N972AT

Part: COVER — MISSING (CABIN) · airframe 47,069 hrs · 31,551 cycles

MID CABIN EMERGENCY LIGHT COVER IS MISSING. MAINTENANCE INSTALLED THE MISSING COVER. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,536 hrs · 31,162 cycles

OVERWING EXIT DOOR EMERGENCY CEILING LIGHT FAILED TO TEST. MAINTENANCE FOUND B5-120 BATTERY PACK TO BE BAD. BATTERY PACK WAS REPLACED PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,480 hrs · 29,860 cycles

AFT EMERGENCY DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51.

Part: PAN — CORRODED (BS 954) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

AFT CARGO DOOR CUTOUT, FWD EDGE BS 954 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 1A. ACCOMPLISHED DOOR PAN SPLICE REPAIR IAW ER/A 553691-14 REV O.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,207 hrs · 28,988 cycles

LONGERON 16L CRACKED AT BS 1022. REPLACED THE LONGERON IAW SRM 53-00-05, REPAIR 2.

Part: SEAT TRACK — CORRODED (BS 994-1028) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

BS 994 TO 1028 SEAT TRACK CORRODED. . REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-41-05.

Part: NOT REPORTED — CORRODED (BS 954) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

BS 954 CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103.0 . REPLACED THE SPLICE IAW SRM 51-41-05 AND DWG 9958214.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT CUSP WEB, BS 598 TO 617, RBL 54.5 CORRODED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.

Part: SEAT TRACK — DAMAGED (BS 986-1053) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

LEFT CENTER SEAT TRACK, LBL 44.5, BS 986 - 1053 HAS AREAS SCRATCHED AND LIGHT CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-20-52-2R REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 146 & 157) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

CORROSION ON THE LOWER SURFACE OF THE FORWARD CABIN SUBFLOOR (E/E CEILING) ON THE FORWARD SIDE OF FLOORBEAM AT BS 146 AT RBL 7, AND AT BS 157 AT RBL 5. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55-1A. REPAIRED IAW SRM 51-70-10-2R-2, AND SRM 51-41-02 PG 1-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

CORROSION ON THE LOWER SURFACE OF THE FORWARD CABIN SUBFLOOR (E/E CEILING) ON THE AFT SIDE OF FLOORBEAM AT STA 200, FROM BL5R TO BL9R. REPAIRED SUB FLOOR CORROSION FROM STA 200-218 RBL2 TO RBL 25 IAW SRM 51-70-10-2R1 AND ENGINEERING EWO 75834-0000-0009.

Part: SEAT TRACK — DAMAGED (BS 465-565) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

SEAT TRACK, RBL 44.5, BS 465 - 565, HAS AREAS OF GOUGING AND CORROSION. BLENDED CORROSION OUT OF LIMITS. REPAIRED IAW SRM 53-20-52 REPAIR 1, RESTORED TOP COAT IAW SRM 51-22-01 ITEM 8.

Part: CUSP WEB — CORRODED (BS 201) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT CUSP WEB CORRODED RBL 44 BS 201. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55-1A-1. PERFORMED TYPICAL REPAIR ON THE CUSP WEB IAW SRM 51-70-10-2R-2.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 43,207 hrs · 28,988 cycles

INTERCOSTAL BETWEEN UPPER FLOORBEAMS IN FORWARD CARGO BSW 617 - 636 CRACKED. REPAIRED THE INTERCOSTAL IAW SRM 51-70-10 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 148-157) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

FLOOR SUPPORT BS 148 - 157, BL0 CORRODED. CLEANED THE CORROSION ON FLOOR SUPPORT IAW SRM 53-00-00-1A, FIG 103, 53-10-51-0I-2, AND 51-30-07-06, FIG 9 BEYOND ALLOWABLE LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-41-05 AND SWG 9936534.

Part: CUSP WEB — CORRODED (BS 889-908) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

BS 889 - 908 CUSP WEB AND ANGLE SPLICE LT SIDE CORRODED. REMOVED CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-00-55. REPLACED THE CUSP WEB IAW SRM 53-00-55, AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 157-180) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

FORWARD CABIN BS 157 - 180, LBL 44 FLOOR SUPPORT CORRODED. REMOVED THE CORROSION IAW SRM 53-00-00 ALLOWABLE DAMAGE 1. FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-05 AND DWG 99366533.

Part: SEAT TRACK — DAMAGED (BS 200-256) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT CENTER SEAT TRACK, RBL 44.5, BS 200 - 256, GOUGED AND CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-52-2R REPAIR 1.

Part: SEAT TRACK — DAMAGED (BS 756-856) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

LEFT CENTER SEAT TRACK BS 756 - 856, LBL 44.5, HAS CORRODED, SCRATCHED, AND GOUGED. BLENDED THE SEAT TRACK AND FOUND OUT OF LIMITS IAW SRM 53-20-52-1A. REPLACED THE SEAT TRACK IAW SRM 53-20-52-2R.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT INBD SEAT TRACK, RBL 22, BS 200 - 256 IS GOUGED AND HAS AREAS OF CORROSION. THE SEAT TRACK WAS FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-20-52-2R REPAIR 1.

Part: CUSP WEB — CRACKED (BS 216) · airframe 43,207 hrs · 28,988 cycles

RIGHT CUSP WEB IS CRACKED AT BS 216, RBL 45. CUT OUT CRACKED AREA IAW SRM 53-00-00-2R 1 & 2. FABRICATED A REPAIR DOUBLER & FILLER IAW SRM 53-00-00 2 R2, AND INSTALLED IAW SRM 51-41-02, 51-41-05, AND 51-41-08.

Part: SEAT TRACK — CORRODED (BS 468) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

UPPER CABIN SEAT TRACK CORRODED AT BS 468 RBL 44.5. BLENDED OUT OF LIMITS. REPAIRED IAW 53-20-52, REPAIR .

Part: FLOORBEAM — CRACKED (BS 737) · airframe 43,207 hrs · 28,988 cycles

FLOORBEAM BS 737, LBL 44 IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-41-02 AND 51-41-05.

Part: SEAT TRACK — DAMAGED (BS 361) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

SEAT TRACK RBL 44.5 IS CORRODED, AND GOUGED BS 332 - 408. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS AT BS 361. REPAIRED IAW SRM 53-20-52-2R REPAIR.

Part: SHEAR TIE — CRACKED (BS 1136) · airframe 43,207 hrs · 28,988 cycles

BS 1136, LONGERON 15R SHEAR TIE IS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-05, SRM 51-40-08, AND DWG 5913596.

Part: CUSP WEB — CORRODED (BS 518) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT CUSP WEB, BS 518, RBL 54.5 CORRODED. REPAIRED THE CUSP WEB IAW SRM 53-08-35-2R-4, AND 53-20-51-01-1.

Part: FLOOR SUPPORT — CORRODED (BS 202-239) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

FORWARD FUSELAGE FLOOR SUPPORT BS 202-218, 221-239, LBL 14 CORRODED. REPLACED THE FLOOR SUPPORT IAW DWG 9936535.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,207 hrs · 28,988 cycles

FUSELAGE, CABIN, RT CUSP WEB, STA 487 R54.5, UNDERSIDE, CORROSION. REPAIRED CUSP WEB STA 389-503 RT SIDE IAW SRM 53-00-55 2R-4. FABRICATED AND INSTALLED 7075-T6. 032 DOUBLER AND 7075-T6. 020. FILLER WET WITH SEALANT IAW SRM 53-00-55 2R-4. ALODINED, PRIMED, AND TOPCOATED REPAIR PARTS AND AREA IAW AMM 51-10-00 370-803.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

FUSELAGE, CABIN, RT CUSP WEB, STA 584 R56.0 AT DOUBLER, UNDERSIDE CORROSION. REPAIRED DAMAGED CUSP 584 RT SIDE, IAW SRM 53-00-55 REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

RIGHT INBOARD SEAT TRACK BL22R STATIONS 465-565 HAS AREAS OF GOUGES AND CORROSION. BLENDED AREA AT VL 22R STA 489-491 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52-1A WITH .036" REMOVED REMAINING MATERIAL .079" WITH NOMINAL AT .115". INSTALLED 3-LUG REPAIR IAW B717 SRM 53-20-52 REPAIR 1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

SUB FLOOR AT STA 157 BL5R CORRODED ON LOWER SURFACE. REPAIRED CORRODED AREA ON SUB FLOOR STA 157 BL5R IAW 51-70-10-2R-2 AND SRM 51-41-02 PG 3 PAR F.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

FUSELAGE, CABIN, RT STA 889 TO 908 R56.0, SPLICE DOUBLER, UNDERSIDE, CORROSION. REPLACED LOWER SKIN SPLICE DOUBLER AT STA 889-908 IAW SRM 51-41-05.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 43,207 hrs · 28,988 cycles

STA 870-889 CORROSION WAS FOUND ON EXISTING CUSP WEB REPAIR DOUBLER AND WAS FOUND TO BE OUT OF LIMITS IAW 51-00-00 .015" MATERIAL REMOVED. REMOVED AND INSTALLED NEW DOUBLER IAW SRM 51-41-02 AND 53-00-55 2R-4 FIG 215.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 43,207 hrs · 28,988 cycles

FWD FLOOR CUSP MEMBRANE CRACKED IN EXISTING REPAIR DOUBLER AT FS190 RBL8. MARKED. REPLACED FWD FLOOR CUSP MEMBRANE REPAIR DOUBLER AT FS 190RBL 8 IAW SRM 51-40-03-0G PAR 16 STEP A, SRM 51-40-03-0G PAR 6 STEP A, SRM 53-00-55-2R-4 NOTE 27, SRM 51-41-08-0G PAR 7 AND SRM 51-41-05 FOR INSTALL AND IAW SRM 51-70-10-2R-2 FOR FABRICATION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,207 hrs · 28,988 cycles

STA 908-927 CORROSION ON BOTH SIDES OF CUSP LT SIDE. INSTALLED EXTERNAL AND RING DOUBLER REPAIR LT CUSP WEB STA 913 FOR BLENDS OUT OF LIMITS REF SRM 53-00-55-2R-4.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,207 hrs · 28,988 cycles

FORMER IS CRACKED JUST ABOVE LONGERON 15L AND STA 1022. REPLACED SHEAR TIE / FORMER WITH NEW SHEAR TIE / FORMER IAW SRM 51-41-02, 51-41-05, AND DRAWING 99122434197.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,207 hrs · 28,988 cycles

FLC DOOR LOWER FWD CORNER HAS A CRACK ON DOOR PAN.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 42,749 hrs · 28,684 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING L2-791 WAS NOT TESTING. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,736 hrs · 27,951 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN SERVICE DOOR EMERGENCY LIGHT IN THE CEILING WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,969 hrs · 27,311 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CUSP WEB — CRACKED (BS 674) · airframe 39,288 hrs · 26,091 cycles

CUSP MEMBRANE FOUND CRACKED AT BS 674. REPAIRED IAW ER/A 533035-14MA.

Part: DOOR FRAME — CRACKED (RT OVERWING) · airframe 39,288 hrs · 26,091 cycles

RT OVERWING FRAME CRACKED IN RADIUS OVER .125 CONDITION 3 FOUND. REPLACED FRAME IAW AMDS WC 5310-01436-03B.

Part: HOLDER — LOOSE (L2 DOOR) · airframe 38,245 hrs · 25,263 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. R & R HOLDER ASSEMBLY IAW SIP.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 38,200 hrs · 25,234 cycles

FORWARD ENTRY DOOR FLASHLIGHT CHARGE INDICATOR LIGHT INOPERATIVE. REPOSITIONED FLASHLIGHT IN HOLDER IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 38,142 hrs · 25,195 cycles

EMERGENCY EXIT LIGHT BROKEN AT CEILING PANEL ROW 1. R & R EXIT LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,551 hrs · 24,789 cycles

AFT OVERHEAD EMER EXIT SIGN INOPERATIVE AFTER TEST. R & R BATTERY PACK IAW MM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 37,353 hrs · 24,657 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. R & R FASTENER IAW AMM.

Part: SCREW — MISSING (R1 DOOR) · airframe 37,150 hrs · 24,521 cycles

R1 DOOR SLIDE GIRT BAR RETAINING BRACKET SCREW MISSING. INSTALLED FASTENER IAW MM.

Part: SUPPORT BRACKET — LOOSE (GIRT BAR) · airframe 35,456 hrs · 23,419 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CENTER SUPPORT BRACKET LOOSE. SECURED BRACKET IAW MM SIP.

Part: SIGN — BROKEN (CABIN) · airframe 35,257 hrs · 23,297 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. REPAIRED COVER IAW SIP.

Part: COFFEEMAKER — LEAKING (GALLEY) · airframe 34,975 hrs · 23,125 cycles

AIR TURNBACK DURING INITIAL CLIMB OUT, ACRID SMELL NOTED IN COCKPIT, FLIGHT ATTENDANT’S REPORTED MILD SMOKE & ELECTRIC ARCING VICINITY OF COFFEE-MAKER CIRCUIT BREAKERS. FOUND NR 2 COFFEE MAKER RACK LEAKING CAUSING WIRING HARNESS BELOW FOR NR 3 COFFEE MAKER TO SHORT. R&R HARNESS & CONNECTOR@ NR 3 COFFEE MAKER RACK IAW WDM. R&R WATER INLET CONNECTOR ASSEMBLY @ NR 2 COFFEE MAKER RACK IAW MM. R&R NR 3 COFFEE MAKER.

Part: DOUBLER — CRACKED (LE SLAT) · airframe 34,645 hrs · 22,918 cycles

LT WING NR 5 SLAT TRACK CUTOUT CRACKED. REPAIRED DOUBLER IAW EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 34,645 hrs · 22,918 cycles

FUSELAGE SKIN CORRODED AT STA 863, LONG 28L. REPAIRED DOUBLER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LOUVER BOX IN AFT ACCESSORY COMPARTMENT ANGLE CRACKED AT UPPER INBD ATTACHMENT TO STATION 1200 FRAME. R & R ANGLE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FUSELAGE SKIN CORRODED AT STA 863, LONG 28L. R & R SKIN IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FRAME CRACKED AT STA 1133, LONG 26L. R & R FORMER IAW SRM & DWG.

Part: DOUBLER — CRACKED (LE SLAT) · airframe 33,728 hrs · 22,365 cycles

LT WING SLAT TRACK NR 5 CUTOUT CRACKED. REPAIRED DOUBLER IAW MM AND EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

CUSP CORRODED BETWEEN STA 598 TO STA 617. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 875. REPAIRED CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 33,728 hrs · 22,365 cycles

FWD CARGO DOOR LOWER FWD CORNER CRACKED BRACKET. R & R SPLICE IAW SRM AND DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 674. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

CUSP WEB CORRODED BETWEEN STA 446 AND STA 465 RT. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR SUPPORT NUT CLIP STRAP CRACKED AT STA 655. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

CUSP CORRODED BETWEEN STA 617 TO STA 636. R & R CUSP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

CUSP ANGLE CORRODED BETWEEN STA 579 TO STA 598. R & R CUSP ANGLE SPLICE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED BETWEEN STA 832 TO STA 851. REPAIRED CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 715. R & R CUSP IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL EDGE CORRODED BETWEEN STA 756 TO STA 794, LBL 44. REPAIRED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 804. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED BETWEEN STA 560 TO STA 579. R & R CUSP IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL EDGE CORRODED. R & R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 760. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RT CUSP CORRODED BETWEEN STA 465 TO STA 484. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 570. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED AT STA 670. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 421. R & R CUSP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

CUSP ANGLE CORRODED BETWEEN STA 579 TO STA 598. R & R CUSP ANGLE SPLICE IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL CORRODED BETWEEN STA 389 TO STA 465, RBL 44. R & R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 617 TO STA 636. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 535. R & R CUSP IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL CORRODED BETWEEN STA 541 TO STA 636, RBL 44. REPAIRED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED BETWEEN STA 389 TO STA 408. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT CUSP CORRODED AT STA 496. REPAIRED CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 636 TO STA 655. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 636 TO STA 710. R & R CUSP IAW SRM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

AFT BULKHEAD DOOR LT MIDDLE STOP FITTING CRACKED. R & R MIDDLE STOP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 851 TO STA 870. REPAIRED CUSP WEB IAW MM AND SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED AT STA 565. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED AT STA 980. REPAIRED CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 889 TO BS 908. REPAIRED CUSP IAW MM AND SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LT CUSP CORRODED AT STA 380. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 579 TO STA 598. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 503 TO STA 513. R & R CUSP IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FORMER CRACKED AT BS 1022, LONG 14R. REPAIRED FORMER IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL CORRODED BETWEEN STA 370 TO STA 389, RBL 44. R & R PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT FRAME WEB CRACKED AT STA 1178. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 541 TO STA 560. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT CUSP CORRODED BETWEEN STA 598 TO STA 617. R & R CUSP IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,728 hrs · 22,365 cycles

L1 DOOR HANDLE MECHANISM FITTING CRACKED INSIDE TOWARDS THE FRONT. R & R INTERCOSTAL IAW SRM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 33,728 hrs · 22,365 cycles

LEFT WING FIXED L/E INBD SIDE BONDING STRAP CRACKED. R & R STRAPS IAW SRM & DWG.

Part: ANGLE — CRACKED (LE SLAT) · airframe 33,728 hrs · 22,365 cycles

LEFT WING NR5 SLAT OTBD SIDE TRACK INBD ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 33,728 hrs · 22,365 cycles

RIGHT WING AT WING ROOT L/E BONDING STRAP CRACKED. R & R STRAPS IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

SHEAR TIE CRACKED AT STA 1161, LONG 2R. R & R SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

SHEAR TIE CRACKED AT STA 1161, LONG 2L. R & R SHEAR TIE IAW SRM AND DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FORMER CRACKED AT BS 1144, LONG 2R. R & R FORMER IAW SRM & DWG.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LONGERON CRACKED AT BS 1133, LONG 2R. R & R LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

RIGHT SIDE MAIN FRAME WING TO BODY FITTING AND STRAP CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 AHF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222AF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 AFT DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222JF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 221 WF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 221UF DELAMINATED. R & R PANEL IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

LEFT SIDE MAIN FRAME WING TO BODY FITTING CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222ABF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 ATF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222PF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 ACF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222FF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222AGF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 223 AF DELAMINATED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222AEF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 AMF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 LF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 RF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 33,728 hrs · 22,365 cycles

FLOOR PANEL 222 AVF DELAMINATED. R & R PANEL IAW SRM.

Part: CABLE — LOOSE (R1 DOOR) · airframe 34,547 hrs · 22,850 cycles

R1 DOOR SLIDE CABLE LOOSE. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: STARTER — FAULTY (APU) · airframe 33,266 hrs · 22,058 cycles

BATTERY CHARGER ALERT WOULD NOT EXTINGUISH FOLLOWED BY UNUSUAL DISCHARGE AND ODOR IN CABIN. REMOVED AND REPLACED MOTOR PER AMM.

Part: FITTING — CORRODED (FUSELAGE)

AFT CARGO BILGE SHEAR CLIPS, STA 927, LONG 28L TO 30, CORROSION. ACCOMPLISHED SHEAR CLIPS SPLICE REPAIR PER B717 SRM 53-00-06 REP 2.

Part: BRACKET — CORRODED (FWD AIRSTAIRS)

FWD AIRSTAIRS TORQUE TUBE BRACKET, CORROSION. ACCOMPLISHED TORQUE TUBE BRACKET REPLACEMENT PER B717 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL31 TO RBL43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148 TO 200, RBL7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL46 TO RBL56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 8 TO LBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-40-02.

Part: FITTING — CORRODED (GIRT BAR)

MAIN CABIN GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 190 TO 200, RBL 7 TO LBL 7, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02 AND 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

NUMEROUS EMERGENCY ESCAPE PATH LIGHTS ON AISLE SIDE OF BUSINESS CLASS SEATS ARE INOP. REPLACED POWER SUPPLY FOR FLOOR EMERGENCY LIGHTS IAW B717 AMM 33-51. TESTS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 28 E-PATH LIGHTS INOP. RELAMPED ROW 28 E-PATH LIGHTS WITH CORRECT BULB TYPE IAW AMM 33-51-04. OPS CHECK NORMAL IAW AMM 33-51-00.

Part: SKIN — DAMAGED (FUSELAGE)

INTERNAL DOUBLER AND FUSELAGE SKIN, STA 1144, LONG L21L TO L22L, DAMAGED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-02784IR.

Part: LONGERON — CRACKED (FUSELAGE)

LEFT FUSELAGE LONGERON, STA 1144 TO L21L, CRACKED. ACCOMPLISHED FUSELAGE LONGERON SPLICE REPAIR PER EA 17-53-02784IR.

Part: SKIN — DAMAGED (VERTICAL STAB)

LEFT SIDE VERTICAL STAB SKIN AND STRUCTURE, DAMAGED. ACCOMPLISHED DOUBLER AND SKIN REPAIR PER EA 17-55-02781IR.

Part: SKIN — DAMAGED (HORIZ STAB)

LEFT SIDE HORIZONTAL STAB SKIN AND STRUCTURE LEADING EDGE, DAMAGED. ACCOMPLISHED LEADING EDGE DOUBLER AND FILLER REPAIR PER EA 17-55-02506IR.

Part: SKIN — DAMAGED (FUSELAGE)

EXTERIOR FUSELAGE SKIN, STA 1124 TO 1144, LONG L18L TO L23L, CREASED. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR PER B717 SRM 53-00-01 REP 6.

Part: MOUNT — DAMAGED (LT ENGINE)

CLIMBING THROUGH APPROX 17,000 FEET, OBSERVED A LEFT ENGINE GENERATOR OFF ALERT, AND A LOUD BANG, FOLLOWED BY A VIOLENT SHAKING OF THE AIRCRAFT. REMOVED AND REPLACED NR 1 ENGINE FORWARD AND AFT MOUNT, APRON, UPPER AND LOWER COWLS, LEFT ELEVATOR AND TABS.

Part: FRAME — DAMAGED (BS 1178)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2987.

Part: FRAME — DAMAGED (BS 1178)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — CRACKED (BS 1178)

FROM N/R N1300620--AFT ACCY. COMPARTMENT FOUND 2 CRACKS IN FRAME ONE CRACK IS 3" LONG AT THE 4 O'CLOCK POSITION SECOND CRACK IS LOCATED 2" ABOVE AND IS 13/4" IN LENGTH STATION 1178 REAR SPAR INSTALLATION CANTED. REMOVED TAIL CONE AND LT PYLON T/E TO ACCESS AREA PER AMM &SRM 53-52-01 AND 51-10-4.REPAIRED LT CANTED FRAME BS 1178 BETWEEN L16 & 17 LT IAW SRM 51-70-11 INSTALLED TAIL CONE & LT PYLON T/E IAW AMM & SRM 53-52-01, 51-10-4 ON W/O 28476-2 NRWC 4661 AND 4660. STRUCTURAL REPAIR REPORT SUBMITTED TO ENGINEERING.

Part: FUSE — BLOWN (POWER SUPPLY)

EMERGENCY LIGHTING INOP AT ROW 11 TO ROW 19 SEATING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY AT POSITION 4 REF B717 MM 33-51. OPS CHECKS GOOD AT THIS TIME.

Part: LONGERON — DENTED (BS 256)

LONGERON 20R AT STA 256 HAS DENT APPROX .25 IN X 1 IN LONG X .061 DEEP DOUBLER WAS APPLIED PER 06-5499. ACCOMPLISHED HFEC TO REPAIRED AREA IAW B717 NDTSPM 06-10-001, NO CRACKS NOTED. INSTALLED U-CHANNEL TO LONGERON 20R IAW B717 SRM 53-00-05.

Part: SKIN — DENTED (BS 218 L18-17L)

DENT AT AFT OF L-1 DOOR. INSTALLED DOUBLER REPAIR AT STA 218 BETWEEN LONGERONS 18L TO 17L IAW 53-00-01 FIG 204.

Part: SKIN — DENTED (FUSELAGE)

SMOOTH DENT FS 237L ON FRAME .25 INCH ABOVE LONG. 18.4 X 1.5 X .067 INCH. D/X= 22.38 WHICH IS CONDITION 2 PER SRM 53-00-01 REPAIR 2 PAGE 210. REPAIRED DENT AT STA 237 BETWEEN L16L - L18L IAW B717 SRM 53-00-01.

Part: HYDRAULIC SYSTEM — LOW (RIGHT)

RIGHT HYD QTY LOW PERFORMED MANUAL GEAR EXTENSION PRIOR TO LANDING. CLEANED W/W & INSPECTED FOR LEAKS. NO LEAKS NOTED REF M/M 32-20. R&R RIGHT AND LEFT NOSE STEERING CYLINDER AND SERVICED RIGHT AND LEFT HYDRAULIC SYSTEM.

Part: BATTERY PACK — DISCHARGED (CABIN)

LOWER EMERGENCY EXIT SIGN AT AFT FLIGHT ATTENDANT STATION DOES NOT ILLUMINATE. OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK ASSY AT FS 879R IAW B717 MM 33-51-03, OPS CHECK NORMAL. RESEATED CANNON PLUG ON B5-125 BATTERY PACK, OPS CHECK GOOD PER B717 AMM 33-51.