N374PA
Registered owner: COPTER LEASE LLC TRUSTEE, NM (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PATHFINDER AVIATION LLC (P3TA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
TWO CRACKS IN BS 827 FRAME AT STR 9RT. REPAIRED PER SRM 53-00-07.
UPPER ATTACH ANGLE ON INTERCOSTAL AT BL 0 BETWEEN BS 380 AND BS 400 AT WL 208 IS CRACKED. REPLACED ANGLE PER SRM 51-10-02.
TWO CRACKS AT RIVET HOLE IN BS 867 FRAME AT STR 9 RT. REPAIRED PER SRM 53-00-07.
TWO CRACKS IN BS 787 FRAME AT RIVET HOLE AT STR 9RT. REPAIRED PER SRM 53-00-07.
INTERCOSTAL AT BS 540 CRACKED AT I/B AFT ATTACH FASTENER AT RBL 1. REPLACED INTERCOSTAL PER DWG 65-52894 AND SRM 51-10-2.
TWO CRACKS IN BS 827 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07.
TWO CRACKS IN BS 787 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07.
TWO CRACKS IN BS 867 FRAME AT STR 9LT. REPAIRED PER SRM 53-00-07.
CRACK IN LOWER RADIUS AT AFT END OF THE LEFT MOUNT HAT CHANNEL FOR THE RADAR TR UNIT. REPAIRED HAT CHANNEL PER SRM 51-70-12.
FOUR CRACKS IN WEB PANEL AT LBL 4 BETWEEN BS 967 AND BS 986. REPAIRED PER DWG 65-46816 AND SRM 51-10-2.
NUMBER 5 SPOILER O/B HINGE I/B SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE PER SRM 51-10-2.
CORROSION AT CLIP NUT HOLE AT LBL 27 ON FLOORBEAM AT BS 312. REPAIRED PER SRM 53-10-51.
NUMBER 5 SPOILER I/B ATTACH BRACKET SUPPORT ANGLES CRACKED. REPLACED ANGLES PER SRM 51-10-2.
IMPACT DAMAGE TO THE FUSELAGE SKIN, FORWARD ENTRANCE DOORWAY BEARSTRAP AND BS 294.5 BULKHEAD SHEAR TIE AND WEB BETWEEN STR 19LT AND STR 20LT. REPAIRED PER EA 53-074.
IMPACT DAMAGE (DENT) AT BS 483 SKIN PANEL BETWEEN STR 21 LT AND STR 22 LT. REPAIRED PER SRM 53-00-01 FIG 229.
AUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN. REPLACED AURAL WARNING CIRCUIT BREAKER PER MM 31-26-00 AND OPS CHECKED. PERFORMED SELF TEST OF AUTO PILOT SYSTEM PER MM 22-02-10 AND 22-03-10. NO DEFECTS NOTED.
RIGHT ENGINE DOESN'T SPOOL UP. ADJUSTED GROUND IDLE PER MM. ADJUSTED SPECIFIC GRAVITY PER MM. TIGHTENED LINE AT BLEED REGULATOR. BOTH ENGINES OPERATE NORMAL PER MM.
DENT AT RIGHT SIDE OF AIRCRAFT AT BS 312 AND STR 20. REPAIRED PER SRM 53-00-01 AND EA 53-121.
DENT IN FUSELAGE SKIN AFT OF L1 DOOR AT STA 400 BETWEEN STR 17 LT AND STR 18 LT. REPAIRED AREA PER SRM 53-00-01 AND EA 53-120.
AFT CARGO DOOR CENTER SECTION OF THRESHOLD CRACKED. WELDED PER BAC 5975.
CORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE IAW SRM 53-60-53.
FOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55A1087. REPLACED HARDWARE AT LOCATIONS F1, F2, F3, F4, F10 PER BOEING SERVICE BULLETIN.
WARNING HORN ON TAKEOFF ROLL. NO LEADING EDGE FLAP/SLAT INDICATION. RESET LEADING EDGE POSITION INDICATOR CIRCUIT BREAKER. SYSTEM OPS CHECKS GOOD PER MM 27-88-00.
FUSELAGE DAMAGED LEFT SIDE FROM BS 907 TO BS 927 AT STR 16 LT, AT BS 907 BETWEEN STR 21 LT AND 22 LT AND FRAME SHEAR TIE DAMAGED AT BS 908 BETWEEN STR 21 LT AND STR 22 LT. REPAIRED DAMAGE PER EA NOS 53-327, 53-331, AND 53-332.
RT EMERGENCY OVERWING EXIT SIGN LOCATOR LIGHT INOPERATIVE. RE-LAMPED LOCATOR LIGHT IAW MM 33-51-11. OPS CHECKS NORMAL.
YAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD.
FWD FLIGHT ATTENDANT JUMPSEAT OUTBOARD EMERGENCY FLASHLIGHT LED WILL NOT FLASH. ITEM DEFERRED PER MEL 25-12, CONTROL NR 0112001. 1/15/2003. R & R BATTERY POWER UNIT AS REQUIRED. OPS CHECK NORMAL. CLEARED MEL 25-12, CONTROL NR 0112001
TAKEOFF WARNING HORN ACTIVATED DURING T/O ROLL, OBSERVED LE FLAPS TRANSIT LIGHT ILLUMINATED, PERFORMED RTO. FOUND NR 1 KRUGER FLAP POSITION SENSOR BAD. R&R PROXIMITY SENSOR PER MM 27-88-11, OPS CHECKED. GOOD.
Takeoff warning horn activated during T/O roll, observed LE flaps transit light illuminated, performed RTO. R&R #1&2 tires and brakes, R&R #3&4 brakes per 32-41 & 32-45; insp anti-skid system per 32-42-00 OK; performed T/O warning test per AD 88-22-09 OK; brake seizure insp per 05-51-04 OK; high energy insp per 05-51-07 no damage found. R&R #1 kruger flap proximity sensor per MM 27-88-11, Ops chk. good.