# Service difficulty reports: JASC 2730

A list on [JASC 2730](https://openairdocs.org/jasc/2730.md).

Reports filed under 2730 · Elevator Control System, newest first.

Page 1 of 53 · 2,647 reports

- [SDR AALA202610191184](https://openairdocs.org/sdr/AALA202610191184.md): Elevator · vibration · Oct 13, 2026 · N918US · Airbus A321231
  > AIRCRAFT WAS GROUNDED: ON DESCENT AT 290 AND SLOWING WITH AIRCRAFT CLEAN, EXCESSIVE VIBRATION WHEN SPEED BRAKES WERE GREATER THAN 1/2. COULD NOT USE SPEED BRAKES GREATER THAN 1/2 DUE TO MODERATE VIBRATION - MAINTENANCE HAS ISOLATED THE SOURCE TO THE ELEVATORS.
- [SDR AALA202610088184](https://openairdocs.org/sdr/AALA202610088184.md): Spring · broken · Oct 7, 2026 · N986NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: NO ELEVATOR FEEL ON ROTATION. NO LIGHTS OR OTHER INDICATIONS NOTED. FOUND ELEVATOR FEEL AND CENTERING SPRING BROKEN. REMOVED AND REPLACED SPRING AS PER AMM 27-31-64-400-802. FORCE FEEL TEST PASSED.
- [SDR SCNA20261002415](https://openairdocs.org/sdr/SCNA20261002415.md): Indication Sys · intermittent · Oct 2, 2026 · N847SY · Boeing 737800*
  > FIRST OFFICER SIDE SPEED LIM FLAG INTERMITTENTLY FLASHING IN FLIGHT RED & BLACK STICK SHAKER AND MAX OP BARS REMOVED. PERFORMED FIM 27-32 TASK 833 WITH NO EXISTING FAULTS ON STALL MANAGEMENT YAW DAMPNER 2 FAULT HISTORY SHOWED FLIGHT MANAGEMENT COMPUTER DATA I
- [SDR 2026FA0000806](https://openairdocs.org/sdr/2026FA0000806.md): Torque Tube · sheared · Oct 1, 2026 · N5352R · Cessna 172F
  > UPON COMPLETING A PREFLIGHT INSPECTION, NOTICED SLIGHT DAMAGE TO THE METAL SKIN THAT RUNS OVER THE CONNECTION POINTS BETWEEN THE HORIZONTAL STAB & ELEVATOR. THE DAMAGE IMPLIED AN OVEREXTENSION OF THE ELEVATOR IN SUCH A WAY WHERE THE METAL SKIN IMPACTED THE CON
- [SDR 2026FA0000738](https://openairdocs.org/sdr/2026FA0000738.md): Trim Motor · defective · Sep 17, 2026 · N2141 · Cirrus SR20
  > ELEVATOR PITCH TRIM MOTOR HOUSING ATTACH SCREWS ARE WORKING LOOSE AND CAUSING EXCESSIVE MOVEMENT OF THE ELEVATOR SYSTEM. IF UNCORRECTED, COULD CASE FLUTTER IN THE ELEVATOR SURFACE DURING FLIGHT.
- [SDR ASAA2026091166836](https://openairdocs.org/sdr/ASAA2026091166836.md): Control Servo · unserviceable · Sep 11, 2026 · N223HA · Airbus A321271N
  > ATB- AIRCRAFT FLUTTER- FELT LIKE DRIVING OVER LARGE SPEED BUMPS CLIMBING THRU FL 240, SPEED 340KTS, SET SELECTED SPEED 300 KTS, VIBRATIONS STOPPED 315KTS: NORMAL ENG VIB & FLT CTL. GROUNDED - YES. FOUND ELEVATOR SERVO CONTROL (34CE3) BINDING. REMOVED AND REPLA
- [SDR AALA202609119088](https://openairdocs.org/sdr/AALA202609119088.md): Elevator System · vibration · Sep 6, 2026 · N109UW · Airbus A320214
  > AIRCRAFT WAS GROUNDED: ON INITIAL CLIMB OUT, WHEN PASSING FL260 AND DOING 335 KNOTS, THERE WAS AN EXTREME VIBRATION FELT THROUGHOUT THE ENTIRE AIRCRAFT. ENGINE VIBRATIONS WERE LOW AND NORMAL. FLIGHT CONTROL PAGE SHOWED NO FLIGHT CONTROLS OUT OF NORMAL RANGE. W
- [SDR SWIA2026081976927](https://openairdocs.org/sdr/SWIA2026081976927.md): Elevator · faulted · Aug 19, 2026 · N804SK · Cndair CL6002D24
  > ELEVATOR SPLIT CAUTION MESSAGE CAME ON IN FLIGHT. HAS STAYED ON AFTER ENGINE SHUTDOWN. REF CP 32892245 FOR LT ELEVATOR POSITION TRANSMITTER, R & R IAW CP 32882985 FOR LT FOR NR 2 ELEVATOR PCU REPLACEMENT. REF CP 32882986 FOR LT NR 3 ELEVATOR PCU REPLACEMENT,
- [SDR HNAA2026082000742](https://openairdocs.org/sdr/HNAA2026082000742.md): Sensor · abnormal · Aug 19, 2026 · N657AE · Emb EMB145LR
  > DURING TAKEOFF ROLL SPS 2 WARNING EICAS MESSAGE AND SPS ADVANCED SPC FAIL ON CMC REJECTED TAKEOFF AT 10 KNOTS. F SLAVED IN SPC, NO FIX. REINSTALLED ORIGINAL. REMOVED AND REPLACED #2 AOA SENSOR IAW AMM 27-36-01, OPS CHECK GOOD. OK FOR SERVICE.
- [SDR SWIA2026080576739](https://openairdocs.org/sdr/SWIA2026080576739.md): Transmitter · faulted · Aug 5, 2026 · N532GJ · Cndair CL6002C11
  > ELEVATOR SPLIT CATION MESSAGE IN FLIGHT (FLIGHT 5640) SEE CP32774877 FOR FDR DOWNLOAD SEE CP32780935 FOR TROUBLESHOOTING AND R & R RT ELEVATOR POSITION TRANSMITTER, SEE CP32784391 FOR R & R LT ELEVATOR POSITION TRANSMITTER.
- [SDR DALA2026073104432](https://openairdocs.org/sdr/DALA2026073104432.md): Control System · out of adjust · Jul 29, 2026 · N693DL · Boeing 757232
  > ATB- DUE ELEVATOR FEEL ISSUE AFTER TAKEOFF. ADJUSTED ELEVATOR CONTROL SYSTEM. ADJUSTED ELEVATOR FEEL SENSOR. TEST PASSED.(8816120)(AIRCRAFT GROUNDED)
- [SDR ABXA20260720327](https://openairdocs.org/sdr/ABXA20260720327.md): Indicator · faulted · Jul 20, 2026 · N220CY · Boeing 767383
  > DURING TAXI OUT, RT ELEVATOR DOESN'T INDICATE FULL TRAVEL. ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED FLIGHT CONTROL POSITION INDICATION IAW ABX MEL 27-08-1. FLIGHT CONTROL MOVEMENT VERIFIED. PLACARDS INSTALLED MAINTENANCE PROCEDURES AC
- [SDR J7SA2026072700494](https://openairdocs.org/sdr/J7SA2026072700494.md): Actuator · unserviceable · Jul 18, 2026 · N200FX · Gulstm GVIIG500
  > DURING FLIGHT, CYAN FCS NO DISPATCH CAS POSTED. CREW WAS ABLE TO CLEAR AND LANDED WITHOUT INCIDENT. DOWNLOADS INDICATED THAT THE REU DETECTED A FORCE FIGHT BETWEEN ELEVATOR ACTUATORS, I.E., ELEVATOR ACTUATORS FORCING IN OPPOSITE DIRECTIONS ON THE SAME SURFACE
- [SDR SWIA2026071576654](https://openairdocs.org/sdr/SWIA2026071576654.md): Elevator System · faulted · Jul 15, 2026 · N707SK · Cndair CL6002C10
  > FLIGHT CREW REPORTS CO-PILOT TRIM QUIT WORKING AT APPROX 5000' AGL, RECEIVED AN ELEVATOR SPLIT MASTER WARNING. ENGAGED AUTOPILOT AC BEGAN PORPOSING, DISCONNECTED TO AP, DISCONNECTED THE ELEVATOR TRIM AND DECLARED AN EMERGENCY AND RETURNED TO THE CITY OF ORIGIN
- [SDR DALA2026071404142](https://openairdocs.org/sdr/DALA2026071404142.md): Dampener · faulted · Jul 13, 2026 · N986AT · Boeing 717200
  > ATB- PERFORMED AN AIR TURN BACK DUE TO SPLIT ELEVATOR INDICATION. REPLACED RT ELEVATOR DAMPER IAW AMM 27-31 OPS CHK GOOD. (8424292) (AIRCRAFT GROUNDED).
- [SDR AALA202606230799](https://openairdocs.org/sdr/AALA202606230799.md): Elevator · out of rig · Jun 21, 2026 · N567UW · Airbus A321231
  > AIRCRAFT WAS GROUNDED: ON TAKEOFF ROTATION AIRCRAFT HAD A SLIGHT RIGHT ROLL. CALM WINDS. ON CLIMB OUT AND CRUISE RUDER TRIM INDICATES.8 TO 1.1 LEFT. AROUND A ONE DEGREE LEFT BANK IN CRUISE. MAINTENANCE ACCOMPLISHED RIGGING OF THE ELEVATORS PER AMM 27-34-00-82
- [SDR AALA202606164984](https://openairdocs.org/sdr/AALA202606164984.md): Hinge Fitting · excess play · Jun 13, 2026 · N8031M · Airbus A319115
  > AIRCRAFT WAS GROUNDED: CLIMBING THROUGH APPROXIMATELY 25000' AT AROUND 315 KNOTS WE EXPERIENCED PRONOUNCED AIRFRAME VIBRATION. RH SIDE ELEVATOR FLUTTERWAS OBSERVED ON THE F/CTL PAGE. AFTER REDUCING THE SPEED, THE VIBRATION CEASED WHEN THE AIRCRAFT PITCHED UP A
- [SDR SWIA2026060976897](https://openairdocs.org/sdr/SWIA2026060976897.md): Hinge Fitting · corroded · Jun 9, 2026 · N936EV · Cndair CL6002B19
  > DURING REMOVAL OF BEARING ON LT ELEVATOR INBD HINGE FITTING, FOUND BEARING BORES TO BE CORRODED AND PITTED. REPLACED THE HINGE FITTING ASSY AT I/B ES16.52 ON LT ELEVATOR, IAW SRM 51-42-06, SRM 51-42-21 AND ELEVATOR ASSY DWG. 601R24025, REV. G. SKYCARD 51-90
- [SDR DALA2026060103329](https://openairdocs.org/sdr/DALA2026060103329.md): Pcu · faulted · May 30, 2026 · N390DA · Boeing 737832
  > DIVERTED TO MEM DUE TO ELEVATOR VIBRATION IN FLIGHT. REPLACED LT ELEVATOR PCU AND RT UPPER HORIZONTAL STABILIZER BLADE SEAL. OPS AND FREEPLAY TESTS GOOD. (LOG 8599376 - AIRCRAFT WAS GROUNDED).
- [SDR N6WA2026052602](https://openairdocs.org/sdr/N6WA2026052602.md): Spcc · faulted · May 26, 2026 · N552GJ · Cndair CL6002C11
  > STALL FAIL CAUTION MESSAGE (B1-007653 R AOA / RESOLVER 1/2 DISAGREE). R & R SPC IAW AMM 27-35-01. OPS GROUND TESTED GOOD IAW AMM 27-35-01-710-801.
- [SDR ABXA20260520218](https://openairdocs.org/sdr/ABXA20260520218.md): Elevator System · faulted · May 20, 2026 · N220CY · Boeing 767383
  > DURING FLIGHT CONTROL, RIGHT ELEVATOR STOPS HALF WAY BEFORE FULL TRAVEL. CREW RETURNED TO THE GATE (BTB). MTC VERIFIED ELEVATOR INDICATION. C/W MAINT. PROCEDURE 27-08-7, DEFERRED PER MEL 27-08-7. PLACARD INSTALLED AND MBCB 5/30/2026 REPETITIVE INSPECTION REQUI
- [SDR IPXA2026042797480](https://openairdocs.org/sdr/IPXA2026042797480.md): Elevator System · faulted · Apr 27, 2026 · N610UP · Boeing 7478F
  > ADD SDR FOR EO-85445-JIC2 FAULT APPROVED PER GMM-MTX 09.05.01.05. LH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. COMPLETE PER SB 747-55-2069. EO COMPLIED WITH.
- [SDR IPXA2026042797478](https://openairdocs.org/sdr/IPXA2026042797478.md): Elevator · not reported · Apr 27, 2026 · N610UP · Boeing 7478F
  > ADD SDR FOR EO-85445-JIC1 FAULT APPROVED PER GMM-MTX 09.05.01.05. LH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. COMPLETE PER SB 747-55-2069. EO COMPLIED WITH.
- [SDR FDEA202604160456](https://openairdocs.org/sdr/FDEA202604160456.md): Control Cable · out of adjust · Apr 16, 2026 · N968FD · Boeing 75728A
  > EXPERIENCED EXTREME UNCOMMANDED PITCH OSCILLATIONS ON CLIMB OUT BETWEEN 3 AND 4 THOUSAND FEET. OSCILLATIONS LASTED 10 TO 15 SECONDS. AIR CRAFT CLEAN CONFIGURATION ACCELERATING TO 250 KNOTS. ENGAGED CENTER AUTOPILOT AND OSCILLATIONS CEASED. MULTIPLE HAND F
- [SDR HNAA2026041200283](https://openairdocs.org/sdr/HNAA2026041200283.md): Switch · failed · Apr 12, 2026 · N683AE · Emb EMB145LR
  > MAIN PITCH TRIM INOP MESSAGE DURING CLIMB USING CAPT YOKE SWITCH. R&R PITCH TRIM SWITCH IAW EMBR AMM 27-40-03. PERFORMED HORIZONTAL STAB ADJUSTMENT TEST EMBR 145 AMM 27-40-00 TROUBLESHOOTED USING EMBR 145 FIM 27-43-00-810-801-A. NO DEFECTS NOTED, A/C GOOD FO
- [SDR CALA2026041315336](https://openairdocs.org/sdr/CALA2026041315336.md): Actuator · faulty · Apr 9, 2026 · N13110 · Boeing 757224
  > ELEV ASYM STATUS MESSAGE REPEAT FROM PREFLIGHT CHECKS (SCEPTRE TRACKING) WHILE T/S ELEVATOR ASYMMETRY FOUND SYMMETRY LIMITER ACTUATOR FAULTY. REMOVED AND REPLACED SYMMETRY LIMITER ACTUATOR AND PERFORMED TEST/OP CHECK REF B757 MM 27-31-03-024-001 ALL WORK ACCOM
- [SDR 2026FA0000249](https://openairdocs.org/sdr/2026FA0000249.md): Motor · defective · Apr 2, 2026 · N2143 · Cirrus SR20
  > ELEVATOR PITCH TRIM MOTOR BASE ATTACH SCREWS (4EA) LOOSE ON MOUNTING BRACKET. EXCESSIVE PLAY IN THIS AREA IS CAUSING EXCESSIVE PLAY IN THE FLIGHT CONTROL. COULD BECOME A FLIGHT CONTROL FLUTTER ISSUE THAT WILL AFFECT FLIGHT.
- [SDR N6WA2026032401](https://openairdocs.org/sdr/N6WA2026032401.md): Pcu · leaking · Mar 17, 2026 · N522GJ · Cndair CL6002C11
  > REPETITIVE PITCH VIBRATION AND FLUTTER ON CLIMBOUT AND AGAIN AT CRUISE AND REPEATED MULTIPLE TIMES DURING DIVERT AND AUTOPILOT WOULD NOT ENGAGE. PERFORMED GVI OF ALL PCU'S AND ELEVATORS. FOUND LH CENTER PCU LEAKING AND SQUEAKING WHILE BEING ACTUATED, ALSO FOU
- [SDR CALA2026031814648](https://openairdocs.org/sdr/CALA2026031814648.md): Computer · failed · Mar 17, 2026 · N17264 · Boeing 7378
  > ELEVATOR FEEL DIFFERENTIAL LIGHT ON BEFORE TAKE OFF. NO DIFFERENCE IN HYD PRESSURE. PERFORMED FIM 27-31 TASK 803, INITIAL EVALUATION, AND FAULT ISOLATION STEP D (1) OMF EXISTING FAULTS SHOWS NO RELATED MSG, FEEL DIFFERENTIAL LIGHT REMAINS ON. CHECKED ELEVAT
- [SDR 2026FA0000156](https://openairdocs.org/sdr/2026FA0000156.md): Flt Controls · not reported · Mar 4, 2026 · N225EL · Gulstm GULFSTREAMGV
  > DURING DEPARTURE FROM KTPA, THE FLT CREW EXPERIENCED A FLT CONTROL MALFUNCTION INVOLVING ELEVATOR SYS. FOLLOWING A RT ELEV HYD OFF CAS MESSAGE, ELEV BECAME LOCKED, REQUIRING DUAL-PILOT INPUT TO MAINTAIN AIRSPEED. CONTROL PARTIALLY RESTORED AT 12, 000 FT AFTER
- [SDR AALA202603041394](https://openairdocs.org/sdr/AALA202603041394.md): Actuator · leaking · Feb 17, 2026 · N313VA · Boeing 7378
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CAPTAIN SIDE CONTROL COLUMN ON TAKE OFF ROTATION WAS LOOSE APPROXIMATELY 3 TO 5 DEGREES AFT AND FORWARD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. FOUND FEEL ACTUATOR LEAKING IN AFT PA
- [SDR QXEA2026021600034](https://openairdocs.org/sdr/QXEA2026021600034.md): Dampener · malfunctioned · Feb 15, 2026 · N634QX · Emb ERJ170200LR
  > IN FLIGHT THE ELEVATOR FEELS STUTTERY ALMOST AS IF IT'S CATCHING ON SOMETHING AS IT MOVES. DURING TH FLIGHT CONTROL CHECK ON THE GROUND IT FELS NORMAL, BUT WHEN TH FO TOOK OFF HE FELT IT AS SOON AS ROTATION AND IT CONTINUED FOR THE ENTIRE FLIGHT. BOTH WITH AUT
- [SDR QXEA2026021600032](https://openairdocs.org/sdr/QXEA2026021600032.md): Dampener · leaking · Feb 12, 2026 · N647QX · Emb ERJ170200LR
  > FLIGHT 2014. ELEVATOR FELT STIFF IN FLIGHT. BOTH CA AND FO SIDE. NO NOTICEABLE "SNAP" OF CONTROL COLUMN UPON AP DISCONNECT. HYD PBIT WAS NORMAL AS WAS THE FLGIHT CONTROL CHECK. WAS NOT ABNORMALLY STIFF ON GROUND. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CHECK
- [SDR AALA202602093390](https://openairdocs.org/sdr/AALA202602093390.md): Computer · leaking · Feb 8, 2026 · N893NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FELT DIFFERENTIAL PRESSURE ON TAKEOFF PITCH PRESSURE WAS HIGH, THEN IN FLIGHT AUTOPILOT DISENGAGED TWICE FOLLOW WITH MASTER CAUTION COMING ON SEVERAL TIMES AND THE FLIGHT CONT ON SIX PACK. AIRCRAFT AIR I
- [SDR HNAA2026020900112](https://openairdocs.org/sdr/HNAA2026020900112.md): Computer · inoperative · Feb 8, 2026 · N692AE · Emb EMB145LR
  > SPS 1 INOPERATIVE ON TAKEOFF ABOVE 80 KNOTS. STALL PROTECTION COMPUTER FAIL MESSAGE ON CMC. FACT 08FEB26 19:41 CLT T/S IAW FIM 27-36-00-810-807-A FAILURE OF STALL PROTECTION COMPUTER. R+R STALL PROTECTION COMPUTER IAW AMM 27-36-00. OPS CHECK GOOD IAW AM
- [SDR HNAA2026020600111](https://openairdocs.org/sdr/HNAA2026020600111.md): Relay · faulted · Feb 5, 2026 · N692AE · Emb EMB145LR
  > SPS ADVANCE ON TAKEOFF STALL PROT TEST LIGHT REMAINED ON. R & R RELAY K0356 AND K0358 IAW AMM 20-13-02. RESEATED SPS CUTOUT 1-2 P/B IAW AMM 20-13-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE AT THIS TIME.
- [SDR 2026FA0000049](https://openairdocs.org/sdr/2026FA0000049.md): Bracket · dented · Jan 21, 2026 · N961LC · Cessna 172D
  > ELEVATOR STOP BOLT BRACKET COMPROMISED DUE TO EXCESSIVE FORCE / WIND DAMAGE, CAUSING THE LOWER ELEVATOR STOP BOLT TO BREAK THE NUT PLATE AND INDENT THE BRACKET REQUIRING REPLACEMENT. THIS FAILURE CAUSES THE AIRCRAFT ELEVATOR TO TRAVEL BEYOND THE ALLOWABLE LIMI
- [SDR AALA202601305490](https://openairdocs.org/sdr/AALA202601305490.md): Hinge Fitting · worn · Jan 20, 2026 · N903AA · Airbus A321231
  > AIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **ORIGINAL REPORT WAS AALA202601260827 SUBMITTTED 1/26/2026 BY TUL** MAINTENANCE REPLACED THE LEFT-HAND ELEVATOR
- [SDR AALA202601306265](https://openairdocs.org/sdr/AALA202601306265.md): Hinge Fitting · worn · Jan 20, 2026 · N903AA · Airbus A321231
  > AIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **ORIGINAL REPORT WAS AALA202601260827 SUBMITTTED 1/26/2026 BY TUL** MAINTENANCE REPLACED THE LEFT-HAND ELEVATOR
- [SDR VNAA2026011311101](https://openairdocs.org/sdr/VNAA2026011311101.md): Warning Message · false activation · Jan 10, 2026 · N514AE · Cndair CL6002C10
  > PITCH FEEL CAUTION MSG. / CYCLED SYSTEM CBS. MSG EXTINGUISHED. NO DEFECTS NOTED AT THIS TIME.
- [SDR ABXA20260107005](https://openairdocs.org/sdr/ABXA20260107005.md): Transmitter · defective · Jan 7, 2026 · N220CY · Boeing 767383
  > DURING TAXI OUT, RIGHT ELEVATOR INDICATOR IS NOT SHOWING FULL DEFLECTION DURING CONTROL CHECK. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED ELEVATOR INDICATION IN REF WITH MEL 27-08-1. REMOVED AND REPLACED RH ELEVATOR POSITION TRANSMITTER IAW B767 AMM 27-38-
- [SDR CALA2026010812808](https://openairdocs.org/sdr/CALA2026010812808.md): Computer · faulted · Jan 6, 2026 · N38446 · Boeing 737924ER
  > FEEL DIFF PRESS LIGHT LIGHT ON FEEL DIFF LIGHT ON INFLIGHT WHEN PITCH CHANGES LOCKED LP DUE TO HISTORY. UNLOCKED BY TOMC PERFORMED FIM 27-31 TASK 815. FROM "FAULT ISOLATION PROCEDURE C" (STEP H) TO H(4). ALL CHECKS PASS, NO LEAKS. DUE TO PREVIOUS WRITE UP THAT
- [SDR DXTA2026010806460](https://openairdocs.org/sdr/DXTA2026010806460.md): Electronic Unit · faulty · Jan 6, 2026 · N406QS · Emb EMB505
  > WHILE CLIMBING THROUGH FL340, RECEIVED PTRIM NML FAIL CAS MESSAGE. FOLLOWED QRH GUIDANCE. ACCOMPANIED WAS ALSO A GND SPLR FAIL MSG. CORRECTIVE ACTION: ARRIVED ONSITE, RECEIVED PART SHIPMENT AND GAINED ACCESS TO THE AIRCRAFT. REMOVED ACCESS PANELS AS REQUIRED T
- [SDR AALA202512093233](https://openairdocs.org/sdr/AALA202512093233.md): Computer · faulted · Dec 8, 2025 · N962AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: INTERMITTENT SPEED LIMITS FLAG ON BOTH PRIMARY FLIGHT DISPLAY AND ON HUD. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHL. REMOVED AND REPALCED PLUG D365 (AALA202512095799), PER SWPM 20-26-11. ALSO, REMOVE
- [SDR VNAA2025121611101](https://openairdocs.org/sdr/VNAA2025121611101.md): Dcu · faulted · Dec 7, 2025 · N504AE · Cndair CL6002C10
  > ELEVATOR SPLIT CAUTION MSG W/ CAS MISCOMP / INTERROGATED MDC DID NOT FIND B1. TS IAW CRJ 700 FIM 31ˆ’41ˆ’00ˆ’810ˆ’802 AND 27ˆ’31ˆ’00ˆ’810ˆ’803. PERFORMED OPS CHECK OF ELEVATOR IAW CRJ 700 AMM 27€“31€“00€“710€“801. REMOVED DCU 1 AND DCU 2 IAW CRJ 70
- [SDR N6WA2025112802](https://openairdocs.org/sdr/N6WA2025112802.md): Control Cable · frayed · Nov 25, 2025 · N564GJ · Cndair CL6002C11
  > ELEVATOR AUTO PILOT CONTROL CABLES FRAYED. REMOVED AND REPLACED ELEVATOR CONTROL CABLES IAW CRJ AMM 27-31-00.
- [SDR 2025FA0000788](https://openairdocs.org/sdr/2025FA0000788.md): Actuator · warning message · Nov 24, 2025 · N540LF · Gulstm GVI
  > EICAS MESSAGE NOTING RIGHT HAND ELEVATOR HYDRAULIC ACTUATOR FAILURE.
- [SDR DALA2025112508579](https://openairdocs.org/sdr/DALA2025112508579.md): Servo Control · excess play · Nov 24, 2025 · N354NB · Airbus A319114
  > EMPENNAGE LH ELEVATOR SERVO CONTROL GREEN HAS PLAY, IT HAS 7.20. REPLACED EMPENNAGE LH ELEVATOR SERVO CONTROL GREEN ACTUATOR EYE END IAW A319 AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319609).
- [SDR DALA2025112508578](https://openairdocs.org/sdr/DALA2025112508578.md): Servo Control · excess play · Nov 24, 2025 · N354NB · Airbus A319114
  > EMPENNAGE RH ELEVATOR SERVO CONTROL BLUE HAS PLAY, IT HAS 7.45. REPLACED EMPENNAGE RH ELEVATOR SERVO CONTROL BLUE ACTUATOR EYE END IAW A319 AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319605).
- [SDR DALA2025112508577](https://openairdocs.org/sdr/DALA2025112508577.md): Servo Control · excess play · Nov 24, 2025 · N354NB · Airbus A319114
  > EMPENNAGE RT ELEVATOR SERVO CONTROL YELLOW HAS PLAY, IT HAS 7.02. REPLACED EMPENNAGE RT ELEVATOR SERVO CONTROL YELLOW ACTUATOR EYE END IAW AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319595).

Next page: https://openairdocs.org/jasc/2730/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 = '2730'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/2730/reports

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