N14871

Part: ANGLE — CORRODED (STA 1338) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND AFT PRESSURE BULKHEAD ANGLE CORRODED AT STA 1338, LONGERON 28R TO 30. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30.

Part: SKIN — GOUGED (STA 1338) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT JACK POINT, STA 1338. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 9.

Part: SKIN — DELAMINATED (FLAP VANE) · airframe 50,675 hrs · 28,919 cycles

MAINTENANCE FOUND THE L/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED . THE FINAL TRIM OUT AREA MEASURED 4.7" X 5.6". THE SKIN WAS REPAIRED IAW ECRA 5750-03755.

Part: SKIN — CRACKED (STA 1338) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND 0.01" CRACK IN FUSELAGE SKIN AT STA 1338 BELOW LONGERON 4R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.

Part: SKIN — CRACKED (STA 1338) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND A 0.01" CRACK IN FUSELAGE SKIN AT STA 1338, LONGERON 10R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.

Part: SKIN — DELAMINATED (FLAP VANE) · airframe 50,675 hrs · 28,919 cycles

MAINTENANCE FOUND THE R/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED. THE FINAL TRIM OUT AREA MEASURED 4.3" X 6.4". THE SKIN WAS REPAIRED IAW ECRA 5750-03756.

Part: SKIN — CRACKED (MAIN CAB DR) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND A 1/4" CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AT LOWER FORWARD CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05.

Part: BELTFRAME — CRACKED (STA 1416) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1416, LONGERON 4L TO 4R. INSTALLED NEW FRAME IAW SRM 51-00.

Part: BELTFRAME — CRACKED (STA 1446) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1446, LONGERON 6R TO 5L. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN TRACK HOLES CORRODED AT STA 1136 - 1155. A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 53-23-00.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,675 hrs · 28,919 cycles

INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK HOLES CORRODED BETWEEN STA 1231-1271. THE TIE DOWN TRACK WAS REPLACED IAW SRM 53-23-0.

Part: LINK — FAILED (NLG FWD DOOR) · airframe 48,322 hrs · 27,395 cycles

WHEN THE GEAR WAS RAISED AFTER TAKEOFF, THE GEAR RETRACTED WITH ALL INDICATIONS NORMAL. THERE WAS A LOUD NOISE INDICATIVE OF THE NOSE GEAR DOOR HANGING DOWN AND WHICH WAS ACCOMPANIED BY STRONG VIBRATION IN THE NOSE GEAR AREA. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE R/H NLG FORWARD DOOR LINK AT FAULT. THE DOOR LINK WAS REMOVED AND REPLACED IAW MM 32-22-01, PAGE 202 AND RIGGING WAS PERFORMED IAW MM 32-22-01, PAGE 202. THE GEAR WAS CYCLED AND OPERATION CHECKED NORMAL.

Part: SLIDE — FAILED (R1 DOOR) · airframe 48,228 hrs · 27,339 cycles

THE R-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.

Part: SLIDE — FAILED (L1 DOOR) · airframe 48,228 hrs · 27,339 cycles

THE L-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,959 hrs · 26,625 cycles

THE LT AND RT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE DURING TEST. THE B5-103 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,738 hrs · 25,932 cycles

INSPECTION FOUND FORWARD ENTRY PORTABLE EMERGENCY LIGHT INOPERATIVE. THE FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-53-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 41 - 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 140 - 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FORWARD RT SIDE CARGO TRACK IN MID PIT CORRODED AT STA 541 - 636. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 200, LBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: STRAP — CORRODED (CARGO DOOR) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND AFT CARGO LOWER DOOR JAMB CORRODED AT FS 1155 - 1211. THE CORRODED STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND ECRA 5310-03027.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 150 - 200, LBL 7 AND RBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, 51-30-5, AND 51-30-1.

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND MID CARGO LOWER DOOR JAMB CORRODED AT FS 640 - 690. THE CORRODED STRAP WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-7, AND 51-10-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RT CUSP WEB CORRODED UNDER FLOOR SUPPORT AT FS 1136 - 1155. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, LBL 11 AND LBL 3 - RBL 3. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND L-1 DOOR JAMB TORQUE BOX SKIN AFT LEG CRACKED AT FS 200. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0781, SRM 51-10-3, 51-30-3, 51-30-2, AND ECRA 5310-04051.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND THREE 2 INCH CRACKS IN LT SIDE VENT BOX AREA UPPER AFT CORNER WEB AT FORWARD SIDE OF FRAME STA 1485. THE CRACKS WERE STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1251 - 1271 BETWEEN LONGERON 22R AND 23R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 20, 51-10-4, 51-10-3, AND 51-30-2.

Part: FLOOR SUPPORT — PUNCTURED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT ANGLE PUNCTURED AT STA 541, L28R TO 28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, FIGURE 7A, AND 51-10-4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE LOWER T-FITTING CRACKED AT FS 864, LONGERON 30. THE T-FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED AT FS 37 BETWEEN LONGERON 6R AND 18R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-60, 53-01, FIGURE 7, 51-10-3, AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AND GOUGED AT FS 290 BETWEEN LONGERON 23L AND 24L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, VIEW 1.

Part: PAN — CRACKED (RT MLG DOOR) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 1 INCH CRACK IN RT MLG I/B DOOR FORWARD SIDE TOP CORNER. THE DOOR PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-30-2, AND 51-30-5.

Part: WEB — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CORROSION ON SUB FLOOR AND UNDER CUSP WEB AT FS 175, LBL 54. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-4, 53-14-1, 51-10-3, 51-30-2, AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD FRAME SUPPORT ANGLE AT FS 229 - 256, LONGERON 1L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL EDGE AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 798. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE TRACK WAS TREATED AND PRIMED FROM FS 522 - 617 AND FROM 700 - 798. FS 617 - 700 WAS FOUND OUT OF LIMITS. A REPAIR TRACK WAS INSTALLED FROM FS 617 - 700 USING REPAIR SPLICES IAW SRM 51-10-4, 53-05, FIGURE 46, 51-10-3, 51-30-2, AND 51-30-1.

Part: FRAME — CORRODED (WINDOW) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CABIN WINDOW FRAME 41L CORRODED ON FORWARD AND AFT FLANGES AT STA 984 AND 1003. A REPAIR AND WINDOW DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0794, ECRA 5330-02998, AND DOUGLAS DRAWING SRO9530053.

Part: WEB — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND SUBFLOOR WEB CORRODED AT FS 218, RBL 11 UPON REMOVAL OF GALLEY SUPPORT AND FITTING. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AND 51-30-8.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND R-1 DOOR JAMB AT AFT CENTER AREA MAIN FRAME BEHIND ROLLER ASSEMBLY DENTED IN RADIUS. THE DOOR STOP WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 42, 51-30-1, AND 51-30-2. A NEW DOOR STOP WAS INSTALLED IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-30-5, AND 51-10-3.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 2.5 INCH CRACK AT FWD END OF DOUBLER ON LT HORIZONTAL STABILIZER LOWER BANANA FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 55-02, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2 AND 51-10-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN UNDER FWD WING TO BODY FAIRING CORRODED AT STA 769 BETWEEN STRINGERS 28R AND 27R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 53 AND FILLET ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 170 BETWEEN LONGERONS 20R - 21R. THE DENTED AREA WAS REPAIRED WITH A DOUBLER IAW SRM 53-04, FIGURE 38G.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 2 INCH CRACK AT FWD END OF DOUBLER ON RT HORIZONTAL STABILIZER LOWER BANANA FAIRING. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 55-01, FIGURE 2.

Part: PAN — CHAFED (CARGO DOOR) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND AFT CARGO DOOR PAN AROUND STOP PADS CHAFED AT 13 LOCATIONS. REPAIRS WERE INSTALLED IAW ECRA 5230-01554 AND SRM 52-03, FIGURE 8.

Part: TAB — DENTED (RUDDER) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RUDDER TAB DENTED ON RT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE RUDDER TAB WAS REPAIRED IAW SRM 51-30-3. THE RUDDER AB WAS REINSTALLED IAW MM 27-20-02. A WEIGHT AND BALANCE WAS PERFORMED IAW SRM 55-40-01.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND THE LT NR 3 SLAT DENTED ON THE LEADING EDGE. THE SLAT WAS REPAIRED IAW SRM 57-06, FIGURE 1 AND ECRA 5720-01170.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RIGHT I/B HORIZONTAL STABLIZER LEADING EDGE SKIN DENTED. THE DENTED AREA WAS TRIMMED OUT. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, ECRA 5513-01006, AND EA 9-5512-A0795.

Part: SKIN — CHAFED (VERTICAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A HOLE CHAFED THROUGH VERTICAL STABILIZER SKIN AT UPPER LT SIDE ABOVE RUDDER FAIRING. A FREEZE PLUG AND DOUBLER WERE INSTALLED IAW EA 9-5532-2-A0792.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A .5 INCH CRACK IN LOWER FUSELAGE LT INSIDE BRACKET AT KEEL CENTER, FS 940. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 53-01, FIGURE 2.

Part: ACCESS DOOR — CHAFED (TAIL CONE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND TAIL CONE ACCESS DOOR FORWARD LIP CHAFED THROUGH AND KNIFE EDGED. THE CHAFED AREA WAS CUT OUT AND TWO DOUBLERS WERE INSTALLED IAW SRM 52-01, FIGURE 4 AND 51-30-2.

Part: DOUBLER — CHAFED (VERTICAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RT SIDE UPPER VERTICAL STABILIZER DOUBLER CHAFED ABOVE RUDDER FAIRING. THE FAIRING WAS REMOVED IAW SRM 51-30-1. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND EA 9-5532-2-A0792. REINSTALLED FAIRING IAW SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: SKIN — CHAFED (RT WING LE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RT WING FIXED LEADING EDGE CHAFED I/B OF TRACK NR 13. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 57-01, FIGURE 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200 - 218, LBL 15. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND DENTS IN LT I/B HORIZONTAL STABILIZER LEADING EDGE SKIN. A SKIN DOUBLER REPAIR WAS INSTALLED IAW EA 9-5512-A0792, DRAWING SRO9550009, SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND ECRA 5513-01006.

Part: CHANNEL — GOUGED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND LT SIDEWALL SUPPORT CHANNEL GOUGED IN TAIL COMPARTMENT AT STA 1401. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-02, FIGURE 3, 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180, LBL 52. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOORBEAM WEB CORRODED JUST UNDER SUB FLOOR MEMBRANE AT FS 200, LBL 54. REPAIRED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND AFT CARGO DOOR SKIN CREASED IN FORWARD MID AREA. THE CREASED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 1. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 1 AND 51-10-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RT CARGO TRACK IN MID PIT CORRODED BETWEEN STA 769 AND 788. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 200, LBL 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FORWARD PIT LT CARGO TRACK CORRODED AT STA 418 - 484. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 148, LONGERON 18L. THE DENT WAS COLD WORKED AND BLENDED IAW SRM 53-01, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW EA 9-5331-2-A0789, SRM 51-10-3, AND 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND THE FUSELAGE LOWER ANTENNA BASE CORRODED AT FS 617, 645, AND 685. THE ANTENNA BASES WERE REMOVED AND NEW ONES WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 51-40-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT FS 256 - 280. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 53-05, FIGURE 4F AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 37, LT SIDE. DOUBLERS WERE INSTALLED IAW SRM 53-30-0, FIGURE 1A, 53-05, FIGURE 4, 51-10-3, AND 51-30-2.

Part: STRAP — CORRODED (CARGO BAY) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND AFT CARGO PIT CEILING O/B CENTER SUPPORT CORRODED AT STA 1174. THE CEILING STRAP SUPPORT WAS REMOVED IAW SRM 51-30-5. A DOUBLER AND CEILING STRAP WERE INSTALLED IAW SRM 53-05, FIGURE 86, PAGE 1, 51-30-5, AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND LT FLOOR SUPPORT LOWER SURFACE CORRODED AT FS 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND AFT FUSELAGE SKIN DENTED AT STA 1225, L23R. THE DENT WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 218, LBL 10 - RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND RIGHT AFT LAV FLOORBEAM CORRODED AT STA 1322. THE CORRODED AREA OF FLOORBEAM WAS TRIMMED OUT IAW SRM 53-05, FIGURE 20A. A REPAIR ANGLE, SHIM, AND WEAR STRIP WERE INSTALLED IAW SRM 53-05, FIGURE 20A AND 51-10-4.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN AFT CARGO AREA AT FS 1231, L29R. A DOUBLER WAS INSTALLED IAW ECRA 5320-01263 AND SRM 51-30-5.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 53-01, AND 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1030 - 1250. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, 51-10-4, AND 51-10-3.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1322 - 1338, LONGERON 30. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-10-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 769 - 788, RBL 15. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND FORWARD CARGO PIT AFT BULKHEAD LOWER FLOOR TRANSITION SUPPORT ANGLE CORRODED. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-30-2.

Part: SUPPORT BRACKET — CORRODED (DOOR FRAME) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND R-1 DOOR JAMB SUPPORT CORRODED AT FS 156 - 200, RBL 55. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 45,137 hrs · 25,588 cycles

INSPECTION FOUND A .5 INCH CRACK IN LEFT MLG W/W FORWARD I/B CORNER ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,137 hrs · 25,588 cycles

EXTERNAL FUSELAGE DENTED AT STA 247 BETWEEN LONG 21L AND 22L. REFORMED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38, 51-10-4, AND 51-10-3.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

RIGHT OUTBOARD SEAT TRACK FS 200 - 250 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2, 51-10-3, AND 51-30-1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 45,137 hrs · 25,588 cycles

LEFT OUTBOARD SEAT TRACK CORRODED AT FS 1090 - FS 1164. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-05 FIG 4F AND 51-10-3.

Part: FITTING — CORRODED (BS 1007)

INSPECTION FOUND LONGERON 30 END FITTING CORRODED IN AFT BAGGAGE BIN AT STA 1007. THE LONGERON END FITTING WAS REPLACED IAW ECRA 5314-01002.

Part: SKIN — DENTED (BS 313)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 313, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: HINGE — CRACKED (PAX DOOR)

INSPECTION FOUND AFT ENTRY DOOR UPPER HINGE CRACKED. THE HINGE WAS REPLACED IAW SRM 51-00-0.

Part: CABLE — OUT OF ADJ (TAIL CONE)

THE AFT FUSELAGE TAIL CONE EXTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.

Part: SKIN — CRACKED (WS 286)

INSPECTION FOUND A 2.5 INCH CRACK ON RT WING LEADING EDGE SKIN AT FORWARD WS XOS 286 AND FORWARD OF ACCESS PANEL CUTOUT. AN INTERNAL AND EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01638. A DIP WAS ISSUED TO REPLACE SCREWS AND BLIND RIVETS AT NEXT 1/4D CHECK OR 2500 FLIGHT HOURS.

Part: SKIN — DENTED (BS 256-275)

LEFT SIDE SKIN DENTED 256 TO 275 LONG 16 TO 18 DENTED SEVERAL TIMES. FABRICATED AND INSTALLED NEW SKIN DOUBLER PER EC/RA 5330-02445.

Part: INTERCOSTAL — CORRODED (SERV DR CUTOUT)

LOWER AFT CORNER OF FORWARD SERVICE DOOR FRAME INTERCOSTAL HAS CORROSION. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: DOOR PAN — TORN (CARGO DR CUTOUT)

AFT CARGO DOOR AFT SIDE CUTOUT AROUND LOCKING CAM BENT, TORN AND SEPARATED. INSTALLED DOUBLER PER SRM 52-05 FIG 26A.

Part: GRD SENSE MECH — OUT OF RIG (NLG)

CLE - FLT 0287 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. THE AIRCRAFT RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE GROUND SENSING CONTROL MECHANISM AND ANTI-RETRACTION CABLE. THE GEAR WAS SWUNG AND OPERATION CHECKED NORMAL. IN ADDITION, THE NLG STRUT WAS SERVICED. A DIP WAS ISSUED TO CHECK THE NLG X-DIMENSION AFTER 4, BUT NO MORE THAN 20 LANDINGS. (X)

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

IAH - FLT 1885 - THE LANDING GEAR WOULD NOT RETRACT INITIALLY AFTER TAKEOFF. THE GEAR HANDLE RELEASE BUTTON WAS USED TO RAISE THE GEAR. MAINTENANCE INSPECTED RIG OF ANTI-RETRACTION CABLE IAW MM 32-31-01, AND FOUND NO FAULTS. A GEAR RETRACTION WAS PERFORMED WITH ALL OPERATION AND INDICATIONS CHECKING NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. (X)