# Service difficulty reports: Boeing 747-230B

A list on [Boeing 747-230B](https://openairdocs.org/model/boeing-747-230b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 13 · 618 reports

- [SDR Q2SA2012042876002](https://openairdocs.org/sdr/Q2SA2012042876002.md): Engine · damaged · Apr 28, 2012 · N760SA · Boeing 747230B · Engine (Turbine/Turboprop)
  > NUMBER FOUR ENGINE STALLED DURING CLIMB AND FLAP CLEAN UP. AT APPROXIMATELY 3000 FEET THE CREW PULLED THE THRUST LEVER BACK TO BREAK THE ENGINE STALL. THEY THEN CONTINUED TO CLEAN UP AND ACCELERATE TO VZ + 100 TILL 10,000 FEET. AFTER PASSING 10,000 FEET THE
- [SDR EIAA20120404037](https://openairdocs.org/sdr/EIAA20120404037.md): Battery Pack · dirty · Apr 4, 2012 · N489EV · Boeing 747230B · Emergency Lighting
  > EMERGENCY EXIT SLIDE LIGHTS UPPER DECK LEFT DOOR SILL INOPERATIVE. REMOVED BATTERY CLEANED BATTERY PACK X631 CONTACTS AND RE-INSTALLED PER B747 MM 33-51-04 PG 204-205, OPS CHECK GOOD.
- [SDR EIAA20120404036](https://openairdocs.org/sdr/EIAA20120404036.md): Floorbeam · cracked · Apr 4, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > UPPER DECK FLOORBEAM VERTICAL WEB CRACKED AT UPPER AND LOWER END BS 420 RBL 80. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER SRM 53-10-07 PG. 47-50A.
- [SDR EIAA20120403035](https://openairdocs.org/sdr/EIAA20120403035.md): Access Panel · gouged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Main Frame
  > NR 3 PYLON RT SIDE INSIDE ACCESS PANEL 473AR DEEP GOUGE JUST UNDER CUT OUT. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-020-2.
- [SDR EIAA20120403034](https://openairdocs.org/sdr/EIAA20120403034.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON RT FRAMES STA 259 AND 234, RT SKIN BELOW LOUVER CUTOUT ARE HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403033](https://openairdocs.org/sdr/EIAA20120403033.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON RT BETWEEN FRAMES STA 248 AND 259, RT INTERNAL SKIN AT STIFFENER 2 TO 4 AND FRAMES HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403032](https://openairdocs.org/sdr/EIAA20120403032.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON RT BETWEEN FRAMES STA 259 AND 270, RT SKIN BETWEEN STIFFENERS 2 AND 3 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403031](https://openairdocs.org/sdr/EIAA20120403031.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON RT BETWEEN FRAMES STA 234 AND 270, RT INTERNAL SKIN BETWEEN STIFFENERS 2 AND 4 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120403030](https://openairdocs.org/sdr/EIAA20120403030.md): Skin · damaged · Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON RT BETWEEN FRAMES STA 234 AND 248, RT INTERNAL SKIN AT STIFFENER 3 AND STIFFENER HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.
- [SDR EIAA20120402029](https://openairdocs.org/sdr/EIAA20120402029.md): Battery · discharged · Apr 2, 2012 · N489EV · Boeing 747230B · Emergency Lighting
  > TWO EA UPPER DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES WITH SERVICEABLE.
- [SDR EIAA20120402028](https://openairdocs.org/sdr/EIAA20120402028.md): Skin · damaged · Apr 2, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON SKIN CAP DOUBLER MOST AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-023-2.
- [SDR EIAA20120330027](https://openairdocs.org/sdr/EIAA20120330027.md): Skin · damaged · Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON SKIN CAP DOUBLER AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-024-2.
- [SDR EIAA20120330026](https://openairdocs.org/sdr/EIAA20120330026.md): Structure · cracked · Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon Miscellaneous Structure
  > NR 4 PYLON O/B SIDE FWD ACCESS CUT OUT HAS CRACK IN UPPER FWD SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2
- [SDR EIAA20120327025](https://openairdocs.org/sdr/EIAA20120327025.md): Angle · damaged · Mar 27, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > LT BS 800 FRAME STR 17L UPPER AFT HOLE IS MISMATCHED COMMON TO STRAP FRAME INNER CHORD AND DOOR STOP FITTING. REMOVED DAMAGE INNER CHORD ANGLE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-021-2.
- [SDR EIAA20120327024](https://openairdocs.org/sdr/EIAA20120327024.md): Skin · cracked · Mar 27, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON I/B SIDE CRACK IN SKIN OF ACCESS CUT OUT, FWD UPPER CORNER NAC273. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2.
- [SDR EIAA20120326022](https://openairdocs.org/sdr/EIAA20120326022.md): Floorbeam · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > ELONGATED HOLE IN UPPER CHORD OF UPPER DECK FLOORBEAM BS 780 LBL 27. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326020](https://openairdocs.org/sdr/EIAA20120326020.md): Strap · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Frame
  > RIGHT BS 800 FRAME STRAP AND STR 17R STRAP HAS 2 EACH HOLES WITH TOOL MARKS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ERCA 489-53-021-2.
- [SDR EIAA20120326019](https://openairdocs.org/sdr/EIAA20120326019.md): Structure · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > BS 2231 O/B CHORD ABOVE STR 19L HAS TOOL MARKS INSIDE HOLE AND HOLE ELONGATED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2.
- [SDR EIAA20120326018](https://openairdocs.org/sdr/EIAA20120326018.md): Floorbeam · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > LOWER CHORD OF UPPER DECK FLOORBEAM BS 560 LBL 87 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326017](https://openairdocs.org/sdr/EIAA20120326017.md): Floorbeam · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > LOWER CHORD OF UPPER DECK FLOORBEAM BS 560 RBL 87.50 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.
- [SDR EIAA20120326016](https://openairdocs.org/sdr/EIAA20120326016.md): Skin · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON CAP SKIN O/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION 17.
- [SDR EIAA20120326015](https://openairdocs.org/sdr/EIAA20120326015.md): Skin · chafed · Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON CAP SKIN I/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION NR 16.
- [SDR EIAA20120326014](https://openairdocs.org/sdr/EIAA20120326014.md): Structure · damaged · Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous Structure
  > BS 2231 I/B CHORD BELOW STR 19L HAS DRILL START. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2
- [SDR EIAA20120306012](https://openairdocs.org/sdr/EIAA20120306012.md): Skin · chafed · Mar 6, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > NR 4 PLYON CAP SKIN I/B SIDE AT NAC 258 HAS CHAFING. REMOVED DAMAGED SECTION OF CAP SKIN, FABBED REPAIR PARTS AND INSTALLED PER EMC ENGINEERING DISPOSITION 3823 AND B747 SRM 54-31-03 PG 2 SHEET 1-4.
- [SDR EIAA20120201009](https://openairdocs.org/sdr/EIAA20120201009.md): Floorbeam · cracked · Feb 1, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 54.50 FWD SIDE HAS CRACK. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER SB 747-53A2431 PART 3 FIG 9.
- [SDR EIAA20120131008](https://openairdocs.org/sdr/EIAA20120131008.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 340 FLOORBEAM LBL 13.25 AFT SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 TABLE 1 FIG 9.
- [SDR EIAA20120131007](https://openairdocs.org/sdr/EIAA20120131007.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 13.12 AND 14.65 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 PART 3 FIG 9.
- [SDR EIAA20120131006](https://openairdocs.org/sdr/EIAA20120131006.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 340 FLOORBEAM LBL 29.50 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-7471587-00 REV J, SB 747-53A2431 REV 2 TABLE 1 FIG 8.
- [SDR EIAA20120131005](https://openairdocs.org/sdr/EIAA20120131005.md): Floorbeam · cracked · Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor Beam
  > BS 360 FLOORBEAM LBL 36.70 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J PART 3 FIG 9.
- [SDR EIAA20120126004](https://openairdocs.org/sdr/EIAA20120126004.md): Reveal · cracked · Jan 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Structure
  > BS 2231 RT DOOR FRAME REVEAL HAS CRACK BETWEEN STR 16R AND 17R. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS PER B747 SRM 53-10-04 FIG 91.
- [SDR EIAA20120119003](https://openairdocs.org/sdr/EIAA20120119003.md): Battery Pack · discharged · Jan 19, 2012 · N487EV · Boeing 747230B · Emergency Lighting
  > UPPER DECK RT "EXIT" DOOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED BATTERY CARTRIDGE FOR RT EXIT DOOR LIGHT SYSTEM OP'S CHECK NORMAL REF: 33-51-00.
- [SDR EIAA20120101001](https://openairdocs.org/sdr/EIAA20120101001.md): Control Quadrant · lack of lube · Jan 1, 2012 · N489EV · Boeing 747230B · Power Lever
  > ON DESCENT THROUGH 8000 FT NR 2 THRUST LEVER SEIZED JUST FORWARD OF IDLE POSITION. CONFIRMED NR 2 THROTTLE SEIZED JUST FORWARD OF IDLE INSPECTED THROTTLE RUN FROM WING ROOT TO MEC NO OBVIOUS DEFECTS NOTED LUBRICATED QUADRANT AND INTERTOCK MECHANISM PER AMM 76
- [SDR EIAA20111229265](https://openairdocs.org/sdr/EIAA20111229265.md): Battery · discharged · Dec 29, 2011 · N487EV · Boeing 747230B · Emergency Lighting
  > UPPER DECK RT EXIT EMERGENCY LIGHT OP. RECHARGED BATTERY, OP CHECK OK REF 33-51-00/501.
- [SDR EIAA20111204258](https://openairdocs.org/sdr/EIAA20111204258.md): Pin · sheared · Dec 4, 2011 · N488EV · Boeing 747230B · Wing, Landing Gear Attach Fittings
  > O/B WING GEAR BEAM PIN RETAINER NUT AND SHAFT SHEARED OFF LT WING. REMOVED AND REPLACED LT WING GEAR SUPPORT BEAM O/B BEARING PIN PER MM 57-15-01 PG 401-410.
- [SDR EIAA20111204257](https://openairdocs.org/sdr/EIAA20111204257.md): Skin · cracked · Dec 4, 2011 · N488EV · Boeing 747230B · Passenger/Crew Doors
  > L1 DOOR SKIN CRACKED AT FASTENER ROW 6.5" UP FROM LOWER GATE HINGE AND 10" FWD OF DOOR TRAILING EDGE. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 52-10-02 FIG. 9 AND ENGINEERING DISPOSITION 3786 ITEM 001.
- [SDR EIAA20111120256](https://openairdocs.org/sdr/EIAA20111120256.md): Battery · discharged · Nov 20, 2011 · N487EV · Boeing 747230B · Smoke Detection
  > FWD LAVATORY SMOKE DETECTOR CHIRPS ONCE EVERY FEW MINUTES, SUSPECT WEAK BATTERY. REMOVED AND REPLACED 9 VOLT BATTERY OP'S CHECKED OK PER SMM 26-13-01 PAGE 401.
- [SDR EIAA20111106247](https://openairdocs.org/sdr/EIAA20111106247.md): Duct · separated · Nov 6, 2011 · N488EV · Boeing 747230B · Pneumatic Distribution System
  > NR 4 ENGINE FIRE FAULT WARNING AND BOTH NACELLE TEMPS READING 8 UNITS. SELECTED "A" LOOP HAD FIRE WARNING BELL AND HANDLE CAUTION LIGHT. PULLED FIRE TEE HANDLE LIGHT AND AURAL WARNING LIGHT EXTINGUISHED/SILENCED. SUSPECT PNEUMATIC LEAK. FIRE BOTTLE WAS NOT
- [SDR TX9Y20111021001](https://openairdocs.org/sdr/TX9Y20111021001.md): Post · cracked · Oct 21, 2011 · N760SA · Boeing 747230B · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND COMMON TO FWD CARGO SUPPORT POST AT MAIN DECK BS 560 FLOORBEAM DURING INSPECTION. SECTION OF POST ENCOMPASSING THE CRACK WAS TRIMMED AWAY, AND REPAIRED IAW SRM D6-13592 REV 120 SUBJECT 53-10-07 FIGURE 7 WAS INSTALLED.
- [SDR EIAA2011235](https://openairdocs.org/sdr/EIAA2011235.md): Squib · no test · Oct 4, 2011 · N489EV · Boeing 747230B · Fire Bottle, Fixed
  > DURING PREFLIGHT FLIGHT, ENGINEER DISCOVERED FIRE BOTTLE SQUIB 3B WOULD NOT TEST. REMOVED AND REPLACED 3B FIRE BOTTLE SQUIB.
- [SDR TX9Y20110928005](https://openairdocs.org/sdr/TX9Y20110928005.md): Skin · cracked · Sep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Plate/Skin
  > DURING MAINTENANCE, NR 1 NACELLE SKIN WAS FOUND CRACKED AT LATCH AREA. THE CRACK IS ABOUT 0.8 IN LENGTH. REMOVED THE DAMAGE BY TRIMMING THE SKIN ASSEMBLY PER SRM 51-10-01. NDT INSPECTED TRIMMED AREA, NO CRACKS FOUND. FABRICATED AND INSTALLED NEW REPAIR FIL
- [SDR TX9Y20110928004](https://openairdocs.org/sdr/TX9Y20110928004.md): Strut · cracked · Sep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Main Frame
  > DURING PERFORMING NR 3 PYLON STRUT CAP SKIN INSPECTION AND MODIFICATION AS PER SB 747-54A2230 R0, CRACK DAMAGE AT NUMEROUS HOLES WERE FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND AT THE BULKHEAD FORWARD FRAMES
- [SDR TX9Y20110928003](https://openairdocs.org/sdr/TX9Y20110928003.md): Bulkhead · cracked · Sep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Bulkhead/Firewall
  > DURING INSPECTION OF THE NR 4 PYLON STA 286 BULKHEAD PER SB 747-54A2202 REV 01, 1EA 0.50 INCHES LONG CRACK WAS FOUND COMMON TO THE FRAME. REPAIRED PER SR 1-1535936828.
- [SDR EIAA2011230](https://openairdocs.org/sdr/EIAA2011230.md): Circuit Card · faulted · Sep 28, 2011 · N487EV · Boeing 747230B · Fire Detection
  > NUMBER 1 ENGINE FIRE DETECTOR A LOOP FAULTED. RESET FIRE DETECTOR CARD PER AMM 26-11-00. OPS CHECKED NORMAL.
- [SDR TX9Y20110928002](https://openairdocs.org/sdr/TX9Y20110928002.md): Structure · corroded · Sep 26, 2011 · N760SA · Boeing 747230B · Trailing Edge Flaps
  > LEFT WING I/B T/E AFT FLAP CONER FOUND HEAVY CORROSION. REPLACE THE LT WING I/B T/E AFT FLAP AS PER AMM 27-51-03.
- [SDR TX9Y20110928001](https://openairdocs.org/sdr/TX9Y20110928001.md): Bear Strap · corroded · Sep 26, 2011 · N760SA · Boeing 747230B · Fuselage Main, Plate/Skin
  > FWD CARGO BS 550-570, STRINGER 46R BEAR STRAP FOUND CORRODED. BEAR STRAP WAS TRIMMED OUT AND INSTALLED REPAIR DOUBLERS AND FILLER, AND SPLICED A NEW SEGMENT OF STRINGER AT S46R. THIS REPAIR WAS ACCOMPLISHED IAW BSR 1-1990327420.
- [SDR TX9Y20110922005](https://openairdocs.org/sdr/TX9Y20110922005.md): Doubler · corroded · Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Miscellaneous Structure
  > FUSELAGE BS 980-1000 WATER SERVICE PORT AREA DOUBLER FOUND CORROSION. FABRICATE AND INSTALL THE NEW DOUBLER (P/N:65B09637-1) AS PER BOEING DRAWING 65B09637.
- [SDR TX9Y20110922004](https://openairdocs.org/sdr/TX9Y20110922004.md): Bear Strap · corroded · Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Plate/Skin
  > FUSELAGE BS 540-560 FWD LAV SERVICE PANEL CUT OUT SKIN FOUND CORROSION. DURING INSPECTION OF THIS DATUM AIRPLANE, CORROSION WAS FOUND ON THE BEAR STRAP (P/N: 65B07201-2) AT FWD LAVATORY SERVICE PANEL CUTOUT AT STA560, STRINGER 46R. THE DAMAGED BEAR STRAP WAS
- [SDR TX9Y20110922003](https://openairdocs.org/sdr/TX9Y20110922003.md): Floorbeam · corroded · Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Floor Beam
  > AFT CARGO BS 1800 RBL 58 FLOORBEAM FOUND CORROSION. FABRICATE AND INSTALL THE FLOORBEAM CHORD (P/N:65B04327-71) AS PER BOEING DRAWING 65B04327.
- [SDR TX9Y20110922002](https://openairdocs.org/sdr/TX9Y20110922002.md): Frame · corroded · Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Frame
  > AFT CARGO BS 1920 RT FRAME INNER CHORD FOUND CORROSION. REMOVE THE CORROSION AS PER SRM 51-10-01. CHECK THE ALLOWABLE WITHIN SRM LIMIT AS PER SRM 53-10-01.
- [SDR TX9Y20110922001](https://openairdocs.org/sdr/TX9Y20110922001.md): Stringer · corroded · Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION OF THIS DATUM AIRPLANE, THE STRINGER 51R (P/N: 65B04483-13) IS FOUND HEAVILY CORRODED ON THE INBOARD SIDE WEB FLANGE AT STA 1958. THE STRINGER AFT END WAS TRIMMED AND A REPAIR SPLICE CHANNEL SIMILAR WITH THE ORIGINAL ONE, BUT WITH EXTENDED C

Next page: https://openairdocs.org/model/boeing-747-230b/reports.md?page=2

## 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 = '747230B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-747-230b/reports

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