1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0 G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49, DWG 65B0578 - [SDR UIEA2026092100894](https://openairdocs.org/sdr/UIEA2026092100894.md): Stiffener · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF > CRACK - FOUND R/H OUTBD ELEVATOR STIFFENER CRACK AT ELEV STA 260.98.(
1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV - [SDR UIEA2026092100895](https://openairdocs.org/sdr/UIEA2026092100895.md): Web · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF > FOUND R/H OUTBD ELEVATOR WEB CRACKED AT ELEV STA 281.8.(
1. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 2. JOB COMPLETED & CONDITION CHK OK.
) - [SDR UIEA2026092100896](https://openairdocs.org/sdr/UIEA2026092100896.md): Support · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF > RT OTBD ELEVATOR SUPPORT CRACK AT ELEV STA 285. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHEE - [SDR UIEA2026092100897](https://openairdocs.org/sdr/UIEA2026092100897.md): Support · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF > FOUND RT OUTBD ELEVATOR SUPPORT CRACK AT ELEV STA 277. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHE - [SDR SWAA2026092146823](https://openairdocs.org/sdr/SWAA2026092146823.md): Fastener · missing · Sep 16, 2026 · N8670A · Boeing 7378H4 > LEFT ELEVATOR OTBD BALANCE WEIGHT INNER MOST TRIM WEIGHT MISSING INBD ATTACH HARDWARE. INSTALLED FASTENER IAW SRM 51-61-04, AND SRM 51-40-02-0G-0-B00387. - [SDR UIEA2026091100873](https://openairdocs.org/sdr/UIEA2026091100873.md): Stiffener · corroded · Sep 11, 2026 · N438GT · Boeing 747409F > CORRODED STRUCTURE, LT HORIZONTAL STAB INTERNAL ELEV STA 256.82 AREA. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 107. FABRICATED NEW PARTS IAW EI T2026A55M-1790, REV 1, & WS 60655. INSTALLED FABRICATED PARTS IAW SRM 51-40-02-0G-0, REV 107, & DWG 65B0 - [SDR IPXA2026090848406](https://openairdocs.org/sdr/IPXA2026090848406.md): Static Wick · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF > RIGHT ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. 83-023. ATA 23-60. QCI: VERIFIED STEP 1 AND 2 - [SDR IPXA2026090848482](https://openairdocs.org/sdr/IPXA2026090848482.md): Static Wick · corroded · Sep 2, 2026 · N463UP · Boeing 75724APF > RH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. VERIFIED STEP 5 C/W - [SDR IPXA2026100836983](https://openairdocs.org/sdr/IPXA2026100836983.md): Frame · damaged · Sep 1, 2026 · N463UP · Boeing 75724APF > LH ELEVATOR UPPER, O/B CONDUCTIVE FRAME HAS BULGING ACROSS FASTENERS. - [SDR SWIA2026082477331](https://openairdocs.org/sdr/SWIA2026082477331.md): Landing · dented · Aug 24, 2026 · N936SW · Cndair CL6002B19 > LEFT ELEVATOR, LEADING EDGE NUTPLATE LANDING, UNDER PANEL 334AB IS DENTED. REPAIRED DAMAGE TO THE LT ELEVATOR FRONT SPAR LOWER FLANGE IAW REO 601R-51-00-309 REV B. - [SDR IPXA2026080892392](https://openairdocs.org/sdr/IPXA2026080892392.md): Splice Plate · corroded · Aug 3, 2026 · N438UP · Boeing 75724APF > UPON REMOVAL OF RT ELEVATOR TIP TRAILING EDGE WEDGE FOUND CORROSION ON UPPER SPLICE PLATE AND UPPER CONDUCTIVE FRAME. INSTALLED ONE UPPER SPLICE PLATE AT RT ELEVATOR IAW SRM 51-40-02-0G-0, & DWG 183N2901. - [SDR UIEA2026061700519](https://openairdocs.org/sdr/UIEA2026061700519.md): Panel · misrepaired · Jun 27, 2026 · N868GT · Boeing 7478F > LEFT & RIGHT OTBD ELEV UPPER INTERCOSTAL PANEL ELEV STA 256.8-306.8 FASTENER INSTALLATIONS DEVIATIONS(SB 747-55-2069 LH & RH O/B ELEV UPPER INTERCOSTAL PANEL ELEV STA 256.8-306.8 FASTENER INSTALLATIONS DEVIATIONS REPAIRED I.A.W RI-55-20-18324 REV.A. NO FURT - [SDR IPXA2026071104567](https://openairdocs.org/sdr/IPXA2026071104567.md): Retainer · corroded · Jun 17, 2026 · N418UP · Boeing 75724APF > LEFT ELEVATOR T/E COUNT FROM OTBD TO INBD NR 2 STATIC WICK BASE HAS CORROSION. REMOVED AND REPLACED NR 2 STATIC WICK BASE ( MOUNTING STATIC DISCHARGER) P/N 16335, BATCH 0004414980 AND WICK DISCHARGER P/N 10-900-25A, BATCH 0004493176 ON SUPPORT PLATE IAW AMM - [SDR IPXA2026063088739](https://openairdocs.org/sdr/IPXA2026063088739.md): Bonding Strap · corroded · Jun 16, 2026 · N429UP · Boeing 75724APF > RIGHT HORIZONAL STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. RL025 VERIFIED ITEMS IN STEP 7 ARE INSTALLED PER DOCUMENTS. - [SDR HNAA2026061700543](https://openairdocs.org/sdr/HNAA2026061700543.md): Doubler · cracked · May 17, 2026 · N657AE · Emb EMB145LR > 00543 RH ELEVATOR UPPER CENTER HINGE DOUBLER IS CRACKED. REMOVED AND REPLACED RH ELEVATOR UPPER CENTER HINGE DOUBLER IAW EMB 145 SRM 55-20-01 REPAIR TYPE A, SECTION A - A, FIG. 229 SEE PIEDMONT MAJOR EO1-55-26-0240 - [SDR SWAA2026061805224](https://openairdocs.org/sdr/SWAA2026061805224.md): Balance Weight · out of tolerance · May 14, 2026 · N500WR · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A) ON BAY 3;P/N: 183A0210-15 ON BAY 4. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766 SEE TASK TTG - [SDR SWAA2026061805225](https://openairdocs.org/sdr/SWAA2026061805225.md): Balance Weight · out of tolerance · May 14, 2026 · N500WR · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A) ON BAY 3;P/N: 183A0210-15 ON BAY 4 FAULT RESOLVED ON OTHER FAULT TTG8Q01CCTK7. - [SDR IPXA2026051623776](https://openairdocs.org/sdr/IPXA2026051623776.md): Stiffener · cracked · May 11, 2026 · N621UP · Boeing 7478F > CRACKED STIFFENER DURING PERFORM EO-94633-REQ1 FOUND LT INBD ELEVATOR STIFFENER CRACK INSTALL NEW STIFFENER IAW SRM 51-40-02-0G REV.48 AND BOEING DWG 65B05701, SH 2, REV J. - [SDR IPXA2026060178921](https://openairdocs.org/sdr/IPXA2026060178921.md): Angle · corroded · May 8, 2026 · N412UP · Boeing 75724APF > L/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STRAP) AT L/H HORZ STAB TO ELEVATOR OTBD IAW SRM 51-40-02-0G-0. - [SDR IPXA2026052178794](https://openairdocs.org/sdr/IPXA2026052178794.md): Frame · debonded · May 8, 2026 · N412UP · Boeing 75724APF > RIGHT ELEVATOR OTBD END UPPER CONDUCTIVE FRAME DISBONDED AT AREA UNDER CORRODED STATIC WICK BASE. - [SDR IPXA2026051147230](https://openairdocs.org/sdr/IPXA2026051147230.md): Angle · corroded · Apr 11, 2026 · N428UP · Boeing 75724APF > L/H HORZ STAB TIP REAR SPAR AND ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS INCLUDING BONDING STRAPS HAVE CORROSION. RL003 INSTALLED 1 EA NEW ANGLE 1 EA NEW JUMPER (BONDING STRAP) AND 1EA INTERCOSTAL FROM LH HORZ STAB TIP REAR SPAR AND ELEVATOR FROM SPA - [SDR DALA2026030301469](https://openairdocs.org/sdr/DALA2026030301469.md): Bearing · failed · Mar 2, 2026 · N309DN · Airbus A321213 > SHIP 3009 - ATB - DUE TO TAIL VIBRATIONS DURING CLIMB AT FL200. VIBRATIONS CEASED AFTER LEVEL OFF. CORRECTIVE ACTION: FOUND LEFT OUTBOARD ELEVATOR HINGE ARM BEARING BAD. REPLACED ELEVATOR HINGE LINE BEARINGS. (LP 7963944) - [SDR SWAA2026011259282](https://openairdocs.org/sdr/SWAA2026011259282.md): Seal · cracked · Jan 8, 2026 · N960WN · Boeing 7377H4 > RH ELEVATOR UPPER SLIDER SEAL CRACKED. R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR AALA202601069133](https://openairdocs.org/sdr/AALA202601069133.md): Clamp · corroded · Jan 6, 2026 · N335PH · Boeing 737823 > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO RIGHT HAND ELEVATOR FRONT SPAR SUPPORT CLIP AT ELEVATOR STA 121.59 AND STABILIZER BL 83.05. REPLACED SUPPORT CLIP PER SRM 51-40-02 - [SDR AALA202601062948](https://openairdocs.org/sdr/AALA202601062948.md): Clamp · corroded · Jan 6, 2026 · N335PH · Boeing 737823 > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO RIGHT HAND ELEVATOR FRONT SPAR SUPPORT CLIP AT ELEVATOR STA 66.54 AND STABILIZER BL 83.05. REPLACED SUPPORT CLIP PER SRM 51-40-02. - [SDR AALA202601061227](https://openairdocs.org/sdr/AALA202601061227.md): Clamp · corroded · Jan 6, 2026 · N335PH · Boeing 737823 > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO RIGHT HAND ELEVATOR FRONT SPAR SUPPORT CLIP AT ELEVATOR STA 176.64 AND STABILIZER BL 83.05. REPLACED SUPPORT CLIP PER SRM 51-40-02. - [SDR CALA2025120211698](https://openairdocs.org/sdr/CALA2025120211698.md): Fitting · broken · Nov 28, 2025 · N826UA · Airbus A319131 > UPON INSTALLATION OF LT ELEVATOR OTBD ELEVATOR SERVO. FOUND BROKEN TAB ON ELEVATOR SIDE. TECHNICIAN WAS CLEANING FLUID IN AREA WHEN THE TAB BROKE OFF & FELL INTO THE LIFT. UPON CLOSER INSPECTION GLUE WAS FOUND ON TAB. TAB IS PART OF THE FITTING TO HOLD COTTE - [SDR SWAA2025112032981](https://openairdocs.org/sdr/SWAA2025112032981.md): Balance Arm · out of tolerance · Oct 27, 2025 · N8623F · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652468. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767. - [SDR SWAA2025112032980](https://openairdocs.org/sdr/SWAA2025112032980.md): Balance Arm · out of tolerance · Oct 27, 2025 · N8623F · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF LT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652467. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766. - [SDR SWAA2025102019405](https://openairdocs.org/sdr/SWAA2025102019405.md): Balance Arm · out of balance · Sep 16, 2025 · N8619F · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHTS ON BAY 2, ON BAY 3. ACCOMPLISHED ON MULTI EA M-22-155-03766. - [SDR SWAA2025091098729](https://openairdocs.org/sdr/SWAA2025091098729.md): Elevator · out of balance · Aug 5, 2025 · N8617E · Boeing 7378H4 > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A) ON BAY 3;P/N: 183A0210-15 ON BAY 4 2025-479466<[01] TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-037 - [SDR JR2R20250720722](https://openairdocs.org/sdr/JR2R20250720722.md): Hinge · gouged · Jul 20, 2025 · N87306 · Emb ERJ170200LL > RIGHT HAND ELEVATOR, #2 HINGE HAS GOUGES NEAR BOLT HOLE. REPAIRED. - [SDR JR2R20250720721](https://openairdocs.org/sdr/JR2R20250720721.md): Hinge · gouged · Jul 20, 2025 · N87306 · Emb ERJ170200LL > RIGHT HAND ELEVATOR, #2 HINGE HAS A DEEP GOUGE NEAR TOGGLE LINK BOLT HOLE. REPAIRED. - [SDR AALA202507243654](https://openairdocs.org/sdr/AALA202507243654.md): Attach Fitting · corroded · Jul 12, 2025 · N855NN · Boeing 737823 > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR TAB CONTROL MECHANISM SPRING ATTACH POINTS LOWER HARDWAR EHAVE EVIDENCE OF CORROSION. REMOVED AND REPLACED AFT RIGHT HAND ELEVATOR TAB CONTROL MECHANISM RETURN SPRINGS LOWER ATTACHING POINT BUSHING, PERFORMED S - [SDR AALA202507247140](https://openairdocs.org/sdr/AALA202507247140.md): Attach Fitting · corroded · Jul 12, 2025 · N855NN · Boeing 737823 > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR TAB CONTROL MECHNISM RETURN SPRINGS LOWER ATTACHING POINTS HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED AFT LEFT HAND ELEVATOR TAB CONTROL MECHANISM RETURN SPRINGS LOWER ATTACHING POINT BUSHING, PERFORMED SAT - [SDR KCSA202507081109](https://openairdocs.org/sdr/KCSA202507081109.md): Frame · gouged · Jul 8, 2025 · N713CK · Boeing 7474B5F > R/H ELEVATOR STA 231 HAS GOUGE ON THE COUNTER BALANCE FRAME - [SDR IPXA2025070366217](https://openairdocs.org/sdr/IPXA2025070366217.md): Support · cracked · Jun 23, 2025 · N607UP · Boeing 7478F > CRACK, SUPPORT OF OUTBD ELEVATOR L/E AREA NEAR ELEN STA 265 (REPLACE). FABRICATE P/N(183U3424-3) PER BOEING DWG 183U3424 SH2 REV. A; 183U3424-3 PL REV."A"AND ORIGINAL PART AS A SAMPLE IAW GMM-MTX CH 9.08 REV.12 REQUIREMENT AND EGAT WORK SHEET NO.50465. INSTAL - [SDR JJBA20250613002](https://openairdocs.org/sdr/JJBA20250613002.md): Support · corroded · May 19, 2025 · N11164 · Emb EMB145XR > FOUND LEVEL 2, MODERATE CORROSION ON LH ELEVATOR RVDT SUPPORT ASSEMBLY STRUCTURAL MOUNT. FOUND LIGHT SURFACE CORROSION AND CLEANED. INSTALLED LH ELEVATOR RVDT SUPPORT. OPS CHECK SAT. NO DEFECTS NOTED AT THIS TIME. - [SDR 9WGA2025091854653](https://openairdocs.org/sdr/9WGA2025091854653.md): Bolt · corroded · May 8, 2025 · N546JN · Doug MD11F > DURING HEAVY MAINTENANCE CORROSION FOUND ON LH OB ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198. - [SDR IPXA2025052172440](https://openairdocs.org/sdr/IPXA2025052172440.md): Support · cracked · May 8, 2025 · N605UP · Boeing 7478F > **SDR FILED OPEN**FAULT - FOUND LH OB ELEVATOR IB FWD STIFFER CRACK. (REPLACE) PAPER FINAL CHECK COMPLETED - [SDR JGVR20250429001](https://openairdocs.org/sdr/JGVR20250429001.md): Attach Bolt · corroded · Apr 29, 2025 · N305QS · Cessna 680CE > MECHANICALLY REMOVED AREAS OF CORROSION LOCATED ON LH ELEVATOR CABLE PULLEY ATTACHMENT BRACKET LOCATED INSIDE BELLY PANEL BAY 154AC AND EXTENDING FORWARD SEVERAL INCHES ONTO FUSELAGE STIFFENER AND DRAIN ATTACHMENT RIVETS PERFORMED NDT AND REPORTED FOR REPAIR D - [SDR DALA2025042803296](https://openairdocs.org/sdr/DALA2025042803296.md): Bearing · migrated · Apr 25, 2025 · N385DZ · Airbus A321211 > SHIP 3085 MIGRATED BEARING HINGE 4 ON RH ELEVATOR. CORRECTIVE ACTION: REPLACED HINGE FITTING #4 ON RH ELEVATOR AS PER A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. (0932798) - [SDR SWAA2025050554065](https://openairdocs.org/sdr/SWAA2025050554065.md): Elevator · out of limits · Apr 13, 2025 · N290WN · Boeing 7377H4 > DURING BALANCE PROCEDURE WAS FOUND CBM OF RT ELEVATOR -73.94 LBFIN IS OUT OF LIMIT IAW B737-700 SRM 51-61-04-0G-0 2025-232426<[01] PERFORMED SECONDARY STATIC BALANCE JIG CHECK AT RT ELEVATOR IAW B737-700 SRM 51-61-04-0G-0; STEPS 5.A (3)(B)1); 5.A (4);5.A (5)(A - [SDR IPXA2024102974638](https://openairdocs.org/sdr/IPXA2024102974638.md): Angle · corroded · Oct 17, 2024 · N446UP · Boeing 75724APF > UPON OK TO INSTALL FOUND LH ELEVATOR O/B BONDING JUMPER ATTACHMENT POINT TO HAVE EXFOLIATED CORROSION ON HORIZONTAL STAB. DOT 142-501. INSTALLED NEW L/H ELEVATOR O/B BONDING JUMPER ATTACHMENT POINT (ANGLE) AND JUMPER STRAP I.A.W. SRM 51-40-02-0G. MATERIAL: P/N - [SDR HNAA2024111101083](https://openairdocs.org/sdr/HNAA2024111101083.md): Hinge · corroded · Oct 11, 2024 · N697AB · Emb EMB145LR > F001692 LH ELEVATOR IB HINGE, IB RIB CORRODED. RAR RIB IAW SRM 51-40-02 - [SDR CALA2024101100813](https://openairdocs.org/sdr/CALA2024101100813.md): Seal · missing · Oct 11, 2024 · N15710 · Boeing 737724 > PDA 2 LEFT ELEVATOR OUTBD LOWER HINGE SEAL MISSING PICS SDR UPDATE REPLACED LT ELEVATOR OUTBD BOTTOM SEAL REF MM 27-31-11-400-801 Next page: https://openairdocs.org/jasc/5524/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 = '5524' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/jasc/5524/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.