N17812

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,441 hrs · 24,648 cycles

THE EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROW 15. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 48,650 hrs · 22,680 cycles

INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED FROM STA 1003 - 1212. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — CRACKED (SUBFLOOR) · airframe 48,650 hrs · 22,680 cycles

INSPECTION FOUND CABIN LT SUBFLOOR SKIN CRACKED AT FS 218. THE SUBFLOOR PANEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW SUBFLOOR WAS INSTALLED IAW SRM 53-14-1, 51-10-4, AND 51-30-1.

Part: SKIN — CRACKED (RT MLG DOOR)

INSPECTION FOUND A 4 INCH CRACK IN PREVIOUS DOUBLER REPAIR OF UPPER FORWARD CORNER RT MLG DOOR. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: CLIP — CRACKED (BS 1003)

INSPECTION FOUND A 2.3 INCH CRACK IN AFT CARGO FORWARD BULKHEAD FRAME CLIP AT STA 1003, LONGERON 28R. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-5, 51-10-3, 51-10-4, AND 51-30-2.

Part: SKIN — DENTED (RUDDER)

INSPECTION FOUND RUDDER SKIN DENTED AT UPPER LEFT SIDE. THE DENTED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3.

Part: CARGO TRACK — CORRODED (BS 427 - 636)

INSPECTION FOUND MID PIT RT CARGO TIE DOWN TRACK CORRODED FROM STA 427-636. THE TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — GOUGED (AILERON)

INSPECTION FOUND LEFT AILERON LOWER SURFACE SKIN GOUGED. THE AILERON WAS REPAIRED IAW ECRA 5750-03367.

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND SEVERAL .125 INCH CRACKS AROUND DOOR SEAL RIVET HOLE AT AFT CARGO DOOR UPPER AFT CORNER. THE FASTENERS WERE REMOVED IAW SRM 52-03, FIGURE 8. DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 52-03, FIGURE 8.

Part: SKIN — DENTED (BS 133)

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.

Part: FLOORBEAM — GOUGED (BS 1174)

INSPECTION FOUND AFT CARGO CEILING FLOORBEAM GOUGED AT FS 1174, RBL 2. A DOUBLER AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-2, 51-10-3, AND 53-04, FIGURE 36.

Part: SKIN — DENTED (BS 560)

INSPECTION FOUND RIGHT EXTERNAL FUSELAGE SKIN DENTED AT STA 560 BETWEEN LONGERON 21R AND 22R. THE DOUBLER WAS REMOVED AND THE AREA WAS COLD WORKED IAW ECRA 5330-01856. A REPAIR WAS INSTALLED IAW SRM 51-10-3, 53-04, FIGURE 38, AND ECRA 5330-01856.

Part: STOP — GOUGED (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-2, 51-10-3, AND 51-30-2.

Part: BRACKET — CRACKED (THRUST REVERSER)

INSPECTION FOUND NR 2 T/R UPPER DOOR I/B SIDE WING FAIRING SUPPORT BRACKET AND ANGLE CLIP CRACKED. THE CRACKS WERE 1 AND 1/8 LONG. THE I/B SIDE SUPPORT BRACKET AND ANGLE CLIP WERE REMOVED IAW SRM 51-30-2. REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-1, AND 51-30-2.

Part: STOP — GOUGED (CARGO DOOR)

INSPECTION FOUND AFT CARGO DOOR STOPS GOUGED IN THREE PLACES. REPAIRS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND ECRA 5330-02819.

Part: STOP — GOUGED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR STOPS GOUGED IN TWO PLACES. DOUBLERS WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5, AND ECRA 5330-02819.

Part: CARGO TRACK — CORRODED (BS 1003 - 1212)

INSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED FROM STA 1003 TO 1212. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SUPPORT — CORRODED (BS 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, LBL 12 TO LBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4.

Part: CARGO TRACK — CORRODED (CARGO BAY)

INSPECTION FOUND AFT CARGO AFT RT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 280)

INSPECTION FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AND DENTED AT FS 280 BETWEEN LONGERONS 22L AND 23L. THE AREA WAS COLD WORKED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 38 AND 51-10-3.

Part: STOP — WORN (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.

Part: SKIN — CRACKED (BS 178)

INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.

Part: STOP — WORN (CARGO DOOR)

INSPECTION FOUND TWO MID CARGO DOOR STOPS WORN. REPAIRED STOPS IAW ECRA 5330-02819.

Part: FLOOR PANEL — CORRODED (BS 160)

INSPECTION FOUND COCKPIT FLOOR SKIN CORRODED AT FS 160, LBL 6. THE CORROSION WAS REMOVED IAW SRM 53-01, FIGURE 2 AND 51-10-3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-04, 51-30-02.

Part: INTERCOSTAL — CORRODED (BS 1309 - 1331)

INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1309-1331, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: STOP — WORN (CARGO DOOR)

INSPECTION FOUND TWO AFT CARGO DOOR STOPS WORN. THE AREAS WERE REPAIRED IAW SRM 52-03, FIGURE 8, 51-30-2, 52-30-7, 51-10-3, AND ECRA 5330-02819.

Part: ANGLE — CRACKED (BS 945)

INSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-04, 51-10-3, AND 51-30-1.

Part: STOP — GOUGED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR STOP GOUGED.. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.

Part: ANGLE — CRACKED (RUDDER)

INSPECTION FOUND A 1 INCH CRACK IN LOWER RUDDER FAIRING AT STIFFENER ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-4.

Part: SEAT TRACK — CORRODED (CABIN)

INSPECTION FOUND O/B SEAT TRACK AT L-2 DOOR AFT EDGE CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 1030 - 1100)

INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AT FS 1030-1100, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.

Part: STOP — WORN (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR STOP WORN. REPAIRED IAW ECRA 5330-02819.

Part: FLANGE — CORRODED (BS 600)

INSPECTION FOUND ANTENNA FLANGE CORRODED IN MID PIT AT STA 600, LONGERON 29L TO 30. THE ANTENNA FLANGE WAS REMOVED AND A NEW FLANGE AND DOUBLER WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION FOUND L-1 DOOR THRESHOLD LOWER SUB FLOOR WEB CORRODED AND ATTACH ANGLE CRACKED. THE SUB FLOOR WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUB FLOOR WEB WAS INSTALLED IAW SRM 53-14-1, FIGURE 1 AND 53-01, FIGURE 4. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: WEB — CRACKED (BS 208)

INSPECTION FOUND A 3 INCH CRACK IN MAIN ENRTY DOOR AFT TORQUE BOX UPPER WEB TENSION LEG AT FS 208, LONGERON 11L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: STOP — GOUGED (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.

Part: SEAT TRACK — CORRODED (BS 1174 - 1300)

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION FOUND FLOORBEAM WEB AT LEFT END OF AIRSTAIR CORRODED AND FITTING FOR AIR STAIR LOCK CORRODED. THE WEB CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-01, FIGURE 1. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-4.

Part: INTERCOSTAL — CRACKED (BS 237)

INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO INTERCOSTAL AFT SUPPORT ANGLE AT STA 237 BETWEEN LONGERON 27R AND 28R. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1030 - 1300)

INSPECTION FOUND LEFT I/B SET TRACK CORRODED AT FS 1030-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 5F.

Part: WEB — CORRODED (BS 1250)

INSPECTION FOUND CUSP WEB CORRODED AT STA 1250, LBL 54. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.

Part: ANGLE — CRACKED (BS 160 - 200)

INSPECTION FOUND A 6 INCH CRACK IN FLOOR SUPPORT ANGLE AT L-2 DOOR, FS 160-200, LBL 58. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: WEB — CORRODED (BS 237)

INSPECTION FOUND LEFT CUSP WEB ON FORWARD SIDE OF FRAME AT STA 237, LONGERON 18L CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER, PLATE, TEE ANGLE, AND BRACKET WERE INSTALLED IAW SRM 53-01, 53-10-2, 51-30-3, AND 51-30-2.

Part: ANGLE — CRACKED (BS 970)

INSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.

Part: FLOORBEAM — CRACKED (FUSELAGE)

INSPECTION FOUND A 3 INCH CRACK IN R-1 DOOR THRESHOLD FLOOR SUPPORT WEB AT FORWARD EDGE OF DOOR CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-30-2, AND 51-30-6.

Part: SKIN — DENTED (BS 465 - 484)

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 465 AND 484 AT LONGERON 21R AND 22R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 8, CONDITION 2. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-3, 51-30-02, AND 53-04, FIGURE 38, VIEW P.

Part: INTERCOSTAL — CRACKED (BS 1338)

INSPECTION FOUND A .05 INCH CRACK IN INTERCOSTAL AT AFT FLOORBEAM FS 1338 RT SIDE JUST FORWARD OF THE AFT ENTRANCE DOOR RT DOOR JAMB. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 180)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180, BL 0 TO RBL 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 200)

INSPECTION FOUND SUB FLOOR CORRODED UNDER SUPPORT AT FS 200, LBL 4 TO RBL 4. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-10-4 AND 51-30-5. THE CORRODED AREA WAS REMOVED IAW SRM 53-01, FIGURE 1B. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 160 - 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160-200, LBL 22 TO LBL 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (BS 1416)

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1416 BETWEEN LONGERONS 24L AND 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, 53-01, FIGURE 38, AND 51-10-3.

Part: WEB — CORRODED (BS 160)

INSPECTION FOUND SUB FLOOR CORRODED AT FS 160, RBL 12. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 18 AND 53-10-3.

Part: FLOORBEAM — CORRODED (BS 160 - 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160-200, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 200 - 370)

INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT FS 200-370. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4.

Part: SEAT TRACK — CORRODED (BS 1030 - 1300)

INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA1030-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: STOP — CHAFED (CARGO DOOR)

INSPECTION FOUND TWO AFT CARGO DOOR STOPS CHAFED. REPAIRS WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-3.

Part: SKIN — DENTED (BS 229)

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 229 BETWEEN LONGERON 18L AND 19L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-4 AND 53-04, FIGURE 25.

Part: FLOORBEAM — CORRODED (BS 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, BL 0 TO LBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-1, 51-10-3, AND 51-30-5.

Part: CLIPS — OUT OF ADJUST (TAIL CONE)

THE EXTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT FIVE POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL CHECK WAS GOOD IAW MM 53-53-00.

Part: CLIPS — OUT OF ADJUST (TAIL CONE)

THE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT FORTY POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL CHECK WAS GOOD IAW MM 53-53-00.

Part: ANGLE — CORRODED (BS 636-693)

INSPECTION FOUND MID BAGGAGE BIN Z-ANGLE CORRODED FROM STA 636 TO 693. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 63.

Part: BEAM — CORRODED (BS 1155-1211)

INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB BEAM CORRODED FROM STA 1155 TO 1211. REPAIRED IAW SRM 53-05.

Part: LONGERON — CRACKED (BS 1418)

INSPECTION FOUND A 4 INCH CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 2.

Part: SKIN — CORRODED (BS 1174)

INSPECTION FOUND CORROSION ON FUSELAGE SKIN UNDER VHF-3 ANTENNA AT STA 1174. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02631.

Part: FITTING — CRACKED (BS 826)

INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 826, LONGERON 19L. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A 1.5 CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE BEAM WAS REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 1155-1212)

INSPECTION FOUND AFT BAGGAGE BIN VERTICAL THRESHOLD SUPPORT BETWEEN STA 1155 AND 1212 CORRODED. A NEW STANDOFF WAS INSTALLED IAW SRM 51-30-2.

Part: FUEL CONTROL — INOPERATIVE (APU)

WHILE OPERATING THE APU IN FLIGHT WITH THE NR 2 GENERATOR PLACARDED INOPERATIVE, THE APU SHUTDOWN. THE APU WOULD NOT RESTART. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE APU FUEL CONTROL UNIT AT FAULT. THE APU FUEL CONTROL UNIT WAS REMOVED AND REPLACED IAW MM 49-30-01, OPERATIONAL CHECKS WERE GOOD.

Part: DNLOCK SENSOR — INOPERATIVE (NLG)

THE NLG RED UNSAFE LIGHT ILLUMINATED DURING DESCENT. ABNORMAL PROCEDURES WERE FOLLOWED, BUT THE LIGHT REMAINED ON. THE INDICATION LIGHTS WERE NORMAL WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOCK SENSOR AT FAULT. THE SENSOR WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED PER MM 32-00 WITH OPERATION AND INDICATIONS CHECKING GOOD.

Part: APU — OIL LEAK (ACFT TAIL)

A FLIGHT ATTENDANT REPORTED SMOKE ENTERED THE CABIN JUST AFTER TAKEOFF FROM DEN. THE SMOKE SOURCE WAS ISOLATED TO AIR CONDITIONING PACKS AND THE AIRCRAFT WAS RETURNED TO DEN. MAIINTENANCE FOUND THE APU WAS BLOWING OIL UP THROUGH PLENUM INTO THE AIR SYSTEM. THE APU WAS REMOVED AND REPLACED PER MM 49-10-00. LEAK AND OPERATIONAL CHECKS WERE GOOD. PART TOTAL CYCLES, 11,261.

Part: SEAT — INOP (LT COCKPIT)

FLT NR 1832 - IAH - THE NR 2 GENERATOR FAILED IN FLIGHT. A SLIGHT ELECTRICAL BURNING ODOR WAS ALSO OBSERVED MOMENTARILY IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 2 GENERATOR GCU WAS RERACKED. AN AC CROSSTIE CHECK WAS PERFORMED WITH THE NR 2 GENERATOR ON LINE AND AT FULL ELECTRICAL LOAD. OPERATION CHECKED GOOD WITH NO FAULTS NOTED. MAINTENANCE FOUND THE CAPTAIN'S SEAT AS THE SOURCE OF THE ELECTRICAL ODOR. THE CAPTAINS SEAT WAS REMOVED AND REPLACED. (M)

Part: DOOR PAN — CRACKED (CARGO DOOR)

HOU - INSPECTION FOUND A 1.5 INCH CRACK UNDER FORWARD LOCK CAM OF AFT CARGO DOOR PAN SKIN. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. (X)

Part: FLOOR — CORRODED (BS 1174)

HOU - INSPECTION FOUND CABIN SUB FLOOR CORRODED ON LEFT SIDE AT STATION 1174. THE CORRODED SECTION WAS REMOVED AND THE SURROUNDING AREA WAS CLEANED IAW SRM 51-10-3. A REPAIR SECTION OF SUB FLOOR WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, SRM 51-30-2 AND 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (BS 175)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 175. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. (M)

Part: FLOOR BEAM — CORRODED (BS 148-200)

HOU - INSPECTION FOUND CORROSION ON FLOOR BEAM AT STA 148 - STA 200, RIGHT OF CENTERLINE. THE FLOOR BEAM WAS REMOVED AND REPLACED IAW SRM 51-10-1. (X)

Part: SUPPORT BEAM — CORRODED (BS 200)

HOU - INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT BEAM CORRODED AT STA 200, CENTERLINE. THE FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-60-0. (X)

Part: ANGLE — CORRODED (PAX DOOR)

HOU - INSPECTION FOUND FLOOR SUPPORT Z-ANGLE CORRODED JUST INBOARD OF MAIN CABIN DOOR. THE Z-ANGLE WAS REPLACED IAW SRM 51-30-2. (X).

Part: FLOOR SUPPORT — CORRODED (BS 160-200)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 160-200, RIGHT OF CENTERLINE. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. (M)

Part: BLKHD SKIN — CORRODED (AFT PRESS BLKHD)

HOU - INSPECTION FOUND CORROSION IN SKIN AT AFT PRESSURE BULKHEAD FORWARD FACE LOWER CENTER AREA. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. (X)

Part: BRACKET — CRACKED (RT WING)

HOU - INSPECTION FOUND A .3750 INCH CRACK IN RT WING UPPER TRAILING EDGE BRACKET AT AILERON OUTBOARD HINGE. THE BRACKET WAS REPLACED IAW SRM 51-30-1. (X)

Part: PANEL — CRACKED (TE LT WING)

HOU - INSPECTION FOUND A .6250 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL LOWER SURFACE. THE PANEL WAS REPAIRED IAW SRM 51-70-1. (X)