N375PA
Registered owner: DA40 LLC, SC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PAN AMERICAN WORLD AWYS INC. | Operator | on 1987-10-27 | Operator named in NTSB report |
Accident & incident history
Operated by PAN AMERICAN WORLD AIRWAYS (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
53 reports on file, 2002-03-10 – 2005-07-15.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,469 hrs · 38,519 cycles
AFT CENTER AISLE EMERGENCY LIGHT INOP. REPLACED AFT RIGHT BATTERY PACK PER MM 33-50.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 45,356 hrs · 38,453 cycles
LIGHT BURNED OUT AT RT EMERGENCY EXIT DOOR. REPLACED BULB, OPS NORMAL.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,142 hrs · 38,316 cycles
L1 OUTSIDE EMERGENCY LIGHT INOP. REPLACED L1 EMERGENCY LIGHT BULB. OPS CHECKS GOOD.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,142 hrs · 38,316 cycles
L1 OUTSIDE EMERGENCY LIGHT INOP. REPLACED L1 EMERGENCY LIGHT BULB. OPS CHECKS GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
SEAT TRACK FROM BS 344 TO BS 380 AT LBL 25 CORRODED. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 44,983 hrs · 38,217 cycles
AFT CARGO DOOR INNER SKIN CRACKED AROUND LIGHTENING HOLE NEAR CENTER OF DOOR. REPAIRED PER SRM 51-70-13.
Part: PANEL — GOUGED (LT RAM AIR) · airframe 44,983 hrs · 38,217 cycles
LEFT RAM AIR CLOSE OUT PANEL GOUGED. REPAIRED PER SRM 51-70-13.
Part: SKIN — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
AFT SERVICE DOOR TOP HINGE CUTOUT IN FUSELAGE SKIN CRACKED. REPAIRED PER SRM 53-60-01.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 3. REPAIRED PER SRM 53-00-53.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D + 7 AT RBL 3. REPAIRED PER SRM 53-00-53.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
CORROSION ON HORIZONTAL FLANGE OF THE RIGHT KEEL BEAM AT BS 520 AT RBL 6.5. REPAIRED PER EA 53-030.
Part: PLATE — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
L1 DOOR FORWARD SILL PLATE CRACKED. WELDED PER BAC SPEC 5975.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
CORROSION ON FLOORBEAM T-CAP AT BS 344 FROM LBL 19 TO LBL 30. REPAIRED PER SRM 53-10-51.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
CORROSION ON THE I/B SIDE OF THE RIGHT KEEL BEAM FORWARD OF BS 540. REPAIRED PER EA 53-028.
Part: PRECOOLER — CRACKED (RT ENGINE) · airframe 44,983 hrs · 38,217 cycles
RIGHT ENGINE PRECOOLER CRACKED IN O/B UPPER FORWARD CORNER. WELDED PER BAC SPEC 5975.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
STRINGER 28 LT SPLICE IS CORRODED AT BS 907. REPLACED STRINGER SPLICE PER SRM 51-10-02 AND 51-40-02.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
INTERCOSTAL ATTACH CLIP CRACKED UNDER AFT END OF RIGHT TRANSITION ANGLE AT BS 947 BETWEEN STR 26 RT AND STR 25 RT. REPLACED ATTACH CLIP PER SRM 51-10-02.
Part: VALVE — FAILED (RT ENG PRECOOLER) · airframe 44,983 hrs · 38,217 cycles
RIGHT ENGINE PRECOOLER VALVE CRACKED. REPLACED PRECOOLER VALVE PER MM 63-12-35.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
SUPPORT ANGLE CRACKED AT BS 767 ABOVE STR 28 LT. REPLACED ATTACH ANGLE PER SRM 51-40-01.
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 44,983 hrs · 38,217 cycles
AFT CARGO DOOR AFT FRAME CRACKED APPROX 16 INCHES ABOVE LOWER AFT CORNER. REPLACED FRAME PER SRM 51-40-05, 51-40-08, AND 51-10-01.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,983 hrs · 38,217 cycles
AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 7. REPAIRED PER SRM 53-00-53.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
CORROSION IN FORWARD END OF RIGHT O/B SEAT TRACK UNDER THE WIND SCREEN. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
CORROSION ON FLOORBEAM T-CAP AT BS 312 AT LBL 19. REPAIRED PER SRM 53-10-51.
Part: VALVE — CRACKED (PRE COOLER) · airframe 44,983 hrs · 38,217 cycles
RIGHT ENGINE PRE-COOLER VALVE CRACKED. REPLACED PER-COOLER VALVE PER MM 36-12-35.
Part: STIFFENER — DAMAGED (WING) · airframe 44,983 hrs · 38,217 cycles
VERTICAL STIFFENER FOR THE FRONT SPAR BULKHEAD AT RBL 6.25 WAS TRIMMED OFF TO ALLOW FOR REPAIR OF KEEL BEAM (SDR 375PA0032). REPAIRED PER EA 57-029.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,983 hrs · 38,217 cycles
AFT CARGO FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT BS 727D +7 AT RBL 7. REPAIRED PER SRM 53-00-53.
Earlier reports · 2002–2004 · 27 reports
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,387 hrs · 37,864 cycles
EMERGENCY FLOOR PATH LIGHTING FROM ROW 15 TO 21 IS INOPERATIVE. REPLACED BATTERY PACK AT STA 753 IAW MM 33-51-00. OPS CHECKS NORMAL.
2003
Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,733 hrs · 37,481 cycles
EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY MISSING AT ROW 16 AREA. INSTALLED EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY PER MM 33-51-81. OPS CHECKS NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,649 hrs · 37,406 cycles
MID TO AFT EMERGENCY FLOOR LIGHTING INOP. REPLACED BATTERY PACK LEFT SIDE MID CABIN. OPS NORMAL PER MM 33-51-00.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,558 hrs · 37,348 cycles
EMERGENCY LIGHTS INOPERATIVE AT FIRST 4 SEATS AND AT OVERWING SECTION. REPLACED BATTERY PACK AT RIGHT SIDE OF CABIN AND AT OVERHEAD COMPARTMENT.
Part: COUPLER — INOPERATIVE (YAW DAMPER) · airframe 43,503 hrs · 37,325 cycles
YAW DAMPER INOPERATIVE. RELEASED ON MEL 22-3-1. 8/16/2003: REPLACED YAW DAMPER COUPLER IAW MM22-12-32 PG.401 AND ACCOMPLISHED OPS. TEST, SELF TEST, SERVO TEST AND RUDDER PRESSURE REDUCER TEST. ALL OK.
Part: WIRE — OPEN (EMERGENCY LIGHT) · airframe 43,493 hrs · 37,321 cycles
FIRST EMERGENCY LIGHT ON LEFT AISLE FLOOR POPPED OFF. FOUND OPEN ON WIRE AT FIRST EMERGENCY LIGHT. RE-SPLICED WIRE. FLOOR PATH OPS CHECKS GOOD.
Part: WINDOW — CRACKED (COCKPIT) · airframe 43,487 hrs · 37,318 cycles
FIRST OFFICER'S SIDE WINDOW CRACKED. REPLACED R-2 WINDOW IAW MM 56-12-11. OPS CHECKS GOOD IAW MM 30-41-12.
Part: CONNECTOR — DIRTY (FUEL METERING) · airframe 43,282 hrs · 37,184 cycles
VARIOUS ANOMALOUS (SIC) INDICATIONS FROM FMA/MCP. A/T ANN RAPIDLY CHANGES MODES, SPURIOUS ALTITUDES APPEAR. IN ALT HOLD A/C CLIMBS & DESCENDS +/- 300 FT. VS MODE CYCLES, ALT HOLD CYCLES. CLEANED AND CHECKED EFIS RT AND CLEANED CONNECTOR TO THE FMA. PERFORMED CHECK THRU CDU. NO DUPLICATE FAILURES PER MM 22-10-00.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,155 hrs · 37,097 cycles
FWD EMERGENCY FLOOR PATH LIGHTING HAS ONE LIGHT INOP AT ROW 1. MOVED FLOOR PATH LENS FROM ROW 7 TO ROW 1. ROW ONE OPS NORMAL. RELEASED ON MEL 33-19-1. ROW 7 HAS 1 FLOOR PATH LIGHT BULB INOP. 05/15/2003: REPLACED BULB AND REINSTALLED LENS ON ROW 7. SYSTEM OPS, CHECKS GOOD PER MM 33-51-02. CLEARED MEL.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 43,096 hrs · 37,063 cycles
THREE EACH BULBS NOT WORKING ON EMERGENCY EXIT LIGHT TEST ON SERVICE CHECK. RECONNECTED WIRING AT SOCKETS. ALL LIGHTS OPS CHECK GOOD PER MM 33-50-00.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 42,942 hrs · 36,967 cycles
EMERGENCY EXIT LIGHTS INOP (4 OF THEM HALFWAY DOWN AISLE). FOUND 2 LIGHTS WITH BOTH CONNECTORS DISCONNECTED. REPLACED CONNECTORS AND OPS CHK GOOD PER MM 33-51-02.
Part: STRIP · airframe 42,866 hrs · 36,925 cycles
3C emergency light strip broken. Removed & replaced track cover. Connected wires, Ops chk. OK per MM 33-51-00.
Part: CONNECTOR · airframe 42,820 hrs · 36,903 cycles
Forward section emergency exit lights inop. Found emergency light connection at row 3 ABC off. Reconnected and repositioned wiring. Lights ops. chk. normal.
Part: BATTERY PACK · airframe 42,760 hrs · 36,867 cycles
Two sections of emergency floor lighting inop. Battery pack low Rt. side. After charging battery pack, Ops check normal.
Part: WIRE · airframe 42,708 hrs · 36,817 cycles
Several emergency exit lights out. Repaired wiring on lights per WDM Chpt. 20. Ops chk OK.
2002
Part: COMPUTER · airframe 42,545 hrs · 36,718 cycles
Auto throttles disengage during take-off when TOGA is engaged. All other TOGA indications are normal. This is an intermittent condition. R&R #2 N1 speed sensor per MM 77-12-01. R&R A/T computer & performed BITE test per MM 22-04-10. Ops checked good.
Part: CONTROL UNIT — MALFUNCTIONED (AUTO THROTTLES) · airframe 42,533 hrs · 36,707 cycles
DURING TAKE-OFF, AUTO THROTTLES DISENGAGE WHEN TOGA BUTTONS ARE ENGAGED. AUTO THROTTLES CAN BE RE-ENGAGED MANUALLY. UNABLE TO DUPLICATE. PERFORMED AUTO THROTTLE BITE TEST. NO FAULTS PER MM 22-31-00
Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 42,488 hrs · 36,671 cycles
AUTO THROTTLE WOULD NOT ARM ON TAKE-OFF. ON DECENT INTO SFB, IN LEVEL CHANGE, AT MOVED FWD & BACK SWITCHING FROM "N" TO "RETARD" REPEATEDLY. CHK'D AUTO THROTTLE COMPUTER & RAN BITE CHK. ON CDU PER MM22-31-00 PG.501-508, NO FAULTS FOUND.
Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 42,483 hrs · 36,668 cycles
AUTO THROTTLE DISENGAGED WHEN AUTO THROTTLE WAS INGAGED FOR TAKE-OFF. RE-RACKED AUTO THROTTLE COMPUTER. RAN BITE TEST ON FMC, SYSTEM TESTS NORMAL.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,357 hrs · 36,580 cycles
SEVERAL EMERGENCY FLOOR LOCATOR LIGHTS ARE INOP. RELAMPED SEVERAL LIGHTS IN FWD TRACK. ALL E-PATH OPS CHECK OK PER MM 33-51-81.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,333 hrs · 36,566 cycles
EMERGENCY EXIT LIGHT ABOVE R2 DOOR AND LOWER RT OF L2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 33-51--51. OPS CHECK NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,333 hrs · 36,566 cycles
EMERGENCY EXIT LIGHT ABOVE R2 DOOR AND LOWER RIGHT OF L2 DOOR INOP. R&R BATTERY PACK IAW 33-51--51. OPS CHECK NORMAL.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,333 hrs · 36,566 cycles
SEVERAL EMERGENCY FLOOR LOCATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED 3 LAMPS. RECONNECTED WIRING ON 2 LIGHT ASSY. ALL OPS CHECK NORMAL IAW AMM 33-50-81.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 42,211 hrs · 36,485 cycles
FWD EMERGENCY FLOOR TRACK LIGHT LENS LOOSE AND INOP. INSTALLED NEW EMERGENCY LIGHT FLOOR ASSY. IAW 737-300 MM 33-51-81.
Part: AUTOTHRUST SYS — MALFUNCTIONED · airframe 41,818 hrs · 36,257 cycles
AUTOTHROTTLES WOULD NOT ENGAGE FOR TAKE-OFF. DURING CLIMB AND CRUISE "A/T LIM" DISPLAYED
Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 41,818 hrs · 36,257 cycles
AUTOPILOT WOULD NOT INTERCEPT LOC AND ATTEMPTED TO CORRECT IN WRONG DIRECTION.
Part: TIRE · airframe 41,845 hrs · 36,216 cycles
Right nose tire failed on take-off at V1 - seperation of tread. R&R both nose wheel/tire assy.'s Inspected A/C IAW MM.Ferried A/C. R&R'd E&E door, nose prox sensor and associated wiring.