PIEDMONT AIRLINES

Operated by Piedmont Airlines (per NTSB report)

an encounter with convective turbulence during descent.

Operated by Piedmont Airlines (per NTSB report)

An inadvertent encounter with convective turbulence.

Operated by PIEDMONT AIRLINES INC (per NTSB report)

the airplanes collision with geese during the takeoff roll.

Operated by Piedmont Airlines (per NTSB report)

an inadvertent encounter with several birds during approach that resulted in substantial damage to the airplane.

Operated by Piedmont Airlines (per NTSB report)

the frozen left main landing gear (MLG) uplock roller due to lack of lubrication and the uplock latch that had worn beyond acceptable tolerances, which prevented the flight crew from extending the left MLG using the alternate extension system. Contributing to the accident were the operator's improper maintenance practices, which did not detect the lubrication issue with the roller and the wear of the latch.

Operated by Piedmont Airlines Incorporated (per NTSB report)

The inadequate communication among ground crew personnel, which resulted in the airplane’s collision with a deice truck.

Operated by PIEDMONT AIRLINES INC (per NTSB report)

An in-flight encounter with convective clouds resulting in moderate turbulence and serious injury to a flight attendant.

Operated by Piedmont Airlines (per NTSB report)

The mechanical overload of the nosewheel steering links for undetermined reasons, which resulted in nose landing gear rotation and its subsequent wedging within the wheel well structure.

Operated by PIEDMONT AIRLINES (per NTSB report)

FAILURE OF THE LINE MECHANIC, A CHECK MECHANIC, AND FIRST OFFICER TO IDENTIFY AND REMOVE THE WHEEL CHOCK FROM THE WHEEL WELL DURING THE REQUIRED INSPECTIONS.

Operated by PIEDMONT AIRLINES (per NTSB report)

THE FIRST OFFICER DID NOT PROPERLY EVACUATE THE AIRPLANE.

Operated by PIEDMONT AIRLINES (per NTSB report)

Operated by PIEDMONT AIRPORT (per NTSB report)

Operated by PIEDMONT AIRLINES (per NTSB report)

Sanction: $50,000 · case closed 2023-05-18

Sanction: $20,000 · case closed 2022-03-30

Sanction not stated · case closed 2013-09-26

Sanction not stated · case closed 2013-09-26

Sanction not stated · case closed 2013-09-26

Sanction: $18,500 · case closed 2011-06-28

Sanction: $35,000 · case closed 2010-01-14

Sanction: $10,000 · case closed 2010-01-14

Sanction: $26,000 · case closed 2007-08-15

Sanction: $23,000 · case closed 2007-08-15

Sanction: $12,000 · case closed 2007-10-29

Sanction: $42,500 · case closed 2010-04-22

Sanction: 7,000 · case closed 2005-12-14

Sanction: $25,000 · case closed 2006-05-11

Sanction: $5,000 · case closed 2001-11-20

Sanction: $9,500 · case closed 2001-08-03

Sanction: $11,500 · case closed 2001-08-03

Sanction not stated · case closed 2001-04-25

Sanction: $5,000 · case closed 2001-04-25

Sanction: $1,100 · case closed 2001-08-08

Sanction: $4,400 · case closed 2000-08-02

Sanction: $13,000 · case closed 2000-05-31

Sanction: $3,500 · case closed 2001-04-17

Sanction: $8,500 · case closed 1999-06-30

Sanction: $7,000 · case closed 2000-04-04

Sanction: $18,500 · case closed 1999-11-18

Sanction: $9,000 · case closed 1999-04-09

Sanction: $21,500 · case closed 1999-10-13

Sanction: $750 · case closed 2002-06-12

Sanction not stated · case closed 2003-04-07

Sanction not stated · case closed 2003-04-07

Sanction not stated · case closed 2003-04-07

Part: INDICATOR — FLUCTUATES (ZONE 500 FUEL) · airframe 49,962 hrs · 46,695 cycles

LEFT FUEL QTY FLUCTUATED +/- 1000 LBS WITH LT TANK INDICATING, 5,000 LBS & STABILIZED AT 4,500 LBS IN FLT. MEL 17AUG26 19:47 CLT B22920 28-9 WING TANK FUEL QTY IND EICAS

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 56,475 hrs · 54,304 cycles

LH FWD EXT EMER LITGHT WILL NOT ILUMINATE. R & R EMER LIGHT ASSY IAW AMM 33-50-10-000/400-801-A. OPS CHECK GOOD, OK FOR SERVICE

Part: PANEL — FAULTED (ZONE 100) · airframe 50,680 hrs · 47,974 cycles

ON CLIMB OUT BLEED 2 LEAK EICAS MSG. REMOVED RT PACK PANEL AND RT PACK VALVE PANEL FOR VISUAL INSPECTION OF BLEED LINES. NO DEFECTS NOTED DURING INITIAL INSPECTION. REINSTALLED PANELS WITH RETAINED HARDWARE.

Part: DOOR — OBSTRUCTED (ZONE 800) · airframe 54,942 hrs · 52,698 cycles

SERVICE DOOR INDICATED OPEN DURING TAKEOFF. CONDUCTED GVI OF SERVICE DOOR. NO DEFECTS NOTED ON EXTERIOR. IN INTERIOR, FOUND RED SAFETY ROPE CAUGHT IN DOOR. REMOVED ROPE. DOOR INDICATES CLOSED. ACFT OK FOR SERVICE AT THIS TIME

Part: RADAR — ABNORMAL (WX SYS) · airframe 48,968 hrs · 45,626 cycles

WX RADAR FAILED IN FLIGHT. FACT 12AUG26 02:49 PHL R+R WX RADAR IAW AMM 34-42-01. OPS CHECK GOOD IAW AMM 34-42-00. A/C OK FOR SERVICE AT THIS TIME

Part: NONE — NONE (NONE) · airframe 44,527 hrs · 40,653 cycles

SEVERE TURBULENCE IN FLIGHT. HSV INSPECTED AIRCRAFT FOR SEVERE TURBULENCE IAW AMM 05-50-27. NO DEFECTS OR FAULTS NOTED. OK FOR SERVICE. HSV CLOSE AIRCRAFT OVERSPEED AT 7,000FT FOR 5 SECONDS (CREW UNABLE TO PROVIDE ACCURATE AIRSPEED DUE TO SEVERE TURBULENCE) INSPECTED AIRCRAFT FOR OVERSPEED INSPECTION PERFORM AMM 05-50-04, NO DEFECTS OR FAULTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: WINDOW — NO DISCREPANCY (ZONE 200) · airframe 45,271 hrs · 41,112 cycles

ABORTED T/O AT 60 KTS DUE TO F/O DV WINDOW NOT SECURED CLOSED. INSP'D F/O DV WINDOW AND OPS CHECKED DV WINDOW. NO DEFECTS NOTED. OK FOR SERVICE.

Part: WIRE — BROKEN (ZONE 200) · airframe 55,622 hrs · 54,001 cycles

SERVICE DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE FOUND BROKEN WIRE ON EXTERNAL SERVICE DOOR LIGHT. REPAIRED IAW SWPM 20-21-00 PERFORMED OPS CHECK IRT 33-50-00-700-801-A OPS CHECK GOOD OK FOR SERVICE.

Part: DUCT — LEAKING (NR 1 ENGINE) · airframe 50,757 hrs · 46,953 cycles

BLEED 1 LEAK IN FLT. R & R ENGINE 1 Y-DUCT IN PYLON. NO FIX. FOUND OVER-WING COUPLING IN BLEED DUCT MISSING INTERNAL O-RING (BLEED SLEEVE) COUPLIN REMAINS DETACHED.

Part: INVERTER — ABNORMAL (ZONE 200) · airframe 45,347 hrs · 42,323 cycles

FWD FLOOR EMERGENCY LIGHT INOP AT FLOORBOARD 231GF. R & R FWD EMERGENCY LIGHT INVERTER IAW AMM33-50-11-04

Part: CLAMP — LEAKING (NR 1 ENGINE) · airframe 50,757 hrs · 46,953 cycles

BLEED 1 LEAK IN FLIGHT, ENGINE BLEED SYSTEMS. TROUBLESHOT BLEED 1 SYSTEM, FOUND CLAMP BETWEEN HSV AND CHECK VALVE TO BE LEAKING. REINSTALLED CLAMP AND TORQUED IAW AMM 36-11-02. OPS CHECKED GOOD. ACFT OKAY FOR SERVICE. RETURNED ACFT TO NORMAL CONFIGURATION.

Part: WARNING MESSAGE — FALSE INDICATION (FUEL QTY) · airframe 50,757 hrs · 46,953 cycles

DURING CRUISE RT TANK INDICATED FROM 2000LB TO 800LB WITH FUEL IMBALANCE MESSAGE. INDICATION RETURNED TO NORMAL IN DESCENT. INSPECTED FUEL QTY, EICAS MATCHES SPR AND MAGNA STICKS. PERFORMED OPS CHECKED IAW AMM 28-41-00. OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,753 hrs · 42,472 cycles

SHEAR CLIP AT FRAME 61 BETWEEN STGR 6R AND 7R IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STGR 6R AND 7R IAW EMB145 SRM 51-40-02

Part: SKIN — CRACKED (ZONE 600) · airframe 54,822 hrs · 51,689 cycles

RIGHT WING HAS CRACK ON LWR SURFACE BTW SPAR 11-12 AT SPAR II.

Part: FUEL TANK — LEAKING (ZONE 200)

STRONG FUEL ODOR IN CABIN AND FLIGHT DECK. FOUND FUEL LEAKING AT FWD FUEL TANK BULKHEAD IN CABIN APPROX STRINGER 17R. R & R SEALANT TO AFFECTED AREA INSIDE FUEL TANK IN REF TO SRM 51-20-01. LEAK CHECK GOOD, NO FURTHER DEFECTS OR SMELLS NOTED AT THIS TIME ACFT OK FOR SERVICE.

Part: VALVE — STUCK (PC AIR FLAP) · airframe 50,724 hrs · 46,912 cycles

EXHAUST FUME ODOR NOTICED WITH PACKS ON, FROM NR 2 ENGINE. PERFORMED GVI AT ENG 2, NO SIGNS OF OIL IN BYPASS OR OTHER ENG AREAS, BOTH PACKS 1 & 2 AREAS APPEAR NORMAL WITH NO MELTED SLEEVES. ON INSPECTION, FOUND PC AIR FLAP VALVE STUCK OPEN, LUBED HINGE AND ACTUATED MULTIPLE TIMES WITH NO DEFECTS NOTED. GROUND RAN A/C FOR 15 MINS NO ODOR NOTED FROM APU BLEED OR BLEED 2

Part: BLEED AIR SYS — LEAKING (APU) · airframe 54,892 hrs · 52,011 cycles

CREW NOTIFIED CLT MX OF EXHAUST FUMES IN COCKPIT. CLT MX CREW REPORTED SMELL IN COCKPIT, CABIN NORMAL, FUTHER TROUBLESHOOTING FOUND APU BLEED CAUSE OF FUMES AND WAS PUT ON MEL. A/C DEPARTED WITH NO FURTHER ISSUES IN FLIGHT.

Part: O-RING — LEAKING (APU) · airframe 56,993 hrs · 54,263 cycles

EXHAUST FUME ODOR IN COCKPIT. MEL C21521, 36-2 APU BLEED SYSTEM. R & R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHKD GOOD. LEAK CHKD GOOD. NO OTHER OR FUMES IN COCKPIT OR CABIN.OK FOR SERVICE AT THIS TIME.

Part: ELECT MODULE — FAULTED (ZONE 300) · airframe 46,650 hrs · 42,350 cycles

ON TAKE OFF ROLL AT V1 FLIGHT CONTROL DID NOT RESPOND TO YOKE MOVEMENT. C/W HORIZONTAL STABILIZER ELECTRICAL/ELECTRONIC OPS CHECK IAW AMM 27-40-00-700-802-A. C/W AURAL WARNING OPS CHECK IAW AMM TASK 31-51-00-700-801-A. C/W ELEVATOR CONTROL CABLE TENSION CHECK IAW AMM TASK 27-31-01-700-801-A. ALL OPS CHECK GOOD.

Part: O-RING — LEAKING (BLEED VALVE) · airframe 56,999 hrs · 54,269 cycles

EXHAUST FUME SMELL IN COCKPIT. APU BLEED SYSTEM. R&R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHECKED GOOD. LEAKS CHECK GOOD.NO OTHER OR FUMES IN COCKPIT OR CABIN.OK FOR SERVICE AT THIS TIME.

Part: RADAR — FAILED (WX SYSTEM) · airframe 46,990 hrs · 44,503 cycles

WING A/I FAIL MSG APPEARED ON EICAS IN ICING CONDITIONS, WING ANTI-ICING SYSTEM. OPS CHECK GOOD IAW AMM 30-00-00. A/C OK FOR SERVICE AT THIS TIME.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 46,370 hrs · 43,627 cycles

EMERGENCY EXIT LIGHT DIRECTLY ABOVE FA JUMPSEAT DOES NOT ILLUMINATE WHEN SET TO ON. R & R EMERGENCY EXIT MARKING SIGN ASSY DIRECTLY ABOVE FA JUMPSEAT IAW EMB 145 33-50-14. OPS CHECK GOOD.

Part: RIB — DAMAGED (RUDDER) · airframe 46,753 hrs · 42,472 cycles

F143997 RUDDER I TOP RIB DAMAGED DURING REMOVAL OF HORIZONTAL STABILIZER. PERFORMED RE-CONTOUR AND SPLICE REPAIR TO THE RUDDER I TOP RIB IAW EMB ETD2026-145-01327 REV. A, AND EO1-55-26-0370

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 46,753 hrs · 42,472 cycles

CARGO DOOR LOWER FRAME HAS MULTIPLE ELONGATED HOLES. REMOVED AND REPLACED CARGO DOOR LOWER FRAME IAW EMB 145 SRM 51-40-02, 51-20-01

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,357 hrs · 42,679 cycles

SHEAR TIE CRACKED AT FR 24 BTW STR 16-17R. R & R SHEAR TIE IAW SRM 51-40-02.

Part: A/C PACK — SMOKE (NR 2) · airframe 46,828 hrs · 43,919 cycles

SMOKE AND FUMES IN FLT DECK AND CABIN WITH PACK 2 RUNNING. SMOKE CLEARED WITH PACK 2, GASPER AND RECIRC SELECTED OFF. INSPECTED PACK 1 AND 2. FOUND PACK 2 ACM TO BE DEFFECTIVE. SEE SEQ 1 ON LOGBOOK PAGE 374458 FOR DISCREPANCY. MEL 27JUL26 18:46 ORF C20828 21-15-2 1 AIR COND PACK N650 AND ABOVE

Part: A/C PACK — ODOR (NR 2) · airframe 48,876 hrs · 45,522 cycles

AFTER SUCCESSFUL AIR CART START, PACK 2 FAILED AND STRONG EXHAUST SMELL FROM PACKS. RAN PACKS ON BOTH ENGINES A/R. NO ODORS, SHUTDOWNS OR DEFECTS NOTED AT THIS TIME. A/C OK FOR SVC

Part: ANGLE — CRACKED (ZONE 100) · airframe 46,357 hrs · 42,679 cycles

LWR FUSE BODY FAIRING 192EL, WING STUB LT FWD RETAING ANGLE L SHAPE CRACKED. REPAIRED IAW SRM 57-20-01

Part: CONTROL PANEL — FAULTED (ZONE 200)

UNABLE TO CONTROL EMERGENCY LIGHTS FROM FLIGHT ATTENDANT PANEL. R & R F/A'S CONTROL PANEL IAW AMM 25-27-09-000 AND 400-801-A. OPS CHECK GOOD. OK FOR SERVICE.

Part: CHECK VALVE — FAULTED (ZONE 200) · airframe 48,820 hrs · 46,334 cycles

SMELL OF EXHAUST FUMES IN FLIGHT DECK FACT 26JUL26 07:22 ROA OPERATED PACK 1&2 WITH E2 BLEED AND VERIFIED NO EXHAUST SMELL COMMING FROM PACK SYSTEM. NO DEFECTS NOTED. 26JUL26 12:41 ROA AIR LEAK WAS PREVIOUSLY FOUND TO BE ON AFT END OF APU BLEED AIR CHECK VALVE ADDITIONAL LEAK WAS FOUND TO BE IN COUPLING AT THE AFT END OF BLEED AIR PIPE WITH THE APU BLEED AIR CHECK VALVE R&R APU BLEED AIR CHECK VALVE IRW AMM 36-12-02 O-RING AT AFT COUPLING WAS FOUND TO BE BROKEN R&R AFT COUPLING O-RINGS AND REINSTALLED ASSOCIATED BLEED PIPE IRW AMM 36-11-09 RAN PACK SYSTEM OFF APU BLEED IN MULTIPLE DIFFERENT CONFIGURATIONS NO SMELL NOTED AT THIS TIME A/C OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 50,434 hrs · 46,679 cycles

WHILE TAXIING BURNING OIL SMELL NOTED IN CABIN AND ON FLIGHT DECK. RAN BOTH PACKS WITH BOTH ENGINES AND APU BLEEDS. NO ODOR NOTED. SUSPECT ODOR TO BE FROM FAILED E2 STARTUP. A/C OK FOR SERVICE AT THIS TIME

Part: A/C PACK — ODOR (NR 1) · airframe 54,838 hrs · 51,947 cycles

OIL SMELL IN FLIGHTDECK FROM PACK 1. FACT 27JUL26 01:02 CLT INSPECTED PAX 1. FOUND TO BE GOOD. FOUND PAX 2 TO HAVE MELTED DUCT. REMOVED AND REPLACED DUCT AS REQUIRED. PERFORMED OP CHECK IAW 21-51-00. OP CHECK GOOD. NO DEFECTS NOTED A/C OKAY FOR SERVICE

Part: FAN — INOPERATIVE (ZONE 200)

REPORTED FUMES/ODOR WITH APU OPERATION. WHILE T/S FPOUND NO 1 RECIRC FAN INOP W FUSE F0059 BLOWN R/R FUSE F0059 IRW AMM 20-13-08 R/R NO 1 RECIRC FAN AND FILTER IAW AMM 21-24-01 OPS AND LEAK CHECK GOOD RAN PACK 1/2 NO ODORS NOTED

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,580 hrs · 43,432 cycles

ROW 15 FLOOR PROXIMITY EMERGENCY LIGHT INOP. R & R ROW 15 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: BLEED VALVE — FAULTED (APU) · airframe 46,214 hrs · 42,316 cycles

BLD VLV CLOSED MSG ON T/O. RAN QRH AND MESSAGE PERSISTED, WENT TO START APU AND APU FAILED WITH APU FAIL MSG FACT 23JUL26 18:15 PHL T/S IAW AMM FIM 36-11-00-810-807A BLOCK 8 AND PERFORMED OPS BLEED SYSTEM. OPS CHECK ISW AMM REF 36-00-00. FOUND NO DEFECTS NOTED AT THIS TIME. AC OK FOR SERVICE

Part: SUPPORT — CRACKED (ZONE 100) · airframe 46,522 hrs · 42,934 cycles

BLEED AIR CROSSBLEED VALVE SUPPORT (ANTI-ROTATION) IS CRACKED IN AFT E&E BAY. RAR VALVE SUPPORT IAW AMM 36-10-01,

Part: ENGINE — HUNG START (NR 2) · airframe 56,911 hrs · 54,167 cycles

NUMBER 2 ENGINE HAD HUNG START WITH WHITE SMOKE AND A FUEL ODOR IN FLIGHT DECK AND CABIN. PERFORMED ENGINE 2 START ON BOTH FADEC CHANNELS IAW MM 72-00-00-860-801 NO DEFECTS NOTED A/C OK FOR SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,357 hrs · 42,679 cycles

REAR FUSE I FR61 STR19L CORRODED. REPAIRED IAW SRM 53-00-03

Part: CHECK VALVE — ABNORMAL (ZONE 200)

STRONG EXHAUST SMELL IN FLT DECK WHEN RUNNING APU AT THE GATE WITH PACK 1. FOUND APU BLEED VALVE INNER GASKET TO BE WORN. R&R BLEED VALVE REF TO AMM 36-12-03. NO FIX TRANSCRIBED TO LP 391921-3 FOR APU BLEED MEL. 26JUL26 12:41 ROA AIR LEAK WAS PREVIOUSLY FOUND TO BE ON AFT END OF APU BLEED AIR CHECK VALVE ADDITIONAL LEAK WAS FOUND TO BE IN COUPLING AT THE AFT END OF BLEED AIR PIPE WITH THE APU BLEED AIR CHECK VALVE R&R APU BLEED AIR CHECK VALVE IRW AMM 36-12-02 O-RING AT AFT COUPLING WAS FOUND TO BE BROKEN R&R AFT COUPLING O-RINGS AND REINSTALLED ASSOCIATED BLEED PIPE IRW AMM 36-11-09 RAN PACK SYSTEM OFF APU BLEED IN MULTIPLE DIFFERENT CONFIGURATIONS NO SMELL NOTED AT THIS TIME A/C OK FOR SERVICE.

Part: SENSOR — FAILED (ZONE 400) · airframe 53,779 hrs · 51,111 cycles

BLEED NR 2 OVERTEMP MESSAGE DISPLAYED, FOLLOWED QRH MESSAGE CLEARED. REF 36-11-00-810-1 CMC MSG DUCT SENSOR FAIL W/ NO OTHER RELATED MESSAGES. R & R BLEED 2 OUTLET TEMP SENSOR IAW AMM 36-20-01 PERFORMED IDLE RUN IRT RUN UP CHECKLIST NO ABNORMAL TEMP READING NOTED FOR 15MIN AC OK FOR SERVICE AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,633 hrs · 42,771 cycles

RT OTBD FLOOR SILL AT FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL AT FR 22 IAW EMB 145 SRM 51-40-02-PR

Part: RIB — CRACKED (ZONE 200) · airframe 46,522 hrs · 42,934 cycles

53-2170 IN COCKPIT, RIB, OVERHEAD PANEL HORIZONTAL LT CRACKED. REPAIRED IAW SRM53-12-13

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,357 hrs · 42,679 cycles

RIGHT UPPER SEAT TRACK SUPPORT CORRODED AT FR45-50. REPAIRED IAW SRM53-00-11

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,357 hrs · 42,679 cycles

SHEAR TIE CRACKED AT FR24 STR 15R. R & R SHEAR TIE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,357 hrs · 42,679 cycles

SHEAR TIE CRACKED AT FR 56, STR 15L. R & R SHEAR TIE IAW SRM 51-40-02

Part: STOP — BROKEN (ZONE 800) · airframe 46,522 hrs · 42,934 cycles

BAGGAGE DOOR VENT FLAP AFT STOP BROKEN. R & R STOP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,357 hrs · 42,679 cycles

AFT FLOOR SUPPORT CRACKED BTW FR16-17. R & R SUPPORT IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 46,522 hrs · 42,934 cycles

CARGO DOOR LIFTING MECHANSM, DRUM AREA, SUPPORT ANGLE CRACKED. REPAIRED IAW AMM 52-32-00

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,357 hrs · 42,679 cycles

SERVICE DOOR FWD SILL CORRODED BTW FR 19-20. REPAIRED IAW SRM 53-21-10

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,753 hrs · 42,472 cycles

CARGO FLOOR RAMP FLOOR SUPPORT AT FR-65 LOWER END AROUND NUT-PLATE HOLE HAS CORROSION. R & R THE CARGO RAMP FLOOR SUPPORT AT FR65 IAW EMB 145 SRM 51-40-02