JASC 5712

Service difficulty reports · 6,970

Reports filed under 5712 · Wing, Rib/Bulkhead, newest first.

Query with SQL
duckdb -csv -c "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 jasc_code = '5712'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS03441324Rib · corrodedINSPECTION TYPE: C, RIGHT WING - NR 18 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). FINAL HOLE SIZE 0.434 INCH AT HOLE NR 4. RIGHT WING NR 18 V/C FLAP O/B LINKAGE I/B RIB REPLACESep 5, 2003 · N682UP · Boeing 747121SDR UPS03441312Rib · crackedINSPECTION TYPE: C, LT WING - NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND AS PER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441305Rib · crackedINSPECTION TYPE: C, RT WING NR 26 V/C FLAP I/B LINKAGE I/B AND O/B SUPPORT RIBS FOUND CRACKED. RT WING NR 26 V/C FLAP I/B LINKAGE BOTH I/B AND O/B RIBS REPLACED IAW SRM 51-10-01 PG 8.Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441304Rib · corrodedINSPECTION TYPE: C, LT WING NR 4 V/C FLAP I/B LINKAGE O/B SUPPORT RIB FOUND CORROSION CRACKED. RIB ASSY REPAIRED IAW SRM 51-10-01 PG 8.Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441303Rib · crackedINSPECTION TYPE: C, LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441302Rib · corrodedINSPECTION TYPE: C, LT WING NR 1 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND FITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 5 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441301Rib · corrodedINSPECTION TYPE: C, LT WING NR 1 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441300Rib · corrodedINSPECTION TYPE: C, LT WING NR 2 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441299Rib · corrodedINSPECTION TYPE: C, LT WING NR 2 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLES NR 2 TO NR 6 AND NR 8 REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-1926Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441294Rib · corrodedINSPECTION TYPE: C, LT WING NR 8 V/C FLAP O/B UNKAGE I/B RIB NR 2 AND NR 3 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 AND NR 3 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441293Rib · corrodedINSPECTION TYPE: C, LEFT WING NR 8 V/C FLAP I/B LINKAGE O/B RIB NR 3, NR 5 AND NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3, NR 5 AND NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441292Rib · corrodedINSPECTION TYPE: C, LT WING NR 9 V/C FLAP I/B UNKAGE O/B RIB NR 2, NR 3 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441291Rib · corrodedINSPECTION TYPE: C, LT WING NR 9 V/C FLAP O/B UNKAGE O/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441290Rib · corrodedINSPECTION TYPE: C, LT WING - NR 10 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 5 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 5 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-1Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441289Rib · corrodedINSPECTION TYPE: C, LT WING NR 10 V/C FLAP I/B LINKAGE O/B RIB NR 4, NR 5 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLE NR 4, NR 5 AND NR 7 REPAIRED AS PER RS 574135066 AND REFER EO B747-5740-19269-A FOSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441288Rib · corrodedINSPECTION TYPE: C, RT WING NR 18 V/C FLAP I/B LINKAGE O/B RIB NR 1 TO NR 3, NR 5, NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 3, NR 5, NR 6 AND NR 8 BOLT HOLES REPAIRED AS PER RS 574135066 AND Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441287Rib · corrodedINSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441286Rib · corrodedINSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE O/B RIB NR 4 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 4 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441285Rib · corrodedINSPECTION TYPE: C, RT WING NR 19 V/C FLAP O/B LINKAGE I/B RIB NR 1, NR 7 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION. NR 1, NR 7 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441284Rib · corrodedINSPECTION TYPE: C, RT WING - NR 19 V/C FLAP O/B LINKAGE O/B RIB NR 1, NR 6 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1, NR 6 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441283Rib · corrodedINSPECTION TYPE: C, RT WING - NR 20 V/C FLAP I/B LINKAGE O/B RIB NR 2, NR 3 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269Sep 5, 2003 · N682UP · Boeing 747121SDR UPS03441282Rib · corrodedINSPECTION TYPE: C, RT WING - NR 20 V/C FLAP O/B LINKAGE I/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441281Rib · corrodedINSPECTION TYPE: C, RT WING NR 26 V/C FLAP O/B LINKAGE I/B RIB NR 1 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441280Rib · corrodedINSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE O/B RIB NR 3 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSep 5, 2003 · N682UP · Boeing 747121SDR UPS03441275Rib · corrodedINSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE IB RIB NR 7 ROTARY ACTUATOR MOUNTING AREA FOUND CORRODED ( COUNT FROM IB CLOCKWISE ). NR 7 BOLT AREA REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.Sep 5, 2003 · N682UP · Boeing 747121SDR QXEA200301087Rib · chafedRT HAND WING RIB IS CHAFED BY FUEL LINE AT STATION YW207 LOWER SURFACE OF UPPER RIB MEMBER 4 INCHES AFT OF PANEL 624AT CUTOUT. REPAIRED IAW DHC-8 SRM 51-00-06, 57-20-00 AND RD 8-57-2664.Aug 30, 2003 · N347PH · Dhav DHC8202SDR 03FDEA01431Rib · crackedLT WING L/E CAVITY, NR 16 RIB CRACKED. LT WING- L/E CAVITY, NR 16 RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.Aug 29, 2003 · N603FE · Doug MD11SDR X6PA200300004Rib · crackedWHILE PERFORMING A 100 HOUR INSPECTION A 1 INCH CRACK AND WARPAGE OF WING RIB P/N 78500-003 AT WING STATION 69.24 RIGHT. A NEW RIB WAS INSTALLED P/N 78500-003 PER AC 43. 13-1B AND A 337 COMPLETED. PIPERS NEW RIB P/N 78500-003 CONTAINS REINFORCEMENT WHICH SHOAug 28, 2003 · N997BW · Piper PA34200SDR 2003UALA00651Rib · crackedLT WING TRAILING EDGE WBL 445.94 RIB 65B08150-99 HAS A CRACK IN THE VERTICAL FLANGE BETWEEN 2 FASTENERS. DAMAGE CAN BE VIEWED FROM OUTBOARD END OF INBOARD FLAP WELL BELOW 65B07818 MIDFLAP DEFLECTOR RAMP.Aug 27, 2003 · N177UA · Boeing 747422SDR UPS03641142Rib · crackedINSPECTION TYPE:C3 NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IS CRACKED ON FORWARD FLANGE. REPAIRED NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IAW GOODRICH ER NR 03-3162Aug 22, 2003 · N323UP · Boeing 76734AFSDR ASOA03392Rib · crackedDURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WLS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53-60 IAW ASA EO 600-57-039A. (M)Aug 21, 2003 · N848AS · Cndair CL6002B19SDR DHL2003805528Frame · wornRIGHT WING OTBD STUB WING L/E FORMER WORN AT XW 454.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 17. INSTALLED ANGLEAug 18, 2003 · N805DH · Doug DC873FSDR DHL2003805513Frame · crackedLEFT WING CTR L/E FORMER CRACKED (STA XFS 335.250 - XFS 329.000). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. HEAT TREATED IAW SRM 51-1-1 PG 17. Aug 15, 2003 · N805DH · Doug DC873FSDR DHL2003805504Frame · crackedRIGHT WING CTR L/E FORMER CRACKED 4.000, AT STA XFS 341.500 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER IAW SRM 57-2-0 PG 9-10 (7075-T6 0.040). CLEANED, Aug 13, 2003 · N805DH · Doug DC873FSDR DHL2003805575Frame · crackedLEFT WING CTR L/E FORMER CRACKED 1.000 AT STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 8, 2003 · N805DH · Doug DC873FSDR DHL2003805522Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 416.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 8, 2003 · N805DH · Doug DC873FSDR DHL2003805517Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 461.372. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAug 8, 2003 · N805DH · Doug DC873FSDR DHL2003805529Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 7, 2003 · N805DH · Doug DC873FSDR DHL2003805516Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 448.561. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 7, 2003 · N805DH · Doug DC873FSDR DHL2003805515Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 347.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INAug 7, 2003 · N805DH · Doug DC873FSDR DHL2003805559Frame · crackedRIGHT OUTER WING INBD L/E FORMER CRACKED 2.000, STA XFS 672.500 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW Aug 6, 2003 · N805DH · Doug DC873FSDR DHL2003805562Frame · crackedRT OUTER WING INBD L/E FORMER CRACKED 1.000, STA XFS 660.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAAug 6, 2003 · N805DH · Doug DC873FSDR DHL2003805561Frame · crackedRIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS 635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. INSTALLED ANGLE DOUBLER WIAug 6, 2003 · N805DH · Doug DC873FSDR DHL2003805560Frame · crackedRT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.641.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE Aug 6, 2003 · N805DH · Doug DC873FSDR DHL2003805523Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 478.897. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED AN ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSAug 6, 2003 · N805DH · Doug DC873FSDR DHL2003805590Frame · crackedRIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEAug 6, 2003 · N805DH · Doug DC873FSDR UPS03441129Rib · crackedINSPECTION TYPE:C RT WING LE NR 18 VC FLAP IB ARM OB RIB AT ILES 802 CRACKED. STOP DRILLED CRACK TRIMMED OFF STIFFENER THE REPAIR FTG AND THE REPAIR STRAP INSTALLED IAW HXRS NR R57-41-35055 AND EO B747-5740-19118-A ISSUED FOR REPLACE THE RIB WITHIN 18 MONTAug 6, 2003 · N676UP · Boeing 747123SDR DHL2003805519Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500 AT XFS 641.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Aug 4, 2003 · N805DH · Doug DC873FSDR DHL2003805526Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 467.323 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Aug 3, 2003 · N805DH · Doug DC873FSDR 03FDEA01246Rib · crackedLEFT WING- SLAT TRACK 2316 INBOARD RIB FOUND CRACK 2C LENGTH OF CRACK APPROX 750 22. LT WING - SLAT TRACK NR 16 INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.Aug 3, 2003 · N596FE · Doug MD11
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