N796AS

Part: SKIN — DAMAGED (BS 257-259) · airframe 53,952 hrs · 30,524 cycles

RIGHT NOSE GEAR DOOR AND ADJACENT STRUCTURE DAMAGED. ACFT GROUNDED. INSTALLED REPAIR DOUBLER TO DAMAGED FUSELAGE SKIN AND REPLACED GEAR DOOR.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 53,852 hrs · 30,466 cycles

INTERCOSTAL ATTACH ANGLE AT BS 348.2 STR 15L IS CRACKED. ACFT GROUNDED. REPAIRED IAW AD20121205-400-53-2.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 53,852 hrs · 30,466 cycles

AFT CARGO DOOR FWD END E BEAM OUTER ANGLE IS CRACKED AT 3RD FASTENER AFT VERTICAL LEG. ACFT GROUNDED. REPAIRED AFT CARGO DOOR FWD END E BEAM OUTER ANGLE IAW T/C AD20131312-400-52-15, REV 00, DATED 18AUG14 AND DWG 65C37547.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 51,958 hrs · 29,221 cycles

AFT CARGO DOOR HANDLE HOUSING GOUGED FROM HANDLE DUE TO MISSING BUMPER. ACFT GROUNDED. REMOVED THE INTERIOR AND EXTERIOR DOOR HANDLES FROM THE AFT CARGO DOOR REF AMM 52-31-14. R & R PAN HOUSING REF SRM 51-40-02 SEALED HOUSING AND RIVETED. INSTALLED DOOR HANDLE REF AMM 52-31-14-004-054. WHILE OPERATING NEW DOOR HANDLE FOUND FWD ROLLER BEARING DAMAGED. REMOVED AND INSTALLED A NEW ROLLER. NO RIG PERFORMED. CLEARANCE BETWEEN ROLLER AND FITTING WITHIN LIMITS REF AMM 52-31-00 STEP 3.E.(10). REMOVED AND INSTALLED FWD ACCESS PANEL, LEAK CK OF ACCESS PANEL GOOD.

Part: SEAL DEPRESSOR — CORRODED (L2 DOOR) · corrosion level 2 · airframe 51,676 hrs · 29,036 cycles

AFTER REMOVAL OF FAIRING COMPOUND, FOUND L2 DOOR LOWER HINGE SEAL DEPRESSOR CORRODED. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, W 1, O .080, R 0, L 1, D .080.

Part: FITTING — CRACKED (SEAL DEPRESSOR) · airframe 51,676 hrs · 29,036 cycles

AFTER REMOVAL OF FAIRING COMPOUND FOUND L2 DOOR UPPER HINGE SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0 , 51-40-05-0G-0, FIG 2.

Part: FITTING — CRACKED (SEAL DEPRESSOR) · airframe 51,676 hrs · 29,036 cycles

AFTER REMOVAL OF FAIRING COMPOUND FOUND R2 DOOR HINGE UPPER SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. REMOVED CRACKED UPPER SEAL DEPRESSOR FITTING AND INSTALLED A NEW SEAL DEPRESSOR FITTING ON FWD FRAME OF R2 DOOR IAW SRM 51-40-02-0G-0.

Part: SEAL DEPRESSOR — CRACKED (BS 960) · airframe 51,676 hrs · 29,036 cycles

AFTER REMOVAL OF FAIRING COMPOUND, FOUND R2 DOOR LOWER HINE SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. REMOVED DAMAGED LOWER SEAL DEPRESSOR FITTING AND INSTALLED A NEW ONE AT THE FWD LOWER FRAME AT THE R2 DOOR IAW SRM 51-40-02-0G-0.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,299 hrs · 28,804 cycles

F/A REPORTS ROW 16DEF EMERGENCY EXIT SIGN FALLING DOWN ON OVERWING EXIT. ACFT GROUNDED. SECURED EXIT SIGN ABOVE SEAT 16F. NO DEFECTS NOTED.

Part: STIFFENER — CORRODED (BS 1122-1127) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

APU BAY RT TORQUE BOX AIR INLET CUT OUT, AFT STIFFENER CORRODED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 294) · airframe 50,849 hrs · 28,523 cycles

RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT BS 294.5 BETWEEN S9-10R. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02, INSTALLED FABRICATED ANGLE STIFFENER IAW SRM 51-40-02.

Part: ANGLE — CRACKED (BS 294) · airframe 50,849 hrs · 28,523 cycles

RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT FS 294.5 BETWEEN STR 12-13 RT. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02 LOCATED AND DRILLED NEW ANGLE STIFFENER IAW SRM 51-40-05, INSTALLED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (BS 294) · airframe 50,849 hrs · 28,523 cycles

RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT BS 294.5 BETWEEN STR 11-12 RT. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-40-05 AND SRM 51-40-02.

Part: FRAME — CRACKED (BS 500A) · airframe 50,849 hrs · 28,523 cycles

FRAME BS 500A CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.

Part: FRAME — CRACKED (BS 480) · airframe 50,849 hrs · 28,523 cycles

FRAME AT BS 480 HAS A CRACK BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW ASA EA AD20062609 400-53-132, REV NEW DATED.

Part: FRAME — CRACKED (BS 787) · airframe 50,849 hrs · 28,523 cycles

FRAME BS 787, CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.

Part: FRAME — CRACKED (BS 727D) · airframe 50,849 hrs · 28,523 cycles

FRAME BS 727D CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.

Part: FRAME — CRACKED (BS 727D) · airframe 50,849 hrs · 28,523 cycles

FRAME BS 727D CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.

Part: FRAME — CRACKED (BS 907) · airframe 50,849 hrs · 28,523 cycles

FRAME BS 907 CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

BS 344 FLOORBEAM HAS A SPOT OF CORROSION ON UPPER CAP AT LBL 10. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS AND REPAIRED IAW EA 400, 53EA 13112.

Part: CHANNEL — CORRODED (BS 312-344) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

L1 DOOR MOPSILL HAS MULTIPLE AREAS OF CORROSION. ACFT GROUNDED. R & R MOPSILL, IAW EA 400-53EA-13151.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

FLOORBEAM UPPER CAP FROM LBL 39-RBL 45 IS CORRODED IN SEVERAL AREAS. ACFT GROUNDED. BLENDED DAMAGE IAW SRM 53-60-51-1A-1. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-60-51-1A-1. REPAIRED DAMAGED TEE IAW EA 400-53EA-13131, REV NEW.

Part: SKIN — CHAFED (LT WING LE FLAP) · airframe 50,849 hrs · 28,523 cycles

LT INBD FOREFLAP UPPER SURFACE CHAFED AT PREVIOUS REPAIR. ACFT GROUNDED. REPAIRED LT INBD FOREFLAP UPPER SURFACE AT PREVIOUS REPAIR IAW SRM 51-20-10-2R-0, REPAIR 4.

Part: CHANNEL — CORRODED (BS 907-1006) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

L2 DOOR MOP SILL HAS CORROSION AT FWD END OF DOORWAY. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. R & R MOP SILL IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

FWD FLOOR SUPPORT, LBL 10, BS 328-344 CORRODED. ACFT GROUNDED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

FLOOR SUPPORT, LBL 10, BS 328 - 344 HAS CORROSION. ACFT GROUNDED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 50,849 hrs · 28,523 cycles

FWD WET INTERCOSTAL, LBL 45, BS 312-328 IS CRACKED AT FASTENER HOLE ON UPPER SURFACE. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 50,849 hrs · 28,523 cycles

LEFT OTBD AFT FLAP OTBD CORNER DELAMINATED. ACFT GROUNDED. REPAIRED LT OTBD AFT FLAP OTBD CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: FLOORBEAM — CORRODED (BS 727) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

AFT CARGO BAY FLOORBEAM TEE SPLICE BETWEEN NR 1 AND 2 FLOOR PANELS HAS MULTIPLE AREAS OF CORRODED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE IAW SRM 53-60-53-1A-1, & 51-40-05-0G-0.

Part: SUPPORT — CORRODED (BS 500G) · corrosion level 2 · airframe 50,849 hrs · 28,523 cycles

FWD CARGO LT TRANSITION IS CORRODED AT STA 500G. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS SRM 53-30-53-1A-1 FABRICATED NEW TRANSITION PANEL IAW 400 SRM 51-40-05-0G-0, 51-20-01-0G-0, SOPM 20-41-02 AND SRM 51-40-02-0G-0, AND SRM 53-30-53-2R-3.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 50,849 hrs · 28,523 cycles

LEFT OTBD AFT FLAP OTBD CORNER DELAMINATED. ACFT GROUNDED. REPAIRED LT OTBD AFT FLAP OTBD CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 50,849 hrs · 28,523 cycles

NR 2 L/E SLAT LOWER T/E HAS POSSIBLE CRACK AT RIVET HEAD, MARKED. ACFT GROUNDED. REPAIRED NR 2 L/E SLAT LOWER T/E SKIN IAW SRM 57-43-01-2R-6.

Part: THRESHOLD — CORRODED (BS 947) · airframe 47,158 hrs · 26,343 cycles

LEFT AFT LAVATORY THRESHOLD AFT HAS BULGED AREA ON AFT SIDE. REPAIRED AFT LAVATORY THRESHOLD BULGING AREA IAW NA 25-46-99, REPAIR 2 & 4 AND EA 400-25EA-10035.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,158 hrs · 26,343 cycles

RT OTBD FORE FLAP PREVIOUS REPAIR ON OTBD L/E CHAFED. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-53-01, FIG 201.

Part: SKIN — DEFORMED (BS 410) · airframe 47,158 hrs · 26,343 cycles

LEFT FUSELAGE SKIN IS DENTED FWD OF THE ALTERNATE STATIC PORT. REPAIRED IAW EA 400-53, EA 10047.

Part: WEDGE — CHAFED (NR 4 SLAT) · airframe 47,158 hrs · 26,343 cycles

RT WING NR 4 SLAT INBD T/E WEDGE LOWER SURFACE IS CHAFED. REPAIRED RT WING NR 4 SLAT INBD T/E WEDGE LOWER SURFACE IAW SRM 51 70 10, REPAIR 4.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 47,158 hrs · 26,343 cycles

AFT CARGO BAY BS 945 AFT FLOOR PANEL HAS CORROSION ON AFT RT END. REMOVED, FABRICATED NEW AND INSTALLED NEW FLOOR PANEL IAW AMM 25-52-51-004-001, PARA C, 25-52-51-404-011 PARA D, SRM 51-40-05, FIG 2, DETAIL I, 51-20-01 PARA G AND SOPM 20-41-02, PARA 6F. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-60-53, FIG 101, DETAIL ,.

Part: WEDGE — CHAFED (NR 5 SLAT) · airframe 47,158 hrs · 26,343 cycles

RT WING NR 5 SLAT INBD T/E WEDGE LOWER SURFACE IS CHAFED ON A PREVIOUS REPAIR. REPAIRED RT WING NR 5 SLAT INBD T/E WEDGE LOWER SURFACE IAW SRM 51 70 10, REPAIR 4.

Part: FLOOR PANEL — CORRODED (BS 727D-727F) · airframe 47,158 hrs · 26,343 cycles

AFT CARGO NR 2 FLOOR PANEL HAS CORROSION. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05, FIG 2, DETAIL I, 51 20 01 PARA 6 AND SOPM 20 41 02, PARA 6.F. REMOVED CORRODED ON NR 2 FLOOR PANEL AND FOUND TO BE OUT OF LIMITS IAW SRM 53 60 53, FIG 19 DETAIL V.

Part: SKIN — DENTED (TE FLAP) · airframe 47,158 hrs · 26,343 cycles

LEFT OTBD FOREFLAP L/E IS DENTED APPORX 6 FROM INBD. REMOVED, FABRICATED AND INSTALLED NEW L/E SKIN IAW SRM 51 40 05, 51 40 02.

Part: FLOOR PANEL — PUNCTURED (BS 727E) · airframe 46,370 hrs · 25,879 cycles

REPORTED HOLE IN FLOOR PANEL, AFT CARGO BAY FS 727E. REMOVED DAMAGED AREA AND SECURED DOUBLER IAW SRM 53-60-53 REPAIR 6 AND SRM 51-70-13.

Part: ENGINE — SURGES (NR 1) · airframe 42,654 hrs · 23,699 cycles

ALMOST TO TOP OF CLIMB (18 MIN INTO FLIGHT) BOTH PILOTS HEARD AN ENGINE SURGE NR 1 N1 99% NR 2 N1 96%. NR 1 N1 CAME RIGHT DOWN TO 96%. ON APPROACH HAD A ONE THROTTLE KNOB WIDTH TO MATCH POWER (31 ENGINE THROTTLE BACK TO MATCH) SURGE WAS VERY NOTICABLE IN PAX CABIN. NO ANNUINCIATORS ILLUMINATED. ACCOMPLISHED TEST NR 8 ACCEL/DECEL CHECK. TEST OK NO DEFECTS NOTED. ACCOMPLISHED TEST 5 POWER ASSURANCE CK. TEST OK NO DEFECT NOTED. THROTTLE STAGGER OF LESS THAN 1 KNOB OBSERVED WITHIN LIMITS.

Part: BEAM — CORRODED (CARGO BAY) · airframe 37,596 hrs · 20,597 cycles

AFT CARGO TIE DOWN BEAM HAS MULTIPLE AREAS OF CORROSION FROM STA 778 TO 860 ALONG STR 26R. REPAIRED AFT CARGO TIE DOWN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

AFT CARGO FLOOR SUPPORT ANGLE STA 793 AND STR 27R CORRODED AT SPLICE. REPAIRED AFT CARGO FLOOR SUPPORT ANGLE IAW ASA EA.

Part: FITTING — GOUGED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

UPON BOLT REPLACEMENT FOUND STR END FITTING STR 10L AFT SIDE STA 1016 LOWER HOLE GOUGED. REMOVED AND REPLACED STR 10L FWD END FITTING IAW SRM.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

UPON BOLT REPLACEMENT FOUND STR END FITTING STR 10L AFT SIDE STA 1016 LOWER HOLE ELONGATED. REMOVED AND REPLACED STR 10L AFT END FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

MAIN CABIN FLOORBEAM CORRODED LBL 43 LBL 26 STA 986. REPAIRED FLOORBEAM BETWEEN RBL 20 LBL 57.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

DENT IN FUSELAGE NEAR FWD WHEEL WELL LT SIDE. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR FILLER AND DOUBLER IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 37,596 hrs · 20,597 cycles

RIGHT WING TANK RIB LOWER CHORD AT WBL 135.5 CRACKED IN RADIUS BETWEEN STRINGER NR 2 AND NR 3 O/B OF HYDRAULIC HEAT EXCHANGER. CUT OUT DAMAGED SECTION OF CHORD, INSTALLED FILLERS AND TEE.

Part: RIB — CRACKED (LT WING) · airframe 37,596 hrs · 20,597 cycles

LEFT WING TANK RIB LOWER CHORD AT WBL 135.5 CRACKED IN RADIUS BETWEEN STRINGER NR 2 AND NR 3 O/B OF HYDRAULIC HEAT EXCHANGER. CUT OUT DAMAGED SECTION OF CHORD, INSTALLED FILLERS AND TEE.

Part: SLAT — DELAMINATED (LE SLAT) · airframe 37,596 hrs · 20,597 cycles

LEFT WING LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED AT O/B EDGE. FABRICATED DOUBLER AND BONDED.

Part: WEDGE — CHAFED (LE SLAT) · airframe 37,596 hrs · 20,597 cycles

LEFT WING NR 3 L/E SLAT CHAFED AT I/B SIDE OF TRAILING EDGE WEDGE LOWER SFT CORNER. FABRICATED DOUBLER AND BONDED.

Part: SKIN — DENTED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT INBOARD AFT FLAP OUTBOARD CORNER DAMAGED. REMOVED DAMAGED AREA, FABBED REPLACEMENT PARTS AND BONDED THE REPAIR.

Part: STOP FITTING — CRACKED (DOOR) · airframe 37,596 hrs · 20,597 cycles

FOUND LWR BEAM ON DOOR CRACKED. STOP DRILLED LWR BEAM PER SRM.

Part: DOOR — DAMAGED (CARGO DOOR) · airframe 37,596 hrs · 20,597 cycles

AFT PIT DOOR HAS CREASE 20 INCHES FWD OF AFT EDGE 13 INCHES FROM TOP. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED.

Part: PLATE — CRACKED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT INBOARD MID FLAP ELEPHANT EAR MOUNT PLATE CRACKED AT LOWER AFT BOLT HOLE. REMOVED DAMAGED PART, INSTALLED NEW PART.

Part: SKIN — DENTED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT I/B TRAILING EDGE WEDGE LOWER SKIN HAS TWO DENTS AT 19 INCHES, 19.8 INCHES FROM I/B END 4.5 INCHES, 5 INCHES FROM TRAILING EDGE. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER AND FILLER REPAIR.

Part: RIB — CRACKED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT INBOARD MID FLAP INBOARD AFT RIB CRACKED. REMOVED DAMAGED RIB, INSTALLED NEW RIB.

Part: SKIN — NICKED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT I/B TRAILING EDGE WEDGE PNL LOWER SKIN NICKED 44.5 INCHES FROM I/B END 5 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER AND FILLER REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT I/B AFT FLAP LOWER SURFACE DENTED AT WBL 116. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN RT SIDE STA 380, STR 17R CLIP CRACKED. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — DENTED (LT FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

LT INBD FOREFLAP HAS NUMEROUS DENTS AT UPPER CHAMBER. BONDED .016 DOUBLER IAW SRM.

Part: STRINGER CLIP — CRACKED · airframe 37,596 hrs · 20,597 cycles

AFT CABIN RT SIDE STA 663.75, STR OR STRINGER CLIP IS CRACKED. REMOVED AND REPLACED IAW SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 37,596 hrs · 20,597 cycles

L1 DOOR WEB CRACKED AND GOUGED BETWEEN STA 312 328 LBL 54. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED REPAIR FILLER AND PARTS.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

WEB BETWEEN STA 967 + 986.5 AT LBL 47 IS CORRODED. REMOVED CORRODED WEB, FABBED REPLACEMENT PART AND INSTALLED REPLACEMENT WEB IAW SRM.

Part: SKIN — PUNCTURED (BS 338) · airframe 37,596 hrs · 20,597 cycles

E AND E COMPARTMENT ACCESS DOOR CUTOUT LT WEB PUNCTURED 2 INCHES ABOVE LATCH STA 338 WL 154. REPAIRED WEB IAW SRM 04 REPAIR DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT I/B FORE FLAP LOWER SURFACE DENTED 14 INCHES FROM I/B END 5 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 37,597 hrs · 20,597 cycles

RIGHT WING INBD AFT FLAP UPPER SURFACE AT WBL 100.5 DENTED 5 INCHES FWD OF T/E. BONDED .016 REPAIR DOUBLER IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 37,597 hrs · 20,597 cycles

RIGHT T/E INBD AFT FLAP UPPER OTBD SURFACE HAS A DENT. BONDED .016 REPAIR DOUBLER IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — ACTIVATED (LE SLAT) · airframe 37,596 hrs · 20,597 cycles

NR 5 SLAT I/B CORNER LOWER SURFACE CHAFED. PREPPED CHAFED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT O/B FORE FLAP LOWER SKIN HAS DENT 43 INCHES FROM I/B END 5.2 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT I/B FORE FLAP UPPER SURFACE HAS DENT. PREPPED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT I/B FORE FLAP LOWER SURFACE DENTED 47 INCHES FROM I/B END AND 3 INCHES, 8 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

AFT PIT FRAME STA 807 CORRODED BETWEEN 26L AND 25L. CUT OUT DAMAGED AREA, RECEIVED PART FROM HEAT TREAT, LOCATED, DRILLED, PRIMED, TOP COATED AND INSTALLED FRAME CHANNEL REPAIR.

Part: SKIN — DENTED (FOREFLAP) · airframe 37,596 hrs · 20,597 cycles

RIGHT I/B FORE FLAP LOWER SURFACE DENTED 38 INCHES FROM I/B END 8 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

AFT PIT FRAME CORRODED STA 787 BETWEEN 26L AND 25L. CUT OUT DAMAGED AREA, RECEIVED PART FROM HEAT TREAT, LOCATED, DRILLED, PRIMED, TOP COATED AND INSTALLED FRAME CHANNEL REPAIR.

Part: ATTACH ANGLE — CRACKED (BS 500E) · airframe 37,597 hrs · 20,597 cycles

FWD PIT INTERCOSTAL ATTACH ANGLE CRACKED AT STA 500E BETWEEN STR 25L AND 26L. REMOVED AND REPLACED ANGLE IN IAW SRM 51 40 02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

WEB AT STA 1006 LBL 44 HAS CORROSION AROUND THE FASTENER HOLE. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 380 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 440 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

SHEAR TIE AT 727D INBOARD OF STRINGER 26R IS CORRODED IN AFT CARGO COMPARTMENT. REMOVED CORRODED PART, FABBED REPLACEMENT PARTS AND INSTALLED THE REPAIR.

Part: STRINGER CLIP — BENT (BS 520) · airframe 37,597 hrs · 20,597 cycles

STRINGER CLIP BENT AT STA 520 ON STR 27R. REPLACED CLIP IAW SRM 51 40 01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

STRINGER AT STA 887 IS CRACKED IN THE AFT CABIN. REMOVED DAMAGE, FABBED REPLACEMENT PARTS AND INSTALLED THE REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 747 CRACKED AT FASTENER ABOVE STR 9L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 747 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 827 CRACKED AT FASTENER ABOVE STR 9R. ACCOMPLISHED REPAIR OF FRAME AT STA 827 RT IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 400 CRACKED AT FASTENER ABOVE STR 9L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 37,596 hrs · 20,597 cycles

CABIN FRAME STA 663.75 STRINGER CLIP CRACKED AT STR 10L. REMOVED CRACKED STRINGER CLIP RECEIVED LOCATED AND DRILLED AND INSTALLED NEW CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 360 CRACKED AT FASTENER ABOVE STR 9L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 867 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 787 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — DENTED (CARGO BAY) · airframe 37,596 hrs · 20,597 cycles

AFT CARGO FRAME AT STA 727C IS DENTED AT STR 24R. CUT OUT DAMAGED AREA, LOCATED AND DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED FRAME REPAIR ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT PIT FRAME DENTED STA 727A BETWEEN STR 24L - 25L. CUT OUT DAMAGED AREA, RECEIVED, TREATED, LOCATED, DRILLED, PRIMED, TOP COATED AND INSTALLED FRAME REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 827 CRACKED AT FASTENER ABOVE STR 9L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 480 CRACKED AT FASTENER ABOVE STR 9L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT PIT FRAME DENTED STA 727A AT STR 25R. CUT OUT DAMAGED AREA, RECEIVED, LOCATED, DRILLED, PRIMED, TOP COATED AND INSTALLED FRAME REPAIR.

Part: FRAME — DENTED (CARGO BAY) · airframe 37,596 hrs · 20,597 cycles

AFT CARGO FRAME AT STA 727F DENTED STR 25L. CUT OUT DAMAGED AREA, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED FRAME REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CABIN FRAME STA 400 CRACKED AT FASTENER ABOVE STR 9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW EA.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CARGO COMPARTMENT FRAME AT STA 727B IS DENTED AT STR 24R. REMOVED DAMAGED AREA, FABRICATED REPAIR PART AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 867 CRACKED AT FASTENER ABOVE STR 9L. ACCOMPLISHED REPAIR OF FRAME AT STA 867 LT IAW EA.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CARGO FRAME STA 727G DENTED AT STR 25R. CUT OUT DAMAGED AREA, LOCATED AND DRILLED, TREATED PRIMED TOP COATED AND INSTALLED NEW REPAIR DOUBLER.

Part: SKIN — DENTED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT I/B TRAILING EDGE AFT FLAP LOWER SKIN HAS A DENT AT 9.8 INCHES FROM I/B END 6 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED EXTERNAL DOUBLER REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

AFT CABIN FRAME STA 907 CRACKED AT FASTENER JUST ABOVE STR 9L MARKED. ACCOMPLISHED REPAIR OF FRAME AT STA 907 LT IAW EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FRAME AT STA 887 + STR 21R FASTENER HOLE DAMAGED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS INSTALLED REPAIR.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

STRINGER CLIP DAMAGED AT STA 887 STR 2R PREVIOUS REPAIR. REMOVED DAMAGED CLIP AND INSTALLED NEW CLIP.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD PIT INTERCOSTAL ATTACH ANGLE CRACKED STA 500F BETWEEN 25L - 26L. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW ATTACH ANGLE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD PIT FRAME TO INTERCOSTAL ATTACH ANGLE CRACKED STA 380 STR 26L. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW ATTACH ANGLE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

FWD CARGO PIT FRAME ATTACH ANGLE CRACKED STA 380 STR 26R. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW ATTACH ANGLE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

MAIN CABIN FLOOR WEB AT STA 987 IS CORRODED. REMOVED DAMAGED WEB, FABBED REPLACEMENT PARTS AND INSTALLED REPLACEMENT PARTS.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

MAIN CABIN FLOOR STRUCTURE AT RIGHT AFT GALLEY SERVICE DOOR MOP SILL CORRODED. REMOVED AND REPLACED R2 MOP SILL.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 37,596 hrs · 20,597 cycles

FLOORBEAM AT STA. 312 RBL 8 CORRODED AT FASTENER. REPAIRED FLOORBEAM UPPER CHORD IAW SRM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT WING I/B FLAP T/E WEDGE HAS PUNCTURE AND DENT. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

L1 DOOR CUTOUT SCUFF PLATE 11B SUPPORT ANGLE CORRODED. REMOVED CORRODED ANGLE, LOCATED, DRILLED AND INSTALLED NEW SUPPORT ANGLE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,596 hrs · 20,597 cycles

L2 DOOR MOP SEAL/CHORD IS CORRODED. REMOVED CORRODED PART AND INSTALLED NEW PART.

Part: SLAT — CHAFED (NR 4) · airframe 37,596 hrs · 20,597 cycles

NR 4 SLAT LWR SURFACE I/B AFT CORNER CHAFED. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER REPAIR.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 37,596 hrs · 20,597 cycles

L1 DOOR CUTOUT LOWER HINGE BOTTOM FITTING CRACKED. REMOVED CRACKED FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,596 hrs · 20,597 cycles

DENT 32 IN AFT OF L2 DOOR IS LESS THAN 3 IN FROM LAP SPLICE AT STA 1016. CUT OUT DAMAGED SKIN AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR FILLER AND DOUBLER.

Part: SKIN — BENT (L1 DOOR) · airframe 37,596 hrs · 20,597 cycles

L1 DOOR UPPER AFT SKIN REPAIR IS BENT. REMOVED PREVIOUS REPAIR, FABBED REPAIR PARTS AND INSTALLED NEW REPAIR.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LT T/E INBD AFT FLAP UPPER SKIN AT WBL 92.8 FWD OF T/E IS DENTED. REMOVED DAMAGED SECTION FABRICATED TREATED PRIMED AND BONDED SKIN AND DOUBLER REPAIR. IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,916 hrs · 20,220 cycles

DENT IN FUSELAGE SKIN JUST BELOW FWD CARGO DOOR. REPAIRED PER SRM 53 00 01 REPAIR 32.

Part: SKIN — DENTED (TE FLAP) · airframe 37,596 hrs · 20,597 cycles

LEFT INBOARD FORE FLAP LWR SURFACE HAS 5 DENTS FROM WBL 84.5 123.8. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 35,878 hrs · 19,615 cycles

NR 8 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 35,878 hrs · 19,615 cycles

NR 1 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 35,878 hrs · 19,615 cycles

NR 7 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 35,878 hrs · 19,615 cycles

NR 2 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: GUST LOCK — STIFF (L1 DOOR) · airframe 35,251 hrs · 19,249 cycles

F/A REPORTS L1 DOOR GUST LOCK IS DIFFICULT TO RELEASE. OPS CHECK OF L1 DOOR GUST LOCK GOOD. LUBRICATED AND NO DEFECTS FOUND.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 34,053 hrs · 18,609 cycles

AFT CABIN BS 986.5 FLOORBEAM LBL 4 FOUND CORRODED AT FASTENER HOLE LOCATION (CLIP NUT). AFT CABIN FLOOR BEAM AT BS 986 LBL 4 CORROSION AT FASTENER LOCATION REPAIRED IAW B737 400 SRM 53 00 51 FIG 201 REPAIR 3.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 1 · airframe 34,053 hrs · 18,609 cycles

AFT CABIN BS 986.5 FLOORBEAM CORRODED AT RBL 40 TO RBL 46 (PREVIOUS REPAIR). REPAIRED WITH REPAIR PART.

Part: ANGLE — CORRODED (BS 993) · corrosion level 2 · airframe 34,053 hrs · 18,609 cycles

R2 DOOR FLOOR STRUCTURE CORROSION FOUND AT BS 993 RBL 42 ON ZEE REPAIRED WITH REPAIR PART.

Part: WEB — CORRODED (BS 986) · corrosion level 2 · airframe 34,053 hrs · 18,609 cycles

R2 DOOR FLOOR STRUCTURE CORROSION FOUND AT BS 986.5 RBL 44 UPPER SURFACE OF WEB. REPAIRED WITH REPAIR PART.

Part: SKIN — DAMAGED (BS 382 S16L) · airframe 34,053 hrs · 18,609 cycles

TEMPORARY FASTENER AT BS 382 STR 16L TO 17L WL 208 DAMAGE AT BS 382 STR 16L TO 17L WL 208. REPAIRED IAW B737 400 SRM 53 00 01, REPAIR 26 FIG 201.

Part: WEDGE — DAMAGED (NR 5 SLAT) · airframe 34,053 hrs · 18,609 cycles

RT WING NR 5 LE SLAT T/E OUTBOARD END FILLING COMPOUND DAMAGE. RT WING L/E SLAT NR 5 T/E OUTBOARD END REPAIRED IAW B 737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (WING) · airframe 34,053 hrs · 18,609 cycles

TWO DENTS FOUND ON LWR SURFACE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS, PERMANENT REPAIR IAW BOEING SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,053 hrs · 18,609 cycles

LT OUTBOARD T/E AFT FLAP LWR SKIN HAS 3 DENTS AT WBL 231.5 TO 240 2.5" FROM T/E. REPAIRED WITH REPAIR PART.

Part: FRAME — CRACKED (BS 616) · airframe 34,053 hrs · 18,609 cycles

CRACK FOUND ON INNER FRAME CHORD AT BS 616 RT WL200 AT STUB BEAM CRACK ON INNER CHORD WAS REPAIRED IAW ASA EA NR 5310 02790.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 34,053 hrs · 18,609 cycles

RT OUTBOARD T/E FORE FLAP L/E GOUGED, REPAIRED WITH REPAIR PART.

Part: WEB — CHAFED (DOOR FRAME) · airframe 34,053 hrs · 18,609 cycles

E/E BAY DOOR LATCH PIN RUBBING ON RT WEB OF DOOR CUT OUT. WEB OF DOOR CUT OUT REPLACED IAW 51-40-02.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,053 hrs · 18,609 cycles

RT WING TRAILING EDGE RT WING INBOARD AFT FLAP LOW SURFACE HAS A SHARP DENT IN LEADING EDGE CAP AT OUTBOARD ACTUATING ROD. DENT ON LT WING TRAILING EDGE RT WING AFT FLAP LOWER SURFACE WAS REPAIRED IAW B737 400 SRM 57 53 01.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 34,053 hrs · 18,609 cycles

RAMP REPORTS 2 DENTS ON HORIZONTAL STAB (LT) 2' FROM TIP. DENTS ON HORIZONTAL STAB (LT) 2' FROM TIP APPROX REPAIRED IAW SRM 55-10-01 FIG 201.

Part: OIL SYSTEM — OVERTEMP (CSD) · airframe 33,376 hrs · 18,268 cycles

IN FLIGHT NR 2 ENGINE CSD OIL HIGH TEMP LIGHT ILLUMINATED. CSD OIL TEMP WAS PEGGED TO RIGHT. NOTE: FLIGHT CREW SHUTDOWN NR 2 ENGINE THEN RESTARTED. ENGINE OPS NORMAL AFTER RESTART. RESET GENERATOR NR 2 PER MM 24 11 00 PGS 101 104. PERFORMED MAINT ON OIL FILTERS PER TC 48524002. OP CHECKS GOOD. RESAFTIED GENERATOR DISCONNECT.

Part: SKIN — DEFORMED (L1 DOOR) · airframe 33,344 hrs · 18,250 cycles

L1 DOOR UPPER AFT CORNER DEFORMED INSTALLED EXTERNAL DOUBLER TO L1 DOOR AFT UPPER CORNER PER EA 5210 01238 AND SRM 52 00 01, 51 40 03.

Part: STRUCTURE — DEFORMED (PAX DOOR) · airframe 33,343 hrs · 18,250 cycles

L1 DOOR UPPER AFT CORNER DEFORMED. RECONTOURED AND INSTALLED REPAIR DOUBLER PER EA 5210 01237 AND 5210 01238.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,655 hrs · 15,020 cycles

EMERGENCY LIGHTS CAME ON MOMENTARLY THEN GOES OFF. REPEAT WRITE UP. CHANGED BATTERY PACK.

Part: CHARGER — MALFUNCTIONED (CABIN) · airframe 27,655 hrs · 15,020 cycles

SEVERAL (4 TOTAL) EMERGENCY LIGHTS COME ON MOMENTARILY THEN GO OUT RIGHT AWAY DURING EMERGENCY LIGHTS TEST. REPLACED BATTERY CHARGER AND BATTERY PACK.

Part: SKIN — CHAFED (LT FORE FLAP) · airframe 30,348 hrs · 16,524 cycles

THE LEFT WING O/B FORE FLAP L/E IS CHAFED OUT OF LIMITS AT THE O/B END. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW ASA EA 5750 02325.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 30,348 hrs · 16,524 cycles

THE RIGHT WING O/B FORE FLAP IS PUNCTURED ON THE LWR SURFACE NEAR THE I/B END. REMOVED DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 APRA 7, 11, 15, 18 AND 20.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 30,348 hrs · 16,524 cycles

RIGHT WING NR 6 SPOILER SURFACE IS PUNCTURED 8 INCHES FROM THE T/E, 12 INCHES FROM THE O/B EDGE (UPPER SURFACE). PREPPED THE DAMAGED AREA OF UPPER SKIN FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 30,348 hrs · 16,524 cycles

THE LEFT WING I/B MIDFLAP T/E IS DENTED AND GOUGED AT THE AFT EDGE ON THE LWR SURFACE. PREPARED THE LWR SKIN FOR BONDING, APPLIED POTTING COMPOUND, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.

Part: SKIN — DENTED (TE FLAP) · airframe 30,348 hrs · 16,524 cycles

THE RIGHT WING O/B AFT FLAP HAS A LARGE DENT JUST BELOW THE SECOND CARRIGE FROM THE O/B END. REMOVED THE DAMAGED AREA OF LWR SKIN AND CORE FABRICATED AND INSTALLED A CORE PLUG SKIN FILLER AND TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 9, 11, 15, 18 AND 20.

Part: SKIN — BENT (L1 DOOR) · airframe 30,348 hrs · 16,524 cycles

THE L 1 DOOR EXTERNAL SKIN IS BENT AT THE UPPER AFT CORNER. CUTOUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND AN EXTERNAL REPAIR DOUBLER IAW SRM 52 00 01 FIG 201.

Part: SKIN — DENTED (BS 806-807) · airframe 30,348 hrs · 16,524 cycles

THE AFT CARGO DOOR EXTERIOR SKIN IS DENTED OUT OF LIMITS 13.25" FROM THE TOP EDGE 11" FROM THE FWD EDGE BETWEEN THE NR 1 AND NR 2 BEAMS. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM 52 00 01 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,154 hrs · 14,743 cycles

AIRCRAFT SUSTAINED DENT AND GOUGED. REPAIRED LOWER SKIN WITH WITH EXTERNAL PER EA 5330 02049.

Part: SKIN — WORN (FS 860-880)

OKC - FOUND WEAR MARKS IN FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5330-02032. (M)

Part: FLOORBEAM — CORRODED (FS 986.5)

OKC - FOUND CORROSION ON BS 986.5 FLOORBEAM UPPER CHORD. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PIECES AND INSTALLED IAW EA 5360-01049. (M)

Part: SKIN — DENTED (L2 DOOR)

OKC - FOUND L-2 DOOR SKIN DENTED 11.5 INCH FORWARD OF AFT EDGE, 12 INCHES BELOW TAP EDGE, AFT OF HANDLE AND 9 INCHES ABOVE AFT END OF DOOR HANDLE. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED DOUBLER IAW ASA EA 5230-01291. (M)

Part: FLOORBEAM — CORRODED (FS 344)

OKC - FOUND CORROSION ON FLOORBEAM AT BS 344 UPPER FLANGE. REMOVED DAMAGE, CORROSION, FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD IAW ASA EA 5320-01710. (M)

Part: SILL — CORRODED (FS 302-379)

OKC - FOUND R1 DOOR MOPSILL IS CORRODED. REMOVED AND REPLACED R-1 DOOR MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (CARGO DOOR)

OKC - FOUND FORWARD CARGO DOOR CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED SUPPORT AND CHANNEL PER B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (FS 915-1006)

OKC - FOUND L2 DOOR MOPSILL IS CORRODED. REMOVED AND REPLACED L2 DOOR MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: MOUNT — CORRODED (GIRT BAR)

OKC - FOUND L1 DOOR GIRT BAR RETAINER MOUNTS CORRODED. REMOVED AND REPLACED MOUNTS IAW B737-400 SRM 51-40-05. (M)

Part: SILL — CORRODED (FS 277-360)

OKC - FOUND L-1 DOOR MOPSILL CORRODED. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE)

OKC - FOUND R-2 DOOR MOPSILL CORRODED. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 51-40-02. (M)

Part: STRUCTURE — BROKEN (T/E FLAP)

OKC - FOUND LEFT OUTBOARD AFT FLAP OUTBOARD CORNER BENT UP AND BROKEN. REPAIRED DAMAGED AREA, IAW B737-400 SRM 51-70-10 PAGES 213, 221, 238, AND 249. (M)

Part: SKIN — DENTED (HORIZONTAL STAB)

OKC - FOUND DENT IN LEFT HORIZONTAL L/E 10 INCH FROM OUTBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIGURE 201, REPAIR 2. (M)

Part: SKIN — DENTED (HORIZONTAL STAB)

OKC - FOUND RIGHT HORIZONTAL STAB HAS 2 EACH DENTS 4 FEET OUTBOARD FROM ROOT ON L/E. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR REPAIR 2. (M)

Part: SKIN — DENTED (RT WING)

OKC - FOUND DENT IN RIGHT L/E 15 FEET OUTBOARD FROM WING ROOT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR 2. (M)

Part: WEB — CORRODED (AFT CARGO DOOR) · airframe 24,373 hrs · 13,242 cycles

CORROSION ON SUB-THRESHOLD WEB AT AFT CARGO DOOR OPENING. CORROSION REMOVAL BLENDED OUT OF LIMITS, REPLACED SUB-THRESHOLD WEB. (K)

Part: PLATE — CORRODED (FUSELAGE) · airframe 24,373 hrs · 13,242 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE NUMEROUS AREAS BSTA 727-767, RBL 21. CORROSION BLENDED OUT OF LIMITS, REPAIRED IAW SRM. (K)

Part: FRAME — CORRODED (FUSE;AGE) · corrosion level 2 · airframe 24,373 hrs · 13,242 cycles

FWD CARGO BAY, CORROSION ON FRAME AT BSTA 500C, WL 148, LBL 5 TO RBL 5. REPAIRED FRAME IAW SRM. (K)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,373 hrs · 13,242 cycles

CORROSION FOUND ON VHF NR 3 ANT. DOUBLER. REPLACED VHF NR 3 ANT. DOUBLER. (K)

Part: PLATE — SCRATCHED (COCKPIT) · airframe 24,373 hrs · 13,242 cycles

UPPER TCAS MOUNTING PLATE IS DAMAGED, REPLACED MOUNTING PLATE. (K)

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 24,373 hrs · 13,242 cycles

FLOOR TO AFT BULKHEAD SUPPORT ANGLE DAMAGED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (K)

Part: PLATE — CORRODED (FUSELAGE) · airframe 24,373 hrs · 13,242 cycles

FLOOR TO SIDEWALL SUPPORT PLATE CORRODED. REMOVED AND REPLACED FLOOR-TO-SIDEWALL SUPPORT PLATE. (K)

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 24,373 hrs · 13,242 cycles

FOOR TO AFT BULKHEAD SUPPORT ANGLE DAMAGED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (K)

Part: SIGN — MISSING (CABIN)

PDX - FOUND FLOOR EXIT SIGN MISSING NEAR L2 DOOR. REPLACED SIGN, OPS NORMAL. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

PDX - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M)

Part: SKIN — DENTED (APU DOOR)

PAE - WHILE PERFORMING C-CHECK, FOUND DENT IN APU EXTERIOR DOOR SKIN 14 INCHES FROM FORWARD EDGE 4 INCHES FROM LEFT EDGE. REPAIRED IAW SRM. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

ANC - ON CLIMB-OUT THROUGH FLT LEVEL 200, NR 2 ENGINE HAD 2 COMPRESSOR STALLS AND SUBSEQUENT FLAME OUT. ENGINE SHUT DOWN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE, OPERATIONAL CHECKED NORMAL, RELEASED. REMOVED ENGINE IS BEING SENT TO GE STRUTHERS FOR EVALUATION. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

ANC - ON CLIMB-OUT THROUGH FLT LEVEL 200, NR 2 ENGINE HAD 2 COMPRESSOR STALLS AND SUBSEQUENT FLAME OUT. ENGINE SHUT DOWN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE, OPERATIONAL CHECKED NORMAL, RELEASED. (M)

Part: PANEL — DAMAGED (WING)

SEA - DURING C-CHECK, FOUND PANEL 8501 DAMAGED ON LOWER SURFACE. REPAIRED IAW EA. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ONT - BEFORE FLIGHT FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 14 INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHTS AT ROW 14. OPERATIONAL CHECKS NORMAL. (M)

Part: CHARGER — INOPERATIVE (CABIN) · corrosion level 3 · airframe 6,214 hrs · 3,538 cycles

SEA - DURING MAINTENANCE CHECK, BOTH LEFT AND RIGHT FORWARD EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND IDENTIFIERS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHT AT OVERHEAD BIN 19ABC WAS FOUND INOPERATIVE. CHECKED AND RELEASED PER MEL 33-15B. ON 8-11-98 RELAMPED, NO HELP. TOOK A VOLTAGE READING AT D007104 AND D007106. VOLTAGE WAS ERRATIC. DID NOT FIND ANY VISIBLE DAMAGE TO WIRING. REQUIRES FURTHER TROUBLESHOOTING. REMAINS ON MEL. ON 8-12-98 FOUND GROUND WIRE DISCONNECTED ABOVE OVERHEAD BIN, RECONNECTED WIRE, NO HELP. PROBLEM GOT WORSE. NO VOLTAGE PRESENT AND NOW LIGHT AT 22ABC WAS INOPERATIVE. REQUIRES FURTHER TROUBLESHOOTING. REMAINS ON MEL. (X)