# N602FF: 1970 Boeing 747-124, registration cancelled 2001-10-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 30, 2001
- Status when cancelled: Valid registration
- Airframe: [Boeing 747-124](https://openairdocs.org/model/boeing-747-124) (registry code 1384874)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 19734
- Year built: 1970
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 1983
- Last registry action: October 30, 2001
- Mode S code: A7CF30
- Owner when cancelled: [A O G Sheetmetal Inc](https://openairdocs.org/faa-owner/A%20O%20G%20SHEETMETAL%20INC)
- Location: [Jamaica, NY](https://openairdocs.org/faa-place/NY/Jamaica)
- Owner type: Corporation
- Owner's area on the map: 40.6779° N, 73.7771° W: Placed by OpenAirDocs at the center of ZIP code 11434, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N602FF
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=602FF
- Page: https://openairdocs.org/deregistered/N602FF-2001-10-30

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 747-124: https://openairdocs.org/model/boeing-747-124.md

## Service difficulty reports (41)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR TWRA0004](https://openairdocs.org/sdr/TWRA0004), Jan 8, 2000: ROD END. BROKEN. AT ARRIVAL UPON OPENING L-2 DOOR, FOUND GIRT BAR LIFT ROD BROKEN. REMOVED AND REPLACED ROD ENDS PER MM 52-11-07. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWRA0001](https://openairdocs.org/sdr/TWRA0001), Jan 5, 2000: LIGHT. INOPERATIVE. DURING DAILY CHECK, FOUND LEFT SIDE FUSELAGE OVERWING EMERGENCY LIGHT ONE INOPERABLE. REPAIRED CONNECTOR DAMAGED BY WATER. OPERATIONAL CHECK OK PER MM 33-51-00.
- [SDR 99ZZZX4375](https://openairdocs.org/sdr/99ZZZX4375), Oct 16, 1999: FLOORBEAM. CRACKED. FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, RBL 99 - RBL 121. SIZE: 2 INCHES, 2 INCHES, 1 INCH AND 1 INCH.
- [SDR 99ZZZX4374](https://openairdocs.org/sdr/99ZZZX4374), Oct 16, 1999: FLOORBEAM. CRACKED. THREE CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, LBL 99 - LBL 121, IN M/D. SIZE: 12 INCHES, 2.5 INCHES, AND 2 INCHES.
- [SDR 99ZZZX4373](https://openairdocs.org/sdr/99ZZZX4373), Oct 16, 1999: FLOORBEAM. CRACKED. FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOOR BEAM WEB AT BS 1420, LBL 99 - LBL 121 IN M/D. SIZE: 5 INCHES, 3 INCHES, 1 INCH AND .0.5 INCH.
- [SDR 99ZZZX4371](https://openairdocs.org/sdr/99ZZZX4371), Oct 16, 1999: FLOORBEAM. CRACKED. FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, LBL 99 - LBL 121 IN M/D. SIZE 3.2 INCHES, 4 INCHES 1.5 INCHES, AND 1.5 INCHES.
- [SDR 99ZZZX4370](https://openairdocs.org/sdr/99ZZZX4370), Sep 29, 1999: SPAR. CORRODED. DURING MAINTENANCE C-CHECK, BEJ FOUND SEVERE CORROSION ON THE REAR SURFACE OF VERTICAL LEG OF THE LEFT WING REAR SPAR UPPER CHORD AT WS 550, WS 520, AND WS 444.
- [SDR 99ZZZX4369](https://openairdocs.org/sdr/99ZZZX4369), Sep 28, 1999: SKIN. CORRODED. DURING MAINTENANCE C-CHECK, BEJ FOUND SEVERE CORROSION ON THE UPPER SURFACE OF THE WING CENTER SECTION (WCS) UPPER SKIN AT BS 1110, LBBL 11.33, AND BETWEEN UPPE
- [SDR 99ZZZX4372](https://openairdocs.org/sdr/99ZZZX4372), Sep 20, 1999: FRAME. CRACKED. WHILE PERFORMING MODIFICATION PER THE SB 747-5342390, A CRACK OF 3 INCHES WAS FOUND IN STA 1480 LOWER BULKHEAD, RT FRAME WEB AFTER REMOVAL OF THE AFTER WEB SPAC
- [SDR TWRA9928](https://openairdocs.org/sdr/TWRA9928), Jul 13, 1999: FASTENERS. FAILED. LEFT WING UPPER WEB TO CHORD FASTENERS SHEARED (ONE EACH) AT FS 636.84 AND (3 EACH) AT FS 655.75, AND FS 646.07. LOWER WEB TO CHORD FASTENERS SHEARED (23 EACH) 
- [SDR TWRA9927](https://openairdocs.org/sdr/TWRA9927), Jul 13, 1999: FASTENERS. CRACKED. RIGHT WING WEB TO CHORD UPPER FASTENERS CRACKED (2 EACH) AT FS 636.84 AND FS 646.07. LOWER WEB TO CHORD FASTENERS CRACKED (ONE EACH) AT FS 636.84 AND FS 646.07.
- [SDR TWRA9907](https://openairdocs.org/sdr/TWRA9907), Feb 16, 1999: SLIDE. CUT. R2 MED SLIDE RAFT EXPIRATION DATE WA COMING DUE, THE SLIDE RAFT WAS USED FOR TRAINING PURPOSES AND INFLATED INTENTIONALLY. DURING SLIDE DEPLOYMENT THE SLIDE WAS
- [SDR TWRA9856](https://openairdocs.org/sdr/TWRA9856), Nov 17, 1998: FUSE. FAILED. DURING 'A' SERVICE, FOUND 'E' ZONE ALL LEFT SIDE EMERGENCY EVACS LIGHT INOPERATIVE. REPLACED FUSE IN THE BATTERY PACK. OPERATIONAL CHECK NORMAL PER MM 33-51-00.
- [SDR TWRA9855](https://openairdocs.org/sdr/TWRA9855), Nov 17, 1998: WIRE. BROKEN. DURING 'A' SERVICE, FOUND MID LAV J AND H, EMERGENCY EVACS LIGHT INOPERATIVE. REPAIRED WIRING. OPERATIONAL CHECK NORMAL AS PER MM 33-50-00. (M)
- [SDR TWRA9851](https://openairdocs.org/sdr/TWRA9851), Aug 29, 1998: SWITCH. BROKEN. AFTER TAKEOFF ROTATION F/O'S CONTROL WHEEL FORCE BECAME VERY HEAVY AND REQUIRED THE CAPTAIN TO TAKE OVER CONTROL F/O'S CONTROL WHEEL HAS 1.5 INCHES OF LOST MOTI
- [SDR TWRA9850](https://openairdocs.org/sdr/TWRA9850), Aug 29, 1998: SWITCH. MALFUNCTIONED. DURING FUEL DUMP, NR 3 MAIN JETTISON PUMP PRESSURE LIGHT REMAINED ON WITH BOTH PUMPS ON. DUMP RATE FROM NR 3 WAS ONE-HALF (50 PERCENT) BELOW NR 2 MAIN. REQUIRED
- [SDR TWRA9823](https://openairdocs.org/sdr/TWRA9823), Apr 20, 1998: SWITCH. FAILED. DURING APPROACH TURNED ON LANDING LGIHTS AND STARTED SMOKING BEHIND SWITCHS. TURNED OFF LIGHTS, SMOKE WENT AWAY. FOUND LEFT OUTBOARD LANDING LIGHT AT FAULT, PUL
- [SDR TWRA97200](https://openairdocs.org/sdr/TWRA97200), Nov 18, 1997: BEARING. SHEARED. DURING A SLIDE/RAFT DEMONSTRATION, 2R MED WAS JAMMED AND GUIDE ARM BEARING SHEARED, FLIGHT ATTENDANTS TRAINING AT JFK. REMOVED AND REPLACED GUIDE ARM BEARING PE
- [SDR TWRA97199](https://openairdocs.org/sdr/TWRA97199), Nov 18, 1997: SLIDE/RAFT. FAILED. DURING A SLIDE/RAFT DEMONSTRATION, FOR TRAINING FOR A GROUP OF F/A'S AT JFK, SLIDE MOUNTED AT 2R DOOR FAILED TO DEPLOY. REMOVED AND REPLACED SLIDE/RAFT PER MM 2
- [SDR 97ZZZM1219](https://openairdocs.org/sdr/97ZZZM1219), Nov 18, 1997: SLIDE/RAFT. FAILED. DURING A SLIDE/RAFT DEMONSTRATION, FOR TRAINING FOR A GROUP OF F/A'S AT JFK, SLIDE MOUNTED AT 2R DOOR FAILED TO DEPLOY. REMOVED AND REPLACED SLIDE/RAFT PER MM 2
- [SDR TWRA97180](https://openairdocs.org/sdr/TWRA97180), Oct 3, 1997: WIRE. BROKEN. DURING B SERVICE, FOUND EVAC LIGHT INOPERATIVE AT SEAT 38C. FOUND WIRE BROKEN, SPLICED WIRE. OPERATIONAL CHECK NORMAL AS PER MM 33-51-00, PAGE 501. (M)
- [SDR TWRA97133](https://openairdocs.org/sdr/TWRA97133), Jun 1, 1997: BATTERY PACK. DISCHARGED. DURING DAILY SERVICE, FOUND LEFT OVERWING EVAC LIGHT INOP (3RD LIGHT). REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK PER MM 33-51-00. (M)
- [SDR TWRA9791](https://openairdocs.org/sdr/TWRA9791), May 4, 1997: ACTUATOR. DEFECTIVE. ON GROUND AT IST AFT CARGO DOOR PUSH PULL RODS FOR DOOR LATCHES, BOTTOM 4 RODS, UPPER LEFT LATCH 1 ROD SHEARED. FORWARD LEFT STRUCTURAL SUPPORT RIPPED, HOLE PUN
- [SDR TWRA9717](https://openairdocs.org/sdr/TWRA9717), Feb 11, 1997: LIGHT. INOPERATIVE. DURING DAILY CHECK, FOUND FORWARD CEILING LIGHT, LEFT SIDE OF 'E' ZONE WILL NOT ILLUMINATE. REMOVED AND REPLACED CEILING LIGHT ASSEMBLY PER MM 33-51-00. OPS CHE
- [SDR TWRA9714](https://openairdocs.org/sdr/TWRA9714), Feb 9, 1997: EXIT SIGNS. INOPERATIVE. L/1-2, R/1-2 MED EXIT SIGNS OVER DOORS DO NOT ILLUMINATE. PERFORMED OPS CHECK PER MM 33-51-00. SYSTEM OPS NORMAL. (M)
- [SDR TWRA9736](https://openairdocs.org/sdr/TWRA9736), Feb 3, 1997: LIGHT. INOPERATIVE. CEILING EVAC LIGHT AT L-1 DOOR INOP. REMOVED AND REPLACED CEILING LIGHT PER MM 33-51-00. (M)
- [SDR TWRA9703](https://openairdocs.org/sdr/TWRA9703), Jan 4, 1997: LIGHT. INOPERATIVE. DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP AT SEAT 17 HJK. REMOVED AND REPLACED CEILING LIGHT PER MM 33-51-00. OPS CHECKED NORMAL. (M)
- [SDR TWRA96385](https://openairdocs.org/sdr/TWRA96385), Dec 26, 1996: LIGHT MODULE. INOPERATIVE. DURING DAILY CHECK, FOUND AIRCRAFT EVAC LIGHT WOULD NOT SHUT OFF AT 1L DOOR. (SHUTOFF AT FLIGHT DECK ONLY). CLEANED SWITCH AT L1 DOOR. OPS CHECK OK PER MM 33-51
- [SDR TWRA96308](https://openairdocs.org/sdr/TWRA96308), Sep 1, 1996: WIRE. BROKEN. DURING DAILY CHECK, FOUND SEAT 35C EVAC LIGHT INOP. REPAIRED BROKEN WIRE AT SEAT HARNESS. OPS CHECKED NORMAL PER MM 33-51-00. (M)
- [SDR TWRA96257](https://openairdocs.org/sdr/TWRA96257), Jul 31, 1996: BULB. FAILED. DURING DAILY CHECK, FOUND NR 4 RIGHT MED UPPER FORWARD SILL CEILING EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKED GOOD PER MM 33-51-00. (M)
- [SDR TWRA96194](https://openairdocs.org/sdr/TWRA96194), Jul 23, 1996: LIGHT. INOPERATIVE. DURING DAILY CHECK, FOUND EVAC CEILING LIGHT INOP BY SEATS 54HJK. REPLACED LIGHT ASSY AT SEAT 54HJK EMERGENCY LIGHT. OPS CHECK NORMAL PER MM 33-51-00. (M)
- [SDR TWRA96199](https://openairdocs.org/sdr/TWRA96199), Jul 22, 1996: BULB. FAILED. DURING DAILY CHECK, FOUND 5R MED SIDEWALL EXIT EVAC LIGHT INOP. RELAMPED, OPS CHECK NORMAL PER MM 33-51-00. (M)
- [SDR TWRA96178](https://openairdocs.org/sdr/TWRA96178), Jul 17, 1996: SMOKE DETECTOR. MALFUNCTION. IN CRUISE AT FL 390, LOWER FWD CARGO FIRE WARNING (BELL/LIGHTS) CAME ON. WHEN FIRE BOTTLE NR 1 WAS DISCHARGED, FIRE WARNING LIGHTS WENT OUT IMMEDIATELY. FM VOL,
- [SDR 96ZZZM1190](https://openairdocs.org/sdr/96ZZZM1190), Jul 17, 1996: AMPLIFIER. MALFUNCTION. IN CRUISE AT FL 390, LOWER FWD CARGO FIRE WARNING (BELL/LIGHTS) CAME ON. WHEN FIRE BOTTLE NR 1 WAS DISCHARGED, FIRE WARNING LIGHTS WENT OUT IMMEDIATELY. FM VOL,
- [SDR TWRA9691](https://openairdocs.org/sdr/TWRA9691), Jul 4, 1996: WIRE. BROKEN. DURING DAILY CHECK, FOUND 65H SEAT EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE, OPS CHECK NORMAL MM 33-51-00. (M)
- [SDR TWRA9672](https://openairdocs.org/sdr/TWRA9672), Jun 29, 1996: LIGHT. INOPERATIVE. DURING DAILY CHECK, MAINTENANCE FOUND CEILING EMERGENCY LIGHT INOPERATIVE IN AISLE OF AFT LAVATORY COMPLEX (N). REPLACED LIGHT ASSY. OPS CHECK OK MM-33-51-00. (
- [SDR TWRA9653](https://openairdocs.org/sdr/TWRA9653), Jun 24, 1996: WIRE. BROKEN. EMERGENCY EGRESS LIGHTS AT 1L FLIGHT ATTENDANT SEAT AND AT SEAT 31HJK ARE INOPERATIVE. FOUND BORKEN WIRES AND REPAIRED PER 33-51-00. OPSCHECK NORMAL. (M)
- [SDR TWRA9652](https://openairdocs.org/sdr/TWRA9652), Jun 24, 1996: LIGHT. INOPERATIVE. DURING DAILY SERVICE, FOUND EMERGENCY EGRESS LIGHT ON 4L MED UPPERBUSTLE INOPERATIVE. REMOVED AND REPLACED 4L MED UPPER BUSTLE LGIHTASSEMBLY. OPS CHECK OK.(M)
- [SDR TWRA9627](https://openairdocs.org/sdr/TWRA9627), May 9, 1996: OVEN. FAILED. DURING CRUISE, CABIN ATTENDANT REPORTED ELECTRICAL SMOKE COMING FROM UPPER DECK OVEN 704 CONTROLLER. PULLED CIRCUIT BREAKER AND REMOVED OVEN. ITEM WAS DEFERRED 
- [SDR TWRA9565](https://openairdocs.org/sdr/TWRA9565), Nov 26, 1995: FAIRING. MISSING. DURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON L
- [SDR 96ZZZM61](https://openairdocs.org/sdr/96ZZZM61), Nov 26, 1995: FAIRING. MISSING. DURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON L

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19951124042029I](https://openairdocs.org/incident/19951124042029I), Nov 24, 1995: Boeing 747100 (N602FF), Savannah, GA, Minor damage. Narrative: aircraft encountered light to moderate turbulence approximately 150 NM west of destination, Hunter army airfield, Savannah, GA. Crew felt momentary…

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