# Boeing 747-4EVF

- Type: Aircraft model (FAA registry)
- Registry code: 13848EA
- Manufacturer (registry): BOEING
- Model: 747-4EVF
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 660
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-747-4evf

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (9)

As reported by operators and repair stations, by the model named in the report.

- [SDR Q2SA20150430223](https://openairdocs.org/sdr/Q2SA20150430223), Apr 30, 2015: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK IS GOUGED BETWEEN BS 1900 AND 1920 LBL 98.58. INSTALLED ALL REPAIR PARTS, SEAT TRACK REPAIR SECTION, 8 EA REPAIR ANGLES AND 2 EA REPAIR ST
- [SDR Q2SA20150430222](https://openairdocs.org/sdr/Q2SA20150430222), Apr 30, 2015: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK IS GOUGED BETWEEN STA 1780 AND 1800, LBL 98.58. INSTALLED REPLACEMENT SECTION SEAT TRACK & REPAIR PARTS ON STA 1740 - 1800 IAW EA 747-5360
- [SDR Q2SA20150428221](https://openairdocs.org/sdr/Q2SA20150428221), Apr 28, 2015: FASTENER. MISINSTALLED. RT SIDE FUSELAGE SKIN, BS 2517 - 2628 HAS 58 PROTRUDING FASTENER HEADS AT RUB STRIP. REF AD 2013-26-12. ACCOMPLISH 747-5380-33-A5764.
- [SDR Q2SA20150428220](https://openairdocs.org/sdr/Q2SA20150428220), Apr 28, 2015: SKIN. SCRATCHED. SKIN PANEL SCRATCH IS OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REPAIRED IAW EA 747-5380-33-A5693.
- [SDR Q2SA20150118215](https://openairdocs.org/sdr/Q2SA20150118215), Jan 18, 2015: KEELBEAM. CORRODED. KEEL BEAM BOTTOM WEB AND DOUBLER HAS CORROSION IN 16 AREAS BETWEEN BS 990 AND 1070. CLEANED CORROSION, CHECKED REMAINING THICKNESS, AND RESTORED FINISH. ALL WOR
- [SDR Q2SA20150105214](https://openairdocs.org/sdr/Q2SA20150105214), Jan 5, 2015: FLOORBEAM. CRACKED. AFT CARGO FLOORBEAM UPPER CAP HAS 2 CRACKS BS 1840, RBL 5 TO LBL 5. REPAIRED IAW EA 747-5360-33-A5712.
- [SDR Q2SA20150104216](https://openairdocs.org/sdr/Q2SA20150104216), Jan 4, 2015: STRUCTURE. GOUGED. FWD CARGO DOOR LOWER AFT CORNER IS GOUGED. REPAIRED IAW EA 747-5234-33-A5694.
- [SDR EPHR20140926002](https://openairdocs.org/sdr/EPHR20140926002), Sep 22, 2014: RIB. BROKEN. DURING ACCOMPLISHMENT OF A FLAP CARRIAGE CHANGE ON THE RT WING, IT WAS NOTED THE T/E RIB ASSY AT WBL 516 WAS BROKEN INTO TWO PIECES. THE DAMAGE WAS REPAIRED BY 
- [SDR EPHR20140926001](https://openairdocs.org/sdr/EPHR20140926001), Sep 22, 2014: RIB. BROKEN. DURING ACCOMPLISHMENT OF A FLAP CARRIAGE CHANGE ON THE LT WING, IT WAS NOTED THE T/E RIB ASSEMBLY, AT WBL 516 WAS BROKEN INTO TWO PIECES. REPAIRED BY REPLACEMEN

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