# Service difficulty reports: JASC 2700 A list on [JASC 2700](https://openairdocs.org/jasc/2700.md). Reports filed under 2700 · Flight Control System, newest first. Page 1 of 35 · 1,742 reports - [SDR YENA2026101200942](https://openairdocs.org/sdr/YENA2026101200942.md): Control Servo · malfunctioned · Oct 10, 2026 · N508JL · Airbus A320232 > FLT#789, DTW-FLL. DURING CLIMB NOTICED A SMALL AMOUNT OF FWD STICK ABOUT 1/4" REQUIRED TO FOLLOW FLIGHT DIRECTORS(NOSE WANTED TO PITCH UP) CONTINUED FOR 30 MINS AFTER TOC & WENT AWAY UNTIL DESCENT, RETURNED & WAS PRESENT FOR DURATION OF FLT. ACFT COMPLETELY CO - [SDR 2026FA0000824](https://openairdocs.org/sdr/2026FA0000824.md): Trim Tab · faulted · Oct 8, 2026 · N814SS · Dhav DHC6 > AILERON TRIM INDICATION, AILERON TRIM TAB POSITION INDICATION. INTERMITTENT ERRATIC FLICKERING OF THE AILERON TRIM INDICATION. SYMPTOM APPEARS RANDOMLY, UNRELATED TO TRIM POSITION OR FLIGHT PHASE, AND HAS PERSISTED ACROSS MULTIPLE COMPONENT REPLACEMENTS. A - [SDR VQMA20261008001](https://openairdocs.org/sdr/VQMA20261008001.md): Actuator · lack of lube · Oct 5, 2026 · N616RR · Gulstm GIV > ELEVATOR TRIM FROZE UP DURING CLIMB OUT, FREED WHEN DESCENDING BELOW FREEZING LEVEL. REMOVED LT & RT ELEVATOR TRIM TAB ACTUATOR ACCESS PANELS AND PERFORMED A DETAILED VISUAL INSPECTION OF THE TRIM TAB ACTUATORS AND ASSOCIATED CABLES. PORTIONS OF THE EXISTING - [SDR DALA2026100605512](https://openairdocs.org/sdr/DALA2026100605512.md): Computer · faulted · Oct 5, 2026 · N817NW · Airbus A330323 > ATO - DUE TO "F/CTL PRIM 1 PITCH FAULT". SWAPPED FCPC1 AND FCPC3 AND PLACED FCPC3 ON MEL THEN REPLACED SERVO VALVE. OK FOR SERVICE. (8991859) - [SDR 2026FA0000813](https://openairdocs.org/sdr/2026FA0000813.md): Arm · backed out · Oct 5, 2026 · N7220N · Cessna 182P > NOTED UNUSUAL FEEL IN ELEVATOR CONTROL DURING INSP. PROBLEM DETERMINED TO BE A HEAVY RUB OF THE TORQUE TUBE USED BY THE PITCH SERVO AND THE LOWER ELEVATOR PRIMARY CONTROL CABLE. THE PITCH SERVO CONTROL ARM WAS FOUND TO HAVE ALL FOUR SCREWS THAT SECURE IT TO TH - [SDR 4T1R00002](https://openairdocs.org/sdr/4T1R00002.md): Spigot · corroded · Oct 2, 2026 · N925G · Bombdr BD7001A10 > DURING THE BORESCOPE INSPECTION OF THE INBOARD FLAP INTERNAL STRUCTURE PER AMM 57-51-00-290-801, STEP F.(3), CORROSION WAS IDENTIFIED INSIDE THE AFT SPIGOT TUBE INNER BORE ON THE RIGHT-HAND INBD. FLAP. REFERENCE BOMBARDIER REPAIR ENGINEERING ORDER 700-57-51-53 - [SDR 2026FA0000804](https://openairdocs.org/sdr/2026FA0000804.md): Flt Controls · corroded · Oct 1, 2026 · N37CL · Cirrus SR22T > ALL FLIGHT CONTROLS BORESCOPED. ALL FLIGHT CONTROLS EXHIBIT CORRISION THROUGHOUT, FLAPS, AILERON, & RUDDER. CORROSION FOUND THROUGHOUT ALONG THE SEAM LINES FROM INADEQUATE SURFACE PREP AND THROUGHOUT THE FLIGHT CONTROL STRUCTURE AND RIVET JOININGS. EXAMINED A - [SDR J7SA2026100200526](https://openairdocs.org/sdr/J7SA2026100200526.md): Fce · unserviceable · Sep 28, 2026 · N308FX · Emb EMB505 > REPEAT FLAP FAIL. REPLACED FCE #1 IAW EMB 505 AMM 27-03-01. OPS AND RIGGING CHECK GOOD. - [SDR DALA2026092705364](https://openairdocs.org/sdr/DALA2026092705364.md): Computer · malfunctioned · Sep 26, 2026 · N353NW · Airbus A320212 > DURING DECENT FOR APPROACH, WITH SPEED BRAKES DEPLOYED. AIRCRAFT MADE AN UNCOMMANDED RIGHT ROLL WITH NOTICEABLE BANK. T/S IAW TSM 27-10-00-810-842A, PERFORMED OPS TEST OF BOTH ELACS 1 & 2. TESTED OK. PERFORMED ELAC TEST IAW AMM 27-93-00-710-001-A. PERFORMED - [SDR DALA2026092805368](https://openairdocs.org/sdr/DALA2026092805368.md): Computer · faulty · Sep 25, 2026 · N352NW · Airbus A320212 > ON THE ARRIVAL TO DTW, THE ACFT HAD A NOSE DOWN PITCH. THE ECAM FOR FLT CONTROL ELAC 2 PITCH FAULT COMPLIED WITH ECAM & QRH. IAW AMM 27 93 34, TSM 27-93-00 810 867 710-001, REPLACED ELAC 2. OPS TESTED GOOD. PERFORMED EFCS AND SIDESTICK TESTING, NO FAULTS. A - [SDR J7SA2026092900524](https://openairdocs.org/sdr/J7SA2026092900524.md): Fce · malfunctioned · Sep 22, 2026 · N355FX · Emb EMB505 > CREW REPORTS FCE1 CB POPS WITH BATTERIES ON. REPLACED FCE # 1 IAW EMB-505 CH 27-03-01. OPS CHECK GOOD. - [SDR IPXA2026092379070](https://openairdocs.org/sdr/IPXA2026092379070.md): Accelerometer · oscillates · Sep 22, 2026 · N314UP · Boeing 76734AF > DURING CLIMB EXPERIENCED NOTICABLE OSCILLATIONS COMING FROM THE TAIL THAT DISSIPATED AT CRUISE. ALL ENG INDICATIONS NORMAL VERTICAL STABILIZER ACCESS PANELS AND RH ELEVATOR PCU PANLES CLOSED IAW AMM 27-31-05 REV149. FOUND FAULT DURING YAW DAMPER SYSTEM BITE PR - [SDR J7SA2026092900523](https://openairdocs.org/sdr/J7SA2026092900523.md): Fce · malfunctioned · Sep 12, 2026 · N391FX · Emb EMB505 > CREW RECEIVED GND SPOILER FAIL ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT CRE. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. OPS CHECKS GOOD. - [SDR J7SA2026092900522](https://openairdocs.org/sdr/J7SA2026092900522.md): Fce · unserviceable · Sep 11, 2026 · N375FX · Emb EMB505 > AFTER ENGINE START "SWPS FAULT", "GND SPLR FAIL", "PTRIM NML FAIL", "SPOILER FAULT" CAS MESSAGES ILLUMINATED. CAS MESSAGES WOULD NOT CLEAR AFTER SHUTDOWN AND POWER RESETS. REPLACED # 2 FCE IAW EMB-505 300 AMM 27-03-01. - [SDR ASAA2026091066874](https://openairdocs.org/sdr/ASAA2026091066874.md): Flt Controls · faulted · Sep 10, 2026 · N489HA · Boeing 717200 > AIRCRAFT HAD HARD ROLL TO THE RIGHT, 10 DEGREES AT GEAR EXTENSION, FLAPS 18 UNIT, 170KTS 2100FT. ASA1074 HNL LDG RWY 26L ON AS1074 ON 9/9/2026. GROUNDED - YES. COMPLIED WITH TSI-000725, ALL ITEMS HAD BEEN COMPLETED AND SUBMITTED. THE SIGNIFICANT EVENT RESPONS - [SDR J7SA2026090300519](https://openairdocs.org/sdr/J7SA2026090300519.md): Fce · faulted · Aug 31, 2026 · N333FX · Emb EMB505 > CREW RECEIVED SPOILER FAIL AND GND SPOILER FAIL CAS UPON TOUCHDOWN. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS TESTED GOOD. - [SDR ASAA2026082966644](https://openairdocs.org/sdr/ASAA2026082966644.md): Flt Controls · faulted · Aug 29, 2026 · N489HA · Boeing 717200 > UNCONTROLLED ROLL ON SHORT FINAL. REPEAT WRITE UP, FLAPS 40, VAPP 143, 400 FEET, AUTOPILOT/AUTO THROTTLES OFF. GROUNDED - YES. COMPLIED WITH TSI-00723 ITEM 1, ALL ITEMS HAD BEEN COMPLETED AND SUBMITTED. THE SIGNIFICANT EVENT RESPONSE PROCESS HAS BEEN COMPLETE - [SDR J7SA2026090100514](https://openairdocs.org/sdr/J7SA2026090100514.md): Fce · faulted · Aug 25, 2026 · N331FX · Emb EMB505 > FLAP FAIL CAS ILLUMINATED AFTER MOVING FLAP LEVER TO NR 1 POSITION. REPLACED FCE NR 1 IAW AMM 27-03-01. REPLACED FLAP SELECTED LEVER AND FLAP POWER DRIVE UNIT IAW AMM 27-53-01 AND 27-51-07. COMPLIED WITH FLAP RIGGING IAW 27-50-00. OPS CHECKS GOOD. - [SDR J7SA2026090100515](https://openairdocs.org/sdr/J7SA2026090100515.md): Fce · faulted · Aug 13, 2026 · N233FX · Emb EMB505 > CONTINUOUS FLAP FAIL UPON BATTERY POWER UP. REPLACED FCE # 1 IAW EMB 505 AMM 27-03-01. - [SDR AALA202608145189](https://openairdocs.org/sdr/AALA202608145189.md): Computer · defective · Aug 12, 2026 · N556UW · Airbus A321231 > AIRCRAFT WAS GROUNDED: THE FLT CREW REPORTED THAT THE ACFT DID NOT TRIM ITSELF PROPERLY DURING PREVIOUS TWO FLTS, BOTH CAPTAIN AND FIRST OFFICER EXPERIENCED UNUSUAL PITCH UP TENDENCIES DURING CLIMB OUT & APPROACH TO LANDING WHILE HAND FLYING ACFT. FLT CREW - [SDR J7SA2026081700512](https://openairdocs.org/sdr/J7SA2026081700512.md): Fce · faulted · Aug 7, 2026 · N382FX · Emb EMB505 > CREW REPORTS FCE2 CIRCUIT BREAKER POPS UPON POWERING ON AIRCRAFT. REPLACED FCE 2 WITH IAW AMM 27-05-01. SPOILER RIG AND OPS TEST SATISFACTORY IAW 27-60-00. - [SDR CALA2026080418250](https://openairdocs.org/sdr/CALA2026080418250.md): Control Unit · faulted · Aug 5, 2026 · N28912 · Boeing 7878 > STABILIZER R2 ADVISORY THIS MESSAGE IS SET WHEN THE R2 CONTROL CHANNEL NOT AVAILABLE FOR TRIM OR WHEN 1ST OFFICER'S TRIM SWITCH HAS BEEN DISAB LED BY COLUMN CUTOUT. R2 REFERS TO ELECTRICAL BUS. DB 27 FCM OPS (RIGHT) DB 27 FCM OPS (CENTER) DB 27 FCM OPS (LT) DE - [SDR HNAA2026080400645](https://openairdocs.org/sdr/HNAA2026080400645.md): Elect Module · faulted · Aug 3, 2026 · N663AR · Emb EMB145LR > ON TAKE OFF ROLL AT V1 FLIGHT CONTROL DID NOT RESPOND TO YOKE MOVEMENT. C/W HORIZONTAL STABILIZER ELECTRICAL/ELECTRONIC OPS CHECK IAW AMM 27-40-00-700-802-A. C/W AURAL WARNING OPS CHECK IAW AMM TASK 31-51-00-700-801-A. C/W ELEVATOR CONTROL CABLE TENSION CHECK - [SDR SIMA20260727001](https://openairdocs.org/sdr/SIMA20260727001.md): Mau · failed · Jul 27, 2026 · N291NN · Emb ERJ170200LR > AVNX MAU 1B FAIL IN FLIGHT. ASSOCIATED MESSAGES SPOILER FAULT AND SPDBRK FAIL. EMERGENCY DECLARED. PERFORM POWER DOWN POWER UP RESET PER QRH 7.2.1 AND 7.2.2. MESSAGE EXTINGUISH A/C OK FOR SERVICE. AND PERFORM QRH 7.3.22 AND AMM 27-00-00. OPS CHECK GOOD - [SDR DXTA2026072709024](https://openairdocs.org/sdr/DXTA2026072709024.md): Trim System · failed · Jul 25, 2026 · N244QS · Cndair CL6002B16 > AT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR. - [SDR DXTA2026072708997](https://openairdocs.org/sdr/DXTA2026072708997.md): Warning Message · illuminated · Jul 25, 2026 · N244QS · Cndair CL6002B16 > AT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR. - [SDR J7SA2026080400507](https://openairdocs.org/sdr/J7SA2026080400507.md): Fce · faulted · Jul 22, 2026 · N368FX · Emb EMB505 > P-TRIM NML FAIL DURING TRIM TESTS. REPLACED FCE 2 AND PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW EMB 505 AMM 27-03-01 AND 27-60-00. - [SDR J7SA2026080400508](https://openairdocs.org/sdr/J7SA2026080400508.md): Fce · faulted · Jul 21, 2026 · N341FX · Emb EMB505 > ON SHORT FINAL TO LAND, CREW RECEIVED AUTO PTRIM FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT CAS. AIRCRAFT LANDED WITHOUT INCIDENT AT KTRI. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKED GOOD. - [SDR FDEA202607170941](https://openairdocs.org/sdr/FDEA202607170941.md): Fcu · failed · Jul 17, 2026 · N656FE · Airbus A300F4605R > DURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04 - [SDR YENA2026071700583](https://openairdocs.org/sdr/YENA2026071700583.md): Fcu · failed · Jul 16, 2026 · N4073J · Airbus A321271NX > FLT 1408, CDG-JFK. (ETOPS) SPD/MARH BUTTON MISSING. R & R FCU (2CA) IAW AMM 22-81-12. OPS CHECK OK. CAT III LAND TEST REQUIRED. - [SDR J7SA2026072200487](https://openairdocs.org/sdr/J7SA2026072200487.md): Flt Controls · multiple fail · Jul 13, 2026 · N359FX · Emb EMB505 > DIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01. - [SDR J7SA2026080400509](https://openairdocs.org/sdr/J7SA2026080400509.md): Fce · faulted · Jul 1, 2026 · N352FX · Emb EMB505 > DESCENDING THROUGH FL340 RECEIVED GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT. CREW RAN QRH AND LANDED WITHOUT INCIDENT. REPLACED FCE #2. ALL OPS CHECKS GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01. - [SDR DALA2026062403743](https://openairdocs.org/sdr/DALA2026062403743.md): Secu · faulted · Jun 24, 2026 · N336NB · Airbus A319114 > DIV TO BOS DUE TO F/CTL SEC 3 FAULT. REPLACED SEC 3 AND RELAY 41CE3. (LP: 8320072, AIRCRAFT WAS GROUNDED) - [SDR DALA2026062203695](https://openairdocs.org/sdr/DALA2026062203695.md): Control Stick · faulted · Jun 22, 2026 · N851NW · Airbus A330223 > ATO - DUE TO PRIM 1 FAULT AT TAKE-OFF. REPLACED CAPTAINS AND F/O SIDESTICKS. (8318232) AIRCRAFT WAS GROUNDED. - [SDR DALA2026061503564](https://openairdocs.org/sdr/DALA2026061503564.md): Computer · faulted · Jun 13, 2026 · N353NB · Airbus A319114 > BOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED) - [SDR DALA2026061203551](https://openairdocs.org/sdr/DALA2026061203551.md): Memory Device · shorted · Jun 10, 2026 · N890DN · Boeing 737932ER > DURING PREFLIGHT IN CVG THE F/O THUMBWHEEL ON LEFT SIDE OF YOKE BEGAN TO SMOKE FOR APPROX 30 SECONDS. FOUND F/O CONTROL WHEEL MEMORY DEVICE INTERNAL SHORT. RPLD MEMORY DEVICE PER B737 AMM 33-11. OP CKS GOOD. NO EVIDENCE OF SMOKE. (LOG 8327226 - AIRCRAFT WAS GR - [SDR VNAA2026051117801](https://openairdocs.org/sdr/VNAA2026051117801.md): Pcu · faulted · May 4, 2026 · N637NN · Cndair CL6002D24 > IB SPOILERONS / IB FLT SPLRS CAUTION IN FLIGHT. REMOVED & REPLACED LH IB MULTI-FUNCTION SPOILER PCU(MPE33) IAW AMM 27-62-01-000/400-801-A02, PERFORMED BLEEDING OF HYD SYSTEM #1 IAW AMM 29-10-00-870-801-A01, LEAK TEST OF THE MULTI-FUNCTION SPOILER DONE IAW - [SDR DALA2026050102766](https://openairdocs.org/sdr/DALA2026050102766.md): Computer · faulted · Apr 30, 2026 · N353NB · Airbus A319114 > ATO - AT APPROXIMATELY 10KTS DUE TO F/CTL ELAC 1 PITCH FAULT. ELAC 1 PLACED ON MEL AND CONTINUED. LATER REPLACED ELAC 1. (LP 8038066 - AIRCRAFT WAS GROUNDED) - [SDR 2026FA0000310](https://openairdocs.org/sdr/2026FA0000310.md): Torque Tube · excess play · Apr 28, 2026 · N408TL · Textrn 408 > PERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RE - [SDR IPXA2026050990937](https://openairdocs.org/sdr/IPXA2026050990937.md): Torque Box · damaged · Apr 26, 2026 · N440UP · Boeing 75724APF > THE R/H LWR FWD TORQUE BOX PANEL HAS A DELAMINATED / DISBONDED AREA (1EA) NEAR THE BOTTOM OF THE PANEL. ALL DAMAGE MARKED IN RED.ACCOMPLISH REPAIR IAW SRM REV 124 CHAPTER 51-70-10-2R-2, SRM 51-70-10-2R-0 REPAIR GENERAL PER SRM 55-30-01-2R-5 TO ACCOMPLISH REPA - [SDR DALA2026042002475](https://openairdocs.org/sdr/DALA2026042002475.md): Unknown · unknown · Apr 20, 2026 · N343NB · Airbus A319114 > ATB - DUE TO AIRCRAFT PITCHING UP WITH A/P OFF. REPLACED ACCELEROMETER UNIT 12CE4, THS ZERO ADJUSTMENT CHECK, AND ELEVATOR FREE PLAY CHECK. NTF, AND ALL OPS CHECK GOOD. (LP: 7729382). AIRCRAFT WAS GROUNDED. - [SDR DALA2026041602405](https://openairdocs.org/sdr/DALA2026041602405.md): Computer · faulty · Apr 14, 2026 · N355NB · Airbus A319114 > ATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. ENG 1 G HYD MON C/B WAS FOUND POPPED. REPLACED ELAC 2. - [SDR QXEA2026041500087](https://openairdocs.org/sdr/QXEA2026041500087.md): Pace · malfunctioned · Apr 14, 2026 · N647QX · Emb ERJ170200LR > URING CRUISE AT FL370, GOT AN AMBER ELEVATOR FAULT. RAN CHKLIST IN QRH. ON PUSHING FCM ELEVATORS BUTTON IN AND OUT, THE MESSAGE WENT AWAY. UPON LANDING, WE GOT FLT CTRL NO DISPATCH. AFTER PARKING, GOT ANOTHER ELEVATOR FAULT, WHICH WENT AWAY ON ITS OWN AFTER AB - [SDR 2026FA0000308](https://openairdocs.org/sdr/2026FA0000308.md): Control Cable · twisted · Apr 13, 2026 · N389T · Cessna T206H > DURING THE REPLACEMENT OF THE PITCH TRIM ACTUATOR, WE ENCOUNTERED DIFFICULTY RIGGING AND PERFORMING THE OPERATIONAL CHECK OF THE ACTUATOR. UPON FURTHER INSPECTION, THE TECHNICIAN FOUND THAT THE ELECTRIC TRIM AND MANUAL TRIM CABLES WERE INTERTWINED INBOARD OF - [SDR CALA2026041415351](https://openairdocs.org/sdr/CALA2026041415351.md): Module · faulted · Apr 12, 2026 · N24980 · Boeing 7879 > SLAT DRIVE FAIL EICAS MESSAGE CHRONIC ISSUE, PERFORMED WIRE CHECK FROM CONNECTOR DE2702003P03B PIN 26,27 & 28 TO DM2789061P01 4,5,3 ON SLAT SKEW SENSOR. WIRE CHECK GOOD. CHECKED WIRE FROM ACE PIN F16 AND F15 ALSO CHECKS GOOD. SLAT SKEW SENSOR & ACE NEED TO - [SDR JJBA20260413010](https://openairdocs.org/sdr/JJBA20260413010.md): Control Unit · inoperative · Apr 11, 2026 · N24128 · Emb EMB145XR > DURING INITIAL CLIMBOUT, PITCH TRIM BACK UP INOPERATIVE AND PITCH TRIM MAIN INOPERATIVE. REMOVED AND REPLACED HSCU. REMOVED AND REPLACED FO'S YOKE TRIM SWITCH. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. - [SDR DALA2026040902256](https://openairdocs.org/sdr/DALA2026040902256.md): Computer · faulty · Apr 7, 2026 · N355NB · Airbus A319114 > ATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. REPLACED ELAC 2. (LP: 8410558) AIRCRAFT WAS GROUNDED - [SDR CALA2026041315324](https://openairdocs.org/sdr/CALA2026041315324.md): Unknown · oscillates · Apr 4, 2026 · N68805 · Boeing 737924ER > SMALL PITCH OCCILATIONS DURING CLIMBOUT. PRONOUN CED BELOW FL210. NOT FEL T THROUGH FLT CONTROLS FLT CREW STATES AIRCRAFT PORPOISING OCCURRED THROUGH ALL PHASES OF FLIGHT WITH NO AUTOPILOT ENGAGED, BUT WAS MOST NOTICEABLE IN CLIMB CONFIGURATION AND BECAME MOR - [SDR CALA2026033014895](https://openairdocs.org/sdr/CALA2026033014895.md): Control Unit · damaged · Mar 24, 2026 · N27213 · Boeing 737824 > ON TAKEOFF, AIRCAFT REQUI RED 5-6 UNITS LT AILERON TO MAINTAIN LE VEL FLIGHT INSPECTED AILERON CABLES ABSB AT B SYSTEM DRUM ASSY. FOUND SHEAR RIVETS SHEARED ON ABSB DRUM. EMERGENCY DECLARED. AILERON POWER CONTROL UNIT REMOVAL AND INSTALATION COMPLETED. ALL O - [SDR R61A2026031100060](https://openairdocs.org/sdr/R61A2026031100060.md): Torque Tube · faulted · Mar 11, 2026 · N638RW · Emb ERJ170100SE > FLAP FAIL EICAS MSG ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TRANSITORY CONDITION OF FLAP CONTROL SYSTEM. INSTALLED CORBAN, TORQUED, AND COTTER PINNED LT TORQUE TUBE BOLTS. Next page: https://openairdocs.org/jasc/2700/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 = '2700' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/jasc/2700/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.