# Service difficulty reports: JASC 5553

A list on [JASC 5553](https://openairdocs.org/jasc/5553.md).

Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, newest first.

Page 1 of 12 · 586 reports

- [SDR VNAA20250715043](https://openairdocs.org/sdr/VNAA20250715043.md): Drag Angle · cracked · Jun 3, 2025 · N599NN · Bombdr CL6002D15
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DA
- [SDR DALA2024092309309](https://openairdocs.org/sdr/DALA2024092309309.md): Flap Track · corroded · Sep 21, 2024 · N348NB · Airbus A319114
  > SHIP 3148 RH WING INB'D FLAP TRACK #2 / ATTCHT BEARING AT RIB 9 CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 620272-14. (0568620)
- [SDR SWAA2024031554034](https://openairdocs.org/sdr/SWAA2024031554034.md): Fitting · corroded · Feb 20, 2024 · N922WN · Boeing 7377H4
  > CORROSION ON FWD AND AFT FACE OF FITTING FDW VERTICAL BST 1016 RBBL 11.55 2024-124241, PERFORMED REPAIR LOCATED FWD AND AFT FACE OF FITTING FDW VERTICAL BST 1016 RBBL 11.55 IAW B737-700 EA 24-153-00515. CORRECTED STEP 4. PERFORMED REPAIR LOCATED FWD AND AF
- [SDR VNAA202403010005](https://openairdocs.org/sdr/VNAA202403010005.md): Drag Angle · cracked · Jan 20, 2024 · N615NN · Bombdr CL6002D15
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00
- [SDR VNAA202403010004](https://openairdocs.org/sdr/VNAA202403010004.md): Drag Angle · cracked · Jan 20, 2024 · N615NN · Bombdr CL6002D15
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER SRM 55-31-00-201-001
- [SDR SWI2024F00056](https://openairdocs.org/sdr/SWI2024F00056.md): Drag Angle · cracked · Oct 28, 2023 · N746SK · Cndair CL6002C10
  > *SUSPECTED CRACK AT R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE (MARKED), (C-CHECK RO 1/30/2024) REPAIRED R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE REF CRJ-700-SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY AND SEE CONTINUATION CARD FOR DETAILS
- [SDR SWI2024F00055](https://openairdocs.org/sdr/SWI2024F00055.md): Drag Angle · cracked · Oct 28, 2023 · N746SK · Cndair CL6002C10
  > *AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED NEW AFT VERTICAL S
- [SDR SWIA202401301028](https://openairdocs.org/sdr/SWIA202401301028.md): Drag Angle · cracked · Oct 28, 2023 · N746SK · Cndair CL6002C10
  > *FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE AND INSTALLED NEWLY FABRICATED FWD DRAG ANGLE, FILLER, AND DOUBLER ON LH SIDE REF CRJ700 SRM 55-31
- [SDR SWI2023F00473](https://openairdocs.org/sdr/SWI2023F00473.md): Unknown · cracked · Sep 5, 2023 · N713EV · Cndair CL6002C10
  > VERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH AFT DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH AFT DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH
- [SDR SWIA202311070905](https://openairdocs.org/sdr/SWIA202311070905.md): Unknown · cracked · Sep 5, 2023 · N713EV · Cndair CL6002C10
  > VERTICAL STABILIZER TO FUSELAGE ATTACHMENT LH FORWARD DRAG ANGLE DOUBLER POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW LH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF CRJ700 SRM 55-31-00-201-001-A01 AND ALL STEP
- [SDR AALA202308154399](https://openairdocs.org/sdr/AALA202308154399.md): Fitting · corroded · Aug 10, 2023 · N909AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER RIGHT HAND FAILSAFE FITTING LOCATED AT BS 1088, S2R. REPLACED FITTING PER SRM 51-40-02.
- [SDR AALA202308157476](https://openairdocs.org/sdr/AALA202308157476.md): Fitting · corroded · Aug 10, 2023 · N909AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER RIGHT HAND AFT FAILSAFE FITTING LOCATED AT BS 1088, S2R. REPLACED FITTING PER SRM 51-40-02.
- [SDR FDEA202210062486](https://openairdocs.org/sdr/FDEA202210062486.md): Fitting · damaged · Oct 6, 2022 · N614FE · Doug MD11F
  > TO CARRY OUT BANJO FORWARD AND AFT FITTING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION AT STATION 2164. REPAIR CARRIED OUT ALONG STATION 2164 RIGHT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA IAW EA 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR I
- [SDR FDEA202210062485](https://openairdocs.org/sdr/FDEA202210062485.md): Fitting · cracked · Oct 6, 2022 · N614FE · Doug MD11F
  > WHILE ACCOMPLISHING LEFT HAND BANJO FORWARD FITTING INSPECTION, FOUND LEFT HAND BANJO AFT FITTING SUSPECTED CRACK AT STATION 2164. LEFT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA REPAIR CARRIED OUT PER E.A #: 1-5530-T0313159 B P4. REPAIR CLASSIFIED A
- [SDR DALA2022041102515](https://openairdocs.org/sdr/DALA2022041102515.md): None · none · Apr 8, 2022 · N301NB · Airbus A319114
  > SHIP 3101 - CRACK SUPPORT VERTICAL WEB LOCATED BETWEEN HINGE 5 TO HINGE 6 ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIR VERTICAL WEB LOCATED BETWEEN HINGE 5 TO HINGE 6 AS PER ER/A 598239-14.(2188943)
- [SDR HNAA2022052500187](https://openairdocs.org/sdr/HNAA2022052500187.md): None · none · Apr 7, 2022 · N625AE · Emb EMB145LR
  > E912345 - VERTICAL STAB TO FUSELAGE LH DRAG ANGLE IS CRACKED AT FWD END.... RAR LH VERTICAL STAB TO FUSELAGE DRAG ANGLE FWD SECTION IAW EMB 145 SRM 51-40-02
- [SDR DALA2022012400475](https://openairdocs.org/sdr/DALA2022012400475.md): None · none · Jan 22, 2022 · N367NW · Airbus A320212
  > SHIP 3267 VERTICAL STABILIZER HINGE FITTING #4 CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING #4 AND FASTENERS PER A320 SRM 55-36-42. (2095237)
- [SDR DALA2022012400474](https://openairdocs.org/sdr/DALA2022012400474.md): None · none · Jan 22, 2022 · N367NW · Airbus A320212
  > SHIP 3267 VERTICAL STABILIZER HINGE FITTING #2 CORRODED. CORRECTIVE ACTION: REPLACED HINGE #2 AND FASTENERS PER A320 SRM 55-36-42. (2095233)
- [SDR DALA2022012400473](https://openairdocs.org/sdr/DALA2022012400473.md): None · none · Jan 22, 2022 · N367NW · Airbus A320212
  > SHIP 3267 VERTICAL STABILIZER HINGE FITTING #7 CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING PER SRM A320 55-36-42. (2095222)
- [SDR DALA2022012400472](https://openairdocs.org/sdr/DALA2022012400472.md): None · none · Jan 22, 2022 · N367NW · Airbus A320212
  > SHIP 3267 VERTICAL STABILIZER HINGE FITTING #5 CORRODED. CORRECTIVE ACTION: REPLACED FITTING PER A320 SRM 55-36-42. (2095217)
- [SDR DALA2022012400471](https://openairdocs.org/sdr/DALA2022012400471.md): None · none · Jan 22, 2022 · N367NW · Airbus A320212
  > SHIP 3267 VERTICAL STABILIZER HINGE FITTING #3 CORRODED. CORRECTIVE ACTION: REPLACED FITTING PER A320 SRM 55-36-42. (2095211)
- [SDR DALA2022012400476](https://openairdocs.org/sdr/DALA2022012400476.md): None · none · Jan 21, 2022 · N367NW · Airbus A320212
  > SHIP 3267 HINGE FITTING NUMBER 1 VERTICAL STABILIZER CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING PER A320 SRM 55-36-42. (2094068)
- [SDR SWAA2022010658653](https://openairdocs.org/sdr/SWAA2022010658653.md): Fitting · corroded · Jan 5, 2022 · N7866A · Boeing 7377Q8
  > CORROSION FITTING ON DRAG BRACE OUTBOARD FWD LOCATED AFT REAR SPAR RT SIDE AT VERTICAL STABILIZER. REPLACED THE FITTING AND FASTENERS ON DRAG BRACE IAW SRM 51-40-02 & DWG 148A8200 REV A.
- [SDR SWIA202164581](https://openairdocs.org/sdr/SWIA202164581.md): None · cracked · Dec 5, 2021 · N713SK · Cndair CL600*
  > * VERTICAL STABILIZER R/H DRAG ANGLE CRACKED AT APPROX. VERTICAL STABILIZER REAR SPAR DATUM 67.5%. (C-CHECK RO 2/22/2022) CUT AWAY CRACKED FWD AND AFT VERTICAL STAB DRAG ANGLES AND INSTALLED REPAIR DOUBLERS AND FILLERS ON R/H SIDE OF VERTICAL STAB. REF:
- [SDR SWIA202164580](https://openairdocs.org/sdr/SWIA202164580.md): None · cracked · Dec 5, 2021 · N713SK · Cndair CL600*
  > * VERTICAL STABILIZER L/H DRAG ANGLE CRACKED AT APPROX. VERTICAL STABILIZER REAR SPAR DATUM 67.5%. (C-CHECK RO 2/22/2022) CUT AWAY CRACKED FWD AND AFT VERTICAL STAB DRAG ANGLES AND INSTALLED REPAIR DOUBLERS AND FILLERS ON L/H SIDE OF VERTICAL STAB. REF:
- [SDR MASA20211101488](https://openairdocs.org/sdr/MASA20211101488.md): Visor · damaged · Oct 14, 2021 · N326MS · Cndair CL6002D24
  > RH LOWER VISOR OF THE VERTICAL TO HORIZONTAL STABILIZER WAS FOUND WITH MULTIPLE ELONGATED HOLES AFFECTING THE INNER PANEL AND BLOCK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 55-32-86-001-001-A02, FIGURE 55-32-86-991-808, ITEM 136, 128, AND 153, EA 48-202
- [SDR DATA20210921001](https://openairdocs.org/sdr/DATA20210921001.md): Fitting · corroded · Sep 17, 2021 · N601CA · Stbros SD360
  > WHILE PERFORMING AN INSPECTION OF THE VERTICAL STABILIZER ATTACH FITTING PER AD 2005-13-31 AND SERVICE BULLETIN SD360-53-45, FOUND CORROSION ON SHEAR ATTACHMENT FITTING P/N SD3-12-6978. FITTING WAS REMOVED AND REPLACED WITH NEW FITTING IAW SB SD360-53-45 AND A
- [SDR SWAA2021091607868](https://openairdocs.org/sdr/SWAA2021091607868.md): Fitting · corroded · Aug 16, 2021 · N413WN · Boeing 7377H4
  > LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER(FTG-LH FWD MAIN)HAS PITTING CORROSION.; / [01] REMOVED LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER - LH FWD MAIN IN IAW SRM 51-40-02-0G-0; [02] VERIFIED 1. OK TO LOCATE AND DRILL NEW FITTING.; [03] PARTIALLY
- [SDR SWAA2021092107654](https://openairdocs.org/sdr/SWAA2021092107654.md): Angle · chafed · Aug 15, 2021 · N570WN · Boeing 7377CT
  > VERTICAL STAB. FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLES HAVE CHAFED; WEAR MARKS; / [01] ORIGINAL MAT THICKNESS 0.063' MINIMUM MAT FOUND 0.032' NO ALLOWABLE MAT LIMITS FOUND; [02] REMOVED 98% OF L/H SKATE ANGLE AS PER B737-700 SRM 51-40-02-0G-0; [03] REM
- [SDR SWIA202161736](https://openairdocs.org/sdr/SWIA202161736.md): None · excess play · Aug 13, 2021 · N946SW · Cndair CL6002B19
  > BOTH CENTER HINGE POINTS AND UPPER HINGE POINT BEARINGS ON THE RUDDER VERTICAL STAB TRAILING EDGE SIDE HAVE EXCESSIVE PLAY, ALL FLAGGED (C-CHECK RO 10/8/2021) REMOVED AND REPLACED WORN BEARINGS ON UPPER AND CENTER HINGE FITTINGS ON RUDDER R VERTICAL STA
- [SDR SWIA2021091060831](https://openairdocs.org/sdr/SWIA2021091060831.md): Drag Angle · elongated · Aug 2, 2021 · N705SK · Cndair CL6002C10
  > VERTICAL STAB RH SIDE HAS (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE. (C-CHECK RO 9/8/2021) VERTICAL STAB RH SIDE (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE REPAIRED PER MHIRJ REO 670-55-31-146 REV €“ DATE 2021-08-05. COMPL
- [SDR SWIA2021091060877](https://openairdocs.org/sdr/SWIA2021091060877.md): Drag Angle · cracked · Jul 6, 2021 · N705SK · Cndair CL6002C10
  > *VERTICAL STAB HAS A CRACKED DRAG ANGLE ON RH SIDE (MARKED) (C-CHECK RO 9/8/21) REPLACED CRACKED VERTICAL STAB DRAG ANGLE WITH NEW, REF BOMBARDIER DWG BA670-35002 REV -F, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM
- [SDR SWIA2021091060876](https://openairdocs.org/sdr/SWIA2021091060876.md): Drag Angle · cracked · Jul 6, 2021 · N705SK · Cndair CL6002C10
  > *VERTICAL STAB HAS A CRACKED DRAG ANGLE ON LH SIDE (MARKED) (C-CHECK RO 9/8/21) REMOVED CRACKED VERTICAL STAB LH SIDE DRAG ANGLE AND REPLACED WITH A SERVICEABLE UNIT (P/N: A670-21186-003) REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-13-001-001
- [SDR SWAA2021080287364](https://openairdocs.org/sdr/SWAA2021080287364.md): Attach Angle · cracked · Jun 23, 2021 · N419WN · Boeing 7377H4
  > CRACK LEADING EDGE SUPPORT ANGLE AT LEVEL BS 1016 AT VERTICAL STABILIZER; 2021-295416 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOC. AT LEVEL BS 1016 AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02; ITEM 9 AND DWG 176A3001; SHEET 20; REV -; [02] REPLACED
- [SDR SWIA2021081060201](https://openairdocs.org/sdr/SWIA2021081060201.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10
  > *RH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPLACED R/H AFT DRAG ANGLE AT THE VERTICAL/FUSELAGE ATTACHMENT AREA REF. CRJ 700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01 DWG BA670-35002 REV F / C/W
- [SDR SWIA2021081060200](https://openairdocs.org/sdr/SWIA2021081060200.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10
  > *RH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPAIRED THE R/H VERTICAL/FUSELAGE FWD DRAG ANGLE, CUT AWAY DAMAGE, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. CRJ 700 SRM 55-31-00-201-001-A01 AND CRJ 700 SRM 51-42-21-001-
- [SDR SWIA2021081060199](https://openairdocs.org/sdr/SWIA2021081060199.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10
  > *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG
- [SDR SIMA20210526005](https://openairdocs.org/sdr/SIMA20210526005.md): Drag Angle · cracked · May 26, 2021 · N663AR · Emb EMB145LR
  > VERTICAL STAB TO FUSELAGE RT SIDE DRAG ANGLE IS CRACKED IN 2 AREAS. (MAJOR REPAIR)-C/A-C/W VERTICAL STAB TO FISELAGE DRAG ANGLE REPAIR IAW ERS-EM-53MR-4355
- [SDR SWAA2021061772822](https://openairdocs.org/sdr/SWAA2021061772822.md): Angle · chafed · May 13, 2021 · N416WN · Boeing 7377H4
  > RT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED AREAS.; DOT 8-29 / CERTIFIED REMOVED AND REPLACED CLOSURE ANGLE AT RT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE; FINAL INSPECTED.;INSPECTED AND CERTIFIED (STEPS #8; #9 AND #
- [SDR SWAA2021061772821](https://openairdocs.org/sdr/SWAA2021061772821.md): Angle · chafed · May 13, 2021 · N416WN · Boeing 7377H4
  > LT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED AREAS. 8-28; / CERTIFIED (RII) STEPS #8; #9 AND #10 INSPECTED.;CERTIFIED LT CLOSURE ANGLE INSTALLATION AND 100% FASTENERS INSTALLATION BY SQUEEZE OUT TIME; INSPECTED.;FINAL INSPECTI
- [SDR HNAA2021051900206](https://openairdocs.org/sdr/HNAA2021051900206.md): Drag Angle · cracked · Apr 15, 2021 · N644AE · Emb EMB145LR
  > RH FUSELAGE TO VERTICAL STAB DRAG ANGLE IS CRACKED AT FWD FITTING AFT END. REMOVED AND REPLACED FWD RH FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IAW EMB 145 SRM 51-40-02.
- [SDR DALA2021031001365](https://openairdocs.org/sdr/DALA2021031001365.md): Hinge · corroded · Mar 9, 2021 · N353NW · Airbus A320212
  > SHIP 3253 FOUND CORROSION ON BORE OF VERTICAL STABILIZER RUDDER HINGE. CORRECTIVE ACTION: REPLACED HINGE PER A320 SRM 55-36-42. (1750426)
- [SDR REXA2021012200023](https://openairdocs.org/sdr/REXA2021012200023.md): Drag Angle · cracked · Jan 6, 2021 · N308PQ · Cndair CL6002D24
  > VERTICAL STAB LT AFT DRAG ANGLE CRACKED. REMOVED ADN REPLACED LT AFT DRAG ANGLE P AV670-21186-003, IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.
- [SDR SWIA202156262](https://openairdocs.org/sdr/SWIA202156262.md): Drag Angle · cracked · Jan 5, 2021 · N760SK · Cndair CL6002C10
  > RH VERTICAL STAB TO FUSELAGE AFT DRAG ANGEL HAS A POSSIBLE CRACK (C-CHECK) RO 2/13/2021 REMOVED AND REPLACED RH AFT DRAG ANGLE ON VERTICAL STAB TO FUSELAGE REF CRJ 700 SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND BOMBA
- [SDR SWIA202056242](https://openairdocs.org/sdr/SWIA202056242.md): Attach Angle · gouged · Dec 7, 2020 · N876AS · Cndair CL6002B19
  > * THE VERTICAL STABILIZER'S LH AND RH FRONT SPAR TO FUSELAGE SPLICE STRAP RIB ATTACH ANGLES ARE GOUGED ON THEIR OUTBOARD SIDES. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 2/9/2021 REMOVED GOUGED DAMAGE ON VERTICAL STAB FRONT SPAR TO FUSELAGE SPLICE STRAP
- [SDR SCNA20201201373](https://openairdocs.org/sdr/SCNA20201201373.md): Skate Angle · worn · Nov 25, 2020 · N817SY · Boeing 7378K2
  > RT AFT SKATE ANGLE IS WORN. ACCOMPLISHED BLEND REPAIR TO VERTICAL FIN CLOSURE ANGLE RT, BS 1032 TO BS 1104, PER ATS ER 20-03566 REV IR AND SCA EA 53-0068 REV 0.
- [SDR SWIA202055346](https://openairdocs.org/sdr/SWIA202055346.md): Drag Angle · cracked · Nov 20, 2020 · N755SK · Cndair CL6002C10
  > VERTICAL STAB TO FUSELAGE ATTCHMENT AFT DRAG ANGLE ON RT SIDE IS CRACKED. C-CHECK RO 1/6/2021. REMOVED AND REPLACED VERTICAL STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON RT SIDE, IAW CRJ 700 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-00
- [SDR SWIA202055779](https://openairdocs.org/sdr/SWIA202055779.md): Drag Angle · cracked · Nov 16, 2020 · N161PQ · Cndair CL6002D24
  > *LH SIDE OF VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK) RO 2/1/2021 REPARIED LH SIDE OF VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202054268](https://openairdocs.org/sdr/SWIA202054268.md): Doubler · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19
  > VERTICAL STABILIZER MOUNT DOUBLER COMMON TO TAIL STINGER HAS CORRODED HARDWARE, MARKED. C-CHECK RO 11/21/2020. REPLACED WITH NEW BOLTS (2 EACH), NEW WASHERS (2 EACH) AND NEW NUTS (2 EACH) ON THE VERTICAL STAB MOUNT DOUBLER COMMON TO TAIL STINGER, REF CRJ-200
- [SDR SWAA2020101319566](https://openairdocs.org/sdr/SWAA2020101319566.md): Attach Angle · chafed · Sep 30, 2020 · N8644C · Boeing 7378H4
  > UPPER FUSELAGE STA 1018, 1077, 1106 & 1124; RBL 13; FUSELAGE TO VERTICAL STAB SKATE ANGLE INBOARD SIDE CHAFE WEAR, MARKED. REMOVED AND REPLACED RT VERTICAL STAB SKATE ANGLE STA 1018 TO 1124 RBL 13, IAW SRM 51-40-02-0G-0 AND BOEING DWG 148A8300 REV. APPLIED T

Next page: https://openairdocs.org/jasc/5553/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 = '5553'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5553/reports

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