# Boeing 747-SR-46

- Type: Aircraft model (FAA registry)
- Registry code: 1384816
- Manufacturer (registry): BOEING
- Model: 747-SR-46
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 494
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-747-sr-46

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 (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 19931021044109I](https://openairdocs.org/incident/19931021044109I), Oct 21, 1993: Boeing 747SR46 (N478EV), Chicago, IL. Evergreen airlines called FAA in new york. Had reason to suspect pilot intoxicated. Crew given alcohol tests.

## Service difficulty reports (412, newest 50)

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

- [SDR EIAA20090028](https://openairdocs.org/sdr/EIAA20090028), Feb 23, 2009: SEAT TRACK. DAMAGED. MAIN DECK CARGO TRACK DAMAGED FROM STA 1880 TO 1980 AT LBL 33.99. REPAIRED PER SRM 53-10-05 FIG 1A.
- [SDR KCSA081221](https://openairdocs.org/sdr/KCSA081221), Apr 9, 2008: FRAME. DAMAGED. BS 1760 FUSELAGE FRAME LOWER CHORD DAMAGED BETWEEN STR-39R AND STR-40R.
- [SDR KCSA081220](https://openairdocs.org/sdr/KCSA081220), Apr 9, 2008: FLOORBEAM. CRACKED. UPPER DECK FLOORBEAM UPPER CHORD CRACKED AT BS 360, 18TH HOLE FROM LT SIDE
- [SDR KCSA081219](https://openairdocs.org/sdr/KCSA081219), Mar 31, 2008: FLOOR SUPPORT. DAMAGED. FLOOR SUPPORT DAMAGED AT STA-2100 RBL-36.
- [SDR KCSA081218](https://openairdocs.org/sdr/KCSA081218), Mar 31, 2008: STRINGER. CORRODED. STR-48R CORRODED AT BS 1480 ON O/B SIDE.
- [SDR KCSA081216](https://openairdocs.org/sdr/KCSA081216), Mar 28, 2008: CAP. DENTED. FWD CARGO STA-920 LBL-12 UPPER CAP DENTED.
- [SDR KCSA081215](https://openairdocs.org/sdr/KCSA081215), Mar 28, 2008: FRAME. BENT. FRAME BENT BETWEEN STA-2180 AND STA-2200 LBL-28.
- [SDR KCSA081214](https://openairdocs.org/sdr/KCSA081214), Mar 28, 2008: FRAME. BENT. FRAME BENT BETWEEN STA-2200 AND STA-2220 LBL-28.
- [SDR KCSA081213](https://openairdocs.org/sdr/KCSA081213), Mar 28, 2008: FRAME. BENT. FRAME BENT AFT OF BULKHEAD 2160 RBL-32.
- [SDR KCSA081212](https://openairdocs.org/sdr/KCSA081212), Mar 28, 2008: PRESSURE PANEL. CORRODED. BELOW MAIN DECK FLOOR UPPER WHEEL WELL PRESSURE WEB SURFACE HAS CORROSION AT BS 1460 LBL-69.
- [SDR KCSA081211](https://openairdocs.org/sdr/KCSA081211), Mar 26, 2008: SKIN. DAMAGED. STA-1760 STR-38R SKIN DAMAGED.
- [SDR KCSA081210](https://openairdocs.org/sdr/KCSA081210), Mar 26, 2008: STIFFENER. DAMAGED. STA-1920 BETWEEN STR-34L AND STR-35L FRAME STIFFENER HAS DAMAGED FLANGE.
- [SDR KCSA081208](https://openairdocs.org/sdr/KCSA081208), Mar 26, 2008: WEB. CRACKED. FWD PIT BILGE TORQUE BOX UPPER WEB CRACKED AT BS 866, LBL-3.
- [SDR KCSA081207](https://openairdocs.org/sdr/KCSA081207), Mar 26, 2008: FRAME. DENTED. FWD PIT FUSELAGE FRAME UPPER CHORD DENTED AT BS 800.
- [SDR KCSA081206](https://openairdocs.org/sdr/KCSA081206), Mar 26, 2008: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK CORRODED AT BS 1800, LBL-99.
- [SDR KCSA081205](https://openairdocs.org/sdr/KCSA081205), Mar 25, 2008: STRINGER CLIP. DAMAGED. STRINGER CLIP DAMAGED AT BS 1520, STR-33R.
- [SDR KCSA081201](https://openairdocs.org/sdr/KCSA081201), Mar 24, 2008: TENSION TIE. BROKEN. FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1840 AND 1860 ABOVE STR-36L.
- [SDR KCSA081200](https://openairdocs.org/sdr/KCSA081200), Mar 24, 2008: TENSION TIE. BROKEN. FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1860 AND 1880 ABOVE STR-36L.
- [SDR KCSA081199](https://openairdocs.org/sdr/KCSA081199), Mar 24, 2008: TENSION TIE. BROKEN. FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1880 AND 1900 ABOVE STR-36L.
- [SDR KCSA081197](https://openairdocs.org/sdr/KCSA081197), Mar 21, 2008: STIFFENER. DAMAGED. STA-1760 FRAME STIFFENER DAMAGED AT RBL-65.
- [SDR KCSA081196](https://openairdocs.org/sdr/KCSA081196), Mar 21, 2008: STIFFENER. DAMAGED. STA-1580 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18.
- [SDR KCSA081195](https://openairdocs.org/sdr/KCSA081195), Mar 21, 2008: FRAME. DAMAGED. STA-1780 FRAME WEB DAMAGED AT RBL-17 ABOVE STR-43R.
- [SDR KCSA081194](https://openairdocs.org/sdr/KCSA081194), Mar 21, 2008: FRAME. DAMAGED. STA-1760 RBL-16 FRAME WEB DAMAGED AROUND FASTENERS.
- [SDR KCSA081193](https://openairdocs.org/sdr/KCSA081193), Mar 21, 2008: SKIN. DAMAGED. STA-400 STR-39R TO STR-40R AT BUTT SPLICE AREA SKIN DAMAGED.
- [SDR KCSA081189](https://openairdocs.org/sdr/KCSA081189), Mar 20, 2008: DOOR FRAME. CRACKED. R-2 DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS APPROX 11 INCHES.
- [SDR KCSA081188](https://openairdocs.org/sdr/KCSA081188), Mar 20, 2008: STIFFENER. DAMAGED. STA-1540 FRAME VERTICAL STIFFENER DAMAGE AT RBL-14.
- [SDR KCSA081187](https://openairdocs.org/sdr/KCSA081187), Mar 20, 2008: FRAME. DAMAGED. STA-1600 FRAME UPPER CHORD DAMAGED AT RBL-15.
- [SDR KCSA081186](https://openairdocs.org/sdr/KCSA081186), Mar 20, 2008: STIFFENER. DAMAGED. STA-1740 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18.
- [SDR KCSA081185](https://openairdocs.org/sdr/KCSA081185), Mar 20, 2008: SKIN. CORRODED. STA-2120 STR-39R TO STR-41R AREAS OF CORROSION AROUND FASTENERS.
- [SDR KCSA081183](https://openairdocs.org/sdr/KCSA081183), Mar 19, 2008: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 530 BETWEEN STR 41L & 42L.
- [SDR KCSA081178](https://openairdocs.org/sdr/KCSA081178), Mar 15, 2008: INTERCOSTAL. CRACKED. FUSELAGE FRAME INTERCOSTAL IS CRACKED BETWEEN STA 2220 & 2240, RBL 46 STR 43R.
- [SDR KCSA081177](https://openairdocs.org/sdr/KCSA081177), Mar 15, 2008: STRAP. CRACKED. AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2160, LBL 28.
- [SDR KCSA081176](https://openairdocs.org/sdr/KCSA081176), Mar 15, 2008: STRAP. MISSING. AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS MISSING A SECTION AT STA 2160, LBL 6.
- [SDR KCSA081174](https://openairdocs.org/sdr/KCSA081174), Mar 13, 2008: SKIN. CRACKED. L3 WINDOW, AFT LOWER CORNER EXTERIOR FUSELAGE SKIN HAS A CRACK EXTENDING FROM FASTENER HOLE .250 INCH LONG AT STA 338, STR 8L.
- [SDR KCSA081170](https://openairdocs.org/sdr/KCSA081170), Mar 11, 2008: FITTING. CRACKED. MAIN ENTRY DOOR 1R UPPER AFT CORNER FITTING CRACKED BS 485.
- [SDR KCSA081169](https://openairdocs.org/sdr/KCSA081169), Mar 11, 2008: DOOR FRAME. CRACKED. MAIN ENTRY DOOR 2L FWD LOWER CORNER FRAME CRACKED BS 808.
- [SDR KCSA081168](https://openairdocs.org/sdr/KCSA081168), Mar 11, 2008: DOOR FRAME. CRACKED. MAIN ENTRY DOOR 4R LOWER AFT CORNER FRAME CRACKED AT PREVIOUS STOP DRILL.
- [SDR KCSA081167](https://openairdocs.org/sdr/KCSA081167), Mar 11, 2008: DOOR FRAME. CRACKED. MAIN ENTRY DOOR 4R TOP AFT CORNER FRAME CRACKED BS 1700.
- [SDR KCSA071464](https://openairdocs.org/sdr/KCSA071464), Oct 11, 2007: BULKHEAD. CHAFED. NR 4 PYLON FWD ENGINE MOUNT BULKHEAD CHORD HAS CHAFING ON FWD OF NAC STA 128.
- [SDR KCSA071459](https://openairdocs.org/sdr/KCSA071459), Oct 10, 2007: STIFFENER. CORRODED. LEFT WING FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT FS 1280.
- [SDR KCSA071455](https://openairdocs.org/sdr/KCSA071455), Oct 8, 2007: BULKHEAD. WORN. NR 4 PYLON HYD LINE B-NUT WORN INTO NAC STA 221.9 BULKHEAD.
- [SDR KCSA071454](https://openairdocs.org/sdr/KCSA071454), Oct 8, 2007: BULKHEAD. WORN. NR 3 PYLON ENG PRESSURE LINE AT NAC STA 221.9 WORN INTO BULKHEAD.
- [SDR KCSA071445](https://openairdocs.org/sdr/KCSA071445), Oct 7, 2007: STOP FITTING. CRACKED. DOOR STOP BACKUP FITTING CRACKED AT BS 1265, STR 22L.
- [SDR KCSA071444](https://openairdocs.org/sdr/KCSA071444), Oct 7, 2007: WEB. DAMAGED. AFT PIT BILGE TORQUE BOX UPPER WEB DAMAGED AT PREVIOUS REPAIR BETWEEN BS 1660 AND 1680, BL 0.
- [SDR KCSA071380](https://openairdocs.org/sdr/KCSA071380), Sep 18, 2007: STRINGER. CRACKED. STR 38L CRACKED BETWEEN BS 480 AND 500.
- [SDR EIA2007154](https://openairdocs.org/sdr/EIA2007154), Aug 29, 2007: ENGINE. OIL CONSUMPTION. PASSING THROUGH FL 200, NR 4 OIL QTY WENT TO "0", OIL TEMP REDLINED, OIL PRESSURE 5 PSI. ENGINE SHUT-DOWN AND RETURNED TO SUU STATION. AIRCRAFT FERRIED TO MZJ A
- [SDR KSCA07062](https://openairdocs.org/sdr/KSCA07062), Aug 8, 2007: UNKNOWN. SMOKE. AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZE
- [SDR KCSA07062](https://openairdocs.org/sdr/KCSA07062), Aug 8, 2007: ENGINE. MALFUNCTIONED. AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZE
- [SDR EIA2007121](https://openairdocs.org/sdr/EIA2007121), Jun 4, 2007: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN THE UPPER DECK STAIR WELL LIGHT ASSY INOP. REMOVE AND REPLACE EMERGENCY LIGHT AT UPPER DECK STAIRWAY PER B747MM 33-51-07. OPS CHECKED GOOD PE
- [SDR EIA2007120](https://openairdocs.org/sdr/EIA2007120), Jun 4, 2007: LIGHT. BURNED OUT. SELF CONTAINED EMERGENCY EXIT LIGHT AT L-5 INOP. REMOVED AND REPLACED SELF CONTAINTED EMERGENCY LIGHT AT L-5 DOOR LOCATION PER B747 MM 33-51-06. OPS CKD GOOD PE

All 412: https://openairdocs.org/model/boeing-747-sr-46/reports.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.