N910AT

Part: LENS — MISSING (EXIT SIGN) · airframe 46,770 hrs · 32,654 cycles

EXIT SIGN FROM OVERWING/AISLE LOCATION MISSING. MAINTENANCE REPLACED THE EXIT SIGN LENS. (LP #5520022)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,591 hrs · 31,862 cycles

THE LEFT AND RIGHT AFT OVER WING EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY B5-119 IAW AMM 33-51. OPS CHECKED NORMAL.

Part: SIGN — BROKEN (CABIN) · airframe 44,345 hrs · 30,996 cycles

EXIT SIGN IN FIRST CLASS IS BROKEN. RE-SECURED EXIT SIGN PER AMM 33-22.

Part: LONGERON — DAMAGED · airframe 43,813 hrs · 30,622 cycles

LONGERON 17L FOUND DAMAGED BEHIND FUSELAGE SKIN. REMOVED SECTION OF THE LONGERON, FABRICATED A 35 INCH SECTION OF REPLACEMENT LONGERON IAW SRM 53-00-05-2R-2, FIG 201, SHEET 1, AND INSTALLED IAW SRM 53-00-05-2R-2, FIG 201. COMPLIED WITH THE PERMANENT REPAIR IAW SRM 53-00-05-2R, PROCEDURE 2, REPAIR 2.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 43,506 hrs · 30,443 cycles

EMERGENCY EXIT SIGN LENS FOUND LOOSE SECURED THE LENS. OK FOR SERVICE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 42,424 hrs · 29,642 cycles

EMERGENCY EXIT COVER DIFFUSER LENS LOOSE AT LOCATION 602. SECURED THE LOOSE LENS. CHECKED OK.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 42,390 hrs · 29,610 cycles

EMERGENCY EXIT DIFFUSER LENS FOUND UNSECURE. SECURED THE LENS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,294 hrs · 29,540 cycles

ON SERVICE CHECK, FOUND THE EXIT LIGHTS OVER SEAT 20 OUT. REPLACED THE EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51. LIGHTS CHECKED GOOD AT THIS TIME.

Part: DOOR FRAME — TORN (CARGO BAY) · airframe 42,148 hrs · 29,425 cycles

FWD CARGO DOOR FRAME AND SKIN TORN. REPAIRED IAW PRI 557273-14, REV 2, AND ER/A 667273-14, REV ORIGINAL, SECTION 1.

Part: SCUFF PLATE — DAMAGED (FWD CARGO DOOR) · airframe 42,148 hrs · 29,425 cycles

FWD CARGO DOOR SCUFF PLATE DAMAGED. REMOVED AND REPLACED THE SCUFF PLATE IAW ER/A 557273-14, REV 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,148 hrs · 29,425 cycles

FWD CARGO DOOR LOWER FRAME, SKIN DENTED AND CRACKED. REPAIRED IAW PRI 557277-14, REV 1, AND ER/A 557277-14, REV ORIGINAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 42,067 hrs · 29,372 cycles

THE CREW RETURNED THE AIRCRAFT TO THE GATE DUE TO STRONG SULFUR TYPE SMELL AFTER SECOND ENGINE START. AFTER ENGINE SHUTDOWN, SMELL REMAINED AND ACTUALLY GOT STRONGER. CREW REPORTED ODOR OCCURRED AFTER DE-ICING PROCEDURE. FOLLOWED ODI PREVENTION FOR ATA2172. REPLACED COALESCER BAGS AND COMPLETED A DUCT BURNOUT. SYSTEM OPERATIONALLY CHECKS NORMAL AND THE AIRCRAFT RETURNED TO SERVICE.

Part: SPOILER — DELAMINATED (LT WING)

DURING UNSCHEDULED MAINTENANCE CHECK LT INBD SPOILER WAS FOUND DELAMINATED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,525 hrs · 28,196 cycles

CORROSION ON FUSELAGE INTERIOR SKIN AND FINGER DOUBLERS FROM STA 1002 TO STA 1012 BETWEEN LONGERONS 22R AND 26R. BLENDED CORROSION ON INTERNAL SKIN. NOMINAL THICKNESS .063. REMAINING .041. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-01, FIG 103, STA 1005 L25R. REMOVED REPAIR DOUBLER, TRIPLER, AND 2 EA INTERNAL FINGER DOUBLERS IAW SRM 51-41-05. REPAIRED DAMAGED SKIN IAW ER/A 547501-14, REV O. REPAIR DOUBLER, TRIPLER, AND FILLERS INSTALLED ON PRI 547501-14, REV REPETITIVE INSPECTION EVERY 8,000 FLIGHT CYCLES GVI.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,085 hrs · 28,600 cycles

FUSELAGE SKIN STA 1002 L-24R - L-25R. CORROSION REPAIRED BY ER/A 547501-14. ACCOMPLISH SECTION II INSPECTIONS EVERY 8000 CYCLES AFTER SECTION I REPAIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

CORROSION ON LONGERON 25R END CAP AND POSSIBLY ON LONGERON 25R FROM STA 1002 TO STA 1022. REPLACED LONGERON 25R END FITTING AT FS 1002 IAW SRM 51-4-05. NO CORROSION NOTED ON LONGERON 25R FS 1002 TO 1022.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

FUSELAGE AFT CARGO LOWER DOOR JAMB HAS NUMEROUS AREAS OF CORROSION FROM THE AFT LOWER STOP FITTING DOWN TO AND AROUND THE FORWARD LOWER STOP FITTING. REPLACED LOWER DOOR JAMB IAW SRM 53-20-15, REPAIR 7.

Part: FORMER — CRACKED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

LEFT CANTED KEEL FORMERS CRACKED AT STA 674 AND STA 714 ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0127. REPAIRED LT CANTED KEEL FORMERS AT STA 674, 696, & 714 ON OTBD END IAW ER/A 545683-14MA, TAG 6782.

Part: ANGLE — CORRODED (CUSP WEB) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

CORROSION FOUND ON CUSP WEB ANGLE IN BOTH FWD AND AFT LOWER CORNERS OF GALLEY SERVICE DOOR. REPAIRED THE ANGLE IAW SRM 53-00-55 REPAIR 3.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

CORROSION ON LONGERON 23R FROM STA 1002 TO STA 1037. MARKED CHECK LIMITS, REPLACE AS REQUIRED, REF ORNRC 69946-0100-0060. REPLACED LONGERON 23R AT FS 1002 TO FS1043 IAW SRM 51-41-02, PARA D, NOTE 3, 51-41-05, PG 17, NR 8.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

FWD CARGO DOOR JAMB LOWER PAN IS CORRODED AT STOPS, MARKED. REPLACED FWD LOWER CARGO DOOR JAMB PAN SECTION WITH PAN SECTION IAW SRM 51-20-15, REPAIR 6, FIG 201. APPLIED LOG DECAL IAW DPS 900-5-1, NR 04.

Part: SEAT TRACK — CORRODED (BS 200) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

RIGHT SEAT TRACK RBL 56 BS 200 AND END FITTING CORRODED. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 51-40-08 AND DWG 5971185.

Part: CUSP WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

WEB AT BS 160-200 RBL 56 CORRODED BEYOND LIMITS. REPLACED THE WEB IAW ER/A 547495-14. A NEW CUSP WEB AND SPLICE DOUBLER WERE FABRICATED IAW ER/A 547495-14. THE TRIMMED SECTION WAS CHECKED FOR CRACKS USING HFEC IAW NDTSPM 06-10-01 .001 NO DEFECTS FOUND. ALL PARTS WERE ALODINED IAW DPSM 900-2-4-1 NO. 01, PRIMED IAW DPSM 900-3-6 01, AND TOPCOATED IAW AMM 51-10-00-370-803. THE NEW REPAIR WAS INSTALLED IAW ER/A 547495-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

FLOOR PANEL SUPPORT STRUCTURE STA 215, RBL11 CORRODED. BLENDED CORROSION AND CHECKED LIMITS ON FLOOR PANEL SUPPORT STRUCTURE. NOMINAL THICKNESS IS .080". REMOVED .035", REMAINING IS .045". FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 103. FABRICATED NEW FLOOR PANEL SUPPORT STRUCTURE IAW DWG NR 9936534. INSTALLED AT STA 2/5, RBL 11 IAW SRM 51-41-01.

Part: FORMER — CRACKED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

RIGHT CANTED KEEL FORMERS AT STA 674, 696, AND 714 CRACKED ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0130. REMOVED FORMERS ON RT CANTED KEEL AT STA 674, 696, AND 714. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO FORMERS IAW ER/A 545683-14MA. COMPLIED WITH ALL STEPS ON ER/A 545683-14MA. INSTALLED FORMERS IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,523 hrs · 28,195 cycles

RIGHT AFT CARGO SEAT TRACK, AFT OF CARGO DOOR, HAS CORROSION AND CHAFING, MARKED. RIGHT AFT SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK AND MATCHED DRILL TO SAMPLE IAW SRM 51-40-08.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

RIGHT CUSP WEB MEMBRANE, STA 200-218 RBL 56-44. CORRODED BEYOND LIMTS. REPLACED RT CUSP MEMBRANE AT STA 210-218, RBL 56-44 IAW SRM 51-41-02, PAR 2. FABRICATED IAW DWG 9936535. THE NEW PART WAS ALODINED IAW PSM 900-2-4-1, 02. THE WEB WAS THEN PRIMED IAW PSM 900-3-6 NR 01, AND THEN IT WAS PAINTED IAW AMM 51-10-00-370-803. THE NEW WEB WAS THEN INSTALLED IAW SRM 51-41-02, SEC 4, 51-41-08, SEC 7, AND 51-41-05, SEC 8.

Part: SEAT TRACK — CORRODED (BS 256-465) · airframe 40,523 hrs · 28,195 cycles

RIGHT INBD SEAT TRACK X 22 BS 256-465 HAS THREE NOTED AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPAIRED IAW SRM 53-20-52 REPAIR 1 FIG 201.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

CORROSION ON LONGERON 24R AND LONGERON 24R END CAP FROM STA 1002 AND STA 1022. REPLACED LONGERON 24R F/S 1002-1022 + FWD END CAP IAW SRM 51-40-05, PG 17, NR 8, SRM 51-41-02, PARA D. NOTE 3, FASTENERS FROM F/S 1002-1022 + SHEAR TIE AT F/S 1002-1022 LT OPEN TO FACILITATE, PRI 547501-14, NR 0100-0074.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,523 hrs · 28,195 cycles

RT CUSP WEB CRACKED STA 823 BETWEEN 2 RIVETS, RBL 44.5. VIEWED IN LIGHTING HOLE WITH MIRROR. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER IAW SRM 53-00-55, REPAIR NR 4. INSTALLED IAW SRM 51-41-02 AND SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CRACKED (BS 245) · airframe 40,523 hrs · 28,195 cycles

ON INSTALLING OTBD RT SEAT TRACK FOUND CUSP WEB CRACKED FROM EOP TRAVELING INBD TO LIGHTNING HOLE AT BS 245. CUT OUT THE DAMAGE & REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,734 hrs · 26,742 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,883 hrs · 26,106 cycles

DURING SERVICE CHECK BOTH EXTERNAL EMERGENCY ILLUMINATION LIGHTS WERE INOPERATIVE. APPLIED MEL 33-51-02A AND LATER REPLACED EMERGENCY BATTERY. OPERATION THEN CHECKED NORMALLY. LP 7066591.

Part: FRAME — CRACKED (BS 674) · airframe 37,565 hrs · 25,837 cycles

RT FUSELAGE MAIN FRAME CRACKED AT FS 674. REPLACED FRAME AT 674 IAW AMDS 5310-01436-03B. LP 1902809.

Part: FRAME — CRACKED (BS 715) · airframe 37,565 hrs · 25,837 cycles

RT FUSELAGE MAIN FRAME CRACKED AT STA 715. REPLACED FRAME AT STA 715 IAW AMDS CARD 5310-01436-03B. LP 1902812.

Part: FASTENER — DAMAGED (BS 1152) · airframe 38,177 hrs · 26,370 cycles

FUSELAGE, DAMAGED FASTENER AT BS 1152, LONGERON-2L AND 3L /527412-14.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,750 hrs · 24,358 cycles

LEFT AFT LOWER TAIL CONE EMER LIGHT INOPERATIVE. R & R CHARGER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,750 hrs · 24,358 cycles

TAIL COMPARTMENT AFT HAND RAIL EMER LIGHT BULB INOPERATIVE. LAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,750 hrs · 24,358 cycles

AFT LOWER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY LIGHT SIGN ASSEMBLY AT AFT BULKHEAD DOOR CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY LIGHT SIGN ASSEMBLY AT R1 DOOR CRACKED. R & R SIGN IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

ROW 1 ABC, EMER EXIT SIGN CRACKED. R & R SIGN IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY EXIT LIGHT LENS ABOVE R2 DOOR CRACKED. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY EXIT LIGHT LENS ABOVE L1 DOOR CRACKED. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY EXIT LIGHT LENS ABOVE R1 DOOR CRACKED. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY EXIT LIGHT LENS ABOVE L2 DOOR CRACKED. R & R LENS IAW MM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 35,757 hrs · 24,363 cycles

MAIN CABIN FLOOR PANEL 221JF DAMAGED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 35,757 hrs · 24,363 cycles

MAIN CABIN FLOORBOARD PANEL 211ALF DAMAGED. R & R PANEL IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT AILERON) · airframe 35,757 hrs · 24,363 cycles

RIGHT WING AILERON OTBD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,757 hrs · 24,363 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, RBL 22. REPAIRED SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,757 hrs · 24,363 cycles

SEAT TRACK CORRODED BETWEEN BS 898 TO 1022, RBL 54. R & R SEAT TRACK IAW SRM.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 35,757 hrs · 24,363 cycles

EMERGENCY EXIT PULL HANDLE LOOSE AT BS 1140, LONGERON 27L. SECURED HANDLE IAW MM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,757 hrs · 24,363 cycles

LONGERON CRACKED AT BS 1045, LONGERON 2L. R & R LONGERON IAW SRM.

Part: HANDSET — FAULTY (CABIN) · airframe 34,492 hrs · 23,555 cycles

ELECTRICAL SMOKE ODOR IN AFT LAVATORY, AFT FLIGHT ATTENDANT`S HANDSET. R & R HANDSET IAW AMM.

Part: CONNECTOR — DISCONNECTED (EVAC SLIDE) · airframe 34,402 hrs · 23,494 cycles

R1 DOOR EMERGENCY EVAC SLIDE Y CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 33,516 hrs · 22,939 cycles

BUSINESS CLASS CEILING EMERGENCY EXIT SIGN MISSING. INSTALLED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 32,571 hrs · 22,374 cycles

OVERHEAD BUSINESS EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT FUSELAGE SKIN HAS CORROSION AT STA 880 STR 28R. REPAIR IAW B717 SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN RIGHT FLOOR CUSP WEB CRACKED AT FS 653 RBR 60. REMOVED DAMAGED DIM 1 1/2" X 3" AT STA 653 CUSP WEB IAW B717 SRM 53-00-55 FIG 203. FABRICATED DOUBLER DIM 6 1/2"X 5 1/2" FROM 7075.T6.032 PO 90015254 IAW B717 SRM 51-40-08 & 53-00-

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR LEFT SIDE CUSP WEB CRACKED AT FS 676 LBL 46. CUT OUT DAMAGE DIM 4.5"X8" AND FAB REPAIR USING P/N 7075T6 .020" PO 90015962 DIM 4.5"X 8" (FILLER) DOUBLER USING 7075T6.032" PO 90014133 DIM 6.5" X 12", ALODINED + PRIMED P

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,943 hrs · 21,986 cycles

AFT ATT SEAT EMERGENCY FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED AFT ATT SEAT FWD EMERGENCY FLASHLIGHT BATTERY IAW B717 25-60-01. OPERATIONAL CHECK COMPLIED WITH. GOOD IAW B717 M/M 25-60-01

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR RIGHT CUSP WEB CRACKED AT FS 674 RBL 46. CUT OUT AREA 36"X 14.9", FABRICATED REPAIR CUSP WEB DIM 36"X14.9 FROM 7075T6.020 PO 90015141, DOUBLER DIM 15.5"X3. 5/8" FROM 7075T6 .032 PO 90015519 IAW B717 SRM 53-00-55 REPAIR

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

INTERNAL FUSELAGE LEFT STA 200 L15L WEB SUPPORT CRACKED. CUT OUT DAMAGE AREA LEFT STA 200 L15L, FABRICATE REPAIR DOUBLER FROM 7075T6 0.50" PO 900143440 FILLER FROM 7075T6 0.040" PO 90014579 AND INSTALLED IAW B717 SRM 53-10-15 51-41-02,

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN ABOVE WING CENTER SECTION LBL 25 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT LBL 25 STA 737 P/N 3925819-1, PO 2300968 IAW B717 SRM 51-41-05, LOCATED & DRILLED NEW SUPPORT IAW B71

Part: BEAM — CRACKED (L1 DOOR) · airframe 31,943 hrs · 21,986 cycles

L1 DOOR UPPER BEAM IS CRACKED AT AFT CORNER. REMOVED FITTING FOR ACCESS AT L1 DOOR UPPER BEAM. FABRICATED DOUBLER REPAIR IAW B717 SRM 51-10-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

RIGHT NLG STRUT DOOR, AFT HINGE CUTOUT CRACKED. STOP DRILLED CRACK IAW B717 SRM 53-10-01 REPAIR 6 FIG 201. VERIFIED STOP DRILLED CRACK IAW B717 NDTM PT. 6 06-10-01. FABRICATED DOUBLER FROM 2024T3 .071 P/O 90013533 IAW B717 SRM 53-10-01 REPAIR 6 FIG 201 51-40-08. ALODINED & PRIMED DOUBLER IAW B717 SRM 51-10-04. INSTALLED DOUBLER IAW B717 51-41-02 & 51-41-05. TOP COATED IAW B717 AMM 51-10-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

FORWARD PIT CARGO DOOR JAMB HAS CORROSION IN A FEW AREAS. FABRICATED SPLICES 2024T3 P/O 90015407 LOCATED & DRILLED NEW PAN IAW B717 SRM 51-40-08 & 53-20-15 REPAIR 6.

Part: BEAM — CRACKED (L1 DOOR) · airframe 31,943 hrs · 21,986 cycles

L1 DOOR UPPER BEAM IS CRACKED AT FWD CORNER. REMOVED FITTING FOR ACCESS AT L1 DOOR UPPER BEAM. FABRICATED DOUBLER REPAIR IAW B717 SRM 51-10-04.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN ABOVE WING CENTER SECTION LBL 45 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT TRACK AT FS 737 LBL 45 P/N 3925812U1 PO 790191430 IAW B717 SRM 51-41-02, 51-41-05, 51-40-08, 51-10-0

Part: ANGLE — CRACKED (L1 DOOR) · airframe 31,943 hrs · 21,986 cycles

L1 DOOR INTERIOR HAS CRACKED VERTICAL ANGLE JUST AFT OF DOOR HANDLE. REMOVED VERTICAL ANGLE L-1 DOOR STA 180 AND INSTALLED IAW B717 SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN - CUSP WEB HAS CORROSION AT STA 503-522 RIGHT SIDE. REMOVED CORROSION AT STA 503-522 RIGHT CUSP WEB IAW B717 SRM 51-10-04. ORIG MAT .020 REMAINING .000 LOSS OF .020 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103. REMOVED DAM

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN - CUSP WEB HAS CORROSION AT STA 446-465 RIGHT SIDE. REMOVED CORROSION AT STA 446-465 CUSP WEB IAW B717 SRM 51-10-04. ORIG MAT .020 REMAINING .000 LOSS OF .020 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103 CUT OUT DAMAGE DIM 1" X 4.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN ABOVE WING CENTER SECTION, RBL 45 SEAT TRACK SUPPORT FITTING IS CRACKED AT LOWER LEG FS 737. REMOVED AND REPLACED SUPPORT SEAT TRACK FROM P/N 392581U1 PO 90014681 AT FS 737 RBL 45 IAW B717 SRM 51-41-02, 51-41-05, 51-40-

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222PF AT STA 541 TO STA 617 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222PF AT STA 541 TO STA 617 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222 PF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 ACF AT STA 696 TO STA 737 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222ACF AT STA 696 TO STA 737 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X40" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222ACF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR PANELS 222 AVF AT STA 889 TO STA 954 RBL 22 TO RBL 44 DELAMINATED. REMOVED & REPLACED FLOOR PANEL PER SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT ACCESSORY COMPARTMENT - AT STA 1133 LONG 2R CRACKED. REPAIR LONGERON & SPLICE IAW B717 SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222LF AT STA 465TO STA 541 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222LF AT STA 465 TO STA 541 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222LF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 RF AT STA 541 TO STA 636 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222RF AT STA 541 TO STA 636 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222RF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 ATF AT STA 889 TO STA 954 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222ATF AT STA 889 TO STA 954 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X 65" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222ATF IAW B717 AMM 53-21-01.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT ACCESSORY COMP - EMERGENCY EXIT PULL - LWR BRACKET CRACKED. REMOVED BRACKET AT THE AFT ASSY COMP EMERGENCY EXIT HANDLE IAW B717 SRM 51-41-02, FABBED BRACKET FROM 2024-T3 .040 PO# 90015161, 2" X 6" IAW B717 SRM 51-30-08, BAC DRAWING 9951070 AND BAC MESSAGE #2 2-13AD ENG, ALODINED & PRIMED IAW B717 SRM 51-10-04, INSTALLED BRACKET / CLIP IAW B717 SRM 51-41-02

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222BF AT STA 389 TO STA 465 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222BF AT STA 389 TO STA 465 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" OAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222BF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 AAF AT STA 674 TO STA 696 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222AAF AT STA 674 TO STA 696 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002 TYPE 3 PO #79019147 DIM: 21"X22" IAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222 AAF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 ABF AT STA 674 TO STA 696 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222ABF AT STA 674 TO STA 696 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X22" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222ABF IAW B717 AMM 53-21-01.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT PIT RIGHT SIDE INTERNAL REPAIR FINGER DOUBLER HAS CORROSION AT FS 1010 LONGERON 24R. REMOVED CORRODED FINGER DOUBLER AND FABRICATED NEW FINGER DOUBLER FROM 7075-T6 .025 PO 90015477 B717 SRM 53-03-01 FIG 213 51-10-04 & 51-41-08 AND INSTALLED

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

LEFT FRAME HAS A CRACK IN RADIOS BELOW FLOOR LEVEL. REMOVED AND REPLACED FRAME AT LEFT FS 715. FRAME P/N SA 95530034-11 PO 2300928 IAW B717 SRM 51-41-05 & 51-41-02, 51-40-08.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222FF AT STA 408 TO STA 446 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222FF AT STA 408 TO STA 446 RBL 22 TO RBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X38" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222FF IAW B717 AMM 53-21-01.

Part: RUB STRIP — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

WING TO BODY FAIRING RUB STRIP HAS CORROSION UNDER FILLET PANEL 160SL 26-013. REMOVED CORRODED RUB STRIP UNDER FILLET FAIRING 150SL IAW B717 MM 53-53-01. TREATED AND PRIMED NEW RUB STRIP IAW B717 SRM 51-10-04. INSTALLED SERVICEABLE RUB STRIP UNDER

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 WF AT STA 313 TO STA 389 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED PANEL 222WF AT STA 313 TO STA 389 RBL 22 TO 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222WF IAW B717 AMM 53-21-0.1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 JF AT STA 465 TO STA 541 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222JF AT STA 465 TO STA 541 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222 JF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 AEF AT STA 696 TO STA 737 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 AGF AT STA 737 TO STA 813 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED PANEL 222AMF AT STA 813 TO STA 889 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM P/N BZZ7002TYP3 PO 790191470 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 AND INSTALLED FLOOR PANEL 222AMF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 UF AT STA 313 TO STA 389 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222UF AT STA 313 TO STA 389 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO 79019147 DIM: 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222UF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 AMF AT STA 813 TO STA 889 LBL 22 TO LBL 44 IS DELAMINATED. REMOVED FLOOR PANEL 222AGF AT STA 737 TO STA 813 LBL 22 TO LBL 44 IAW B717 AMM 53-21-01, FABRICATED FLOOR PANEL FROM: BZZ7002TYPE3 PO #79019147 DIM: 21"X76" OAW B717 SRM 53-20-50 REPAIR 3 & INSTALLED FLOOR PANEL 222 AGF IAW B717 AMM 53-21-01.

Part: CONNECTOR — CORRODED (RT AILERON) · airframe 31,943 hrs · 21,986 cycles

RIGHT WING AILERON ROTARY TRANSDUCER CONNECTOR CORRODED. REMOVED AND REPLACED AILERON ROTARY TRANSDUCER CONNECTOR ON RIGHT WING IAW B717 WDM 22-12-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 AHF AT STA 737 TO STA 813 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,943 hrs · 21,986 cycles

MAIN CABIN FLOOR 222 APF AT STA 813 TO STA 889 RBL 22 TO RBL 44 IS DELAMINATED. REMOVED & REPLACED PANEL PER SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT PIT BILGE, LONGERON 28R HAS AREAS OF CORROSION FS 958 TO FS 927. REMOVED CORROSION AT STA 908 INTERCOSTAL IAW B717 SRM 51-10-04. ORIG MAT .063 REMAINING .039 LOSS OF .024 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103. FABRICATED NEW INTERCOSTAL IAW B717 SRM 51-40-08 & SMALL CONTROL PO 2040744 FROM 7075 .063 P/O 9957704. HEAT TREATED TI 7075T6 IAW FASER # 2-37153-801 REV A. ALODINED, PRIMED, TOP COATED IAW B717 SRM 51-10-04. INSTALLED INTERCOSTAL IAW B717 SRM 51-41-02 & 51-41-05 & FAY SEALED PARTS IAW B717 SRM 51-20-05, DIM OF INTERCOSTAL (5"X19")

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 31,943 hrs · 21,986 cycles

LEFT WING L/E TO BODY ATTACH ANGLE CRACKED AT FS 636. LOCATED & DRILLED NEW STRAP P/N 5919110U97 P/O 790191630 IAW B717 SRM 51-41-08. ALODINED STRAP IAW B717 SRM 51-10-04. INSTALLED NEW STRAP IAW B717 SRM 51-40-02. PERFORMED SATISFACTORY ELECTR

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 31,943 hrs · 21,986 cycles

RIGHT WING L/E TO BODY ATTACH ANGLE IS CRACKED AT FS 636, LONGERON 20R. LOCATED & DRILLED NEW STRAP P/N P/O 2229015 IAW B717 SRM 51-40-08. ALODINED STRAP IAW B717 SRM 51-10-04, INSTALLED NEW STRAP IAW B717 SRM 51-40-02. PERFORMED ELECTRICAL BOND

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

AFT PIT BILGE AREA, LOWER SHEAR TIE CORRODED AT FS 1038 RBL 2. REMOVED CORROSION SHEAR TIE FABRICATED NEW IAW B717 SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 31,943 hrs · 21,986 cycles

C2 CARGO DOOR JAMB LOWER PAN CORRODED ALONG EXTERIOR SIDE STA 954 TO STA 994 88-2. REMOVED CORROSION C2 CARGO DOOR PAN IAW B717 SRM 51-10-04. ORIG MAT .050 REMAINING .022 LOSS OF .028 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103. REMOVED WEB. LOCATED & DRILLED PAN P/N J060228 P/O 2465941 & SPLICES P/N J060228U19 P/O 2300930 & P/N J060228U21 P/O 2300930 IAW B717 SRM 51-40-08 & 53-20-15 REPAIR 7 FIG 201. ALODINED, PRIMED & TOP COAT ALL PARTS IAW B717 SRM 51-10-04. FAY SEALED ALL PARTS IAW B717 SRM 51-40-05. INSTALLED PAN, SPLICES, WEB & 3 (EA) GUSSETS IAW B717 SRM 51-41-02, 51-41-05 & 53-20-15 REPAIR 7 FIG 201 MDDR 239754 ASSIGNED.

Part: COVER — MISSING (CABIN) · airframe 30,447 hrs · 20,984 cycles

RT EEPLS COVER MISSING AT ROW 10. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN)

COVER ON EMERGENCY PATH LIGHTING ON 10D IS MISSING. INSTALLED LENS IAW AMM 33-51-04. OPS CHECK OF EMERGENCY LIGHTING SYSTEM NORMAL IAW AMM 33-51-00.

Part: PIN — PULLED (EVAC SLIDE)

RE-INSPECTED STW 221873 ON R-1DOOR SLIDE FOUND PIN PULLED OUT OF SLIDE. REMOVED AND REPLACED R-1 DOOR SLIDE PER AMM 25-60.

Part: BATTERY — DISCHARGED (CABIN)

ROW 1, 2, 3 AND 10 SEAT EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED BATTERIES AND POWER SUPPLY PER B717 AMM 33-51-03 POWER SUPPLY IS BS-118 AND OPS CHECKED GOOD PER AMM 33-51-00.

Part: SOCKET — DEFECTIVE (CABIN)

ROW 20 THROUGH 24 EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LT SOCKETS AT ROW 22DEF, B5-118 AND 119 EMERGENCY LT BATTERY PACKS AND B5-118, 119 BATTERY CHARGERS - OPS CHECKS GOOD. (REF B717 AMM 33-51)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS OUT AT ROWS 20-24 AND LOWER EXIT LIGHTS ON OVERWING EXITS. REMOVED AND REPLACED BATTERY SUPPLY ASSY IAW B717 33-51 LOCATED AT ROWS 3 AND 24. OPS CHECKED GOOD IAW B717 33-51.

Part: SLIDE — UNSERVICEABLE (TAILCONE)

TAIL CONE SLIDE S/N 1477 INFLATE BOTTLE PRESSURE INDICATION BELOW NORMAL. REMOVED AND REPLACED TAIL CONE SLIDE REF B717 AMM 25-61 P/N 64210-103 OFF 1417 ON 1231.

Part: LANYARD — BROKEN (EVAC SLIDE)

GIRT BAR LANYARD BROKEN ON FWD ENTRY DOOR. REMOVED AND REPLACED L-1 DOOR EVAC SLIDE LANYARD REF AMM / 25-61.

Part: ANGLE — CORRODED (FUSELAGE)

PASSENGER ENTRANCE DOOR JAMB ANGLE, STA 198, LBL 55, CORROSION. ACCOMPLISHED DOOR JAMB ANGLE REPLACEMENT PER B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 167, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FITTING — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT FRAME CLIP, STA 1152, LONG L2L, CRACKED. ACCOMPLISHED FRAME CLIP REPLACEMENT PER EA 17-53-03019IR.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

GALLEY ENTRANCE AFT GIRT BAR ATTACH FITTING, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE, BETWEEN GIRT BAR ATTACH FITTINGS STRAP PANEL, CORROSION. ACCOMPLISHED STRAP PANEL REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 20, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR SUPPORT ANGLE, STA 148 TO 158, LONG L18R, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-01.

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE DOOR JAMB GAP PANEL, STA 148 TO 158, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: REPAIR — DETERIORATED (THRUST REVERSER)

NR 1 ENGINE, TR DEFLECTOR DOOR ACOUSTIC LINER, PREVIOUS REPAIR DETERIORATED. ACCOMPLISHED ACOUSTIC LINER DOUBLER REPAIR PER B717 SRM 51-40-02 AND B717 SRM 54-30-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 207, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TWO CABIN FLOOR SUPPORTS, STA 200, BL 0 TO LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORTS REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 256, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 41, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 240, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: LIGHT — DAMAGED (CABIN)

ROW 10 FORWARD EMERGENCY LIGHT ASSEMBLY DAMAGED. REPLACED EMERGENCY PATH LIGHT ASSEMBLY, AND OPS CHECK GOOD PER AMM 33-51-04.

Part: LENS — MISSING (CABIN)

SEAT 19DEF EMERGENCY EXIT LIGHT LENS MISSING AND BOTH BROKEN. INSTALLED NEW BULBS 2 EACH AND LENS COVER ON SEAT 19DEF EMERGENCY EXIT LIGHT IAW B717 AMM 33-51, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

OVERWING EXIT EMERGENCY LIGHT ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY IAW B717 MM 33-51-00, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CEILING EMERGENCY LIGHT AT ROWS 27, 28 INOP. RELAMP, NO HELP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY ASSY IAW AMM 33-51-03, OPS CHECK NORMAL IAW 33-51-00.

Part: LENS — MISSING (CABIN)

RED ESCAPE PATH LIGHT LENS MISSING FROM SEAT SIDE 21D. INSTALLED E-PATH LIGHT LENS PER B717 AMM 33-51.

Part: LENS — MISSING (CABIN)

SEAT 1D EMERGENCY LIGHT COVER MISSING. INSTALLED MISSING EMERGENCY LIGHT LENS. OK FOR SERVICE. REF MM 33-51.

Part: FUSE — UNSERVICEABLE (CABIN)

EMERGENCY LIGHTS ABOVE PASSENGER DOOR AND GALLEY SERVICE DOOR INOP (LIGHTS IN CEILING). REMOVED AND REPLACED FUSES ON BATTERY PACKS B5-259 & B5-235 REF CMM 33-50-02. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOP AT SEAT ROWS 1-3. REMOVED & REPLACED EMERGENCY BATTERY & CHARGER IN REF TO AMM 33-51. OPS CHECK GOOD AT THIS TIME. LOCATION B5-118.

Part: COMPRESSOR — STALLED (LT ENGINE)

LEFT ENGINE COMPRESSOR STALLED AND TGT REDLINED ON SHUT DOWN. TGT-1180 C. EMERGENCY LANDING MADE. REMOVED AND REPLACED NR 1 ENG ON W/O 190329 TASK CARD 603. AUTO LAND ACCOMPLISHED ON W/O 190329 TASK CARD 625.

Part: FRAME — CORRODED (BS 870)

AFT CARGO COMPARTMENT BILGE FRAME 870 FWD & AFT FACE HAS CORROSION AT STR 30. INSTALLED "Z" FRAME REPAIR AT LOWER CARGO COMPARTMENT FRAME STA 870 BETWEEN LONG. 27 LT & 27 RT PER B717 SRM 53-20-07 REPAIR 3 FIG 201.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR LOWER JAMB HAS CORROSION. INSTALLED NEW PAN SECTION AND SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE ON SEAT ROWS 20 FED TO 25 FED. REPLACED BATTERY SUPPLY ASSY'S.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP AT SEATS 21DEF THROUGH 25DEF. REMOVED AND REPLACED BATTERY PACKS S3-388 AND S3-384, OPS CHECK GOOD.

Part: SKIN — DENTED (BS 212)

DENT ON RIGHT SIDE OF FUSELAGE AFT OF R1 DOOR STA 212 53-00-01 REPAIR 2. INSTALLED DOUBLER REPAIR AT RIGHT SIDE OF FUSELAGE AFT OF R1 DOOR STA 212 AS PER B717 SRM.

Part: SKIN — DENTED (BS 218-246)

DENT APPROX 6 INCHES UP FROM L18 AND 8 INCHES AFT OF STA 218. INSTALLED DOUBLER REPAIR STA 218 TO STA 246 AS PER B717 SRM 53-00-01 REPAIR NR 6.

Part: SKIN — DENTED (FUSELAGE)

DENT ON RT SIDE AFT OF R1 DOOR STA 212 BETWEEN LONG 15 AND 16 RT. INSTALLED FLUSH REPAIR PER B717 SRM 53-00-01 FIG 204 REPAIR 2.

Part: SKIN — DENTED (BS 237 L24R)

DENT FOUND ON LWR FUSELAGE RIGHT SIDE AFT OF FWD DRAIN MAST. INSTALLED DOUBLER REPAIR AT RIGHT SIDE AFT OF FWD DRAIN MAST AS PER B717 SRM 53-00-01 FIG 204.

Part: LINE — LEAKING (HYD SYSTEM)

ON APPROACH INTO PHF, RIGHT HYD SYS LOW ALERT ON EAD FOLLOWED QRH EMERGENCY DECLARED, NORMAL LANDING OCCURRED WITH GEAR DOORS UP. FOUND RT O/B SPOILER ACTUATOR LINES LEAKING AT ACTUATOR B NUT SLEEVE. REPLACED BOTH LINES REF 20-10, RTS 27-60, SERVICED HYD SYS & LEAK CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

LOWER EMERGENCY LIGHTS FROM 1-10 DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY IAW 717 MM 33-51, OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERG LIGHTS AT ROWS 123&10 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERG LIGHT BATTERY SUPPLY ASSY AND REMOVED AND REPLACED PROXIMITY LIGHT ASSY ROW 10 FWD IN REF TO MM 33-51

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ROW 1 TO 10 EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY FLOOR AISLE LIGHT ASSY AT ROW 5. OPS CK GOOD. REMOVED AND REPLACED B5-118 BATTERY PACK.