N955AT

Part: BEAM — CRACKED (ZONE 100) · airframe 63,743 hrs · 45,686 cycles

CRACK WAS FOUND ON INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR. SUMMARY OF NRC 00578: INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR WAS REPAIRED PER PRI 624376-14 REV 2 AND ERA 624376-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624376 ADDED FOR AC 9514. (LP #0865402)

Part: PAN — CRACKED (ZONE 800) · airframe 63,743 hrs · 45,686 cycles

CRACK ON PAN NEXT TO AFT HINGE DOOR (UPPER AREA) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: PAN NEXT TO AFT HINGE DOOR (UPPER AREA) OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0866764)

Part: PAN — CRACKED (ZONE 100) · airframe 63,743 hrs · 45,686 cycles

CRACK ON OUTER PAN BTW BEAM 1 AND 2 (AFT EDGE) OF FWD CARGO DOOR WAS FOUND. SUMMARY OF NRC 00552: OUTER PAN AND INNER PAN BTW BEAM #1 AND BEAM #2 (AFT EDGE) AT FWD CARGO DOOR WERE REPAIRED PER ER/A 624433-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624433-14 REV 2. ASSOCIATED ER/A 14-624433 ADDED FOR AC 9514. (LP #0866701)

Part: PAN — CRACKED (ZONE 100) · airframe 63,743 hrs · 45,686 cycles

CRACK WAS FOUND ON INNER PAN AT AFT CARGO DOOR AT STOP FITTING ON BEAM 5 AFT EDGE. SUMMARY OF NRC 00577: INNER PAN ON BEAM 5 AFT EDGE OF AFT CARGO DOOR WAS REPAIRED PER ER/A 566665-14 REV A SECTION II: PERMANENT REPAIR AND PRI 566665-14 REV 4. ASSOCIATED ER/A 14-566665 ADDED FOR AC 9514. (LP #0866700)

Part: PAN — CRACKED (ZONE 800) · airframe 63,743 hrs · 45,686 cycles

CRACKS (2 EA) WERE FOUND ON INNER PAN AT AFT CARGO DOOR STOP FITTING ON BEAM 1 STA Y=990. SUMMARY OF NRC 00589: INNER PAN ON AFT SIDE BETWEEN STOP #1 AND STOP #2 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 624383-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624383-14 REV 3. (LP #0860120)

Part: PAN — CRACKED (ZONE 200) · airframe 63,743 hrs · 45,686 cycles

CRACKS (2 EA) ON OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES. SUMMARY OF NRC 00111: DAMAGED AREA OF OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #0857625)

Part: BEAM — CRACKED (ZONE 100) · airframe 63,743 hrs · 45,686 cycles

CRACK WAS FOUND ON BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 00574: BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. WERE REPAIRED PER PRI 624316-14 REV 3 AND ERA 624316-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624316 ADDED FOR AC 9514. (LP #0851459)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00183: CORROSION LEVEL 2. INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 624284-14 REV 2 AND ER/A 624284-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624284 ADDED FOR AC 9514. (LP #0851040)

Part: HINGE FITTING — CORRODED (ZONE 500 FLAP) · airframe 63,743 hrs · 45,686 cycles

AN ELONGATED HOLE INBD ON INBD FACE ON HINGE FLAP #3 AT LH WING, ALONG WITH CORROSION ON BOTH HOLES INBD/OUTBD HINGE. SUMMARY OF NRC 00543: HINGE FLAP #3 AT LH WING WAS REPAIRED PER PRI 624271-14 REV 1 AND ER/A 624271-14 REV ORIGINAL. ASSOCIATED ER/A 14-624271 ADDED FOR AC 9514. (LP #0840661)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00177: CORROSION LEVEL 2. FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. PERFORM A DETAIL VISUAL INSPECTION 25,000 CYCLES AFTER REPAIR INSTALLATION AND REPEAT EVERY 6,500 CYCLES PER B717 SRM 53-20-07-2R-3 REPAIR 3 PARAGRAPH 6 A. TABLE 205. (LP #0840417)

Part: HINGE FITTING — DAMAGED (ZONE 600 FLAP) · airframe 63,743 hrs · 45,686 cycles

AN ELONGATED HOLE WAS FOUND AT THE RH WING FLAP HINGE FITTING #3 PIVOT POINT. SUMMARY OF NRC 00535: RH WING FLAP HINGE FITTING #3 WAS REPAIR PER PRI 624272-14 REV 1 AND ER/A 624272-14 REV ORIGINAL. ASSOCIATED ER/A 14-624272 ADDED FOR AC 9514. (LP #0840814)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

FRAME CLIP STA 1022 BTW LONG 28RH TO 28LH, AFT CARGO COMPARTMENT, WAS FOUND CORRODED OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS 0.048 IN PER B717-200 SRM 53-00-01-1A ALLOWABLE DAMAGE PAR 4.C.(2) FIG 103. SUMMARY OF NRC 00633: CORROSION LEVEL 2. FRAME CLIP STA 1022 BTW LONG 28RH TO 28LH WAS REPAIRED PER B717-200 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND 53-20-06-2R PROCEDURE 2 REPAIR 2. (LP #0839252)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON ANGLE CUSP BTW STA Y=197 TO STA Y=210 OF FWD GALLAY SERVICE DOOR AT CABIN PASSENGER. SUMMARY OF NRC 00283: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=197 TO STA Y=210 OF FWD GALLEY SERVICE DOOR AT CABIN PASSENGER WAS REPAIRED PER PRI 624120-14 REV 4 AND ER/A 624120-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624120 ADDED FOR AC 9514. (LP #0833566)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 63,743 hrs · 45,686 cycles

CRACK ON CUSP WEB (BELOW AREA) IN X=-54 AND STA 257, STA 277, STA 656, STA 674, STA 818, AND STA 937 AT CPAX. SUMMARY OF NRC 00336: CUSP WEB AT STA 277, STA 257, STA 818, STA 937 WERE REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4, CUSP WEB BTW STA 655 TO STA 715 WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP MANUAL 30-10-70 PAR I PG 14. LOG PAGE DEFERRED TO DECAL CONDITION MONITOR PER TOPP 30-10-70 TO BE INSPECTED AT THE APPROPRIATE CHECK INTERVAL. (LP #0832577)

Part: SKIN — DAMAGED (ZONE 300) · airframe 63,743 hrs · 45,686 cycles

LH ELEVATOR WAS FOUND DENTED AND SCRATCHED ON UPPER SKIN. SUMMARY OF NRC 00575: LH ELEVATOR WAS REPAIRED PER B717-200 SRM 51-70-13-2R REPAIR 2. PERFORM DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR I PAGE 14. LOG PAGE DEFERRED TO DECAL CONDITION MONITOR PER TOPP 30-10-70 TO BE INSPECTED AT THE APPROPRIATE CHECK INTERVAL. (LP #0829203)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON ANGLE CUSP BTW STA Y=190 TO STA Y=200 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00270: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=190 TO STA Y=200 OF FWD ENTRY DOOR AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 REPAIR 3. (LP #0828450)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 63,743 hrs · 45,686 cycles

CRACK ON CUSP WEBS (LOWER AND UPPER AREA) IN X=54 AND STA 225, STA 237, STA 258, STA 655, AND STA 663. ALSO, X=58 AND STA 668, STA 807 AT CPAX WAS CRACKED. SUMMARY OF NRC 00442: CUSP WEBS IN X=54 AND STA 225, STA 237, STA 258, STA 655, STA 663, ALSO X=58 AND STA 668 WERE REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 AND STA 807 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-01-2R. CUSP WEB IN X=54 AND STA 225 WAS ATTENDED UNDER NRC 00280 AND LP 0820562. (LP #0828892)

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00062: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 53-20-15 -2R-7. (LP #0822834)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION OUT OF LIMITS FOUND AT WEB STA 200 TO STA 216 X=25 TO X=54. SUMMARY OF NRC 00492: CORROSION LEVEL 2. WEB STA 200 TO STA 216 X=25 TO X=54 WAS FABRICATED PER DWG 9910078 REV JC. AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-08-0G. (LP #0821476)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=194 TO STA Y=200 X=56 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00276: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=194 TO STA Y=200 X=56 OF FWD ENTRY DOOR AT PASSENGER CABIN WAS MANUFACTURATED PER DWG 9910078-173 AND WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-08-0G. (LP #0822729)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON CUSP WEB, REWORKED AREAS AT X=58 STA 866 AND STA 840-847 WAS FOUND OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS OF 0.010IN PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4.C. FIG 101. SUMMARY OF NRC 00531: CORROSION LEVEL 2. CUSP WEB AT STA 832 TO STA 851 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 209, AND CUSP WEB AT X=58 STA 866 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 212. (LP #0819939)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON WEB BTW STA Y=225 TO STA Y=228 X=56 AT FWD CABIN PASSENGER. SUMMARY OF NRC 00280: CORROSION LEVEL 2. CUSP WEB STA 216 TO 237 X=45 TO X=57 WAS FABRICATED PER DWG 993053 REV CF. AND WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0820562)

Part: PAN — CRACKED (ZONE 800) · airframe 63,743 hrs · 45,686 cycles

CRACK WAS FOUND ON AFT SIDE ON BEAM 4 OUTER PAN AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00508: AFT SIDE ON BEAM 4 OUTER PAN AT FWD COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0819812)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION OUT OF LIMITS IN REF NRC 188: CORROSION ON SIDE TRACK (RH) BWT STA 644 TO 648 SEAT TRACK FLANGE: WITH ORIGINAL THICKNESS =0.060" AND MINIMUM REMAINING THICKNESS IS 0.025". THEREFORE, IT IS OUT LIMITS PER B717-200 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 PAR 4 FIGURE 101 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00491: CORROSION LEVEL 2. SIDE TRACK (RH) BWT STA 598 TO 655 WAS FABRICATED PER DWG 5965421 REV E AND REPLACED PER B717 SRM 51-41-05-0G AND 51-41-01-0G. (LP #0816574)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 63,743 hrs · 45,686 cycles

CRACK ON CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 AT PAX CABIN. SUMMARY OF NRC 00495: CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 WERE REPAIRED PER B717-200 SRM 53-00-55-2R FIG 226 REP 4, AND DWG 9930538 REV K, AND RING DOUBLERS (3 EA) ON CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 WERE INSTALLED PER B717-200 SRM 53-00-55-2R FIG 226, REP 4. (LP #0809365)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00271: CORROSION LEVEL 2. CORRODED FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT CABIN (W2) WERE REPLACED PER B717-200 SRM 51-41-05-0G AND DWG: 9981474 REV: K. (LP #0808785)

Part: FRAME — CRACKED (ZONE 100) · airframe 63,743 hrs · 45,686 cycles

CRACK ON FRAME STA Y=1037, L-17L AND L-17R AT CPAX. SUMMARY OF NRC 00379: FRAME STA Y=1037, L-17L AND L-17R AT CPAX WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0808878)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,743 hrs · 45,686 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00275: CORROSION LEVEL 2. CORRODED FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT CABIN (W2) WAS REPLACED PER DWG 9981474-15 REV L AND PER B717-200 SRM 51-41-05-0G. (LP #0808643)

Part: PAN — CRACKED (ZONE 800) · airframe 63,743 hrs · 45,686 cycles

CRACK WAS FOUND ON INNER PAN OF THE AFT EDGE AT FWD CARGO DOOR. SUMMARY OF NRC-00306: AFT EDGE AT FWD CARGO DOOR CRACK ON INNER PAN WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0800119)

Part: DRAIN — CRACKED (LT WINDOW) · airframe 61,749 hrs · 44,027 cycles

CRACK ON DRAIN OF LH CLEAR VIEW WINDOW AT COCKPIT. SUMMARY OF NRC 00080: LH CLEAR VIEW WINDOW RETAINER AT COCKPIT WAS REPAIRED PER ERA 616781-14 REV ORIGINAL. ASSOCIATED ER/A 14-616781 ADDED FOR AC 9514. (LP #0264952)

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 61,636 hrs · 43,929 cycles

RMLG FIXED STRUT OB ATTACH POINT BORE BUSHING CORRODED. REPLACED BUSHING PER BOEING DWG 5924841 ON NRC 008. (LP #0033263)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LWR FRAME SECTION STA 120 DAMAGED DURING LANDING. C/W PRI 610432-14 REV 0. C/W PRI 610432-14 REV 1. C/W PRI 610432-14 REV 2. C/W PRI 610432-14 REV 3. C/W PRI 610432-14 REV 4. C/W PRI 610432-14 REV 5. C/W ERA 610432-14 REV B PRIS 0-5 MATCH FINAL ERA. (LP #2968352)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LHS NLG SUPPORT BEAM DAMAGED ON LANDING. REMOVED DAMAGED NLG SUPPORT BEAM PER BOEING DWG 9910088. REPLACED NLG SUPPORT BEAM PER BOEING DWG 9910088. (LP #2963209)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LOWER SKIN PANEL ASSY 5911401-537 DAMAGED DRUING LANDING. REMOVED -537 SKIN ASSY PER DWG 5911401. LOCATED AND DRILLED NEW SKIN ASSY PER DWG 5911401. APPLIED TOP COAT TO ASSEMBLY PARTS PER B717 SRM 51-22-01. INSTALLED DOUBLERS TO SKIN PER DWG 5911401. PRIMED EXTERIOR SURFACE OF SKIN PER B717 SRM 51-22-01. INSTALLED SKIN ASSY PER DWG 5911401. (LP #2946623)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LOWER FRAME SECTION AT STA 160 DAMAGED DURING LANDING. (REF PAPER NR 012) REMOVED LOWER FRAME SECTION STA 160 PER B717 SRM 51-40-02. C/W REV 0 OF PRI 610940-14. C/W REV 1 OF PRI 610940-14. C/W PRI 610940-14 REV 2. C/W ERA 610940-14 REV ORIG. PRIS 0-2 MATCH FINAL ERA. REPLACED LOWER FRAME SECTION STA 160 REF ERA 610940-14 AND DWG 9911515. (LP #2940983)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

C/W ERA 610811-14 INTERNAL DOUBLER FABRICATION DAMAGED DURING LANDING. C/W PRI 610811-14 REV 0. C/W ERA 610811-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #2934596)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LH NLG SKIN PANEL 5911400-99 DAMAGED DURING LANDING. REF NR 066: C/W PRI 610190-14 REV 0. C/W PRI 610190-14 REV 1. C/W PRI 610190-14 REV 2. C/W PRI 610190-14 REV 3. C/W ERA 610190-14 REV ORIG. PRI REVS 0-3 MATCH FINAL ERA. (LP #2920961)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

SEVEN LONGERONS STA 110-120 STR 28L-28R WERE DAMAGED DURING LANDING. (REF BUFF NR 010) LOCATED AND DRILLED LONGERON SECTIONS PER B717 DWG 5911401. INSTALLED 7 EA LONGERON SECTIONS STA 110-120 STR 28L-28R PER B717 SRM 51-40-02 AND DWG 591140. (LP #2919459)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

STA 110 BULKHEAD AND LWR CHORD DAMAGED DURING LANDING. REMAINING SECTIONS OD ST110 CHORD REMOVED. REMOVED DAMAGE SECTION OF BULKHEAD PER B717 SRM 53-10-08-2R REPAIR 1. FABRICATED -3 THROUGH -23 REPAIR PARTS PER B717 SRM 53-10-08-2R REPAIR 1 AND ERA 610394-14 REV O. PERFORMED HFEC INSPECTION OF TRIMMED EDGES PER B717 SRM 53-10-08-2R REPAIR 1. NO CRACKS INDICATED. FPI OR REPAIR PARTS ACCOMPLISHED ON SONTS 4021. TREATED, PRIMED, AND PAINTED REPAIR PARTS PER B717 SRM 53-10-08- 2R REPAIR 1. FABRICATED -1 AND - 2 REPAIR DOUBLERS AND TAPERED FILLERS PER B717 SRM 53-10-08-2R REPAIR 1. PERFORMED FPI ON PARTS -1 AND -1 2 REPAIR DOUBLERS AND TAPERED FILLER PER B717 SRM 53-10-08-2R REPAIR 1 AND NDTSPM PART 8. NO DEFECTS NOTED. PRIMED -1 AND -2 REPAIR PARTS PER B717 SRM 53-10-08-2R REPAIR 1. INSTALLED REPAIR PARTS PER B717 SRM 53-10-08-2R REPAIR 1 AND ERA 610394-14 REV 0. C/W PRI 610394-14 REV 0. C/W ERA 610394-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #2919661)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

-39 AND -22 CHORDS AT STA 110 BULKHEAD DAMAGED DURING LANDING. REMOVED DAMAGED PORTION OF -39 AND -22 CHORDS PER B717 SRM 51-70 -11-2R-2. FABRICATED NEW -22 SECTION AND REPAIR ANGLES PER B717 SRM 51-70-11-2R-2 AND PRI 610765-14 REV 0. TREATED AND PAINTED PER B717 SRM 51- 70-11-2R-2 AND PRI 610765-14. INSTALLED REPAIR PARTS. COMPLETED REPAIR OF -22 CHRD REF B717 SRM 51-70-11-2R-2 AN PRI 610765-14 REV 0. FABRICATED -39 REPAIR PARTS REF B717 SRM 51-70-11-2R-2 AND PRI 610765-14 REV 0. TREATED AND PAINTED REF B717 SRM 51-70-11-2R-2. INSTALLED AND COMPLETED REPAIR ON -39 CHORD REF B717 SRM 51-70-11-2R-2 AND PRI 610765-14 REV 0. C/W PRI 610765-14 REV 0. C/W ERA 610765-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #2919806)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

E&E DOOR SURROUND JAMB PAN AND SUPPORT FRAMES DAMAGED DURING LANDING. REMOVED E&E DOOR SURROUND JAMB PAN PER B717 SRM 51-40-02. INSTALLED E&E JAMB PAN AND SUPPORT FRAMES PER B717 SRM 51-40-02 AND DWG 9911550. (LP #2919766)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LONGERON AT STA 160-STA 180 STR 30 DAMAGED DURING LANDING. REMOVED LONGERON AT STA 160 - STA 180 STR 30 PER B717 SRM 51-40- 02. REPLACED LONGERON AFT STA 160- STA 180 STR 30 PER B717 SRM 51-40-02 AND DWG 5911401. (LP #2919466)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

RHS NLG SUPPORT BEAM WAS DAMAGED ON LANDING. C/W PRI 610297-14 REV 0. C/W PRI 610297-14 REV 1. C/W ERA 610297-14 REV ORIG. PRI REVS 0 AND 1 MATCH FINAL ERA. (LP #2919777)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

LOWER FRAME SECTION STA 132 WAS DAMAGED DURING LANDING. MAINTENANCE REMOVED LOWER FRAME SECTION PER B717 SRM 51-40-02. LOCATED AND DRILLED NEW SPLICES PER B717 DWG 9911512. INSTALLED NEW SPLICES AND REPLACEMENT 132 FRAME SECTION PER B717 SRM 51-40-02 AND DWG #9911512. (LP #2882770)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,832 hrs · 43,224 cycles

SHIP 9514 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AFTER NOT BEING ABLE TO EXTINGUISH THE "NLG UNSAFE" INDICATION ON APPROACH. THE QRH WAS COMPLIED WITH AND COMMUNICATIONS WITH MCC WAS ESTABLISHED, BUT THE NOSE LANDING GEAR FAILED TO EXTEND. THE CREW MADE A SUCCESSFUL NOSE-GEAR-UP LANDING AND MAINTAINED RUNWAY CENTERLINE. THE PASSENGERS EVACUATED THE AIRCRAFT ONTO THE RUNWAY VIA BOTH FORWARD EXIT SLIDES. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS. (LP #4636558)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,274 hrs · 42,735 cycles

WHILE REMOVING CEILING PANELS MAINTENANCE FOUND A BROKEN EMERGENCY LIGHT WIRE. THE WIRE WAS REPAIRED PER SWPM 20-30. THE OPERATIONAL CHECK WAS GOOD. (LP #4025352)

Part: NONE — NONE · airframe 60,008 hrs · 42,504 cycles

FOUND OVER WING INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE #7 EMERGENCY LIGHT BATTERY POWER SUPPLY, LOCATION 685R, PER B717 AMM 33-51. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (LP #4026293)

Part: FRAME — CRACKED · airframe 57,984 hrs · 40,646 cycles

FRAME AT STA Y1116 AND STR R11 CRACKED. REMOVED DAMAGED AREA PER B717SRM 53-00-07-2R-1. FABRICATED & INSTALLED REPAIR PARTS IAW B717 SRM53-00-07-2R-1. (LP #2182161)

Part: NOT REPORTED — NOT REPORTED · airframe 57,886 hrs · 40,566 cycles

DENT ON CENTER FIXED FLAP VANE LOWER SKIN BTW XV2 283 TO XV2 279 (LH WING). SUMMARY OF NRC 00088: CENTER FIXED FLAP VANE LOWER SKIN BTW XV2 283 TO XV2 279 (LH WING) WAS REMOVED PER B717 AMM: 27-50-02-000- 802. DAMAGE AREA WAS REPAIR PER B717 S.R.M. 51-70-02-0G PAR. 15 A. (1) TO (15) IN REFERENCE TO B717 SRM 57-53-01-2R-1 PAR. 4 D. THE SAME CENTER FIXED FLAP VANE LOWER SKIN BTW XV2 283 TO XV2 279 (LH WING) WAS INSTALLED PER B717 AMM 27-50-02-400-801 STE F( 4) TO G. (LP #2162316)

Part: NOT REPORTED — NOT REPORTED · airframe 57,890 hrs · 40,569 cycles

CRACKS (3 EA) ON INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE (IN REF SETTLEMENT AREA OF REFUEL ACCESS PANEL LATCHES). SUMMARY OF NRC 00079: INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE WAS REPAIRED PER ERA 598025-14 REV. ORIGINAL, PRI REV. 0 AND SRM 57- 40-01 REPAIR 3 FIG. 201 AND 202. ASSOCIATED ER/A 14-598025 ADDED FOR AC 9514. (LP #2162243)

Part: NOT REPORTED — NOT REPORTED · airframe 57,886 hrs · 40,566 cycles

CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1040 LONG 14RH. SUMMARY OF NRC 00049: FUSELAGE SKIN STA Y=1040 LONG 14RH WAS REPAIRED PER ERA 597705-14 REV. ORIGINAL SECTION 1. PERMANENT REPAIR AND PRI REV. 0,1,2,3 AND 4. REPETITIVE INSPECTIONS WILL BE MONITORING UNDER LP #2160713. (LP #2161936)

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

LIGHTNING STRIKE ON UPPER AREA OF OUTBD ELEVATOR TAB AT LH HORIZONTAL STABILIZER. SUMMARY OF NRC 00083: LH GEARED TAB WAS REMOVED AND SAME WAS INSTALLED PER B717 AMM 27-31-05. ALSO WAS REPAIRED PER B717 SRM 51-70-09-2R-5 AND SRM 51-70-09-0G. (LP #2160054)

Part: SKIN — CRACKED (BS 1037 L13-14R) · airframe 57,912 hrs · 40,588 cycles

REFERENCE ER/A 597705-14 FUSELAGE / SKIN / Y=1037, L-13R TO L- 14R / CRACKS, RESULTING IN A BOEING APPROVED RE-ENFORCING REPAIR . ACCOMPLISH SECTION II: REPETITIVE GENERAL VISUAL INSPECTION EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT ASSOCIATED ER/A 14-597705 ADDED FOR AC 9514. (LP #2160713)

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

CRACK ON ANGLE STA Y=1167 BTW LONG 2R AND 3R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00152: ANGLE STA Y=1167 BTW LONG 2R AND 3R AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 PER ER/A 597825-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI REV 0 AND REV 1. REPETITIVE INSPECTIONS : PERFORM DVI , WITHIN 3000 FLIGHT CYCLES AFTER SECTION I (PERMANENT REPAIR) ACCOMPLISHMENT ON 15MAR22 AND REPEAT AT INTERVALS NOT TO EXCEED 3000 FLIGHT CYCLES THEREAFTER PER ER/A 597825-14 REV. ORIGINAL. SECTION II UNDER LOG 2158201. ASSOCIATED ER/A 14-597825 ADDED FOR AC 9514. (LP #2159846)

Part: FRAME — CRACKED (BS 1166 L1-3R) · airframe 57,912 hrs · 40,588 cycles

ER/A 597825-14, FUSELAGE / MAIN FRAME / CLIP AND ANGLE, STA. 1166, L1-L3R / CRACK AND TRAPPED FASTENER. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. ACCOMPLISH ER/A 597825-14, SECTION II INSPECTION WITHIN 3000 FLIGHT CYCLES AFTER SECTION I ACCOMPLISHMENT ON 15MAR22 AND REPEAT AT INTERVALS NOT TO EXCEED 3000 FLIGHT CYCLES THEREAFTER. ASSOCIATED ER/A 14-597825 ADDED FOR AC 9514. (LP #2158201)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON ANGLE ON STA 1053 BTW LONG 28LH AND 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00261: ANGLE ON STA 1053 BTW LONG 28LH AND 28RH WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G AND DWG 9915561 REV. CG. (LP #2155703)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON INTERCOSTAL BTW 1022-1037 AND S30 C2. SUMMARY: INTERCOSTAL WAS REPLACED PER B-717 SRM 51-41-02-0G AND 51-41-05-0G PAR. 8. (LP #2155420)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON CHANNEL BTW STA 908 TO STA 927 AT AFT CARGO COMPARTMENT IN REF NRC 00187. SUMMARY OF NRC 00258: CORROSION LEVEL 2, CHANNEL BTW STA 908 TO STA 927 WAS REPLACED CHANNEL PER B717 SRM 51-40-08-0G PAR 3. (LP #2154412)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON LONGERON SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT. SUMMARY 00238: CORROSION LEVEL 2, LONGERON SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717 SRM 51- 41-05-0G AND 51-41-01-0G. (LP #2154356)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON LONGERON CHANNEL 29LH AND STA 957 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00190: CORROSION LEVEL 2, CHANNEL REPAIR WAS REPLACED PER B-717 SRM 53-00-05-2R. AND SRM 51-41-05-0G. (LP #2151046)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON SPLICE DOUBLER OF AFT DOOR JAMB AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00026: CORROSION LEVEL 2, SPLICE DOUBLER OF AFT DOOR JAMB AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53- 20-15-2R-6. (LP #2151681)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON PRODUCTION DOUBLER ATTACHED ON FWD FACE OF AFT PRESSURE BULKHEAD, BTW LONG 29LH TO 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00262: CORROSION LEVEL 2, PRODUCTION DOUBLER WAS REPLACED PER B717 SRM 51-41-05-0G AND DRAWING 5910130 ITEM 61 REV. ET. (LP #2150705)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON FWD PREVIOUS REPAIR DOUBLER AT FWD CARGO COMPARTMENT DOOR JAMB AREA. SUMMARY OF NRC 00192: CORROSION LEVEL 2, REPAIR DOUBLERS WERE REPLACED PER B717 SRM 53-20-15-2R-6 FIG. 201. (LP #2148640)

Part: NONE — NONE · corrosion level 2 · airframe 57,886 hrs · 40,566 cycles

CORROSION ON SPLICE DOUBLER OF FWD DOOR JAMB AT AFT CARGO COMPATMENT. SUMMARY OF NRC 00028: CORROSION LEVEL 2, DOUBLERS REPAIR WAS REPLACED PER B-717 SRM 53-20-15-2R-7 REPAIR.7. (LP #2149003)

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00151: LONGERON 2RH STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #2147774)

Part: NONE — NONE · airframe 57,881 hrs · 40,563 cycles

SHIP 9514 - THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT ATL. THIS WAS DUE TO AN "APU FIRE" INDICATION AT 26,000 FEET DURING CLIMB OUT. THE APU HAD BEEN OFF FOR MORE THAN 15 MINUTES BY THEN. THE CAPT RAN THE QRH APU FIRE CHECKLIST IN ITS ENTIRETY, FIRING BOTH BOTTLES, AND THE FIRE INDICATION REMAINED ILLUMINATED. NO SMOKE, HEAT, OR ODOR WAS EVER PRESENTED. THE AIRCRAFT STOPPED ON THE RUNWAY AND WAS MET BY ARFF WHO VERIFIED NO FIRE OR SMOKE WAS PRESENT. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE #1 AND #2 APU COMPARTMENT FIRE EXTINGUISHER BOTTLES PER B717 AMM 26-21. NO FAULTS WERE FOUND AFTER TROUBLESHOOTING PER B717 FIM 26-12-00-810-804. MAINTENANCE ALSO REPLACED THE FDCU PER B717 AMM 26-12. OPERATIONAL CHECK WAS GOOD. (LP #8312790)

Part: NONE — NONE · airframe 57,370 hrs · 40,138 cycles

THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS PER B717 AMM 33-51-14. OPERATIONAL CHECK WAS GOOD. (LP #8347215)

Part: SENSOR — MALFUNCTIONED (WOW) · airframe 56,016 hrs · 38,926 cycles

SHIP 9514 - THE FLIGHT CREW DECLARED AN EMERGENCY WHILE ON APPROACH DUE TO THE "PSEU FAIL" ILLUMINATING. THE CREW COMPLIED WITH QRH AND RESET THE GROUND PROXIMITY CIRCUIT BREAKER. IT WAS AN UNEVENTFUL LANDING AT NORMAL SPEED, BUT THEN THE "AGS FAIL", "SPOILER FAULT", AND "CABIN PRESS MANI FAIL" ALL ILLUMINATED. THE CFR CREW RESPONDED AND CHECKED THE BRAKE TEMPERATURES, WHICH WERE ALL NORMAL. CORRECTIVE ACTION: MAINTENANCE RAN BITE AND IT FAULTED THE WOW SENSOR CODE 326103. THE RIGHT WEIGHT ON WHEELS SENSOR WAS REPLACED AND ADJUSTED. ALL RTS TESTS PASSED. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #7465290)

Part: PANEL — MISSING (RT ELEVATOR) · airframe 54,162 hrs · 37,368 cycles

DURING W/A NOTICED 2 CIRCULAR INSPECTION DISKS MISSING FROM RIGHT LOWER ELEVATOR SURFACE. LOG-PAGE UPDATED @ 04MAR20 2344 UTC 02 CORR BY ATL 04MAR20 ATA 5523 RII: N ENTR W INSTALLED INSP. PNLS. (LP #5106954)

Part: LIGHT — DAMAGED (CABIN) · airframe 52,380 hrs · 36,034 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 604. MAINTENACE REINSTALLED THE CABIN SIDEWALL LIGHT LENS, (LT SIDE).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,083 hrs · 35,225 cycles

THE L1 DOOR AND COCKPIT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE L1 DOOR AND COCKPIT EMERGENCY LIGHTS PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4250450)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,921 hrs · 35,112 cycles

THE OVERHEAD EMERGENCY EXIT SIGN FOR THE OVERWING EXITS WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-120 AND THE POWER SUPPLY REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4616688)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,270 hrs · 33,970 cycles

DURING AN EMERGENCY LIGHT TEST, THE R1 LIGHT DID NOT WORK. THE BATTERY PACK WAS REPLACED. A TEST WAS PERFORMED. TESTED OK IAW AMM 33-51-00 710-801.

Part: FIRE BOTTLE — UNSERVICEABLE (CABIN) · airframe 49,248 hrs · 33,958 cycles

OUT OF LIMITS WEIGHT ON AFT/RT LAVATORY FIRE EXTINGUISHER CONTAINER. EXTINGUISHER ASSY WAS REMOVED AND A SERVICEABLE EXTINGUISHER ASSY WAS INSTALLED PER AMM 26-25-01.

Part: SKIN — WORN (LE SLAT) · airframe 49,248 hrs · 33,958 cycles

WORN RT WING SLAT PANEL NR 1 LOWER SKIN STA XFS=145. WEAR ON RT WING SLAT WAS REPAIRED, AS A PERMANENT REPAIR PER ER/A 566779-14 REV ORIGINAL AND ETI-17-18-038 REV 3.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 49,248 hrs · 33,958 cycles

DENTED AREA WAS FOUND DISBONDED. RT INBOARD FIXED FLAP VANE, LOWER SURFACE, DISBONDED AREA WAS REPAIRED IAW SRM 57-53-01-2R-1.

Part: SKIN — CRACKED (BS 1133) · airframe 49,248 hrs · 33,958 cycles

CRACKED EXTERNAL FUSELAGE SKIN BS 1133 BETWEEN STRINGERS 2L AND 3L. THE SKIN WAS REPAIRED IAW ER/A 566630-14AD, REV ORIG, AND ETI-17-18-029, REV 2.

Part: FRAME — CRACKED (BS 1037) · airframe 49,248 hrs · 33,958 cycles

CRACKED FRAME BS 1037 BETWEEN LONGERONS 14L. THE FRAME WAS REPAIRED IAW ER/A 566736-14, REV ORIG.

Part: FRAME ANGLE — CRACKED (BS 1052) · airframe 49,248 hrs · 33,958 cycles

CRACKED FRAME ANGLE ON THE LT AFT LAVATORY AREA BS 1052, BETWEEN LONGERONS 18L AND 19L. THE FRAME ANGLE WAS REPLACED IAW DWG 9915561, REV CG, SRM 51-41-05-0G, AND 51-41-02-0G.

Part: FRAME — CRACKED (BS 1037) · airframe 49,248 hrs · 33,958 cycles

CRACKED FRAME, BS 1037, LONGERON 13R. THE FRAME WAS REPAIRED IAW ER/A 566676-14, REV ORIG, AND ETI-17-18-034, REV 1.

Part: SKIN — DAMAGED (SLAT) · airframe 49,248 hrs · 33,958 cycles

DUE TO WEAR FOUND ON THE RT WING SLAT PANEL NR 1, LOWER SKIN, XFS 145, REMOVED AND REPLACED THE SLAT PANEL IAW AMM 27-80-01 AND ADJUSTED IAW AMM 27-80-01-830-802. RT WING NR 1 SLAT WAS REPAIRED IAW ER/A 566779-14, REV. ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 889-1022) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON THE LT & RT CARGO TRACK BS 889 TO 1022. THE CARGO TRACKS WERE REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.

Part: FRAME — CORRODED (BS 954) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON FRAME, BS 954, BETWEEN LONGERONS 25 AND 28. THE FRAME WAS REPAIRED IAW SRM 51-41-05-0G, AND 53-20-07-2R-3-.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX. CORROSION LEVEL 2, L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX WAS REPAIRED PER ER/A 566681-14 REV ORIGINAL AND ETI-17-18-035 REV 1.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 49,248 hrs · 33,958 cycles

AD 2016-09-05, AA 5530-01048: CRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER. REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.

Part: FRAME ANGLE — CORRODED (BS 900) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON THE FRAME ANGLE, BS 908, BETWEEN LONGERONS 29 AND 30R, THE FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06-2R-2, REPAIR 2, 51-41-02-0G, AND 51-41-05-0G.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 49,248 hrs · 33,958 cycles

CRACKED RT WING LOWER ACCESS PANEL AT THE TRAILING EDGE AREA XRS 150. THE ACCESS PANEL WAS REPAIRED SRM 57-50-01-2R, 51-41-01 0G, AND 51-41-05-0G.

Part: STIFFENER — CRACKED (BS 813-816) · airframe 49,248 hrs · 33,958 cycles

CRACKED VERTICAL STIFFENER BS 813 TO 816, BL 0, FWD BULKHEAD AFT FACE. THE STIFFENER WAS REPAIRED IAW SRM 53-00-00-2R, FIG-201, SHEET 1.

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566676-14. DISPLACED LAV TO GAIN ACCESS TO INSPECTION AREA. PERFORMED VISUAL REPETITIVE INSPECTION PER ERA 566676-14 REV.0 SECTION II. NO ITEMS NOTED. RIGHT LAV REINSTALLED ON NRC #00341. GENERAL VISUAL INSPECTION ON REPAIR AREA WAS PERFORMED PER ERA 566676-74 REV. ORIGINAL SECTION II STEP 1 AND DAMAGE WAS NOT FOUND. INSPECTOR STAMP TECHOPS 201114916. (LP #0462445)

Part: CAP — CRACKED (BS 1022) · airframe 49,248 hrs · 33,958 cycles

CRACKED CAP BS 1022, LONGERON 7R AND 7L. THE CAP WAS REPAIRED IAW ETI 17-18-026, REV 1, AND ER/A 566634-14, REV ORIGINAL.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 49,248 hrs · 33,958 cycles

CRACKS ON FLOOR PANELS #221CF, 221BF, 222ARF, 222AMF, 223JF, AND FLOOR PANEL P/N SP95530011-3 AT PAX CAB (CPAX). NRC 00506: FLOOR PANELS #221CF, 221BF, 22AMF, 223JF, AND SP95530011-3 WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R FLOOR PANEL #222ARF WAS RE-INSPECTED AND NO DAMAGE WAS FOUND IN REF B-717 AMM 05-21-02. FLOOR PANELS WERE INSTALLED WITH CARD JIC 2040-0024. (LP #0458282)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,248 hrs · 33,958 cycles

DELAMINATION ON FLOOR PANELS #211ANF, 221WF, 222GF, 222TF, 222AAF, 222AMF, 222AEF, 222AHF, 222AVF, 222ATF, AND 222DF AT PAX CABIN. NRC 00508: FLOOR PANELS #222AAF, 221WF, 222GF, 211ANF, 222AHF, 222AEF, 222AVF, AND 222ATF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R. FLOOR PANELS #222TF AND 222DF WERE REINSPECTED PER AMM 05-21-02 AND DELAMINATION WAS NOT FOUND. FLOOR PANEL #222AMF WAS ATTENDED WITH NRC 00506. FLOOR PANELS WERE INSTALLED WITH CARD JIC 2040-0024. (LP #0458830)

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 49,248 hrs · 33,958 cycles

CRACKS ON THE LT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. THE PAN WAS REPIARED IAW SRM 53-20-15-2R-8.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 49,248 hrs · 33,958 cycles

DENT ON THE AFT CARGO DOOR. REPAIRED IAW SRM 53-02-01-2R-1, FIG 202, SHEET 1, AND SRM 51-41-02.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 49,248 hrs · 33,958 cycles

CRACKED AFT VENTRAL DOOR FRAME LT FITTING BS 1064, LBL 14.5, Z=37. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: FITTING — CRACKED (BS 665 BULKHEAD) · airframe 49,248 hrs · 33,958 cycles

CRACKED FITTING BS 665, LONGERON 24 OF AFT BULKHEAD IN THE FWD CARGO BAY. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: SKIN — DENTED (BS 275-294) · airframe 49,248 hrs · 33,958 cycles

DENT ON FUSELAGE SKIN BETWEEN BS 275 - 294, LONGERON 18L TO 19L. REPAIRED IAW SRM 53-20-01-2R, PROCEDURE 5, FIG 202,

Part: DOOR FRAME — CRACKED (RT OVERWING EXIT) · airframe 49,248 hrs · 33,958 cycles

CRACKS ON THE RT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. REPAIRED IAW SRM 53-20-15-2R-8.

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

PERMANENT REPAIR WAS PERFORMED ON EXTERNAL SKIN PER B-717 SRM 53-02-01-2R-1 FIG. 202 SHEET 1. VISUAL INSPECTION WAS PERFORMED PER B717 SRM 53-02-01-2R PROCEDURE 1 PAR. 6A AND NO FUTHER DAMAGE FOUND. REPETITIVE 8000 CYCLES INSPECTION PER B717 SRM 53-02-01-2R-1 PARAGRAPH 6A IS IN PLACE. (LP #0457459)

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

SEVERAL CORROSION POINTS ON FWD BULKHEAD. THE BULKHEAD WAS REPAIRED IAW ER/A 566355-14, REV ORIGINAL, AND ETI-17-18-027 REV 1.

Part: ACCESS PANEL — CORRODED (WING) · airframe 49,248 hrs · 33,958 cycles

CORROSION ON FUEL ACCESS PLATES #620EB, 620CB, 620DT, AND 620AT. (AD) (PTAS). NRC 00491: DUE TO EXCESSIVE DAMAGE BY CORROSION 2, FUEL ACCESS PLATES #620AT, 620EB, AND 620DT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 AND FUEL ACCESS PLATE #620CB WAS REPLACED PER B717 IPC 57-23-01-01. (LP #0455946)

Part: WEB — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACKED WEB BETWEEN BEAMS 4 & 5, THE WEB WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9955763, REV M.

Part: FLOOR SUPPORT — CRACKED (BS 674-737) · airframe 49,248 hrs · 33,958 cycles

CRACK ON FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX (CPAX). NRC 00260: FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX WERE REPLACED PER B717 SRM 51-41-02-0G , 51-41-05-0G , 51-40-08-0G. (LP #0455100)

Part: FLOOR PANEL — CRACKED · airframe 49,248 hrs · 33,958 cycles

CRACKED CHANNEL OF FLOOR PANEL: THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50-2R-5, REPAIR 5.

Part: SKIN — CRACKED (BS 1076) · airframe 49,248 hrs · 33,958 cycles

CRACKED SKIN, BS 1076, BETWEEN LONGERONS 13L TO 14L. THE SKIN WAS REPAIRED IAW ER/A 566546-14, REV ORIGINAL, AND ETI-17-18-022, REV 2.

Part: NONE — NONE · airframe 57,886 hrs · 40,566 cycles

FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566546-14 AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR ASSOCIATED ER/A 95-566546 ADDED FOR AC 9514. PERFORMED A GENERAL VISUAL INSPECTION REF ERA 566546-14 REV ORIGINAL. NO DEFECTS NOTED. GENERAL VISUAL INSPECTION WAS PERFORMED PER ER/A NO 566546-14 REV. ORIGINAL SECTION II AND NO FURTHER DAMAGE FOUND. OK TO CONTINUE... (LP #0455687)

Part: ACCESS PANEL — CRACKED · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CRACKED FUEL ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.

Part: ACCESS PANEL — CRACKED · airframe 49,248 hrs · 33,958 cycles

CRACKED FUEL ACCESS PANLE. THE ACCESS PANEL WAS REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=1043 TO Y=1053 X=54. LEVEL CORROSION 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G.

Part: SUPPORT — WORN (VENTRAL DOOR) · airframe 49,248 hrs · 33,958 cycles

WEAR ON RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER SRM 52-10-02-2R REPAIR 16.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 49,248 hrs · 33,958 cycles

CRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.

Part: ACCESS PANEL — CRACKED (WING) · airframe 49,248 hrs · 33,958 cycles

CRACK ON FUEL ACCESS PLATES 520CB. FUEL ACCESS PLATE WAS REPLACE PER IPC 57-23-01-01 ITEM 442J.

Part: FORMER — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACKED LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.

Part: FORMER — CRACKED (BS 679) · airframe 49,248 hrs · 33,958 cycles

CRACKED LT AND RT FORMERS AT BS 679. THE FORMERS WERE REPAIRED IAW SRM 53-00-06-2R-2.

Part: FLOOR PANEL — DAMAGED · airframe 49,248 hrs · 33,958 cycles

CRACK IN CHANNEL, ALSO BENT CHANNEL AND SKIN OF FLOOR PANEL 222AQF AND 222XF. FLOOR PANELS WERE REPAIRED (PERMANENT REPAIR) PER SRM 51-20-09-0G, SRM 53-20-50-2R-5, & SRM 51-41-02-0G.

Part: FORMER — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACKED LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.

Part: LANYARD — DAMAGED (EVAC SLIDE) · airframe 49,248 hrs · 33,958 cycles

BROKEN STRANDS ON L1 AND R1 EMERGENCY SLIDE LANYARDS. LANYARDS WERE REPLACED PER AMM 25-61-01 400-801.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON LONG 8 RT STA Y=1022 AT CPAX. LONGERON 8R WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R, 51-41-02-0G, & 51-41-05-0G.

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 49,248 hrs · 33,958 cycles

CRACKED FITTING BETWEEN BEAMS 4 & 5, AFT EDGE AT AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.

Part: LONGERON — CRACKED (BS 1022) · airframe 49,248 hrs · 33,958 cycles

CRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: LONGERON — CRACKED (BS 1022) · airframe 49,248 hrs · 33,958 cycles

CRACKED LONGERON 8L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: PAN — CRACKED (CARGO DOOR) · airframe 49,248 hrs · 33,958 cycles

CRACK UPPER PAN, MID SECTION ON FWD CARGO COMPARTMENT DOOR. UPPER PAN ON MID SECTION WAS REPAIRED PER SRM 52-30-02-2R.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON SHEAR CLIP STA Y=1022 BTW LONG 13R TO 14R AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

A CRACK WAS FOUND ON THE CUSP WEB BTW STA Y=370 AND 389 X=-58 DURING CORROSION REMOVAL AT CAB PAX. CUSP WEB BTW STA Y=370 AND 380 X=-58 WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4., 51-41-02-0G.

Part: ANGLE — WORN (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

WEAR ON LT ANGLE ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. ANGLE WAS REPLACE PER SRM 51-41-04-0G, 51-41-05-0G, 51-41-02-0G, AND DWG 9929480 REV BW.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK WAS FOUND ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 DURING CORROSION REMOVAL AT CAB PAX. CRACK WAS BLENDED OUT PER SRM 53-00-00-1A FIG. 101 (ET) HFEC INSPECTION WAS PERFORMED ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 AT CAB PAX ON BLEND OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001. BLENDED AREA WAS EVALUATED AS FOLLOW MAXIMUM MATERIAL REMOVED 0.060'' AND MAXIMUM ALLOWABLE MATERIAL REMOVED IT'S 0.100'' THEREFORE IT'S WITHIN LIMITS PER B717 SRM 53-00-00-1A FIG. 101 AREA WAS TREATED AND PAINTED PER B717 SRM 51-10-04-0G PAR 15, 21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK SHEAR CLIP STA Y=1022 BTW LONG 13L TO 14L AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON LT CUSP WEB IN STA Y=877 TO Y=889, AND X=54 TO X=60. CORROSION LEVEL 2, CUSP WEB WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4 FIG 211 SHEET 1 AND FIG 215 SHEET 1.

Part: BEAM — CRACKED (PAX DOOR) · airframe 49,248 hrs · 33,958 cycles

CRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 202.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON LONG 4 LT STA Y=1022 AT CPAX. LONG 4 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.

Part: BEAM — CRACKED (PAX DOOR) · airframe 49,248 hrs · 33,958 cycles

CRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 201.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON LONG 6 LT STA Y=1022 AT CPAX. LONG 6 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON AFT LT LAVATORY FLOOR AREA STA Y=1073 X=22 Z=-1. CORROSION LEVEL 2, PLATE WAS REPLACED PER SRM 51-41-05-0G.

Part: BEAM — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR. BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR WAS REPLACED PER SRM 51-41-02 AND 51-41-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,248 hrs · 33,958 cycles

CRACK ON LONG 13 RT STA Y=1037 AT CPAX. CRACK ON LONG 13 RT STA Y=1037 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R-2 FIG 201.

Part: ACCESS PANEL — DAMAGED (LT WING AILERON) · airframe 49,248 hrs · 33,958 cycles

CRACK AND DENTS ON AILERON ACCESS PANEL 530HA, LT WING. REPAIRED IAW ER/A 566323-14 REV. ORIGINAL ASSOCIATED ER/A 00-566323.

Part: BEAM — CRACKED (PAX DOOR) · airframe 49,248 hrs · 33,958 cycles

CRACK ON BEAM NR 6 MID SECTION AT THE PASSENGER DOOR. REPAIRED IAW ER/A 559578-14MA, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 389) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 224.

Part: CUSP WEB — CRACKED (BS 579-598) · airframe 49,248 hrs · 33,958 cycles

CRACKED CUSP WEB BETWEEN BS 579 TO 598, RBL 54 - 60. THE CUSP WEB WAS REPLACED IAW DWG 9910151, REV BL, SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G.

Part: SPLICE — CORRODED (BS 579-598) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON FUSELAGE SPLICE BETWEEN BS 579 TO 598, LONGERON 18R AND 19R. THE SPLICE WAS REPLACED IAW DWG 9910151, REV BL, AND SRM 51-41-05-0G.

Part: FLOORBEAM — CORRODED (BS 148) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON THE FLOORBEAM AT BS 148, BETWEEN RBL 30 AND 44. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-01-2, FIG 1, AND 51-40-08-0G.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 49,248 hrs · 33,958 cycles

CRACK ON THE RT CUSP WEB BS 218 TO 237, BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 49,248 hrs · 33,958 cycles

CORROSION ON FUEL ACCESS PANELS 520CT AND 620CT. THE ACCESS PANELS WERE REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.

Part: PAN — CRACKED (BS 889) · airframe 49,248 hrs · 33,958 cycles

CRACKED LOWER FWD CORNER OF THE RT WINDOW RING PAN BS 889. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: CUSP WEB — CRACKED (BS 655-674) · airframe 49,248 hrs · 33,958 cycles

CRACKED CUSP WEB BETWEEN BS 655 TO 674, RBL 54 - 60. THE DAMAGE WAS REMOVED IAW SRM 53-00-55-2R-4, FIG 216.

Part: PAN — CRACKED (BS 851) · airframe 49,248 hrs · 33,958 cycles

CRACKED UPPER AFT CORNER OF THE RT WINDOW RING PAN BS 851. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: PAN — CRACKED (BS 870-889) · airframe 49,248 hrs · 33,958 cycles

CRACKED AFT UPPER CORNER OF THE LT WINDOW RING PAN AT BS 889 AND 870. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: PAN — CRACKED (BS 696) · airframe 49,248 hrs · 33,958 cycles

CRACKED UPPER FWD CORNER OF THE LT WINDOW RING PAN BS 696. THE PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G AND SRM 51-41-05-0G.

Part: PAN — CRACKED (BS 579-908) · airframe 49,248 hrs · 33,958 cycles

CRACKED LOWER FWD CORNER OF THE LEFT WINDOW RING PAN BS 579 AND 908. THE WINDOW RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 49,248 hrs · 33,958 cycles

CRACK ON L1 DOOR FRAME WEB BS 207, LONGERON 11L AND 15L. THE DOOR FRAME WEB WAS REPAIRED IAW SRM 53-10-15-2R-1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,182 hrs · 33,917 cycles

TAILCONE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51-03. OPS CHECKED GOOD.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 46,459 hrs · 32,085 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER AT DOOR L1 WAS LOOSE. MAINTENANCE REINSTALLED THE COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DAMAGED (RUDDER) · airframe 44,094 hrs · 30,290 cycles

ZR = 80.384 SKIN AT FRONT SPAR PILLOWING. SKIN IAW ERA 544413-14 LOG 2382278.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 44,094 hrs · 30,290 cycles

AFT CARGO, DOOR LOWER ENTRY JAMB CORRODED. REPAIRED THRESHOLD SECTION TO BE INSTALLED IAW SRM 53-20-15, REPAIR 7.

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 45,737 hrs · 31,578 cycles

FWD CARGO, LOWER DOOR FRAME CORRODED. REPAIRED IAW SRM 53-20-15.

Part: LONGERON — CORRODED (BS 898-954) · corrosion level 2 · airframe 45,737 hrs · 31,578 cycles

AFT CARGO LONGERON 29L FOUND CORRODED BS 898-954. REPAIRED IAW SRM 53-00-05 REPAIR 3 FIG 201.

Part: FITTING — GOUGED (NR 2 SLAT TRACK) · airframe 44,094 hrs · 30,290 cycles

RT WING NR 2 SLAT OTBD HINGE TRACK FITTING GOUGED ON UPPER EDGE. REPAIR ACCOMPLISHED IAW PRI 544515-14, REV 0 WAITING FOR FINAL ER/A. REPAIRED IAW PRI 544515-14 REV 0 AND ER/A 54415-14, REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,031 hrs · 28,743 cycles

DURING LINE CHECK, NOTED PHOTOLUMINESCENT STRIP MISSING IN CABIN AT EXIT ROW. REPLACED STRIP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,979 hrs · 28,700 cycles

DURING LINE CHECK, FOUND EMERGENCY LIGHTS FROM 16-19 ON CEILING INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY REF AMM 33-60. OPS CKS GOOD. LP 6978684.

Part: LANYARD — MISROUTED (L1 DOOR) · airframe 39,582 hrs · 26,641 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD MISROUTED. REROUTED LANYARD IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 39,063 hrs · 26,306 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 39,063 hrs · 26,306 cycles

CUSP WEB CRACKED AT BS 218, STRINGER 53L. CUSP WEB IAW SRM.

Part: SUPPORT FRAME — CRACKED (FUSELAGE) · airframe 39,063 hrs · 26,306 cycles

RT MLG WW BODY DOOR CUT OUT SUPPORT FRAME LUG CRACKED. REPAIRED FRAME IAW SRM.

Part: TUBE — LEAKING (NR 1 ENGINE) · airframe 37,461 hrs · 25,090 cycles

OIL LEAK AT NR 1 ENG. R & R NR 1 ENG OIL FEED TUBE & BOSS ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,826 hrs · 24,925 cycles

12D SEAT TRIM WITH EMERGENCY LIGHTING UNATTACHED FROM SEAT. REMOVED AND REPLACED FWD BAY ASSY AT 12D PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 34,189 hrs · 23,242 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (CATWALK)

ONE LAMP WILL NOT ILLUMINATE FOR TAIL COMPARTMENT WALK WAY E-PATH. REMOVED & REPLACED ONE LAMP FOR THE TAIL COMPARTMENT WALKWAY E-PATH OPS CHECK WAS NORMAL REF CH 33-51-14 OF THE BOE 717 MM.

Part: BATTERY — DISCHARGED (CABIN)

E-PATH LIGHTS INOP AT SEAT ROWS 1DF, 2DF, AND 3DF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY AND EMERGENCY BATTERY ASSEMBLY PER B717 AMM 33-51, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT SEATS 1 DF, 2DF, 3DF AND AISLE MARKER INOP. FOUND POWER SUPPLY B5-118 OUTPUT TO LIGHTS INOP. REMOVED AND REPLACED BATTERY AND POWER SUPPLY REF MM 33-51.

Part: PIN — DISLODGED (EVAC SLIDE)

L1 DOOR SLIDE PIN DISLODGED. REMOVED AND REPLACED L1 DOOR SLIDE PER 717 AMM 25-61.

Part: SIGN — BROKEN (CABIN)

EXIT SIGN FROM ABOVE R1 DOOR BROKEN. REMOVED AND REPLACED LENS COVER REF MM 33-28.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS NOT WORKING ON SEAT ROWS 1, 2 & 2. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY AS REQUIRED, OPS CHECKED GOOD WORK PERFORMED IAW 717 FIM 33-50 & AMM 33-51.

Part: STRUCTURE — CRACKED (PYLON)

LEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: STRUCTURE — CRACKED (PYLON)

RIGHT PYLON APRON LOWER 2ND HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: FRAME — DAMAGED (FUSELAGE)

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: STRUCTURE — CRACKED (PYLON)

RIGHT PYLON APRON LOWER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: PAN — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR AFT OF UPLOCK OUTER PAN, CRACKED. ACCOMPLISHED OUTER PAN DOUBLER REPAIR PER TRA 17-52-00139.

Part: PANEL — CRACKED (LT WING)

LEFT WING INBOARD BUTE DOOR, CRACKED. ACCOMPLISHED BUTE DOOR DOUBLER REPAIR PER EA 17-57-02514IR.

Part: FMU — UNSERVICEABLE (NR 2 ENGINE)

ENGINE RIGHT SYSTEM FAULT ON FINAL. A/C WOULD NOT SLOW BELOW 150 KNOTS ON FINAL, HAD TO GO AROUND WITH NO AUTO-THROTTLES TO GET CONTROL. REQUIRED RIGHT RUDDER ON LANDING. REMOVED AND REPLACED NR 2 ENGINE FMU IAW AMM 73-21-03. OPS CHECKED AND LEAK CHECKED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

CHECK L-1 DOOR SLIDE FOR PROPER INSTALLATION. REMOVED AND REPLACED SLIDE ASSEMBLY REF 25-61.

Part: SLIDE — UNSERVICEABLE (GALLEY DOOR)

GALLEY DOOR PACK SLIDE PRESSURE GAUGE INDICATING IN THE RED. REMOVED AND REPLACED GALLEY DOOR SLIDE PER MM 25-61.

Part: SLIDE — DAMAGED (R1 DOOR)

R-1 GALLEY DOOR EVAC SLIDE ARMING STRIP LOOSE STICKING OUT OF SLIDE PACK (LANYARD ASSY). REMOVED AND REPLACED R1-DOOR SLIDE PER MM 25-61.

Part: FRAME — CRACKED (BS 1178)

TWO EACH CRACKS, BOTH 1 INCH LONG IN RADIUS OF CANTE FRAME LEFT SIDE STA 1178 LONG 16 LEFT. INSTALLED FORMED ANGLE REPAIR PER SRM 51-70-11 F-201.

Part: PAN — CORRODED (CARGO DOORWAY)

FWD CARGO COMPARTMENT LOWER DOOR CUTOUT PAN. CUT OUT BETWEEN FUSELAGE STA 370 TO 427 HAS SURFACE CORROSION. REPLACED LOWER DOOR PAN AT FWD CARGO COMPARTMENT IAW B717 SRM 53-20-15 REPAIR 6.

Part: TIRE — FAILED (NR 3)

NR 3 TIRE FAILED. REMOVED AND REPLACED NR 3 MAIN TIRE AND WHEEL ASSY REF AMM 32-41.

Part: SKIN — DENTED (BS 218 L17L)

SMOOTH DENT AT FS 218.5, 4.0 INCHES LEFT HAND SIDE BELOW LONG 17 DENT IS 1 X 1 X .022 INCH D/X=45.45 PER SRM 53-00-01 REPAIR 2 PAGE 210. INSTALLED PERMANENT REPAIR AT LT SIDE FS 218.5 LONGERON 17 IAW B717 SRM 53-00-01 REPAIR 6 AND RES 06-0705. MATERIAL USED 7075 T6. SIZE 15.25 X 14 INCH.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTS VERY DIM AT AFT OVER WING EXIT LOWER LIGHTS / ROW 25-31. R/R POWER SUPPLY IAW B717 MM 33-51 OPS CHECK NORMAL.

Part: SKIN — DENTED (BS 229)

DENT ON LT SIDE FUSE BETWEEN L17 AND L18 NEAR STA 229. REQUIRES REPAIR WITHIN 4500 FLT HRS AS PER SRM 53-00-01 REPAIR TO COND 3. START TIME 9538:04. INSTALLED PERMANENT DOUBLER REPAIR AT BS 213.5 TO 229 AND BETWEEN L16L AND L18L (15.5 X 14) IAW B717 SRM 53-00-01 FIG 201 REPAIR 6. MATERIAL AND SIZE USED FILLER 2024T-3.050 X 15.5 X 14.0 DOUBLER, T-3 2024 .063 X 15 X14 INCH, FINGER DOUBLER 2024T, .025 X 18 X 17 INCH.

Part: SKIN — DENTED (BS 242)

DENT ON LEFT SIDE OF FUSELAGE STATION 242 AT L18 REQUIRES HIGH FREQ EDDY CURRENT INSP PER RES 05-1161. INSTALLED FLUSH SKIN PANEL REPAIR AT FS 242 AND L18 LEFT SIDE OF FUSELAGE IAW B717 SRM 53-00-01 FIG 201.

Part: DISPLAY — SHORTED (SEAT 11AC)

PAX & F/A REPORTED SMOKE /ELECT ARCHING ASSOCIATED WITH X/M SATELLITE SYSTEM AT SEATS 11/A/C. PULLED SYSTEM BREAKERS SMOKE/ ARCHING CEASED. UNEVENTFUL DIVERT TO RIC. REMOVED AND REPLACED DASDU UNDER SEAT 11 AC.

Part: SKIN — DENTED (BS 237)

FOUND DENT LEFT SIDE OF AIRCRAFT AT LONGERON 18 - 3 INCHES BY 1 INCH BY .0625 DEEP AT STATION 237. INSTALLED PERMANENT DOUBLER REPAIR AT STA 229 TO STA 264 BETWEEN L-16L TO 18L IAW B717 SRM 51-00-01 FIG 401. MATERIAL AND SIZE USED. DOUBLER 2024T3-.063 X 36.25 X 14.5 INCH, FILLER .050 X 35 X 14 INCH 2024 T-3, FINGER DOULBER 38.25 X 16.5 X .025, 7075T3.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING EMERGENCY LIGHT OPS CHECK, WHILE PERFORMING SERVICE CHECK, SEAT ROW 20 DEF LIGHT FAILS TO LIGHT. REPAIRED WIRING AT SEAT ASSY. PER B717 SWPM 20-30-12 AND SWPM 20-10-13, AND WDM 33-51-14 OPS CHECK NORMAL IAW AMM 33-51-00.

Part: BATTERY — DISCONNECTED (CABIN)

GALLEY AND STATION 218 EMERGENCY LIGHTS INOP. FOUND BATTERY UNPLUGGED FROM B5-259. RECONNECTED, OP CHECK OK.

Part: CONTROL UNIT — INOPERATIVE (LEFT IDG)

IMMEDIATELY AFTER TAKE OFF, SMOKE (ELECTRICAL) AND FUMES FROM FLOOR VENTS IN BUSINESS CLASS. LOST LEFT DC BUSS. FOUND LEFT HAND PCDU TO BE FAULT. REMOVED AND REPLACED LEFT HAND PCDU AND LEFT IDG.