N982AT
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AFT BULKHEAD DOOR WARNING ANNUNCIATION SYSTEMS, PERFORMED ADJUSTMENT OF AFT B/H DOOR PROX SENSOR IAW B717 AMM 52 -70/803. (1672780) (AICRAFT GROUNDED).
LT & RT WING EMERGENCY LIGHT INOPERATIVE. R & R WING EMERGEMCY LIGHT BATTERY PER AMM 33-51. OPS CHKD GOOD OK FOR SVC. (8873908) (AIRCRAFT GROUNDED)
CRACK ON ANGLE, BS 1178, ABOVE LT PYLON, EXTERNAL FUSELAGE. REPAIRED IAW ER/A 633070-14. (1511986)
CRACK ON EXTERNAL FUSELAGE SKIN BTW BS 1076, LONGERONS 13-14 RT. REPAIRED PER ER/A 633129-14 (1510684)
ERA 633129-14 SECTION I ISSUED FOR REPAIR TO BS 1076, L14R SKIN FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 633129-14 (1510528)
CRACK WAS FOUND IN OVERWING FRAME TAB Y= 696 RH SIDE AT PAX CABIN. CORRECTIVE ACTION: OVERWING FRAME TAB Y= 696 RH SIDE AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, SRM 51-41-05 (1502762)
ATO- CREW ABORTED TAKEOFF AT 20 KTS FOR AN AFT BULKHEAD DOOR WARNING. MAINTENANCE FOUND AFT CABIN BULKHEAD DOOR SENSOR BRACKET LOOSE AND RESECURED.(1477597)
AFT BULKHEAD DOOR CAUTION MESSAGE ON TAXI OUT FOR TAKEOFF. T/S PER FIM 52-70-00-810-809 CHECK PSEU SENSOR. CLEAN AND ADJUST PROX SENSOR PER B717 AMM 52-70 (7521980)
ABORTED TAKEOFF APPROX. 35KTS DUE TO AFT CABIN BULKHEAD DOOR INDICATION. REPLACED BULKHEAD DOOR PROX SENSOR. OK FOR SERVICE.(1140292)
AIRCRAFT 9549, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. CORRECTIVE ACTION: REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER B717 AMM 33-51. OPS CHECK GOOD. (LP 7315329)
DURING CHECK OF THE EXTERIOR LIGHTS, LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258403)
CRACKS ON SKIN WERE FOUND AFTER REMOVAL STOP FITTING ON AFT EDGE BEAM 2 APROX. SUMMARY OF NRC 00531: SKIN ON AFT EDGE BEAM 2 APROX WAS REPAIRED PER PRI 615938-14 REV 1 AND ERA 615938-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615938 ADDED FOR AC 9549. (LP #0257132)
CRACKS ON FUSELAGE SKIN (2 EA) ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) AT FUSELAGE. SUMMARY OF NRC 00072: FUSELAGE SKIN ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) WAS REPAIRED PER ERA 615858-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPETITIVE INSPECTIONS: ACCOMPLISH SECTION II WITHIN 24 MONTHS AFTER SECTION I WAS PERFORMED AND REPETITIVELY EVERY 24 MONTHS THEREAFTER. LP #0251086. (LP #0255820)
WEAR ON EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R. SUMMARY OF NRC 00018: EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R WAS REPAIRED PER ERA 577681-14 REV B SECTION II: PERMANENT REPAIR AND PRI 577681-14 REV 1 PART C. REPAIR APPROVAL IS LIMITED TO 58,000 TOTAL AIRCRAFT CYCLES. ADDITIONAL ENGINEERING AUTHORIZATION (ERA REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93, UNDER LOG PAGE #0252688. ASSOCIATED ERA 14-577681.
WEAR ON TRACK FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 AND OTBD SPOILER XTE 341. SUMMARY OF NRC 00134: FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G AND TRACK FITTING SUPPORT OF SETTLEMENT AREA OTBD SPOILER XTE 341 WAS BLENDED OUT AND (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED WITH ORIGINAL THICKNESS OF 0.085IN AND REMAINING THICKNESS ON AREA REWORKED IS 0.076IN. THEREFORE, AREA REWORKED IT IS WITHIN LIMITS PER B717-200 SRM 57-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 2 B. (LP #0246947)
CORROSION ON FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -X=43, Y= 200 BTW -X=46 TO -X=50 AND Y=200 BTW X=5 TO -X=5 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00681: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160 TO Y=200 X= 6, Y=180 BTW -X=10 TO -X=43, Y=200 BTW -X=46 TO -X=50 AND Y=200 BTW X=5 TO -X=5 AT PASSENGER CABIN STRUCTURE WERE FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-01-0G, AND 51-41-05-0G. (LP #0240010)
CRACK ON L1 DOOR PANE FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168. SUMMARY OF NRC 00704: L1 DOOR PAN FWD SIDE BTW #1 BEAM AND UPPER EDGE STA 168 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0234210)
CORROSION ON FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. FRAME CLIP STA Y=908 BTW LONG 28L AND 28R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0230532)
CORROSION ON LOWER SKIN OF OUTBD FLAP VANE AT RT WING. OTBD FLAP VANE AT RT WING WAS REPLACED BY ONE SERVICEABLE OTBD FLAP VANE (0228760).
FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER HAS A LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER PER ERA 596251-14AD REV A SECTION III TIME LIMITED REPAIR. REPETITIVELY INSPECT THE SUBJECT REPAIR EVERY 24 MONTHS (730 DAYS) PER ASSOCIATED ERA 596251-14AD REV A SECTION IV FROM DATE OF ACCOMPLISHMENT OF SECTION III REPAIR. ASSOCIATED ERA 00-596251 ADDED FOR AC 9549. (LP #0223851)
CRACK ON HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC: 00120. HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 52-30-01-2R PROCEDURE 1 REPAIR 1. (LP #0222418)
CORROSION ON STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 FWD CARGO COMPARTMENT. SUMMARY OF NRC 00625: CORROSION LEVEL 2. STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-08-0G. (LP #0221234)
CRACK WAS FOUND AT CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00678: CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIG.215. (LP #0206279)
CRACK ON RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00518: RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ALONG THE CUT OUT EDGES, NO CRACKS WERE FOUND PER DC-MD/BOEING NDTSPM PART 6. 06-10-01.001. (LP #0203722)
CORROSION ON RH PREVIOUS REPAIR DOUBLERS STA Y=451-464 AND Y=479 (LOWER SURFACE) X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00524: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER STA Y=451-464 AND Y=479 (LOWER SURFACE) X=- 60 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-00-55-2R-4 REPAIR 4. (LP #0203708)
CRACK ON RH CUSP WEB (LOWER SURFACE) STA Y=672 X=- 57 AT PASSENGER CABIN. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=672 X=- 57 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND AFTER TRIM-OUT PER B717 DC/MD NDTSPM PART 6. 06-10-01.001. (LP #0203725)
THE EMERGENCY LIGHTS AT THE LOWER AFT, LT AND RT OVERWING EMERGENCY DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4138625)
DURING EXTENSION AND RETRACTION OF NLG RETRACT ACTUATOR PER STEP 22 FOLLOWING GEAR MAINTENANCE, THE ACTUATOR CONTACTED THE REAR WHEELWELL BULKHEAD CAUSING DAMAGE. NRC 005-0003:3221-4001/013 00035; REPAIRED IAW ER/A 601048-14 REV. ORIG AND PER PRI 601048-14 REV 01. CLOSING REQUIREMENTS RII: INSPECTOR 00746460. (LP #2339754)
L/H O/B FIXED STRUT MOUNT HAS CORROSION ON OUTBOARD/FWD MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/002 00023 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331304)
L/H O/B FIXED STRUT MOUNT HAS CORROSION AND TOOLING MARKS ON OUTBOARD/AFT MOUNT HOLE SURFACE. SUMMARY SEE NRC 004-0003: 3211-4003/001 00022 COMPLIED WITH PRI 600942-14 REV. 0, PRI 600942-14 REV 1, AND FINAL ER/A 600942-14 REV ORIGINAL. (LP #2331305)
RIGHT MLG ATTACH FITTING CHAFED AND CORRODED WHERE FIXED STRUT MOUNTS. -M- SUMMARY SEE NRC 008-0003: 3211-4004/001 00018 PRI 600916-14 REV. 0 PRI 600916-14 REV. 1 AND FINAL ER/A 600916-14 REV. ORIGINAL HAVE BEEN COMPLIED WITH. (LP #2330440)
TAIL CONE SLIDE PACK CABLE RETAINER BROKEN. THIS ITEM IS RII PER TOPP 40-30-05 QC5146. REPLACED CABLE RETAINER PER SAFRAN CMM 25-66-20 QC 5270. (LP #8745178)
THE AFT LEFT & RIGHT EMERGENCY EXIT OVERWING THRESHOLD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230 PER B717 AMM 33-51-04. THE EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. (LP #8262534)
MAIN CABIN FLOOR SUPPORT UNDER FLOOR PANEL 221AF FOUND CORRODED. MAINTENANCE REPLACED SUPPORT PER BOEING DWG 9936534, AND B717 SRM 51-40-02. (LP #2076902)
THE RIGHT HAND GALLEY CABIN EMERGENCY EXIT SIGN LIGHT HAS BROKEN WIRES. -M- SUMMARY SEE NRC 001-0010:2500-2647/113 00431: REPAIRED WIRES PER REF B717 SWPM 20-10-03. OPERATIONAL CHECK WAS GOOD. (LP #2076170)
AFT CARGO. FLOOR BOARD SUPPORT/FORMER CORRODED AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER. (M) FLOOR BOARD SUPPORT/FORMER AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER FOUND CRACK, FOUND TO BE 100% OUT OF LIMITS PER B717 SRM 53-00-00-1A 3. REPAIRED AFT CARGO. FLOOR BOARD SUPPORT ANGLE AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER PER B717 SRM 51-70-05-2R 5. OK CIC 8. APPLIED CIC ON REPAIR AREA PER PS 900-2 NO. 09 9. CORROSION LEVEL: 2. (LP #2074161)
FLOOR BEAM CRACKED AT STATION Y=737 RH OVERWING FRAME ATTACH POINT. REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072760)
FLOOR BEAM CRACKED AT STATION Y=737 LH OVERWING FRAME ATTACH POINT. MAINTENANCE REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072758)
RH FUSELAGE WINDOW BELT WINDOW #12 AT STA 446-465 HAD A LIGHTNING STRIKE. FOLLOW ON ACTION REQUIRED. ERA 596251-14 ISSUED. FOLLOW ON ACTION REQUIRED SECT I TBA DURING C-CHK VISIT IN MSP DEC2021. SECT II HFEC INSPECTIONS TBA AT EVERY 24 MONTH INTERVALS AFTER SECT I. SECT III PERM REPAIR NOT TO EXCEED 10,000 FC AFTER SECT I. ASSOCIATED ERA 00-596251 ADDED FOR AC 9549. CORRECTION TO PREVIOUS ENTRY. PERFORM SECTION III PRIOR TO AIRCRAFT ACCUMULATING 45000 TOTAL FLIGHT CYCLES OR 10089 FC FROM 30DEC 21. HFEC INSPECTON WAS PERFORMED, NO CRACKS WERE FOUND ON BLENDED AREA PER ERA 596251-14 REV ORIGINAL, SECTION II REPETITIVE INSPECTIONS, STEP 1. SUMMARY OF NRC 00356: RH SIDE WINDOW BELT PANEL AT WINDOW #12 WAS REPAIRED PER ERA 596251-14AD REV B SECTION III: PERMANENT REPAIR. REPETITIVE INSPECTIONS: TO BE ACCOMPLISHED EVERY 24 MONTH INTERVALS AFTER SECTION III WAS PERFORMED UNDER LP #0223851 REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL FLIGHT CYCLES (21,037 FLIGHT CYCLES FROM 38,963 TOTAL FLIGHT CYCLES AS OF 28 FEB 24). CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 06MAR24 AND LOG COMMENTS. (LP #2067714)
THE EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN SWITCHED ON. MAINTENANCE REPLACED THE BATTERY PACK REF B717 AMM 35-31-03. OPERATIONAL CHECK WAS GOOD. (LP #7374989 )
ON TAXI-IN, WHEN ATTEMPTING TO OPEN A FOGGED-UP WINDOW WITH WINDSHIELD ANTI-FOG SELECTED ON, THE WINDOW JAMMED ON THE CAPT HEADSET CAUSING A SHORT. THE RESULT WAS A LOUD BUZZ AND A FIREBALL THAT QUICKLY EXTINGUISHED. THE CB Z-26 ALSO TRIPPED. MAINTENANCE PULLED C/B Z26 AND Z25 AND DISCONNECT WIRE FROM CAPT CLEARVIEW WINDOW. THE CAPT SLIDING WINDOW THERMOSWITCH HARNESS WAS REPLACED PER B717 AMM 30-42. TERMINATED HARNESS ENDS REF B717 WDM 3-42-01. OPERATIONAL CHECK WAS GOOD. BREAKERS STAYED IN. WIRING ON A/C SIDE CHECKED GOOD.
THE CABIN EMERGENCY LIGHTS FLICKER WHILE IN ARMED POSITION VERY OCCASSIONALY. MAINTENANCE REPLACED THE RELAY R2-5133 PER B717 WDM 24-51-01. OPERATIONAL CHECK WAS GOOD. NOTED NO DEFECTS.
MAINTENANCE FOUND THAT THE FWD EMERGENCY LIGHTS FAILED DURING A SERVICE CHECK TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51. OPS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE.
THE R1 DOOR EXIT SIGN LENS WAS MISSING. MAINTENANCE INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51.
ONE EMERGENCY LIGHT WAS OUT IN THE TAIL COMPARTMENT. MAINTENANCE FOUND A DISCONNECTED WIRE AND CONNECTED IT. OPS CHECKED GOOD.
0.5 INCH CRACK WAS FOUND ON VERTICAL STAB. FRONT SPAR CAP RT SIDE. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.
DISTRESS AT LT & RT SIDES OF VERTICAL STABILIZER LE SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.
ELONGATED HOLES AT THE LT & RT SIDES OF VERTICAL STABILIZER L.E. FRONT SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.
DURING INSPECTION, AN ELONGATED HOLE ON THE LE REMOVABLE FAIRNG LT SIDE WAS FOUND. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.
CRACKED FRAME BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.
CRACKED FRAME BS 1022 ON LONGERON 7L AT PASSENGER CABIN AREA. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.
CORROSION ON THE LT WEB DOOR FRAME BS 200, LONGERONS 17 AND 18L REPAIRED IAW ETI-17-17-093, REV. 2 AND ER/A 559514-14 REV. ORIGINAL.
CORROSION ON CTR FUEL TANK SKIN STA Y=742 BTW X=-20 TO X=-60 AT RT WHEELWELL SLANT PANEL AREA AMDS 5300-2003. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.
CORROSION ON THE RT CARGO TRACK BETWEEN BS 895 & 954, BS 994 & 1022 IN THE AFT CARGO BAY. THE SECTION OF CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-40-08.
CORROSION ON CENTER FUEL TANK UPPER SKIN FROM Y=737 TO Y=756, X=22 TO X=60, ALSO Y=705-710, X=-56 TO X=-60 AT CABIN PAX WING BOX AREA AMDS 5300-2008. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.
CORROSION ON CENTRAL FUEL TANK SKIN BELOW SLANT PANEL STA Y=742 BTW X=18 TO X=25 LT WHEEL WELL AMDS 0593-2002. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.
CRACK ON FIXED COWL APRON HINGE, LATCH ASSEMBLY AFT OF LOWER FAN COWL DOOR ENGINE LT. CRACK ON FIXED COWL WAS REPAIRED PER SRM 54-00-00 REP 1 HINGE, GUSSET, AND CLIP WERE REMOVED AND REINSTALLED PER SRM 51-41-02-0G AND 51-41-05-0G.
CRACKED FRAME ANGLE BS 1022 BELOW OF LONGERON 14L IN THE PAX CABIN. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05, AND DWG 9912243, REV JS.
ELONGATE HOLES ON THE FUEL ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.
HOLES ELONGATED AT FUEL ACCESS PANEL 520GB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, PAR 5, REPAIR 2, CONDITION II.
CRACKED STRAP ON FRONT OF DOOR FRAME WEB BS 200 LONGERON 18L. THE STRAP WAS REPLACED IAW SRM 51-41-08, AND SRM 51-41-05.
CRACKED FRAME ANGLE BS 1022, LONGERON 14L. FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9912243, REV JB.
CRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 15L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.
CRACK ON FUSELAGE SKIN BS 1076 BETWEEN LONGERONS 15 - 13L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.
CRACK ON INTERCOSTAL IN THE CEILING AREA BETWEEN BS 617 - 636, BL 0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1.
CRACKED LONGERON 2R, BS 1133 IN THE AFT ACCESSORIES BAU AREA. A REPAIR SPLICE WAS INSTALLED SRM 53-00-05-2R.
CRACKED FRAME ANGLE BS 1022, LONGERON 14R. THE DAMAGE WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-00-06-2R, AND DWG 9912243, REV JB.
TWO CRACKS WERE NOTED ON THE FUSELAGE SKIN, BETWEEN 1076 AND 1087, L-14L. ER/A 559501-14 SECTION I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION FOR SECTION II IS REQUIRED. ACCOMPLISH ER/A 559501-14 SECTION II INSPECTION AT C-CHECK INTERVALS FROM SECTION I, NOT TO EXCEED 24 MONTH INTERVALS. FOLLOW ON ACTION IS REQUIRED. ASSOCIATED ER/A 95-559501 ADDED FOR AC 9549. **REDEFERRED LOG TO QC, ESTAB MON INSP **20-0553-8-6826 S/N 09549 REP. C/W DECAL CONDITIONAL INSPECTION, FOUND GOOD. NO FURTHER DEFFECT NOTED. ITEM 5 SHOULD STATE REF ERA 559501-14 REV ORIG SECT 2. C/W ER/A 559501-14 SECTION II INSPECTION . C/W DECAL CONDITIONAL INSPECTION, FOUND GOOD. NO FURTHER DEFECT NOTED. (LP #0104508)
DISBONDED AREAS AT DENTS 6, 7, AND 18 ON RT WING AFT MOVABLE FLAP VAN. REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND OPN 1031 CARD 2000-8149-02.
CRACKED FRAME ANGLE BETWEEN LONGERONS 3R &3L, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.
CRACKED PAN LOWER AREA INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02-2R PROCEDURE 1, REPAIR 1, FIG 201.
CRACKED LOWER FITTING INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPLACED IAW SRM 51-41-01, AND 51-41-05.
DELAMINATION WAS FOUND BELOW DENTS NR 3 & 12 OF RT WING FLAP FORWARD MOVEABLE VANE LOWER SURFACE. REPAIRED SRM 57-53-01, FIG 201, REP 1.
CORROSION ON RT SEAT TRACK RBL 22 BTW BS 822 & 937. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R, REPAIR 5.
CRACKED FRAME ANGLE, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.
CRACKED INTERCOSTAL BETWEEN BEAMS 4 AND 5, BS 181, FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9955763, REV M.
CRACK ON LT FORMER BS 694, LONGERON 26L. THE FRAME WAS REPAIRED IAW SRM 51-70-11, REP 1.
CORROSION ON RUBSTRIP OF FUEL ACCESS DOOR 520JB I. NEW RUB STRIP 520JB WAS REPLACED PER B717-200 SRM 57-10-01-2R REP 3 PAR 6. (LP #0098256)
WEAR AND NICKS ON PREVIOUS REPAIR DOUBLERS STA 907 LT/LWR ALSO STA 909 LT/UPPER AT PASSENGER CABIN RING PANS AREA. REPAIR DOUBLERS WERE REPLACED PER SRM 56-20-02 REPAIR 1 FIGURE 202.
CRACK ON RT RING PAN (FWD UPPER CORNER) STA Y=756 AT PAX CABIN (CPAX). RING PAN WAS REPAIRED PER SRM 56-20-02-2R-1 REPAIR 1.
CRACKED LONG 6 RT ON STA 1022. AT PASSENGER CABIN AREA. LONG 6 RT ON STA 1022. WAS REPAIRED PER SRM 53-00-05-2R-2-, FIG 201.
CRACKED LONGERON 6 LT ON STA 1022 AT PASSENGER CABIN AREA. LONGERON WAS REPAIRED PER SRM 53-00-05-2R-2, FIG 201.
CORROSION ON SETTLEMENT AREA ON FUEL TANK ACCESS 520CT AND 520DT. FUEL TANK ACCESS 520CT AND 520DT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.
ELONGATE HOLES ON FUEL TANK ACCESS PANEL 620DB. THE ACCESS PANEL WAS OUT OF LIMITS FOR EXCESSIVE DAMAGES IAW SRM 57-10-01 AND WAS REPLACED.
CRACK ON RT FORMERS Y=715 , Y= 694 AT UNDERWING CANTED KEEL , INTERNAL STRUCTURE. FRAMES WERE REPAIRED PER SRM 51-70-11-2R. HFEC INSPECTION WAS PERFORMED AND 01 CRACK OF 0.4" ON RT FORMER Y=694 AT UNDERWING CANTED KEEL, INTERNAL STRUCTURE AND 01 CRACK OF 0.5" ON RT FORMER Y=715 WERE FOUND PER NDT SPM 06-10-01.001.
CORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 520FT. FUEL TANK ACCESS 520FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WAS REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.
CORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 620CT AND 620FT. FUEL TANK ACCESS 620CT AND 620FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.
CRACKED LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA. LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.
CRACKED LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA. LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.
CRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1.
CRACKED SKIN BTW BEAM NR 1-2 AT HOUSING AREA FWD CARGO COMPARTMENT DOOR (C1). SKIN WAS REPAIRED PER SRM 52-30-01-2R-1, FIG 201.
CRACKED LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.
CRACKED LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA. LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR1 FIG 201.
CRACKED LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.
CRACKED LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.
CRACKED LT LOWER RING PAN BS 618. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 201.
CRACKED NR 1 BEAM FWD EDGE AT FWD PASSENGER DOORWAY. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 202.
CORROSION ON FLOOR SUPPORT BS 140 AND RBL 50. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.
CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO 200, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.
BROKEN FLOOR PANEL 211ANF. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R, REP 3 AND REPLACED.
CORROSION ON RT CUSP WEB BS 549 TO 553 BETWEEN RBL 54 TO 60 IN THE PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.
CRACKED NR 1 BEAM, AFT EDGE AT FWD PASSENGER DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 201.
CRACK ON THE RT NLG DOOR FRAME BEAM RBL 46 AT NLG W/W. REPAIRED IAW SRM 53-10-14, REP 2.
EMERGENCY LIGHT DETACHED AT SEAT 19B ATTACHED THE EMERGENCY LIGHT. OK FOR SERVICE.
DURING LINE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EMERGENCY LIGHTING IN THE TAILCONE; THEY WOULD FLASH ON AND THEN GO OFF. MAINTENANCE REPLACED THE BATTERY AND THE OPERATIONAL CHECK WAS GOOD. (LP #9118010)
FLIGHT CREW REPORTED L1 DOOR HIT THE FUSELAGE AT TOP AFT CORNER. IAW AMM 52-11 DURING VERTICAL ADJUSTMENT FOUND PLAY IN VERTICAL ADJUSTMENT AREA. FOUND DOOR DAMAGE AT SEVERAL AREAS, REPLACED L1 DOOR IAW AMM 52-11. REBUSHED LOWER HINGE FITTING, PRESSURIZATION LEAK CHECKED GOOD. INSTALLED DOOR INTERIOR TRIM IAW AMM 52-11.
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE AFT OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.
DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOOR L1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.
EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 - 14. REPLACED THE BATTERY PACK AT B5-227 IAW AMM 33-51-03.
R1 DOOR EMER EVAC SLIDE CUT OUT LOWER SUPPORT BRACKET LOOSE. R & R BRACKET ASSEMBLY IAW SRM.
STAND BY LIGHT INOPERATIVE AT ROW 12. REPAIRED WIRE IAW SWPM & AMM.
AFT CATWALK EMER LIGHT BULB INOPERATIVE. REPLACED BULB IAW MM.
FORWARD EMER FLASHLIGHT INOPERATIVE. ADJUSTED FLASHLIGHT IAW AMM.
AFT CATWALK EMER LIGHT BULB INOPERATIVE. R & R BULB IAW MM.
AFT OVERHEAD EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.
FORWARD OVERWING DOOR EMER LIGHT BULB INOPERATIVE. R & R LIGHT IAW MM.
AFT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.
MAIN CABIN FLOOR WEB DOUBLER LOCATED BETWEEN BS 160 - 180, RBL 50 CRACKED. R & R WEB IAW SRM & DWG.
MAIN CABIN UPPER CUSP ANGLE CORRODED BETWEEN BS 200 - 218, RBL 55. R & R CUSP ANGLE IAW SRM & EA.
CUSP WEB CRACKED BETWEEN BS 636 - 655, RBL 44. R & R CUSP WEB IAW SRM & DWG.
FORWARD CABIN FALSE TRACK CORRODED AT BS 173, RBL 7. R & R FALSE TRACK IAW SRM & DWG.
R1 DOOR ESCAPE SLIDE GIRT BAR FWD FLOOR FITTING CORRODED. R & R FITTING IAW SRM & DWG.
R1 DOOR ESCAPE SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. R & R FITTING IAW SRM & DWG.
MEMBRANE CORRODED AT BS 198, RBL 50. REPAIRED MEMBRANE IAW SRM.
MAIN CABIN CUSP WEB CRACKED BETWEEN BS 579 TO 598, LBL 54. R & R MAIN CABIN CUSP WEB IAW SRM & DWG.
MEMBRANE CORRODED AT BS 204, RBL 58. R & R MEMBRANE IAW SRM & DWG.
MAIN CABIN FRAME CRACKED AT BS 674, LONGERON 18R. R & R FRAME IAW DWG.
LEFT WW FWD VERTICAL CHANNEL AT DOOR CUT OUT CRACKED. R & R CHANNEL IAW SRM & DWG.
MAIN CABIN FRAME CRACKED AT BS 674, LONGERON 18R. R & R FRAME IAW DWG.
MAIN CABIN FLOOR PANEL 222MF DELAMINATED AT BS 500, RBL 40. REPAIRED PANEL IAW SRM.
RT FORWARD OVERWING EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.
CUSP WEB CRACKED BETWEEN BS 636 TO BS 655 RBL 44. REPAIRED WEB IAW SRM.
LT CABIN WINDOW FRAME DOUBLER NR 35 CRACKED AT LOWER AFT CORNER OF WINDOW PANE. REPAIRED DOUBLER IAW SRM & DRAWING.
RT WING NR 5 SLAT INBD SIDE OF NR 12 TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.
RT SIDE INTERIOR ANGLE CRACKED AT OTBD END AT BS 674. R & R ANGLE IAW SRM & DRAWING.
FRAME SUPPORT CRACKED AT BS 655 STRINGER 18L. R & R SUPPORT FROM IAW SRM & DRAWING.
UNDERWING BARREL KEEL BEAM LT SIDE INTERIOR ANGLE CRACKED AT BS 696. R & R ANGLE IAW SRM & DRAWING.
RT CUSP WEB CORRODED BETWEEN BS 465 TO BS 484. REPAIRED WEB IAW SRM.
LT DOUBLER CUSP WEB CORRODED BETWEEN BS 579 TO STATION 598. R & R WEB IAW SRM & DRAWING.
RT CUSP WEB CORRODED BETWEEN BS 484 TO BS 503. R & R CUSP WEB IAW SRM.
RT INTERIOR ANGLE CRACKED AT BS 696. REPAIRED ANGLE IAW SRM & DRAWING.
LT CUSP WEB CORRODED BETWEEN BS 408 TO BS 427. R & R CUSP WEB IAW SRM.
RT CUSP WEB CORRODED BETWEEN BS 446 TO BS 465. R & R CUSP WEB IAW SRM.
LT SIDE INTERIOR ANGLE CRACKED AT BS 715. REPAIRED ANGLE IAW SRM & DRAWING.
UNDER WING BARREL KEEL BEAM, LT SIDE INTERIOR ANGLE CRACKED AT BS 674. R & R ANGLE IAW SRM & DRAWING.
MAIN CABIN PRESS BULKHEAD EMERGENCY EXIT SIGN COMPOSITE SUPPORT BROKEN. REPAIRED SUPPORT IAW SRM.
LT CABIN WINDOW FRAME DOUBLER NR 36 CRACKED AT UPPER FWD CORNER. REPAIRED DOUBLER IAW SRM & DRAWING.
AFT PRESS BULKHEAD DOOR JAMB LT FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.
MAIN CABIN AFT PRESS BULKHEAD DOOR JAMB LT FITTING CRACKED. R & R FITTING IAW DRAWING.
RT CUSP WEB CORRODED BETWEEN BS 655 TO BS 715. R & R CUSP WEB IAW SRM.
SEAT TRACK CORRODED BETWEEN BS 671 TO BS 810 RBL 44. R & R SEAT TRACK IAW SRM & DRAWING.
LT CUSP WEB CORRODED BETWEEN BS 655 TO BS 715. R & R CUSP WEB IAW SRM.
AFT PRESS BULKHEAD DOOR JAMB RT FITTING CRACKED AT FASTENER HOLES. R & R FITTING IAW SRM.
RT CABIN WINDOW FRAME DOUBLER NR 35 CRACKED AT LOWER AFT CORNER OF WINDOW PANE. REPAIRED DOUBLER IAW SRM & DRAWING.
AFT RT VENT BOX DOUBLER ON AFT SIDE ATTACH TO FRAME CRACKED. R & R DOUBLER IAW SWA EA.
TAIL CONE LATCH RELEASE CABLE CLEVIS CORRODED. R & R CLEVIS IAW AMM.
RT WW FWD WING TO BODY FAIRING STRUCTURE CRACKED AT OTBD END BS 750. REPAIRED STRUCTURE IAW SRM.
RT WW SHROUD ON WING TO BODY FAIRING STRUCTURE DOUBLER CRACKED AT BS 800. REPAIRED STRUCTURE IAW SRM.
RT FRAME CRACKED AT BS 715. R & R FRAME IAW DRAWING.
LT FRAME CRACKED AT BS 696, CRACKED AT OVERWING FLOOR BEAM. R & R FRAME IAW DRAWING.
FORMER CRACKED AT BS 1087 BETWEEN LONGERON 1L TO LONGERON 2L. R & R FORMER IAW SRM.
LT MLG DOOR HINGE FWD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.
RT MLG DOOR HINGE FWD ATTACH ANGLE CRACKED. R & R ANGLE IAW DRAWING & SRM.
RT JAMB CORRODED BETWEEN BS 370 TO BS 427. REPAIRED JAMB IAW SRM.
RT EMERGENCY LIGHTS MISSING BETWEEN ROW 2 & ROW 3. INSTALLED LAMP IAW AMM.
ROW 2D EMERGENCY PATH LIGHT MISSING. REPLACED 2D EMERGENCY PATH LIGHT BULB OPS CHECKED GOOD IAW AMM. NO DEFECTS AT THIS TIME.
EMERGENCY ESCAPE PATH LIGHTS LENS COVER MISSING AT SEAT 2D. INSTALLED LENS RSF MM.
SIGN COVER MISSING AT ROW 21/22 FELL OFF AND NOT FOUND. FOUND SIGN COVER EXIT SIGN AND RE-INSTALLED, OK FOR SERVICE REF 33-51 AMM.
R1 DOOR FLOOR SUPPORT FITTING, STA 196, RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02.
FORWARD ENTRY FLOOR SUPPORT, STA 196, LBL 15 TO LBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-1-04 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 196 TO 210, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY FLOOR STRAP, STA 168 TO 200, RBL 56, CORROSION. ACCOMPLISHED FLOOR STRAP REPLACEMENT PER B717 SRM 51-41-01, 51-40-08 AND 51-10-04.
FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, LBL 58, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 200, RBL 9 TO RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 148, RBL 39, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 200, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY FLOOR SUPPORT, STA 180, RBL 8 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY FLOOR PAN, STA 168, RBL 58, CORROSION. ACCOMPLISHED FLOOR PAN REPLACEMENT PER B717 SRM 51-40-08, 51-10-04 AND 51-41-02.
FORWARD ENTRY FLOOR SUPPORT, STA 160 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 51-41-02, 51-40-08, 51-10-04 AND 53-10-51.
FORWARD ENTRY SHEAR WEB, STA 200 TO 203, RBL 23 TO RBL 29, CORROSION. ACCOMPLISHED SHEAR WEB SPLICE REPAIR PER B717 SRM 51-70-10 AND 53-10-51.
FORWARD ENTRY SHEAR WEB, STA 200 TO 203, RBL 40 TO RBL 43, CORROSION. ACCOMPLISHED SHEAR WEB SPLICE REPAIR PER B717 SRM 51-70-10 AND 53-10-51.
EMERGENCY LIGHTS AT SEATS 1D, 2D, 3D INOPERATIVE. REMOVED AND REPLACED BATTERY SUPPLY ASSEMBLY AT STA 341 PER AMM 33-51. CHECKS OK.
PINS HOLDING ESCAPE SLIDE PACK AT L1 DOOR MISSING. REMOVED AND REPLACED SLIDE PACK PER MM 25-61-01.
COMPRESSOR STALL LEFT ENGINE AFTER TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD 603. LEAK AND OPS CHECK GOOD.
GIRT BAR RETAINER AT GALLEY DOOR BROKEN. REMOVED AND REPLACED GIRT BAR RETAINER AND INSTALLED BACK ON COVER DOOR FOR SLIDE IAW MM 26-61, OK TO CONTINUE SERVICE.
AFT CARGO COMPARTMENT LONGERON SECTION, STA 908 TO 946, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3041.
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.
EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2985.
AFT CARGO COMPARTMENT LONGERON SECTION, STA 908 TO 946, LONG L29L, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3040.
AFT CARGO COMPARTMENT LONGERON SECTION, STA 946 TO 974, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER SRM 51-10-04. SEE NR 3045.
F/A REPORTS L1 DOOR SLIDE PRESSURE LOW. REPLACED L1 DOOR SLIDE PER AMM 25-61-01-6.
RUDDER SUPPORT BULKHEAD CRACKED AT 3 O`CLOCK POSITION STA 1178. REPAIRED RUDDER SUPPORT BULKHEAD CRACK AT STA 1178 L18 IAW B717 SRM 51-70-11. COMPLETED AAR N/R 5837 W/O 2000274 - OK FOR SERVICE.
EMERGENCY LIGHT SYSTEM INOPERATIVE. FOUND ON F/A PANEL SWITCH IN ON POSITION. RESET SWITCH, SYSTEM OPS NORMAL AS REQUIRED.
CRACK NOTICED AT AFT FUSELAGE INT LEFT CANTED BLKD STA 1178.225 L16L AFT OF HYD S/O VALVE. INSTALLED DOUBLE REPAIR AT AFT FUSELAGE INTERNAL LT CANTED BLKD STA 1178.225 L16L IAW B717 SRM 51-70-11 FIG 201 REPAIR 1, MEASURE 12" X 3".
AFT CARGO DOOR CUT OUT LOWER PAN HAS CORROSION. FOUND CORROSION OUT OF LIMITS TRIMED OUT DAMAGE SECTION AND INSTALLED NEW SECTION AND SPLICES IAW B717 SRM 53-20-15 FIG 201.