# Service difficulty reports: JASC 5750

A list on [JASC 5750](https://openairdocs.org/jasc/5750.md).

Reports filed under 5750 · Wing, Control Surfaces, newest first.

Page 1 of 24 · 1,157 reports

- [SDR UIEA2026082600803](https://openairdocs.org/sdr/UIEA2026082600803.md): Skin · delaminated · Sep 11, 2026 · N642GT · Boeing 7673Y0
  > LEFT WING T/E OTBD FLAP LOWER SKIN, BETWEEN FLAP FAIRINGS, FOUND DELAMINATED. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07, PAR 5 A(1). NO FURTHER DEFECTS NOTED.
- [SDR QXEA2026070600153](https://openairdocs.org/sdr/QXEA2026070600153.md): Unknown · sparks · Jul 2, 2026 · N624QX · Emb ERJ170200LR
  > PASSENGER REPORTED ELECTRICAL SPARKS OBSERVED MID FLIGHT WING RETRACTING FLAPS AND SPOILERS UP. REMOVED FROM SERVICE. EXTENDED FLAPS AND SLATS COMPLIED WITH VISUAL INSPECTION NO DEFECTS NOTED. COMPLIED WITH SPOILER SYSTEM OPERATIONAL TEST IAW AMM TASK 27-60-0
- [SDR FDEA202606280938](https://openairdocs.org/sdr/FDEA202606280938.md): Spoiler · delaminated · Jun 28, 2026 · N680FE · Airbus A300F4605R
  > LH WING #3 SPOILER CENTER HINGE OUTBD ARM OUTBD WEB FOUND DELAMINATION. SIZE:40MM*25MM, DEPTH: 1.1MM COMPLIED WITH EA 6-5750-T0387764 P1, EA TITLE:WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE DELAMINATI
- [SDR SWAA2026072827428](https://openairdocs.org/sdr/SWAA2026072827428.md): Access Panel · corroded · Jun 24, 2026 · N8649A · Boeing 7378H4
  > CORROSION ON BRACKET OF ACCESS PANEL 191CR AT LOWER FUSELAGE. REPLACED BRACKET OF ACCESS PANEL 191CR AT LOWER FUSELAGE IAW SRM 51-10-02, I?TEM 9, SRM 51-40-02, & DWG 149A7147, SHEET 2, REV A.
- [SDR FDEA202604150447](https://openairdocs.org/sdr/FDEA202604150447.md): Skin · delaminated · Apr 15, 2026 · N163FE · Boeing 767300
  > DELAMINATION ON L EDGE FLAP SKIN AT 24" FROM INB EDGE. RH OUTB FLAP RH WING, RH OUTBD FLAP ON LE FLAP SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 5 AND SRM 51-70-17-0G PAR 4A FIG 10 REV 94 DEC 15/2025
- [SDR SWI2025F01700](https://openairdocs.org/sdr/SWI2025F01700.md): Shaft · damaged · Aug 24, 2025 · N897SK · Cndair CL6002D24
  > LEFT INBOARD FLAP, VANE ACTUATOR AT 584AB, SHAFT HAS MARRING, COMPLIED WITH THE REPAIR OF THE LT INBD FLAP VANE ACTUATOR AT 584AB IAW REO 670-57-52-257, REV B. OPS CHECKED GOOD.
- [SDR SWAA2025092305983](https://openairdocs.org/sdr/SWAA2025092305983.md): Access Panel · elongated · Aug 19, 2025 · N7751A · Boeing 7377BD
  > ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SCNA20250627235](https://openairdocs.org/sdr/SCNA20250627235.md): Flap Track · excess play · Jun 8, 2025 · N5693A · Boeing 7378
  > UPON DISASSEMBLY OF THE R/W I/B AFT FLAP TRACK FOR EXCESSIVE AXIAL PLAY. FOUND O/B TRACK, I/B SIDE, O/B FACE HAS EXCESSIVE WEAR. O/B FLAP FITTING I/B LUG AT R/W I/B AFT FLAP FOUND TO BE OUT OF LIMITS DUE TO THE DAMAGE IS JUST NEXT TO THE EDGE OF THE BUSHING.
- [SDR SWAA2025060266658](https://openairdocs.org/sdr/SWAA2025060266658.md): Fairing · delaminated · May 2, 2025 · N285WN · Boeing 7377H4
  > PANEL 643EB (#7 CANOE FAIRING CONE) IS DELAMINATED.<[01] RECEIVED NEW PANEL 643EB LOCATED AND DRILLED IAW SRM 51-40-05 AND AIPC 27-51-28-04;;[02] RECEIVED NEW PANEL 643EB LOCATED AND DRILLED IAW SRM 51-40-05 AND AIPC 27-51-28-04; AND DWG 113A9252 REV A;[03] NE
- [SDR FDEA202503230482](https://openairdocs.org/sdr/FDEA202503230482.md): Skin · dented · Mar 23, 2025 · N175FE · Boeing 7673S2F
  > RH WING, SLAT # 10, TRAILING EDGE WEDGE, UPPER SURFACE WITH HAIL DAMAGE RH WING, SLAT # 10, T/E WEDGE, UPPER SURFACE WAS REPAIRED IAW EA #:H-5750-T0382644 RELEASE DATE: MAR 22,2025.
- [SDR SWAA2025042407617](https://openairdocs.org/sdr/SWAA2025042407617.md): Plate · cracked · Mar 19, 2025 · N8688J · Boeing 7378H4
  > RT WING WIGGLE PLATE CRACKED AT PANEL 651EB FWD ATTACH POINT. <[01] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.; [02] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02. C/W INSPECTION.
- [SDR SWAA2025042307786](https://openairdocs.org/sdr/SWAA2025042307786.md): Plate · worn · Mar 18, 2025 · N8688J · Boeing 7378H4
  > LEFT WING - DEFLECTION CONTROL RIB; SERRATED PLATE WORN AT ATTACH POINT. <[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.070?. DAMAGE FOUND TO BE BEYOND ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-02-1A-1.; [02] CUT OUT AFFECTED DAMAGE AREA I.
- [SDR SWAA2025040202176](https://openairdocs.org/sdr/SWAA2025040202176.md): Plate · cracked · Mar 4, 2025 · N287WN · Boeing 7377H4
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2025-168012 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMA
- [SDR SWAA2025012890024](https://openairdocs.org/sdr/SWAA2025012890024.md): Fairing · pulled · Jan 27, 2025 · N225WN · Boeing 7377H4
  > #3 FLAP FAIRING RUB STRIP RIVETS PULLED THROUGH WIDTH MEASUREMENTS FOR HOLES FROM LEFT TO RIGHT 0.259 0.228 0.255 0.204 0.209<[01] PERFORMED REPAIR 2 ALTERNATIVE 1 IN REF TO SRM 57-53-70-2R-2, WIDTH MEASUREMENTS FOR HOLES: 0.259, 0.228, 0.255, 0.204, AND 0.209
- [SDR FDEA202501230122](https://openairdocs.org/sdr/FDEA202501230122.md): Access Panel · cracked · Jan 23, 2025 · N114FE · Boeing 7673S2F
  > WING RH ACCESS PANEL 666 MT, PERFORATED WING RH ACCESS PANEL 666 MT WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 SHEET 3 AND B767 SRM 51-70-10-2R REPAIR 4 FIG 201 SHEET 1 REV 90 AUG 15,2024
- [SDR SWAA2025020381655](https://openairdocs.org/sdr/SWAA2025020381655.md): Access Panel · cracked · Dec 29, 2024 · N213WN · Boeing 7377H4
  > CRACK INTERNAL AREA FLAP TRACK FAIRING ACCESS PANEL 642BB OUTBOARD RETAINER RT WING 2024-773818<[01] REPLACED OUTBOARD RETAINER ON INTERNAL AREA FLAP TRACK FAIRING ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G.;[02] REPLACED OUTBOARD RETAINER ON INTE
- [SDR UIEA2024112901131](https://openairdocs.org/sdr/UIEA2024112901131.md): Pseu · malfunctioned · Nov 29, 2024 · N1997A · Boeing 76733A
  > AS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(<P>TROUBLESHOT & FOUND PSEU CARD MSG 002 AND TARGET MSG 266, TARGET MSG 266, FOUND RH MSG 002, SENSOR HARNESS 266, R/R PER AMM 3
- [SDR SWAA2025010270821](https://openairdocs.org/sdr/SWAA2025010270821.md): Panel · cracked · Nov 23, 2024 · N8607M · Boeing 7378H4
  > CRACK ACCESS PANEL 661BB AT RT WING 2024-728194<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189443 DUE DATE: 06/MAR/25.;[02] TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 25-JAN-25;[03] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600 S
- [SDR SWAA2024120270144](https://openairdocs.org/sdr/SWAA2024120270144.md): Bracket · cracked · Nov 20, 2024 · N8672F · Boeing 7378H4
  > RIGHT WING SHELF PANEL 651FB; THE BRACKET FOR THE GEAR ACTUATOR FLEX LINE GUIDE IS CRACKED.<[01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED BRACKET PER SRM 51-40-02.
- [SDR FDEA202411201702](https://openairdocs.org/sdr/FDEA202411201702.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R
  > 1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB26, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB26~27,S-2.2~S-2.1 FOR REPAIR I.A.W FEDEX EA NO:T6-5750-
- [SDR WRXR20241115004](https://openairdocs.org/sdr/WRXR20241115004.md): Flap · gouged · Nov 15, 2024 · N540EG · Cndair CL6002C10
  > CHAFING FOUND ON RH I/B FLAP PANEL 684ET. PERFORMED BLENDING ON RH I/B FLAP PANEL 684ET IAW EA# A1-670-57-00066 REV-- REV DATE 2024-11-08. PERFORMED NDI, NO CRACKS NOTED. APPLIED ALODINE-BONDERITE, M-CR 1132, PB31454331, EXP:04/03/25. REMOVED AND REPLACED FA
- [SDR SWAA2024120257453](https://openairdocs.org/sdr/SWAA2024120257453.md): Bracket · cracked · Nov 6, 2024 · N8672F · Boeing 7378H4
  > PANEL 551FB HAS CRACKED WIRING HARNESS STANDOFF BRACKET(MARKED).<[01] REMOVED AND REPLACED BRACKET PER ARM 51-40-02;[02] CW
- [SDR FDEA202407010907](https://openairdocs.org/sdr/FDEA202407010907.md): Skin · worn · Jul 1, 2024 · N141FE · Boeing 7673S2F
  > RH WING, SLAT #8, TRAILING EDGE, NEAR INNER AUXILIARY TRACK, LOWER SKIN WITH WEAR. RH WING, SLAT #8, TRAILING EDGE, NEAR INNER AUXILIARY TRACK, LOWER SKIN WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R FIG 201 (SHEET 1) PAG 150,151,1
- [SDR FDEA202405270824](https://openairdocs.org/sdr/FDEA202405270824.md): Rib · cracked · May 27, 2024 · N729FD · Airbus A300B4622R
  > ONE CRACK (10MM) WAS FOUND AT R/H WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB20 S-2.7~2.8 AND DOUBLER REPAIR AT RIB19-20 S2.1R, RT CENTER FLAP IAW EA T6-5750-T0379321 P1, REPAIR CLASSIFIED AS MAJOR CAT.A PER
- [SDR FDEA202403010226](https://openairdocs.org/sdr/FDEA202403010226.md): Skin · dented · Mar 1, 2024 · N160FE · Boeing 7673S2F
  > LEFT WING, OUTBOARD TRAILING EDGE FLAP AT LOWER PANEL BETWEEN OTEF STA 3.75 AND OTEF STA 83.73, BETWEEN FWD SPAR AND MID SPAR WITH DENT. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT LOWER PANEL BETWEEN OTEF STA 3.75 AND OTEF STA 83.73, BETWEEN FWD SPAR AND MI
- [SDR AALA202402069940](https://openairdocs.org/sdr/AALA202402069940.md): Turnbuckle · damaged · Jan 29, 2024 · N893NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: THE FLAPS INDICATED ASYMMETRICAL BETWEEN 0 AND 1, WITH BOTH OUT OF ZERO. AIRCRAFT RETURN TO AND LANDED SAFELY AT MSY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR (AALA202401304708): REMOVED AND RE
- [SDR FDEA202401280119](https://openairdocs.org/sdr/FDEA202401280119.md): Hinge Bracket · corroded · Jan 28, 2024 · N528FE · Doug MD11F
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07.OVERSI
- [SDR SWAA2024022743650](https://openairdocs.org/sdr/SWAA2024022743650.md): Gusset · cracked · Jan 22, 2024 · N459WN · Boeing 7377H4
  > LEFT WING: UPPER T/E PANEL ABOVE #1 PYLON AFT TIP; LOWER SUPPORT GUSSET CRACKED AT TRANSVERSE WEB ATTACH POINT; LWR ATTACH FASTENER<[01] REMOVED AND REPLACED SUPPORT GUSSET AT TRANSVERSE WEB LEFT WING AT UPPER TRAILING EDGE FIXED PANEL ABOVE #1 PYLON AFT TIP I
- [SDR AALA202401173924](https://openairdocs.org/sdr/AALA202401173924.md): Carriage · flattened · Jan 12, 2024 · N781AN · Boeing 777223
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND OUTBOARD FLAP INBOARD TRACK INBOARD UPPER ROLLER HAS FLAT SPOT. REMOVED AND REPLACED LEFT HAND OUTBOARD FLAP INBOARD TRACK AUXILIARY SUPPORT CARRIAGE. PER B777-200 AMM 27-51-23-000-801 AND AMM 27-51-24-400-801. ADJUSTMEN
- [SDR FDEA202312181947](https://openairdocs.org/sdr/FDEA202312181947.md): Slat · debonded · Dec 18, 2023 · N791FD · Boeing 757200
  > #9 SLAT FOUND DISBONDED.
- [SDR SWAA2024011631079](https://openairdocs.org/sdr/SWAA2024011631079.md): Support Beam · cracked · Dec 12, 2023 · N8312C · Boeing 7378H4
  > CRACK ON SUPPORT BEAM LOCATED TRAILING EDGE DEFLECTION CONTROL RIB AT LT WING 2023-751706<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR LOC TRAILING EDGE ON SUPPORT BEAM LOCATED TRAILING
- [SDR AALA202312126138](https://openairdocs.org/sdr/AALA202312126138.md): Gear · corroded · Dec 3, 2023 · N800AN · Boeing 7878
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING NUMBER 7 SLAT OUTBOARD TRACK SECTOR GEAR HAS CORROSION. REMOVED, REPAIRED AND INSTALLED RIGHT HAND WING NUMBER 7 SLAT OUTBOARD TRACK SECTOR GEAR. PER BOEING CMM 27-83-21 AND AMM B7887-A-27-81-00-22A-280B-A.
- [SDR FDEA202311011819](https://openairdocs.org/sdr/FDEA202311011819.md): Slat · dented · Nov 1, 2023 · N969FD · Boeing 757200
  > LH WING UPPER SURFACE OF SLAT #3 T/E WEDGE HAS 1 DENT LOCATED 83" FROM I/B EDGE AND 4.5" FROM T/E REPAIRED 1EA DENT ON LH WING #3 SLAT T/E WEDGE UPPER SURFACE BY PERFORMING PERMANENT REPAIR IAW B757 SRM 57-43-02-1A, 57-43-02-2R AND 51-70-10-2R
- [SDR DALA2023103108947](https://openairdocs.org/sdr/DALA2023103108947.md): Unknown · unknown · Oct 30, 2023 · N319NB · Airbus A319114
  > SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 5 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #5 ON LH AS PER AIRBUS CMM 57-51-54. (0041896)
- [SDR FDEA202310041700](https://openairdocs.org/sdr/FDEA202310041700.md): Flap · delaminated · Oct 4, 2023 · N132FE · Boeing 767300
  > RH WING INBOARD FLAP, MAIN FLAP, LEADING EDGE OUTBOARD SIDE WITH DISBONDED RH WING INBOARD MAIN FLAP LEADING EDGE OUTBOARD SIDE WAS REPAIRED IAW B767 SRM 57- 53-01-2R REPAIR 1 FIG 201 SHEET 1,2,5 TABLE 1 AND SRM 51-70-05-0G PARAG 5A PAGE 1,29,37 AND 45 FIG
- [SDR FDEA202309251645](https://openairdocs.org/sdr/FDEA202309251645.md): Flap · chafed · Sep 25, 2023 · N914FD · Boeing 757200
  > LEFT WING I/B MAIN FLAP LOWER SURFACE AT MLG AFT TRUNNION FAIRING CONTACT HAS CHAFFING WEAR MARKS. EVALUATED L/W I/B MAIN FLAP LE LOWER SURFACE CHAFFED AND FOUND TO BE WITHIN ALLOWABLE LIMITS AND RESTORED FIBERGLASS OUTER PLY ON LE AND NO DEFECTS NOTED IAW
- [SDR SWAA2023083191807](https://openairdocs.org/sdr/SWAA2023083191807.md): Access Panel · cracked · Aug 20, 2023 · N966WN · Boeing 7377H4
  > R/H FWD O/B ACCESS PANEL 193CR IS SHOWING A CRACK SEE DOT<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA AS MARKED AT PANEL #193CR AS PER B737 SRM 51-70-04-2R-1 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N; MATERIAL USED PO#1791128 AND PO#1690463;[02] APPLIED PERMANENT
- [SDR FDEA202308191459](https://openairdocs.org/sdr/FDEA202308191459.md): Bracket · corroded · Aug 19, 2023 · N631FE · Doug MD11F
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZ
- [SDR SWAA2023091188581](https://openairdocs.org/sdr/SWAA2023091188581.md): Panel · elongated · Aug 12, 2023 · N225WN · Boeing 7377H4
  > ELONGATED HOLE ON LEADING EDGE ACCESS PANEL 621LB RT WING (1 EA) 2023-490744<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189416; DUE DATE: 19/DEC/23;[02] TOOL USED: SCALE P/N:CR5200 S/N:8342514510 DUE DATE: 13-FEB-24;[03] TOOL USED: HOT BONDER PN: HCS9200B-
- [SDR FDEA202308041357](https://openairdocs.org/sdr/FDEA202308041357.md): Aileron · damaged · Aug 4, 2023 · N179FE · Boeing 767300
  > LH WING, OUTBOARD AILERON, TRAILING EDGE, OUTBOARD END WITH LIGHTNING STRIKE LH WING, OUTBOARD AILERON TRAILING EDGE OUTBOARD END WAS REPAIRED IAW E.A.#: H-2710- T0375526 RELEASE DATE: AUG 01, 2023
- [SDR SWAA2023083092549](https://openairdocs.org/sdr/SWAA2023083092549.md): Panel · bulged · Aug 3, 2023 · N966WN · Boeing 7377H4
  > R/H FWD O/B ACCESSPANEL # 193CR HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL 193CR AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N; MATERIAL USED PO#1791128 ANA PO#1690463
- [SDR SWAA2023080784335](https://openairdocs.org/sdr/SWAA2023080784335.md): Bracket · cracked · Aug 1, 2023 · N7819A · Boeing 7377Q8
  > LEFT MAIN WHEEL WELL UPPER T/E PANEL SUPPORT BRACKET CRACKED ON FORWARD SIDE<[01] REMOVED AND REPLACED LEFT MAIN WHEEL WELL UPPER T/E PANEL SUPPORT BRACKET IAW SRM 51-10-02 AND SRM 51-40-02.
- [SDR SWAA2023082882998](https://openairdocs.org/sdr/SWAA2023082882998.md): Panel · cracked · Jul 27, 2023 · N224WN · Boeing 7377H4
  > R/H WING I/B FLAP TRACK ACCESS PANEL # 194CR HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED DAMAGE TO PANEL 194CR PER SRM 51-70-04-2R-9 PARA 4.E; SRM 51-70-04-2R-9 PRIMED AND TOP COAT PER AMM 51-21-72-370-51-21-73-370-803804. REPAIR COMPLETE.;[02] VERIFIED C
- [SDR SWAA2023082883227](https://openairdocs.org/sdr/SWAA2023082883227.md): Panel · cracked · Jul 27, 2023 · N224WN · Boeing 7377H4
  > L/H WING I/B FLAP TRACK ACCESS PANEL # 194CL HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED DAMAGE TO PANEL 194CL PER SRM 51-70-04-2R-9 PARA 4.E; SRM 51-70-04-2R-9 PRIMED AND TOP COAT PER AMM 51-21-72-370-51-21-73-370-803804. REPAIR COMPLETE.;[02] VERIFIED C
- [SDR SWAA2023072882753](https://openairdocs.org/sdr/SWAA2023072882753.md): Rod · broken · Jul 27, 2023 · N7885A · Boeing 73776N
  > L/H WING TRAILING EDGE; AFT OF PYLON; SHELF SUPPORT ROD BROKEN.<[01] REMOVED AND REPLACED ROD ASSY PER SOPM 20-50-01. CLEARANCE CHECK GOOD
- [SDR CALA2023072602339](https://openairdocs.org/sdr/CALA2023072602339.md): Screw · missing · Jul 23, 2023 · N37419 · Boeing 737924ER
  > PDA 3 CANOE 3 IS MISSING A SCREW. INSTALLED SCREW ON #3 CANOE. INSTALLED MISSING SCREW IN #3 CANOE. OK TO CONTINUE.
- [SDR FDEA202307201261](https://openairdocs.org/sdr/FDEA202307201261.md): Flap · damaged · Jul 20, 2023 · N279FE · Boeing 767300
  > RIGHT WING INBOARD TRAILING AFT FLAP, LOWER SURFACE WITH NICK AT 19.75" FROM INBOARD EDGE AND 9.5" FROM LOWER EDGE RH WING AFT FLAP INBOARD TRAILING EDGE FLAP, WEDGE LOWER SURFACE AT POSITION IFS 122.4-124.9, SKIN WAS REPAIRED IAW SRM B767 57-53-01-2R REP
- [SDR ABXA20230815172](https://openairdocs.org/sdr/ABXA20230815172.md): Skin · gouged · Jul 19, 2023 · N750AX · Boeing 767232
  > DURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A GOUGE DAMAGE ON THE LH WING INBOARD, AFT FLAP, LEADING EDGE PANEL SKIN AT THE INBOARD SIDE APPROXIMATELY AT IFS 104. AFFECTED AREA WERE BLENDED PER WITH MINIMUM REMAINING MATERIAL OF 0.082 I
- [SDR SWAA2023080779205](https://openairdocs.org/sdr/SWAA2023080779205.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4
  > R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.
- [SDR SWAA2023080779206](https://openairdocs.org/sdr/SWAA2023080779206.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4
  > R/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.<

Next page: https://openairdocs.org/jasc/5750/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 jasc_code = '5750'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5750/reports

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