# N17753: 2002 Boeing 737-7V3

- Status: Valid registration
- Airframe: [Boeing 737-7V3](https://openairdocs.org/model/boeing-737-7v3) (registry code 13844D1, 149 seats)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 30463
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 15, 2015
- Certificate issued: July 19, 2022
- Expires: July 31, 2029
- Mode S code: A13651
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17753
- Page: https://openairdocs.org/aircraft/N17753

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B22 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7V3)

None in force.

### Matched by engine (CFM International CFM56-7B22 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N17753.

## FAA accident and incident reports

None matched to N17753.

## Service difficulty reports (66, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA2026081418640](https://openairdocs.org/sdr/CALA2026081418640), Aug 12, 2026: SLIDE. UNDAMAGED. L2 DOOR SHOWING EXCESS SLIDE MATERIAL. TUCKED AND SECURED THE EXCESS GIRT MATERIAL FOR DOOR SLIDE 2L. REF 25-66-01
- [SDR CALA2026050716051](https://openairdocs.org/sdr/CALA2026050716051), May 5, 2026: LIGHT. BROKEN. EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - ROW 10 AISLE EMERGENCY LIGHT FOUND BROKEN REPLACED AISLE EMERGENCY LIGHT. OPS CHECK GO
- [SDR CALA2026042915819](https://openairdocs.org/sdr/CALA2026042915819), Apr 28, 2026: BATTERY PACK. NO TEST. EMERGENCY LIGHT BATTERY PACK M1674 FAILED CAPACITY CHECK. REPLACED M1674 EMERG BATTERY, OPS CHK GOOD PER MM #33-51-06-960-805.
- [SDR CALA2026010712757](https://openairdocs.org/sdr/CALA2026010712757), Jan 5, 2026: ENGINE. FAULTED. ENG 2 LAGS BY 10 SECS WHEN SPOOLING TO 40 PCT N1. ABOVE 40PCT IT ACCELERATES NORMALLY INFO FROM FLIGHT CREW. ON DESCENT N1 WOULD NOT GO ABOVE 29%, T/O AND CRUIS
- [SDR CALA2025122412406](https://openairdocs.org/sdr/CALA2025122412406), Dec 21, 2025: CIRCUIT BREAKER. CRACKED. CAPTAIN`S PITOT FAULT LIGHT ILLUMINATED. INITIAL INSPECTION FOUND CIRCUIT BREAKER OPEN. AIR RETURN WHILE PERFORMING VISUAL INSPECTION OF THE HEATERS, CAPT PITOT
- [SDR CALA2025122412397](https://openairdocs.org/sdr/CALA2025122412397), Dec 21, 2025: PITOT TUBE. FAULTED. CAPT PITOT LIGHT ON, LIGHT WITH ASSOCIATED TRIPPED C/B. REMOVED AND REPLACED CAPT PITOT PROBE IAW AMM 34-11-01. OPS CHECKED GOOD. BREAKER REMAINS IN. REFER TO L
- [SDR CALA2025120411778](https://openairdocs.org/sdr/CALA2025120411778), Nov 30, 2025: TUBE. SHORT. ALERTING DUCT PRESSURE LOW FOR NR 1 ENG. ON DESCENT. PRESSURE CONSISTENT AT 8 PSI VS 35 PSI. DURING INSPECTION OF SENSE LINES AND FITTINGS, FOUND SHORT ELBOW SE
- [SDR CALA2025101309964](https://openairdocs.org/sdr/CALA2025101309964), Oct 10, 2025: GUARD. DAMAGED. AFT FA STATION EMERGENCY LIGHT ACTIVATION SWITCH COVER DAMAGED. REPLACED SWITCH GUARD REF IPC 33-51-01-56. OPS CHECK OF SWITCH AND GUARD GOOD. SDR FILED FOR EME
- [SDR CALA2025100209530](https://openairdocs.org/sdr/CALA2025100209530), Oct 2, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHTS NOT ARMED LIGHT, ONE LAMP INOP. RELAMPED AND OPS CHKD OK.
- [SDR CALA2025091909049](https://openairdocs.org/sdr/CALA2025091909049), Sep 17, 2025: STARTER GEN. FAULTED. APU DROPPED OFF LINE PUT THE GENERATORS OFF, BACK ON, THE APU BUSS STRONG SMOKE ODOR. R & R APU STARTER/GENERATOR IAW AMM TASK 49-41-21-400-801 UP TO STEP H,7. 
- [SDR CALA2025091809020](https://openairdocs.org/sdr/CALA2025091809020), Sep 16, 2025: HOUSING. BROKEN. ECONOMY PASSENGER SEAT EMERGENCY PATH LIGHTING INSPECTION. EPL HOUSING MOUNTING TABS BROKEN ROWS 21, 25. R & R EPL HOUSING AT ROW 25 IAW CMM 25-21-56. ROW 21 NE
- [SDR CALA2025081507829](https://openairdocs.org/sdr/CALA2025081507829), Aug 15, 2025: COVER. PULLED. FAS REPORT DOOR 2L SLIDE COVER HOUSING BOLT PULLING OUT. FOUND BOLT TO BE TIGHT AND SLIDEPACK SECURE. NO DEFECTS NOTED
- [SDR CALA2025072106771](https://openairdocs.org/sdr/CALA2025072106771), Jul 20, 2025: UNKNOWN. ODOR. APU DISCONNECTED ON ITS OWN. FOLLOWED BY BURNING SMELL IN CABIN COCKPIT PERFORMED INSPECTION PER AMM 05-51-26. NO DEFECTS NOTED. ALSO PERFORMED INSPECTION OF AP
- [SDR CALA2025053005135](https://openairdocs.org/sdr/CALA2025053005135), May 27, 2025: SENSOR. FAULTED. L FLAP TRANSIT LIGHT ON AT CRUISE.SLAT 2 AMBER QRH DID NOT CLEAR LWR TOCS LOG CREATED AND LOGPAGE LOCKED BY TOMC FOUND FAULT SL2 PROX OUTBOARD FAULT MX MESSAGE 
- [SDR CALA2024122301627](https://openairdocs.org/sdr/CALA2024122301627), Dec 20, 2024: APU. FAULTED. LOW OIL LIGHT APU SHUT DOWN ACCOMPLISHED APU BITE PROCEDURE, FOUND MAINT MESSAGE 49-91007. OIL LEVEL FULL. PERFORMED API OIL INSPECTION REF TASK 12-13-31-200-80
- [SDR CALA2024121201487](https://openairdocs.org/sdr/CALA2024121201487), Dec 10, 2024: POWER SUPPLY. FAULTED. AISLE EMERGENCY LIGHTS ROWS 29-34 AND AFT ENTRY CEILING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY M1672 AND BATTERY PACK IN AFT GALLEY OVERHEAD. ALL EMERGENCY
- [SDR CALA2024121001459](https://openairdocs.org/sdr/CALA2024121001459), Dec 6, 2024: SLIDE. OUT OF POSITION. DOOR 2R SLIDE EXCESS MATERIAL PROTRUDING FROM SLIDE CONTAINER. PERFORMED ESCAPE SLIDE RENDER SAFE CHECKLIST, REMOVED SLIDE PACK ASSY, RE-STOWED Z-FOLD, AND REIN
- [SDR CALA2024090602397](https://openairdocs.org/sdr/CALA2024090602397), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TA SK NSA EMX N/R 00097.
- [SDR CALA2024090602396](https://openairdocs.org/sdr/CALA2024090602396), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. SUPPORT T ASK NSA EMX N/R 00099.
- [SDR CALA2024090602395](https://openairdocs.org/sdr/CALA2024090602395), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. SUPPORT T ASK NSA EMX N/R 00102.
- [SDR CALA2024090602394](https://openairdocs.org/sdr/CALA2024090602394), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. SUPPORT T ASK NSA EMX N/R 00101.
- [SDR CALA2024090602393](https://openairdocs.org/sdr/CALA2024090602393), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED.SUPPORT TAS K NSA EMX N/R 00100.
- [SDR CALA2024090602392](https://openairdocs.org/sdr/CALA2024090602392), Aug 26, 2024: FITTING. CRACKED. SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. SUPPORT T ASK NSA EMX N/R 00098.
- [SDR CALA2024070101947](https://openairdocs.org/sdr/CALA2024070101947), Jun 28, 2024: INTERCOSTAL. DAMAGED. R-1 DOOR FWD INTERCOSTAL AT UPPER TORQUE BOX BEAM HAS OVERSIZED HOLE AT .3407" DIA. WITH AN E.D OF -38". P/N 141A6524-10. 25-JUNE-2025 PER ECRA 5210-03326 PART 
- [SDR CALA2024062601903](https://openairdocs.org/sdr/CALA2024062601903), Jun 20, 2024: SKIN. DAMAGED. FUSELAGE REPAIR AT BS 264-275 STR 4-6 LH REQUIRES A CATAGORY B REPAIR INSPECTION PER SRM 53-00-01-2R-3 REPAIR 3 TABLE 204. MAJOR REPAIR.
- [SDR CALA2024061801852](https://openairdocs.org/sdr/CALA2024061801852), Jun 12, 2024: PRESSURE DECK. CRACKED. SIGNS OF A SMALL CRACK ON PRESSURE DECK AT STATION 663.75 AT APPX RBL 35. THIS LOG PAGE IS FOR ESFR REPORTING PURPOSES ONLY. SEE NON-ROUTINE 1980186 FOR WORK PE
- [SDR CALA2024061801849](https://openairdocs.org/sdr/CALA2024061801849), Jun 12, 2024: PRESSURE DECK. CRACKED. SIGNS OF 1 EA. CRACK APPX 1IN LONG ON PRESSURE DECK AT STA 663.75 AT APPX LBL 35. WORK PERFORMED. 57-10-10-2R-3. REPAIRED VERTICAL PRESSURE DECK PER SRM 57-10-1
- [SDR CALA2023052901691](https://openairdocs.org/sdr/CALA2023052901691), May 27, 2023: TIRE. VIBRATION. REJECTED TAKE-OFF DUE EXTREME VIBRATION FROM NOSEWHEEL GEAR AT 1 10K. REPLACED BOTH NOSE TIRES.
- [SDR CALA2023020600342](https://openairdocs.org/sdr/CALA2023020600342), Feb 6, 2023: SWITCH. NOT REPORTED. LNDG GEAR WOULDNT RAISE QRH 3 TIMES GEAR CAME UP REPLACED MANUAL EXTENSION SYSTEM DOOR SWITCH.
- [SDR CALA2023012000167](https://openairdocs.org/sdr/CALA2023012000167), Jan 19, 2023: WINDOW. CRACKED. L2 OUTER PANE CRACKED IN FLIGHT REMOVED AND REPLACED L2 WINDOW PER AMM 56-21-11. WINDOW CONTROLLER STILL NEEDED WILL NOT RESET NIS CLE.
- [SDR CALA2022082902204](https://openairdocs.org/sdr/CALA2022082902204), Aug 29, 2022: NONE. MISSING. *THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 08/29/2022* PDA 2 LEFT PACK EXH DIFFUSER DOOR STOP (L-ANGLE) 
- [SDR CALA2022082902205](https://openairdocs.org/sdr/CALA2022082902205), Aug 28, 2022: DIFFUSER. NONE. REF LOG 9413668......THIS LOG CREATED TO FILE SDR REPORT FOR DIFFUSER MFG P/N 2215628 DAMAGED. REF IPC 21-51-03-06A.
- [SDR CALA2022041801011](https://openairdocs.org/sdr/CALA2022041801011), Apr 18, 2022: COMPUTER. INOPERATIVE. A/T LIMIT INDICATION SHOWS ON AUTOTHROTTLE THRUST MODE DISPLAY ADDED INFLIGHT FAULT 01 DISPLAYED ON CDU PERFORMED A/T BITE, CURRENT STATUS NO FAULTS. PERFORMED 
- [SDR CALA2021082301417](https://openairdocs.org/sdr/CALA2021082301417), Aug 23, 2021: SEAL. MISSING. PDA 3 AERODYNAMIC SEAL MISSING ON RIGHT WING AFT TRAILING EDGE FLAP JUST O/B OF #7 CANOE FAIRING. ADDED PHOTO. ADDED PHOTO. REQUEST CDL. REF CDL 575390 DISPATCH
- [SDR CALA2021073001215](https://openairdocs.org/sdr/CALA2021073001215), Jul 29, 2021: SKIN. CORRODED. FUSELAGE SKIN CORRODED AND BULGED AT LAVATORY BLOWER PORT. ADDED PIC. PERFORMED STEP ON SRM 53-70-01-2R-3 PARA 4 STEP A THRU D COMPLETED STEP 4. (E), (G), (H), 
- [SDR CALA2021071801118](https://openairdocs.org/sdr/CALA2021071801118), Jul 18, 2021: TRIM SYSTEM. LACK OF LUBE. PER FLIGHT CREW: HEAVY/DELAYED RESPONSE IN THE AILERONS AND RATCHETING NOISE HEARD DURING ALL ROLL INPUTS AFTER TAKEOFF. PITCH INPUTS WERE NORMAL. PERFORMED GEN
- [SDR CALA2021071601107](https://openairdocs.org/sdr/CALA2021071601107), Jul 15, 2021: SKIN. CRACKED. FOUR CRACKS FOUND AT LEFT STAB STA 147.90 LOWER SURFACE. CRACK NO.1, 9" FROM FRONT TO REAR; CRACK NO. 2, 17" (FRONT TO REAR). CRACK NO. 3, 25" (FRONT TO REAR). 
- [SDR CALA2021071201081](https://openairdocs.org/sdr/CALA2021071201081), Jul 12, 2021: SKIN. CRACKED. FOUR CRACKS FOUND AT LEFT STAB STA 147.90 LOWER SURFACE. CRACK NO.1, 9" FROM FRONT TO REAR; CRACK NO. 2, 17" (FRONT TO REAR). CRACK NO. 3, 25" (FRONT TO REAR). 
- [SDR CALA2018070301533](https://openairdocs.org/sdr/CALA2018070301533), Jun 15, 2018: WINDOW FRAME. DAMAGED. L1 WINDOW FRAME REPAIR ACCOMPLISHED DURING HEAVY MAINTENANCE (D1).
- [SDR CALA2018062101461](https://openairdocs.org/sdr/CALA2018062101461), Jun 11, 2018: SKIN. CRACKED. RIGHT HORIZONTAL STAB LOWER SKIN WAS CRACKED AT HSS 101.9, AND 29.12, FIVE INCHES AFT OF L/E. CRACK WAS .75. REMOVED DAMAGED AND INSTALLED EXTERNAL DOUBLER IAW 
- [SDR CALA2018062101459](https://openairdocs.org/sdr/CALA2018062101459), Jun 11, 2018: SKIN. CRACKED. RIGHT HORIZONTAL STAB LWR SKIN WAS CRACKED HSS 129.5 & 10.5 INCHES AFT OF L/E. THE CRACK WAS .375 INCH. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW SRM 55
- [SDR CALA2018062101451](https://openairdocs.org/sdr/CALA2018062101451), Jun 10, 2018: FRAME. CRACKED. FRAME AT STA BS 460 BETWEEN S-8L AND S-9L CRACKED. INTERIM REPAIR AS PER PART 1 OF ECRA 5311-01950.
- [SDR CALA2018060601432](https://openairdocs.org/sdr/CALA2018060601432), Jun 5, 2018: SKIN. CRACKED. LEFT HORIZONTAL STAB LOWER SKIN WAS CRACKED 1 INCH LONG AT STAB STATION 138.70 AND 17.625 INCHES AFT OF THE LE. . INSTALLED A REPAIR DOUBLER IAW SRM 55-10-01, R
- [SDR CALA2018060531370](https://openairdocs.org/sdr/CALA2018060531370), May 27, 2018: FRAME. CRACKED. THE FRAME WAS CRACKED AT BS 787, BETWEEN STRINGERS 8R TO 9R. REPAIRED THE FRAME IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018060531369](https://openairdocs.org/sdr/CALA2018060531369), May 27, 2018: FRAME. CRACKED. THE FRAME WAS CRACKED AT BS 747, BETWEEN STRINGERS 8R AND 9R. REPAIRED THE FRAME IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018060531368](https://openairdocs.org/sdr/CALA2018060531368), May 27, 2018: FRAME. CRACKED. THE FRAME WAS CRACKED AT BS 727D, BETWEEN STRINGERS 8R - 9R. REPAIRED THE FRAME IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018060531363](https://openairdocs.org/sdr/CALA2018060531363), May 25, 2018: FRAME. CRACKED. FRAME WAS CRACKED AT BS 597, BETWEEN STRINGERS 8R AND 9R. REPAIRED IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018060531362](https://openairdocs.org/sdr/CALA2018060531362), May 25, 2018: FRAME. CRACKED. CABIN FRAME CRACKED AT BS 400, BETWEEN STRINGERS 8R AND 9R. REPAIRED IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018060531350](https://openairdocs.org/sdr/CALA2018060531350), May 22, 2018: FRAME. CRACKED. FRAME CRACKED AT BS 827 BETWEEN STRINGERS 8L - 9L. REPAIRED IAW EA 5310-04716, REV I, OP 1.
- [SDR CALA2018053101343](https://openairdocs.org/sdr/CALA2018053101343), May 21, 2018: FRAME. CRACKED. FRAME CRACKED AT BS 440, BETWEEN STRINGERS 8R AND 9R. REPAIRED THE FRAME IAW EA 5310-04716, REV I, OP 1.

All 66: https://openairdocs.org/aircraft/N17753/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56-7B22 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Earlier aircraft with N17753

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17753 before.

- [Cancelled 1994-11-17](https://openairdocs.org/deregistered/N17753-1994-11-17): Beech A36, S/N E1018. Exported to Brazil. Owner: [American Fox Trading Inc](https://openairdocs.org/faa-owner/AMERICAN%20FOX%20TRADING%20INC), [Oakland Park, FL](https://openairdocs.org/faa-place/FL/Oakland%20Park)
- [Cancelled 1948-04-27](https://openairdocs.org/deregistered/N17753-1948-04-27): Aeronca K, S/N K-19, built 1937. Owner: [Syrek Anna](https://openairdocs.org/faa-owner/SYREK%20ANNA), [Rochelle Park, NJ](https://openairdocs.org/faa-place/NJ/Rochelle%20Park)

## Related

- Other Boeing 737-7V3 aircraft: https://openairdocs.org/model/boeing-737-7v3/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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