# Boeing 747-200

- Type: Aircraft model (FAA registry)
- Registry code: 1384847
- Manufacturer (registry): BOEING
- Model: 747-200
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 490
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-747-200

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 19910423016579I](https://openairdocs.org/incident/19910423016579I), Apr 23, 1991: Boeing 72722C (N727CK), Lexington, KY, Minor damage. Left outboard main gear tire blew on departure. Continued to destination airport. Landed safely.

## Service difficulty reports (651, newest 50)

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

- [SDR 2010FA0000478](https://openairdocs.org/sdr/2010FA0000478), May 17, 2010: STIFFENER. CRACKED. PYLON NR 2 STIFFENER NR 3 CRACK
- [SDR 2010FA0000477](https://openairdocs.org/sdr/2010FA0000477), May 17, 2010: STIFFENER. CRACKED. PYLON NR 1 STIFFENER LOWER FLANGE NO.3 CRACK AT NAC. STA.256
- [SDR UPS09454498](https://openairdocs.org/sdr/UPS09454498), Jan 13, 2009: SLIDE. OUT OF POSITION. INSPECTION TYPE:C R1 DOOR - UNABLE TO STOW LWR DOOR LINING FLAP PNL DUE TO OBSTRUCTION BY DOOR SLIDE RAFT. R1 DOOR LWR LINING REMOVED PER AMM 25-23-07-400-802 R
- [SDR UPS08451380](https://openairdocs.org/sdr/UPS08451380), Jan 5, 2008: SIGN. INOPERATIVE. INSPECTION TYPE:N/A EXIT SIGN, LT & FWD OF UPPER DECK RT DOOR INOP. PREVIOUSLY DEACTIVITED, APPLIED DEACTIVATED PLACARD PER EO B747-3350-15296-B.
- [SDR UPS08451372](https://openairdocs.org/sdr/UPS08451372), Jan 3, 2008: CADC. MALFUNCTIONED. INSPECTION TYPE:N/A ATB - RVSM - CAPTAINS ALTIMETER 1500' OF ALTITUDE AT 330, WENT TO ALT STATIC SOURCE. AS PER MM 34-11-00 AND 34-12-01 INSP NR 1 CADC AND PITO
- [SDR UPS07450908](https://openairdocs.org/sdr/UPS07450908), Oct 10, 2007: STRINGER. DAMAGED. STR 45L DAMAGED. REMOVED STR 45L DAMAGE AS PER SRM 53-10-03. FABRICATED SPLICES FOR REPAIR AS PER SRM 53-10-03. INSTALLED NEW STRINGER AND SPLICES AS PER SRM 53
- [SDR UPS07450487](https://openairdocs.org/sdr/UPS07450487), Aug 23, 2007: BATTERY PACK. LOOSE. INSPECTION TYPE:N/A EMERGENCY -EXIT- SIGN AT CREW SERVICE DOOR INOP. FOUND BATTERY PACK LOOSE. SECURED, OPERATIONAL NORMAL PER AMM 33-51-02.
- [SDR UPS07450578](https://openairdocs.org/sdr/UPS07450578), Aug 17, 2007: STIFFENER. CRACKED. INSPECTION TYPE:C NR 2 PYLON RIGHT UPPER STIFFENER FOUND CRACKED JUST AFT OF FWD ENGINE MOUNT NR 13 HOLE AT INTERNAL ANGLE (1.125 INCH APPROX). NR 2 PYLON AFT O
- [SDR UPS07450579](https://openairdocs.org/sdr/UPS07450579), Aug 14, 2007: ANGLE. CRACKED. INSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM AFT SIDE O/B ANGLE CRACKED AS MARKED (CRACK LENGTH .75 INCH). NR 2 PYLON REAR EN
- [SDR UPS07450511](https://openairdocs.org/sdr/UPS07450511), Aug 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND SUSPECTED CRACK. CRACK LENGTH .3125 INCH. NR 3 PYLON REAR ENG
- [SDR UPS07450493](https://openairdocs.org/sdr/UPS07450493), Aug 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C NR 1 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED (CRACK LENGTH .375 INCH). NR 1 PYLON REAR ENGINE M
- [SDR UPS07450492](https://openairdocs.org/sdr/UPS07450492), Aug 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C NR 4 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED. CRACK LENGTH .3125 INCH APPROX. NR 4 PYLON REAR ENGI
- [SDR UPS07450581](https://openairdocs.org/sdr/UPS07450581), Aug 13, 2007: RIB. CRACKED. INSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B & I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 22
- [SDR UPS07450580](https://openairdocs.org/sdr/UPS07450580), Aug 13, 2007: RIB. CRACKED. INSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B AND I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 277-4) FWD SIDE (CRACK LENGTH 
- [SDR UPS07450501](https://openairdocs.org/sdr/UPS07450501), Aug 13, 2007: FITTING. CORRODED. INSPECTION TYPE:C RIGHT BLG WHEEL WELL DOOR FWD SIDE INTERNAL FITTING FOUND CORROSION. CORROSION BLEND OUT 0.045" X 1" X 3" RIGHT B/G WHEEL WELL DOOR FWD SIDE I
- [SDR UPS07450513](https://openairdocs.org/sdr/UPS07450513), Aug 11, 2007: FITTING. CRACKED. INSPECTION TYPE:C M/D R3 DOOR CUTOUT FWD LWR CORNER FITTING CRACKED. CRACK LENGTH .5 INCH. M/D R3 DOOR CUTOUT FWD LWR CORNER FITTING REPLACED AS PER SRM 51-10-0
- [SDR UPS07450527](https://openairdocs.org/sdr/UPS07450527), Aug 10, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND 1 EA HOLE CRACK AT WEB DOUBLER AT STR 11R LOCATION. M/D RIGHT BS 820 TENSION TIE TO FRA
- [SDR UPS07450534](https://openairdocs.org/sdr/UPS07450534), Aug 9, 2007: FRAME. CRACKED. INSPECTION TYPE:C AFT CARGO COMPT STA 1580 FRAME FOUND CRACK ADJACENT TO SIDE GUIDE SUPPORT BRACKET AT S39R. CRACK LEGNTH .25 INCH. AFT CARGO COMPT BS 1580 STR 
- [SDR UPS07450533](https://openairdocs.org/sdr/UPS07450533), Aug 9, 2007: FRAME. CRACKED. INSPECTION TYPE:C AFT CARGO COMPT STA 1600 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA STR 39R. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1
- [SDR UPS07450532](https://openairdocs.org/sdr/UPS07450532), Aug 9, 2007: FRAME. CRACKED. INSPECTION TYPE:C AFT CARGO COMPT STA 1560 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA AT STR 39R. CRACK LENGTH .3125 INCH. AFT CARGO COMPT 
- [SDR UPS07450531](https://openairdocs.org/sdr/UPS07450531), Aug 9, 2007: FRAME. CRACKED. INSPECTION TYPE:C AFT CARGO COMPT STA 1540 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA AT S39R. CRACK LENGTH .25 INCH. AFT CARGO COMPT BS 15
- [SDR UPS07450512](https://openairdocs.org/sdr/UPS07450512), Aug 9, 2007: LONGERON. CRACKED. INSPECTION TYPE:C RIGHT W/G WHEEL WELL STA 1248 LONGERON CRACK APPROX 0.850 INCH AS MARKED. RIGHT W/G WHEEL WELL BETWEEN BS 1244 TO BS 1270 O/B LONGERON REPAIRE
- [SDR UPS07450500](https://openairdocs.org/sdr/UPS07450500), Aug 9, 2007: ANGLE. CORRODED. INSPECTION TYPE:C RIGHT W/G WHEEL WELL STA 1319 VERTICAL ANGLE ATTACHED TO LONGERON FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.065" X .5" X 4" , HAS EXCEE
- [SDR UPS07450499](https://openairdocs.org/sdr/UPS07450499), Aug 9, 2007: RIB. CORRODED. INSPECTION TYPE:C RIGHT BLG I/B WHEEL WELL DOOR FWD AREA FOUND BULGE AS MARKED. RIGHT BLG I/B WHEEL WELL DOOR FWD SUPPORT RIB REPLACED AS PER SRM 51-10-01 PG 9 
- [SDR UPS07450491](https://openairdocs.org/sdr/UPS07450491), Aug 9, 2007: SUPPORT FITTING. WORN. INSPECTION TYPE:C RIGHT BLG I/B WHEEL WELL DOOR FWD INTERIOR DOOR SUPPORT FITTING FOUND WORN. RIGHT BLG I/B WHEEL WELL DOOR FWD INTERIOR DOOR SUPPORT FITTING RE
- [SDR UPS07450530](https://openairdocs.org/sdr/UPS07450530), Aug 8, 2007: SHEAR WEB. CRACKED. INSPECTION TYPE:C M/D BETWEEN TENSION TIE RIGHT SLOPING SHEAR WEB CRACKED AT BS 820. CRACK LENGTH 1.5 INCH. M/D BETWEEN BS 820 TO BS 840 TENSION TIE RIGHT SLOPI
- [SDR UPS07450529](https://openairdocs.org/sdr/UPS07450529), Aug 7, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C M/D LEFT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 12 HOLE CRACK AT FRAME WEB DOUBLER. M/D LEFT BS 820 TENSION TIE TO FRAME ATTACH DOUBL
- [SDR UPS07450528](https://openairdocs.org/sdr/UPS07450528), Aug 7, 2007: CHANNEL. DAMAGED. INSPECTION TYPE:C M/D LEFT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 20, 23, 24 HOLE WITH PILOT HOLE AT AFT CHANNEL. M/D LEFT BS 820 TENSION TIE TO FRAME 
- [SDR UPS07450521](https://openairdocs.org/sdr/UPS07450521), Aug 7, 2007: CHANNEL. DAMAGED. INSPECTION TYPE:C M/D RIGHT BS 940 TENSION TIE TO FRAME CONNECTION FOUND NR 4 HOLE CRACK AT FWD CHANNEL RUNNING DOWN. CRACK LENGTH 0.060 INCH. M/D RIGHT BS 940 
- [SDR UPS07450520](https://openairdocs.org/sdr/UPS07450520), Aug 7, 2007: CHANNEL. DAMAGED. INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 23 AND 24 HOLE WITH PILOT HOLE. M/D RIGHT BS 820 TENSION TIE TO FRAME AFT CHANNEL NR
- [SDR UPS07450518](https://openairdocs.org/sdr/UPS07450518), Aug 7, 2007: FRAME. CRACKED. INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT FRAME WEB. CRACK LENGTH .0625 INCH APPROX. M/D RIGHT BS 820 TENSION
- [SDR UPS07450516](https://openairdocs.org/sdr/UPS07450516), Aug 7, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C M/D LEFT BS 900 TENSION TIE TO FRAME CONNECTION FOUND NR 5 AND 13 HOLE CRACK AT FWD CHANNEL. CRACK LENGTH 0.030" AND 0.040". M/D LEFT BS 900 T
- [SDR UPS07450515](https://openairdocs.org/sdr/UPS07450515), Aug 7, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C M/D RIGHT BS 900 TENSION TIE TO FRAME CONNECTION FOUND NR 5, 13, 14 HOLE CRACK AT FWD CHANNEL. CRACK LENGTH 0.030", 0.040", 0.060". M/D RIGHT 
- [SDR UPS07450514](https://openairdocs.org/sdr/UPS07450514), Aug 7, 2007: SKIN. CRACKED. INSPECTION TYPE:C U/D RIGHT BS 340 - 360 S6R LAP JOINT TOP ROW FASTENER ROW 1EA HOLE FOUND CRACK AT FX SKIN RUNNING AFT APPROX .125 INCH BEYOND RIVET HEAD. FX S
- [SDR UPS07450526](https://openairdocs.org/sdr/UPS07450526), Aug 6, 2007: CHANNEL. DAMAGED. INSPECTION TYPE:C M/D RIGHT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 20 HOLE OVAL AT AFT CHANNEL. M/D RIGHT BS 840 TENSION TIE TO FRAME AFT CHANNEL NR 20
- [SDR UPS07450525](https://openairdocs.org/sdr/UPS07450525), Aug 6, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 3 HOLE CRACK AT FRAME WEB DOUBLER RUNNING UP. CRACK LENGTH 0.030 INCH. M/D RIGHT BS 
- [SDR UPS07450524](https://openairdocs.org/sdr/UPS07450524), Aug 6, 2007: FAILSAFE. CRACKED. INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT FAILSAFE CHORD RUNNING UP. CRACK LENGTH 0.040 INCH. M/D LEFT BS 880 
- [SDR UPS07450523](https://openairdocs.org/sdr/UPS07450523), Aug 6, 2007: FITTING. CRACKED. INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT TIE CLIP RUNNING DOWN. CRACK LENGTH 0.040 INCH. M/D LEFT BS 880 STR 
- [SDR UPS07450522](https://openairdocs.org/sdr/UPS07450522), Aug 6, 2007: FITTING. CRACKED. INSPECTION TYPE:C M/D RIGHT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT TIE CLIP RUNNING UP AND DOWN. CRACK LENGTH 0.040 INCH. M/D RIGHT BS
- [SDR UPS07450519](https://openairdocs.org/sdr/UPS07450519), Aug 6, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 6, 7, 16 HOLE CRACK AT AFT CHANNEL. CRACK LENGTH 0.030 INCH. M/D LEFT BS 880 TENSION 
- [SDR UPS07450517](https://openairdocs.org/sdr/UPS07450517), Aug 6, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C M/D LEFT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 4 HOLE CRACK AT FWD CHANNEL RUNNING UP AND DOWN. CRACK LENGTH 0.040 INCH. M/D LEFT BS
- [SDR UPS07450412](https://openairdocs.org/sdr/UPS07450412), Jul 27, 2007: FIRE LOOP. DAMAGED. INSPECTION TYPE:N/A ON CLIMBOUT THE FWD PANEL FIRE DETECTION LIGHT WAS FLICKERING; NR 4 ENGINE NACELLE TEMP IND -A- WAS FLICKERING FROM 0 TO 9 AT SAME TIME & RA
- [SDR UPS07450171](https://openairdocs.org/sdr/UPS07450171), Jul 15, 2007: FLOOR PANEL. CRACKED. 3.5 INCH CRACK IN BULK CARGO COMPARTMENT FLOOR BETWEEN OBI BOXES. REPAIRED IAW SRM 51-40-02 FIG 1.
- [SDR UPS07450142](https://openairdocs.org/sdr/UPS07450142), Jul 10, 2007: O-RING. CUT. INSPECTION TYPE:N/A HYDRAULIC SYSTEM NR 1 FLUID LOSS IN FLIGHT. FOUND CUT O-RING ON LEFT NOSE WHEEL STEERING ACT TRANSFER TUBE. REPLACED SEALS IAW 32-51-05. OPS
- [SDR UPS07450174](https://openairdocs.org/sdr/UPS07450174), Jul 5, 2007: SKIN. CHIPPED. INSPECTION TYPE:C NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE CHIPPED AT 5 O`CLOCK POSITION. CRACK LENGTH .1875 INCH. NR 3 ENGINE AFT EXHAUST SLEEVE E
- [SDR UPS07450189](https://openairdocs.org/sdr/UPS07450189), Jul 4, 2007: SKIN. DENTED. INSPECTION TYPE:C EMP RIGHT TAIL CONE SKIN SURFACE FOUND A DENT MARK AT STA 2755 BETWEEN 17R & 18R. EMP RIGHT TAIL CONE SKIN BS 2750 TO 2762 STR 17R - 18R AREA 
- [SDR UPS07450335](https://openairdocs.org/sdr/UPS07450335), Jul 3, 2007: PLATE. MISINSTALLED. INSPECTION TYPE: C M/D BS 940 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST IB FASTENER HOLE FOUND SHORT EDGE MARGIN. M/DECK BS 940 RT TENSION TIE FWD ATTAC
- [SDR EIA2007124](https://openairdocs.org/sdr/EIA2007124), Jun 5, 2007: LIGHT. NO TEST. RT DOOR 5R EMERGENCY LIGHT INOP. REMOVED AND REPLACED 5R EMERGENCY EXIT LIGHT ASSY PER B747 MM 33-51-00.
- [SDR UPS07449644](https://openairdocs.org/sdr/UPS07449644), Apr 19, 2007: SKIN. DELAMINATED. INSPECTION TYPE:N/A NR 5 FLT SPOILER HAS UPPER SURFACE SKIN PEELING BACK AND DELAMINATED APPROX 25 PERCENT OF SURFACE AREA. REMOVED AND REPLACED NR 5 FLT SPOILE
- [SDR EIA2007062](https://openairdocs.org/sdr/EIA2007062), Apr 1, 2007: FIRE LOOP. MALFUNCTIONED. AFTER TO FROM CYQX DURING CLIMB OUT APU FIRE DETECTION SYSTEM INDICATED A FALSE FIRE WARNING FOR 1 SECOND FOLLOWED BY "B" LOOP REMAINING ILLUMINATED. AFTER APPR

All 651: https://openairdocs.org/model/boeing-747-200/reports.md

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