# Service difficulty reports: Boeing 747-228F

A list on [Boeing 747-228F](https://openairdocs.org/model/boeing-747-228f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 199 reports

- [SDR Q2SA2011121953010](https://openairdocs.org/sdr/Q2SA2011121953010.md): Fire Detector · false indication · Dec 19, 2011 · N753SA · Boeing 747228F · Fire Detection
  > WHEEL WELL FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED AFTER TAKEOFF AND GEAR UP. EXECUTED QRH MEMORY ITEMS AND DUMPED 139,000 LBS OF FUEL. ACFT RETURNED, VISUALLY VERIFIED NO ACTUAL WHEEL FIRE EXISTED IN ANY POSITION. FALSE WARNING. VISUALLY CHECKED A
- [SDR Q2SA753009](https://openairdocs.org/sdr/Q2SA753009.md): Tire · damaged · Jul 27, 2011 · N753SA · Boeing 747228F · Tire
  > UPON TAKEOFF, TOWER CALLED AND ADVISED THE CREW OF "LEAVING RUBBER ON THE RUNWAY". THE CREW RETURNED TO HAAB AND FOUND TREAD LOSS ON THE NUMBER EIGHT TIRE. IN ADDITION TO THE TIRE DAMAGE THE AIRCRAFT ALSO EXPERIENCED DAMAGE TO PANELS 193 C AND D. NUMBER EIG
- [SDR Q2SA754013](https://openairdocs.org/sdr/Q2SA754013.md): Fan · faulty · May 14, 2011 · N754SA · Boeing 747228F · Air Distribution Fan
  > AT 10,000 FEET, ELECTRICAL SMELL AND LIGHT SMOKE ENTERED THE COCKPIT. COMPLETED SMOKE SOURCE IDENTIFICATION PROCEDURE AND ELECTRICAL SYSTEM SMOKE OR FIRE CHECKLIST. THE SMOKE DISSIPATED ALONG WITH THE SMELL AT LANDING. TAXIED CLEAR OF THE RUNWAY TO PARKING
- [SDR Q2SA754012](https://openairdocs.org/sdr/Q2SA754012.md): Line · loose · Apr 1, 2011 · N754SA · Boeing 747228F · Hydraulic System, Main
  > NR 1 HYDRAULIC SYSTEM QUANTITY LOW. RE-TORQUED HYDRAULIC LINE FROM THE NR 1 SYSTEM, RIGHT BODY GEAR DOOR LINE PER AMM 20-11-05, PG 401. OPERATIONAL AND LEAK CHECKED NORMAL PER AMM 29-11-00, PG 501. OK FOR SERVICE.
- [SDR Q2SA754011](https://openairdocs.org/sdr/Q2SA754011.md): Sequence Valve · cracked · Mar 29, 2011 · N754SA · Boeing 747228F · Landing Gear Retraction/Extension System
  > AFTER DEPARTURE FROM JNB, NR 1 ENGINE EDP AND ADP LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. HYDRAULIC PRESSURE AND QUANTITY INDICATED "0". PERFORMED QRH PROCEDURES FOR AFFECTED HYDRAULIC SYSTEM. DECLARED EMERGENCY INBOUND TO ADD.
- [SDR Q2SA754010](https://openairdocs.org/sdr/Q2SA754010.md): Fan · vibration · Feb 9, 2011 · N754SA · Boeing 747228F · Air Distribution Fan
  > FLIGHT DECK FAN RUMBLES WITH OCCASIONAL BURNED ODOR, SWITCHED OFF AND CIRCUIT BREAKER PULLED. PERFORMED SMOKE INSPECTION REFERENCE AMM 5-51-00, NO DEFECTS NOTED. REMOVED AND REPLACED RECIRCULATING FAN IAW AMM 21-25-06, OPS CHECKED NORMAL IAW 21-25-06.
- [SDR Q2SA753008](https://openairdocs.org/sdr/Q2SA753008.md): Fan · faulty · Jan 9, 2011 · N753SA · Boeing 747228F · Air Distribution Fan
  > FLIGHT DECK FAN IS BURNED UP. SEVERE ELECTRICAL BURNING SMELL WHEN TURNED ON. FOLLOW UP TO ASSIGNED DI 23969 - REMOVED AND REPLACED FLIGHT COMPARTMENT AIR RECIRCULATING FAN IAW B747 AMM 21-25-06, OPS CHECK GOOD. THIS CLEARS DI 23969 - PLACARD REMOVED.
- [SDR Q2SA754009](https://openairdocs.org/sdr/Q2SA754009.md): Connector · damaged · Dec 11, 2010 · N754SA · Boeing 747228F · Fire Protection System Wiring
  > DURING INITIAL CLIMB, THE FIRE ENGINE WARNING BELL FOR NR1 ENGINE SOUNDED BRIEFLY. AT THAT TIME THE CREW PERFORMED AN INSTRUMENT SCAN AND FOUND THE ENGINE INDICATIONS WERE NORMAL. APPROX 10 SECONDS LATER, THE NACELLE TEMP WENT FULL SCALE AND THE FIRE BELL SOUN
- [SDR Q2SA753007](https://openairdocs.org/sdr/Q2SA753007.md): Unknown · smoke · Nov 27, 2010 · N753SA · Boeing 747228F · Air Distribution System
  > SMOKE IN THE COCKPIT ON DESCENT. INSP ACFT IAW AMM 5-51-50. NO TROUBLE FOUND IN AIR-CONDITIONING SYS. REMOVED ALL PANELS IN F/E AREA P6, P7 AND P12 AND LOOKED FOR DAMAGE AND NONE FOUND. OPENED P52 PANEL, SMELL OF SMOKE SEEMS TO BE CENTERED THERE, NO SMOKE AT
- [SDR VGQY2010082900130](https://openairdocs.org/sdr/VGQY2010082900130.md): Frame · cracked · Aug 30, 2010 · N753SA · Boeing 747228F · Fuselage Main, Frame
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND CRACK INDICATION ON 2 EA HOLES ON FRAME AND 2 EA HOLES ON FWD CHANNEL AT RT BS 820 AT TENSION TIE AREA. CHANNEL CUT OUT AS PER SRM 53-10-11 FIGURE 2 REVISION 117. FRAME CUTOUT AS PER SRM 53-10-04 FIGURE 132 REVISIO
- [SDR VGQY2010082900129](https://openairdocs.org/sdr/VGQY2010082900129.md): Frame · cracked · Aug 30, 2010 · N753SA · Boeing 747228F · Fuselage Main, Frame
  > DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 900, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TENSION TIE AND FRAME AT RT BS 900 REPAIR CARRIED OUT REPAIR ON FWD CHANNEL AS PER SRM 53-10-11 REV 117 FIGURE 2.
- [SDR VGQY2010082900128](https://openairdocs.org/sdr/VGQY2010082900128.md): Shear Tie · cracked · Aug 30, 2010 · N753SA · Boeing 747228F · Fuselage Internal Mounting Structure
  > DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 860, FOUND 02 HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TENSION TIE AND FRAME AT RT BS 860 CARRIED OUT REPAIR ON FWD 'C' CHANNEL AS PER SRM 53-10-11 REV 117 FIGURE 2.
- [SDR VGQY2010082900126](https://openairdocs.org/sdr/VGQY2010082900126.md): Floorbeam · cracked · Aug 29, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE ELONGATED AT BS 380 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE RBL 15. INSURANCE CUT ON FASTENER HOLE CARRIED-OUT PER SB 747-53A2439 REV 2. FINAL HOLE SIZE 0.341". HFEC INSPECTION CARRIED-OUT PER B747 NDTM
- [SDR VGQY2010082900125](https://openairdocs.org/sdr/VGQY2010082900125.md): Floorbeam · cracked · Aug 29, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 340 UPPER DECK FLOORBEAM AFT FLANGE LBL 15 AT 6 O'CLOCK BY PLAIN VIEW. INSURANCE CUT ON FASTENER HOLE CARRIED-OUT PER SB 747-53A2439 REV 2. FINAL HOLE SIZE 0.341". HFEC INPECTION
- [SDR VGQY2010082900124](https://openairdocs.org/sdr/VGQY2010082900124.md): Floorbeam · cracked · Aug 29, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 340 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE LBL 35 AT 12 O'CLOCK BY PLAIN VIEW. TRIMMED-OUT AND FABRICATED REPAIR FILLER AND STRAP INSTALLED PER SB B747-53A2429 REV 2.
- [SDR VGQY2010081900114](https://openairdocs.org/sdr/VGQY2010081900114.md): Skin · cracked · Aug 19, 2010 · N753SA · Boeing 747228F · Fuselage Main, Plate/Skin
  > HFEC OPEN HOLE CARRIED OUT AND FOUND CRACK INDICATION 01 EA HOLE AT 6 O'CLOCK DIRECTION BY LOOKING INBD AT FWD UPPER CORNER OF LOWER LOBE OF AFT CARGO DOOR CUTOUT. CRACKED AREA TRIMMED OUT AS PER SRM 53-30-03 FIGURE 62 REVISION 117. HFEC INSPECTION CARRIED OU
- [SDR VGQY2010081700113](https://openairdocs.org/sdr/VGQY2010081700113.md): Frame · cracked · Aug 17, 2010 · N753SA · Boeing 747228F · Fuselage Main, Frame
  > CABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 840, FOUND 01EA HOLE CRACK INDICATION ON FRAME WEB AND DOUBLER STACK UP. FRAME AT RIGHT BS 840 CUT OUT PER SRM 53-10-04 FIGURE 133 REVISION 117. HFEC INSPECTION CARRIED OUT ON CUT OUT AREA & F
- [SDR VGQY2010081700112](https://openairdocs.org/sdr/VGQY2010081700112.md): Channel · cracked · Aug 17, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > CABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 840, FOUND 01EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL AS PER MARKED. REPAIR CARRIED OUT PER B747 SRM 53-10-11 REV 117 FIGURE 2.
- [SDR VGQY2010081600111](https://openairdocs.org/sdr/VGQY2010081600111.md): Fitting · damaged · Aug 16, 2010 · N753SA · Boeing 747228F · Fuselage, Landing Gear Attach Fittings
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 RT LWR CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081600110](https://openairdocs.org/sdr/VGQY2010081600110.md): Fitting · damaged · Aug 16, 2010 · N753SA · Boeing 747228F · Fuselage, Landing Gear Attach Fittings
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 L LWR CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081600108](https://openairdocs.org/sdr/VGQY2010081600108.md): Fitting · damaged · Aug 16, 2010 · N753SA · Boeing 747228F · Fuselage, Landing Gear Attach Fittings
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027, LT FWD VERTICAL CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081600107](https://openairdocs.org/sdr/VGQY2010081600107.md): Structure · cracked · Aug 16, 2010 · N753SA · Boeing 747228F · Fuselage Main, Structure
  > NOSE WHEEL WELL - DURING REMOVAL OF CHORD FOR EAM 4753027 MODIFICATION, RT FWD VERTICAL CHORD FOUND CRACKED. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081600106](https://openairdocs.org/sdr/VGQY2010081600106.md): Fitting · damaged · Aug 16, 2010 · N753SA · Boeing 747228F · Fuselage, Landing Gear Attach Fittings
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT AFT VERTICAL CHORD SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081400103](https://openairdocs.org/sdr/VGQY2010081400103.md): Fairing · cracked · Aug 14, 2010 · N753SA · Boeing 747228F · Leading Edge Devices
  > LEFT WING -NR 6 LEADING EDGE V/C FLAP BULLNOSE FAIRING FOUND CRACK AT O/B AREA. REMOVED AND REPLACED PER AMM 27-81-02 REV 143.
- [SDR VGQY2010081400102](https://openairdocs.org/sdr/VGQY2010081400102.md): Support Channel · cracked · Aug 14, 2010 · N753SA · Boeing 747228F · Leading Edge Devices
  > RIGHT WING KRUEGER FLAP NR 14 LOWER SUPPORT CHANNEL FOUND CRACKED AT O/B AREA. FLAP ASSEMBLY REMOVED AND REPLACED PER AMM 27-81-01 REV 143.
- [SDR VGQY2010081400101](https://openairdocs.org/sdr/VGQY2010081400101.md): Support Channel · cracked · Aug 14, 2010 · N753SA · Boeing 747228F · Leading Edge Devices
  > RIGHT WING KRUEGER FLAP NR 15 UPPER SUPPORT CHANNEL FOUND CRACKED AT O/B END. REMOVED AND REPLACED PER AMM 27-81-01 REV 143.
- [SDR VGQY2010081400100](https://openairdocs.org/sdr/VGQY2010081400100.md): Web · cracked · Aug 14, 2010 · N753SA · Boeing 747228F · Trailing Edge Flaps
  > RIGHT WING VC FLAP NR 23 FOLDING NOSE I/B FITTING SUPPORT AREA WEB FOUND CRACKED. FLAP NR 23 REMOVED AND REPLACED PER AMM 27-81-02 REV 143.
- [SDR VGQY2010081400099](https://openairdocs.org/sdr/VGQY2010081400099.md): Web · cracked · Aug 14, 2010 · N753SA · Boeing 747228F · Trailing Edge Flaps
  > RIGHT WING VC FLAP NR 23 FOLDING NOSE O/B FITTING SUPPORT AREA WEB FOUND CRACKED. FLAP ASSEMBLY REMOVED AND REPLACED PER AMM 27-81-01 REV 143.
- [SDR VGQY2010081300098](https://openairdocs.org/sdr/VGQY2010081300098.md): Skin · dented · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Main, Plate/Skin
  > FUSELAGE AT ABOUT STA 2300 BETWEEN STRINGER 11R TO 12R FOUND DENT. DENT MARK AT FUSELAGE STA 2120 TO STA 2140 TRIMMED-OUT, REPAIR DOUBLER FABRICATED AND INSTALLED PER SRM 53-30-03 REV 117 FIGURE 1. REPAIR REPETITIVE INSPECTION THRESHOLD AT 15,000FC WITH IN
- [SDR VGQY2010081300097](https://openairdocs.org/sdr/VGQY2010081300097.md): Skin · dented · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Main, Longeron/Stringer
  > FUSELAGE AT ABOUT STRINGER 43L, STA 545 FOUND DENT. DENT MARK AT FUSELAGE STA 545 BETWEEN STA STRINGERS 42L AND 43L TRIMMED-OUT, REPAIR DOUBLER FABRICATED AND INSTALLED AT STA 540-560, STA 42-44L PER SRM 53-30-03 REV 117 FIGURE 1.
- [SDR VGQY10081300097](https://openairdocs.org/sdr/VGQY10081300097.md): Stringer · dented · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Main, Longeron/Stringer
  > FUSELAGE AT ABOUT STRINGER 43L, STA 545 FOUND DENTED.
- [SDR VGQY2010081300096](https://openairdocs.org/sdr/VGQY2010081300096.md): Channel · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > CABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 800, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TRIMMED OUT & FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.
- [SDR VGQY2010081300095](https://openairdocs.org/sdr/VGQY2010081300095.md): Channel · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > CABIN - DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT RT BS 880, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TRIMMED OUT & FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.
- [SDR VGQY2010081300094](https://openairdocs.org/sdr/VGQY2010081300094.md): Channel · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 860, FOUND 01 EA HOLE CRACK INDICATION ON FWD CHANNEL. CHANNEL TRIMMED OUT; FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.
- [SDR VGQY2010081300093](https://openairdocs.org/sdr/VGQY2010081300093.md): Channel · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 820, FOUND 01 EA HOLE CRACK INDICATION ON FWD CHANNEL. FWD CHANNEL AT LT BS STA 820 TRIMMED OUT. FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. NEW CHANNEL INSTALLED PER SRM
- [SDR VGQY2010081300092](https://openairdocs.org/sdr/VGQY2010081300092.md): Frame · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Main, Frame
  > CABIN - DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 820, FOUND 01 EA HOLE CRACK INDICATION ON FRAME WEB AND DOUBLE STACK UP. REPAIR CARRIED OUT AS PER B747 SRM 53-10-11 REV 117 FIGURE 2.
- [SDR VGQY2010081300091](https://openairdocs.org/sdr/VGQY2010081300091.md): Structure · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT AFT VERTICAL CHORD FOUND CRACKED. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081300090](https://openairdocs.org/sdr/VGQY2010081300090.md): Structure · corroded · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND LT AFT VERTICAL CHORD AT STA 340 LT CORROSION EXCEEDED LIMITS. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.
- [SDR VGQY2010081300089](https://openairdocs.org/sdr/VGQY2010081300089.md): Structure · cracked · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT UPPER CHORD CRACKED. RT UPPER CHORD FABRICATED PER DWG 65B07941, LT UPPER CHORD REMOVED AND REPLACED PER SRM 51-30-02 REV 117.
- [SDR VGQY2010081300088](https://openairdocs.org/sdr/VGQY2010081300088.md): Structure · corroded · Aug 13, 2010 · N753SA · Boeing 747228F · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF NOSE WHEEL WELL MODIFICATION (EAM 4753027) FOUND LT AFT VERTICAL CHORD AT STA 340 CORROSION EXCEEDED LIMITS. LT UPPER CHORD FABRICATED PER BOEING DWG 65B02941, CONTROL NO: P0225289 LT UPPER CHORD REMOVED AND REPLACED PER SRM 51-30-02
- [SDR VGQY2010081300087](https://openairdocs.org/sdr/VGQY2010081300087.md): Skin · damaged · Aug 13, 2010 · N753SA · Boeing 747228F · Cargo/Baggage Doors
  > AFT CARGO DOOR LWR SKIN EDGE FOUND TRIM-OUT OF ABOUT.5 INCH FROM THE EDGE AT STA 1875 -1880. NEW FILLER AND DOUBLER FABRICATED USING 2024T3-0.12" MATERIAL AND INSTALLED AT AFT CARGO DOOR LOWER SKIN AT STA 1875-1880 PER SRM 52-30-06 REV 117 FIGURE 1.
- [SDR VGQY2010081100077](https://openairdocs.org/sdr/VGQY2010081100077.md): Floorbeam · cracked · Aug 11, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 420 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 3 AT 6 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR BOEING UPPER TEE HOLES FOUND CRACKED STA 420 & STA 520.
- [SDR VGQY2010081000075](https://openairdocs.org/sdr/VGQY2010081000075.md): Skin · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON, PYLON SKIN FOUND CRACK AT PANEL 463AR CUTOUT AREA. NO SRM REPAIR. HFEC INSPECTION CARRIED OUT PER SA NDTPM D6-7170 REV 134 PART 6 51-00-00 FIGURE 23 ON PYLON NR 2 PANEL SKIN 463AR CUTOUT AREA. FOUND NO CRACK EVIDENT.
- [SDR VGQY2010081000074](https://openairdocs.org/sdr/VGQY2010081000074.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE RBL 15 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK
- [SDR VGQY2010081000073](https://openairdocs.org/sdr/VGQY2010081000073.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE RBL 10 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOOR BEAM UPPER T-CHORD HOLES FOUND CRAC
- [SDR VGQY2010081000072](https://openairdocs.org/sdr/VGQY2010081000072.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 15.5 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRAC
- [SDR VGQY2010081000071](https://openairdocs.org/sdr/VGQY2010081000071.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 10 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK
- [SDR VGQY2010081000070](https://openairdocs.org/sdr/VGQY2010081000070.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 5 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOOR BEAM UPPER T-CHORD HOLES FOUND CRACK
- [SDR VGQY2010081000069](https://openairdocs.org/sdr/VGQY2010081000069.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE BBL 0 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK A
- [SDR VGQY2010081000068](https://openairdocs.org/sdr/VGQY2010081000068.md): Floorbeam · cracked · Aug 10, 2010 · N753SA · Boeing 747228F · Fuselage Main, Floor Beam
  > HFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE RBL 22 AT 6 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER TEE CHORD HOLES FOUND CRACK AT ST

Next page: https://openairdocs.org/model/boeing-747-228f/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 = '747228F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-747-228f/reports

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