# Service difficulty reports: Boeing 747-200B

A list on [Boeing 747-200B](https://openairdocs.org/model/boeing-747-200b.md).

Newest first. General aviation reporting is voluntary.

- [SDR 1119200701](https://openairdocs.org/sdr/1119200701.md): Tire · failed · Nov 19, 2007 · N361FC · Boeing 747200B · Tire
  > ON TO ROLL, AIRCRAFT AIRFRAME SHUDDERED AT 155KTS. CONTINUED TAKEOFF, REPORTED TO TOWER POSSIBLE BLOWN TIRE. DEBRIS CONFIRMED ON RUNWAY. ALL SYSTEMS INCLUDING BRAKE TEMPS GOOD, CONTINUED. (25) MINUTES INTO FLIGHT, NR 1 HYDRAULIC SYSTEM FAILURE - RETURNED T
- [SDR 0331200702](https://openairdocs.org/sdr/0331200702.md): Engine · bird ingestion · Mar 31, 2007 · N361FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > AT ROTATION NR 2 ENG VIB ANNUNICATOR LIGHT & ENG VIB LIGHT FOR NR 2 ENG ILLUM, ACCOMPANIED BY VIB & ABNORMAL SOUND. NR 2 ENG SECURED IAW CHECKLIST, NO VIB NOTED AFTER SHUTDOWN. FUEL JETTISON, ACFT RETURNED WITHOUT FURTHER INCIDENTS. ON POSTFLIGHT INSPECTIO
- [SDR EIA2007061](https://openairdocs.org/sdr/EIA2007061.md): Smoke Detector · no test · Mar 28, 2007 · N486EV · Boeing 747200B · Smoke Detection
  > NR 5 A LOOP SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR PER 26-14-01, TEST OK.
- [SDR 0312200701](https://openairdocs.org/sdr/0312200701.md): Hose · worn · Mar 12, 2007 · N535FC · Boeing 747200B · Hydraulic System, Main
  > AFTER TAKEOFF, WITH LG RETRACTED, OBSERVED HYDRAULIC SYSTEM NR 4 LOOSE WITH BOTH NR 4 EDP, ADR LOW PRESSURE ON. AOM 2-2-55 AND 2-2-59 FOLLOWED, RETURNED TO DEPARTURE.FOUND LT WING GEAR DOOR ACTUATOR HYDRAULIC LINE WORN. REMOVED AND REPLACED HYDRAULIC LINE,
- [SDR 1023200603](https://openairdocs.org/sdr/1023200603.md): Warning Light · illuminated · Oct 23, 2006 · N361FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > ON DEPARTURE (GYD), JUST AFTER V1, NR 1 ENGINE VIBE LIGHT ILLUMINATED, VIBE METER NR 1 OFF SCALE HIGH, INCLUDING VIBRATION AS WELL. ENGINE SHUT DOWN, FUEL DUMP, AND RETURNED TO (GYD).CORRECTIVE ACTIONS, PENDING.
- [SDR 1017200602](https://openairdocs.org/sdr/1017200602.md): Engine · power loss · Oct 17, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > DURING CLIMB FROM (ELLX) AT AROUND FL 180 FT, NR 1 THROTTLE IS AT FORWARD STOP TO MAINTAIN CLIMB THRUST. IN CRUISE NR 1 THROTTLE IS AT 1.5 UNITS - (4) KNOBS AHEAD OF ENGINES 2, 3, 4. NOTE ALL ENGINE PARAMETERS NORMAL AT LOW ALT, BELOW 189 THROTTLE POSITIONS
- [SDR 0925200603](https://openairdocs.org/sdr/0925200603.md): Compressor · stalled · Sep 20, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > DURING TO ROLL (SKBO), APPROX. 125 KTS., NR 4 ENGINE COMPRESSOR STALLED - ABORTED TO, RETURN TO GATE. FINDINGS - CORRECTIVE ACTIONS - TBD.
- [SDR 0808200601](https://openairdocs.org/sdr/0808200601.md): Engine · none · Aug 8, 2006 · N362FC · Boeing 747200B · Engine (Turbine/Turboprop)
  > ON TAKEOFF AT SGES (AGT), NR 3 ENGINE BEGAN TO VIBRATE AND AMBER ENGINE VIB LIGHT CAME ON. ENGINE SHUTDOWN AND PROCEDURE TO COMPLETE THE HIGH ENGINE VIBRATION RB211 CHECKLIST. DISCREPANCY DUE TO BIRDSTRIKE/INJESTION. PERFORMED CONDITIONAL ENGINE BIRDSTRIKE
- [SDR EIA2006160](https://openairdocs.org/sdr/EIA2006160.md): Smoke Detector · no test · Aug 3, 2006 · N471EV · Boeing 747200B · Smoke Detection
  > NR 5 LOWER LOBE SMOKE DETECTOR, NO TEST. REPLACED SAME.
- [SDR 0623200604](https://openairdocs.org/sdr/0623200604.md): Control Wheel · binding · Jun 23, 2006 · N262FC · Boeing 747200B · Trailing Edge Flap Control System
  > ON CLIMBOUT BEFORE LEVEL FLT WITH FLAPS EXTENDED CONTROL WHEEL BINDING & ABRUPT YAWING MOTIONS WITH MINOR VIBRATION & RUMBLE EXPERIENCED AT FLAPS 10.5 DEGREE WITH AP ENGAGED. BINDING WAS STILL PRESENT WITH MINIMUM YAWING MOTION ON APPROACH (MIA). BINDING & Y
- [SDR 0622200603](https://openairdocs.org/sdr/0622200603.md): Rivet · sheared · Jun 22, 2006 · N362FC · Boeing 747200B · Drag Control System
  > AFTER DEPARTURE FROM MIA, AILERONS DURING MANUAL CLIMB APPEARED HEAVY AND WERE BINDING. ALTITUDE 350/AUTOPILOT A & B NORMAL. DURING DESCENT AUTOPILOT A&B TURN RATE NORMAL. AUTOPILOT C EXCESSIVE TURN RATES IN BOTH LEFT AND RIGHT TURNS. NOTICE MINOR VIBRATIO
- [SDR 0609200602](https://openairdocs.org/sdr/0609200602.md): Valve · leaking · Jun 8, 2006 · N362FC · Boeing 747200B · Fuel Storage
  > ON GROUND, FUEL SPILL THRU RT WING, AFTER REFUELING AIRCRAFT. FOLLOW PROCEDURES IN FUELING MANUAL FOR FUEL SPILLAGE. DURING INSPECTION, FOUND BOTH THE NR 2 AND NR 3 DRAIN VALVE LEAKING. REPLACED BOTH VALVES, CLEAN FUEL TANKS, INSPECTED, AND CLOSED TANK PLAT
- [SDR EIAA2006038](https://openairdocs.org/sdr/EIAA2006038.md): Indicator · failed · Mar 26, 2006 · N487EV · Boeing 747200B · Engine EGT/TIT Indicating System
  > DURING FLIGHT, NR 2 EGT FAILED TO 0 ON DESCENT, INTERMITTENT FAILURE, SEEMED TO FAIL DURING POWER REDUCTION NEVER GOT AN OFF FLAG. CHECKED CONNECTORS ON HARNESS AND PYLON ON NR 2 ENG AND P-2 PANEL. COULD NOT DUPLICATE, ALL WIRE CHECKS WERE NORMAL COMPARED TO
- [SDR 740002](https://openairdocs.org/sdr/740002.md): Engine · shutdown · Mar 22, 2006 · N740SA · Boeing 747200B · Engine (Turbine/Turboprop)
  > NR 2 ENGINE SHUTDOWN FOR UNKNOWN REASON, ACCOMPANIED BY A LOUD BANG. QRH CHECKLIST ACCOMPLISHED. AIRCRAFT RETURNED TO PANC.
- [SDR 1022200501](https://openairdocs.org/sdr/1022200501.md): Window · cracked · Oct 22, 2005 · N535MC · Boeing 747200B · Flight Compartment Windows
  > RIGHT FORWARD NR 1 WINDOW HAS DELAMINATION AND POSSIBLE CRACK. INSPECTED WINDOW, AND FOUND ACCEPTABLE FOR FLIGHT IAW MEL 56-1-1, NR 1 WINDOW OUTER GLASS PLY CRACKED ONLY, AND VISIBILITY THROUGH ASSOCIATED WINDSHIELD IS ACCEPTABLE, AND VISION IS NOT IMPAIRED O
- [SDR UPS01435784](https://openairdocs.org/sdr/UPS01435784.md): Brake Assy · inoperative · May 1, 2001 · N522UP · Boeing 747200B · Landing Gear Brake System
  > WHILE EXITING RAMP NO NORMAL BRAKES AVAILABLE MOMENTARILY. INSPECTED ALL SYSTEM FOR LEAKS, NONE FOUND. PERFORMED OPERATION OF BRAKE SYSTEM ON NR 4, NR 1 AND RESERVE SYSTEM. FOUND NORMAL IAW MM 32-40-00. OK FOR SERVICE.
- [SDR UPS01435638](https://openairdocs.org/sdr/UPS01435638.md): Wire · damaged · Apr 21, 2001 · N521UP · Boeing 747200B · Light System Wiring
  > INSPECTION TYPE:N/A EMERGENCY LIGHT INOP UPPER DECK EXIT FWD PANEL REPAIRED PULLED WIRE, OPS CK GOOD
- [SDR UPS01435326](https://openairdocs.org/sdr/UPS01435326.md): Fire Detector · malfunctioned · Mar 21, 2001 · N522UP · Boeing 747200B · Fire Detection
  > INSPECTION TYPE:N/A NR 4 ENGINE FIRE DETECTION LIGHT ILLUMINATED REMOVED AND REPLACED NR 4 ENGINE UPPER AFT TEST DECTECTOR ASSY. I.A.W. MMNL 26-11-00. OPERATIONAL CHK SYSTEM NORMAL.
- [SDR UPS01434803](https://openairdocs.org/sdr/UPS01434803.md): Spar Cap · corroded · Jan 30, 2001 · N524UP · Boeing 747200B · Wing Spar
  > INSPECTION TYPE:IN PER EO-13738A REPAIR RT WING LWR SKIN FWD ANGLE ATTACH CHORD. *S/D* REPAIR ACCOMPLISHED PER EO -13738A.
- [SDR UPS00434524](https://openairdocs.org/sdr/UPS00434524.md): Light · inoperative · Dec 3, 2000 · N520UP · Boeing 747200B · Emergency Lighting
  > INSPECTION TYPE:N/A AFT EMERGENCY EXIT LIGHT AT CREW ENTRY DOOR L1 IS INOP R&R BATTERY ASSY PER 33-50-00 OPS CK OK
- [SDR UPS00434521](https://openairdocs.org/sdr/UPS00434521.md): Battery Pack · discharged · Dec 2, 2000 · N520UP · Boeing 747200B · Emergency Lighting
  > INSPECTION TYPE:N/A AFT EMERGENCY LIGHT AT CREW ENTRY DOOR L1 IS INOP EMERGENCY LIGHT BY CREW STAIRS (AFT) INOP R/R BATTERY ASSY ONLY, PER 33-50-00 OPS CHK OK
- [SDR UPS00434525](https://openairdocs.org/sdr/UPS00434525.md): Stringer · corroded · Nov 30, 2000 · N523UP · Boeing 747200B · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:N/A AFT CARGO COMPT CORROSION ON STR 49 RH BETWEEN STA 1920 TO 1960 CORRODED PORTION STRINGER REMOVED. FABRICATED NEW STRINGER AND REINF ORCEMENT IAW SRM 53-10-23 FIG 2 ACCOMPLISHED REPAIR IAW SRM 53-10-03
- [SDR UPS00434268](https://openairdocs.org/sdr/UPS00434268.md): Light · inoperative · Oct 30, 2000 · N524UP · Boeing 747200B · Emergency Lighting
  > INSPECTION TYPE:N/A, L1 DOOR AFT EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKS GOOD.
- [SDR UPS00433554](https://openairdocs.org/sdr/UPS00433554.md): Indicator · malfunctioned · Aug 10, 2000 · N524UP · Boeing 747200B · Engine RPM Indicating System
  > INSPECTION TYPE:N/A, AIR TURNBACK - ALL FOUR ENG N1 INDICATORS NOT EFFECTIVE FOR AIRCRAFT. REMOVED AND REPLACED INDICATORS. TPCR FILED FOR PROPER EFFECTIVITY REFERENCE LOG PAGES 418722, 418723, AND 418724.
- [SDR UPS00433344](https://openairdocs.org/sdr/UPS00433344.md): Flap · malfunctioned · Jul 11, 2000 · N524UP · Boeing 747200B · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A, FLAPS WON''T DRIVE TO COMMANDED POSITION.
- [SDR UPS00433745](https://openairdocs.org/sdr/UPS00433745.md): Cap · cracked · Jul 7, 2000 · N524UP · Boeing 747200B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RT WING - TRAILING EDGE SUPPORT BEAM UPPER CAP DEEP CORROSION AND A LONG CRACK WERE FOUND AT THE UPPER AFT FLANGE OF THE UPPER CHORD. REPAIR ACCOMPLISHED PER IAI EO 89310 AND AS APPROVED BY FAA-8110-3 FORM. THE CHORD AT WBL 360 TRIMMED OU
- [SDR UPS00433247](https://openairdocs.org/sdr/UPS00433247.md): Angle · corroded · Jun 28, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, REINFORCING ANGLE AT BS 360 RT BETWEEN STR 3 A AND STR 10 IS CORRODED. ANGLE FABRICATED IAW SRM 51-20-01 AND REPLACED IAW SRM 51-30-02.
- [SDR UPS00433073](https://openairdocs.org/sdr/UPS00433073.md): Support Bracket · damaged · Jun 28, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, FUSELAGE WING TO BODY FAIRING SUPPORT BRACKET CRACKED AT BS 1265, BELOW LOWER REAR SPAR SPLICE RT. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-03 FIG 1.
- [SDR UPS00433072](https://openairdocs.org/sdr/UPS00433072.md): Support Bracket · cracked · Jun 28, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. WING TO BODY SUPPORT CRACKED AT BS 1265, BELOW REAR SPAR SPLICE LT SIDE. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40--03 FIG 1
- [SDR UPS00433341](https://openairdocs.org/sdr/UPS00433341.md): Spar · corroded · Jun 27, 2000 · N521UP · Boeing 747200B · Trailing Edge Flaps
  > INSPECTION TYPE:C REF NRC 44298572 44298580 44298584 44298590, PLEASE REPLACE LEFT I/B MIDFLAP ASSY DUE CORROSION ON FRONT SPAR LOWER CHORD AND UPPER SURFACE DOUBLER PLATE. LT MIDFLAP ASSY REPLACED PER MM 27-51-01.
- [SDR UPS00433060](https://openairdocs.org/sdr/UPS00433060.md): Stiffener · cracked · Jun 23, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CRACK IN NOSE WHEEL WELL AT BS 300 RBL 22. CRACK IN STIFFENER. NOSE WHEEL WELL CRACKED STIFFENER REPLACED STIFFENER IAW SRM 51-300-02
- [SDR UPS00433064](https://openairdocs.org/sdr/UPS00433064.md): Angle · cracked · Jun 22, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CRACK FOUND IN ANGLE AT BS 486 STR 26 LT IN FWD CARGO HOLD. ANGLE REPLACED IAW SRM 51-30-02
- [SDR UPS00433059](https://openairdocs.org/sdr/UPS00433059.md): Seat Track · cracked · Jun 22, 2000 · N521UP · Boeing 747200B · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C. SEAT TRACK CRACKED BS 440 AND BS460 RBL 64. SECTION OF SEAT TRACK REPLACED FROM BS 430 TO BS 460 IAW SRM 53-10-0 5, FIG. 1A, DETAIL 1V
- [SDR UPS00433061](https://openairdocs.org/sdr/UPS00433061.md): Strap · cracked · Jun 21, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. FRAME TIE DOWN STRAP BROKEN FWD OF RT OUTFLOW VALVE BS 2020 LBL 15. NEW TIE DOWN STRAP FABRICATED AND INSTALLED IAW 51-30-02 AND SRM 5 1-20-1
- [SDR UPS00433067](https://openairdocs.org/sdr/UPS00433067.md): Angle · cracked · Jun 18, 2000 · N521UP · Boeing 747200B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. FWD CARGO BAY TWO CRACKED ANGLES ON WEATHER RADAR TRAY BS 380 RT SIDE NOSE WW, CRACKED ANGLES REMOVED IAW SRM 51-30-02. NEW ANGLES FABRICATED IAW BAC 5300. NEW ANGLES INSTALLED IAW SRM 51-30-02
- [SDR UPS00433269](https://openairdocs.org/sdr/UPS00433269.md): Frame · cracked · Jun 13, 2000 · N521UP · Boeing 747200B · Fuselage Main, Frame
  > INSPECTION TYPE:C, UPPER DECK FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STRINGER AT BS 500 AT STR 10 RT. REPAIR CARRIED OUT IAW QUERY NOTE 34/200 AND SRM 51-10-06. TRIM OFF FRAME SEGMENT AND FABRICATE DOUBLER PENETRANT INSP ALL NEW PARTS APPROVED 8110 ISS
- [SDR UPS00433315](https://openairdocs.org/sdr/UPS00433315.md): Rivet · loose · Jun 9, 2000 · N521UP · Boeing 747200B · Leading Edge Devices
  > INSPECTION TYPE:C, LOOSE RIVETS IN TORQUE TUBE DRIVES AT VARIOUS LOCATIONS I/B END NR 15 KRUEGER FLAP, I/B AND O/B OF NR 1 L/E PDU, I/B AND O/B OF NR 3 PDU RT, OUTPUT OF L/E NR 4 PDU, I/B AND O/B OF NR 3 LT PDU, TORQUE TUBE AT NR 5 VCF, TORQUE TUBE AT NR 4 VCF
- [SDR UPS00433325](https://openairdocs.org/sdr/UPS00433325.md): Channel · corroded · Jun 7, 2000 · N521UP · Boeing 747200B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RT WING L/E CORROSION ON L/E FALSE WORK SUPPORT CHANNEL AT OLES 1373 4 AND OLES 1444. CORROSION REMOVED DEPTH 10, AREA RE-PROTECTED IAW SRM 51-10-02.
- [SDR UPS00433301](https://openairdocs.org/sdr/UPS00433301.md): Strap · corroded · Jun 7, 2000 · N521UP · Boeing 747200B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER IN SPAR SKIN EXT AT OLES 1116 RT. REPAIR CARRIED OUT IAW Q/NOTE 8/2000 AND SRM 57-30-03 FIG 4. BLENDED OUT CORROSION / SPLICE REPAIR.
- [SDR UPS00433300](https://openairdocs.org/sdr/UPS00433300.md): Channel · corroded · Jun 7, 2000 · N521UP · Boeing 747200B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER FALSE WORK PANEL FWD OF SUPP CHANNEL AT SEVERAL LOCATIONS AT OLES 1066 OUT TO NR 4 ENG. REPAIR CARRIED OUT IAW QUERY NOTE 4/2000 AND SRM 51-30-01 AND 51-30 -06. REMOVED CORRODED BEAM SECTION AND SPLICE IN
- [SDR UPS00433302](https://openairdocs.org/sdr/UPS00433302.md): Panel · corroded · Jun 6, 2000 · N521UP · Boeing 747200B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RIGHT WING L/E LOWER FALSE WORK PANEL IS BULGING AT O/B WING JACK PAD LOCATION. REPAIR CARRIED OUT IAW QUERY NOTE 7/2000 AND SRM 57-30-01 AND 57-30-03. BLENDED OUT CORRODED AREA AND INSTALLED FILLER AND RETURNED AREA TO ORIGINAL DIMENSIO
- [SDR UPS00433267](https://openairdocs.org/sdr/UPS00433267.md): Floorbeam · corroded · Jun 6, 2000 · N521UP · Boeing 747200B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER DECK FLOORBEAM WEB AT BS 460 RBL 60. REPAIRED IAW QUERY NOTE N521 UP/3/2000 AND SRM 53-10-07 FIG 11. CUT OUT CORRODED AREA AND SPLICED IN FABRICATED WEB. APPROVED 8110 ISSUED FOR THIS REPAIR.
- [SDR UPS00432609](https://openairdocs.org/sdr/UPS00432609.md): Line · not closed · May 12, 2000 · N520UP · Boeing 747200B · Pitot/Static System
  > INSPECTION TYPE:C, AIR TURNBACK DUE TO FAILURE OF AIRSPEED AND ALTIMETER SYSTEM. AFTER DEBRIEF WITH CREW, FLS COMPLETED AN INSPECTION OF A/C, FOUND CAPT''S AND F/O''S PITOT DRAIN LINES UNCAPPED IN THE E & E BAY. THE FLAP SYS WAS OVERSPED. *S/D* CAPPED PITO
- [SDR UPS00432530](https://openairdocs.org/sdr/UPS00432530.md): Frame · cracked · May 3, 2000 · N520UP · Boeing 747200B · Fuselage Main, Frame
  > INSPECTION TYPE:C 44, UPPER DECK, FRAME CRACKED AT STRINGER CUTOUT AT STA 500 LT, STR 11L. PLEASE REPAIR/RECTIFY. REPAIR ACCOMPLISHED IAW APPROVED REPAIR PER 8110-3. ALL THE ACTIVE CRACK TIPS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLED
- [SDR UPS00432510](https://openairdocs.org/sdr/UPS00432510.md): Stringer · corroded · Apr 22, 2000 · N520UP · Boeing 747200B · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C 44, FWD CARGO, EVIDENCE OF CORROSION FOUND ON STRINGER AT BS 984 STR 38 LT. STRINGER FABRICATED PER WORK SHOP ORDER E0169804 AND INSTALLED IAW SRM 51-30-02. REPAIR ACCOMPLISHED IAW SRM 53-10-03.
- [SDR UPS00432520](https://openairdocs.org/sdr/UPS00432520.md): Frame · cracked · Apr 12, 2000 · N520UP · Boeing 747200B · Fuselage Main, Frame
  > INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 240 STR 14 LT. REPAIR CARRIED OUT IAW SRM 53-10-04, FIG 14 AND CONTINUE WITH INSPECTIONS IN ACCORDANCE WITH SB 53A2265.
- [SDR UPS00432519](https://openairdocs.org/sdr/UPS00432519.md): Frame · cracked · Apr 12, 2000 · N520UP · Boeing 747200B · Fuselage Main, Frame
  > INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 200 STR 14. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED 8110-3, DETAILS OF REPAIR TEXT AS FOLLOWS. THESE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INST
- [SDR UPS00432518](https://openairdocs.org/sdr/UPS00432518.md): Frame · cracked · Apr 12, 2000 · N520UP · Boeing 747200B · Fuselage Main, Frame
  > INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB CRACKED AT CUTOUT FOR STR AT BS 200 STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED REPAIR DETAILED I N 8110-3.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '747200B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-747-200b/reports

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