N568UA

Part: FRAME — CORRODED (BS 1420) · airframe 81,729 hrs · 27,521 cycles

ON REMOVAL OF THE AFT CARGO FRAME, BS 1420, STRINGERS 24L TO 27R, FOUND CORROSION ON THE FRAME. FOUND OUT OF LIMITS IAW SRM 53-00-07-A1, FIG 101. REPAIRED IAW ECRA 5360-01484, REV- .

Part: FLOOR SUPPORT — CORRODED (BS 1300) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT RBL 9 CORRODED, FOUND TO BE OUT OF LIMITS BS 1300 IAW SRM 53-00-53, FIG 101, DETAIL 5, ALLOWABLE DAMAGE 1. REPAIRED IAW AMM 53-30-94-320-8061 AND ECRA 5310-07397.

Part: FRAME — CORRODED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FRAME, BS 1400 BETWEEN STRINGERS 27L TO 27R CORRODED AT MULTIPLE AREAS. FOUND OUT OF LIMITS IAW SRM 53-00-07-A1, FIG 101. REPAIRED IAW ECRA 5310-07373, REV A.

Part: INTERCOSTAL — CRACKED (BS 1400-1420) · airframe 81,729 hrs · 27,521 cycles

DURING REMOVAL OF THE AFT CARGO INTERCOSTAL BETWEEN BS 1400 & 1420, A CRACK WAS FOUND ON LOWER FLANGE, FOUND OUT OF LIMITS IAW SRM 53-00-04-A1-F101. FABRICATED A NEW INTERCOSTAL AND INSTALLED.

Part: WEDGE — DELAMINATED (NR 3 SLAT) · airframe 81,729 hrs · 27,521 cycles

ON VISUAL INSPECTION OF THE NR 3 SLAT TRAILING EDGE WEDGE, FOUND AN AREA OF DELAMINATION, 40 INCHES FROM THE INBD END, 6.5 INCHES FROM THE TOP, ABOUT 4 INCHES IN DIAMETER. REMOVED AND REPLACED THE NR 3 SLAT IAW MM 27-81-02.

Part: FLOORBEAM — CORRODED (BS 1220) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOORBEAM, BS 1220, STRINGERS 27L TO 27R CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-07-A1, DETAIL II. REPAIRED IAW ECRA 5360-01482, REV-, PART 2.

Part: FLOOR SUPPORT — CORRODED (BS 1445.6-1500) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT LBL 16, BS 1445.6 TO 1500 CORRODED REMOVED THE CORROSION IAW SRM 53-00-53, AD1, PG 105, FIG 101, DETAIL V. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 4-7, AND DWG 146N5390, REV C.

Part: STRINGER — CORRODED (BS 1400-1420) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO STRINGER 29L BETWEEN BS 1400 AND 1420 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-03-A1, FIG 101. REMOVED, FABRICATED AND INSTALLED A NEW STRINGER SECTION IAW SRM 51-40-02, AND DWG 146N3305.

Part: SKIN SPLICE — CORRODED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO SKIN SPLICE AT BS 1400 BETWEEN STRINGERS 28L AND 29L HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-01-A1, FIG 101. REMOVED AND REPLACED THE SKIN SPLICE IAW SRM 51-40-02, AND DWG 146N3305.

Part: STRINGER SPLICE — CORRODED (BS 1452-1465) · airframe 81,729 hrs · 27,521 cycles

FOUND THE STRINGER SPLICE 29L, BS 1452 TO 1465, TO BE CORRODED ON LOWER SURFACE. FOUND OUT OF LIMITS IAW SRM 53-00-53-A1, FIG 101. FABRICATED A NEW STRINGER SPLICE AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 1200 - 1343.5) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT, LBL 7.55 FROM BS 1200 TO 1343.5 CORRODED AT MULTIPLE AREAS. FOUND OUT OF LIMITS IAW SRM 53-00-53-A1, DETAIL V. REPAIRED IAW SRM 53-00-53-R1, FIG 201.

Part: BULKHEAD — CRACKED (BS 1896) · airframe 81,729 hrs · 27,521 cycles

TAIL COMPT 313AL BS 1896, LBL 33 UPPER CANTED BULKHEAD IS CRACKED. ACCOMPLISHED EC/RA 5380-01184, REV -.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1343) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT RBL 7.55, BS 1200 TO 1343.5 CORRODED AT MULTIPLE AREAS. BLENDED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, ALLOWABLE DAMAGE. REPAIRED.

Part: STRINGER — CORRODED (BS 1460) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO STRINGER SPLICE 22L, BS 1460 CORRODED, FOUND OUT OF LIMITS IAW SRM 53-00-53-A1. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-02, PG 1-10, AND DWG 146N3400.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1500) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT RBL 10.45 FROM BS 1445.6 TO 1500 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53AD1, DETAIL 5, FABRICATED A NEW FLOOR SUPPORT IAW DWG 146N5390, AND SRM 51-40-02, DWG 146N5447, AND INSTALLED.

Part: STRINGER — CORRODED (BS 1460) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO STRINGER 20L, BS 1460 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG. 101. REMOVED AND THE STRINGER SPLICE IAW SRM 51-40-02, PG 1-10, AND DWG 146N3400.

Part: SKIN — CORRODED (BS 1120-1140) · airframe 81,729 hrs · 27,521 cycles

MLG W/W INTERNAL SKIN BETWEEN BS 1120 AND 1140, RBL 65 CORRODED. FOUND OUT OF L IMITS IAW SRM 53-40-14, FIG 101. ACCOMPLISHED EC/RA 534 0-01834 PART 1 INTERIM REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1343.5-1445.6) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT, RBL 16.1, BS 1343.5 - 1445.6 CORRODED AT MULTIPLE AREAS. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, AD 1, DETAIL 5, AND DWG 1-517-2226. REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: ANGLE — CORRODED (BS 1630-1640) · airframe 81,729 hrs · 27,521 cycles

CORROSION FOUND ON THE R4 DOOR CUTOUT FWD INTERCOSTAL OTBD ANGLE BETWEEN BS 1630 AND 1640, JUST BELOW R-4 DOOR POWER ASSIST ACTUATOR. FOUND OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL 6. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 5 1-40-02, PG 1-10, AND DWG 146N8734.

Part: CREASE BEAM — CORRODED (BS 900-1040) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN, RT CREASE BEAM INBD ANGLE FROM BS 900 - 1040 RBL 62, CORRODED AT MULTIPLE AREAS. FOUND OUT OF LIMITS IAW SRM 53-40-13, FIG 101. CUT OUT DAMAGE AREA AND INSTALLED A PERMANENT REPAIR IAW SRM 53-00-13-R2.

Part: ANGLE — CORRODED (STA1630-1640) · airframe 81,729 hrs · 27,521 cycles

CORROSION ON THE L4 DOOR CUTOUT FWD INTERCOSTAL OTBD ANGLE BETWEEN BS 1620 AND 1640 JUST BELOW L/4 DOOR POWER ASSIST ACTUATOR. THE INTERCOSTAL ANGLE WAS FOUND OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL 6. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-40-02, PG 1 - 10, AND DWG 146N8734.

Part: INTERCOSTAL — CRACKED (BS 660) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN, RT BS 660, STRINGER 16R HAS A CRACKED INTERCOSTAL REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-10-02, PG 2-5, AND DWG 143N83-37.

Part: SHEAR TIE — CORRODED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO AT BS 1400, BETWEEN STRINGER 28L - 29L, FOUND THE SHEAR TIE TO BE 100% EXFOLIATED. FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02, PAGES 2 - 5 AND DWG 146N1602, REV 8/84.

Part: SUPPORT — CORRODED (BS 1460-1480) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO VHF ANTENNA DOME NUT SUPPORT DOUBLER BETWEEN BS 1460 AND 1480, STRINGER 29 AND 30R CORRODED. REMOVED, FABRICATED, AND INSTALLED DOME NUT SUPPORT DOUBLER BETWEEN BS 1460 - 1480 IAW SRM 51-40-02, PG2 - 3, 31, AND DWG 140N2058. DOUBLER OUT OF LIMITS DUE TO 100% EXFOLIATION IAW SRM 51-40-02, PG 31, FIG 8.

Part: STRINGER SPLICE — CORRODED (BS 1460) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO STRINGER SPLICE 21L, BS 1460 CORRODED. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, AD1, DETAIL 2. FABRICATED A NEW STRINGER SPLICE. DRILLED, AND INSTALLED THE STRINGER SPLICE IAW DWG 146N3400 AND SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 1040-1180) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN RT CREASE BEAM INBD ANGLE, BS 1180 TO BS 1040 HAS CORROSION AT MULTIPLE AREAS. ACCOMPLISHED A REPAIR IAW ECRA 5340-01833.

Part: FLOORBEAM — CORRODED (BS 1320) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOORBEAM BRAKET CORRODED BS 1320, LBL 20. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-5 3, AD1, DETAIL 4. REMOVED AND REPLACED THE FLOORBEAM BRACKET IAW DRAWING 146N1007.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1343.5) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT, RBL 10.45, BS 1200 - 1343.5 CORRODED AT MULTIPLE AREAS. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-00-53, AD. 1P. REMOVED AND REPLACED THE SUPPORT IAW DWG 146N5390, REV I. C, AND SRM 51-40- 02, PG 2, PAR. 4, AND PAGE 7 PAR. D.

Part: SHEAR TIE — CORRODED (BS 1580) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO SHEAR TIE CORRODED BS 1580 BETWEEN STRINGERS 27R AND 28R REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, AND DWG 146N1020,

Part: FLOOR SUPPORT — CORRODED (BS 1200-1343.5) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT LBL 16.10, BS 1200 TO 1343.5 CORRODED AT MULTIPLE AREAS. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-53, REPAIR 1, PAR 4.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT, RBL 2.9, BS 1495 - 1640 CORRODED AT MULTIPLE AREAS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, AD1, DETAIL V, ACCOMPLISHED A PERMANENT REPAIR AT RBL 2.9 BS 1510 IAW SRM 53-00-53, REPAIR 1, PG 201.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FRAME BS 1540 SHEAR TIE, BETWEEN STRINGERS 27 AND 28R CORRODED. FOUND THE SHEAR TIE OUT OF LIMITS IAW SRM 53-00-07-A1, PG 1. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, PG 1 - 10, AND DWG 140N2002.

Part: STRINGER SPLICE — CORRODED (BS 1460) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO STRINGER 18L SPLICE, BS 1460 CORRODED. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-4 0-02, AND DWG 146N3400.

Part: FLOOR SUPPORT — CORRODED (BS 720-740) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN FLOORBEAM AND ADJACENT FLOOR SUPPORT BETWEEN BS 720 & 740, RBL 60 HAS CORROSION ON THE UPPER SURFACE. BLENDED THE CORROSION ON THE FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV, ALLOWABLE DAMAGE I. REPLACED IAW SRM 51-40-02, AND DWG 143N5522.

Part: CREASE BEAM — CORRODED (BS 780) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN LT CREASE BEAM AT BS 780 HAS CORROSION ON THE UPPER SURFACE. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, AD1, DETAIL VIII. ACCOMPLISHED EC/RA 5310-07371.

Part: FLOOR SUPPORT — CORRODED (BS 720-740) · airframe 81,729 hrs · 27,521 cycles

ON REMOVAL OF MAIN CABIN FLOOR BOX BEAM, DISCOVERED CORROISON ON THE ATTACHED SUPPORT CHANNEL BETWEEN BS 720 - 740, RBL 60 UPPER SURFACE. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV, ALLOWABLE DAMAGE I. REPLACED THE SUPPORT CHANNEL IAW SRM 51-40-02, AND DWG 143N5410.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT FROM BS BS 1510, RBL 7.55 CORRODED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, ADI, DETAIL V ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-53, REPAIR I, PG 201.

Part: SHEAR TIE — CORRODED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FRAME BS 1400 SHEAR TIE BETWEEN STRINGERS 27L AND 28L HAS CORROSION. FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 53-00-07, AD 1, DETAIL II. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 AND DRAWING 146N1008.

Part: FLOOR SUPPORT — CORRODED (BS 1495-1640) · airframe 81,729 hrs · 27,521 cycles

THE BULK CARGO FLOOR SUPPORT LBL 7.55, BS 1495 TO 1640 HAS CORROSION AT MULTIPLE AREAS. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, AD1, DETAIL 5. REPAIRED IAW SRM 53-00-53, REPAIR 1, PG 201.

Part: FRAME ANGLE — CORRODED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FRAME SUPPORT ANGLE AT BS 1400, STRINGERS 26L AND 27L CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, ALLOWABLE DAMAGE 1, FIG 101, DETAIL V, AND DWG 146N1008, REV.

Part: SHEAR TIE — CORRODED (BS 1620) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO BAY SHEAR TIE HAS EXFOLIATED CORROSION AT BS 1620 BETWEEN STRINGERS 22R AND 23R. THE SHEAR TIE WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE SHEAR TIE SRM 51-40-02, AND DWG 146N1022.

Part: STRINGER CLIP — CORRODED (BS 996-1020) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN, STRINGER CLIP 16R BETWEEN BS 996 AND 1020 CORRODED. FOUND THE STRINGER CLIP OUT OF LIMITS IAW SRM 53-00 -03, PG 101, FIG 101, DETAIL 2. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, PH 1-10, AND DWG 140N2001.

Part: FLOOR SUPPORT — DENTED (BS 1400) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT LBL 10.45, BS 1400, DENTED. REPAIRED IAW SRM 53-00-53, REPAIR 1, PG 201 TO 204 AND PG 208, FIG 201.

Part: GUSSET — CRACKED (FWD CARGO DOOR) · airframe 81,729 hrs · 27,521 cycles

FWD CARGO DOOR FWD AND AFT UPPER GUSSETS HAVE CRACKS. REMOVED AND REPLACED THE GUSSETS IAW DRAWING 143N6603, AND SRM 51-40-02.

Part: FLOOR SUPPORT — GOUGED (BS 560) · airframe 81,729 hrs · 27,521 cycles

ON REMOVAL OF FWD CARGO BAY RIGHT SIDE KICK PANEL BETWEEN BS 560 TO 530, RBL 19, FOUND A GOUGE ON THE FLOOR SUPPORT. THE FLOOR SUPPORT WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V, ALLOWABLE DAMAGE. CUT, FABRICATED AND INSTALLED A REPAIR ANGLE AND FILLER IAW 51-70-11, PG 1-8.

Part: STRINGER CLIP — CORRODED (BS 970) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN, STRINGER 16R CLIP AT BS 970 CORRODED. REMOVED CORROSION IAW DRAWING 140N20 01, REV D. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101. REMOVED AND FABRICATE D CLIP IAW DRAWING 140N2001 AND REPLACED.

Part: ATTACH ANGLE — CRACKED (FWD CARGO DOOR) · airframe 81,729 hrs · 27,521 cycles

FWD CARGO DOOR CUT OUT LWR AFT CORNER, CATWALK ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, PARA 7D, AND DWG 143N5320, REV.

Part: FLOOR SUPPORT — CORRODED (BS 650-655) · airframe 81,729 hrs · 27,521 cycles

FWD CARGO FLOOR SUPPORT, BS 650 - 655, RBL 11 HAD TWO FASTNER HOLES CORRODED. BLENDED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-53, REPAIR 1, FIG 201.

Part: INTERCOSTAL — CORRODED (BS 1540-1560) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO INTERCOSTAL HAS CORROSION BETWEEN BS 1540 AND 1560, STRINGER 26 - 27R. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG 146N5434, AND SRM 51-40-02, PAR. 4, PG 2-3, AND PAR 7 PG 6-7.

Part: FLOOR SUPPORT — CORRODED (BS 1495-1640) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT FROM BS 1495 TO 1640 CORRODED. REMOVED CORROSION AND REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: INTERCOSTAL — CORRODED (BS 1612) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO BAY INTERCOSTAL HAS CORROSION ON BOTH SIDE BS 1612 BETWEEN STRINGER 29 AND 30L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, AD I, DETAIL II, PG 103, REMOVED AND REPLACED THE INTERCOSTAL IAW DWG 146N5432.

Part: FLOOR SUPPORT — CORRODED (BS 1495-1640) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT FROM BS 1495 TO 1640 HAS CORROSION AT MULTIPLE AREAS. REMOVED THE CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-53, ALLOWABLE DAMAGE 1, DETAIL V. REPAIRED IAW SRM 53-00-53 REPAIR 1.

Part: SHEAR TIE — CORRODED (BS 1640) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO BAY SHEAR TIE CORRODED AT BS 1640 BETWEEN STRINGER 23 AND 24R. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, ADI DETAIL II. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 146N8711, REV R, AND SRM 51-40-02, PAR 4E, PG 3.

Part: FLOOR SUPPORT — DENTED (BS 593) · airframe 81,729 hrs · 27,521 cycles

FWD CARGO BAY FLOOR SUPPORT, BS 593, RBL 15 HAS DEEP GOUGE AND SCRAPE ON UPPER SURFACE. ON FURTHER EVALUATION FOUND THE GOUGE TO BE A DENT. OUT OF LIMITS IAW SRM 53-00-53. FIG 101, PG 102. REPAIRED THE FLOOR SUPPORT IAW SRM 53- 00-53, FIG 201, REPAIR 1.

Part: INTERCOSTAL — CORRODED (BS 740-760) · airframe 81,729 hrs · 27,521 cycles

FWD CARGO, INTERCOSTAL HAS CORROSION ON THE OTBD SURFACE AND LOWER FLANGE BETWEEN BS 740 TO 760, OTBD OF STRINGER 27L. AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, PG 103, DETAIL II. REMOVED AND REPLACED THE INTERCOSTA L IAW DRAWING 143N5499, AND SRM 51-40-02, PG 2.

Part: FLOOR SUPPORT — CORRODED (BS 1445.6 - 1500) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT, RBL 7.55, BETWEEN BS 1445.6 TO 1500 CORRODED AT MULTIPLE AREAS. BLENDED THE CORROSION IAW SRM 53-60-53, IDENTIF 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, AD. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG PL146N5390, AND SRM 51-40-02, PG 4-7.

Part: FLOOR SUPPORT — CORRODED (BS 1640 - 1640) · airframe 81,729 hrs · 27,521 cycles

CORROSION FOUND ON THE MAIN CABIN FLOOR SUPPORT BETWEEN BS 1620 AND 1640, LBL 20. FOUND TO BE OUT OF LIMITS IAW SRM 53-0 0-51, ALLOWABLE DAMAGE 1, FIG 101, DETAIL III. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 & DWG 146N5281.

Part: CHANNEL — CORRODED (LT OVERWING DOOR) · airframe 81,729 hrs · 27,521 cycles

AFT LEFT OVERWING EXIT DOOR HAS CORROSION ON THE HAT CHANNEL AT THE BOTTOM OF THE DOOR. REMOVED THE CORROSION ON THE OVERWING DOOR, FOUND TO BE OUT LIMITS IAW SRM 52-20-02, AD 1, FIG 101, DETAIL III. FABRICATED A NEW HAT CHANNEL AND STRAP IAW DWG 414N1003, LOCATED AND DRILLED AND INSTALLED THE HAT CHANNEL AND STRAP IAW SRM 51-40-02, AND DWG 144N6302.

Part: CREASE BEAM — CORRODED (BS 337-395) · airframe 81,729 hrs · 27,521 cycles

AFT OF L1 DOOR, BS 337 - 395, LBL 65, STRINGER 17L, CREASE BEAM LWR SIDE HAS CORROSION ON WEB. REMOVED CORROSION AND FOUND FOUND TO BE OUT OF LIMITS IAW SRM 5 3-10-15. FABRICATED A WEB AND INSTALLED A NEW WEB IAW DWG PL 141N8322.

Part: BOX BEAM — CORRODED (BS 1637) · airframe 81,729 hrs · 27,521 cycles

ON REMOVAL OF A CORRODED LAVATORY FITTING, FOUND CORROSION AT BS 1637 ON THE BOX BEAM FOR THE LAVATORY FITTING SUPPORT LBL 25. REMOVED AND REPLACED THE BOX BEAM IAW SRM 51-40-02, PAR 4, AND 7.

Part: INTERCOSTAL — CHAFED (L4 DOOR) · airframe 81,729 hrs · 27,521 cycles

L4 DOOR CUTOUT FWD INTERCOSTAL INNER SURFACE CHAFED AT BS 1640, JUST FWD OF UPPER DOOR STOP. BLENDED THE INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, AD 1, REMOVED STRAP IAW SRM 51-40-02. FABRICATE AND INSTALLED IAW DWG 146N8731, AND SRM 51-40-02.

Part: FLOOR SUPPORT — DENTED (BS 1390-1420) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT, LBL 7.55, BS 1390 AND 1420 DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG. 101 ALLOWABLE DAMAGE I, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51- 40-02 AND DWG. 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1445.6-1500) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT RBL 16, BETWEEN BS 1445.6 TO 1500 CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 146N5390, REV C.

Part: CHANNEL — CORRODED (OVERWING DOOR) · airframe 81,729 hrs · 27,521 cycles

FORWARD LEFT OVERWING EXIT DOOR HAS CORROSION ON THE HAT C HANNEL AT THE BOTTOM OF THE DOOR. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 52-20-02, AD 1, FIG 101, DETAIL III. FABRICATED A NEW HAT CHANNEL IAW DWG 414N1003, AND INSTALLED IAW 51-40-02 AND DWG 144N6302.

Part: CREASE BEAM — CORRODED (BS 1120-1140) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN, RT CREASE BEAM AT STRINGER 17R BETWEEN BS 1120 AND BS 1140 HAS CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-A1. FABRICATED AND I NSTALLED A NEW DOUBLER IAW SRM 51-40-02 AND DWG 144N5211.

Part: FLOOR SUPPORT — CORRODED (BS 1445.6-1500) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT LBL 7.55 FROM BS 1445.6 TO 1500 HAS CORROSION AT MULTIPLE AREAS. REMOVED & REPLACED THE FLOOR SUPPORT IAW DWG 146N5390, REV C, AND SRM 51-40-02, PAR 4, PG 2-3 & PAR 7, PG 6-7. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53, AD 1, DET V.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT STR LBL 2.9 FROM BS 1 445.6 TO BS 1500 HAS CORROSION ON MULTIPLE AREAS. REMOVED CORROSION AT BULK CARGO FLOOR SUPPORT STR LBL 2.9 FROM BS 1445.6-1500 MAX MATERIAL LOSS .031" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ADI DETAIL V. REMOVED AND REPLACED STR IAW DWG 146N5390 AND SRM 51-40-02 PAR 7D PG 6- 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

BULK CARGO FLOOR SUPPORT STR LBL 10 .45 FROM BS 1445.6 TO BS 1500 HAS CORROSION ON MULTIPLE AREAS. REMOVED AND REPLACED BULK CARGO FLOOR SUPPORT STRINGER AT STA 14 45.6 TO STA 1500 LBL 10.45 IAW DWG NR 146N5390 REV "C" AND SRM 51-40-02 PARA 4 PAGES 2 AND 3, AND PARA 7 PAGES 6 AND 7.

Part: STRAP — CRACKED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN AFT FLOOR SUPPORT STABILIZATION STRAP IN AFT CARGO AT APPROX BS 1360 RBL 45 CRACKED. REMOVED AND REPLACED STABILIZATION STRAP SEGMENT AT STA 1360 TO 1380 RBL 45 IAW SRM 53-00-51 REPAIR 12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN STA 324 AND STA 345 AT LBL 20 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AT MAIN CABIN FLR SUPPORT BETWEEN STA 324 AND STA 345 AT LBL 20 L=2.00" W=2.00" D=.015", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 AD 51 DETAIL III. INSTALLED NEW FLR SUPPORT P/N 141N5170-30 PO SAG1850560 IAW SRM 51-40-02 PG 2 PARA 4.

Part: FITTING — CORRODED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

AFT CARGO FLOOR SUPPORT STGR 27R CLIP AT BS 1320 HAS CORROSION. REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT S-27R CLIP AT BS 1320 IAW DWG NR 146N1021 REV D. MECHANICALLY MEASURED DAMAGE ON S-27R CLIP AT BS 1320, MAT LOSS IS 0.030. FOUND OUT OF LIMITS IAW SRM 53-00-03 AD 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN AFT FLOOR SUPPORT INTERCOSTAL ANGLE BETWEEN APPROX BS 1420 AND BS1440 BL0 CRACKED. REMOVED AND REPLACED 1 EA ANGLE AT MAIN CABIN AFT FLOOR SUPPORT APPROX BS 1420 AND 1440 BL 0 IAW SRM 51-40-02 AND DRAWING 146N5180.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 81,729 hrs · 27,521 cycles

CABIN FLOOR STA 480-500 RBL10 INTERCOSTAL UPPER ANGLE IS CRACKED SEVERAL AREAS. REMOVED AND REPLACED 1 EA ANGLE ON MAIN CABIN FLOOR STA 480 TO STA 500 RBL 10 INTERCOSTAL (UPPER ANGLE) IAW SRM 53-00-5 1 REPAIR 4.

Part: GUSSET — CORRODED (BS 1680) · airframe 81,729 hrs · 27,521 cycles

CORROSION ON MAIN CABIN FLOOR GUSSET AT BS 1680, BL-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. FABRICATED A REPLACEMENT GUSSET IAW DWG 146 N5230. INSTALLED IAW SRM 51-40-02, AND DWG 146N5230.

Part: FLOORBEAM — CORRODED (BS 1678) · airframe 81,729 hrs · 27,521 cycles

CORROSION ON MAIN CABIN FLOORBEAM ANGLE AT BS 1678, RBL 53. REMOVED CORROSION AND FOUND TO BE OUT OF LIMI TS IAW SRM 53-0 0-51, FIG 101, DETAIL III. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, PG 2 IT EM 4.

Part: FLOOR SUPPORT — CRACKED (BS 1520-1540) · airframe 81,729 hrs · 27,521 cycles

MAIN CABIN AFT FLOOR SUPPORT BETWEEN BS 1520 & 1540, BL0 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: OVEN — SMOKE (GALLEY) · airframe 81,599 hrs · 27,496 cycles

OVEN 507 MID GALLEY SMOKING HEAVILY. REPLACED THE OVEN.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 81,553 hrs · 27,487 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. OPS CHECKED THE SLIDE ARMED INDICATION, CHECKED GOOD.

Part: GIRT BAR — LACK OF LUBE (R1 DOOR SLIDE) · airframe 81,531 hrs · 27,483 cycles

R1 DOOR WILL NOT DISARM, INSPECTED ESCAPE SLIDE IAW AMM 25-66-00. NO FAULT FOUND. LUBE GIRT BAR. OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (L2 DOOR AREA) · airframe 81,394 hrs · 27,457 cycles

SLIDE LIGHT ABOVE THE L2 DOOR CAME OUT. SECURED THE SLIDE LIGHT. OPS GOOD WITH DOOR ARMED.

Part: HOOK — MISSING (L1 DOOR SLIDE) · airframe 80,081 hrs · 27,202 cycles

L1 DOOR SLIDE ARMED WINDOW INDICATOR BANNER STOWAGE CLIP MISSING. SECURED DOOR SLIDE BANNER CLIP.

Part: WARNING MESSAGE — ILLUMINATED (LT WING SLIDE) · airframe 77,879 hrs · 26,780 cycles

EICAS MESSAGE LT WING SLIDE CAME WHILE ON FINAL APPROACH AT 3000FT ABOVE THE GROUND ALL INDICATIONS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERWING SLIDE) · airframe 77,868 hrs · 26,778 cycles

LEFT WING SLIDE EICAS MESSAGE ON APPROACH UPON ARRIVAL. FOUND LT WING SLIDE DOOR CLOSED,BITE TEST OF THE PSEU IAW AMM 32-09-04 . BITE CHECK OK,SHOWED DOOR CLOSED, TARGET TESTED GOOD, NO FURTHER ACTION.

Part: CREASE BEAM — CORRODED (BS 1400-1420) · airframe 77,840 hrs · 26,772 cycles

CORROSION ON THE MAIN CABIN RT CREASE BEAM BETWEEN BS 1400 AND 1420

Part: SEAT TRACK — CORRODED (BS 740) · airframe 77,840 hrs · 26,772 cycles

CORROSION ON SEAT TRACK AT BS 740, RBL 50. REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED IAW SRM 51-40-02 FIG 2 AND SRM 53 -30-52.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 77,840 hrs · 26,772 cycles

CORROSION ON SEAT TRACK AT BS 720, RBL 30. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 PAR 7 FIG 12.

Part: LIGHT — INOPERATIVE (R2 SLIDE) · airframe 76,759 hrs · 26,559 cycles

2R SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 73,983 hrs · 26,014 cycles

REPORT TO CREW AROUND ROW 2, A BURNING ODOR. ACCOMPLISHED OPERATION CHECK OF ALL SEAT MOTORS & LIGHTS AT ROWS 2 & 3, NOTHING INOPERATIVE. FLIGHT ATTENDANT REPORTED NO LIGHTS FLICKERING & NOTHING ABNORMAL. NO SMOKE, ODOR WAS AN ELEC ODOR FOR 2 MIN OR LESS. SUSPECT PAX CELL PHONE CHARGER WENT BAD, ATTENDANT REPORTED PLUGGED IN AT 2B.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 73,016 hrs · 25,828 cycles

EMERGENCY LIGHTS INOPERATIVE AT OVERWING EXITS LT FWD & RT AFT DOORS. SECURED CONNECTOR AT POWER SUPPLY 20 ABC. EXIT LIGHTS CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 70,212 hrs · 25,288 cycles

SMOKE DETECTOR ON FIRST CLASS LAVATORY INOPERATIVE. REPLACED SMOKE DETECTOR.

Part: COVER — MISSING (EXIT SIGN) · airframe 69,733 hrs · 25,195 cycles

EXIT SIGN COVER MISSING OVER DOOR 4L. REPLACED DOOR 4L EXIT SIGN COVER.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 69,372 hrs · 25,127 cycles

EMERGENCY EXIT SIGN LT FWD OF FWD OVERWING EXIT L778 IS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT L778 PCN 560-0798 IAW AMM 33-51-10-201, OPERATIONS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (CABIN) · airframe 68,702 hrs · 25,000 cycles

RT AFT ENTRY DOOR INDICATED ON EICAS. CLEANED & ADJUSTED GIRT BAR.

Part: APU — SHUTDOWN (APU BAY) · airframe 68,639 hrs · 24,988 cycles

WHILE STARTING THE NR 2 ENG, THE APU AUTO-SHUT DOWN. CREW DISCONTINUED NR 2 ENG START ATTEMPT. WITH THE ASSISTANCE OF THE CREW, THEY RESTARTED THE APU, ACP SECOND START ATTEMPT USING THE APU AIR SOURCE, SECOND NR 2 ENG START ATTEMPT WAS NORMAL, APU FUNCTION WAS NORMAL, OK TO CONTINUE.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 68,185 hrs · 24,900 cycles

CREW REPORTED SMOKE IN THE MID GALLEY OVEN AREA. FOUND HEATING ELEMENT CONTAMINATED BY GRAVY.

Part: CONTACT — DIRTY (L2 DOOR) · airframe 68,116 hrs · 24,880 cycles

2L WILL NOT ARM, ARM LIGHT INOPERATIVE. CLEANED ARM LIGHT CONTACTS & CYCLED ARMING LEVER SEVERAL TIMES. ARM LIGHT CHECKED GOOD. FOUND NO OTHER DEFECTS.

Part: INTERCOSTAL — CRACKED (BS 1200) · airframe 67,874 hrs · 24,832 cycles

MAIN CABIN INTERCOSTAL CRACKED BS 1200, BL 0, WL 208. R & R INTERCOSTAL IAW SRM 51-40-02 PARA 4 FIG 8 & DRAWING 140N2308.

Part: INTERCOSTAL — CORRODED (BS 1600 - 1620) · corrosion level 2 · airframe 67,874 hrs · 24,832 cycles

INTERCOSTAL BETWEEN BS 1600 - 1620 AT RBL 2 IN AFT CARGO PIT HAS CORROSION ON FWD LOWER END. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 PAR 4 FIG 4.

Part: SEAT TRACK — DAMAGED (BS400) · airframe 67,874 hrs · 24,832 cycles

CABIN SEAT TRACK BS 400 RBL 24.5 HAS A PREVIOUS BLEND ON UPPER FLANGE. R & R SEAT TRACK IAW DRAWING 141N5131.

Part: B-NUT — LOOSE (SLAT ACTUATOR) · airframe 67,692 hrs · 24,768 cycles

FLUID LEAKING OUT OF WEEP HOLE UNDER LT WING. FOUND 'B' NUT LOOSE ON NR 3 SLAT ACTUATOR. TIGHTENED 'B' NUT. OPERATIONS CHECKED NORMAL, NO LEAKS NOTED.

Part: BLADE — TORN (WINDSHIELD WIPER) · airframe 67,559 hrs · 24,722 cycles

CAPTAIN`S WIPER BLADE TORN. REPLACED CAPT WINDSHIELD WIPER BLADE IAW MM.

Part: WIRE — BROKEN (WATER HEATER) · airframe 67,522 hrs · 24,708 cycles

FOUND WIRE W2632-H-PR BROKEN AT WATER HEATER, NOT REPAIRABLE. REF WDM30-71-11, PG 4.

Part: MOTOR — FAILED (WINDSHEILD WIPER) · airframe 67,391 hrs · 24,667 cycles

F/O WINDSHIELD WIPER RUNS WITH SWITCH IN THE "OFF" POSITION. REPLACED F/O WINDSHIELD WIPER MOTOR, OPS CHECKED NORMAL.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 67,112 hrs · 24,581 cycles

R4 DOOR WILL NOT ARM. ADJUSTED GIRT BAR AND FLOOR FITTING. OPS CHECKED NORMAL.

Part: HEADSET — DEFECTIVE (COCKPIT) · airframe 67,074 hrs · 24,569 cycles

NR 1 PILOT'S HEADSET IS DEFECTIVE. REPLACED HEADSET.

Part: CIRCUIT BREAKER — DEFECTIVE (COCKPIT) · airframe 67,058 hrs · 24,562 cycles

CREW REPORTS MAIN BAT CHARGER EICAS STATUS MSG. FOUND CIRCUIT BREAKER C301, LEG A1 LOW VOLTAGE. REPLACED C-B C301 SYS OPS CKS NORMAL.

Part: CHARGER — FAILED (MASTER BATTERY) · airframe 67,018 hrs · 24,551 cycles

STATUS MESSAGE FOR MAIN BATTERY CHARGER. REPLACED MAIN BATTERY CHARGER IAW AMM. MESSAGE CLEARED AND CHARGER OPS CHECKED NORMAL.

Part: SWITCH — DIRTY (R2 DOOR SLIDE) · airframe 66,915 hrs · 24,521 cycles

R2 DOOR ARMED INDICATOR LIGHT INOPERATIVE. ALL OTHER INDICATIONS OPERATE NORMAL. CLEANED SWITCH AND LIGHT TESTED GOOD.

Part: BOLT — UNDERTORQUED (R1 WINDOW) · airframe 66,824 hrs · 24,491 cycles

R1 WINDOW HAS AN AIR LEAKING IN THE UPPER RT CORNER. PERFORMED PRESSURE LEAK CHECK PER AMM 05-51-24. FOUND LEAKS DUE TO WINDOW RETAINING BOLTS ARE UNDER TORQUED BY 15 TO 20 INCH POUNDS. TORQUED BOLTS AND LEAK CHECKED GOOD.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 66,790 hrs · 24,480 cycles

MAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY CHARGER.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR) · airframe 66,721 hrs · 24,457 cycles

L1 DOOR UNSECURE, POPS UP IN FLIGHT AND WILL NOT LOCK BACK DOWN. RETURNED TO FIELD. ADJUSTED DOOR MECHANISM IAW AMM 52-11-00 & 52-11-13. PRESSURIZED ACFT HANDLE STAYED DOWN IN LOCKED POSITION.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 66,721 hrs · 24,456 cycles

AFT CARGO DOOR SKIN LOWER AFT CORNER DAMAGED. REPAIRED DOOR IAW SRM 52-30-01 REPAIR 4 FIG 201.

Part: FRAME — DAMAGED (BS 1380) · airframe 66,721 hrs · 24,456 cycles

BS 1380 FRAME ANGLE DAMAGED. REPAIRED FRAME.

Part: SKIN — DAMAGED (BS 759) · airframe 66,721 hrs · 24,456 cycles

FUSELAGE SKIN BS 759, 9 INCHES BELOW S26L. INSTALLED REPAIR DOUBLER ON IAW SRM 53-00-01 REPAIR 2 FIG 201 TABLE V.

Part: SKIN — DAMAGED (BS 698-722 S27L) · airframe 66,721 hrs · 24,456 cycles

FUSELAGE SKIN BS 698-722 STR 27L DAMAGED. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 2. THIS CAT 'B' REPAIR IN ZONE A.

Part: SKIN — GOUGED (NR 2 NACELLE) · airframe 66,721 hrs · 24,456 cycles

TWO GOUGES IN O/B NR 2 PYLON SKIN. NAC STA 160, BL 16RT, WL 142. REPAIR PLYON SKIN IAW ECR A 5451-01120.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,721 hrs · 24,456 cycles

REPAIRED FUSELAGE SKIN AT BS 215.50, RBL 14 .10 RECEIVED 1ST& 2ND STG APPRL.

Part: SKIN — DENTED (BS 214) · airframe 66,721 hrs · 24,456 cycles

DENT IN FUSELAGE SKIN AT BS 214 AND 9 INCHES BELOW S22R. REPAIRED DENT IAW ECRA 5311-01594. ACCOMPLISHED HFEC OF CUTOUT IAW NDTM 51-00-16 & 51-00-19. NO CRACKS NOTED. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 710) · airframe 66,721 hrs · 24,456 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 710, EIGHT INCHES BELOW S27R. REPAIRED FUSELAGE SKIN IAW SRM REPAIR 2. ACCOMPLISHED HFEC IAW NDT 51-00-16 & 51-00-19.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 66,721 hrs · 24,456 cycles

AFT CARGO DOOR SKIN LOWER AFT CORNER IS GOUGED. INSTALLED REPAIR DOUBLER AT AFT CARGO DOOR SKIN LWR AFT CORNER IAW SRM 51-40-05 FIG 2, 51-40 -02 PARA 7, 4 AND 52-30-01 RPR 4 FIG 201. ACCOMPLISHED HFEC IAW ND T 51-00-19. NO CRACKS NOTED. MAJOR REPAIR.

Part: SKIN — DENTED (BS 358) · airframe 29,534 hrs · 10,803 cycles

FORWARD LOWER FUSELAGE HAS A SMALL DENT AT BS 358 AND S23R. INSPECTED DENT, NO CRACKS NOTED IAW HFEC. DENT IS WITHIN LIMITS OF SRM 53-00-01 & OK FOR CONTINUED SERVICE WITHOUT FURTHER ACTION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,721 hrs · 24,456 cycles

FUSELAGE SKIN DAMAGED. INSTALLED REPAIR IAW SRM 53-00-01 FIG 201 REPAIR 2.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 66,721 hrs · 24,456 cycles

CORROSION ON AFT CARGO DOOR SILL LOWER ANGLE. REPAIRED AFT CARGO DOOR SILL OUTBD DOOR SILL IAW ECRA 5300-01487. MAJOR REPAIR

Part: SKIN — GOUGED (BS 705 S27L) · airframe 66,721 hrs · 24,456 cycles

DEEP GOUGE IN FUSELAGE SKIN BS 705 S27L. INSTALLED REPAIR DOUBLER BS 698-722 IAW SRM 53-00-01 FIG 201 REPAIR 2. ACCOMPLISHED HFEC IAW NDT 51-00-16 & 51-00-19, NO CRACKS NOTED.

Part: SKIN — MISREPAIRED (BS 716) · airframe 66,721 hrs · 24,456 cycles

LIGHTNING STRIKE REPAIR AT BS716 .5" BELOW STR 27L DOESN'T MEET SRM REQUIREMENTS. *SUPPLEMENTAL DATA UPDATE* MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER TO FUSELAGE SKIN BS 698-722 STR 27L IAW SRM 53-00-01 FIG 201 RPR 2. ACCOMPLISHED HFEC IAW NDT 51-00-16 & 51-00-19.

Part: SKIN — GOUGED (BS 759) · airframe 66,721 hrs · 24,456 cycles

DEEP GOUGE IN FUSELAGE SKIN BS 759, 9 INCHES BELOW S26L. INSTALLED REPAIR DOUBLER ON SKIN IAW SRM 53-00-01 FIG 201 REPAIR 2. ACCOMPLISHED HFEC IAW NDT 51-00-19 & 51-00-16 NO CRACKS FOUND. MAJOR REPAIR.

Part: SKIN — GOUGED (BS 705 S27L) · airframe 66,721 hrs · 24,456 cycles

DEEP GOUGE IN FUSELAGE SKIN BS 705 ON S27L. INSTALLED REPAIR DOUBLER ON FUSELAGE SKIN AT BS 698 TO 722 S27L IAW SRM 53-00-01 FIG 201 REPAIR 2. HFEC INSPECTION ACCOMPLISHED IAW NDT MANUAL 51-00- 16, NO CRACKS NOTED. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1433) · airframe 66,721 hrs · 24,456 cycles

SKIN DAMAGED ACCOMPLISHED DOUBLER REPAIR AT BS 1433 PER SRM 53-00-01 REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 1680 S28L) · corrosion level 2 · airframe 66,721 hrs · 24,456 cycles

AFT CARGO BAY SHEAR TIE AT BS 1680 S28L CORRODED. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-40-07 PAR 4 FIG 5 AND PAR 7. MAJOR REPAIR.

Part: SKIN — GOUGED (BS 1160) · airframe 66,721 hrs · 24,456 cycles

FINE ROWS OF GOUGES BELOW ADF ANTENNA LBL 6 AT CROWN AREA BS 1160. REMOVED FINE GOUGES IAW SRM 51-10-02, PAR 6, FIG 1. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 646 S27R) · airframe 66,721 hrs · 24,456 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 646, SIX INCHES BELOW S27R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 201 REPAIR 3.

Part: SKIN — DAMAGED (BS 646 S27R) · airframe 66,721 hrs · 24,456 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 646, SIX INCHES BELOW S27R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-00-01 FIG 201 REPAIR 3.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 66,721 hrs · 24,456 cycles

R4 DOOR CUTOUT AFT FRAME INTERCOSTAL ATTACH TEE ANGLE NR 3 IS CRACKED. NR 3 TEE ANGLE REPLACED.

Part: FLOOR SUPPORT — DAMAGED (BS 365.25) · airframe 66,721 hrs · 24,456 cycles

MAIN CABIN BS 365.25 RBL 26 FLOOR SUPPORT DOUBLER HAS DOUBLE DRILLED HOLE. REPAIRED IAW ECRA 5315-01065. MAJOR REPAIR.

Part: SKIN — DEBONDED (NR 9 SLAT) · airframe 66,721 hrs · 24,456 cycles

DISBONDED NR 9 SLAT UPPER SURFACE T/E WEDGE 29 INCHES FROM O/B, 6 INCHES FROM AFT. REPAIRED IAW SRM 51-70-10 REPAIR 4 FIGURE 201.

Part: SKIN — DAMAGED (BS 1700 S17L) · airframe 66,721 hrs · 24,456 cycles

CREASE AT FUSELAGE BS 1700 S17L. REPAIRED AREA IAW SRM 53-00-01 FIG 201 REPAIR 3. NDT INSPECTED AREA BEFORE REPAIR WAS INSTALL IAW NDT MANUAL 51-00-19 AND 51-00-16 AND NO DEFECTS NOTED.

Part: AMPLIFIER — INOPERATIVE (PA/INTERPHONE) · airframe 66,259 hrs · 24,306 cycles

CABIN CREW REPORTED PA AND INTERPHONE INOPERATIVE. REPLACED AMPLIFIER, OPS CHECKED OK.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 66,215 hrs · 24,290 cycles

DOOR 4R IS DIFFICULT TO ARM. ARM LEVER FEELS LOOSE AND MUSHY WHEN ARMING THE DOOR. VERIFIED NO BLOCKAGE IN GIRT AND ARMING, CYCLED ARMING -DISARM SEVERAL TIMES, OPS SATISFACTORY. STIFFNESS RETURNED TWO FLT CYCLES LATER IN (LGA). MADE ADJUSTMENTS OF GIRT BAR ASSY PER AMM, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,678 hrs · 24,119 cycles

DOOR 4L OUTSIDE EMERGENCY LIGHT IS INOP. RELAMPED, OPS OK.

Part: HOUSING — DEFECTIVE (R2 DOOR) · airframe 65,450 hrs · 24,046 cycles

DOOR 2R ARM LIGHT INOPERATIVE. VERIFIED SLIDE ENGAGED. REPLACED LIGHT HOUSING ASSY. OPS CHECK DOOR, CHECK GOOD.

Part: RESERVOIR — DEPLETED (R4 DOOR) · airframe 64,752 hrs · 23,803 cycles

DOOR 4R IS EXTREMELY HARD TO ARM. FOUND DOOR EMERGENCY POWER RESERVOIR DEPLETED. REPLACED PER MM.

Part: RELAY — MALFUNCTIONED · airframe 64,454 hrs · 23,699 cycles

STATUS MESSAGE POWER TRANSFEER UNIT. TROUBLESHOT PER FIM 29-22-00 FIG 1 04. REPLACED RELAY RAN BOTH ENGINES AND NO EICAS MESSAGE.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 63,896 hrs · 23,517 cycles

NR 5 LE SLAT HAS 7 FOOT LONG DELAMINATION AFT OF LEADING EDGE. REMOVED NR 5 LE SLAT. REPAIRED SLAT PER MM.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 63,793 hrs · 23,488 cycles

ROW 12 AND ROW 40 FLOOR EMERGENCY EXIT LIGHTS MISSING END OF STRIP. REPLACED END CAPS 2 AT ROW 12 AND ROW 40 (PCN 160-7705).

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,439 hrs · 23,369 cycles

EXIT SIGN MISSING 4L. REPLACED LENS.

Part: CAP — MISSING (CABIN) · airframe 62,197 hrs · 22,918 cycles

EMERGENCY ESCAPE LIGHTING STRIP END CAPS MISSING NEXT TO 1B. REPLACED END CAP.

Part: CAP — MISSING (CABIN) · airframe 62,197 hrs · 22,918 cycles

EMERGENCY ESCAPE LIGHTING STRIP END CAPS MISSING AT 40C. REPLACED END CAP.

Part: CONNECTOR — NOT SEATED (COCKPIT) · airframe 62,132 hrs · 22,893 cycles

OVERHEAD PRESSURIZATION IND PNL INTEG LIGHTING IS 75 PCT INOP DIFF NEEDLE AND DIAL NOT ILLUM. COMPLIED WITH MEL. RESEATED CONNECTORS ON OVERHEAD PRESSURIZATION PANEL LIGHTING, OPS CHECKS GOOD.

Part: CONNECTOR — DAMAGED (LT SLIDE BOTTLE) · airframe 61,984 hrs · 22,840 cycles

LEFT SLIDE BOTTLE PRESS WILL NOT TEST. BOTTLE PRESSURE VERIFIED. READS 2725. FOUND PRESSURE SWITCH ON BOTTLE TO BE OPEN. CONDUCTED TROUBLESHOOTING OF LEFT INFLATION BOTTLE PRESSURE TEST LIGHT. FOUND CONNECTOR D5530 LEFT SLIDE BOTTLE PRESSURE, INTERMITTENT, DISCONNECTED & DISASSEMBLED. REPLACED CONNECTOR D5530 REF WDM.

Part: CLAMP — DAMAGED (NLG) · airframe 61,131 hrs · 22,535 cycles

NLG HARNESS CLAMP DAMAGED. REPLACED CLAMP IAW EG5122 NLG HARNESS CHECK.

Part: BEAR STRAP — CORRODED (BS 1400-1420) · airframe 60,932 hrs · 22,452 cycles

AFT CARGO BEAR STRAP BETWEEN BS 1400 AND BS 1420 RBL 23 HAS CORROSION. MAJOR REPAIR. REPAIRED BEAR STRAP AT AFT CARGO PER PD 57-53-140 AND EVA 80920.

Part: STRINGER — CORRODED (BS 1420 S29R) · airframe 60,932 hrs · 22,452 cycles

CORROSION ON STRINGER 29R AT STA 1420. MAJOR REPAIR. REMOVED CORRODED STRINGER AND FOUND OUT OF LIMITS. FABRICATED REPLACEMENT STRINGER, ACCOMPLISHED HFCF INSP AND FOUND CRACK FREE. INSTALLED STRINGER AND SPLICE REPAIR IAW SRM. TREATED & PRIMED IAW AMM MM.

Part: FLOORBEAM — CORRODED (BS 1681.8) · airframe 60,932 hrs · 22,452 cycles

CORROSION AT CABIN FLOOR SUPPORT SHEAR TIE STA 1681.8, BL 0 - RBL 40. MAJOR REPAIR. REPAIRED AFT DECK WEB AT STATION 1680 - 1690 RBL 27-53 IAW EA PD 57-53-134.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,932 hrs · 22,452 cycles

CORROSION INBD SEAT TRACK STA 676 TO 684 RBL 25 OUT OF LIMITS. SUPPLEMENTAL DATA UPDATE RPL'D SEAT TRACK BTW STA 640 - 695, RBL 25, RPR'D INTERCOSTAL BTWN STA 660 - 680, RBL 25, FABBED AND INSTALLED REPAIR ANGLE AND SHIM PER SRM.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 60,932 hrs · 22,452 cycles

CORROSION ON FLOORBEAM UPPER CHORD, BS 1660, LBL 9.5 - LBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION ON FLOORBEAM PER SRM. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA ON UPPER CHORD SAT 1660 LBL 12- LBL-27, NDT AND HFEC AREA AND FOUND IT TO BE CRACK FREE. FABRICATED DRILLED AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,501 hrs · 22,312 cycles

STA 365 FLOORBEAM UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED ON SM W-U E9952H PER SRM FROM LBL 8.5 TO RBL 59.

Part: FLOORBEAM — CORRODED (STA 1640) · airframe 60,501 hrs · 22,312 cycles

STA. 1640 FLOORBEAM CORR. 0 BL TO 59 RBL, TOP FLG. MAJOR REPAIR ACCOMPLISHED: REPAIRED PER SRM, REPAIR. NR 5, ON SM W-US E9906H, E9917H & E9959H.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 59,886 hrs · 22,076 cycles

1RT SLIDE LIGHT ABOVE DOOR, DIM WHEN SLIDE DISARMED. GIRT BAR DISARMS NORMALLY. CLEANED GIRT BAR PROX SENSOR, NO HELP. REPLACED "SLIDE" LIGHT CAP. OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 59,793 hrs · 22,039 cycles

EMERGENCY LIGHT INOP IN CABIN, JUST INBD OF AFT LAV. REPAIRED DAMAGE EMERGENCY LIGHT STRIP (FOUND UNPLUGGED).

Part: WINDOW — BURNED (COCKPIT) · airframe 59,787 hrs · 22,036 cycles

RIGHT FWD WINDOW-NOTICED 2 SCORCH MARKS LOWER PANE NEAR INBD WIPER BLADE. REPLACED WINDOW IAW MM.

Part: BOTTLE — UNDERSERVICED (OVERWING SLIDE) · airframe 59,686 hrs · 21,998 cycles

EMERGENCY ESCAPE TEST 2 LIGHT INOP. TEST 2L LIGHT INOP DURING TEST. BOTTLE PRESSURE INDICATES 2600 PSI 29F. BOTTLE LOW PRESSURE INDICATION SYS STILL WILL NOT TEST. SERVICED LT SLIDE OVERWING BOTTLE. REARMED OFF WING ESCAPE SLIDE SYS.

Part: BOTTLE — NO TEST (OVERWING SLIDE) · airframe 59,615 hrs · 21,972 cycles

RT OVERWING SLIDE BOTTLE DOES NOT TEST ON P32 PANEL, TEST 2. REPLACED SLIDE INFLATION PRESSURE BOTTLE ASSY.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 59,375 hrs · 21,885 cycles

FOUND CAPTAINS SLIDING WINDOW DIFFICULT TO OPEN THE FIRST TIME AFTER THE AIRCRAFT IS PRESSURIZED. AFTER THAT IT OPENS EASILY, ADJUSTED LOWER LINK ARM. PRESSURIZED ACFT TO 1.5 PSI AND WINDOW WAS DIFFICULT TO OPEN AND NEEDED MORE THEN THE 7LBS MAXIMUM ALLOWED PER THE ABOVE AMM. ADJUSTED WINDOW PER MM. PRESSURIZED, NO HELP. FOUND LOWER CAM LOCK RUBBING ON FRAME NEXT TO CAM LOCK STUD. ADJUSTED VERTICAL ADJUSTMENT REF MM. PRESSURIZED TO 2.5. WINDOW UNLOCKS AND OPENS NORMAL.

Part: SKIN — SCRATCHED (BS 392 S16L) · airframe 59,248 hrs · 21,844 cycles

ON WALK AROUND FOUND SCRATCH ON FUSELAGE 1 FOOT AFT AND 6 INCHES ABOVE LOWER EDGE OF DOOR 1L. REPAIRED IAW UA-EVA-80245. AT STA 392, STR 16L, 2 EA BLIND BOLTS INSTALLED.

Part: FUEL/OIL COOLER — FAULTY (ENGINE) · airframe 59,145 hrs · 21,801 cycles

NUMBER 2 HOC. DUE TO 8 QTS OIL ADDED AND OIL USAGE TRENDING UP PERFORM HOC TROUBLESHOOTING PER MM, BAG & BREATHER CHECK. RUN ENGINE AT 80% N2 FOR 10 MINUTES. REPAIR ANY LEAKS FOUND. IF UNABLE TO RUN AT HIGH-POWER, ACCOMPLISH STATIC LEAK CHECK (GEARBOX PRESSURE CHECK) PER MM. ACCOMPLISHED HOC CHECK. NO LEAKS NOTED. REMOVED FUEL OIL HEAT EXCHANGER ASSY WITH BYPASS VALVE, BUILD UP NEW ASSY IAW. REPLACED FUEL-OIL HEAT EXCHANGER ASSY WITH BYPASS VALVE ASSY IAW MM. RAN ENGINE PER JRH, OP CHK LEAK OKAY.

Part: LIGHT — UNSECURE (FWD CABIN) · airframe 58,920 hrs · 21,718 cycles

FWD CABIN EMERGENCY LIGHTS LOOSE AND CATCHING ON SECONDARY BARRIER. SECURED EMERGENCY STRIP AT FWD CLOSET.

Part: GATE — CRACKED (PAX DOOR) · airframe 58,886 hrs · 21,709 cycles

MAIN ENTRY DOOR 1 RT UPPER GATE IS CRACKED IN 2 LOCATIONS. REPLACED GATE ASSY.

Part: MECHANISM — LACK OF LUBE (SLIDE ARMING) · airframe 57,944 hrs · 21,371 cycles

DOOR 4 RT IS HARD TO ARM AND DISARM. REMOVED SLIDE AT DOOR 4R FOR ACCESS TO LUBE ARMING MECH. REINSTALLED SAME SLIDE REF MM 25 -66-01 ARMING OPS GOOD. IN PRESENTS OF A INSPECTOR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,634 hrs · 21,255 cycles

EMERGENCY LIGHT ABOVE 21ABC INOP DURING TEST. REPLACED M735 EMERGENCY LIGHTS PWR SUPPLY, LITE OPS RETURNED TO NORMAL DURING TEST.

Part: DOOR — BINDING (R2) · airframe 57,570 hrs · 21,231 cycles

DOOR 2L WILL NOT OPEN FROM OUTSIDE WITHOUT ASSISTANCE. YOU CAN BOUNCE THE DOOR HARD TO GET IT TO BREAKOVER AND OPEN OR PUSH FROM INSIDE. ALSO HAS A POPPING SOUND. IT STICKS IN THE HALFWAY OPEN POSITION. DOOR 2R REMOVED FOR REPAIRS. WORKING HINGE REPLACEMENT ON AIRFRAME AND BEARING REPLACEMENT ON DOOR HANDLE. DOOR HANDLE BEARINGS DONE AND SOLD TO INSP LWR CAM PLATES INSTALLED ON FRAME. STARTED DOOR INSTALLATION UPPER AND LOWER BOLTS INSTALLED, LWR GUIDE ARM 3 BOLTS INSTALLED, 4TH BOLT NEEDS INSTALLED AND DOOR RIG. INSTALLED DOOR AND RIGGED UP TO STEP 5(I) P514 OF MM. CONTINUED WITH DOOR RIG THRU STEP 2.G.5(K). ACP'D INSTALLATION OF DOOR THRU END OF MM.

Part: CONTROLLER — FAULTY (COCKPIT WINDOW) · airframe 57,479 hrs · 21,198 cycles

WINDOW EICAS MSG DISPLAYED. POSITION 4.(1=L FWD, 2=L SIDE, 3=R FWD, 4=R SIDE) INOP LGT ILLUM. INOP LGT DID NOT EXTINGUISH WHEN SW WAS RECYCLED TO OFF THEN ON. BITE SHOWS CONTROL UNIT FAULT. OTHER WINDOWS HEAT OK. SUSPECT 563-9025. NO BURNING OR ARCING NOTICED IN WINDOW. RPL WINDOW HEAT CONTROLLER IAW MM. BIT TEST FAULTS NR 2 WINDOW. CK'D FOR PWR & GRD AT WINDOW. GOOD GRD, NO POWER. NR 3 WINDOW PWR & GRD CHECKED GOOD. REINSTALLED ORIGINAL HEAT CONTROLLER. CHANGED MEL TO 3041N. FOUND CRACK RUNNING THROUGH TERMINALS J6, J7, J8 TO EDGE OF RT SLIDING WINDOW. REPLACED RT SLIDING WINDOW.

Part: COVER — MISSING (CABIN) · airframe 57,316 hrs · 21,143 cycles

EEL LIGHT STRIP COVER ABOUT 15 INCHES OF THE AFT SECTION OF COACH MISSING. REPLACED MISSING EEL LIGHT COVER IN LAST 15 INCHES OF COACH SECTION.

Part: SWITCH — FAULTY (L3 DOOR SLIDE) · airframe 56,657 hrs · 20,880 cycles

DOOR 3L SLIDE ARMED CONDITION LIGHT ABOVE DOOR INOP. SWITCHED LENS COVERS WITH DOOR 3L, NO HELP. REPLACED SWITCH S10222, TESTS OK. COMPLETED RII INSP OF 3L SLIDE ARMING INDICATION, ALL OPS NORMAL.

Part: SLIDE — FAULTY (L4 DOOR) · airframe 56,647 hrs · 20,876 cycles

DOOR 4L SLIDE NEEDS REPLACEMENT. REPLACED SLIDE. ACCOMPLISHED RII INSTALLATION INSPECTION OF NR 4 SLIDE. NO DEFECTS NOTED.

Part: RESERVOIR — UNKNOWN (PAX DOOR) · airframe 56,647 hrs · 20,876 cycles

NR 4L PASSENGER DOOR EMERGENCY POWER RESERVOIR NEEDS REPLACEMENT. REPLACED IAW MM 52-11-30. OPS CHECKED GOOD.

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 56,501 hrs · 20,814 cycles

EMERGENCY ESCAPE PATH LIGHTING STRIP INOP NEXT TO FWD CLOSET. CABLE FOUND FAULTY. ADJUSTED/SPLICED CABLE, OP CHKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,501 hrs · 20,814 cycles

EMERGENCY ESCAPE PATH LIGHTING STRIP INOP NEXT TO FWD AFT LAV. REPLACED AFT EMERGENCY LIGHT STRIP, CHECKS OK.

Part: FRAME — CORRODED (BS 1680 S29-30R) · airframe 55,402 hrs · 20,378 cycles

FOUND CORROSION ON FRAME AT STA 1680 BETWEEN STR 29 RT AND STR 30. MAJOR REPAIR ACCOMPLISHED: PERFORMED A GVI OF FUSELAGE STRUCTURE BETWEEN BS 1664-1700 AND STR 26L-26R. FOUND CORROSION ON FRAME, BS 1681 AND SHEAR TIE BETWEEN ST R-27L-28L. REMOVED FRAME AND FABRICATED A NEW FRAME PER BAC DWG 146N1032-3, REV B AND INSTALLED PER BAC DWG 146N1025, REV C AND SRM 51-40-2.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 55,397 hrs · 20,377 cycles

FOUND CORROSION AFT PIT AFT OF AFT BULKHEAD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,397 hrs · 20,377 cycles

EMERGENCY LIGHT STRIP BETWEEN SEATS 16 AND 23 INOP. REPLACED STRIP. ALL OPS NORMAL.

Part: FRAME — CORRODED (BS 1680 S29R) · airframe 55,397 hrs · 20,377 cycles

AFT LOWER FUSELAGE INTERNAL BILGE AREA, SHEAR TIE FWD FACE HAS CORROSION, BS 1681, STR 27L-28L. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE PER BAC DWG 140N2002-1011 AND INSTALLED.

Part: OXYGEN SYSTEM — LOW PRESSURE · airframe 54,146 hrs · 19,857 cycles

OXYGEN SYSTEM PRESSURE LOW AT 1200. SERVICED TO FULL AT 1750 PSI.

Part: POWERPACK — FAULTY (CABIN) · airframe 53,965 hrs · 19,791 cycles

MID LAV FWD EMERGENCY LOCATOR SIGN STA 697 FACING FWD EXIT SIGN INOP, CHECKED POWER AVAILABLE AT DISCONNECT IN CEILING PANEL AREA IS 4.5 VOLTS NEED NEW SIGN OR OPEN IN WIRING TO SIGN. REPLACED EMERGENCY POWER PACK AND BATT AT FWD CTR ENTRY WAY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,965 hrs · 19,791 cycles

DOOR 1R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK NORMAL.

Part: EXTINGUISHER — LEAKING (FWD GALLEY) · airframe 53,732 hrs · 19,702 cycles

FWD GALLEY WATER FIRE EXT LEAKING. REPLACED WATER FIRE EXTINGUISHER.

Part: O-RING — LEAKING (EVAC SLIDE)

DOOR 2 SLIDE LOW BOTTLE. BOTTLE TO VALVE O-RING LEAKING. REPLACED BOTTLE.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 51,006 hrs · 18,702 cycles

CREW O2 READING 1200 (LOW). CAUSE, UNKNOWN. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE.

Part: PROXIMITY SWITCH — FAILED (L2 DOOR SLIDE) · airframe 50,967 hrs · 18,687 cycles

NO SLIDE ARMED LIGHT 2L. FOUND PROXIMITY SWITCH FAILED. REPLACED PROX SWITCH "A" S10218, OPS CHECKED GOOD.

Part: HOSE — DEFECTIVE (COCKPIT) · airframe 50,006 hrs · 18,330 cycles

OXYGEN MASK HOSE DEFECTIVE AT 1(1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS: CAPT O2 MASK DOES NOT FIT SNUG OR HOSE COMPLETELY INFLATE WHEN PUT ON. FOUND DIAPHRAGM STIFFENED PER SHOP FINDINGS. REPLACED MASK ASSY.

Part: STRUCTURE — CORRODED (RT LE SLAT) · airframe 49,365 hrs · 18,113 cycles

FLT DIVERTED DUE TO RIGHT L/E SLAT MATERIAL LIBERATION. THE RIGHT SLAT BETWEEN THE ENGINE AND THE FUSELAGE WAS DISINTEGRATING. AT THE TIME OF THE RADIO PATCH THE AIRCRAFT HAD A 12 X 8 X 2 INCH PIECE MISSING FROM THE SLAT. MAJOR REPAIR ACCOMPLISHED. THE PRIMARY FAILURE MODE IS MOISTURE INGRESSION. THIS LED TO CORROSION OF HONEYCOMB AND A WEAKENED BONDING RESULTING IN HONEYCOMB PULLING OUT OF ADHESIVE FILLETS. THE LAST SHOP REPAIR DID NOT REPLACE ALL OF THE HONEYCOMB SECTIONS. APPLIED FIBERGLASS REPAIR TO TWO INBOARD AREAS OF DELAMINATION AND CONTOURED HONEYCOMB ON 4 OUTBOARD REPAIRS AND SANDED PAINT FROM REPAIR AREAS.

Part: WHEEL — VIBRATES (NLG) · airframe 49,205 hrs · 18,049 cycles

NOSE WHEEL VIBRATES AT GEAR RETRACTION.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 49,146 hrs · 18,028 cycles

FLT EXPERIENCED OZONE ENCOUNTER. DESCENDED TO FL290. FLIGHT CREW WAS ON O2 FOR A SHORT DURATION DUE TO STRONG ODOR IN THE COCKPIT. COCKPIT OXYGEN PRESSURE WAS AT 1070 PSI, BELOW MINIMUM SPECIFICATIONS. SERVICED OXYGEN. CAUSE OF ODOR NOT ESTABLISHED.

Part: FAN — ODOR (CABIN) · airframe 48,868 hrs · 17,930 cycles

OILY ODOR ON TAKEOFF AND CLIMB. PRETTY STRONG ODOR. TURNED THE RT RECIRCULATION FAN OFF. LESSENED THE ODOR.

Part: WIRE HARNESS — CHAFED (LAVATORY TANK) · airframe 46,271 hrs · 16,994 cycles

LAV K WIRE HARNESS BURNT AT LAV TANK DUMP VALVE CABLE BRACKET. 6-8 WIRES BURNED THROUGH AND BIRDCAGE. WIRING HARNESS WAS CHAFED THROUGH BY LAV TANK DUMP CABLE. HARNESS WAS NOT SECURED PROPERLY AWAY FROM THE CABLE DURING PREVIOUS OVERHAUL. CABLE MOVED EVERY TIME THE TANK WAS DUMPED AND GRIND AWAY AT THE HARNESS UNTIL IT MADE THROUGH THE INSULATION. REPLACED WIRE HARNESS 2 FT PIGTAIL FABRICATED FOR P4 AND P5 TO SPLICE INTO HARNESS. IMPLEMENTED PIGTAIL FABRICATION. PULLED AND COLLARED P34 AV FILL VALVE C-B AND FILL CONTROL LAV CIRCUIT BREAKERS. A NEW STEP ADDED TO ROUTINE CARDS TO INSURE HARNESS IS SECURED AWAY FROM CABLE.

Part: UNKNOWN — UNKNOWN (CABIN TEMP) · airframe 44,690 hrs · 16,406 cycles

DIVERTED DUE TO DIFFICULTY MAINTAINING CONTROL OVER THE AFT CABIN TEMP.

Part: DUCT — LOOSE (CABIN AIR) · airframe 44,691 hrs · 16,407 cycles

RETURNED TO THE FIELD AT ORD AFTER A DUCT CAME LOOSE IN THE AFT CABIN CEILING.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 42,360 hrs · 15,575 cycles

RETURNED TO ANC UNDER AN AMBER ALERT DUE TO A HYDRAULIC PROBLEM. LEFT HAND ENGINE HYDRAULIC PUMP FAILED. REPLACED LEFT HAND PUMP PER MM29-11-05. ALSO REPLACED PRESSURE FILTER AND CASE DRAIN FILTERS. CHECKED AND REPLACED ELECTRIC HYDRAULIC PUMP CASE DRAIN FILTER PRECAUTIONARY, NO METAL FOUND. RETURNED AIRCRAFT TO SERVICE.

Part: TERMINAL BLOCK — CRACKED (LT GENERATOR) · airframe 41,643 hrs · 15,297 cycles

RETURNED TO FIELD DUE TO MULTIPLE CB'S TRIPPED PRIOR TO ROTATION, MULTIPLE EICAS MSG'S. LEFT GENERATOR CONTACTOR, C901, PHASE -B- TERMINAL LUG WAS FOUND CRACKED / BROKEN, PROMOTING ELECTRICAL PROBLEMS AND CAUSING SOME CIRCUIT BREAKERS TO POP. THE TERMINAL LUG WAS REPLACED, THE AFFECTED C/BS WERE RESET AND CORRESPONDING SYSTEM OPS CHECKS WERE DONE AND AIRCRAFT RETURNED TO SERVICE.

Part: RESERVOIR — LOW (SLIDE)

FILL ON LOW SIDE OF GREEN BAND WITHIN MANUAL TOLERANCE. SLIDE WAS REMOVED FROM AIRCRAFT DUE TO LOW INFLATION CYLINDER PRESSURE. WHEN RECEIVED AT COMPONENT SHOP, PRESSURE INDICATOR NEEDLE WAS REPORTED TO STILL BE WITHIN THE GREEN 'GO' BAND. RESERVOIR PRESSURE WAS TOPPED-OFF AND NO LEAKS WERE DETECTED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 37,903 hrs · 14,542 cycles

AFT RT GALLEY AREA, STA 1700 BETWEEN RBL 42 AND RBL 56, DOUBLER PLATE CORRODED, (FLOOR DOUBLER). CORROSION DAMAGE FOUND. AFT DECK PLATE REPAIRED USING DOUBLER AND TRIPLER. PIN BEAM WAS REPLACED, AND A REPAIR TO THE BS 1701 FLOOR BEAM WEB ACCOMPLISHED FOR ACCESS TO REMOVE THE PIN BEAM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

LEFT FUSELAGE SKIN DENTED AT FRAME STA 761, BETWEEN STRINGERS 16L AND 15L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER - TRIPLER AND FILLERS.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

AFT PIT FRAME DENTED BS 1500 STR 25L TO STR 26L. INSTALLED "J" ANGLE REPAIR.

Part: SWITCH — SHORTED (L4 DOOR SIGN) · airframe 39,703 hrs · 14,542 cycles

EMERGENCY LIGHT TEST SWITCH AT 4L DOOR IS INOPERATIVE, SHORTED S10295. *S/D* REPLACED SWITCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

FLOORBEAM T-CAP AT BS 324, RBL 55 TO RBL 60 IS CORRODED. SPLICED IN A NEW PORTION OF THE FLOORBEAM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

AFT PIT AT STA 1415 BETWEEN STRINGER 26R & 27R BEAR STRAP CORRODED. AREA FASTENER WERE REMOVED AND CORROSION WAS BLENDED AND REMOVED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

AFT PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT AREA OF DAMAGE. FABRICATED AND INSTALLED NEW SPLICE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

AFT PIT STA 1420 ABOVE STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALLED SPLICE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

AFT PIT FRAME DENTED ON INBOARD FLANGE AT STA 1520 BETWEEN STR 25L AND 27L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALLED SPLICE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,703 hrs · 14,542 cycles

FLOORBEAM T-CAP AT BS 365 RBL 0 TO RBL 64 R CORRODED SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 37,553 hrs · 13,797 cycles

LEFT WING INBOARD TRAILING EDGE AFT FLAP IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FLAP PER SRM 57-53-01 AND TIMCO REO (EVA) G-09637.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,553 hrs · 13,797 cycles

DENT ON LEFT SIDE OF FUSELAGE, MEASURES .125 INCH DEEP BY 3 INCH WIDE, LOCATED AT BS 610 BETWEEN STR 15L-16L JUST BELOW WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,553 hrs · 13,797 cycles

CORROSION FOUND ALONG AFT PIT LOWER DOOR SILL, ADJACENT STRINGER 26R, BS 1380-1440. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW STRAP REPAIR.

Part: ENGINE — FAILED (NR 2) · airframe 35,430 hrs · 12,977 cycles

AIRCRAFT LOST NR 2 ENGINE AT ROTATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,534 hrs · 10,803 cycles

FUSELAGE SKIN DAMAGED STA 580 STR 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: HOUSING — LOOSE (APU COMPRESSOR) · airframe 28,170 hrs · 10,313 cycles

APU SHUTDOWN INFLIGHT. SUPPLEMENTAL DATA UPDATE FOUND DRIVEN COMPRESSOR ON APU SCROLL HOUSING P/N 3826140-5, WITH BOLT INSERTS LOOSE AND THREADS DAMAGED. THE BACKSHROUD BOLTS P/N MS9489-27 WERE TORQUED TO SPECIFIC VALUES, BUT STAT-O-SEALS WERE NOT CRUSHED. OIL LEAKED PAST THE STAT-O-SEALS, INTO THE BLEED DUCT AIR STREAM, THROUGH THE IMPELLER DIFFUSER. THE APU AUTO SHUTDOWN FOR LOW OIL PRESSURE.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

CREW REPORTED, ELECTRICAL SMELL IN COCKPIT. SMELL INTERMITTENT.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE LIGHT STRIP AT THRESHOLD OF AFT LAV INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP AT AFT LAV THRESHOLD WITH NEW LIGHT ASSEMBLY, OPERATION CHECKS NORMAL.

Part: COOLING FAN — FAILED (APU)

SMOKE IN AFT AND F0RWARD CABIN AFTER LEVEL OFF AT 37,000 FEET. SMOKE BEGAN TO DISSIPATE AT 24,000 FEET IN DESCENT AND CLEAR AT 10,000 FEET. FLIGHT DIVERTED TO PHX. THE APU HAD A SEVERE COOLING FAN FAILURE WHICH CAUSED OIL TO LEAK INTO THE INLET PLENUM, CONTAMINATING THE AIR CONDITIONING SYSTEM. THE COOLING FAN HAD THE SHROUDED ROTOR. THE APU ALSO SUSTAINED FOREIGN OBJECT DAMAGE TO THE COMPRESSOR IMPELLERS. PART TOTAL CYCLES, 2,599.