# Boeing 747-2D3B

- Type: Aircraft model (FAA registry)
- Registry code: 1384805
- Manufacturer (registry): BOEING
- Model: 747-2D3B
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 495
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-747-2d3b

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 (182, newest 50)

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

- [SDR UIEA200800335](https://openairdocs.org/sdr/UIEA200800335), Oct 30, 2008: FAIRING. DAMAGED. LT WING NR 1 CANOE FAIRING AT WBL 743.828 WAS DAMAGE ON CARGO LOADING. CANOE WAS REMOVED PER ATLAS DMI M08-227. AREAS OF CANOE AT FAIRING STA 147.766 LOWER SIDE
- [SDR UIEA2008002272](https://openairdocs.org/sdr/UIEA2008002272), Aug 1, 2008: SKIN. CHAFED. LEFT WING INBOARD FLAP, AFT FLAP S/N 000204 UPPER SKIN HAS 4 EACH AREAS OF CHAFING CAUSED BY LONG BOLTS ON MID-FLAP. AREAS ARE WBL 248.0, 297.0, 339.0 AND 425.0
- [SDR UIEA200800270](https://openairdocs.org/sdr/UIEA200800270), Jul 26, 2008: WIRE HARNESS. DAMAGED. NR 2 ENG SHUT DOWN IN FLIGHT DUE TO HIGH EGT INDICATION - EGT WAS READING 1047C FOR 70 SECONDS. FOUND EGT HARNESS DAMAGED. REMOVED AND REPLACED HARNESS AND OPS 
- [SDR UIEA200800210](https://openairdocs.org/sdr/UIEA200800210), May 14, 2008: MEC. FAILED. AT FL 320 ON DESCENT, NR 1 ENGINE N1, N2 AND EGT ROLLED BACK WITH NO THROTTLE RESPONSE. RESTART NO HELP. SHUT DOWN FOR LANDING. REPLACED NR 1 MEC PER AMM 73-21-
- [SDR UIEA200800183](https://openairdocs.org/sdr/UIEA200800183), May 8, 2008: MEC. FAILED. INFLIGHT ENGINE SHUTDOWN. AT TOD, DURING ENGINE THROTTLE BACK NR 1 ENGINE ROLLED BACK DOWN TO 30 PERCENT N1 WITH NO THROTTLE RESPONSE. CREW SHUT DOWN ENGINE AND
- [SDR UIEA200800182](https://openairdocs.org/sdr/UIEA200800182), May 6, 2008: FAN BLADE. BIRD INGESTION. BIRD STRIKE AT TAKEOFF TO FUSELAGE AND ENGINE NR 1 FAN BLADES. ACCOMPLISHED BIRD STRIKE INSPECTION FOR FUSELAGE AND NR 1 ENGINE AND OVERWEIGHT LANDING CHECKS AS
- [SDR UIEA200800161](https://openairdocs.org/sdr/UIEA200800161), Apr 27, 2008: SKIN. CRACKED. RT I/B ELEVATOR HAS A 2.0 INCH CRACK AT TRAILING EDGE OF ELEVATOR STA 154.0, CAUSED BY GROUND EQUIPMENT. ACCOMPLISHED INTERIM REPAIR AS PER B747-200 SRM 51-40-0
- [SDR UIEA200800151](https://openairdocs.org/sdr/UIEA200800151), Apr 15, 2008: PANEL. DAMAGED. LT WING UPPER SURFACE NR 5 SPOILER CENTER HINGE GAP PANEL DAMAGED, ALSO, INBOARD, OUTBOARD AND CENTER HINGE CUT-OUT AND FORWARD PANEL OF CENTER HINGE DAMAGED, S
- [SDR UIEA200800150](https://openairdocs.org/sdr/UIEA200800150), Apr 15, 2008: PANEL. DELAMINATED. RT WING UPPER FIXED TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS AN AREA OF 5.0 INCH BY 2.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747
- [SDR UIEA200800149](https://openairdocs.org/sdr/UIEA200800149), Apr 15, 2008: SKIN. CRACKED. MAIN ENTRY DOOR L-1 EXTERIOR SKIN, UPPER HINGE CUT-OUT PREVIOUS DOUBLER REPAIR, LOWER RADIUS CORNER IS CRACKED. VERIFIED CRACK WITH HFEC AS PER B747-200 NDT MAN
- [SDR UIEA200800110](https://openairdocs.org/sdr/UIEA200800110), Apr 6, 2008: SMOKE DETECTOR. MALFUNCTIONED. DIVERSION TO YJT DUE TO "MAIN DECK CARGO SMOKE DET ZONE 4 LIGHT ILLUMINATED WITH CARGO AND MASTER FIRE ANNUNCIATOR LIGHTS ILLUMINATED. AFTER LANDING RETESTED OK
- [SDR UIEA200800099](https://openairdocs.org/sdr/UIEA200800099), Apr 1, 2008: LEAD. CHAFED. REJECTED TAKEOFF, NR 3 EGT WENT TO OFF SCALE HIGH WITH RED BALL. NR 3 ENGINE EGT SHOWED 1074 DEGREES FOR 1 SEC. FOUND THERMOCOUPLE LEAD WAS DEFECTIVE WHILE PERF
- [SDR UIEA200800064](https://openairdocs.org/sdr/UIEA200800064), Feb 21, 2008: FITTING. CRACKED. AFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. AFTER DISASSEMBLY (REFERENCE SDR UIEA200800063) FOUND FORWARD POSITION ROTARY LIFT ACTUATOR FRAME REINFO
- [SDR UIEA200800063](https://openairdocs.org/sdr/UIEA200800063), Feb 21, 2008: FITTING. CRACKED. AFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. FOUND AFT POSITION ROTARY LIFT ACTUATOR FRAME REINFORCEMENT FITTING CRACKED. REPLACED FITTING 65B38174-3
- [SDR UIEA200800021](https://openairdocs.org/sdr/UIEA200800021), Jan 26, 2008: SKIN. CRACKED. LT WING LEADING EDGE LOWER SURFACE, OUTBOARD FUELING DOOR FRAME CUT-OUT HAS A COMPOSITE CRACK AT OUTBOARD SIDE, FORWARD EDGE. PERMANENT REPAIR ACCOMPLISHED AS P
- [SDR UIEA200800020](https://openairdocs.org/sdr/UIEA200800020), Jan 26, 2008: STRUCTURE. DELAMINATED. LT MAIN LANDING GEAR OUTBOARD STRUT DOOR HAS AN 18.0 INCH LONG SECTION AT LEADING EDGE OF MATERIAL SEPARATING. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09
- [SDR UIEA200800019](https://openairdocs.org/sdr/UIEA200800019), Jan 26, 2008: PANEL. DELAMINATED. RT WING NR 10 SPOILER PANEL HAS A 5.0 INCH BY 5.0 INCH AREA OF DELAMINATION AT UPPER SIDE, OUTBOARD, TRAILING EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-
- [SDR UIEA200800018](https://openairdocs.org/sdr/UIEA200800018), Jan 26, 2008: SKIN PANEL. DELAMINATED. RT WING LOWER FIXED LEADING EDGE HAS A 12.0 INCH LONG BY 10.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 18, SHEET 1,
- [SDR UIEA200800017](https://openairdocs.org/sdr/UIEA200800017), Jan 14, 2008: SMOKE DETECTOR. DIRTY. AIRCRAFT DIVERTED TO SNN DUE TO NR 4 CARGO LIGHT SMOKE DETECTOR LIGHT CAME ON IN CRUISE. NR 4 A/B SMOKE DETECTORS CLEANED AND OPS CHECKED IAW 26-14-00, OPS CHEC
- [SDR UIEA200700472](https://openairdocs.org/sdr/UIEA200700472), Nov 16, 2007: PANEL. DELAMINATED. RT WING LEADING EDGE, INBOARD OF LANDING LIGHTS, INTERIOR AREA OF LEADING EDGE, COMPOSITE SKIN IS DELAMINATED. AREA IS 64.0 INCH BY 20.0 INCH. INTERIM REPAIR WA
- [SDR UIEA200700467](https://openairdocs.org/sdr/UIEA200700467), Nov 2, 2007: PANEL. DELAMINATED. LT WING UPPER L/E FIXED PANEL BETWEEN AISLES 170.0 TO AISLES 630.72 HAS AN AREA DELAMINATION, AREA IS 58.0 INCH LONG BY 50.0 INCH WIDE. INTERIM REPAIR WAS ACCOM
- [SDR UIEA200700465](https://openairdocs.org/sdr/UIEA200700465), Oct 26, 2007: PANEL. DELAMINATED. UPPER SURFACE OF LEFT WING INBOARD NR 2 ENGINE FIBERGLASS HAS HOLE AND DENT. REPAIRED PER XEO 57-102607 TRANS TO NON MEL N07-126. REINSPECTED IN ORD AND ACCOMPL
- [SDR UIEA200700432](https://openairdocs.org/sdr/UIEA200700432), Oct 3, 2007: SENSOR. FAILED. AIR TURN BACK, AT ROTATION STICK SHAKER CAME ON AND STAYED ON UNTIL LANDING. VR SPEED WAS 129 KNOTS. REMOVED AND REPLACED LEFT AOA SENSOR AND STALL WARNING COMP
- [SDR UIEA200700427](https://openairdocs.org/sdr/UIEA200700427), Oct 1, 2007: SKIN. TORN. LT INBOARD ELEVATOR, TRAILING EDGE COMPOSITE SKIN TIP AREA HAD GROUND DAMAGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747 SRM 51-40-09, FIG 1A, SHEET 1 AND FIG 8,
- [SDR UIEA200700425](https://openairdocs.org/sdr/UIEA200700425), Oct 1, 2007: SKIN. DAMAGED. LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2613 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/
- [SDR UIEA200700422](https://openairdocs.org/sdr/UIEA200700422), Oct 1, 2007: SKIN. DAMAGED. FUSELAGE TAIL CONE LOWER AREA FROM FS 2742 TO 2792 SKIN AND FRAMES SCRAPED AND DENTED DUE TO TAIL DRAG. REMOVE AND REPLACED LOWER SECTION OF CONE FROM STA 2742 
- [SDR UIEA200700426](https://openairdocs.org/sdr/UIEA200700426), Oct 1, 2007: SKIN. DAMAGED. LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2594 TO 2604.0 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACE
- [SDR UIEA200700424](https://openairdocs.org/sdr/UIEA200700424), Oct 1, 2007: FRAME. DAMAGED. AFT LOWER FUSELAGE AT FS 2658 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 53-10-04 FIG 75 SHEETS 1 THRU 15. 
- [SDR UIEA200700423](https://openairdocs.org/sdr/UIEA200700423), Oct 1, 2007: FRAME. DAMAGED. AFT LOWER FUSELAGE AT FS 2638 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3, AND SRM 51-30-02. 
- [SDR UIEA200700353](https://openairdocs.org/sdr/UIEA200700353), Sep 4, 2007: SEAL. DAMAGED. AIR TURN BACK DUE TO NOSE GEAR DOOR OPEN INDICATION AFTER GEAR RETRACTION. FLIGHT CREW ADVISED, ACTUAL DOOR OPEN FAULT AND NOT INDICATION. AFTER ARRIVAL, MX INS
- [SDR UIEA200700250](https://openairdocs.org/sdr/UIEA200700250), Jun 16, 2007: PUMP. LEAKING. NR 2 HYD LEAK STOPPED WITH 1.8 GALLONS REMAINING. EDP TO SUPPLY OFF. REMOVED AND REPLACED HYD PUMP AND CASE DRAIN RETURN FILTER, OPS AND LEAK CHECKED OKAY.
- [SDR UIEA200700233](https://openairdocs.org/sdr/UIEA200700233), May 25, 2007: SKIN. DENTED. NR 3 ENGINE RT THRUST REVERSER EXTERIOR SKIN LOWER AREA AT 5 O'CLOCK POSITION HAS 3 EACH DENTS. PERMANENT REPAIR WAS ACCOMPLISHED AS PER GE CF6-50 ENGINE MANUAL
- [SDR UIEA200700145](https://openairdocs.org/sdr/UIEA200700145), Mar 26, 2007: WIRE. CHAFED. AFTER T/O FROM AMS, WHERE NR 3 ENGINE B LOOP WAS DEFERRED AS INOP. NR 3 ENGINE FIRE BELL AND LIGHT ILLUMINATED, NR 3 ENGINE A LOOP WAS ERRATIC AND WAS AT 10 ON 
- [SDR UIEA200700130](https://openairdocs.org/sdr/UIEA200700130), Mar 4, 2007: STRAP. CRACKED. CRACKS FOUND ON BS 800 LT STRAP AND INNER CHORD AT NR 2 MAIN ENTRY DOOR. REPAIRED ACCOMPLISHED IAW SR ID NR 1-289052431 AND FAA FORM 8100-9.
- [SDR UIEA200700125](https://openairdocs.org/sdr/UIEA200700125), Mar 2, 2007: SKIN. CORRODED. M/DECK RT NR 3 MED CUTOUT AFT UPPER CORNER SKIN STA1319, STR 17R-18R FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-289657194-1, 747 SRM 53-30
- [SDR UIEA200700128](https://openairdocs.org/sdr/UIEA200700128), Mar 2, 2007: DOUBLER. SEPARATED. NR 3 PYLON FWD FIXED FAIRING LT EXTERIOR SURFACE AFT CORNER SKIN DOUBLER SEPARATED. FAIRING REPLACED BUT NUMEROUS FASTENERS HOLES FOUND MISALIGNED. TIME LIMIT R
- [SDR UIEA200700124](https://openairdocs.org/sdr/UIEA200700124), Mar 2, 2007: BULKHEAD. CORRODED. BS 1250, L WLG W/W CANTED PRESSURE BULKHEAD, NR 2 PACK COOLING DUCT CUTOUT FOUND CORROSION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-289645346-1 THRU -5 A
- [SDR UIEA200700129](https://openairdocs.org/sdr/UIEA200700129), Mar 2, 2007: SKIN. CORRODED. FOUND M/DECK STA1241 FRAME AND SKIN SPLICE AREA HAS HOLE, CRACKED AND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-29020776-1 AND -6 AND FAA FORM 
- [SDR UIEA200700127](https://openairdocs.org/sdr/UIEA200700127), Mar 2, 2007: STRINGER. CORRODED. FWD CARGO COMPARTMENT STA 978, STR 47L FOUND CORRODED. FWD CARGO COMPARTMENT STA978, STR47L REPLACED AS PER SRM 51-10-01.
- [SDR UIEA200700126](https://openairdocs.org/sdr/UIEA200700126), Mar 2, 2007: INTERCOSTAL. CRACKED. UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 420, LBL 50. U/DECK FLOOR SUPPORT INTERCOSTAL AT BS420, LBL 50 REPLACED AS PER SRM 51-30-02.
- [SDR UIEA200700107](https://openairdocs.org/sdr/UIEA200700107), Mar 1, 2007: STRINGER. CRACKED. M/DECK ZONE "C" LT SIDEWALL STRUCTURE STA 905, STR-10L FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 53-10-03, FIG 4.
- [SDR UIEA200700106](https://openairdocs.org/sdr/UIEA200700106), Mar 1, 2007: KEELBEAM. BULGED. FOUND KEEL BEAM BOTH SIDES WEB BULGE FOUND AT BS 1450. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286690602-1 THRU -10.
- [SDR UIEA200700101](https://openairdocs.org/sdr/UIEA200700101), Feb 28, 2007: SHEAR TIE. CRACKED. RT STA 840 FWD CHANNEL TENSION TIE AT 12 O'CLOCK FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID 1-288425027-1 AND -6, 1-289012875-1, SB747-53-2502 AND
- [SDR UIEA200700100](https://openairdocs.org/sdr/UIEA200700100), Feb 28, 2007: SKIN. CRACKED. NR 3 ENGINE LT CORE COWL SKIN BOND DOUBLER CRACKED AT AIR EXHAUST DUCT AFT LOWER PORTION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286833874-1 THRU -6, DW
- [SDR UIEA200700099](https://openairdocs.org/sdr/UIEA200700099), Feb 28, 2007: SKIN. PUNCTURED. NR 20 VC FLAP FOLDING NOSE I/B END SKIN PUNCHED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290202458-1 THRU -3 AND FAA FORM 8100-9.
- [SDR UIEA200700098](https://openairdocs.org/sdr/UIEA200700098), Feb 28, 2007: STRINGER. CRACKED. M/DECK LT SIDE STA 875, STR9L FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03, FIG.4
- [SDR UIEA200700097](https://openairdocs.org/sdr/UIEA200700097), Feb 28, 2007: CREASE BEAM. CRACKED. M/DECK RTH SIDE STA 940, S-8R CREASE BEAM WEB FOUND CRACKED. CREASE BEAM WEB REPLACED AS PER SRM 51-10-01 AND 51-30-02.
- [SDR UIEA200700096](https://openairdocs.org/sdr/UIEA200700096), Feb 28, 2007: STRINGER. CORRODED. FOUND FWD CARGO COMPT STA 980, STR 43R IS CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.
- [SDR UIEA200700095](https://openairdocs.org/sdr/UIEA200700095), Feb 28, 2007: CREASE BEAM. CRACKED. FOUND M/DECK STA960, S-7R CREASE BEAM SUPPORT ANGLE FOUND CRACKED. CREASE BEAM SUPPORT WEB REPLACED AS PER SRM 51-10-01.
- [SDR UIEA200700094](https://openairdocs.org/sdr/UIEA200700094), Feb 28, 2007: STRINGER. CRACKED. M/DECK STA 895 STR 7R FOUND CRACKED. STRINGER REPAIRED ACCOMPLISHED AS PER SRM 53-10-03 FIG 4.

All 182: https://openairdocs.org/model/boeing-747-2d3b/reports.md

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