N927AT

Part: ENGINE — SURGES (LEFT) · airframe 58,161 hrs · 42,561 cycles

ATB- RETURNED TO MSP DUE TO LEFT ENGINE SURGING. REDUCED THRUST AND SURGING STOPPED. REPLACED LEFT ENGINE. OPS CHECK NORMAL. (8225854).

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 57,837 hrs · 42,267 cycles

ATB TO ATL DUE TO NR 1 ENGINE COMPRESSOR STALL ON CLIMB OUT. BORESCOPED LT ENGINE AND FOUND MULTIPLE BLADES IN HPC DAMAGED. REPLACED ENGINE.(7723471)

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 57,641 hrs · 42,067 cycles

SHIP 9572 EMERGENCY LIGHT EXTERIOR DON'T TURN ON. CORECTIVE ACTION: OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. TEST OK.(6377081)

Part: FUEL CELL — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN AFT FLANGE STA 747 X=-55 TO X=-59. REPAIRED PER PRI 626998-14.

Part: SKIN — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 INITIAL INSPECTION: CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 BTW. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN STA 1076 BTW LONG 13-14 LH WAS REPAIRED PER REPAIR ERA PRI 626436-14AD (1105456)

Part: HINGE — CORRODED (ZONE 500 FLAP) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 AFTER MIDLE FLAP HINGE , CORROSION ON HINGE FITTING HOLES AT LH FLAP. ALSO SCRATCHES HINGE BOLTS (3EA). CORRECTIVE ACTION: HINGE FITTING HOLES AT LH FLAP WERE REPAIRED PER PRI 626829-14 (1101699)

Part: SKIN — CORRODED (ZONE 100) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 IN REF NRC 00308, CORROSION ON CENTER WING UPPER SKIN BTW STA Y= 715/720 X = -60 AT WING BOX. CORRECTIVE ACTION: CORROSION ON CENTER WING UPPER SKIN BTW STA Y= 715/720 X = -60 AT WING BOX WAS REPAIRED PER ERA 626657- 14 AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626657-14 (1100109)

Part: PAN — CRACKED (ZONE 800) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, SEVEN (7 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO DOOR INNER PAN AFT EDGE AT STOPS #1, # 3 & 5. ADDITIONALLY, A GOUGE WAS FOUND BETWEEN STOP FITTINGS #1 AND #2. CORRECTIVE ACTION: TRIMMED OUT THE DAMAGED AREAS, REAMED ELONGATED HOLES, BLENDED OUT THE WORN AREAS, FABRICATED AND INSTALLED REPAIR PARTS PER ER/A 626718-14. (LP 1091605)

Part: PAN — CRACKED (ZONE 800) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO DOOR INNER PAN FWD EDGE AT STOP #2. ADDITIONALLY, AN EXISTING REPAIR WAS FOUND INSTALLED AT THE FWD EDGE BETWEEN STOPS #1 & #2. REMOVED THE EXISTING REPAIRS, TRIMMED OUT THE DAMAGED AREAS, INSPECTED AND FABRICATED REPAIR REINFORCEMENT PARTS AND INSTALLED PER ER/A 626721-14.

Part: PAN — CRACKED (ZONE 800) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC 5231-2005, FIVE (5 QTY) CRACKS WERE FOUND AFFECTING THE FWD CARGO DOOR AT LOWER INNER AND OUTER PAN BETWEEN STA Y=389 AND Y=408 AS FOLLOWS: TWO (2 QTY) CRACKS AT INNER PAN AND THREE (3 QTY) CRACKS AT OUTER PAN. TRIMMED OUT THE CRACKED AREAS AT BOTH PANS, PERFORMED STOP-DRILLS AT CRACK #5 AND FABRICATED AND INSTALLED REPAIR PARTS PER ER/A 1088507. (LP 1088507)

Part: PAN — CRACKED (ZONE 800) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC. 5231-2005, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE FWD CARGO DOOR INNER & OUTER PANS AT THE AFT EDGE BETWEEN STOPS 1 & 2. ADDITIONALLY, AFTER REMOVAL OF THE EXISTING REPAIR AND STOP #1, SIX (6 QTY) HOLES WITH GOUGES WERE FOUND AFFECTING THE AREA OF THE STOP #1 AND STOP #2. CORRECTIVE ACTION: TRIMMED OUT THE CRACKED AREAS, REAMED THE AFFECTED HOLES THROUGH THE INNER PAN AND INTERNAL DOUBLER, ENLARGED THE TRIM OUT, REAMED THE INTERNAL DOUBLER, PERFORMED INSPECTIONS AND FABRICATE/INSTALL REINFORCEMENT PARTS. (LP 1075755)

Part: HINGE FITTING — CORRODED (ZONE 500 FLAP) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 DURING HCK AT QRO, CORROSION WAS NOTED ON THE LH INBD T/R FWD FLAP HINGE FITTING, XW 251. CORRECTIVE ACTION: ER/A REVISION REQUIRED TO INCORPORATE DTE IS REQUIRED WITHIN 24 MONTHS FROM 24JUN2025. IF ER/A REVISION IS NOT ACCOMPLISHED BY 23JUN2027, REMOVE A/C FROM REVENUE SERVICE. (1055210)

Part: NOT REPORTED — NOT REPORTED · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 DTA ER/A 626436-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 30-JUN-25. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. CORRECTIVE ACTION: C/W ER/A 00-626436. (1061415)

Part: SKIN — CORRODED (ZONE 500 LE) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CORROSION ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING. CORRECTIVE ACTION: CORROSION LEVEL 2. AREA ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING WAS REPAIRED PER ERA 626626-14 REV ORIGINAL (1047860)

Part: TAB — DELAMINATED (ZONE 300) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 DELAMINATED CONTROL TAB OF RH ELEVATOR. CORRECTIVE ACTION: CONTROL TAB OF RH ELEVATOR WAS REPAIRED PER PRI 626667-14 REV. 2. AND ER/A 626667-14 REV ORIGINAL. (1044468)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CORROSION OUT LIMITS,IN REF TO NRC 00250 :CORROSION ON TIE TRACKS THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LH STA Y=896- 1022. CORRECTIVE ACTION: DAMAGED AREA WERE AJUSTED AND DRILLED PER DAL DWG S2922357 REV. - AND REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 51-41-05-0G. (1044543)

Part: NONE — NONE (NONE) · airframe 57,611 hrs · 42,037 cycles

DTA ER/A 626583-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. CORRECTIVE ACTION: C.W ERA 626583.

Part: BEAM — CRACKED (ZONE 800) · airframe 57,611 hrs · 42,037 cycles

CRACK BEYONDS STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR. STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR WAS PERFORMED AND NOT ADDITIONAL ACTIONS WERE NECESARY BECAUSE AREA WAS FOUND REPAIRED, AND THE STOP DRILL PERFORMED IS WITHIN REQUIREMENTS OF PREVIOUS REPAIR PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 1028598)

Part: SKIN — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, CRACK ON EXTERNAL FUSELAGE SKIN STA 1037 AND 1152 BTW LONG 13-RH-14RH. CORRECTIVE ACTION: TRIMMED SKIN, DOUBLER TO REMOVE CRACKS, AND PREFORMED HFEC PROCEDURE. FABRICATED SKIN FILLERS, SHIMS, AND DOUBLERS. INSTALLED REPAIR PARTS PER ER/A 626434-14. (LP 1026435)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, CORROSION WAS FOUND OUT LIMITS ON SEAT TRACKS STA Y=906-1015 X=-56 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACKS STA Y=906-1015 X=-56 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1 FIG 201. (LP 1017261)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, CORROSION ON RH OUTB SEAT TRACK (X-56) ON STA Y465 TO STA 484 AT PAX CABIN. WITH AN ORIGINAL THICKNES; ON CROWN= 0.115"; BOTTOM= 0.100"; AND MINIMUM REMAINING THICKNESS ON CROWN= 0.080" BOTTOM= 0.055. CORRECTIVE ACTION: RH OUTB SEAT TRACK (X-56) ON STA Y465 TO STA 484 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP 1014828)

Part: SKIN — CRACKED (ZONE 100) · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A LOWER FUSELAGE INCLUDING RADOME AND LOWER WING FILLETS INSPECTION PER WC 0593-2009, ONE DENT WITH TWO CRACKS WAS FOUND AFFECTING THE FUSELAGE SKIN AT STA 69.55 AND L-20R. CORRECTIVE ACTION: THIS ER/A AUTHORIZES TRIMMING OUT THE DENTED AND CRACKED AREA, PERFORMING INSPECTIONS, AND FABRICATED AND INSTALLED REPAIR PARTS. (LP 1014273)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT (2EA) FROM STA Y=160 TO 200 X=7 AND X= - 7. ALSO, CORROSION ON FLOOR SUPPORT STA Y=145 TO 147 X= -29, STA 148 X= - 32 TO - 44. CORECTIVE ACTION: FLOOR SUPPORT (2EA) FROM STA Y= 160 TO 200 X=7 AND X= - 7, STA 148 X= - 32 TO - 44 WERE REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 51-41-02-0G. FLOOR SUPPORT STA Y=145 TO 147 X= -29 WAS REPLACED. (LP 1002179)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

AIRCRAFT 9572, CORROSION ON RH MID SEAT TRACK (X=-44) ON STA Y= 200-218 AT PAX CABIN WITH AN ORIGINAL THICKNESS ON CROWN=0.115IN BOTTOM= 0.100IN AND MINIMUM REMAINING THICKNESS ON CROWN= 0.079IN BOTTOM= 0.052IN THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-20-52-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR. 4 FIG. 101. CORRECTIVE ACTION: RH MID SEAT TRACK (X=-44) ON STA Y= 200-218 AT PAX CABIN WAS REPAIRED PER B717-200 SRM B717 SRM 53-20-52-2R REPAIR 5. (LP 1001605)

Part: MEMBRANE — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CORROSION OUT OF LIMIT ON MEMBRANE, STA Y 160 TO 197 BTW X=44 TO X= 54; STA Y 200 BTW X= 52 & X=54 AT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-02 (0995815)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 INITIAL INSPECTION: CRACK ON CUSP WEB STA Y=657 X=57 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4 (0995798)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 IN REF NRC 00391 AFTER REMOVAL SEAT TRACK, CORROSION WAS FOUND ON DIAPHRAGM STA Y=200 TO 220 APROX X:-44 AT CABIN PAX. CORRECTIVE ACTION: REPAIRED PER PER B717 -200 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (0993688)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CORROSION OUT LIMITS, IN REF TO NRC 00467: CORROSION ON FLOOR SUPPORT FROM STA 1022 TO Y=1059 X=44, AT AFT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-01-0G. (0990577)

Part: WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y=258 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990756)

Part: WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CRACK ON MEMBRANE STA Y=813 X=45 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990285)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 DUE TO CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200, X=10, WAS MEASURE WITH ORIGINAL THICKNESS: 0.070IN MINIMUM REMAINING THICKNESS 0.042 IN THEREFORE IT IS AREA OUT LIMITS. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-02 (0986603)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CRACK ON MEMBRANE STA Y=715 X=44 AT LH PASSENGER CABIN (CPAX). REPAIRED PER B717-200 SRM 53-00-55-2R-4 (09881240988124)

Part: WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 CRACK ON MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00 -55-2R PROCEDURE 4 REP.4. (0980496)

Part: TORQUE TUBE — CORRODED (ZONE 300) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 ON REF AMDS 2027-2004 CORROSION ON SPLINE AND BORE OF RUDDER DRIVE TORQUE TUBE P/N 5912802-13, ALSO CORROSION ON WASHER LOWER BRG P/N 2913035-1 OF RUDDER CONTROL AFT FUSELAGE // EMPENNAGE. CORRECTIVE ACTION: RUDDER TORQUE TUBE WAS REPLACED BY SERVICEBALE. AND VERIFIED PER B717-200 AIPC 27-21-30-01(0976430)

Part: WEB — CRACKED (ZONE 200) · airframe 57,611 hrs · 42,037 cycles

SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y =692 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55. (0976468)

Part: SPAR — CRACKED (ZONE 500) · airframe 57,611 hrs · 42,037 cycles

-AD- LH WING SPAR CRACK. LEFT WING SPAR REPARED PER ERA 621363-14AD REV ORG. FINAL ERA REV ORG HAS BEEN RECEIVED AND MATCHES PRI REV. 21. ASSOCIATED ER/A 14-621363 ADDED FOR AC 9572. (LP #6377060)

Part: NONE — NONE (NONE) · airframe 57,611 hrs · 42,037 cycles

-AD- PER ERA 621363-14 AD REV 0 STAGE VIII STEP 9, PRIOR TO ACCESS CLOSE-UP, PERFORM A GENERAL VISUAL INSPECTION OF THE AREA FOR CLEANLINESS, AS DEFINED IN TOPP 40-10-10. A) ENSURE ALL TOOLS, RAGS, SHAVINGS, DEBRIS, ETC. HAVE BEEN REMOVED. B) PAY PARTICULAR ATTENTION TO ADJACENT WIRING OR SYSTEMS COMPONENTS. ERA 621363-14AD REV O STAGE VIII STEP 9 WAS PREVIOUSLY COMPLIED WITH ON STEP 7. ASSOCIATED ER/A 14-621363 ADDED FOR AC 9572. RESTORE AND CLOSE FUEL TANKS GVI. (LP #0943791)

Part: SPAR — CRACKED (ZONE 600) · airframe 57,611 hrs · 42,037 cycles

-AD- DUE TO CRACK INDICATION, COMPLY WITH RH WING SPAR REPAIR PER ERA 621441-14AD REV ORIG. SPAR REPAIRED PER PRI 621441-14AD REVS 0 THRU 8. COMPARED PRI 621441-14 REVS 0 THRU 8 WITH ERA 621441-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621441-14 REV ORIG. ALL RII ITEMS C/W. ASSOCIATED ER/A 14-621441 ADDED FOR AC 9572. (LP #0943827)

Part: HINGE FITTING — WORN (ZONE 500 FLAP) · airframe 57,611 hrs · 42,037 cycles

-AD- LH WING, OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. COMPLIED WITH ERA 623200-14AD REV ORG. REPAIRED LH WING OUBOARD FLAP HINGE POINT AC SIDE PER ERA 623200-14AD REV ORIG. REWORKED AND BUSHED LH WING OUTBOARD FLAP HINGE POINT, INBOARD FITTING PER PRI 623200-14AD REV 0. COMPARED PRI 623200-14AD REV 0 AND ERA 623200-14AD REV ORIG AND ALL MATCH. ERA 623200-14AD REV ORIG COMPLIED WITH. ASSOCIATED ER/A 14-623200 ADDED FOR AC 9572. (LP #0943470)

Part: NONE — NONE (NONE) · airframe 57,611 hrs · 42,037 cycles

-AD- PER ERA 621441-14AD REV ORIG STEP 25, PERFORM GVI OF RH WING AREA BEFORE ACCESS CLOSE UP. STEP 25 OF ERA 621441-14AD REV O WAS COMPLIED WITH ON NRC 11 DURING OK TO CLOSE FUEL PANELS. GVI OF RH WING ACCESS AREA WAS COMPLIED WITH ON NON ROUTINE 11, DURING OK TO CLOSE FUEL TANK PANELS. (LP #0943833)

Part: HINGE FITTING — WORN (ZONE 500 FLAP) · airframe 57,608 hrs · 42,036 cycles

LH WING OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. MACHINED IB AND OB LUGS TO REMOVE DAMAGE. OB LUG BORE FINAL SIZE IS .533. IB LUG FINAL SIZE IS .594. INNER FACE OF IB LUG SPOTFACED .880 DIAMETER WITH .060 RADIUS TO A DEPTH OF .076. REMAINING LUG THICKNESS IS .182. FPI INSPECTED AREA PER OHN 27-50-5 PARA 2, J, (2). NO ITEMS NOTED. (LP #0933114)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 57,608 hrs · 42,036 cycles

CRACK IN LH WING REAR SPAR LOWER CAP RADIUS. REFERENCE AA NUMBER FC 5720-01103. CRACK LOCATION IS XRS 156.950. SUMMARY NRC 010-0001:5720-01103-01A/001 00001 COMPLIED WITH PRI 621210-14 REV 0 AND REV 1 AND ENSURED IT MATCHES ERA 621210-14 REV ORIG SECTION 1 STEPS 1-8. COMPLIED WITH ERA 621210-14 REV ORIG SECTION 1 STEPS 9-10. COMPLIED WITH ERA 621210-14 REV ORIG SECTION 2. (LP #0584242)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 56,582 hrs · 41,159 cycles

CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00091: CORROSION LEVEL 2. AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-05-0G, AND 51-41-02-0G. (LP #0287200)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,727 hrs · 38,796 cycles

THE EMERGENCY LIGHTS ON THE GALLEY OVERHEAD, AT SEATS 1-14, AND AT SEATS 24-29 ARE INOPERATIVE. MAINTENANCE FOUND BAD BATTERY PACKS AND BATTERY RACKS AT B5- 259, B5-227, AND B5-120. ALL WERE REPLACED PER AMM 33-51. OPERATIONAL CHECKS WERE GOOD. OK FOR SERVICE.

Part: NONE — NONE · airframe 53,200 hrs · 38,316 cycles

DURING THE SERVICE CHECK, THE OVER WING AFT LOWER EMERGANCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENACE REPLACED THE BATTERY PACK AT LOCATION B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9128858)

Part: NONE — NONE · airframe 53,053 hrs · 38,185 cycles

DOOR 1 RIGHT GIRT BAR SEEMED TO COME LOOSE FROM SLIDE. PIN CAME LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RE-HOOKED THE PIN REF B717 AMM 52-11. VISUAL INSPECTION OK. (LP #9235181)

Part: SIGN — MISSING · airframe 52,411 hrs · 37,595 cycles

THE EMERGENCY EXIT SIGN COVER IS MISSING AT STA 600. MAINTENANCE INSTALLED THE SIGN COVER LENS. (LP #2261915)

Part: FRAME — CORRODED · corrosion level 2 · airframe 52,083 hrs · 37,294 cycles

AFTER CORROSION REMOVAL IN FRAME CLIP STA Y=927 LONGERON 29 LH / 29RH, OT=0.050", RT=0.011" WAS FOUND OUT OF LIMITS PER B717-200 SRM 53-00-00-A01. PAR 4.C. (REF. NRC 00080) . SUMMARY OF NRC 00163: CORROSION LEVEL 2, CLIP STA Y=927 LONGERON 29 LH / 29RH WAS REPLACED PER DWG 9915524 REV. "P" & B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2186835)

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 52,074 hrs · 37,288 cycles

CORROSION ON FRAME CHANNEL STA Y=908 BTW LONGERON 29 LH / 29 RHAT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00079: CORROSION LEVEL 2, FRAME CHANNEL STA Y=908 BTW LONGERON 29 LH / 29 RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. MAINTENACE REQUIREMENTS: PERFORM A VISUAL INSPECTION , INITIAL EVERY 25,000 FLIGHT CYCLES, REPETITIVE 6,500 FLIGHT CYCLES PER B717 SRM 53- 20-07-2R-3 PARAGRAPH 6.A TABLE 205/REPAIR 3. (LP #2186831)

Part: CHANNEL — CRACKED · airframe 52,074 hrs · 37,288 cycles

A CRACK WAS FOUND ON CHANNEL AT STA Y=737 AND X=55 AT RH PASSENGER CABIN. SUMMARY OF NRC 00107: CHANNEL ON STA Y=737 AND X=55 AT RH PASSENGER CABIN WAS REPAIRED PERMANENTLY PER ER/A 598274-14 REV. ORIGINAL SEC.I AND PRI REV. 2. INSPECTION REQUIREMENT WILL BE UNDER LOG PAGE #2187345. ASSOCIATED ER/A 14-598274 ADDED FOR AC 9572. (LP #2187443)

Part: FRAME — CRACKED · airframe 52,074 hrs · 37,288 cycles

CRACK ON FRAME STA=1130 BTW STRINGERS 2 AND 3 RH SIDE AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00115: PERMANENT REPAIR WAS PERFORMD ON FRAME STA=1130 BTW STRINGERS 2 AND 3 RH SIDE AT AFT ACCESSORY COMPARTMENT PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #2185005)

Part: NONE — NONE · airframe 51,613 hrs · 36,903 cycles

CAPT WINDSHIELD SHOWED SPARKS TOP LEFT. MAINTENANCE FOUND CAPT WINDSHIELD TEMP SENSOR WIRES TOUCHING SPRING. ADJUSTED WIRES. CAPTS WINDSHIELD HEAT CHECKS GOOD. A/C OK FOR SERVICE. (LP #8297415)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,909 hrs · 35,443 cycles

THE CABIN CEILING EMERGENCY LIGHT LENS MISSING AT ROW 12. MAINTENANCE INSTALLED LENS COVER. (LP #7578966)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,471 hrs · 35,094 cycles

THE FRONT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. THE LIGHTS DIRECTLY OVER THE EXITS AND THEY WERE FOUND ON THE SERVICE CHECK. MAINTENANCE REPLACED THE BATTERY PACK B5-230, PER B717 AMM 33-51. OPERATIONAL TEST WERE GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 47,568 hrs · 33,448 cycles

THE EMERGENCY EXIT SIGN ABOVE DOOR 1L IS MISSING AND INOPERATIVE. MAINTENANCE INSTALLED A NEW LENS COVER. EMERGENCY LIGHT EXIT SIGN NOW CHECKS GOOD AT DOOR 1L IAW B717 AMM 33-51. (LP #1361214)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,758 hrs · 32,858 cycles

THE EMERGENCY CEILING LIGHTS AT ROW 10 THRU 13 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-227 REF AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6005927)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 46,577 hrs · 32,705 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING AT LOCATION 600. MAINTENANCE REPLACED THE COVER WHICH WAS FOUND ON THE FLOOR. OPERATIONS IS NORMAL AND THE AIRCRAFT IS OKAY TO CONTINUE SERVICE. (LP #1143587)

Part: TIRE — FAILED (MLG) · airframe 45,132 hrs · 31,639 cycles

SHIP 9572 - THE CREW RETURNED THE AIRCRAFT BACK TO DTW DUE TO VIBRATIONS ON ROTATION. TOWER ALSO REPORTED TIRE DEBRIS WAS LEFT ON THE RUNWAY. THE LANDING GEAR RETRACTED NORMALLY AND ALL OTHER INDICATIONS WERE GOOD, BUT AN EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE #3 AND #4 TIRES AND CHANGED THE #3 BRAKE. (LP #4722876)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,013 hrs · 31,559 cycles

MULTIPLE EMERGENCY LIGHTS OUT IN THE CABIN. MAINTENACE REPLACED BATTERY PACKS B5-118 AND B5-119 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4722813)

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 43,496 hrs · 30,514 cycles

CRACKED AND ELONGATED HOLES AT AFT CARGO COMPARTMENT SCUFF PLATE. AFT CARGO COMPARTMENT SCUFF PLATE WAS REPAIRED PER ER/A 542149-14MA REV A.

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION ON FRAME BS 1022, BETWEEN LONGERONS 27L TO 27R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,496 hrs · 30,514 cycles

CRACK ON WEB OF VENT LOUVER STA Y=1200 AND 1:00 POSITION APPROX AT AFT ACCESSORY COMPT. WEB OF VENT LOUVER STA Y=1200 AND 1 HRS POSITION WAS REPAIRED PER SRM 53-00-00-2R FIG 201.

Part: ANGLE — CRACKED (LT WING) · airframe 43,496 hrs · 30,514 cycles

CRACK ON SPLICE AND ANGLE ON INNER SKIN LT WING L/E STA XOS:296. SPLICE AND ANGLE WERE REPLACED ON INNER SKIN LT WING L/E STA XOS:296 PER SRM 51-41-02-0G, 51-41-05-0G, 57-40-01, AND DWG 9919326 REV E.

Part: LONGERON — CRACKED (BS 1134) · airframe 43,496 hrs · 30,514 cycles

CRACKED LONGERON 2R, BS 1134 IN THE AFT ACCESSORY COMPARTMENT AREA. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, FIG 201.

Part: RUB STRIP — DAMAGED (BS 560-917) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION, DISBONDED, AND CRACKED RUB STRIPS AT LH FILLET PANELS FROM BS 560 TO 917. THE RUB STRIPS WERE REPLACED IAW SRM 53-20-70-01, AND SRM 51-20-05.

Part: SKIN — CRACKED (BS 1076) · airframe 43,496 hrs · 30,514 cycles

CRACKED FUSELAGE SKIN BS 1076, BETWEEN LONGERONS 13R - 14R. THE SKIN WAS REPAIRED IAW ER/A 567482-14 ,REV. ORIGINAL AND ETI-17-18-063 REV. 3.

Part: FRAME ANGLE — CRACKED (BS 1023) · airframe 43,496 hrs · 30,514 cycles

CRACKED FRAME ANGLE, BS 1023, LONGERON 7R. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-068, REV 2, AND ER/A 567515-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 43,496 hrs · 30,514 cycles

CRACKED DOOR FRAME WEB BS 207, LONGERON 11L. THE DAMAGED AREA WAS REPAIRED SRM 53-10-15-2R, PROCEDURE 1.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION OUT OF LIMITS IAW NRC 00520. CORROSION ON FUEL ACCESS PANEL 520EB, LT WING. THE FUEL ACCESS PANEL WAS REPLACED IAW AMM 28-00-00 AND JIC CARD 2040-0010 JOB 001-0295.

Part: SLAT TRACK — WORN (LT WING) · airframe 43,496 hrs · 30,514 cycles

WEAR ON THE SLAT TRACK DOOR NR 8 AT THE LT WING. SLAT TRACK DOOR WAS REPLACED IAW ER/A 540095-14MA, REV A, SECTION II.

Part: DOOR — CRACKED (LT WING) · airframe 43,503 hrs · 30,518 cycles

CRACK ON BUTTE DOOR INBOARD TRAILING EDGE LOWER CORNER LT WING. THE BUTTE DOOR WAS REPAIRED IAW SRM 57-00-00-2R, REPAIR 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,496 hrs · 30,514 cycles

DELAMINATED FLOOR PANELS #211ARF, 211AQF, AND 222APF AT COCKPIT/PAX CABIN. NRC 00711: FLOOR PANELS #211ARF, 211AQF, AND 222APF WERE FABRICATED, REPLACED, IDENTIFIED PER B-717 SRM 53-20-50-2R-3. FLOOR PANELS WERE INSTALLED PER JIC NUMBER 2040-0058. (LP #0496238)

Part: SEAL DEPRESSOR — WORN (BS 994) · airframe 43,496 hrs · 30,514 cycles

WEAR ON THE SEAL DEPRESSOR AND DEPRESSOR SPLICE BS 994, BETWEEN LONGERONS 24R - 25R. REPAIRED IAW SRM 53-20-15-2R-4.

Part: STRAP — CRACKED (BS 1178) · airframe 43,496 hrs · 30,514 cycles

CRACKED PYLON TO FUSELAGE STRAP, BS 1178 BETWEEN LONGERONS 16 - 17R. THE STRAP WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-05-0G, AND DWG 5966498, REV T.

Part: RUB STRIP — DAMAGED (BS 560-917) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION AND DISBONDED RUB STRIPS AT RH FILLET PANELS FROM BS 560 TO 917 IAW AMDS 5331-2003. THE RUB STRIPS WERE REPLACED IAW SRM 51-20-70-0I, AND SRM 51-20-05-0G, PAR 7.

Part: BEAM — CRACKED (BS 206) · airframe 43,496 hrs · 30,514 cycles

CRACKED BEAM NR 1 BS 206. THE BEAM WAS REPLACED IAW SRM 51-41-02-0G, 51-41-04-0G, 51-41-05-0G, DWG 9911582 REV T, AND 9911579 REV L.

Part: FITTING — CRACKED (BS 664) · airframe 43,496 hrs · 30,514 cycles

CRACKED RT FITTING BS 664, RBL 19. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G.

Part: FORMER — CRACKED (BS 679-715) · airframe 43,496 hrs · 30,514 cycles

CRACKED FORMER ON STA Y=679,Y=694, AND Y=715 RH SIDE AT CANTED KEEL INTERNAL STRUCTURE. (FUS). NRC 00573: FORMERS WERE REPAIRED PER B717 SRM 51-70-11 REPAIR 1. (LP #0492941)

Part: SEAT TRACK — CORRODED (BS 237-240) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORRODED SEAT TRACK RBL 44, BETWEEN BS 237, AND 240. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-20-52-2R-1, FIG 201, REPAIR 1.

Part: FRAME — CRACKED (BS 1021) · airframe 43,496 hrs · 30,514 cycles

CRACKED FRAME ANGLE BS 1021, LONGERON 16L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9912243, REV JS.

Part: CHANNEL — CRACKED (CABIN) · airframe 43,496 hrs · 30,514 cycles

CRACKED CHANNELS ON FLOOR PANELS #222AF, 223EF, AND 222ZF. (CPAX). NRC 00605: FLOOR PANELS WERE REPAIRED PER B717 SRM 53-20-50-2R-5. HFEC INSPECTION WAS ACCOMPLISHED ON CHANNELS ON FLOOR PANELS #222AF, 223EF, AND 222ZF NO CRACKS WERE FOUND AFTER STOP DRILLS PER DC/MD NDTSPM 06-10-01.001.

Part: FLOORBEAM — CRACKED (BS 120) · airframe 43,496 hrs · 30,514 cycles

CRACKED FLOORBEAM ANGLE BS 120 LBL 50 & RBL 50. REPLACED THE ANGLE IAW SRM 51-41-02-0G, 51-41-05-0G, 51-41-08-0G, AND DWG 9911559, REV A.

Part: STOP FITTING — CRACKED (PAX DOOR FRAME) · airframe 43,496 hrs · 30,514 cycles

CRACK ON STOP FITTING AT THE AFT ENTRY DOOR FRAME, LONGERON 14R. THE STOP FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-02.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 43,496 hrs · 30,514 cycles

CRACKED INTERCOSTAL BETWEEN BS 617 - 636. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R, REPAIR 1.

Part: FORMER — CRACKED (BS 679) · airframe 43,496 hrs · 30,514 cycles

CRACKED FORMER BS 679. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REPAIR 1.

Part: FRAME ANGLE — CRACKED (BS 1021) · airframe 43,496 hrs · 30,514 cycles

CRACK ON THE FRAME ANGLE BS 1021, LONGERON 14L. REPAIRED IAW SRM 53-00-06-2R.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,496 hrs · 30,514 cycles

DELAMINATION ON FLOOR PANELS #221AF, 221BF, 221CF, 221DF, AND 221KF AT PAX CAB (CPAX)(W1). NRC 00611: FLOOR PANELS #221AF, 221BF, 221CF, 221DF, AND 221KF AT PAX CAB WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3. FLOOR PANELS WERE INSTALLED PER CARD-JIC 2040-0024 JOB 001-0061. (LP #0490101)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 43,503 hrs · 30,518 cycles

DENTS ON LOWER SKIN ON THE RT FWD FLAP MOVEABLE VANE. LOWER FLAP VANE SKIN WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4.

Part: ANGLE — CRACKED (BS 737) · airframe 43,496 hrs · 30,514 cycles

CRACKED VERTICAL ANGLE AT BS 737, BELOW THE SEAT TRACK RBL 44. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9923417, REV B.

Part: SUPPORT — CRACKED (BS 737) · airframe 43,496 hrs · 30,514 cycles

CRACKED VERTICAL SUPPORT BS 737 BELOW THE SEAT TRACK LBL 44. THE SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 43,496 hrs · 30,514 cycles

CRACKED FLOOR PANEL 221EF. THE FLOOR PANEL WAS FABRICATED, AND REPLACED IAW SRM 53-20-50-2R-3.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 43,503 hrs · 30,518 cycles

DENT ON UPPER SKIN, 16 INCHES FROM ROOT TO TIP AND 12 INCHES FROM TRAILING EDGE TO LEADING EDGE, ON THE RT AFT FLAP MOVEABLE VANE. THE UPPER SKIN WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4.

Part: CUSP WEB — CRACKED (BS 675) · airframe 43,496 hrs · 30,514 cycles

CRACKED CUSP WEB, BS 675, BETWEEN RBL 44 TO 46. REPAIR IAW SRM 53-00-55-2R-4, FIG 221.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,496 hrs · 30,514 cycles

DELAINATION ON FLOOR PANELS #221VF, 222CF 222DF, 222GF, 222JF, 222QF, AND 222PF AT PAX CAB (CPAX) (FWD PANELS). NRC 00613: FLOOR PANELS #221VF, 222CF, 222DF, 222GF, 222JF, 222QF, AND 222PF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3. FLOOR PANELS WERE INSTALLED WITH CARD 2040-0024 JOB-001-0061. (LP #0489947)

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 43,496 hrs · 30,514 cycles

CRACKED FUEL TANK ACCESS PANEL 520CB ON THE LT WING. THE ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 540-560) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

REPAIR DOUBLER CORRODED ON THE CUSP WEB, BETWEEN BS 540 - 560 LBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.

Part: HINGE — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

RIGHT ELEVATOR HINGE NR 5 AND 6, CORRODED. THE HINGE WAS REPAIRED IAW OHM 27-30-2, AND FOUND WITHIN LIMITS. FABRICATED BUSHINGS.

Part: PAN — CRACKED (BS 954) · airframe 43,496 hrs · 30,514 cycles

CRACKED INNER PAN (SEEN FROM OUTSIDE) BS 954 BTW BEAM 1-2 AT AFT CARGO COMPARTMENT DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R FIG. 204.

Part: ANGLE — CRACKED (BS 408) · airframe 43,496 hrs · 30,514 cycles

CRACKED ANGLE BETWEEN BEAM NR 5 AND UPPER FWD EDGE, BS 408 AT THE FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957664, REV N.

Part: FRAME — CRACKED (BS 1021) · airframe 43,496 hrs · 30,514 cycles

FRAME ANGLE CRACKED, BS 1021, LONGERON 16R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.

Part: INTERCOSTAL — CRACKED (BS 408) · airframe 43,496 hrs · 30,514 cycles

INTERCOSTAL CRACKED BS 408, BETWEEN BEAM NR 5 TO UPPER EDGE AT THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957664, REV N.

Part: CUSP WEB — CRACKED (BS 673) · airframe 43,496 hrs · 30,514 cycles

CRACKED CUSP WEB, BS 673, BETWEEN RBL 54 TO 60. REPAIRED IAW SRM 53-00-55-2R-4.

Part: BEAM — CRACKED (NLG WW) · airframe 43,496 hrs · 30,514 cycles

CRACKED LT DOOR FRAME BEAM AT THE NLG WHEEL WELL. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R, FIG 201.

Part: BEAM — CRACKED (NLG WW) · airframe 43,496 hrs · 30,514 cycles

CRACKED RT DOOR FRAME BEAM, AT THE NLG WHEEL WELL. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R, FIG 201.

Part: FRAME — CRACKED (BS 1021) · airframe 43,496 hrs · 30,514 cycles

FRAME ANGLE CRACKED, BS 1021, LONGERON 14R, THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.

Part: TEE FITTING — CRACKED (BS 389) · airframe 43,496 hrs · 30,514 cycles

CRACKED TEE FITTING, BS 389 LOWER EDGE, AT THE FWD CARGO DOOR. THE TEE FITTING WAS REPLACED IAW SRM 51-41-01-0G, 51-41-05-0G, AND DWG 3926046, REV B.

Part: CUSP WEB — CRACKED (BS 594) · airframe 43,496 hrs · 30,514 cycles

THE RT CUSP WEB WAS CRACKED BS 594, BETWEEN RBL 54 - 56. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 217.

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 43,496 hrs · 30,514 cycles

SEVERAL CRACKS BS 655 - 672, 674, 698, AND 715 ON THE LT CUSP WEB. THE CUSP WEB WAS REPLACED IAW SRM 53-00-55-2R, FIG 203.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 43,496 hrs · 30,514 cycles

CRACKED FLOOR PANEL 221PF. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R-3.

Part: STRAP — CORRODED (BS 168-169) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORRODED STRAP NEXT TO THE DOOR FRAME WEB BETWEEN BS 168 - 169, RBL 56. THE STRAP WAS REPLACED IAW SRM 53-10-15-0I-2, FIG.1, SRM 51-41-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 43,496 hrs · 30,514 cycles

FLOOR PANEL 211ANF DELAMINATED IN THE COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R-3 AND CARD 2040-0024.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 43,496 hrs · 30,514 cycles

CRACKED FLOOR PANEL 211ALF IN THE COCKPIT. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R-3 AND INSTALLED IAW CARD 2040-0024 JOB 001-0061.

Part: CUSP WEB — CORRODED (BS 381) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

RIGHT CUSP WEB CORRODED BS 381, BETWEEN RBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED ON CUT OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 53-00-55-2R FIG. 207.

Part: CUSP WEB — CORRODED (BS 896-898) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 896 - 898, BETWEEN LBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED BETWEEN BS 896 - 898, LBL 56 TO 60, NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL, IAW NDT SPM 06-10-01.001. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.

Part: CUSP WEB — CORRODED (BS 299) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

RIGHT CUSP WEB CORRODED BS 299 BETWEEN RBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED AFTER CUT OUT, AND NO CRACKS WERE FOUND IAW NDT SPM PART 6, 06-10-01.001. REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: INTERCOSTAL — CRACKED (BS 184) · airframe 43,496 hrs · 30,514 cycles

CRACKED INTERCOSTAL BS 184 BTW BEAM 4-5 AT THE L1 DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: CUSP WEB — CRACKED (BS 218-228) · airframe 43,496 hrs · 30,514 cycles

CRACKED RT CUSP WEB, BS 218 - 228, RBL 56 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.

Part: CUSP WEB — CRACKED (BS 718-724) · airframe 43,496 hrs · 30,514 cycles

CRACKED RT CUSP WEB BETWEEN BS 718 - 724, RBL 54 TO 60. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R, FIG 204. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINES, NO CRACKS INDICATIONS WERE FOUND IAW NDT SPM 06-10-01.001.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION ON METALIC STRIP AND WEB OF FWD SERVICE DOOR TRESHOLD.FILLER AND PANEL WERE REPLACED IAW DWG 9957828, REV Y.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 43,496 hrs · 30,514 cycles

CRACK ON INTERNAL ANGLES, FWD & AFT UPPER CORNERS AND FWD LOWER CORNER. AT THE RT AFT EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION ON PLATES OF FWD SERVICE DOOR ENTRY. THE PLATES WERE REPLACED IAW SRM 51-40-08-0G.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 43,496 hrs · 30,514 cycles

CRACK ON INTERNAL ANGLE, AFT UPPER CORNER AT THE LT AFT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.

Part: PAN — CRACKED (BS 579) · airframe 43,496 hrs · 30,514 cycles

CRACK ON RING PAN UPPER CORNER RT FWD FRAME BS 579. REPAIRED IAW SRM 56-20-02-2R1, FIG 202.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 43,496 hrs · 30,514 cycles

CRACKED FLOOR PANEL 223FF IN THE PAX CABIN. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R-3.

Part: PAN — CRACKED (BS 696) · airframe 43,496 hrs · 30,514 cycles

CRACKED RING PAN UPPER CORNER AFT OF FRAME, BS 696. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 203. HFEC INSPECTION WAS ACCOMPLISHED, CRACKS FOUND IAW NDT SPM 06-10-01.001.

Part: PAN — CRACKED (BS 832) · airframe 43,496 hrs · 30,514 cycles

CRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 832. AREA WAS REPAIRED IAW SRM 56-20-02-2R1 FIG 202.

Part: PAN — CRACKED (BS 370) · airframe 43,496 hrs · 30,514 cycles

CRACKED OUTER PAN BS 370 BETWEEN BEAMS 2 - 1. REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 43,496 hrs · 30,514 cycles

DELAMINATION ON FLOOR PANEL 222AMF IN THE PAX CABIN. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50, 2R-3.

Part: PAN — CRACKED (BS 427) · airframe 43,496 hrs · 30,514 cycles

CRACKED OUTER PAN BS 427 BETWEEN BEAMS 2 - 1, REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.

Part: PAN — CRACKED (BS 655) · airframe 43,496 hrs · 30,514 cycles

CRACKED RING PAN CORNER AFT FRAME, BS 655. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION ACCOMPLISHED, NO CRACKS FOUND IAW NDT SPM 06-10-01.001.

Part: PAN — CRACKED (BS 794) · airframe 43,496 hrs · 30,514 cycles

CRACK ON RING PAN LOWER CORNER AFT FRAME BS 794. AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202.

Part: ANGLE — CORRODED (BS 180 FLOORBEAM) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORRODED FLOORBEAM BS 180, RBL 10 TO 43. THE FLOOR BEAM WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: PAN — CRACKED (BS 889) · airframe 43,496 hrs · 30,514 cycles

CRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 889. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW SPM 06-10-01.001.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORRODED FLOOR SUPPORT IN LBL 7 BETWEEN BS 148 - 200. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-01-0G.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,496 hrs · 30,514 cycles

NR 1 BEAM CRACKED, L1 DOOR. REPAIRED IAW SRM 52-10-02-2R-7, FIGURES 201 & 202.

Part: CUSP WEB — CRACKED (BS 699) · airframe 43,496 hrs · 30,514 cycles

CRACKED RT CUSP WEB BS 699, BETWEEN RBL 54 TO 60. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R, FIG. 204.

Part: SKIN — SCRATCHED (BS 446-465) · airframe 43,496 hrs · 30,514 cycles

SCRATCHES ON TOPSIDE SKIN BETWEEN BS 446 AND 465, LONGERONS 3L TO 3R. THE SCRATCHES WERE BLEND OUT IAW SRM 53-02-01-2R, PAR 5.A. HFEC WAS ACCOMPLISHED, NO CRACKS FOUND AFTER BLEND OUT IAW SRM 53-02-01-2R PAR. 5.A.(1)(A)2, & NDT SPM 06-10-01.001 WAS ACCOMPLISHED SPM N.D.T. 04-00-07 PAR.5 FIG. 3 SHEET 1 AND 2 FOUND TO BE WITHIN LIMITS IAW SRM 53-01-01-1A CONDITION 1. AREAS WERE TREATED AND PAINTED IAW SRM 51-10-04 PAR 21, AND 15.

Part: SKIN — CRACKED (BS 994) · airframe 43,496 hrs · 30,514 cycles

EXTERNAL REPAIR DOUBLER WAS FOUND CRACKED BS 994 BETWEEN LONGERONS 24R - 26R. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-12, FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORRODED FLOOR SUPPORT BS 200 BETWEEN RBL 10 TO 52. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION ON THE FLOOR SUPPORT, RBL 44 - 54, BS 160 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: FLOOR SUPPORT — CORRODED (BS 200) · corrosion level 2 · airframe 43,496 hrs · 30,514 cycles

CORROSION ON THE FLOOR SUPPORT, BS 200 BETWEEN LBL 14 TO RBL 5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.

Part: PLATE — CRACKED (BS 1053) · airframe 43,496 hrs · 30,514 cycles

CRACKED PLATE BS 1053, LBL 58. THE PLATE WAS REPLACED IAW SRM 51-41-05-0G, AND DWG 9910154, REV AM.

Part: SLIDE — OUT OF TOLERANCE (R1 DOOR) · airframe 42,997 hrs · 30,196 cycles

ON SERVICE CHECK FOUND R1 SLIDE IN NO GO RANGE. REPLACED SERVICE DOOR SLIDE IAW T/C 2561-9005. INSTALLED A NEW R1 DOOR SLIDE. OPS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,130 hrs · 29,619 cycles

FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN STA 232 AND L-16L TO L-18L. REPAIRED FUSELAGE SKIN STA 229 TO 262 BETWEEN LONGERON 18LT TO 15LT IAW SRM 53-00-01 REPAIR 6. THIS IS A PERMANENT REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 42,130 hrs · 29,619 cycles

FRAME FORMER AT STA 237 L-17L HAS DENT DAMAGE. REPAIRED FRAME FORMER AT STA 237 BETWEEN LONGERON 17LT TO 16LT IAW SRM 53-00-06 REPAIR 2, 53-20-06 REPAIR 2, AND DRAWING 9911523 REV E. THIS IS A PERMANENT REPAIR WITH NO SPECIAL FOLLOW UP INSPECTIONS.

Part: LONGERON — DENTED (FUSELAGE) · airframe 42,130 hrs · 29,619 cycles

L-17L HAS DENT DAMAGE AT STA 237. REPAIRED LONGERON 17LT BETWEEN STA 229 TO 245 IAW SRM 53-00-05 REPAIR 2. THIS IS A PERMANENT REPAIR WITH NO SPECIAL FOLLOW UP INSPECTIONS.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,786 hrs · 29,358 cycles

OVERWING EMERGENCY EVACUATION LIGHTS ARE INOPERATIVE. R&R OVERWING EMERGENCY EVAC BATTERY POWER SUPPLY PER MM 33-51. OPS CHK GOOD. OK FOR SVC.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,954 hrs · 28,728 cycles

DENT DAMAGE TO FUSELAGE PANEL 150GL. FOUND DENT DAMAGE TO BE 6.00" LENGTH BY 1.750" WIDTH BY .062" DEEP. REPAIRED IAW ER/A 553960-14 REV ORIGINAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,182 hrs · 28,222 cycles

DURING THE TURN AROUND CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT STA 706 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY FOR THE NOTED LIGHTED AREA AND THE OPERATIONAL CHECK WAS GOOD.

Part: ENGINE — MAKING METAL (NR 1) · airframe 40,164 hrs · 28,211 cycles

THE FLIGHT CREW DIVERTED THE AIRCRAFT TO JFK AFTER THE NR 1 ENGINE EXPERIENCED A STALL DURING INITIAL CLIMBOUT AND WAS SHUTDOWN. MAINTENANCE FOUND METAL IN THE TAILPIPE AND HAS REPLACED THE ENGINE.

Part: WIRE — SHORTED (CABIN) · airframe 40,129 hrs · 28,184 cycles

THE FLIGHT CREW FOUND ALL OF THE EEPL CIRCUIT BREAKERS WERE TRIPPED AND WOULD NOT RESET. THIS PREVENTED THEIR CONTROL THE EMERGENCY PATHWAY LIGHTING IN THE CABIN. MAINTENANCE REPLACED ONE BATTERY PACK DUE TO BEING WARM TO THE TOUCH, ANOTHER BATTERY PACK DUE TO DISCOLORATION OF THE CIRCUIT BOARD, AND REPAIRED A WIRE WHICH WAS SHORTED TO GROUND. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,647 hrs · 27,028 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY LIGHTING WOULD NOT TURN OFF. LIGHTS WOULD REMAIN ON AFTER POWER WAS REMOVED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,647 hrs · 27,028 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EMERGENCY LIGHTING IN THE CABIN FROM THE F/A PANEL. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS, LOCATED IN THE AFT CARGO, AND THE OPS CHECK WAS GOOD.

Part: DOOR FRAME — CORRODED (BS 954-994) · corrosion level 2 · airframe 38,630 hrs · 27,015 cycles

AFT CARGO COMPT DOOR LOWER JAMB UNDER SCUFF PLATE CORRODED BS 954-994. REPAIRED IAW SRM 53-20-15, REPAIR 7.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,475 hrs · 25,262 cycles

DURING SERVICE CHECK, LT AND RT FORWARD OVERWING INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND TESTED IAW AMM 33-51.

Part: DOUBLER — CRACKED (NOT REPORTED) · airframe 43,496 hrs · 30,514 cycles

EXTERNAL REPAIR DOUBLER WAS FOUND CRACKED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-12, FIG 201.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,364 hrs · 22,733 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BATTERY IAW MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

AFT CABIN EMERGENCY DOOR FLOORBOARD FRAME CORRODED BETWEEN BS 1022 TO BS 1053, RBL 20. REPAIRED FRAME IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

RT WW FWD DOOR CUT OUT INBD FITTING CRACKED AT BS 737, RBL 10. R & R FITTING IAW SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 33,364 hrs · 22,733 cycles

LT WW FWD VERTICAL DOOR CUT OUT ANGLE CRACKED AT BS 756, LBL 57. REPAIRED ANGLE IAW SRM.

Part: FITTING — CRACKED (LT MLG WW) · airframe 33,364 hrs · 22,733 cycles

LT MLG WW FWD CUT OUT CLIP CRACKED AT STATION 737, LBL 40. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

RT LOUVER UPPER AFT AT EXISTENT REPAIR DOUBLER ON WEB CRACKED. R & R WEB PANEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

LT LOUVER AT CANT FRAME 1178 ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222ADF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222LF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: PANEL — DELAMINATED (LT SPOILER) · airframe 33,364 hrs · 22,733 cycles

LEFT WING OTBD SPOILER PANEL DELAMINATED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 221WF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

LT WING TO BODY ANGLE CRACKED AT BS 806, LONGERON 22L. R & R ANGLE IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222YF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222ATF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,364 hrs · 22,733 cycles

MAIN CABIN FLOOR PANEL 222AVF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: BRACKET — CRACKED (SLAT TRACK) · airframe 33,364 hrs · 22,733 cycles

RT WING FIXED LE AT SLAT TRACK NR 8 INBD SIDE SPRING DOOR GUARD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 33,364 hrs · 22,733 cycles

LT WING TE LOWER SIDE PANEL CRACKED AROUND FWD SIDE OF INBD BUTE DOOR. R & R PANEL IAW SRM & DRAWING.

Part: SUPPORT FITTING — CRACKED (RT MLG WW) · airframe 33,364 hrs · 22,733 cycles

RT WW FWD DOOR CUTOUT HYD LINE FOR GND CONNECTOR SUPPORT CLIP CRACKED. R & R CLIP IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,364 hrs · 22,733 cycles

RT WING TO BODY ANGLE BRACKET CRACKED AT BS 806, LONGERON 2R. R & R BRACKET IAW SRM & DRAWING.

Part: PANEL — CRACKED (LT WING) · airframe 33,364 hrs · 22,733 cycles

LT WING LOWER PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: LENS — MISSING (CABIN) · airframe 33,958 hrs · 23,103 cycles

RT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 12. RELAMPED LENS IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,751 hrs · 21,707 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER AMM.

Part: LIGHT — MISSING (CABIN) · airframe 31,584 hrs · 21,611 cycles

RIGHT EMERGENCY PATH LIGHT MISSING AT ROW 3. INSTALLED LAMPS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 3,069 hrs · 20,634 cycles

EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 3,069 hrs · 20,634 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED AT BS 474, RBL 57. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED BETWEEN BS 541 TO BS 560, RBL 57. REMOVED AND REPLACED WEB IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

FORWARD CARGO DOOR CUTOUT CORRODED BETWEEN BS 372 TO BS 410. REMOVED AND REPLACED CUTOUT IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED AT BS 633, RBL 54.5. REMOVED AND REPLACED WEB IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

STRINGER CORRODED AT BS 827, STR 27R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED BETWEEN BS 560 TO BS 541, LBL 57. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED BETWEEN BS 446 TO BS 465, RBL 57. REMOVED AND REPLACED WEB IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

AFT CARGO DOOR CUTOUT CORRODED BETWEEN BS 952 TO BS 990. REPAIRED CUTOUT IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

STRINGER CORRODED BETWEEN BS 946 TO BS 986, STR 29R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED BETWEEN BS 484 TO BS 503, RBL 57. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

CUSP WEB CORRODED AT BS 655, RBL 54.5. REMOVED AND REPLACED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,069 hrs · 20,634 cycles

SHEAR TIE CORRODED AT BS 1022, BETWEEN STR 20L TO STR 29L. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 29,049 hrs · 19,955 cycles

R1 DOOR EVAC SLIDE RELEASE LATCH UNSECURED. SECURED R1 DOOR SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN)

EPL CLEAR LENS MISSING AT ROW 18. INSTALLED LENS AS REQUIRED.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

INFLATION CABLE PINS FOUND LAYING ON THE FLOOR FOR R1 DOOR. REMOVED AND REPLACED FORWARD SERVICE DOOR ESCAPE SLIDE IAW B717 25-61-03, OK FOR SERVICE.

Part: RETAINER — CORRODED (FUSELAGE)

GALLEY ENTRANCE BOTTOM EDGE SEAL RETAINER, CORROSION. ACCOMPLISHED BOTTOM EDGE SEAL RETAINER REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 8 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 144 TO 152, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 200, RBL 44 TO RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: SKIN — CRACKED (FUSELAGE)

PASSENGER ENTRANCE AREA AREA FUSELAGE SKIN, STA 208, LONG L15L, CRACKED. ACCOMPLISHED AREA FUSELAGE SKIN DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 156, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: COVER — MISSING (CABIN)

ROW 10 MISSING EPL COVER (CLEAR). REPLACED COVER IAW AMM 33-51.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: PAN — DAMAGED (CARGO DOOR)

AFT CARGO DOOR LOWER PAN REPAIR. ACCOMPLISHED REPAIR.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ROW 1-10 INOPERATIVE. REMOVED AND REPLACED EMERG LIGHT BATT PWR SUPPLY PER AMM 33-51-03 OPS CHECK GOOD.

Part: SEAL — LEAKING (FUEL FILTER BOWL)

TOWER ADVISED FLUID COMING OUT OF LT ENGINE DURING CLIMBOUT. TOP OF CLIMB, BALANCED FUEL TANKS, IN 15 MINUTES, LEFT TANK WAS 800 POUNDS LOW. OPENED NR 1 ENGINE COWL AND FOUND FUEL FILTER BOWL SEAL LEAKING. REMOVED AND REPLACED FUEL FILTER AND SEAL IAW B717 AMM 73-11-01. LEAK CHECK GOOD IAW B717 71-00-11.