N975AT

Part: RELAY — FAULTY (CABIN) · airframe 45,971 hrs · 31,267 cycles

OVERWING EMERGENCY LIGHTS WON'T EXTINGUISH AFTER SETTING EMERGENCY LIGHT SWITCH TO OFF AS REPORTED BY 2ND SHIFT (WILL ONLY SWITCH OFF ON 'ARM' POSITION). T/S PER FIM 33-51-00-802. REMOVED AND REPLACED OVERWING EMER EVAC LIGHTS BATTERY PACK RELAY R2-273 IAW AMM 33-51. OPERATIONAL CHECK SATISFACTORY INCLUDING OW EMERG EVAC LIGHTS.

Part: CUSP WEB — CORRODED (BS 416-417) · airframe 43,821 hrs · 29,760 cycles

CORROSION ON THE CUSP WEB, RBL 54 AND 60, BS 416 TO 417, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.

Part: HINGE — DAMAGED (LT WING LE FLAP) · airframe 42,112 hrs · 28,494 cycles

ELONGATED HOLE ON LT WING OUTBOARD FLAP FWD OUTBOARD HINGE IAW NRTC 00456. THE HINGE WAS REMOVED IAW AMM 20-50-01 AND AMM 27-50-01. THE BEARING WAS REPLACED, AND THE HINGE WAS REPAIRED IAW ER/A 552872-14 REV ORIGINAL

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

CRACKED EXTERNAL FUSELAGE SKIN STA 1021 BTW LONG 13/14 LT. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ETI-17-16-183 REV. ORIGINAL AND ER/A 552865-14 REV ORIGINAL SECTION I. PERFORM REPETITIVE EXTERNAL GENERAL VISUAL INSPECTION OF THE REPAIR EVERY C-CHECK OR 24 MONTHS WHICHEVER COMES FIRST AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR PER ER/A 552865-14 REV ORIGINAL SECTION II. THIS INSPECTION WILL BE MONITORED UNDER LOG PAGE 2808839.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

AFT ACCESSORY COMPARTMENT HAS A CRACK ON STIFFENER STA Y=1200 CANT LONG PROJECTION 2L. STIFFENER WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201 IN REF ORNRC 00394.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

AFT CARGO COMPARTMENT HAS A CRACK ON VERTICAL SUPPORT STA Y=816 LONG 30 (AMDS 5331-2001). CRACK DIMENSION IS .650". CRACK IN VERTICAL SUPPORT WAS STOP DRILLED PER SRM 53-00-00 FIG 201, HFEC WAS ACCOMPLISHED. NO CRACK WERE FOUND AFTER STOP DRILL PER NDT SPM 06-10-01.001. REPAIR PARTS WERE FABRICATED AND INSTALLED PER SRM 53-00-00 FIG 201, SRM 51-20-09, AND 51-41-02.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 42,112 hrs · 28,494 cycles

FWD CARGO DOOR: CRACK ON ANGLE UPPER EDGE OF DOOR BETWEEN BS 408-410. DAMAGE AREA WAS REPAIRED IAW SRM 52-00-00 REPAIR 2, AND DWG 9957663 REV W.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

FWD CARGO COMPARTMENT HAS A CRACKED SUPPORT ON STA Y=655 BTW LONGS 23R AND 24R. SUPPORT WAS REPAIRED PER SRM 53-00-00 FIG 201 SHEET 1 REF ONNRC 363.

Part: BULKHEAD WEB — CRACKED (BS 218) · airframe 42,112 hrs · 28,494 cycles

FWD CARGO COMPARTMENT HAS CRACKED WEB OF FWD BULKHEAD BS 218, 15 INCHES ABOVE LONGERON 27. THE BULKHEAD WAS REPAIRED BS SRM 53-00-00 REPAIR 1.

Part: LONGERON — CRACKED (BS 1152) · airframe 42,112 hrs · 28,494 cycles

IN THE AFT ACCESORY COMPARTMENT THERE IS A CRACK ON LONGERON 4L, BS 1152. THE LONGERON WAS REPAIRED IAW SRM 53-00-05, REPAIR 2, FIGURE 201, 51-40-08, AND 51-41-05.

Part: FRAME — CRACKED (BS 1037) · airframe 42,112 hrs · 28,494 cycles

CRACK ON FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07 REPAIR 4, 51-41-01, AND 51-41-05.

Part: LONGERON — CRACKED (BS 1152) · airframe 42,112 hrs · 28,494 cycles

AFT ACCESORIES COMPARTMENT HAS A CRACK ON LONGERON 3L BS 1152. REPAIRD IAW SRM 53-00-05 REPAIR 2 FIGURE 201 AND 51-41-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

BARREL KEEL BEAMS; CRACKS ON RT/LT FRAMES KEEL AREA FROM STA Y=655 TO Y=737. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, SRM 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, AND 37. CRACK FRAME DIMENSIONS, STA 679LH 0.656 IN , 694RH 0.906 IN, AND 715R 0.406 IN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

CRACK ON FRAME CLIP AT STA Y=1022 BTW LONG 16L AND LONG 17L. FRAME CLIP WAS REPLACED PER DWG 9912243 REV JS, SRM 51-41-02 AND 51-41-05.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

FWD CARGO COMPARTMENT: CRACKED RT SUPPORT ON STA Y=664 LONG PROJECTION 23R AND 24R. FITTING WAS REPLACED PER SRM 51-41-02.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,112 hrs · 28,494 cycles

CORROSION ON FUEL ACCESS PLATE 620DT. CORROSION WAS REMOVED ON COUNTERSINK AREA AND SETTLEMENT SURFACE ON ACCESS PLATE 620DT PER SRM 51-10-04 PAR 26, COUNTERSINK AREA WAS MEASURED MAXIMUM COUNTERSINK DIAMETER ALLOWABLE IS 0.660", MAX DIAMETER MEASURED IS 0.705" THEREFORE IS OUT OF SERVICE DUE TO EXCESSIVE DAMAGE IN 4 AREAS COUNTERSINK ADJACENT PER SRM 57-10-01 REPAIR 2 CONDITION II (A). FUEL ACCESS PLATE WAS REPLACED.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,112 hrs · 28,494 cycles

L1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 1. REPAIRED IAW SRM 52-10-02 REPAIR 7 FIGURE 201.

Part: CUSP WEB — CRACKED (BS 656-674) · airframe 42,112 hrs · 28,494 cycles

CRACK ON LT CUSP WEB LBL 54 - 60, BS 656 - 674 . REPAIRED IAW SRM 53-00-55 FIG 215.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,112 hrs · 28,494 cycles

L1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 7. REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 201.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 42,112 hrs · 28,494 cycles

CRACKED DOOR FRAME WEB BS 207 LONGERON 11 AND 15L. REPAIRED IAW SRM 53-10-15.

Part: FRAME — CRACKED (BS 1022) · airframe 42,112 hrs · 28,494 cycles

CRACKED FRAME ANGLE ON BS 1022, LONGERONS 13 - 14L. REPLACED IAW DWG 9912243 REV. JS, SRM 51-41-02 AND 51-41-05.

Part: CUSP WEB — CRACKED (BS 671-674) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT CUSP WEB BS 671 - 674, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 203.

Part: CUSP WEB — CRACKED (BS 652-655) · airframe 42,112 hrs · 28,494 cycles

CRACKED CUSP WEB BS 652 - 655, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 211.

Part: SKIN — DELAMINATED (RUDDER TAB) · airframe 42,112 hrs · 28,494 cycles

DELAMINATON ON RUDDER TAB SKIN. THE RUDDER TAB SKIN WAS REPAIRED IAW SRM 55-41-01 REPAIR 1, AND 51-70-02 REPAIR 3 PAR 5.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 42,112 hrs · 28,494 cycles

DELAMINATED FLOOR PANEL 211ALF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 42,112 hrs · 28,494 cycles

DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.

Part: PAN — CRACKED (BS 794) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT RING PAN LOWER FWD CORNER BS 794. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.

Part: PAN — CRACKED (BS 832) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.

Part: PAN — CRACKED (BS 889) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT RING PAN LOWER FWD CORNER BS 889. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 42,112 hrs · 28,494 cycles

PUNCTURES ON RT CUSP WEB BTW STA Y=974 TO Y=975 AND BTW Y=989 TO Y=990, X=49R. PUNCTURE WAS DRILLED, DAMAGE WAS REMOVED PER SRM 53-00-00 PAR 2, AND FASTENERS WERE INSTALLED PER SRM 51-41-02.

Part: PAN — CRACKED (WINDOW) · airframe 42,112 hrs · 28,494 cycles

CRACK ON LOWER FWD CORNER AT RING PAN WINDOW LT SIDE BTW STA Y 598-617. CRACKED RING PAN LOWER FWR CORNER BTW STA Y=598-617 LT, WAS REPAIRED PER SRM 56-20-02 FIG 202.

Part: PAN — CRACKED (BS 851) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT RING PAN UPPER & LOWER AFT CORNERS BS 851. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.

Part: PAN — CRACKED (BS 696) · airframe 42,112 hrs · 28,494 cycles

CRACKED RT RING PAN UPPER FWD CORNER BS 696. REPAIRED THE RING PAN WAS REPAIRED IAW SRM 56-20-02 FIG. 202.

Part: SKIN — DELAMINATED (LT WING SPOILER)

DURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.

Part: SKIN — DELAMINATED (LT WING SPOILER)

DURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE LOWER AND UPPER SURFACE. SUP: P/N 5940974-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,841 hrs · 29,037 cycles

DURING ATG4 MODIFICATION, MAINTENANCE NOTED THAT ALL FIVE HOLES COMMON TO THE SKIN OF THE SHEAR TIE WERE DAMAGED AND DID NOT PASS NDT INSPECTION. REPAIRED IAW ER/A 00-545433.

Part: SKIN — CRACKED (BS 1076) · airframe 41,791 hrs · 28,262 cycles

SKIN CRACKED AT BS 1076 LONGERON 14R. REPAIRED THE SKIN IAW PRI 542271-14 REV. 0 AND ER/A 542271-14 REV. ORIGINAL.

Part: CABLE — FRAYED (ESCAPE SLIDE) · airframe 38,562 hrs · 25,646 cycles

DURING SERVICE CHECK, FOUND TAILCONE SLIDE KEVLAR DEPLOYMENT CABLE FRAYED. REPLACED AFT TAILCONE SLIDE DEPLOYMENT CABLE IAW AMM 25-61. LP 7277097.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,398 hrs · 24,678 cycles

DURING LINE CHECK, NOTED CEILING EXIT LIGHTS IN FIRST CLASS AND 2 ROWS OF COACH EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK, BS-227 IAW AMM 33-51.

Part: LENS — CRACKED (CABIN) · airframe 35,640 hrs · 23,139 cycles

R1 DOOR EXIT LIGHT LENS CRACKED. R & R LENS ASSEMBLY IAW AMM.

Part: WIRE — LOOSE (CABIN) · airframe 35,640 hrs · 23,139 cycles

RT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.

Part: WIRE — LOOSE (CABIN) · airframe 35,640 hrs · 23,139 cycles

LT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 35,640 hrs · 23,139 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED WIRE IAW WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,260 hrs · 22,880 cycles

AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,260 hrs · 22,880 cycles

OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R OVERWING EMERGENCY LIGHTS BATTERY PACK IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

INTERCOSTAL CRACKED BETWEEN STATION 619 & 636, BL 0. R & R INTERCOSTAL IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

STRINGER SPLICE 6R DAMAGED & CRACKED AT BS 246. R & R STRINGER SPLICE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 598 TO STATION 617, STRINGER 18L. REPAIRED WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

LONGERON CRACKED AT STATION 1133, LONGERON 2R. R & R LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

LONGERON CRACKED AT STATION 1133, LONGERON 2L. R & R LONGERON IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

SEAT TRACK CRACKED WEB SPLICE BETWEEN STATION 636 TO STATION 655, RBL 44. R & R PLATE IAW DRAWING SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FRAME SUPPORT ANGLES CRACKED AT STATION 1166, BETWEEN LONGERON 3R TO LONGERON 3L. R & R ANGLE IAW DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

DORSAL SUPPORT ANGLE CRACKED BETWEEN STATION 1095 TO STATION 1133, LONGERON 2R. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FRAME FORMER CRACKED AT BS 1053, LONGERON 3L. R & R CLIP IAW DRAWING & SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FRAME FORMER CRACKED AT STATION 1152, LONGERON 3R. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FRAME CORRODED AT STATION 908, BETWEEN STRINGER 29R & STRINGER 29L. REPAIRED FRAME IAW SRM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 35,260 hrs · 22,880 cycles

LT WING TE FLAP HINGE FAIRING 530 HB MOVEABLE FAIRING LOWER SECTION DELAMINATED. R & R FAIRING IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FWD CARGO PIT FUSELAGE SKIN CORRODED. REPAIRED SKIN IAW EA.

Part: LIGHT — DAMAGED (EXTERIOR) · airframe 35,260 hrs · 22,880 cycles

LT EXTERNAL EMERGENCY LIGHT AFT OF WING DAMAGED. R & R LIGHT ASSEMBLY IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

SHEAR TIE CRACKED AT STATION 1152, BETWEEN STRINGER 1 TO STRINGER 2R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

SHEAR TIE CRACKED AT STATION 1166, BETWEEN STRINGER 2L TO STRINGER 3L. R & R SHEAR TIE IAW DRAWING.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CUSP WEB CRACKED AT BS 674 LONGERON 18R. R & R WEB IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 35,260 hrs · 22,880 cycles

EMERGENCY EXIT LIGHT LENS CEILING PANEL 222GC CRACKED. R & R LENS IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FS STRUCTURE INNER WINDOW FRAME SURROUND CRACKED IN LOWER FORWARD CORNER AT BS 560, STRINGER 14L. R & R FRAME IAW DRAWING & AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

PASSENGER CABIN FLOOR SEAT TRACK AT LT SIDE INBD CORRODED AT STATION 986. R & R TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 737+12" TO STATION 737+14, STRINGER 18L. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 522 TO STATION 541, STRINGER 18L. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 870 TO STATION 889, STRINGER 18L. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 541 & STATION 560, STRINGER 18L. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 794 TO STATION 813, STRINGER 18L. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED AT BS 351+10" STRINGER 18L. REPAIRED WEB IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FRAME CRACKED AT STATION 1053, STRINGER 18L. R & R BRACKET IAW DRAWING & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 560 & STATION 579, AT STRINGER 18L. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM CORRODED AT STATION 832 TO STATION 851, STRINGER 18L. REPAIRED CREASE BEAM APE SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CREASE BEAM WEB CORRODED AT BS 313+5" STRINGER 18L. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CUSP WEB SUPPORT BRACKET CORRODED AT STATION 648, LONGERON 18R. R & R BRACKET IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

TAIL COMPARTMENT, AFT SIDE OF STATION Y-1178.225 CANTED FRAME APPROXIMATELY 10:O'CLOCK POSITION LBL 17, CLIP CRACKED. R & R CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

CENTER WING BOX FLOOR FITTING CRACKED AT STATION 737, RBL 45. R & R FITTING IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

OVER WING FLOOR BEAM CRACKED AT BS 696 LONGERON ON 18L. R & R BEAM YAW DRAWING.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

INTERCOSTAL ATTACH BRACKET CRACKED AT BS 237, BETWEEN STRINGER 27R & 28R. R & R BRACKET IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FLOOR BOARDS SEAT TRACK VERTICAL SUPPORT LOWER ATTACH POINT CRACKED AT STATION 737, LBL 45. R & R BRACKET IAW SRM & DRAWING.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

INTERCOSTAL CRACKED ATTACH BRACKET AT BS 237, BETWEEN STRINGER 27L & 28L. R &R BRACKET IAW SRM & DRAWING.

Part: PLATE — CRACKED (RT MLG WW) · airframe 35,260 hrs · 22,880 cycles

RT MAIN WW AFT INBD LOWER BULKHEAD AREA SHROUD PLATE CRACKED. R & R SHROUD IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,260 hrs · 22,880 cycles

FWD CARGO LOWER DOOR JAMB FRAME CORRODED BETWEEN STATION 370 TO STATION 427, RBL 16 TO RBL 18. REPAIRED DOOR JAMB FRAME IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 35,561 hrs · 23,094 cycles

RT EMERGENCY LIGHT LENS CAP MISSING AT ROW 1. INSTALLED LENS IAW AMM.

Part: AILERON — CRACKED (RT WING) · airframe 35,368 hrs · 22,972 cycles

RT AILERON CRACKED AT TE. REPAIRED AILERON IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,168 hrs · 22,837 cycles

RT EMERGENCY ESCAPE LIGHT ASSEMBLY INOPERATIVE AT ROW 1. R&R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 32,596 hrs · 21,241 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER M/M.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 32,511 hrs · 21,183 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,083 hrs · 20,897 cycles

EEPLS INOP BETWEEN ROW 25 TO ROW 31. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,604 hrs · 20,578 cycles

EMERGENCY LIGHT ABOVE R1 DOOR INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: RUDDER — OUT OF ADJUST (TAIL) · airframe 31,281 hrs · 20,378 cycles

EXCESSIVE/ABNORMAL AMOUNT OF RT AILERON TRIM REQUIRED DURING FLAPS 40 EXTENSION. ADJUSTED RUDDER PER MM.

Part: CONNECTOR — DEFECTIVE (CABIN)

ROW 10 EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED CONNECTOR AT SEAT 10DEF. REF WDM 33-51 OPS CHECK GOOD.

Part: MOUNT — CORRODED (FUSELAGE)

G2 GALLEY FITTING MOUNTS, CORROSION. ACCOMPLISHED GALLEY FITTING MOUNTS REPLACEMENT PER B717 SRM 51-41-01.

Part: PAN — CRACKED (CABIN)

OBSERVERS SEAT CUT OUT CABIN FLOOR PAN, CRACKED. ACCOMPLISHED CABIN FLOOR PAN FILLER REPAIR PER B717 SRM 51-40-02 AND 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 200, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 51-10-04, 51-40-08 AND 53-10-51.

Part: SEAT TRACK — CORRODED (BS 160-200)

SEAT TRACK, STA 160 TO 200, LBL 8, CORRODED. ACCOMPLISHED SEAT TRACK REPLACEMENT PER SRM 51-40-08 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (BS 229)

FLOOR SUPPORT, STA 229, LBL 18, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-40-02, 51-40-03 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

L1 DOOR FLOOR SUPPORT, STA 179, LBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (BS 200)

FLOOR SUPPORT, STA 200, BL 0, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-40-02, 51-40-08, 51-10-51 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (BS 200)

FLOOR SUPPORT, STA 200, RBL 17, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-41-02, 51-40-08 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 200)

FLOOR SUPPORT, STA 200, LBL 12, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-40-02, 51-40-08, 51-10-51 AND 51-41-02.

Part: SEAT TRACK — CORRODED (BS 230)

SEAT TRACK, STA 230, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE PER SRM 53-20-52, 51-40-08 AND 51-40-02.

Part: SEAT TRACK — CORRODED (BS 160)

SEAT TRACK STA 160 RBL 8 CORRODED. ACCOMPLISHED SEAT TRACK REPLACEMENT PER SRM 51-40-03, 51-40-02 AND 53-10-51.

Part: FLOOR SUPPORT — CORRODED (BS 256)

FLOOR SUPPORT, STA 256, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 51-40-08 AND 53-10-51.

Part: PAN — CORRODED (BS 200)

FORWARD CABIN FLOOR PAN, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR PAN REPLACEMENT PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (BS 196)

FLOOR SUPPORT, STA 196, LBL15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-41-02, 51-10-04, 51-40-08 AND 53-10-51.

Part: LENS — BROKEN (EXIT SIGN)

L1 DOOR EXIT SIGN COVER BROKEN. REMOVED AND REPLACED LENS ASSY, OK FOR SERVICE REF AMM 33-28.

Part: COVER — MISSING (CABIN)

CABIN OVERHEAD LIGHTED "EXIT" SIGN MISSING ABOVE ROW ONE. REPLACED "EXIT" SIGN COVER OVER ROW 1 AISLE IAW B717 MM 33-51. OPS GOOD.

Part: COMPRESSOR — STALLED (LT ENGINE)

LEFT ENGINE COMPRESSOR STALL ALERT IN CLIMB THROUGH FL230. TRANSFERRED TO NRWC N082031 ITEM 1, ENGINE FAILED BORESCOPE, REF ITEM 3 LOG PAGE 1696965.

Part: SIGN — UNSECURE (CABIN)

AFT EMERGENCY RED COVER ON AFT BULKHEAD EXIT WILL NOT STAY ON. AFT BULKHEAD EXIT SIGNS SECURED NO DEFECTS NOTED MM 33-20.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

WHEN PERFORMING EMERGENCY LIGHT PREFLIGHT TEST, NO ILLUMINATION OF COCKPIT LIGHT. CYCLED SWITCH, LIGHT CHECK OK PER MM 33-51.

Part: LENS — OUT OF POSITION (CABIN)

FOUND LENS FOR EMERGENCY PATH LIGHTING AT 2D KNOCKED OFF. DURING LENS INSTALLATION, SHORTED BATTERY SUPPLY. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY PER AMM 33-51. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OPS CHECKS GOOD B171 AMM 33-51.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT BILGE FRAME, STA 927, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED BILGE FRAME SPLICE REPAIR PER B717 SRM 53-00-06 REPAIR 2.

Part: DOUBLER — CRACKED (FUSELAGE)

RT VENT BOX INTERNAL DOUBLER & EXISTING OUTER STIFFENER CRACKED. INSTALLED NEW INTERNAL DOUBLER & OUTER STIFFENER PER SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR LOWER JAM CORRODED BEYOND LIMITS. CUT OUT CORRODED AREA, INSTALLED REPLACEMENT PAN IAW B717 SRM 51-40-02.

Part: ANGLE — CRACKED (CARGO DOOR)

FWD CARGO DOOR REAR EDGE ANGLE IS CRACKED. INSTALLED DOUBLER REPAIR PER B717 SRM 52-30-02 FIG 201.

Part: BATTERY PACK — DISCHARGED (CABIN)

SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD, REF MM 33-51.

Part: LIGHT — WILL NOT TEST (TAIL COMP)

TAIL COMPARTMENT EMERGENCY LIGHT DID NOT TEST ON A CHECK L2-738. CLEANED LIGHT TERMINALS, OPS CHECK GOOD IAW B717 MM 3353.

Part: STRUT — LOW (NLG)

NOSE GEAR FAILED TO RETRACT CYCLED GEAR AND STILL FAILED TO RETRACT. LOCKED OKAY IN DOWN POSITION. INSPECTED AIRCRAFT NO DEFECT WITH NOSE GEAR OR RETRACTION SYSTEM. PUT AIRCRAFT ON JACK, CYCLED GEAR THROUGH 5 TIMES. NO DEFECTS NOTED DURING RETRACTION CHECK PER M/M 32-30. FOUND NOSE STRUT SERVICE TO BELOW, SERVICED NOSE STRUT PER MM 32-21. JACKED AIRCRAFT AGAIN AND RETRACTED GEAR. NO DEFECT NOTED. GEAR OPS CHECKS GOOD ON GROUND.