JASC 5710

Service difficulty reports · 4,462

Reports filed under 5710 · Wing Main, Frame Structure, newest first.

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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 = '5710'
  ORDER BY difficulty_date DESC"

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SDR UPS02239607Rib · crackedINSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12.Sep 22, 2002 · N930UP · Boeing 72722CSDR UPS02439735Structure · damagedINSPECTION TYPE: C RT WING LE CAVITY FRONT SPAR LOWER CHORD VERTICAL FLANGE THICKNESS FOUND BLENDED PREVIOUSLY AT OLES 1322, PLS CHK LIMITATION. (20 INCHES O/B WING JACK AREA) RT WING L/E FRONT SPAR LWR CHORD VERTICAL FLANGE AT OLES 1322 IS REPAIRED AS PERSep 16, 2002 · N680UP · Boeing 747SR46SDR UPS02239398Web · crackedINSPECTION TYPE:C CRACK ON WEB ABOVE NO5 L/E FLAP I/B CORNER. CRACK STOP DRILLED IAW 727 SRM 51-10-01 NDT CARRIED OUTIAW NDT MAN 5 1-00-00 PT 6 FIG 4, CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM REF 51-40-02.Aug 30, 2002 · N941UP · Boeing 72722CSDR 02FDEA00609Structure · scratchedFUSELAGE RIGHT SIDE LWR SURFACE OF WING ROOT AT WING TO BODY FILLET (154AB) SCRATCHED. REMOVED & REPLACED SKIN PER EA. 1-5330-66000.Aug 25, 2002 · N601FE · Doug MD11SDR UPS02239194Stiffener · corrodedINSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060.Aug 17, 2002 · N926UP · Boeing 72731CSDR 0203049952Spar · crackedDuring HCK in DHN, the rear spar chord was found cracked. Repaired per EA 99-131324Aug 8, 2002 · N916RW · Doug DC931SDR CA020829006Structure · cracked(CAN) CRACK ALONG EXISTING PATH FOUND. AIRCRAFT RETURNED TO MAINTENANCE BASE. CRACK IS OUTBOARD OF BL-165 19 INCHESAug 8, 2002 · Lkheed 188ASDR COOSDR020203Panel · delaminatedRIGHT WING, TRAINLING EDGE - LOWER FIX PANEL (PN 65216522) DELAMINATED.Jul 1, 2002 · N128NA · Boeing 7272J7SDR DHL2002806506Former · crackedDURING C-CHECK FOUND RT WING CTR L/E LOWER FORMER 1 INCH CRACK STA XFS 329.000. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.Jun 30, 2002 · N806DH · Doug DC873FSDR DHL2002806524Former · crackedAT C-CHECK, FOUND RT WING CTR L/E FORMER 1 INCH CRACK STA XFS 310.250. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.Jun 30, 2002 · N806DH · Doug DC873FSDR DHL2002806521Former · crackedFOUND DURING C-CHECK, RT WING CTR L/E LWR FORMER 1 INCH CRACK STA XFS347.750. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10.Jun 30, 2002 · N806DH · Doug DC873FSDR DHL2002806525Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH AT STA XFS 697.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 7.Jun 29, 2002 · N806DH · Doug DC873FSDR DHL2002806507Former · crackedDURING C-CHECK FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED 1 INCH AT XFS 603.750. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED NEW DOUBLER PER SRM 57-2-0 FIG 2.Jun 29, 2002 · N806DH · Doug DC873FSDR DHL2002806523Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .25 INCH XFS 691.250. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 29, 2002 · N806DH · Doug DC873FSDR DHL2002806522Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH XFS 622.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 29, 2002 · N806DH · Doug DC873FSDR DHL2002806516Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .625 INCH AT XFS 641.250. STOP DRILLED CRACK PER SRM 57-2-0 PG 9. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED NEW ANGLE AND FASTENERS PER SRM 57-2-0 PG 9-10 AND SRM Jun 27, 2002 · N806DH · Doug DC873FSDR 0202159975Cap · corrodedDuring an MCK in ATL, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at three locations was determined to be ouit of limits. Repaired per EA 99-190532.Jun 27, 2002 · N9339 · Doug DC931SDR 0202149975Cap · corrodedDuring Mck in Atl, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at one location was determined to be out of limit. Repaired per EA 99-190519.Jun 27, 2002 · N9339 · Doug DC931SDR QXEA0200912Wing · leakingPDX- LEAKING FUEL RESIDUE NOTED AT 3 RIVETS ON TOP SIDE OF THE LT WING, CLOSE TO THE WING AND NACELLE AT STATION YW189.000 & THE FRONT SPAR X384.500. REPAIRED IAW DHC-8 SRM 51-40-11 AND APPLIED PR1422B 1/2 SEALANT.Jun 21, 2002 · N374PH · Dhav DHC8202SDR DHL2002806517Former · crackedDURING C-CHECK, FOUND LT WING O/B LEADING EDGE FORMER CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER WITH NEW FASTENERS PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 7, 2002 · N806DH · Doug DC873FSDR SWAA021283Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 AND S-3. REPAIRED CHORD PER BFG ER.Jun 5, 2002 · N362SW · Boeing 7373H4SDR DHL2002745501Fitting · crackedDuring C Check "Discrepancy"- R/H Wing rear spar O/B attach fitting crackecked ( Gear beam attach fitting).1) Removed R/Wing R/spar O/B attach fitting for main gear beam I.A.W. B-727 S/B 57-167 R2.2) Drilled-up new replacement fitting P/N 65-16289-12 per B-727Jun 3, 2002 · N745DH · Boeing 727224SDR NACA20020021Spar Cap · corrodedDISCREPANCY: During "C" inspection, I.G. corrosion was discovered on the L/H wing aft spar lower chord, from w.s. 224.5 TO w.s. 241.0.CORRECTIVE ACTION: Lower spar cap being replaced from LBL 70.5 to W.S. 259.May 21, 2002 · N930FT · Boeing 72723SDR IXXA0200056SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED IN THE LEFT WING LEADING EDGE TOP SIDE AT STATION XFS 825. REMOVAL ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIRMay 11, 2002 · N728PL · Doug DC862SDR UPS02438009Fitting · corrodedINSPECTION TYPE:C FX - R/H BS 1241 WING CENTER SECTION REAR SPAR WEB AFT SURFACE BULKHEAD FITTING FOUND COR BETWEEN FASTENER #2 AND #9. R/H BS 1241 WING CENTER SECTION REAR SPARE WEB AFT FACE BULKHEAD FTG BETWEEN FASTENER #2 & #9 CORROSION REMOVED AS PER UMar 24, 2002 · N525UP · Boeing 747212BSDR 2002F00384Torque Box · crackedDURING SCHEDULED INSPECTION A 2 INCH CRACK WAS FOUND AT THE LEFT MAIN LANDING GEAR TORQUE BOX AFT WEB WALL, LOWER INBOARD CORNER. MAINTENANCE INSTALLED ANGLE AND WEB PER SRM 51-40-01, FS 1284, WSL 319, LBL 222.Feb 18, 2002 · N188AT · Lkheed 10113851SDR 2002FA0000260Strut · damagedWING STRUTS HAD FILLED WITH WATER FROM SITTING OUTSIDE. RUST STAINS VISIBLE FROM OUTSIDE OF STRUT. WHEN POKED WITH AN AWL IT PUSHED A HOLE INTO STRUT AND DRAINED WATER. DRILLED A .0312 HOLE IN BOTTOM OF OTHER 3 STRUTS AND WATER CAME OUT IN EXCESS OF 1 CUP EFeb 1, 2002 · N2762E · Bbavia 7CCMSDR AUS20020248Structure · corroded(AUS) UPPER RT WING TOP CHORD CORRODED. CORROSION LOCATED AT ZONE 6-76, WS 351RT TO WS 355 RT.Jan 30, 2002 · Boeing 72777CSDR G1X2002F00000Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE Jan 28, 2002 · N105GX · Israel GALAXYSDR USAA020067Beam · crackedPIT - FOUND LEFT MLG BEAM SUPPORT WITH TWO CRACKS MERGED INTO ONE AT 1.5 INCH LONG, RT MLG BEAM SUPPORT FTG TOP FASTENER INBOARD OF BEAM. REPLACED FITTING PER BOEING SB 737-57-1216 REV 2 DATED 2/6/99. (M)Jan 23, 2002 · N391US · Boeing 7373B7SDR QXEA0200102Bearing · roughPDX - LT AILERON OUTBOARD HINGE BEARING IS ROUGH. REPLACED BEARING IAW DHC-8 MM PSM 1-82-2, 20-21-52, TASK 20-21-52-390-801.Jan 17, 2002 · N356PH · Dhav DHC8202SDR 0200099603Panel · crackedDuring HCK in ATL a crack was found in the aft flange of the right trapezoidal panel. Repair accomplished in accordance with EA 96-185424.Jan 8, 2002 · N603NW · Doug DC932SDR AUS20011437Bolt · sheared(AUS) H11 BOLT LOCATED AT STN 1241/LBBL 127/WL 163 SHEARED. FOLLOWING REMOVAL OF THE BOLT CORROSION WAS FOUND IN THE BULKHEAD FITTING BORE. FOUND DURING ULTRASONIC INSPECTION.Dec 30, 2001 · Boeing 747338SDR 0105209613Spar Cap · corrodedDuring Mck in DHN the right wing rear spar upper cap was found corroded at the inboard hole. Repaired per EA 96-187657.Dec 27, 2001 · N613NW · Doug DC932SDR QXEA0102162Structure · leakingPDX - FUEL LEAK ON LT WING LOWER SKIN AT STATION 2635 AND STRINGER 2.9 JUST AFT AND OUTBOARD OF FUEL PANEL 71A. REPAIRED IAW FOKKER MM 28-11-06, PAGE 403.Dec 21, 2001 · N488US · Fokker F28MK4000SDR QXEA0102080Structure · crackedPDX - SUSPECTED CRACK IN WING STRUCTURE RADIATING FROM LOWER SMALL BOLT LOCATED OUTBOARD OF RIGHT MAIN LANDING GEAR AFT TRUNNION POINT AT WS 117.165. REPAIRED IAW FOKKER SRM 51-35-02, PARAGRAPH 2 C (3), PAGE 2 AND SRM 57-02-09, PAGE 2, PARAGRAPH 3.Dec 14, 2001 · N488US · Fokker F28MK4000SDR IY22002F00000Structure · corrodedDURING PREPARATION OF AIRCRAFT FOR PAINT, CORROSION WAS FOUND ON THE TOP OF THE LEFT WING BETWEEN WING STATIONS 125.00 TO 181.10 AND SPAR NR 5 TO 8 UNDER A RAISED BACK COVER. THE CORROSION IS AS MUCH AS .044 INCHES DEEP. WHEN THE COVER WAS REMOVED, NUMEROUS Dec 13, 2001 · N972H · Lear 25DSDR 2002F00257Structure · damagedLEFT WING TIP DAMAGED AT YYZ. REMOVED AND REPLACED LEFT WING TIP FORWARD AND AFT ASSEMBLY (P/N 65-73719-505A AND 6573719-369) PER 8737-400 M/M 57-21-11. (M)Dec 12, 2001 · N37NY · Boeing 737400SDR QXEA0102045Structure · corrodedPDX - CORROSION INSIDE RT WING FUEL TANK AT STRINGER 2.36. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.Dec 8, 2001 · N488US · Fokker F28MK4000SDR MWEA011469Angle · crackedRIGHT WING - FORWARD LOWER WING TO FUSELAGE ATTACH ANGLE UPPER FLANGE IS CRACKED BETWEEN LONGERON 22 AND 23 RIGHT -- REMOVED CRACKED ANGLE. LOCATED AND INSTALLED NEW ANGLE.Dec 4, 2001 · N300ME · Doug DC915SDR QXEA0102006Structure · chafedPDX - STRUCTURE IS CHAFED AT LOWER ATTACH POINT FOR LT WING ROOT FAIRING 91J. REPAIRED IAW HORIZON AIR EA 4-57-569.Nov 20, 2001 · N482US · Fokker F28MK4000SDR CA011109014Fastener · sheared(CAN) DURING A 12C INSPECTION (7200 HOUR) MAINTENANCE PERSONNEL FOUND SEVERAL SHEARED HILOCKS ON THE LEFT HAND WING AT RIB NR 6.THE LEFT HAND LANDING GEAR WAS REMOVED AND AREA INSPECTED, NO STRUCTURAL DAMAGE WAS FOUND. 22 HILOCKS WERE REPLACED AND GEAR REINSTAOct 13, 2001 · Emb EMB110P1SDR MWEA011336Spar · unserviceablePREVIOUS REPAIR AT LEFT WING STATION 164 THAT STRADDLES #3 FLAP HINGE, AND ON THE AFT WING SPAR IN THE SAME AREA. -- REMOVED AND REPLACED SPAR TEE SECTION AND SPLICE. FABRICATED AND INSTALLED WEB SPLICE REPAIR.Oct 1, 2001 · N814ME · Doug DC981SDR UPS01836976Fitting · crackedINSPECTION TYPE: C1, RIGHT WING STRINGER 64 END/SPLICE FITTING IS CRACKED AT FRONT SPAR. REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 3644046,AND SRM. 51-1-20DSep 28, 2001 · N867UP · Doug DC873SDR UPS01836975Fitting · crackedINSPECTION TYPE: C1, LEFT WING STRINGER 64 END SPLICE FITTING IS CRACKED AT FRONT SPAR. REMOVED,FABRICATED,AND REPLACED FITTING I.A.W. DWG. 3644046.AND SRM. 51-1-20DSep 26, 2001 · N867UP · Doug DC873SDR ABXA010507Skin · crackedRIGHT WING AT STATION XW 253 OUTBD OF #3 PYLON AT LEADING EDGE, WAS CRACKED. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 57-2-1 FIG 2H.Sep 25, 2001 · N815AX · Doug DC863SDR AALA20011815Structure · damagedTUL - FOUND MAINTENANCE ENTRY DAMAGED RIGHT WING FROM L/E OF NR 5 SLAT BACK TO THE AILERON AT INBOARD ATTACH POINT. FABRICATED AND INSTALLED DOUBLER TO LOWER RIGHT WING LEADING EDGE OF NR 5 SLAT BACK TO AILERON AT INBOARD ATTACH POINT IAW ESO 80559. (M)Sep 18, 2001 · N462AA · Doug DC982SDR MWEA011142Frame · bentRIGHT WING SUPPORT FRAME OUTBOARD OF TAT TELESCOPING IS BENT. -- FABRICATED AND INSTALLED STIFFNER.Aug 30, 2001 · N701ME · Doug MD88SDR QXEA0101475Structure · leakingPDX -FUEL LEAKING FROM HI LOCK, BOTTOM OF LEFT WING 13 INCHES FORWARD OF LEFT LANDING GEAR FORWARD TRUNNION. REMOVED AND REPLACED HI LOCKS AND SEALED SAME IAW F28 SRM 51-30-02. SEALED HI LOCK COLLARS IAW F28 MANUAL 28-11-00 PARAGRAPHS 4A,5A,B,C AND D.Aug 28, 2001 · N491US · Fokker F28MK4000SDR 16824Fitting · damagedYUL---DURING 4C INSPECTION YUL MAINTENANCE, AS PER COEX 5710-01025, INSPECTED AND REWORKED THE RT REAR WING SPAR FITTINGS BETWEEN WING RIBS 7/8 AND RIB 12. AIRCRAFT RETURNED TO SERVICE.Aug 27, 2001 · N16824 · Aerosp ATR42320
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