SPIRIT AIRLINES, LLC

Operated by Spirit Airlines LLC (per NTSB report)

The airplane’s encounter with turbulence during descent resulting in a serious injury to a flight attendant who was standing at the time of the encounter.

Operated by Spirit Airlines (per NTSB report)

The airplane’s encounter with moderate convective turbulence during descent.

Operated by Spirit Airlines Inc. (per NTSB report)

The captain’s inadvertent aggressive application of the brakes during taxi which resulted in a sudden stop. Contributing to the accident was the flight attendants’ failure to notify the flight crew of the unsecure cabin.

Operated by SPIRIT AIRLINES INC (per NTSB report)

The flight’s encounter with convective turbulence.

Operated by SPIRIT AIRLINES INC (per NTSB report)

The captain’s pitch up input to avoid an overspeed condition, which resulted in a flight attendant falling and fracturing her ankle. Contributing was the airplane’s excessive airspeed during the transition to the automation-managed descent profile.

Operated by Spirit Airlines (per NTSB report)

The ingestion of a bird into the right engine during the takeoff roll caused a fan blade to fracture near the blade platform resulting in high fan blade off loads and engine vibrations sufficient to result in an eventual failure of a fuel tube in the right engine that sprayed fuel onto hot engine cases, igniting an undercowl engine fire and triggering a rejected takeoff.

Operated by Spirit Airlines (per NTSB report)

An abrupt flight control input by the flight crew during descent that caused a flight attendant to fall and fracture their ankle.

Operated by Spirit Airlines Inc (per NTSB report)

A worn component within each engine integrated drive generator (IDG) resulted in the loss of electrical power supplied to several flight deck displays and systems while on approach to landing. The component, a fixed cylinder block, had significant wearing of its reworked brass liners resulting in the IDGs producing a frequency output outside of their specified design limit.

Operated by SPIRIT AIRLINES INC (per NTSB report)

an encounter with convectively induced turbulence associated with towering cumulus clouds during descent.

Operated by Spirit Airlines (per NTSB report)

The airplane’s encounter with severe turbulence.

Operated by SPIRIT AIRLINES INC (per NTSB report)

an inadvertent encounter with convective turbulence that resulted in a flight attendant injury.

Operated by Spirit Airlines, Inc. (per NTSB report)

an encounter with convective turbulence.

Operated by Spirit Airlines (per NTSB report)

The air traffic controller's failure to ensure the runway surface area was clear of vehicles before clearing an aircraft for takeoff. Also causal was the flight crew's decision to initiate a takeoff while the Runway Status Lights (RWSL) Takeoff Hold Lights (THLs) were activated. Contributing to the incident was the lack of a standard procedure for vehicle operators to request runway clearances and resultant "hear back/read back" error between the vehicle operator and the air traffic controller.

Operated by Spirit Airlines (per NTSB report)

A high pressure turbine 2nd stage blade separation due to stress corrosion cracking in the J channel cooling cavity. The failed blade entered the gas path and caused substantial damage to the low pressure turbine. The engine was subsequently left at a high power setting for approximately four minutes, exposing the turbine hardware to temperatures that exceeded the material annealing temperature and resulted in in failure and separation of multiple engine components.

Operated by SPIRIT AIRLINES INC (per NTSB report)

Following a bounced landing, the pilot in command activated his sidestick controller while the first officer was in control of the airplane, which subsequently resulted in the overcontrol of pitch and a tailstrike. Contributing to the circumstances of this accident were the pilot-in-command's failure to properly activate his sidestick takeover push button prior to his remedial action, and the operator's insufficient emphasis on bounced landing recovery techniques and tailstrike avoidance procedures.

Sanction: $97,056 · case closed 2025-11-20

Sanction: $146,500 · case closed 2024-08-12

Sanction: $14,500 · case closed 2023-10-19

Sanction: $2,500 · case closed 2014-07-21

Sanction: $15,000 · case closed 2014-10-15

Sanction: $17,500 · case closed 2014-11-04

Sanction: $17,853 · case closed 2014-06-16

Sanction: $4,000 · case closed 2014-07-16

Sanction: $17,500 · case closed 2014-11-04

Sanction: 11000 · case closed 2012-08-28

Sanction: $44,660 · case closed 2011-04-29

Sanction: $50,000 · case closed 2009-09-11

Sanction: $34,725 · case closed 2009-06-15

Sanction: $30,000 · case closed 2006-08-11

Sanction: $5,000 · case closed 2001-08-08

Sanction: 4,000 · case closed 2005-11-10

Sanction: $6,000 · case closed 2000-09-11

Sanction: $5,500 · case closed 2001-01-25

Sanction: $67,000 · case closed 2000-07-13

Sanction: $30,000 · case closed 1999-11-12

Sanction: $7,500 · case closed 2000-11-28

Sanction: $5,000 · case closed 2002-04-17

Sanction: $30,000 · case closed 2002-09-04

Sanction: $12,500 · case closed 2002-09-09

Sanction: $3,000 · case closed 2003-01-21

Sanction: $7,500 · case closed 2002-09-25

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 4,700 hrs · 2,027 cycles

TAIL STRIKE FINAL REPAIR.-RETURN TO SERVICE IN ACCORDANCE WITH FAR 49.9. AS AUTHORIZED BY THIS REPAIR STATION MANUAL, THE FOLLOWING PERSON CERTIFIES THAT THE WORK SPECIFIED BY THE CUSTOMER/OPERATOR WAS CARRIED OUT IN ACCORDANCE WITH FAA AIRWORTHINESS REGULATIONS AND OPERATORS FAA APPROVED MAINTENANCE PROGRAM (IF APPLICABLE) AND IN RESPECT TO THE WORK PERFORMED THE ARTICLE IS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 12,240 hrs · 5,270 cycles

STRONG SOCK SMELL ON TAKE OFF PACK 1 OFF ISOLATED SMELL-REF TSM 05-50-00-810-831-A C/W AMM 49-00-00-200-814-A NO DEFECT NOTED INSPECTING APU OR FUSELAGE. RAN PACKS IAW AMM 21-00-00 NO ODOR NOTED. LEVEL A DECONTAMINATION C/W.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 27,182 hrs · 12,477 cycles

FLASH LIGHT BY FO RIGHT LEG IS MISSING.-REPLACED FO SIDE FLASH LIGHT IAW EMERG EQUIP DRAWING A320 SPACE FLEX, REV 3

Part: MEGAPHONE — INOPERATIVE (ZONE 900) · airframe 42,957 hrs · 19,695 cycles

FA REPORTS FUMES SMELL AFT CABIN AFTER TAKE OFF-PER TSM 05-50-00-810-831-A DECISION TABLE TYPE 7 CORRECTIVE ACTION. PERFORMED GVI OF APU AND HYD COMPONENTS NO DEFECTS NOTED. LEVEL A DECONTAMINATION PERFORMED AND NO SMELL NOTED. A/C OK FOR SVC. DESCRIPTION OF FUMES / ODOR(S)-UNFAMILAR CHEMICAL,VISIBLE SMOKE / HAZE-NO,FUME / ODOR INTENSITY-MODERATE,MEDICAL ATTENTION REQUIRED-NONE

Part: UNKNOWN — ODOR (CABIN) · airframe 43,350 hrs · 19,844 cycles

DESCENT THROUGH 6000' FT FA CALLED AND REPORTED ODOR. ODOR DISSIPATED AFTER EQRM PROCEDURE. HAD PACK 2 OFF-PERFORMED TSM 05-50-00-810-831-A TYPE 6 LEVEL A. NO DEFECTS NOTED. PERFORMED INSP OF APU IAW AMM 49-00-00-200-814. NO SIGNS OF LEAKAGE. CREW RAN AND ISOLATED ENGS AND PACKS. UNABLE TO DUPLICATE ANY ODORS OR FUMES. AC OK FOR SERVICE. MOC# 111830,

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 4,630 hrs · 2,018 cycles

FWD MEGAPHONE INOPERATIVE. R/R FWD MEGAPHONE IAW SPIRIT AIRLINES EMERGENCY EQUIP DRAWING A321 SPACEFLEX, REV 3

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 28,618 hrs · 12,791 cycles

MEGAPHONE AT L1 DOOR INOPERATIVE. REMOVED AND REPLACED MEGAPHONE AT L1 DOOR IAW SPIRIT A321 EMERGENCY EQUIPMENT DRAWINGS

Part: UNKNOWN — ODOR (CABIN) · airframe 43,302 hrs · 19,821 cycles

BOTH FA WORKING IN AFT CABIN DESCRIBED A STRONG ODOR ON THE GROUND IN BNA AND IN THE FLIGHT ON ARRIVAL INTO MCO. THE ODOR DESCRIBED AS DIRTY SOCKS AND BODY ODOR. ONE FLIGHT ATTENDENT DESCRIBED NOT FEELING WELL AFTER EXPERIENCING THE ODOR-PER TSM 05-50-00-810-831-A IDENTIFIED FUME EVENT AS TYPE 10 MISCELLANIOUS ODOR (AMBIENT ODOR AND HYGIENE ODOR). CANNOT DUPLICATE ODOR. ACCOMPLISHED GVI FOR ENG 1/2 IAW AMM 71-00-00 FOUND NO LEAKS NOTED. ENG 1/2 OIL WITHIN LIMITS IAW AMM 12-13-79. PERF GVI ON APU IAW AMM 49-00-00. NO DEFECTS AND LEAKS NOTED. APU OIL WITHIN LIMITS IAW 49-90-00 PERF ENG 1/2 IDLE RUN IAW AMM 71-00-00. CANNOT DUPLICATE ODOR. A/C OK FOR CONT SVC

Part: SKIN PANEL — DENTED (ZONE 100) · airframe 30,076 hrs · 13,735 cycles

DENT ON EXTERNAL SKIN BTW FR. 27 AND FR. 28 AND BTW STR.42L AND STR. 43L RAF-01 6021562-02 GENERATED (SDR)-PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOCATED BTW FR.27 AND FR.28 AND STR 42L TO STR 43L LOWER FUSELAGE IAW A320 SRM 53-21-11-300-087 REPAIR CATEGORY B INSPECTIONS REQUIRED AT 60,000 FC / 120,000 FH IAW A320 SRM 53-21-11-205-068.

Part: A/C PACK — ODOR (ZONE 100) · airframe 42,879 hrs · 19,660 cycles

DURNING CRUISE @ 380,FA`S IN REAR OF AIRCRAFT SAID THEY SMELLED "DIRTY SOCK"FUMES. PUT PACK 2 OFF AND CLOSED XBLEED,FA`S REPORTED NO CHANGE PACK 2 ON,THEN PACK 1 OFF. FA`S REPOERTED FUMES WERE BETTER AND IMPROVING.CONT`D ON TO KDTW AND WHEN P WAS LESS THAN 1.0 PSI WE SHUT OFF PACK 2 AND OPENED RAM AIR . AFTER RAM AIR OPEN FA`S REPORTED NO FUMES.-PERFORMED LEVEL A DECONTAMINATION OF THE ECS IAW AMM 21-00-00-615-802-A NO CABIN ODOR NOTED.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 41,424 hrs · 19,060 cycles

FWD MEGAPHONE INOP .-R & R FWD MEGA PHONE REF AMM 25-65-51. NO DEFECTS NOTED.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 24,174 hrs · 10,854 cycles

FA MEGAPHONE IS NOT TESTING PROPERLY-R & R MEGAPHONE. REF. AMM 25-65-51.

Part: TRANSDUCER — FAULTY (ENG VIBRATION) · airframe 26,670 hrs · 12,146 cycles

N1 ENGINE PEAK 8.1. HIGH VIBRATION CLB POWER.-R+R VIBRATION TRANSDUCER IAW AMM 77-32-15-00-010-B AND R+R BOTH VIBRATION HARNESS IAW AMM 77-32-43-400-010-A PREFORMED OPS CHECK IAW AMM 77-32-34-710-041-A A/C OK FOR SERVICE

Part: MEGAPHONE — FAULTY (ZONE 200) · airframe 34,578 hrs · 15,509 cycles

FOWARD MEGA PHONE GOING OFF IN FLIGHT -R/R FOWARD MEGA PHONE IAW AMM 25-65-51. OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 25,939 hrs · 11,517 cycles

FA R3 JUMP SEAT FLASHLIGHT INOP-R/R R3 JUMPSEAT FLASH LIGHT BATT IAW SPIRIT AIRLINES EMERG. EQUIP DAWING SPACE FLEX REV 3

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 53,417 hrs · 2,228 cycles

FLT ATTENDANT REPORTS FWD MEGAPHONE INOP -INSTALLED MEGAPHONE IAW AMM 25-65-00 MOC 68056

Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 27,295 hrs · 12,241 cycles

CREW REPORTED L2 DOOR BOTTLE GAUGE NEEDLE ON RED-R/R L2 DOOR ESCAPE-SLIDE INFLATION RESERVOIR REF AMM 25-62-49

Part: UNKNOWN — ODOR (CABIN) · airframe 5,144 hrs · 2,210 cycles

DURING DESCENT FA REPORTS ROW 40 INTERMITENT ODOR OF BURNED WIRES OR ELECTRICAL BURNING. NO SMOKE PRESENT. FOLLOW TSM 05-50-00-810-831-A ID AS LEVEL A, TYPE 10 INSP AFT CABIN FOR BURNT BALLAST AND OTHER ITEMS THAT CAN CAUSE THE ODOR. COULD NOT DUPLICATE THE ODOR. OK TO CONT SERVICE. SUSPECT PAX USED A VAPE.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 5,320 hrs · 2,220 cycles

ZONE-B FWD F/A STATION MEGAPHONE VOLUME KNOB ABSENT-REMOVED AND REPLACED ZONE-B FWD F/A STATION MEGAPHONE IAW NKS DRAWING "A321 NEO EMER EQUIP"

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 34,084 hrs · 15,537 cycles

FA REPORTS AFT FLASHLIGHT PUSH TO TEST BUTTON NOT WORKING. R & R FA REAR GALLEY FLASHLIGHT ASSY IAW AMM 25-65-00.

Part: SHAFT — SHEARED (PUMP) · airframe 20,630 hrs · 9,351 cycles

AIR RETURN, G SYSTEM HYDRAULIC RESVR OVHT. T/S PER TSM 29-11-00-810-802-A. REMOVED NR 1 PUMP FIND SHAFT SHEAR OFF. INSTALLED REPLACEMENT PUMP IAW AMM 29-11-51. OPS AND LEAK CHKD GOOD AT THIS TIME.

Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 25,608 hrs · 11,480 cycles

L2 OVERHEAD SLIDE RESERVOIR INDICATOR INDICATOR IN THE RED.-R/R L2 ESCAPE SLIDE INFLATION RESERVOIR IAW AMM 25-62-49 OK FOR SERVICE. NO FUTHER DEFECTS NOTED

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 17,438 hrs · 7,241 cycles

L2 DOOR JUMPSEAT FA FLASH LIGHT FLASH RED. R & R L2 JUMPSEAT FA IAW SPIRIT AIRCRAFT DRAWING A320 THIS CLEARS MDDR 129905 MOC NOTIFIED PLACARD REMOVED DMI LOGPAGE UPDATED

Part: A/C PACK — CONTAMINATED (NR 2) · airframe 5,946 hrs · 2,498 cycles

FA'S REPORTED FUMES/ODOR IN AFT CABIN DURING DECENT AROUND 8,000', TURNED OFF PACK 2, CLOSED XBLEED PER PROCEDURE, FUMES LESSENED-PERFORMED TSM TASK 05-50-810-831 IAW AMM 21-00-00-615-802-A LEVEL A DECOMTAMINATION OF THE ENVIRONMENTAL CONTROL SYS. FOUND NO EVIDENCE OF CONTAMINATION, A/C OKAY FOR CONT. SVC.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 39,720 hrs · 18,906 cycles

R2 FA FLASHLIGHT INOP, R &R R2 FLASHLIGHT, OPS CHKD GOOD IAW CMM 25-60-13. THIS CLEARS DMI 6004608-1.

Part: APU BAY — CONTAMINATED (ZONE 100) · airframe 5,966 hrs · 2,725 cycles

SUSPECTED FOUL ODOR / FUME EVENT AFT CABIN.-PERFORMED TSM 21-00-00 AND TSM 05-50-00. FROM DESCISION TABLE INSPECTED APU AREA, FOUND AND CLEANED RESEDUAL HYD FLUID. PERFORMED DECONTAMINATION PER AMM 21-00-00. NO LEAKS NOTED WITH HYD SYS. NO ODOR PRESENT AT THIS TIME.

Part: FAN — FAILED (ZONE 100) · airframe 28,417 hrs · 12,701 cycles

DURING FLIGHT WE COULD HEAR A LOUD HUMMING NOISE FROM NOSE SECTION. AFTER LANDING, WE GOT A REAL STRONG SMELL OF BURNING. THIS PERSISTED UNTIL PARKING. AFTER SHUT DOWN WE COULD HEAR A LOUD BUZZING FROM AVIANICS BAY BLOWER FAN WAS SHUT OFF AND SMELL AND SOUND STOPPED ( BLOWER FAN (AVIONICS VENTILATION) VENT AVNCS SYS FAULT NOT DISPLAYED )--

Part: SUPPORT — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORROSION LOWER SUPPORT, STR 23R, FR 66 - 68, IN THE AFT GALLEY AREA. PERFORMED A PERMANENT REPAIR ON THE SUPPORT IAW SRM 53-41-14-300-001,. THIS REPAIR IS CATEGORY A.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORROSION SEAT TRACK -Y1292, BTW FR 12 - 24 IN THE FWD GALLEY AREA, REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWGS D53212367, D53112627, & D53135202.

Part: HINGE FITTING — CORRODED (ZONE 300 ELEV) · airframe 39,950 hrs · 18,324 cycles

CORROSION FOUND ON HINGE FITTINGS, RT ELEVATOR, NR 1, 2, 3, AND 5, REPAIRED IAW SRM 55-26-41-300-010,

Part: HINGE FITTING — CORRODED (ZONE 300 ELEV) · airframe 39,950 hrs · 18,324 cycles

CORROSION FOUND ON LT ELEVATOR HINGE FITTINGS NR 1, 2, 3, AND 5. REPAIRED IAW SRM 55-26-41-300-010.

Part: FITTING — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORRODED CENTER FITTING, BTW FR 66 - 68, STR 23L AFT GALLEY AREA. REPLACED THE CENTER FITTING IAW SRM 51-42-11, AND DWG D53480009.

Part: FITTING — CORRODED (ZONE 100) · airframe 39,950 hrs · 18,324 cycles

CORROSION ON LOWER CORNER CUTOUT, FRAME 28 IN FWD CARGO BAY. REPLACED THE FITTING ON THE LOWER CORNER CUTOUT IAW SRM 51-42-11, & DWG E53230005.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORRODED SEAT TRACK, +Y1162, BTWN FR 68 - 69 IN THE AFT GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53470150, ISSUE S, D53472088, ISSUE G, & D38370318.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORRODED SEAT TRACK, -Y254, BTWN FR 12 - 24, IN THE FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWG D53135166, DWG D53911108, DWG D53212367, AND DWG D53135202.

Part: DUMMY RAIL — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORRODED DUMMY RAIL, Y503.2, BTWN FR 12 - 16, IN THE FWD GALLEY AREA. REPLACED THE DUMMY RAIL IAW SRM 51-42-11, DWG D53112758, DWG D53110984, & DWG D53114410.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORRODED SEAT TRACK, -Y765 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, DWG D53472816, ISSUE F, DWG D57472000, ISSUE A,, DWG D53472093, ISSUE F. REPAIR IS CATEGORY A.

Part: SUPPORT — CORRODED (AFT GALLEY) · airframe 39,950 hrs · 18,324 cycles

CORRODED LOWER SUPPORT, STR 23L BTW FR 66 - 68 IN THE AFT GALLEY AREA. PERFORMED REPAIR INSTRUCTIONS ON THE LOWER SUPPORT IAW SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,950 hrs · 18,324 cycles

CORROSION FLOOR SUPPORT TY254 LOC BTW FR12/ FR24 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW DWG D53135202 ISSUE:A, D53911757 ISSUE:H AND D53212367 ISSUE: DOO.

Part: BOTTLE — DEPLETED (ZONE 800) · airframe 6,774 hrs · 2,775 cycles

R3 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R3 DOOR ASSIST BOTTLE IAW AMM 52-10-00

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 19,698 hrs · 8,319 cycles

FLIGHT ATTENDANT REPORTED AN ODOR OF HUMIDITY & VOMIT, ODOR IN FRONT & AFT CABIN ON FINAL APPROACH, ABOUT 2,000 FT. FOUND APU OVERSERVICED DURING INSPECTION OF THE APU UPON ODOR IN THE CABIN IAW TSM 05-50-00-810-831-A, & AMM 49-00-00-200-811-A , DRAINED APU IAW AMM 49-90-00, CLEANED APU ENGINE, APU ACCESS DOOR AND INTAKE AREA IAW AMM 49-00-60-100-807. SERVICED APU TO PROPER LEVEL . COMPLETED IAW AMM 49-00-00-200-811-A, PARAGRAPH 4. D.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 26,513 hrs · 12,050 cycles

R1 DOOR ASSIST ACTUATOR PRESSURE LOW. SERVICED R1 DOOR ASSIST ACTUATOR PRESSURE IAW AMM 52-10-00.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 6,424 hrs · 2,844 cycles

FWD FA MEGAPHONE FS INOPERATIVE. REPLACED MEGAPHONE IAW AMM 25-65-51.

Part: KNOB — MISSING (MEGAPHONE) · airframe 31,290 hrs · 13,922 cycles

FWD MEGA PHONE MISSING VOLUME KNOB. -R&R FWD MEGAPHONE IN REF W/CMM 25-60-01. OPS CHECK GOOD.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 40,067 hrs · 18,394 cycles

CRACK INDICATION ON RT FRAME 68 STOP FITTING 6 AT AFT GALLEY AREA FROM LOWER INBD HOLE OF DOOR RAF-01 60233854-02 GENERATED. -PERFORMED REPAIR ON RH FRAM 68 LOWER INBOARD HOLE OF DOOR FITTING 6 AT AFT GALLEY AREA IAW SRM 53-41-12-300-008 SRM 53-41-12-300-010, DWG D534800820, & AMM 52-13-31-400-002-A REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500FC (FH NO RELEVANT) SUBSEQUENT INSPECTION AT INTERVAL OF 10700FC IAW SRM 53-41-12-205-009

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 40,067 hrs · 18,394 cycles

CORROSION ON LOWER SILL LOCATED AT FR. 68 STR. 23R IN AFT GALLEY. PERFORMED PERMANENT REPAIR AT THE GALLEY SILL FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A, INSPECTION NOT REQUIRED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,067 hrs · 18,394 cycles

CORRODED SEAT TRACK -Y254, FR 12 - FR 24 FWD GALLEY AREA. REPLACED SEAT TRACK -Y254, FR 12 - FR 24 AT FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, AND DWGS D53111462, D53135202, & D53212367.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,067 hrs · 18,394 cycles

CORROSION SEAT TRACK +Y254, FR 12 - FR 24 AT FWD GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DWG D53112816.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,067 hrs · 18,394 cycles

CORRODED SEAT TRACK, +Y1292, FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, & DWG D53212367, D53111472, D53135202, & D53112627.

Part: HINGE FITTING — CORRODED (ZONE 300) · airframe 40,067 hrs · 18,394 cycles

CORROSION ON HINGE FITTING 1, 2, 3, & 5 LT ELEVATOR. REPAIRED THE HINGE FITTING NR 1, 2, 3, & 5 LT ELEVATOR IAW SRM 55-26-41-300-004.