CRACKED (BS 221) · airframe 62,790 hrs · 45,976 cycles

CRACK ON RT CUSP WEB BS 221, X 57.5. CRACKED CUSP WEB WAS REMOVED NEW WEB WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,790 hrs · 45,976 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,790 hrs · 45,976 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,790 hrs · 45,976 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRCATED IAW AMM 53-20-01-201.

Part: INTERCOSTAL — CRACKED (TAILCONE) · airframe 62,790 hrs · 45,976 cycles

CRACK ON RT INTERCOSTAL IN THE TAILCONE. INTERCOSTAL REMOVED, NEW FABRICATED, DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-2, 51-10-4, 51-10-03 PAR 14AND 21, DWG 4911957, REV AV.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,790 hrs · 45,976 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 53-20-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,790 hrs · 45,976 cycles

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

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON SETTLEMENT AREA ON ACCESS PANEL NR 1409C. REPLACED.

Part: CUSP WEB — CORRODED (BS 510-517) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER BETWEEN BS 510 - 517, X 53 - 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131-A-13.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,790 hrs · 45,976 cycles

CRACKED LONGERON 12L BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG 18 AND 51-10-3, PAR 21 - 14.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON FRAME ANGLE AT BS 1309, BETWEEN LONGERON 29L - 29R. FRAME ANGLE WAS REPAIRED IAW SRM 53-030, FIG 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,790 hrs · 45,976 cycles

CRACKED LONGERON 16L BS 1437. LONGERON REMOVED. NEW LONGERON SECTION WAS DRILLED, ADJUSTED, TREATED AND PAINTED. NEW LONGERON INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.

Part: ANGLE — CRACKED (R1 DOOR FRAME) · airframe 62,790 hrs · 45,976 cycles

CRACKED ANGLE ON BEAM 1 AFT END AT R1 DOOR. ANGLE WAS REPLACED IAW DWG 9911582 REV-T AND SRM 51-10-2.

Part: CUSP WEB — CORRODED (BS 565-577) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON CUSP WEB REPAIR DOUBLER BETWEEN BS 565 -577 X-54 AND X-60. DOUBLER WAS REPAIRED IAW SRM 53-05, FIG 131A-7, 51-30-2, 51-30-1, 51-10-3 PAR 14-21, AMM 20-30-1, 20-12-01 AND DS 900-5-1, NR 4 PAR.

Part: SEAT TRACK — CORRODED (BS 333-335) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON LT SEAT TRACK X 54, BS 333 - 335. DAMAGED AREA WAS CUT OUT, ADJUSTED, TREATED, PAINTED AND INSTALLED. CIC WAS APPLIED IAW SRM 53-05, FIG 4A AND 51-10-3, PAR 21,14 AND 38 AND ERA NR 485415-14MA, REV ORIGINAL.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 62,790 hrs · 45,976 cycles

CRACKED ANGLE ON BEAM 4 AFT END AT R1 DOOR STRUCTURE. ANGLE WAS REMOVED IAW SRM 51-30-2, AND FABRICATED IAW DWM 9911579, REV L. NEW ANGLE WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, AND INSTALLED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1309-1287) · airframe 62,790 hrs · 45,976 cycles

CRACK FOUND ON INTERCOSTAL BS 1287 - 1309 BETWEEN X 22, AND X -22. INTERCOSTAL REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 525-538) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON CUSP WEB BS 525 - 538, BETWEEN X-54 AND X -60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: MEMBRANE — CRACKED (BS 196) · airframe 62,790 hrs · 45,976 cycles

CRACK ON MEMBRANE AT BS 196 X=9. MEMBRANE REPAIRED IAW ETI-88-14-159 AND E/RA 528218-14, REV ORIGINAL, 1614055.

Part: SEAT TRACK — CORRODED (BS 408) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND WEAR ON SEAT TRACK PLUG X 22 BS 408,. REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3, PAR 14 AND 21, 51-30-1.

Part: SEAT TRACK — CORRODED (BS 437) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION FOUND ON SEAT TRACK PLUG X 54, BS 437. REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3, PAR 14 AND 21, 51-30-1.

Part: SEAT TRACK — CORRODED (BS 686) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND WEAR ON SEAT TRACK PLUG, X 22, BS 686. REPAIRED IAW SRM 53-05, FIG 4A, 51-30--1, 51-30-3, PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 436-600) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON SEAT TRACK Y=-22 BETWEEN BS 463 - 600. REPAIRED IAW SRM 53-05, FIG 4A 51-30-1, 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 1057) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND WEAR ON SEAT TRACK PLUG X 54 BS 1057. REPAIRED IAW SRM 53-05, FIG 4A, 51-30-1, 51-10-3, PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 703) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND WEAR ON SEAT TRACK PLUG X 54 BS 703. REPAIRED IAW SRM 53-05, FIG 4A, 51-30-1, 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 996) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION AND WEAR ON SEAT TRACK PLUG, X 22 BS 996. REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3 PAR 14 AND 21, 51-30-1.

Part: FLOORBEAM — DAMAGED (BS 826) · airframe 62,790 hrs · 45,976 cycles

ELONGATED HOLE ON FLOORBEAM, BS 826 BETWEEN X=44 TO X= 22 AT PAX CABIN, FLOORBEAM ANGLE WAS REPLACED IAW SRM 53-14-30, FIG 10.

Part: CUSP WEB — CORRODED (BS 845-864) · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB REPAIR BS 845 - 864 BETWEEN X-54 TO X-60. REPAIR REPLACED IAW SRM 53-05, FIG 131A-14. REPAIR FABRICATED, TREATED & PRIMERED AND INSTALLED IAW SRM 53-05, FIG 131A-14, 51-10-3 PAR 21 AND 14 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 886-905) · corrosion level 2 · airframe 62,790 hrs · 45,976 cycles

CORROSION ON RT CUSP WEB REPAIR BS 886 - 905 BETWEEN X-54 TO X-60. REPAIR WAS REMOVED, NEW REPAIR FABRICATED, TREATED, PRIMERED AND INSTALLED IAW SRM 51-30-2, 53-05, FIG 131A-4, 51-10-3, PAR 21&14 AND SRM 53-05, FIG 131A-4.

Part: CUSP WEB — CORRODED (BS 630-634) · airframe 68,009 hrs · 49,757 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB BS 630 AND 634, X 54 AND X 60 AND WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 62,790 hrs · 45,976 cycles

FUSELAGE SKIN MID CARGO DOOR GOUGED AT BS 636, BETWEEN LONGERONS 24 - 26R. REPAIRED IAW ERA 330438-14, SECT 1.

Part: CUSP WEB — CRACKED (BS 798-800) · airframe 62,790 hrs · 45,976 cycles

CRACKED LT CUSP WEB FROM BS 798-800 AND X=44. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-19, 51-30-1, 51-30-5, 51-30-2, 51-10-3 PAR 21 AND 14 51-10-3 PAR 38.

Part: HANDLE — STUCK (EMERGENCY EXIT) · airframe 62,790 hrs · 45,976 cycles

MAINTENANCE DISCOVERED THAT THE RT FWD OVERWING EMERGENCY ESCAPE HATCH WAS OUTER HANDLE RELEASE WAS STUCK. THIS WOULD PREVENT PROPER OPERATION OF THE ESCAPE HATCH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR HANDLE WAS CLEANED IAW PS 900-1 NR 6.

Part: ANGLE — CRACKED (BS 1338) · airframe 62,790 hrs · 45,976 cycles

CRACKED ANGLE ON BS 1338 BETWEEN LONGERONS 6-7L. REPLACED ANGLE IAW SRM 51-30-2, 51-30-5 AND DWG -9915558, REV A.

Part: DOUBLER — CRACKED (BS 1463-1474) · airframe 62,790 hrs · 45,976 cycles

CRACKED ELEVATOR ACCUMULATOR ACCESS CUT OUT BETWEEN BS 1463-1474. DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-2, DWG 5917683, REV A4, AND SRM 51-30-2 AND 51-30-5.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,634 hrs · 45,234 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATH LIGHTING AT SEAT 13D WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMP AND THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS FOUND TO BE LOOSE AND THE FRAME HOLE WAS CRACKED AT THE 4:30 POSITION. CRACKED FRAME REPLACED DURING THIS MAJOR MX CHECK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS FOUND TO BE LOOSE AND THE FRAME HOLE WAS CRACKED AT THE 8:30 POSITION. CRACKED FRAME REPLACED DURING MAJOR MX CHECK.

Part: FRAME — CRACKED (BS 1510) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS FOUND TO BE LOOSE AND THE FRAME HOLE WAS CRACKED AT THE 7:00 POSITION. CRACKED SECTION OF FRAME AT BS 1510 WAS REPLACED IAW SRM 51-30.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE RELEASE SPRING BRACKETS WERE FOUND TO BE WORN ON THE LT & RT SIDES. REPLACED LT & RT SPRING BRACKETS IAW SRM 51-30. THE REQUIRED INSPECTION WAS COMPLETED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS FOUND TO BE LOOSE AND THE FRAME HOLE WAS CRACKED AT THE 9:00 POSITION. FRAME WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 834) · corrosion level 2 · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, CORROSION WAS FOUND AT BS 834 CUSP WEB. CORROSION REMOVED AND REPAIR DOUBLER INSTALLED IAW SRM 53-05, FIG 131A-13.

Part: LONGERON — CRACKED (BS 1420) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, LONGERON 2R CRACKED AT BS 1420. REPLACED LONGERON AFT END FITTING AND FABRICATED NEW SPLICE IAW SRM 53-14 AND INSTALLED IAW SRM 51-01.

Part: PIN — RUSTED (TAILCONE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE LT & RT TAIL CONE SLIDER BLOCKS WERE FOUND TO HAVE RUSTED PINS. THE RUSTED PINS WERE REPLACED ON THE LT & RT SLIDER BLOCKS IAW AMM 20-10-01 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: COTTER PIN — MISSING (TAILCONE RELEASE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE CAM MECHANISM WAS NOTED TO HAVE MISSING COTTER PINS ON THE ROLLER BEARING BOLT NUTS. THE MISSING COTTER PINS WERE INSTALLED ON THE CAM MECHANISM IAW AMM 20-10-01 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: BUSHING — WORN (TAILCONE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE TEE PIN BUSHINGS WERE FOUND TO BE WORN. THE BUSHINGS WERE REPLACED IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: BRACKET — DAMAGED (TAILCONE) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION IN MSP, THE RT UPPER TAIL CONE LATCH BRACKET WAS NOTED TO HAVE A SHEARED FASTENER HEAD. THE FASTENER WAS REPLACED ON THE RT UPPER TAIL CONE LATCH BRACKET IAW SRM 51-30.

Part: SKIN — CRACKED (BS 1380) · airframe 59,965 hrs · 44,096 cycles

DURING SCHEDULED INSPECTION, A .2500 INCH LONG CRACK WAS NOTED IN THE ACFT SKIN AT A FASTENER HOLE APPROX 2 INCHES ABOVE L14L AT BS 1380. REPAIRED IAW ER/A 517219-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,149 hrs · 42,835 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FROM ROW 10 - 20 WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,813 hrs · 42,599 cycles

DURING LINE CHECK, MX FOUND THAT THE EXIT SIGN FOR THE EMERGENCY PATHWAY LIGHTING AT THE FWD OVERWING ESCAPE HATCH OF THE CABIN WAS TOO DIM TO PROVIDE ESCAPE GUIDANCE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 54,337 hrs · 40,225 cycles

FLIGHT CREW FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,403 hrs · 39,624 cycles

DURING LINE CHECK, MX FOUND EMERGENCY CEILING LIGHTS AT STA 500 - 700 INOP. MX REPLACED BATTERY POWER SUPPLY. OPS OF LIGHTS NOW CHECKS OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 51,294 hrs · 38,221 cycles

EMERGENCY LIGHT PATH LIGHT AT SEAT 3C/D INOP. FOUND PWC DISCONNECTED UNDER SEAT, RECONNECTED SAME, OPS NML. ACFT OK FOR SERVICE.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 48,324 hrs · 36,334 cycles

RT PASSENGER CABIN WINDOW RING PAN AT FS 1041 HAD THE TYPICAL CRACK AT THE FWD LWR FASTENER, AND AN ELONGATED HOLE NEARBY. THE WINDOW BELT DOUBLER ALSO HAD A SLIGHTLY MISDRILLED HOLE. THE CRACK END FASTENER WAS TRIMMED OFF, AND A REPAIR ANGLE INSTALLED. THE ELONGATED HOLE WAS BUSHED AND THE MISDRILL MARK WAS BLENDED OUT. THE INSTALLED REPAIR WAS FAA APPROVED BY THE OEM BOEING.

Part: SKIN — GOUGED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

FUSELAGE SKIN AT FS 125, BETWEEN L-29L AND L-30 WAS FOUND WITH A LIGHTNING STRIKE BEYOND SRM 53-04 FIG 38 LIMITS. THE DAMAGE WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED. REPAIR IS TIME-LIMITED FOR DTA PURPOSES.

Part: BEAM — DAMAGED (CARGO BAY) · airframe 48,324 hrs · 36,334 cycles

DURING BLEND OUT, FOUND ELONGATED HOLES ON C2 DOOR JAMB BEAM. ELONGATED HOLE WERE DRILLED UP IAW SRM 51-10-4. BUSHINGS WERE FABRICATED IAW ERA 471657-14 REV ORIG. BUSHINGS WERE INSTALLED IAW ERA 471657-14 REV ORIG. REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

CRACK ON FUSELAGE SKIN AT STA Y=1437 LONG 2RT. DAMAGE WAS REMOVED IAW SRM 53-04D FIG 27. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2 AND IDENTIFIED IAW PS 900-5-1 NR 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

CRACK ON FUSELAGE SKIN AT STY Y=1437, LONGERON 2 RT. FUSELAGE SKIN WAS REPAIRED PER SRM 53-04D FIG 27.

Part: FITTING — CRACKED (LT SPOILER) · airframe 48,324 hrs · 36,334 cycles

CRACKED FITTING FOR LT WING I/B FLIGHT SPOILER TORSION BAR O/B SIDE STA XRS=233. CRACKED FITTING FOR LT WING I/B FLIGHT SPOILER TORSION BAR WAS REPLACED IAW DRAWING 5923264.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

A 0.562 INCH CRACK ON FUSELAGE SKIN AT STA Y=175 ON THE WD UPPER CORNER AT THE FWD SERVICE DOOR JAMB. CRACK WAS REMOVED IAW SRM 53-05 FIG 112. NO CRACKS FOUND. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 112.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

EXFOLIATION CORROSION ON LWR BEAM OF MID CARGO COMPARTMENT LWR DOOR JAMB BETWEEN STA Y=636-693. CORROSION REMOVED IAW SRM 51-10-3, FOUND OUT OF LIMITS. INSTALLED NEW LOWER BEAM IAW SRM 51-30-1, -2, AND -5.

Part: BEAM — CORRODED (AFT CARGO BAY) · airframe 48,324 hrs · 36,334 cycles

EXFOLIATION CORROSION ON LWR BEAM OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y=1155-1212. REMOVED CORROSION IAW SRM 51-10-3, AREA FOUND OUT OF LIMITS. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 123 AND IDENTIFIED IAW PS 900-5-1 NR 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,324 hrs · 36,334 cycles

BLEND OUT WITHOUT ID TAG ON FUSELAGE SKIN BETWEEN STA Y=712 TO 732 AND LONG 24-26RT. BLEND OUT WAS FOUND OUT OF LIMITS IAW SRM 53-04D FIG 38 TABLE A. DAMAGE WAS CUT OUT IAW SRM 53-04 FIG 129. NEW SKIN AND DOUBLER WERE INSTALLED IAW SRM 53-04D FIG 126 AND WERE IDENTIFIED IAW PS 900-5-1 NR 04.

Part: HANDSET — FIRE (CABIN) · airframe 46,853 hrs · 35,360 cycles

F/A FORWARD HOLD HANDSET SPARKED AND CAUGHT FIRE AT HANDSET CONNECTOR. FOUND WIRING ON HANDSET SHORTED NEAR HANDSET. REPLACED HANDSET. CKS OK.

Part: HANDLE — OPEN (WHEEL WELL) · airframe 42,473 hrs · 32,612 cycles

AFTER TAKEOFF LANDING GEAR WILL NOT RETRACT. FOUND RT LANDING GEAR MANUAL DOOR RELEASE HANDLE IN OPEN POSTION. OPERATED DOOR MANUAL RELEASE PER M/M SYSTEM OPS OK. DOOR RELEASE HANDLE STOWED AND SECURED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,857 hrs · 32,179 cycles

EMERGENCY ESCAPE PATH LIGHT OUT AT 23DE. RELAMPED, CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 37,143 hrs · 28,807 cycles

NR 2 ENGINE N1/EGT EXCEEDANCE. ABORTED TAKEOFF AT 100 KIAS. REPLACED FAN.

Part: NOSE COWL — MISSING (NR 2 ENGINE) · airframe 35,681 hrs · 27,801 cycles

NUMBER 2 ENGINE COWLING LOOSE. PORTION MISSING. FOUND ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RIGHT NOSE COWL ASSY PER MM. ASSOC PARTS REPLACED AS FOLLOWS, THERMOSTATIC REGUALTOR VLV 759702239 S/N 5969C. NOSE COWL A/I SHUTOFF VLV 754001305 S/N 23227. DUCT 759102267 S/N N/A.

Part: HEATER — BURNED (STATIC PORT) · airframe 34,545 hrs · 26,991 cycles

PASSING 26000 THE FLT/ATT NOTIFIED COCKPIT THAT THEIR WAS AN ELECTRICAL ODOR IN THE AREA OF SEAT 22A. FOLLOWED POM. RETURNED TO CVG. ODOR CONTINUED FOR 15 MINS. NEVER REACHED FWD CABIN OR COCKPIT. NO SMOKE. TROUBLESHOT FOUND LEFT STATIC PORT HEATER INOPERATIVE AND BURN DAMAGED. REPLACED SAME.

Part: LINE — LEAKING (RT HYD MODULE) · airframe 33,517 hrs · 26,272 cycles

ON DESCENT RT HYD QTY DROPPED TO 2 QTY AND PRESS TO ZERO C/W EMERGENCY PROCEDURES TURNED XFER PUMP OFF. REPLACED RT HYD LINE TO FILTER MODULE.

Part: CSD — MALFUNCTIONED (GENERATOR) · airframe 33,295 hrs · 26,116 cycles

ON TAXI LT GENERATOR TRIPPED AND AC X-TIE LOCKOUT MSG ILLUM. RESET NG. STARTED APU TO PWR THE LT BUS AFTER RESETTING X-TIE. AT 125 KTS RT GENERATOR OFF AND X-TIE MSG RESET GEN, NO HELP. THE RT BUSS WAS DEAD. RT GEN VOLTS AND FREQS ZERO. REPLACED BOTH GENERATORS AND LEFT CSD. ALSO, REPLACED X-TIE RELAY.

Part: LINK — FAILED (NLG DOOR) · airframe 33,248 hrs · 26,077 cycles

VIBRATION. AFTER GEAR RETRACTION, GEAR RECYCLED SAME RESULT. CAME ON TO ATL. AT ARRIVAL IN ATL FOUND LT NOSE GEAR DOOR OPEN. REPLACED LT FWD NOSE GEARDOOR LINK. JACKED NOSE GEAR AND CYCLED GEAR, OPERATION, CHECKS GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 30,690 hrs · 24,239 cycles

AT FLT LEVEL 230 DURING CLIMB FLOW LIGHT ILLUM, A MAX DESCENT TO 10,000 FT, O2 MASKS DEPLOYED. FINALLY AT 10,000 FT ABLE TO REGAIN AUTO 2. CLIMBED TO FL220 FOR REMAINDER OF FLT. AUTO 2 WORKED OK REST OF FLT. REPLACED AUTO CONTROLLER 1.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,115 hrs · 22,340 cycles

ELECTRICAL ODOR THROUGH OUT CABIN AND COCKPIT, AIRBORNE. RETURNED TO A-03. MIXED REPORTS FROM THE FLIGHT CREW ON THE EXACT ODOR. AIRCRAFT WAS INSPECTED AT THE GATE FOR ANY ELECTRICAL PROBLEMS OR POPPED CIRCUIT BREAKERS, NONE NOTED. APU AND PACKS WERE OPERATED, WITH NO ODOR NOTED. NR 2 ENGINE WAS REPLACED 01/06/01, AND FLT 356 WAS THE FIRST FLT SINCE ENG CHANGE.

Part: FAN — FAILED (CARGO BAY) · airframe 27,750 hrs · 22,073 cycles

ELECTRICAL FUMES THROUGH-OUT CABIN. FOUND RECIRC FAN BAD. REPLACED SAME.

Part: FAN — MELTED (CARGO BAY) · airframe 27,750 hrs · 22,073 cycles

OBSERVED SMOKE IN AFT CABIN AT GATE. BURNING ELECTRICAL SMELL. FOUND RECIRC FAN BURNT. REPLACED FAN ASSY. ALSO REPLACED RELAYS R2-278 AND R2-279 PRECATIONARY. FAN OPS CKS NORMAL.

Part: FAN — FAILED (AFT CABIN) · airframe 27,750 hrs · 22,073 cycles

FUMES IN AFT CABIN, SMELL IS ELECTRICAL. REPLACED RECIRC FAN FOR BEING BURNT AND FAILED.

Part: BOLT — WORN (NR 1 PYLON)

THE NR 1 PYLON APRON SUPPORT BOLT HAS WORN SURFACES ON BOTH ENDS. THIS ER/A AUTHORIZES THE MANUFACTURE OF THE BOLT (DAC P/N 4938184-3) PER DRAWING 4938184, USING SUBSTITUTE MATERIAL 17-4PH HT TR 180-200 KSI.

Part: SKIN — GOUGE (CARGO DOORWAY)

THE FUSELAGE SKIN AT THE FORWARD EDGE OF THE MID CARGO DOOR CUTOUT WAS FOUND GOUGED. THE RESULTING CUTOUT MEASURED 1.25 BY 2.25. THIS DAMAGE WAS REPAIRED WITH A DOUBLER AND APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DATED 7-11-97

Part: SKIN — CORROSION (BS 759-779)

CORROSION WAS FOUND UNDER THE RIGHT RUB STRIP IN SEVERAL LOCATIONS BETWEEN STA 759 AND 779 BETWEEN STR 27R AND STR 29R. THE RUB STRIP IS LOCATED WHERE THE WING TO BODY FAIRING MEETS THE FUSELAGE. THIS STRIP WAS REPAIRED WITH A DOUBLER AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DTD 7-11-97.

Part: SKIN — DENT (BS 237)

THE FUSELAGE SKIN WAS FOUND DENTED IN TWO PLACES AT STR 17L BETWEEN FS 237 AND 258. THE CUTOUT DIMENSIONS FOR THE AFT CUTOUT ARE 6 BY 4 BEGINNING AT STA 252. THIS AREA WAS REPAIRED PER MD-88 SRM 53-04, FIG 12B CLASS I.

Part: PACKS — FAILED (LT/RT)

ON CLIMBOUT THROUGH 30,000 FT, RT PACK TRIPPED OFF, TEMP VALVE FULL HOT. CHECKLIST ACCOMPLISHED. WHILE ATTEMPTING TO RESET THE RT PACK, THE LT PACK TRIPPED OFF. CABIN ALT BEGAN CLIMBING AT 1,500 FPM. CABIN EXEEDED 10K FT MASK DEPLOYED BY CREW. EMERGENCY DESCENT ACCOMPLISHED.

Part: BULB — FAILED (CABIN)

F/C EMERGENCY ESCAPE PATH LIGHTING INOP.