N797AS

Part: SHEAR TIE — CORRODED (BS 500) · corrosion level 2 · airframe 53,860 hrs · 30,305 cycles

FWD CARGO BAY, BS 500 BETWEEN STRINGERS 27 - 28R AFT SIDE OF FRAME HAS CORROSION. ACFT GROUNDED. R & R FRAME ANGLE IAW SRM 51-40-02-0G-0.

Part: STRINGER — CRACKED (BS 382-400) · airframe 53,860 hrs · 30,305 cycles

AFTER REMOVING STRINGER CLIP AT BS 380 S-8R STR WAS FOUND TO BE CRACKED. ACFT GROUNDED. REPAIRED STRINGER IAW ASA EA 400 53EA 16105, THIS IS A CATEGORY B REPAIR DTE FOR FIRST AND SECOND STAGE HAS BEEN GRANTED. THIRD STAGE APPROVAL IS REQUIRED PRIOR TO THE INSPECTION THRESHOLD OF 66,000 TOTAL FLT CYCLES REFER TO 400 53DTI 16105.

Part: WEB — CRACKED (BS 303) · airframe 53,860 hrs · 30,305 cycles

FWD CABIN AT BS 303 ON WEB ON 4L AREA IS CRACKED. ACFT GROUNDED. R & R WEB IAW SRM

Part: STRAP — CRACKED (BS 303) · airframe 53,860 hrs · 30,305 cycles

INTERCOSTAL STRAP AT BS 294, STRINGER 4L IS CRACKED. ACFT GROUNDED. FAB, LOCATED AND DRILLED NEW STRAP IAW SRM 51-40-05-0G-0.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 53,860 hrs · 30,305 cycles

FWD WET AREA INTERCOSTAL CRACKED AROUND 2 FASTENER HOLES ON UPPER FLANGE BETWEEN BS 312-328 AT LBL44. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FITTING — CRACKED (BS 1138) · airframe 53,860 hrs · 30,305 cycles

LEFT AFT LOWER HORIZONTAL THRUST BEAM FITTING IS CRACKED, REF TASK SB737-55-1091-400-1 STEP 17, REQUIRES ISSUANCE OF EC SB737-55-1091-400-2. ACFT GROUNDED. R & R HORIZONTAL STABILIZER UPPER AND LOWER LT CORNER FITTINGS IAW EA 400 55EA-16060.

Part: ANGLE — CRACKED (BS 277-294) · airframe 53,860 hrs · 30,305 cycles

PASSENGER CABIN FUSELAGE STIFFENER ANGLE CRACKED FWD OF R1 DOOR AT WL 240. ACFT GROUNDED. R & R ANGLE BETWEEN 12R AND 13R IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 907) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS 907 IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15.

Part: FRAME — CRACKED (BS 727F) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS 727F IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400 -3-107, REV 00, DATED 11SEP15, FIG 2.

Part: FRAME — CRACKED (BS 480) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15.

Part: FRAME — CRACKED (BS 480) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS 480 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20061609-400-53-107, REV 00, DATED 11SEP15, FIG 2.

Part: FRAME — CRACKED (BS 907) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS 907 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 400-53-107, REV 00, DATED 11SEP15, FIG 2.

Part: FRAME — CRACKED (BS 380) · airframe 53,860 hrs · 30,305 cycles

FRAME AT BS 380 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 S400-53-107, REV 00, DATED 11SEP15, FIG 2.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 53,860 hrs · 30,305 cycles

RT WING NR 4 L/E SLAT INBD T/E WEDGE HAS POSSIBLE AREA OF DELAMINATION AT EDGE, MARKED. ACFT GROUNDED. REPAIRED RT WING NR 4 SLAT L/E IB T/E WEDGE AT EDGE IAW SRM 51-70-10-2R-4 REPAIR 4.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,900 hrs · 29,066 cycles

EMERGENCY EXIT SIGN BESIDE RT OVERWING EXIT FELL OFF. ACFT GROUNDED. REPLACED EMERGENCY EXIT SIGN FLOOR PROXIMITY LIGHT FOR RT AFT OVERWING EXIT REF AMM 33-51-81 OPS CK GOOD. NOTE COVER ONLY.

Part: FRAME — DAMAGED (BS 351) · airframe 50,736 hrs · 28,407 cycles

STUB FRAME HAS FIVE DAMAGED FASTENER HOLES AT BS 351 BETWEEN STRINGERS 16 - 17L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20121205-400-53-107.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 50,736 hrs · 28,407 cycles

LEFT INBD MID FLAP UPPER SKIN IS CHAFED ON INBD EDGE. ACFT GROUNDED. CHAFE ON LT INBD MID FLAP UPPER SKIN WAS ON EXISTING REPAIR. REPAIRED UPPER SKIN IAW SRM 57-53-01-2R-3.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 50,736 hrs · 28,407 cycles

RIGHT INBD MID FLAP IS CHAFED AT THE VERY INBD TOP SIDE, JUST AFT OF INBD SIDE SEAL. ACFT GROUNDED. CHAFE ON RT INBD MID FLAP UPPER SKIN WAS ON A EXISTING REPAIR. REPAIRED UPPER SKIN IAW SRM 57-53-01-2R-3.

Part: FLOORBEAM — CORRODED (BS 772.6) · corrosion level 2 · airframe 50,682 hrs · 28,373 cycles

CORROSION FOUND FLOOR PANEL FLOORBEAM SPLICE AT BS 772.6, AFT CARGO BAY. ACFT GROUNDED. REPLACED TEE SPLICE AND REINSTALLED FLOOR PANELS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 49,354 hrs · 27,577 cycles

EMERGENCY LIGHT LOCATOR SIGNS ADJACENT TO L1 AND R1 DOORS HAVE BROKEN LENSES. ACFT GROUNDED. R & R LENS AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: SCREW — SHEARED (L1 GUIDE ARM) · airframe 47,840 hrs · 26,633 cycles

FORWARD ENTRY DOOR (L-1) WILL NOT FULLY OPEN. DOOR HANDLE OPENS ABOUR 2/3 OF FULL AND DOOR ITSELF OPENS ABOUT 3-5. (NO PRESSURIZATION ISSUES NOTED) (NO COMMUICATION ISSUES NOTED). ACFT GROUNDED. FOUND SCREW THAT SECURES FORWARD ENTRY DOOR GUIDE ARM PIN SHEARED & PIN BACKED OUT. REPLACED GUIDE ARM PIN, PN 141A6076-1, WASHER, PN 141A6077-1, AND SCREW, PN BACS12ER06K6 REF. MM 52-11-21-404-007-003. RE-ASSEMBLED DOOR AS NECESSARY & RE-INSTALLED SLIDE PACK, REF MM 25-61-35-402-003. DOOR LINER INSTALLATION REF. MM 52-11-31-404-009. DOOR OPENS & CLOSES NORMALLY.

Part: FLANGE — CORRODED (BS 1138-1147) · corrosion level 2 · airframe 47,373 hrs · 26,351 cycles

APU COMPT. RT SIDE APU AIR INLET FLANGE FASTENER HOLES HAVE CORROSION. REMOVED CORRODED AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-80-13 1A 2, FIG 101. R & R STRINGER IAW SRM 51-40-02-0G-0 PAR D PG 6.

Part: STIFFENER — CORRODED (BS 117) · corrosion level 2 · airframe 47,373 hrs · 26,351 cycles

APU COMPARTMENT RT SIDE APU AIR INLET FLANGE HAS CORROSION ON OTBD SIDE. REMOVED STIFFENER AT RT SIDE APU AIR INLET FLANGE AND REPLACED WITH NEW STIFFENER IAW SRM 51 40 02 AND 51 40 05, W .75 O .060 R .045 L 20 D .15.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

LT WING INBD FOREFLAP UPPER SURFACE REPAIR DOUBLER IS CHAFED AT MID SECTION. REPLACED DOUBLER IAW SRM 51-70-10-2R-4 ON LT WING INBD FOREFLAP.

Part: FLANGE — CORRODED (BS 663-706) · airframe 47,373 hrs · 26,351 cycles

AFTER REMOVAL OF LT LOWER BLADE SEAL RETAINER, FOUND UPPER FLANGE CORRODED, LT WHEEL WELL MANIFOLD UPPER FLANGE. ACFT GROUNDED. R & R UPPER FLANGE IAW SRM 51-40-02 AND SRM 51-30-04-06-0.

Part: SKIN — DENTED (BS 422.2) · airframe 47,373 hrs · 26,351 cycles

LT FUSELAGE AT STA 422.2 5IN BELOW 14L IS A DENT WITHIN 3IN OF LAP SEAM C. REPAIRED DENT AT FUSELAGE STA 4202 BETWEEN STR 14L AND STR15L IAW ASA EA 400-53EA-10114 YELLOW DOT APPLIED.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

LT WING OTBD FOREFLAP L/E SKIN IS CHAFED AT INBD CORNER. REPAIRED LT WING OTBD FOREFLAP L/E SKIN IAW SRM 57 53 01 2R 1, FIG 201.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

RT WING OTBD FOREFLAP UPPER SURFACE IS CHAFED TWO PLACES. REPAIRED RT WING OTBD FOREFLAP UPPER SURFACE IAW SRM 51 70 10 2R 4, REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

LT WING INBD MIDFLAP L/E SKIN IS CHAFED AT MID SECTION. REPAIRED LT WING INBD MIDFLAP L/E IAW SRM 57 53 01 2R 2.

Part: SKIN — CHAFED (SPOILER) · airframe 47,373 hrs · 26,351 cycles

RT WING INBD GROUND SPOILER LOWER SURFACE IS CHAFED MULTIPLE PLACES. ACFT GROUNDED. REMOVED AND REINSTALLED REPAIRED RT INBD GROUND SPOILER IAW SRM 51 70 10, PG 46 737 400 AMM 27 62 12 004 001, STEPS 2.D 1-12.E AND AMM 27 62 12 004 001, STEPS 3E 3 THRU 3F.4 GROUND SPOILER FUNCTIONAL TEST GOOD IAW AMM 27 61 12 004 001, STEP 3E 14.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

RT WING INBD FOREFLAP UPPER SURFACE INBD REPAIR DOUBLER IS CHAFED AT INBD AFT CORNER. ACFT GROUNDED. REPAIRED CHAFE DAMAGE IAW SRM 51 70 10, REPAIR 4, PG 1.

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 47,374 hrs · 26,351 cycles

NR 2 SLAT INBD LOWER SURFACE IS CHAFED. REPAIRED CHAFE ON NR 2 SLAT INBD LOWER SURFACE IAW SRM 51 70 10 2R 4, REPAIR 4, PARA 20, PG 48.

Part: WEDGE — CHAFED (RT WING SLAT) · airframe 47,373 hrs · 26,351 cycles

RT WING NR 5 SLAT T/E WEDGE LOWER SURFACE IS CHAFED AT INBD CORNER REPAIRED NR 5 SLAT LOWER INBD CORNER T/E WEDGE IAW SRM 51 70 10 2R 4, PERMANENT REPAIR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

RT WING INBD FORFLAP UPPER SURFACE REPAIR DOUBLER IS CHAFED. ACFT GROUNDED. BONDED REPAIR OF RT WING INBD FOREFLAP UPPER SURFACE REPAIR DOUBLER IAW SRM 51 70 10, REPAIR 4. (PERMANENT REPAIR).

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 47,373 hrs · 26,351 cycles

NR 2 SLAT INBD LWR SURFACE IS CHAFED. REPAIRED CHAFE ON NR 2 SLAT INBD LOWER SURFACE IAW SRM 51-70-10-2R-4. REPAIR 4, PARA 20 PG 48.

Part: WEB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 47,373 hrs · 26,351 cycles

FWD CARGO BAY AFT CUTOUT FRAME AT BS 492 AT STR 23R UPPER STRAP ON REVEAL WEB IS CORRODED. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED STRAP IAW DWG NR 65-20723.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 47,373 hrs · 26,351 cycles

AFT CARGO BAY FLOOR PANEL CRACKED. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL IAW SRM 51-40-05-0G-0 AND AMM 25-52-51-004-001 AND AMM 25-52-51-404-011.

Part: UNKNOWN — MULTIPLE FAIL · airframe 45,494 hrs · 25,213 cycles

DURING CLIMBOUT, AUTOTHROTTLE FAILED, TRANSPONDER FAILED, GROUND PROXIMITY FAILED, ACARS REPORTED INCORRECTLY, ENGINE LOW IDLE ILLUMINATED ON THROTTLE REDUCTION, CABIN ALTITUDE HORN WENT OFF (NO MASKS DROP) ACFT GROUNDED. REPLACED M990 GROUND SENSE LOGIC BOARD IN E-11, REPLACED S105 AND S106 GROUND SENSING PROXIMITY SWITCH AND AIR SENSING PROXIMITY SWITCH IAW AMM 32-09-20-724-05. OP CHECKED GOOD IAW AMM 32-09-20-724-05 STEP L. PERFORMED MLG SAFETY SENSOR TEST REF MM 32-09-01-825-002, BOTH AIR & GROUND OPS NORMAL. R & R M991. DURING DVI OF S105 & S106 AIR/GROUND SENSOR WIRING RUN FOUND OLD HARNESS RUBBED INTO FLANGE OF AIR GROUND SENSOR BRACKET ASSY. REPLACED 1 TORN ADEL CLAMP REPOSITIONED WIRING HARNESS TO PREVENT CHAFING ON STRUCTURE AND APPLIED TEFLON TAPE TO POTENTIAL WEAR AREAS INSPECTED WIRING NO DAMAGE NOTED. REF CHAP 20 20-10-13. REPLACED M1110. REPLACED NLG SAFETY SENSOR REF MM32-09-02. FOUND NO BINDING IN GROUND SHIFT CABLE, RIG CHECKED OK, NO ADJUSTMENTS MADE. REF MM 27-61-51. RECONNECTED GROUND SHIFT CABLE AT TORSION LINK REF MM 27-62-51. ACCOMPLISHED OPS CHECKS OF TSR STEPS 2,3,4 REF MM32-09-20, MM32-09-02-725-008 AND MM32-09-20 RESPECTIVELY. OPS CHECKS NORMAL. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT IAW MIG-56. NO DISCREPANCIES NOTED FCF SUCCESSFUL.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 43,906 hrs · 24,300 cycles

F/A REPORTS L1 DOOR STIFF AND HARD TO OPEN AND CLOSE. VERIFIED THAT THE L1 DOOR IS TOO HARD TO SWING OPENED PER AMM 52 11 00 755 051 STEP D(5)(C) J. LUBED L1 DOOR MECHANISM PER MM 12 25 21 643 007. LUBED L1 DOOR HANDLE MECHANISM PER MM 12 25 21 603 001. ACCOMPLISHED FORWARD ENTRY DOOR TEST REF MM 52 11 00 755 051. OPS CHECK GOOD.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 43,871 hrs · 24,277 cycles

1ST CLASS F/A REPORTED, SHE GOT THE L1 DOOR HALF WAY OPEN AND IT WAS VERY DIFFICULT TO OPEN ALL THE WAY. F/O WAS REQUIRED TO OPEN IT ALL THE WAY. EXCESSIVE DRAG FROM HINGE ARMS RIDING DOOR SKIN. DOOR IS VERTICALLY HIGH. ADJUSTED DOOR VERTICALLY DOWN .050" ADJUSTED GUIDE ARM ASSY AND VERIFIED DOOR SKIN CLEARANCES AND STOP PIN SETTINGS REF MM 52 11 00 705 007. 80023 INSP 10. OPS CHECK FOUND TO BE SATISFACTORY. SMOOTH AND NORMAL. REF 52 11 00 705 060.

Part: SIGN — BROKEN (CABIN) · airframe 41,590 hrs · 22,852 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT L1 DOOR IS BROKEN. REMOVED AND REPLACED EXIT LOCATOR SIGN AND PERFORMED TEST PER B737 400 AMM 33 51 81 962 011. OPS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

CORROSION ON FUSELAGE FLOORBEAM BS 986.5 LBL 20 AND RBL 45. REPAIRED FLOORBEAM IAW ASA EA 400 53EA 04881.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

AFTER REMOVAL OF PARTS TO ACCESS FLOORBEAM REPAIR AT BS 986 FOUND CORROSION ON LOWER SURFACE OF SHEAR WEB AT BS 986 LBL 42. FABRICATED NEW SHEAR WEB AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FLOOR STRUCTURE SUPPORT AT BS 986 TO BS 1006 RBL 32 CRACKED. REMOVED AND REPLACED FLOOR STRUCTURE SUPPORT IAW B737 400 SRM 51 40 02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

AFTER REMOVAL OF PARTS TO ACCESS FLOORBEAM REPAIR AT BS 986 FOUND CORROSION ON CREASE BEAM WEB AT BS 1008 RBL 42. REMOVED CORRODED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: SILL — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

R2 DOOR MOP SILL CRACKED AT APPROX BS 989. REMOVED AND REPLACED MOP SILL IAW B737 400 SRM 51 40 02.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 41,492 hrs · 22,802 cycles

RT HORIZONTAL STABILIZER LEADING EDGE HAS DENTS WITH GOUGES OVER A RIV 80 IN FROM INBOARD END. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 41,492 hrs · 22,802 cycles

RT HORIZONTAL STABILIZER LEADING EDGE HAS TWO DENTS WITH GOUGES OVER A RIB 80 INCHES FROM INBOARD END. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

LT INBOARD SEAT TRACK HAS SEVERAL GOUGES BS 540 TO BS 727+5. REMOVED DAMAGED SECTION AND INSTALLED NEW SEAT TRACK IAW B737 400 SRM 51 40 05.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

LT INBOARD SEAT TRACK HAS SEVERAL GOUGES BS 520 - 540. REMOVED DAMAGED SECTION AND INSTALLED NEW SEAT TRACK IAW B737 400 SRM 51 40 05.

Part: FITTING — CORRODED (TE FLAP) · airframe 41,492 hrs · 22,802 cycles

RT OUTBOARD FLAP OUTBOARD ROLLER GUIDE FITTING IS CHAFED. REMOVED AND REPLACED FITTING IAW B737 400 SRM 51 40 02 AND 57 51 90.

Part: ANGLE — CHAFED (FLAP TRACK) · airframe 41,492 hrs · 22,802 cycles

RT WING INBOARD FIXED TRAILING EDGE OUTBOARD ANGLE ATTACHED TO FLAP TRACK FAIRING IS CHAFED. REMOVED DAMAGED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 01 51 40 05 AND 51 40 02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FLOOR PANEL SPLICE PLATE AT BS 772 HAS BARE METAL SPOTS CORROSION. DOUBLE DRILLED HOLES AT EACH END AND LOOSE FASTENERS FABRICATED REPLACEMENT SPLICE PLATE AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT NR 5 LT CAP STRIP IS CORRODED, BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT FLOOR BOARD IS CORRODED ON EDGES, REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 303.9 HAS CHAFE MARK ON INTERCOSTAL TIE STRAP AT STRINGER 4L AND INTERCOSTAL IS CRACKED IN RADIUS. REMOVED INTERCOSTAL AND REPLACED WITH NEW IAW B737 400 SRM 53 00 04.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT NR 3 LT CAP STRIP IS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW B737 400 SRM 53 30 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 30 01 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT NR 4 LT CAP STRIP IS CORRODED BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: SUPPORT BRACKET — CHAFED (RT WING) · airframe 41,492 hrs · 22,802 cycles

RT WING INBOARD TRAILING EDGE UPPER FIXED PANEL AFT LOWER SUPPORT BRACKET CHAFED AT AFT END, BLENDED SUPPORT BRACKET FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 57 51 02. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 21 21 51 20 01 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT LOWER SILL BEAM IS CORRODED ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED LOWER SILL WEB IAW B737 400 SRM 51 40 02.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FORWARD PIT NR 3 LT CAP STRIP IS CORRODED BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 50 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FORWARD PIT NR 3 RT CAP STRIP IS CORRODED, BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 30 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FORWARD PIT NR 2 RT CAP STRIP IS CORRODED BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 30 53. FABRICATED AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05 51 20 01 AND BOEING SOPM 20 41 02.

Part: SKIN — DENTED (SPOILER) · airframe 41,492 hrs · 22,802 cycles

NR 4 SPOILER UPPER SURFACE HAS A CLUSTER OF DENTS WITHIN 6 IN. REPAIRED SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FLOOR STRUCTURE AT BS 986 TO BS 1006 RBL 32 CRACKED. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (SPOILER) · airframe 41,492 hrs · 22,802 cycles

NR 5 SPOILER UPPER SURFACE HAS A CLUSTER OF DENTS WITH CREASES IN CENTER. REPAIRED DENT DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FLOORBOARD — CORRODED (CARGO BAY) · airframe 41,492 hrs · 22,802 cycles

AFT PIT FLOOR BOARD NR 5 IS CORRODED ON BOTTOM SID. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 60 53 51 40 05 AND 51 20 01.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

SHEAR TIE AT BS 727E STR 26R TO STR 27R DAMAGED OUT OF LIMITS. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

APU TORQUE BOX AIR INLET LOWER SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED LOWER SUPPORT IAW B737 400 SRM 51 40 02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

APU TORQUE BOX AIR INLET UPPER SUPPORT ANGLE HAS CORROSION ON OUTBOARD SIDE. REMOVED AND REPLACED SUPPORT ANGLE IAW B737 400 SRM 51 40 02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT CARGO LOWER SIDEWALL LINER SUPPORT ANGLE IS CORRODED ON LOWER SURFACE. REPAIRED SIDEWALL LINER SUPPORT ANGLE IAW B737 400 SMR 51 70 11.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

RT APU TORQUE BOX CORRODED ON LOWER SURFACE OF WEB BS 1118. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED IAW B737 400 SRM 51 70 13.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT LT CAP STRIP NR 2 CORRODED BLENDED CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 30 53 51 30 01 51 20 01 AND BOEING SOPM 20 41 02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

DOUBLE DRILLED HOLE THRU SKIN AND SHEAR TIE AT BS 500F BETWEEN STR 27R AND STR 28R. REPAIRED SKIN IAW ASA EA 400 53EA 04882.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT INTERNAL SECTION OF APU AIR DUCT CUT OUT CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW B737 400 SRM 51 40 02.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 41,492 hrs · 22,802 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT / CARGO TRACK ANGLE CRACKED IN MOUNT FLANGE RADIUS AT BS 727G RBL 14. REPAIRED CARGO TRACK ANGLE IAW B737 400 SRM 53 00 53 FIG 201 REPAIR 1.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

RT TRANSITION PANEL BETWEEN BS 727E +12 AND BS 767 HAS CORROSION AROUND FASTENER HOLES. REPLACED WITH NEW PANEL IAW B737 400 SRM 53 60 53.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT NR 4 RT SIDEWALL TRIM STRIP IS CORRODED. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 60 53 AND 51 20 01.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT FORWARD BULKHEAD RETAINER STRIP IS CORRODED. REMOVED CORRODED STRIP AND INSTALLED NEW PART IAW B737 400 SRM 53 60 53 51 40 05 AND 51 20 01.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

LT TRANSITION PANEL BS 830 TO BS 727E+8 HAS MULTIPLE AREAS OF SURFACE CORROSION AROUND FASTENER HOLES. INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

CORROSION ON RADIAL STIFFENERS BL 0 BS 1016. REPAIRED RADIAL STIFFENERS IAW BOEING DRAWING 65C28106.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE HAS A MISDRILLED HOLE AT THE RADIUS BS 727E+18 LBL 3. REPAIRED SUPPORT ANGLE IAW ASA EA 400 53EA 04918 REV NEW DATED 04 MAR 11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,492 hrs · 22,802 cycles

RT CARGO TRACK CORRODED BETWEEN BS 900 AND BS 947. REMOVED AND INSTALLED NEW TRACK IAW B737 400 SRM 53 60 53 FIG 101.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

CRACKED STRINGER TIE CLIP AT BS 947 STR 25R. REMOVED CRACKED STRINGER TIE CLIP AND INSTALLED NEW PART IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 787 FRAME CRACKED BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

CORROSION ON SHEAR TIE AT BS 1006 AFT SIDE OF FRAME BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 747 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 827 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 500E WEB ATTACH CLIP IS CRACKED AT STR 26R. REMOVED CRACKED CLIP FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.

Part: RIB — CRACKED (LT WING) · airframe 41,492 hrs · 22,802 cycles

LEFT WING TANK RIB LOWER CHORD AT WBL 135.5 CRACKED IN RADIUS BETWEEN STR 2 AND STR 3. REPAIRED RIB CHORD IAW ASA EA 400 57 EA 04870.

Part: ANGLE — CRACKED (TE FLAP) · airframe 41,492 hrs · 22,802 cycles

LEFT WING TRAILING EDGE FIXED PANEL ON OUTBOARD SIDE OF NR 3 FLAP TRACK FAIRING HAS A CRACK AT AFT END IN RADIUS. REMOVED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

CORROSION ON L 2 DOOR OPENING LOWER INNER CHORD. REMOVED AND REPLACED IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 LT SIDE AT BS 867. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: RIB — CRACKED (RT WING) · airframe 41,492 hrs · 22,802 cycles

RIGHT WING TANK RIB LOWER CHORD AT WBL 135.5 CRACKED IN RADIUS BETWEEN STR 2 AND STR 3. REPAIRED RIB CHORD IAW ASA EA 400 57 EA 04870.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

CORROSION ON R2 DOOR OPENING LOWER INNER CHORD. REMOVED CORROSION FOUND OUT OF LIMITS IAW B737 400 SRM 53 60 51 FIG 101. REMOVED AND REPLACED WITH NEW INNER CHORD IAW B737 400 SRM 51 40 02.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT PIT LOWER SILL BEAM WEB BS 847 867 STR 25R IS CORRODED AROUND NUT PLATES ON BOTH UPPER AND LOWER SURFACES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW WEB IAW B737 400 SRM 53 60 15 AND 51 40 02.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 500F WEB ATTACH CLIP IS CRACKED AT STR 26R. REMOVED CRACKED CLIP FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.

Part: WEB — CHAFED (ELEVATOR) · airframe 41,492 hrs · 22,802 cycles

RIGHT ELEVATOR INBOARD BALANCE BAY INBOARD WALL CHAFED. REMOVED AND REPLACED RIGHT ELEVATOR INBOARD BALANCE BAY INBOARD WALL IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 500D SHEAR TIE IS CORRODED BETWEEN STR 27R AND STR 28R. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201. THIS REPAIR IS A CATEGORY B REPAIR AND REQUIRES INSPECTION AT 66 000 TOTAL FLIGHT CYCLES.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FORWARD PIT SIDEWALL SUPPORT ATTACH BRACKET AT BS 500F CRACKED AT STR 21R. REMOVED CRACKED BRACKET FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

BS 500F SHEAR TIE IS CORRODED BETWEEN STR 27R AND STR 28R. REPAIRED SHEAR TIE IAW ASA EA 400 53EA 04882.

Part: ANGLE — CRACKED (RT WING) · airframe 41,492 hrs · 22,802 cycles

RIGHT WING TRAILING EDGE FIXED PANEL ON OUTBOARD SIDE OF NR 6 FLAP TRACK FAIRING HAS A CRACK AT AFT RIVET. REMOVED CRACKED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01 51 40 02 51 20 01 AND BOEING SOPM 20 41 02.

Part: SKIN — DENTED (SPOILER) · airframe 41,492 hrs · 22,802 cycles

RIGHT WING INBOARD NR 5 SPOILER LOWER SURFACE HAS A CLUSTER OF DENTS THAT EXCEEDS THE ALLOWABLE DAMAGE LIMITS 4 IN X 8 IN AREA AT AFT INBOARD CORNER. REPAIRED RIGHT WING NR 5 SPOILER LOWER SURFACE AFT INBOARD CORNER IAW B737 400 SRM 51 70 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 LT SIDE AT BS 787. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 RT SIDE AT BS 400. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 LT SIDE AT BS 360. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED BS 400 BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 LT SIDE AT BS 747. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 41,492 hrs · 22,802 cycles

FORWARD PIT TRANSITION PANEL ON THE LEFT SIDE IS CORRODED BETWEEN BS 500E AND 500G. FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 30 53 FIG 201.

Part: SKIN — DENTED (SPOILER) · airframe 41,492 hrs · 22,802 cycles

NR 5 SPOILER LOWER SURFACE HAS A CLUSTER OF DENTS THAT EXCEED THE ALLOWABLE DAMAGE LIMITS 4 IN X 8 IN AREA AT AFT INBOARD CORNER. REPAIRED SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 RT SIDE AT BS 867. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

L1 DOOR MOPSILL CORRODED AT BS 344 TO BS 360. REMOVED CORROSION FOUND OUT OF LIMITS IAW B737 400 SRM 53 10 15 FIG 101. REMOVED AND REPLACED MOPSILL IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

MOPSILL AT R1 DOOR IS CORRODED BS 294 TO BS 344. REMOVED MOPSILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 10 15, 51 40 02, 51 40 05 AND BOEING DWG 65 45875.

Part: MOUNT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

L1 DOOR GIRT BAR RETAINER MOUNT IS CORRODED BS 312. REMOVED CORROSION FOUND OUT OF LIMITS IAW B737 400 SRM 53 10 15 FIG 101. NEW GIRT BAR MOUNT TO BE INSTALLED ON ASA TASK CARD 45199001.

Part: MOUNT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

L1 DOOR AFT GIRT BAR RETAINER MOUNT IS CORRODED BS 314. REMOVED CORROSION FOUND OUT OF LIMITS IAW B737 400 SRM 53 10 15 FIG 101. NEW GIRT BAR RETAINER MOUNT TO BE INSTALLED ON ASA TASK CARD 45199001

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,492 hrs · 22,802 cycles

L1 DOOR MOPSILL IS CORRODED AT BS 344 TO BS 360. REMOVED CORROSION FOUND OUT OF LIMITS IAW B737 400 SRM 53 10 15 FIG 101. REMOVED AND REPLACED MOPSILL IAW B737 400 SRM 51 40 02.

Part: FAIRING — CHAFED (THRUST REVERSER) · airframe 41,492 hrs · 22,802 cycles

NR 2 ENGINE INBOARD THRUST REVERSER STRUT FAIRING IS CHAFED. REMOVED CHAFED FAIRING AND INSTALLED NEW PART IAW B737 400 SRM 51 40 05.

Part: SKIN PANEL — DENTED (RT WING) · airframe 41,492 hrs · 22,802 cycles

RT FIXED WING PANEL UPPER SURFACE (FWD OF NR 5 SPOILER) HAS A CLUSTER OF DENTS. REPAIRED PANEL IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: HINGE FITTING — DAMAGED (SPOILER) · airframe 41,492 hrs · 22,802 cycles

NR 5 SPOILER INBOARD HINGE FITTING LOWER END HAS AN ELONGATED BOLT HOLE AT THE LOWER TRAILING EDGE PANEL FORWARD SUPPORT ROD ATTACH POINT. REMOVED AND REPLACED UPPER AND LOWER FITTINGS IAW B737 400 SRM 51 40 02 AND AMM 20 50 11.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 41,068 hrs · 22,569 cycles

HOLE IN AFT PIT DOOR OUTER SKIN AFT CORNER. INSTALLED REPAIR DOUBLER IAW B737 400 SRM 52 00 01 REPAIR 3.

Part: GASKET — BLOWN (RT WING) · airframe 40,812 hrs · 22,413 cycles

RT WINGBODY OVERHEAT LIGHT ON INTERMITTENTLY AT CRUISE ALT REMAINED ON AFTER BLEED AND PACK TURNED OFF. PERFORMED BITE AND OPS CHECK MM 26 18 00. FOUND ALARM CODE 64 CLEANED ALARM NO FAULTS CURRENT OR HISTORY SYS OPS NORMAL E.QUICK 36251. PERFORMED VISUAL INSPECTION OF PNUMATIC DUCTING FROM 2 ENG TO ISOLATION VLV & RT PACK AREA. FOUND BLOW OUT GASKET AT DUCT TO EXT AIR CONNECTER THAT APPEARED TO BE DIRECTING BLEED AIR ON FIRE LOOP. ALL FIRE LOOPS APPEARED TO HAVE NO DAMAGE. REMOVED & REPLACED GROUND AIR CONNECTOR GASKET & LEAK CHECK GOOD. REF AMM 36 11 45 404 011. RAN NR 2 ENG & OP CHECKED PACKS WITH NO FAULTS NOTED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,492 hrs · 22,802 cycles

AFT CARGO COMPARTMENT BS 727D FRAME LOWER SIDEWALL SUPPORT ANGLE CORRODED/GOUGED STR 21R TO STR 26R. REPAIRED SIDEWALL SUPPORT ANGLE IAW B737 400 SRM 51 70 11.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 38,022 hrs · 20,767 cycles

RT NR 4 LE SLAT INBD UPPER AFT LOWER SKIN IS CHAFED. REPAIRED NR 4 SLAT.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 38,022 hrs · 20,767 cycles

LT NR 3 L/E SLAT INBD LWR SURFACE CHAFED ON AFT CORNER. REPAIRED DAMAGE AT INBD LOWER SURFACE.

Part: INTERCOSTAL — CORRODED (BS 727A-727B) · corrosion level 2 · airframe 38,022 hrs · 20,767 cycles

AFT CARGO COMPARTMENT INTERCOSTAL AT STA 727A TO 727B STRINGER 28L CORRODED. CORROSION REMOVAL OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL.

Part: SKIN — CHAFED (HORIZONTAL STAB) · airframe 38,022 hrs · 20,767 cycles

RT HORIZONTAL STAB AFT LOWER LUG CUTOUT SKIN IS CHAFED. REMOVED AND REPLACED SKIN .

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 38,022 hrs · 20,767 cycles

LT WING INBD FLAP EXHAUST GATE TOP SURFACE FWD OTBD EDGE CHAFED. REMOVED AND REPLACED UPPER SKIN.

Part: SKIN — CHAFED (HORIZONTAL STAB) · airframe 38,022 hrs · 20,767 cycles

LT HORIZONTAL STAB AFT LOWER LUG CUTOUT SKIN IS CHAFED. REMOVED FABBED REPLACEMENT AND INSTALLED.

Part: WEDGE — TORN (LT WING TE FLAP) · airframe 38,023 hrs · 20,767 cycles

LEFT INBOARD MID FLAP T/E WEDGE TORN. REPAIRED WITH DOUBLER AND FILLER PER SRM 51 70 10.

Part: FLAP TRACK — WORN (LT WING TE FLAP) · airframe 38,022 hrs · 20,767 cycles

LT OTBD AFT FLAP ALL 4 TRACKS HAVE WORN AREAS FROM ROLLERS. REMOVED AND REPLACED 4 TRACKS.

Part: SKIN — CHAFED (TE FLAP) · airframe 38,022 hrs · 20,767 cycles

LT WING I/B MID FLAP CHAFED ON TOP I/B SIDE EDGE IN MIDDLE OF FLAP.

Part: WEB — CORRODED (CARGO BAY) · airframe 38,022 hrs · 20,767 cycles

AFT CARGO AT DOOR CUTOUT LOWER TORQUE BOX FORWARD CORNER WEB HAS CORROSION UNDER NUT PLATE. REMOVED AND REPLACED WEB.

Part: FLAP TRACK — GROOVED (FOREFLAP) · airframe 38,022 hrs · 20,767 cycles

RIGHT O/B FORE FLAP O/B TRACK GROOVED ON LOWER FORWARD END. REPLACED FORE FLAP TRACK.

Part: FLAP TRACK — CORRODED (FOREFLAP) · airframe 38,022 hrs · 20,767 cycles

RIGHT O/B FORE FLAP I/B TRACK PITTED. REPLACED FORE FLAP TRACK.

Part: FLAP TRACK — GROOVED (FOREFLAP) · airframe 38,022 hrs · 20,767 cycles

RIGHT O/B FORE FLAP CENTER TRACK LOWER FORWARD END IS GROOVED. REMOVED AND REPLACED TRACK.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 38,022 hrs · 20,767 cycles

NR 3 SLAT DELAMINATED ON I/B UPPER SURFACE. BONDED DOUBLER AND FILLER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 38,022 hrs · 20,767 cycles

LEFT WING O/B AFT FLAP INBOARD CORNER PREVIOUS REPAIR DELAMINATED UPPER SURFACE. REPAIRED THE DAMAGED AREA OF THE LT WING.

Part: SKIN — CRACKED (LE SLAT) · airframe 38,022 hrs · 20,767 cycles

RIGHT WING NR 6 SLAT LOWER AFT EXTERNAL SKIN CRACKED AT RIVET FSS 603. REPAIRED SKIN.

Part: DOOR — CRACKED (RT MLG) · airframe 38,022 hrs · 20,767 cycles

RT MLG WING DOOR CRACKED IN 2 EA PLACES AFT EDGES. REPAIRED CRACKED DAMAGE.

Part: DOUBLER — DELAMINATED (FOREFLAP) · airframe 38,022 hrs · 20,767 cycles

RT IB FOREFLAP UPPER SURFACE PREVIOUS REPAIRS DELAMINATED 48" FROM I/B EDGE 9" FROM TE. REPAIRED AND BONDED RT IB FORE FLAP.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 38,022 hrs · 20,767 cycles

LT WING OB AFT FLAP UPPER SURFACE HAS 2 AREAS OF DELAMINATION BETWEEN REPAIRS. REPAIRED DAMAGED AREAS.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,023 hrs · 20,767 cycles

G4 GALLEY AFT MOUNT WEB CRACKED. REPAIRED WITH DOUBLER FILLER AND PLATE PER EA 400-53EA-02386.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,289 hrs · 20,306 cycles

FUSELAGE SKIN DENT BS 727G STR 25 AND 26 RT. REPAIRED DENT AT BS 727G.

Part: ACTUATOR — BYPASSING (RT MLG) · airframe 35,495 hrs · 19,292 cycles

AFTER GEAR EXTENSION ON FINAL, DID NOT GET A GREEN LIGHT ON THE RIGHT MAIN. WENT TO FLAPS 15 AND HAD GEAR HORN. RAN THE CHECKLIST AND DID A MANUAL GEAR EXTENSION. THIS WORKED, RECEIVED A GREEN LIGHT AND LANDED. JACKED A/C. CYCLED GEAR, RT MAIN DOES NOT FULLY RETRACT OR EXTEND. SUSPECT TRANSFER CYLINDER OR MAIN ACTUATOR DEFECTIVE. SWAPPED THE LT & RT TRANSFER CYLINDERS, NO HELP. SWAPPED CYLINDERS BACK, LEAK/OPS CHECK OK REF MM 32 32 71. REMOVED & REPLACED THE RT MLG ACTUATOR AND RT MLG BEAM HANGAR. OPS/LEAK CHECKED OK. PERFORMED MAIN LANDING GEAR OPERATIONAL TEST. TEST PASSED GEAR RETRACTS/EXTENDS NORMALLY AND ALL INDICATIONS ARE NORMAL. DE JACKED A/C. REF MM 32 32 11, MM 32 32 93, MM 32 32 00.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,479 hrs · 18,752 cycles

RT WING T/E AFT OB FLAP, 3 EACH DENTS CLOSE TOGETHER 5 TO 2 INCHES FROM T/E AND 21 INCHES FROM IB END. PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DAMAGED (BS 1026 S20L) · airframe 34,479 hrs · 18,752 cycles

WHILE INSTALLING REPAIR AT 1028 DAMAGED SKIN NOTED AT STA 1026 JUST ABOVE STR 20L (SEVERAL PROTRUDING DENTS). CUTOUT DAMAGED SKIN FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-80-01, FIG 201, REPAIR 3.

Part: SKIN — DENTED (FOREFLAP) · airframe 34,479 hrs · 18,752 cycles

LT WING IB FORE FLAP DENT WITH A CREASE ON UPPER SURFACE CENTER AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (BS 807 S26-27R) · airframe 34,479 hrs · 18,752 cycles

RT EXTERNAL FUSELAGE DENT BELOW AFT PIT OPENING STA 807, STR 26R TO STR 27R CUTOUT DAMAGED AREA FABRICATED FILLER AND REPAIR DOUBLER LOCATED DRILLED AND INSTALLED IAW EA 5330 02363 AND EA 12774.

Part: SKIN — DENTED (BS 1028) · airframe 34,479 hrs · 18,752 cycles

LT EXTERNAL FUSELAGE DENT ABOVE REPAIR AT STA 1028, STR 13L, CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED IAW DRM 53-80-01, FIG 201, REPAIR 3.

Part: SKIN — DENTED (BS 1001 S5L) · airframe 34,479 hrs · 18,752 cycles

LT EXTERNAL FUSELAGE PROTRUDING DENT AT STA 1001 ON STR 5L CUT OUT DAMAGED AREA FABRICATED FILLER DOUBLER AND TRIPLER LOCATED DRILLED AND INSTALLED IAW EA 5330-02364 AND EA 12771.

Part: SKIN — DENTED (BS 909) · airframe 34,479 hrs · 18,752 cycles

RT EXTERNAL FUSELAGE PROTRUSION DENT AT STA 909 ON STR 17R CUTOUT DAMAGED AREA FABRICATED FILLERS DOUBLER TRIPLER LOCATED DRILLED AND INSTALLED IAW EA 5330 02365 AND EA 12769.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,479 hrs · 18,752 cycles

FWD CARGO DOOR HAS APPROX 1 INCH DENT WITH CREASE IN AFT CENTER OF DOOR SKIN CUT OUT DAMAGED AREA FABRICATED LOCATED DRILLED AND INSTALLED IAW EA 12766 AND EA NR 533002368.

Part: SKIN — DENTED (BS 1040 S12-13L) · airframe 34,479 hrs · 18,752 cycles

FUSELAGE DENT AT STA 1040 AND BETWEEN STR 12L TO 13L US CREASED REF SAD 5088799 CUT OUT DAMAGED AREA FABRICATED REPAIR DOUBLER AND INSTALLED IAW DRM 53-80-01, FIG 201 REPAIR 3.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,479 hrs · 18,752 cycles

AFT CARGO DOOR EXTERNAL SKIN HAS NUMEROUS DENTS WITH CREASES REMOVED DAMAGED SKIN FABRICATED LOCATED DRILLED AND INSTALLED A REPLACEMENT SKIN IAW SRM 52-30-01 FIG. 201-51-40-02 PG. 2.

Part: SKIN — DENTED (BS 1016) · airframe 34,479 hrs · 18,752 cycles

DENT ON FUSELAGE SKIN, STA1016 +16 LBL 8 IS CREASED REF SAD ITEM 5050829 CUT OUT DAMAGED AREA FABRICATED DOUBLER LOCATED DRILLED AND INSTALLED IAW SRM 53-80-01, FIG. 201, PAGES 201TO 205.

Part: SKIN — DENTED (SPOILER) · airframe 34,479 hrs · 18,752 cycles

RT WING IB GROUND SPOILER HAS MULTIPLE DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,479 hrs · 18,752 cycles

LT WING OB AFT FLAP HAS SEVERAL DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,479 hrs · 18,752 cycles

RT WING IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 34,479 hrs · 18,752 cycles

LT WING NR4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS, PREPARED DAMAGED AREA, FABRICATED FILLERS AND REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 34,479 hrs · 18,752 cycles

LT WING IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE (4 EACH). PREPARED DAMAGED AREA FABRICATED FILLERS AND DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 34,479 hrs · 18,752 cycles

RIGHT WING NR 8 SPOILER HAS DENT ON LOWER SURFACE 5 INCHES FROM O/B END. PREPARED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,479 hrs · 18,752 cycles

RT WING IB FORE FLAP DENTED ON UPPER SURFACE 6 INCHES FROM OB EDGE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 34,479 hrs · 18,752 cycles

LT WING NR3 SPOILER LOWER SURFACE HAS ONE DENT 9 INCHES FROM OB END, PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (FOREFLAP) · airframe 34,479 hrs · 18,752 cycles

LT WING OB FORE FLAP HAS SEVERAL DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,479 hrs · 18,752 cycles

LT WING OB AFT FLAP HAS SEVERAL DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 34,479 hrs · 18,752 cycles

LT WING NR4 GROUND SPOILER HAS SEVERAL DENTS ON UPPER SURFACE, PREPARED DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 34,479 hrs · 18,752 cycles

NR 2 SPOILER HAS DENT ON UPPER SURFACE ABOUT 9 INCHES FROM O/B END. PREPARED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 34,479 hrs · 18,752 cycles

LT WING NR1 SPOILER, 2 EACH DENTS ON LOWER SURFACE, PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.

Part: MEC — MALFUNCTIONED (LT ENGINE) · airframe 32,420 hrs · 17,689 cycles

ON ROUTE LAX TO YVR LEFTHAND ENGINE FLAMED OUT IN CRUISE AT FL340. DESCENDED TO FL200 PERFORMED AIR RESTART THEN DIVERTED TO SEA WHERE AIRCRAFT CHANGE WAS MADE BEFORE CONTINUING ON TO YVR. REPLACED ENGINE FUEL PUMP AND MEC (MAIN ENGINE CONTROL). AFTER ENGINE BORESCOPE REVEALED NO DAMAGE, AIRCRAFT AND ENGINE WERE DECLARED SERVICEABLE. SUSPECT MEC WAS CAUSE. FOLLOW-UP ASSESSMENT IS BEING SCHEDULED WITH VENDOR.

Part: FRAME — DENTED (FUSELAGE) · airframe 27,043 hrs · 14,685 cycles

FOUND FWD CARGO FRAME DENTED. REPAIRED PER SRM 51 70 11 AND EA 5330 02062.

Part: SKIN — CHAFED (RT WING FLAP) · airframe 27,043 hrs · 14,685 cycles

RT WING IB MID FLAP UPPER SKIN CHAFED. REPAIRED PER SRM 57 53 01 FIG 201 REPAIR 3.

Part: SILL — CORRODED (BS 913-1007) · corrosion level 2 · airframe 27,043 hrs · 14,685 cycles

FOUND AFT ENTRY SILL CHORD CORRODED. AFT ENTRY SILL CHORD REPLACED WITH MADE REPAIR PART.

Part: SILL — CORRODED (BS 927-987) · corrosion level 2 · airframe 27,043 hrs · 14,685 cycles

FOUND AFT GALLEY SILL CHORD CORRODED. REPLACED PART WITH NEW PART PER SRM 51 40 02.

Part: SKIN — WORN (FUSELAGE) · airframe 27,043 hrs · 14,685 cycles

FUSELAGE SKIN WORN AT DORSAL FIN CONTACT AREA. REPAIRED PER ASA EA 5330 02065.

Part: SKIN — BENT (E/E BAY DOOR) · airframe 24,999 hrs · 13,551 cycles

EE BAY DOOR EXTERNAL SKIN BENT ON EDGE AT SEVERAL PLACES. REMOVED AND REPLACED EE BAY DOOR SKIN. (K)

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,999 hrs · 13,551 cycles

SKIN GOUGED. REPAIRED IAW EA. (K)

Part: STRAP — CORRODED (CARGO BAY) · airframe 24,999 hrs · 13,551 cycles

AFT CARGO SUPPORT STRAP THRESHOLD HAS CORROSION. REMOVED AND REPLACED STRAP. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,999 hrs · 13,551 cycles

CORROSION ON INTERCOSTAL. REMOVED, FABRICATED AND REPLACED INTERCOSTAL. (K)

Part: SKIN — WORN (MID FLAP)

SEA - DURING C-CHECK INSPECTION, FOUND LEFT OUTBOARD MID FLAP SKIN WORN FROM AFT FLAP CARRIAGE CONTACT WITH OUTBOARD AFT FLAP TRACK AREA. REPAIRED IAW EA 5750-01496. (M)

Part: FITTING — GOUGED (RT AILERON)

SEA - DURING C-CHECK INSPECTION, FOUND RIGHT AILERON INBOARD HINGE FITTING IS GOUGED FROM CONTACT WITH SUPPORT FITTING ON AIRCRAFT. REPAIRED IAW ASA EA 2710-01056. (M)

Part: SKIN — GOUGED (FUSELAGE)

SEA - DURING C-CHECK INSPECTION, FOUND APU COMPARTMENT FORWARD FUSELAGE HINGE CUTOUT GOUGED. BLENDED GOUGED AREA AND INSTALLED DOUBLER IAW EA 5330-01384. (M)

Part: SKIN — GOUGED (FUSELAGE)

SEA - DURING C-CHECK INSPECTION, FOUND APU COMPARTMENT FORWARD FUSELAGE HINGE CUTOUT GOUGED. BLENDED GOUGED AREA AND INSTALLED DOUBLER IAW EA 5330-01384. (M)

Part: TANK — CHAFED (APU)

SEA - DURING C-CHECK, FOUND APU OIL TANK RIDING ON UPPER SHROUD ON THE LEFT SIDE OUTBOARD EDGE CAUSING RUB DAMAGE. BLENDED OUTBOARD EDGE OF APU OIL TANK UPPER SHROUD IAW EA 4910-01059. (M)

Part: LIGHT — INOPERABLE (CABIN)

SEA - DURING MAINTENANCE CHECK THE AFT EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERABLE. REPLACED LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (X)

Part: SKIN — DENTED (BS 1050)

OAK - DURING SC WALKAROUND, FOUND LARGE DENT AT STATION 1050, AFT OF L2 DOOR APPROXIMATELY 24 INCHES ABOVE WL. INSTALLED DOUBLER REPAIR PER SRM 53-00-01 AND 53-00-03. (M)

Part: MECHANISM — LACK OF LUBE (L-1 DOOR)

SEA - FLT 62 - L-1 DOOR BINDS. LUBRICATED DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L2 DOOR)

LAX - PRIOR TO FLIGHT 675, THE L2 DOOR WAS REPORTED AS BINDING. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)